N427PG STATUS REPORT BELL HELICOPTER TEXTRON

BELL 427 · Maintenance Manual

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Overview

This document is a status report for the Bell 427 helicopter, detailing maintenance inspections, component conditions, and scheduled tasks. It includes information on flight hours, landing counts, and various inspections required for compliance and safety.

Owner/Operator: Helicopter Flight Services, Inc.
Total airframe hours: 2,093.8
Total landings: 4,368
Engines: 2 PW207D with varying hours and cycles.
Cost of maintenance: 19,348.05+
Next scheduled inspections include 50-hour and 150-hour checks.
Conditional inspections are required after specific incidents.
Annual first aid kit inspection due by 23-Aug-2024.

Document

Source

Originally published by helitrader.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at helitrader.com

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Document details

Type: Maintenance Manual
Year: 2023
File size: 1.1 MB
Publisher: helitrader.com
Language: en

Specifications & performance

Extracted from this document.

Specifications

Airframe hours: 2093.8 Hrs
Total landings: 4368 Ldg

Performance

Next inspection due: 22-Nov-2023

Weight & balance

Cg limits: N/A
Total weight: N/A

About this document

What is the N427PG STATUS REPORT BELL HELICOPTER TEXTRON?

The N427PG STATUS REPORT BELL HELICOPTER TEXTRON is a maintenance manual for the BELL 427, dated 2023.

Where does the N427PG STATUS REPORT BELL HELICOPTER TEXTRON come from?

This copy of the N427PG STATUS REPORT BELL HELICOPTER TEXTRON was originally published by helitrader.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the N427PG STATUS REPORT BELL HELICOPTER TEXTRON published?

The N427PG STATUS REPORT BELL HELICOPTER TEXTRON — the BELL 427 maintenance manual on file — is dated 2023.

Documentation completeness

2/7

Most owners only have the POH. Here's the essential set for the BELL 427.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins on file
Type Certificate (TCDS)

More BELL 427manuals & documents

In this document

General Information

The report provides an overview of the helicopter's status, including hours flown and landing counts.

Aircraft Stats / Limitations

Details on required inspections and their due dates, including visual inspections for cracks and delamination.

Time Limits / Maintenance Checks

Outlines periodic inspections and their schedules, including 50-hour, 150-hour, and 600-hour checks.

Conditional Inspections

Lists inspections required after specific events such as hard landings or sudden stoppages.

Leveling and Weighing

Includes details on the aircraft's weight and the next weighing due date.

Parking, Mooring, Storage

Instructions for examining loose equipment and ensuring proper storage conditions.

Safety notes

Inspect for evidence of cracking or delamination.
Conditional inspections required after hard landings.
Inspect for sudden stoppage of the tail rotor.
Main rotor overspeed incidents require inspection.
Inspect after lightning strikes for potential damage.

Full document text

N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner: Helicopter Flight Services, Inc Operator: Airframe Bell 427 56019 15-Nov-2023 2,093.8 Hrs 4,368 Ldg 0 RIN(Ldg) 4,368 RIN(2) 4,368 RIN(3) Eng 1 PW207D PCE-BF0037 15-Nov-2023 2,093.8 Hrs 2,880 Enc 467 IMPCYC 1,919 CTCYC 2,666 PTCYC Eng 2 PW207D PCE-BF0036 15-Nov-2023 2,040.9 Hrs 2,748 Enc 1,196 IMPCYC 1,739 CTCYC 2,547 PTCYC Program Type: Periodic Inspection, General Categories: FAA,FAR 135 Cost: 19,348.05+ Man Hrs: 591.9+ Analyst: Jim Coates jcoates@traxxall.com Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ▼ 0 - GENERAL 25-CUS-002 Annual First Aid Kit Inspection RE 0 A/F Mos 23-Aug-2023 12 23-Aug-2024 8.2 Months Hrs 2,061.6 Ldg 4,224 ▼ 4 - AIRCRAFT STATS / LIMITATIONS 5-15-016 Perform a detailed visual inspection for evidence of cracking or delamination on the inside and outside edges of the flexures. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 4 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg ▼ 5 - TIME LIMITS/MAINTENANCE CHECKS 5-15 50 Hour Inspection - Periodic RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 5 A/F (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +1m 02-May-2024 4.5 Months (+31 Days) Hrs 2,051.3 50 +5 2,101.3 7.5 Hrs (+5) Ldg 5-15-001 Review helicopter log book and ensure all recorded discrepancies have been corrected. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 5 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-16 150 Hour Inspection - Periodic RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 5 A/F (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +1m 02-May-2024 4.5 Months (+31 Days) Hrs 2,051.3 150 +15 2,201.3 107.5 Hrs (+15) Ldg 5-16A 300 Hour Inspection - Periodic RE 5-00-00, Scheduled Inspections 5 A/F (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +1m 02-May-2024 4.5 Months (+31 Days) Hrs 2,051.3 300 +30 2,351.3 257.5 Hrs (+30) Ldg 5-17 600 Hour / Annual Inspection - Periodic RE 5-00-00, Scheduled Inspections 5 A/F (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +1m 03-May-2024 4.5 Months (+31 Days) Hrs 2,051.3 600 +60 2,651.3 557.5 Hrs (+60) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 1/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-32 25 Hour Scheduled Component Inspection RE (N/A) 5-00-00, Component Maintenance Req. 5 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg 5-34 300 Hour Scheduled Component Inspection RE 5-00-00, Component Maintenance Req. ≈15-Apr-2024 5 A/F (SOURCE: BHT-427-MM) Mos Hrs 1,945.4 300 +10% 2,245.4 151.6 Hrs (+30) Ldg 5-36 600 Hour Scheduled Component Inspection RE 5-00-00, Component Maintenance Req. ≈15-Aug-2024 5 A/F (SOURCE: BHT-427-MM) Mos Hrs 1,764.9 600 +10% 2,364.9 271.1 Hrs (+60) Ldg 5-37 600 Hour / 12 Month Scheduled Component Inspection RE 5-00-00, Component Maintenance Req. 5 A/F (SOURCE: BHT-427-MM) Mos 28-Apr-2023 12 +30d 28-Apr-2024 4.3 Months (+30 Days) Hrs 2,051.3 600 +10% 2,651.3 557.5 Hrs (+60) Ldg 5-38 1200 Hour / 24 Month Scheduled Component Inspection RE 5-00-00, Component Maintenance Req. 5 A/F (Tol. Adjustment: -26d) (SOURCE: BHT-427-MM) Mos 02-Oct-2023 24 +30d 06-Sep-2025 1.7 Years (+30 Days) Hrs 2,075.8 1,200 +10% 3,275.8 1,182 Hrs (+120) Ldg 4,291 5-39 24 Month Scheduled Component Inspection RE 5-00-00, Component Maintenance Req. 5 A/F (SOURCE: BHT-427-MM) Mos 03-Oct-2022 24 +30d 03-Oct-2024 9.6 Months (+30 Days) Hrs Ldg 5-41 300 Hour Scheduled Optional Equipment Inspection RE 5-00-00, Optional Equipment ≈01-Aug-2024 5 A/F (SOURCE: BHT-427-MM) Mos Hrs 2,051.3 300 +10% 2,351.3 257.5 Hrs (+30) Ldg 5-44-001 Conditional Inspection - Hard Landing RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) (NOTE: A hard landing is an accident or incident in which the impact of the helicopter with the ground causes severe pitching of the main rotor or results in noticeable yielding or cracking of the fuselage pylon support structure or the landing gear.) Mos Hrs Ldg 5-45-001 Conditional Inspection - Sudden stoppage - tail rotor - power “on” or “off” RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) (NOTE: Sudden stoppage is any rapid deceleration of the rotor drive system. This may be caused by the seizure of the tail rotor drive system or by contact of the tail rotor blades with the ground, water, snow, dense vegetation or other objects of sufficient mass.) Mos Hrs Ldg 5-46-001 Conditional Inspection - Sudden stoppage - main rotor - power “on” or “off” RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) (NOTE: Sudden stoppage is any rapid deceleration of the rotor drive system. This may be caused by seizure of the transmission or by contact of the main rotor blades with the ground, water, snow, dense vegetation, or other object of sufficient mass.) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 2/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-47-001 Conditional Inspection - Main rotor overspeed RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) (NOTE: Main rotor overspeed is any incident above 104% main rotor RPM (power “on”) or above 107% main rotor RPM (power “off”).) Mos Hrs Ldg 5-48-001 Conditional Inspection - Overtorque RE (A/R) 5-00-00, Conditional Inspections

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5 A/F (SOURCE: BHT-427-MM) (NOTE: An overtorque is an incident in which torsional loads are greater than those permitted are applied to the helicopter dynamic system.) Mos Hrs Ldg 5-49-001 Conditional Inspection - After lightning strike RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) (NOTE: Because lightning behavior is difficult to predict, do a full inspection of the helicopter. Lightning damage can show as burn marks, heat discoloration, arc marks, or as small weld marks (where the metal has melted and become solid again). Honeycomb and other composite materials may show signs of delamination.) Mos Hrs Ldg 5-50-001 Conditional Inspection - One Engine Inoperative (OEI) RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) (NOTE: The IIDS will monitor and record parameter exceedances and OEI events for maintenance purposes. The IIDS will provide a warning (“MAINT ENGINE”) in red indicating that an OEI EXCEEDANCE has been recorded.) Mos Hrs Ldg 5-51-001 Conditional Inspection - One Engine Inoperative (OEI) limit override / use of RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) (NOTE: The IIDS will monitor and record parameter exceedances and OEI events for maintenance purposes. The IIDS will provide a warning (“MAINT ENGINE”) in red indicating that an OEI EXCEEDANCE has been recorded.) Mos Hrs Ldg 5-52-001 Conditional Inspection - Compressor stall or surge RE (A/R) 5-00-00, Conditional Inspections 5 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg ASB 427-01-3 Airspeed Limitation Decal, Replacement of P/N 427-020-671-109 and 427-020-671-1 11 Decal(s) RE (-) Alert Service Bulletin 5 A/F Eff: 18-Sep-2001 (NOTE: At the next 50 Hour scheduled inspection. Model 427 helicopters serial numbers 56029 and subsequent, and model 427 serial numbers 58001 and subsequent, will have the intent of this bulletin accomplished prior to delivery.) Mos Hrs Ldg ASB 427-01-5 FAA Type Certification Kit P/N 427-706-019-101/-103 Deactivation and Addition of Drainage Holes for Common Configuration RE (-) Alert Service Bulletin 5 A/F Eff: 09-Nov-2001 Complied With PCW logbook#1 Mos 10-Oct-2002 Hrs Ldg ASB 427-01-5 Part 1 FAA Type Certification Kit P/N 427-706-019-101/-103 Deactivation and Addition of Drainage Holes for Common Configuration RE (-) Alert Service Bulletin 5 A/F Eff: 09-Nov-2001 Complied With PCW logbook#1 Mos 10-Oct-2002 Hrs Ldg ASB 427-01-5 Part 2 FAA Type Certification Kit P/N 427-706-019-101/-103 Deactivation and Addition of Drainage Holes for Common Configuration RE (-) Alert Service Bulletin 5 A/F Eff: 09-Nov-2001 Complied With PCW logbook#1 Mos 10-Oct-2002 Hrs Ldg ASB 427-03-10 Airspeed Limitation Decal P/N 427-020-671-121, -123, -125, -127 and -129, Introduction of RE (-) Alert Service Bulletin 5 A/F Eff: 05-Dec-2003 Complied With PCW logbook #3 Mos 21-Oct-2005 Hrs 464.1 Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 3/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ASB 427-04-11 Pratt & Whitney Canada PW207D Turboshaft Engines Automatic Low Cycle Fatigue Calculation, Verification of RE (-) Alert Service Bulletin 5 A/F Eff: 13-Jan-2004 Complied With PCW logbook #3 Mos 21-Oct-2005 Hrs 464.1 Ldg ASB 427-09-27 BHT 427 MM, Chapter 4, Correction of RE (-) Alert Service Bulletin 5 A/F Eff: 01-Sep-2009 Complied With Found PCW Mos 30-Apr-2010 Hrs 1,035.6 Ldg TB 427-02-08 Increased Gross Weight (IGW) 6550 lbs Kit P/N 427-706-021-101, -103, -105, Introduction of T (A/R) Optional, Technical Bulletin 5 A/F Eff: 18-Dec-2002 Mos Hrs Ldg TB 427-03-11 Introduction of "Warning Rotating Shaft No Hand Hold" Decal on Transmission Pylon Mounts RE (-) Optional, Technical Bulletin 5 A/F Eff: 05-Mar-2003 (NOTE: Model 427 helicopters serial number 56039, 58004 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg ▼ 8 - LEVELING AND WEIGHING. 08-Weigh Aircraft Weighing RE 8 A/F Mos 23-Aug-2023 36 23-Aug-2026 2.7 Years Hrs 2,061.6 Ldg 4,224 ▼ 10 - PARKING, MOORING, STORAGE AND RETURN TO SERVICE 5-17-002 LOOSE EQUIPMENT - Examine the tail rotor tie-down strap assembly for condition. RE 5-00-00, Scheduled Inspections 10 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-003 LOOSE EQUIPMENT - Examine the main rotor tie-downs for condition. RE 5-00-00, Scheduled Inspections 10 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-004 LOOSE EQUIPMENT - Examine the pitot cover for condition. RE 5-00-00, Scheduled Inspections 10 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-005 LOOSE EQUIPMENT - Examine the engine inlet covers for condition. RE 5-00-00, Scheduled Inspections 10 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-006 LOOSE EQUIPMENT - Examine the engine inlet cover snaps for security on the cover and fuselage. RE 5-00-00, Scheduled Inspections 10 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 4/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-17-007 LOOSE EQUIPMENT - Examine the exhaust covers for condition. RE 5-00-00, Scheduled Inspections 10 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg ▼ 11 - PLACARDS AND MARKINGS 5-15-006 Examine the placards, the decals and the markings. Ensure they are legible, applied correctly and are in agreement with the applicable helicopter configuration. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 11 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg ▼ 12 - SERVICING - ROUTINE MAINTENANCE 12998-001 Oil / Lubricant Servicing - Filter/Hydraulic RE 12-00-00, Servicing Inspections 12 A/F (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d 03-May-2024 4.5 Months (+30 Days) Hrs 2,051.3 600 +10% 2,651.3 557.5 Hrs (+60) Ldg 12998-002 Oil / Lubricant Servicing - Oil/Hydraulic RE 12-00-00, Servicing Inspections 12 A/F (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d 03-May-2024 4.5 Months (+30 Days) Hrs 2,051.3 600 +10% 2,651.3 557.5 Hrs (+60) Ldg 12998-003 Oil / Lubricant Servicing - Rotor Brake Reservoir RE 12-00-00, Servicing Inspections 12 A/F (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d 03-May-2024 4.5 Months (+30 Days) Hrs 2,051.3 600 +10% 2,651.3 557.5 Hrs (+60) Ldg 12998-004 Oil / Lubricant Servicing - Oil/Tail Rotor Gearbox RE 12-00-00, Servicing Inspections 12 A/F (Tol. Adjustment: -7d) (SOURCE: BHT-427-MM) Mos 04-Nov-2023 6 +30d 27-Apr-2024 4.3 Months (+30 Days) Hrs 2,092.8 300 +10% 2,392.8 299 Hrs (+30) Ldg 4,362 12998-005 Oil / Lubricant Servicing - Filter/Transmission RE 12-00-00, Servicing Inspections 12 A/F (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d 03-May-2024 4.5 Months (+30 Days) Hrs 2,051.3 600 +10% 2,651.3 557.5 Hrs (+60) Ldg 12998-006 Oil / Lubricant Servicing - Oil/Transmission RE 12-00-00, Servicing Inspections 12 A/F (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d 03-May-2024 4.5 Months (+30 Days) Hrs 2,051.3 600 +10% 2,651.3 557.5 Hrs (+60) Ldg 12998-007 Oil / Lubricant Servicing - Engine Oil Filter RE 12-00-00, Servicing Inspections ≈30-Aug-2025 12 A/F (SOURCE: BHT-427-MM) Mos Hrs 1,939.4 800 +10% 2,739.4 645.6 Hrs (+80) Ldg 12998-008 Oil / Lubricant Servicing - Engine Oil Filter RE 12-00-00, Servicing Inspections ≈25-Jun-2024 12 A/F (SOURCE: BHT-427-MM) Mos Hrs 1,514.9 800 +10% 2,314.9 221.1 Hrs (+80) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 5/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 12998-009 Oil / Lubricant Servicing - Oil/Engine RE 12-00-00, Servicing Inspections ≈20-May-2026 12 A/F (SOURCE: BHT-427-MM) Mos Hrs 3,000 +10% 3,000 906.2 Hrs (+300) Ldg 12998-010 Oil / Lubricant Servicing - Oil/Engine RE 12-00-00, Servicing Inspections ≈20-May-2026 12 A/F (SOURCE: BHT-427-MM) Mos Hrs 3,000 +10% 3,000 906.2 Hrs (+300) Ldg 12998-011 Oil / Lubricant Servicing - Oil/Ground Handling Wheel RE (-) 12-00-00, Servicing Inspections 12 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg 12999-001 Lubricate - Swashplate Bearing (Two Places) RE 12-00-00, Lubrication Schedule ≈04-Jan-2024 12 A/F (Tol. Adjustment: -4d) (SOURCE: BHT-427-MM) Mos 04-Nov-2023 3 +30d 30-Jan-2024 41 Days (+30) Hrs 2,092.8 50 +10% 2,142.8 49 Hrs (+5) Ldg 4,362 12999-002 Lubricate - Pitch Change Link Bearing (Four Places) RE 12-00-00, Lubrication Schedule ≈04-Jan-2024 12 A/F (Tol. Adjustment: -4d) (SOURCE: BHT-427-MM) Mos 04-Nov-2023 3 +30d 30-Jan-2024 41 Days (+30) Hrs 2,092.8 50 +10% 2,142.8 49 Hrs (+5) Ldg 4,362 12999-003 Lubricate - Hydraulic Pump Drive Adapter RE 12-00-00, Lubrication Schedule ≈01-Aug-2024 12 A/F (SOURCE: BHT-427-MM) Mos Hrs 2,051.3 300 +10% 2,351.3 257.5 Hrs (+30) Ldg 12999-004 Lubricate - Forward Tail Rotor Driveshaft (Two Places) RE 12-00-00, Lubrication Schedule 12 A/F (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d 03-May-2024 4.5 Months (+30 Days) Hrs 2,051.3 600 +10% 2,651.3 557.5 Hrs (+60) Ldg 12999-005 Lubricate - Oil Cooler Blower Hanger Bearing (2 Places) - P/N 407-340-339-103 RE (N/A) 12-00-00, Lubrication Schedule 12 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg 12999-006 Lubricate - Oil Cooler Blower Hanger Bearing (Two Places) - P/N 407-340-339-101 RE (N/A) 12-00-00, Lubrication Schedule 12 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg 12999-007 Lubricate - Oil Cooler Blower Hanger Bearing (Two Places) - P/N 407-340-339-107 RE 12-00-00, Lubrication Schedule ≈15-Apr-2024 12 A/F (SOURCE: BHT-427-MM) Mos Hrs 1,945.4 300 +10% 2,245.4 151.6 Hrs (+30) Ldg 12999-008 Lubricate - Segmented Tail Rotor Driveshaft Hanger Bearing (Four Places) - P/N 407-340-339-103 RE (N/A) 12-00-00, Lubrication Schedule 12 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg 12999-009 Lubricate - Segmented Tail Rotor Driveshaft Hanger Bearing (Four Places) - P/N 407-340-339-101 RE (N/A) 12-00-00, Lubrication Schedule 12 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 6/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 12999-010 Lubricate - Segmented Tail Rotor Driveshaft Hanger Bearing (Four Places) - P/N 407-340-339-107 RE 12-00-00, Lubrication Schedule ≈15-Apr-2024 12 A/F (SOURCE: BHT-427-MM) Mos Hrs 1,945.4 300 +10% 2,245.4 151.6 Hrs (+30) Ldg 12999-011 Lubricate - Tail Rotor Pitch Change Mechanism (Two Places) RE 12-00-00, Lubrication Schedule 12 A/F (Tol. Adjustment: -2d) (SOURCE: BHT-427-MM) Mos 04-Nov-2023 3 +30d 01-Feb-2024 43 Days (+30) Hrs 2,092.8 300 +10% 2,392.8 299 Hrs (+30) Ldg 4,362 12999-012 Lubricate - Ground Handling Wheel (Three Places) RE (-) 12-00-00, Lubrication Schedule 12 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg 5-15-004 Service and lubricate the helicopter as necessary. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 12 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-16-012 Examine the color and level of the fluid in the system reservoir. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 12 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-32-002 Lubricate bearings with grease Royco 13 per MIL-G-25013 lubricant (C-026) RE (N/A) 5-00-00, Component Maintenance Req. 12 A/F (SOURCE: BHT-427-MM) Mos Hrs Ldg 5-34-004 TAIL ROTOR DRIVE SYSTEM - Lubricate bearings with the appropriate grease outlined inTable 12-2. RE 5-00-00, Component Maintenance Req. ≈15-Apr-2024 12 A/F 5-34 (SOURCE: BHT-427-MM) (NOTE: This component inspection applies to the P/N 407-340-339-101/-107 hanger bearing.) Mos Hrs 1,945.4 300 +10% (2,245.4) 151.6 Hrs (+30) Ldg ▼ 21 - AIR CONDITIONING AND PRESSURIZATION 21-CUS-001 I.C.A. - Air Comm 25-Hour Inspection - STC SR00418DE RE ≈25-Nov-2023 21 A/F Mos 10-Oct-2023 Hrs 2,078.9 25 2,103.9 10.1 Hrs Ldg 4,312 21-CUS-002 I.C.A. - Air Comm 100-Hour Inspection - STC SR00418DE RE ≈12-Jan-2024 21 A/F Mos 05-May-2023 Hrs 2,051.3 100 2,151.3 57.5 Hrs Ldg 427-MMS-22 (1) Perform a IDS Cooling system operational check RE Supplemental Inspection ≈21-Dec-2027 21 A/F (SOURCE: 427-MMS-22) Mos Hrs 2,370.8 1,200 3,570.8 1,477 Hrs Ldg 427-MMS-22 (2) IIDS Cooling Fan Bearings Replace RE Supplemental Inspection ≈09-Dec-2031 21 A/F (SOURCE: 427-MMS-22) Mos Hrs 5,000 5,000 2,906.2 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 7/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-17-008 VENTILATION - Examine the ram air system for condition and correct operation. RE 5-00-00, Scheduled Inspections 21 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg ASB 427-16-40 Rev A Air Conditioner Blower Motor Connector, Inspection of RE (-) Alert Service Bulletin 21 A/F Eff: 05-Aug-2016 Complied With Found PCW Mos 28-Apr-2016 Hrs 1,568.7 Ldg TB 427-03-14 Cabin Heater Bleed Air Shutoff Valve P/N S-9730EC-1 and Particle Separator Kit P/N 427-706-012 Bleed Air Shutoff Valve P/N S-9730EC-2, Relocation of RE (-) Recommended, Technical Bulletin 21 A/F Eff: 17-Jun-2003 Mos Hrs Ldg TB 427-03-14 Part 1 Cabin Heater Bleed Air Shutoff Valve P/N S-9730EC-1 and Particle Separator Kit P/N 427-706-012 Bleed Air Shutoff Valve P/N S-9730EC-2, Relocation of T (A/R) Recommended, Technical Bulletin 21 A/F Eff: 17-Jun-2003 Mos Hrs Ldg TB 427-03-14 Part 2 Cabin Heater Bleed Air Shutoff Valve P/N S-9730EC-1 and Particle Separator Kit P/N 427-706-012 Bleed Air Shutoff Valve P/N S-9730EC-2, Relocation of T (A/R) Recommended, Technical Bulletin 21 A/F Eff: 17-Jun-2003 Mos Hrs Ldg ▼ 24 - ELECTRICAL POWER 243037 Generator Control Unit RE (O/C) 24 ENG1 Unknown Unknown Mos 25-Aug-1999 Hrs 0 Enc 0 243037 Generator Control Unit RE (O/C) 24 ENG2 Unknown Unknown Mos 24-Aug-1999 Hrs 0 Enc 0 243137 Main Battery RE (O/C) 24 A/F Unknown Unknown Mos 21-Oct-2000 Hrs 0 Ldg 0 ASB 427-01-6 In-Line Electrical Terminal Junctions, Replacement of RE (-) Alert Service Bulletin 24 A/F Eff: 05-Nov-2001 Complied With PCW logbook#1 Mos 19-Aug-2002 Hrs Ldg ASB 427-06-14 Bus Bar, Replacement of RE (-) Alert Service Bulletin 24 A/F Eff: 07-Nov-2006 Mos Hrs Ldg ASB 427-06-14 Part 1 Bus Bar, Replacement of RE (-) Alert Service Bulletin 24 A/F Eff: 07-Nov-2006 Complied With PCW logbook #3 (NOTE: No later than March 31, 2007. Helicopters S/N: 56001 through 56031, 58001 and 58002 equipped with Flight Instrument Kit P/N: 427- 706-002, which have not complied with TB 427-02- 07 Instrument Cooling Fans, Installation Of.) Mos 01-Dec-2006 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 8/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ASB 427-06-14 Part 2 Bus Bar, Replacement of RE (-) Alert Service Bulletin 24 A/F Eff: 07-Nov-2006 (NOTE: No later than March 31, 2007. Helicopters S/N: 56001 through 56031, 58001 and 58002 equipped with Flight Instrument Kit P/N: 427- 706-002, which have complied with TB 427-02-07 Instrument Cooling Fans, Installation Of, and Helicopters S/N: 56032 through 56054, equipped with Flight Instrument Kit P/N: 427-706-002.) Mos Hrs Ldg TB 427-02-06 Battery Relay Diode, 2430CR4, Removal of RE (-) Recommended, Technical Bulletin 24 A/F Eff: 18-Jun-2002 (NOTE: Model 427 helicopters serial number 56031 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg TB 427-03-12 Relay Box P/N 427-075-161-101 and 427-075-162-101 Inspection for Internal Corrosion an Waterproofing RE (-) Recommended, Technical Bulletin 24 A/F Eff: 23-Apr-2003 (NOTE: Model 427 helicopters serial number 56031 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg TB 427-09-25 427 Relay Box Improvement RE (-) Recommended, Technical Bulletin 24 A/F Eff: 27-Jan-2009 (NOTE: Model 427 helicopters serial number 56068 and subsequent, will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg ▼ 25 - EQUIPMENT/FURNISHINGS 2021-19-01 Cabin Equipment/Furnishings - Comfort Clip Interfering with the Seat Belt Inertia Reel RE (-) Mandatory 25 A/F Eff: 13-Oct-2021 Not Applicable Comfort clips not installed (NOTE: COMPLIANCE: Within 25 hours time-in-service after the effective date of this AD: (i) Remove each comfort clip from service. (ii) Inspect each shoulder harness seat belt for a rip and abrasion. If there is a rip or any abrasion, before further flight, remove the shoulder harness seat belt from service.) Mos 14-Oct-2021 Hrs 1,969.6 Ldg 250099-0101 Emergency Locator Transmitter (ELT) Battery RE Component Recommended Replacement 25 A/F Unknown Unknown Certified Date 31-Oct-2020 (Manual Adjustment: -8d) 0 Mos 30-Nov-2020 88 22-Feb-2028 4.2 Years Hrs Ldg 250100-0101 Emergency Locator Transmitter (ELT) RE (O/C) 25 A/F Unknown Unknown Mos 01-Apr-2001 Hrs 0 Ldg 0 25-CUS-001 Annual Life Vest Inspection RE 25 A/F Mos 23-Aug-2023 12 23-Aug-2024 8.2 Months Hrs 2,061.6 Ldg 4,224 5-17-009 EQUIPMENT AND FURNISHINGS - Examine the interior panels, carpets and upholstery for condition and make sure that they are clean. RE 5-00-00, Scheduled Inspections 25 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 9/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-17-010 EQUIPMENT AND FURNISHINGS - Examine the complete crew and passenger seats for condition, pan cushion placement, security of installation, damage and chaffing. RE 5-00-00, Scheduled Inspections 25 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-011 EQUIPMENT AND FURNISHINGS - Examine the crew and passenger seat energy absorber reference marks. Replace the seat assembly if the reference mark is below the reference point. RE 5-00-00, Scheduled Inspections 25 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-012 EQUIPMENT AND FURNISHINGS - Examine the complete crew and passenger restraint assemblies for condition, correct operation and security. RE 5-00-00, Scheduled Inspections 25 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg ASB 427-07-16 Cargo Hook Stress Corrosion Cracks RE (-) Alert Service Bulletin 25 A/F Eff: 26-Mar-2007 Not Applicable No Hook Mos 15-Feb-2008 Hrs 832.2 Ldg ASB 427-10-30 Cargo Hook Equipment Kit P/N 427-706-900-101 and -109 Improvement of RE (-) Alert Service Bulletin 25 A/F Eff: 08-Feb-2010 Not Applicable No hook PCW (NOTE: Model 427 helicopters serial numbers 56078 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery.) Mos 30-Apr-2010 Hrs 1,035.6 Ldg ASB 427-15-39 Seat Belt Comfort Clips, Removal of RE (-) Alert Service Bulletin 25 A/F Eff: 11-Jan-2016 Complied With Found PCW Days 24-Jul-0210 Hrs Ldg FAR 91.207 Emergency Locator Transmitter (ELT) Inspection and Test per FAR 91.207 (d) RE FAR91, FAR 91 25 A/F Unknown Unknown Mos 01-May-2023 12 01-May-2024 4.4 Months Hrs Ldg IL GEN-19-144 ACR Electronics Artex-Branded Emergency Locator Transmitter G-Switch Testing And Maintenance (Service Bulletin - SB1000) T (A/R) Information Letter 25 A/F Eff: 25-Jun-2019 Mos Hrs Ldg ▼ 26 - FIRE PROTECTION 261100-0101 Cartridge Fire Ext. (J1 Port) RE 04-00-00, Life Limit 26 A/F No.1 30600-12 00873/0166 New Manufactured Date 31-Jul-2015 (SOURCE: BHT-427-MM) 0 Yrs 31-Jul-2015 10 31-Jul-2025 1.6 Years Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 10/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 261100-0102 Cartridge Fire Ext. (J1 Port) RE 04-00-00, Life Limit 26 A/F No.2 30600-12 00302/156 New Manufactured Date 31-Jul-2015 (SOURCE: BHT-427-MM) 0 Yrs 31-Jul-2015 10 31-Jul-2025 1.6 Years Hrs Ldg 261100-0201 Cartridge Fire Ext. (J2 Port) RE 04-00-00, Life Limit 26 A/F No.1 30600-13 00821/0166 New Manufactured Date 31-Jul-2015 (SOURCE: BHT-427-MM) 0 Yrs 31-Jul-2015 10 31-Jul-2025 1.6 Years Hrs Ldg 261100-0202 Cartridge Fire Ext. (J2 Port) RE 04-00-00, Life Limit 26 A/F No.2 30600-13 00823/156 New Manufactured Date 31-Jul-2015 (SOURCE: BHT-427-MM) 0 Yrs 31-Jul-2015 10 31-Jul-2025 1.6 Years Hrs Ldg 262100-0101 Fire Extinguisher Reservoir RE (O/C) On Condition 26 A/F No.1 427-369-510-103 0166 (SOURCE: BHT-427-MM) Mos 21-Dec-2021 Hrs 1,824.3 Ldg 262100-0101-OH OVERHAUL - Fire Extinguisher Reservoir RE 5-00-00, Overhaul 26 A/F No.1 427-369-510-103 0166 (SOURCE: BHT-427-MM) Yrs 21-Dec-2021 5 +30d 21-Dec-2026 3 Years (+30 Days) Hrs 1,824.3 Ldg 262100-0102 Fire Extinguisher Reservoir RE (O/C) On Condition 26 A/F No.2 427-369-510-103 0156 (SOURCE: BHT-427-MM) Mos 21-Dec-2021 Hrs 2,338.2 Ldg 262100-0102-OH OVERHAUL - Fire Extinguisher Reservoir RE 5-00-00, Overhaul 26 A/F No.2 427-369-510-103 0156 (SOURCE: BHT-427-MM) Yrs 21-Dec-2021 5 +30d 21-Dec-2026 3 Years (+30 Days) Hrs 2,338.2 Ldg 26-CUS-001 Portable Fire Extinguisher RE (-) 26 A/F 10633 Unknown Serviceable Mos Hrs Ldg 26-CUS-002 Portable Fire Extinguisher 30-Day Inspection RE 26 A/F 10633 Unknown (UPDATE NOTE: Inspected Fire bottle IAW Amerex Corp maintenance instruction placard in the bottle. Fire extinguisher returned to service. ) Days 19-Dec-2023 30 18-Jan-2024 29 Days Hrs Ldg 26-CUS-003 Portable Fire Extinguisher 12-Month Weight Check. RE 26 A/F 10633 Unknown Mos 30-May-2023 12 30-May-2024 5.4 Months Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 11/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-17-013 FIRE PROTECTION - Examine the hand-held fire extinguisher and the quick release for condition and security. RE 5-00-00, Scheduled Inspections 26 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-014 FIRE PROTECTION - Examine the engine heat-sensing elements for condition, damage and security. RE 5-00-00, Scheduled Inspections 26 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-015 FIRE PROTECTION - Examine the left and right fire extinguisher reservoirs for condition and security. Make sure they show the correct pressure. RE 5-00-00, Scheduled Inspections 26 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-016 FIRE PROTECTION - Examine the discharge tubes for condition and security. RE 5-00-00, Scheduled Inspections 26 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-018 FIRE PROTECTION - Perform all recommended manufacturers inspections on the fire extinguisher reservoir. RE 5-00-00, Scheduled Inspections 26 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg ASB 427-13-36 Fire Bottle Outlet Tube Protective cap P/N SC.625-24, Introduction of RE (-) Alert Service Bulletin 26 A/F Eff: 05-Aug-2013 Complied With Found PCW Mos 11-Mar-2014 Hrs 1,340.2 Ldg ▼ 27 - FLIGHT CONTROLS ASB 427-02-08 Cyclic Centering Switch, Relocation of RE (-) Alert Service Bulletin 27 A/F Eff: 07-Jun-2002 Complied With PCW logbook #1 Mos 29-Mar-2003 Hrs Ldg ASB 427-08-20 Collective Control Idler Link Assembly P/N 427-001-532-101 Inspection and Modification of RE (-) Alert Service Bulletin 27 A/F Eff: 27-Feb-2008 Complied With Found PCW Mos 24-Apr-2008 Hrs 852.4 Ldg ASB 427-09-23 Lever Assembly P/N 407-001-320-105 and 407-001-320-109, One Time Inspection of RE (-) Alert Service Bulletin 27 A/F Eff: 10-Mar-2009 Complied With Found PCW Mos 18-Mar-2009 Hrs 926.8 Ldg ASB 427-10-34 Flight Control Bearing P/N MS27645-4A; Inspection and Replacement of RE (-) Alert Service Bulletin 27 A/F Eff: 10-Dec-2010 Complied With Found PCW Mos 13-Jun-2011 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 12/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ASB 427-10-34 Part 1 Flight Control Bearing P/N MS27645-4A; Inspection and Replacement of RE (-) Alert Service Bulletin 27 A/F Eff: 10-Dec-2010 Complied With Mos 13-Jun-2011 Hrs Ldg ASB 427-10-34 Part 2 Flight Control Bearing P/N MS27645-4A; Inspection and Replacement of RE (-) Alert Service Bulletin 27 A/F Eff: 10-Dec-2010 Complied With Mos 13-Jun-2011 Hrs Ldg TB 427-07-24 Adjustable Directional Control Pedal P/N 407-001-012-101, Introduction of RE (-) Optional, Technical Bulletin 27 A/F Eff: 29-Mar-2007 (NOTE: Model 427 helicopters serial number 56061 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg TB 427-09-26 Introduction of New Tail Rotor Actuator Idler Assembly P/N 427-001-723-103 RE (-) Recommended, Technical Bulletin 27 A/F Eff: 26-Oct-2009 (NOTE: Model 427 helicopters serial number 56068 and subsequent, will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg ▼ 28 - FUEL 5-16-001 Examine the engine fuel feed lines for condition. Inspect for proper installation and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-002 Examine the fuel shut-off valve assembly for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-003 Examine the fuel shut-off valve control cable, brackets and handle assembly for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-004 Examine the fuel vent lines for condition. Inspect for proper installation and security. Ensure the fuel vent lines are not clogged. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-005 Examine the fuel drain valves for static leaks. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-006 Visually inspect fuel samples for contamination. Take samples from each fuel cell. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 13/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-16-007 Visually inspect the fuel cavity vent/drains from under the cabin floor for fuel leakage. Ensure that the vent/drains are not clogged. Examine the aft cell grommets for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-008 Examine the ground connection and fuel filler cap for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 28 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-17-001 Inspect all fuel system, oil system, and hydraulic system filler caps for proper functioning and sealing. Make sure the sealing O-rings within the filler caps are in good condition. Repair or replace the filler caps or replace sealing O-rings as required. Record accomplishment of this inspection in Historical Record. RE 5-00-00, Scheduled Inspections 28 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-019 FUEL SYSTEM - Perform an operational check of the fuel shut-off valve. Ensure that the control cable and shut-off valve are smooth through its full range of operation. RE 5-00-00, Scheduled Inspections 28 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg IL GEN-19-142 Utilization of Anti-Icing Additive in the Fuel System T (A/R) Information Letter 28 A/F Eff: 07-May-2019 Mos Hrs Ldg IL GEN-20-148 Utilization of Biocide Additive in the Fuel System T (A/R) Information Letter 28 A/F Eff: 06-Jul-2020 Mos Hrs Ldg TB 427-01-1 Fuel Transfer Control Unit (FTCU) P/N 427-375-010-101, Replacement of RE (-) Recommended, Technical Bulletin 28 A/F Eff: 14-Mar-2001 (NOTE: Model 427 helicopters serial numbers 56025 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg TB 427-03-13 Fuel Feed Hose Assembly P/N 427-366-280-101, Introduction of RE (-) Optional, Technical Bulletin 28 A/F Eff: 04-Jun-2003 (NOTE: Model 427 helicopters serial number 56041 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg TB 427-05-22 FUEL SYSTEM IMPROVEMENT OF RE (-) Optional, Technical Bulletin 28 A/F Eff: 27-Feb-2007 (NOTE: 56047 and subsequent will have the intent of this bulletin completed before delivery) Mos Hrs Ldg ▼ 29 - HYDRAULIC POWER 2003-04-14 Hydraulic Solenoid Tee Fitting P/N AS1003W060404, and Tubes - Replacement RE (-) Mandatory 29 A/F Eff: 04-Apr-2003 Not Applicable Found PCW Bell Helicopters Logbook#1 Days 31-Aug-2002 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 14/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 2009-25-08 Hydraulic pump driveshaft assembly RE (-) Mandatory 29 A/F Eff: 28-Dec-2009 Complied With By part number Mos 16-Feb-2010 Hrs 1,014.4 Ldg 5-16-009 Examine the hydraulic system for general condition, leaks and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 29 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-010 Examine all rigid and flexible hoses for security and general condition. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 29 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-011 Examine the pressure and return filters for impending bypass indication. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 29 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-013 Examine the hydraulic actuators for leakage and correct attachment. Clean exposed area of cylinder piston with hydraulic fluid and a clean lint-free cloth. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 29 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-015 Examine the hydraulic pump for leaks. Inspect for proper installation and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 29 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg ASB 427-01-2 Hydraulic Solenoid "Tee Fitting" P/N AS1003W060404, Tubes P/Ns 427-080-058-101 and 427-080-003-101, Replacement of RE (-) Alert Service Bulletin 29 A/F Eff: 20-Aug-2001 (NOTE: At next scheduled hydraulic filter and fluid replacement but no later than August 31, 2002.Model 427 helicopters serial numbers 56032 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg ASB 427-05-12 Rev A Clevis Assembly Hydraulic Servo Assembly, Part Number 41011300 and 41011700 RE (-) Alert Service Bulletin 29 A/F Eff: 14-Nov-2005 Complied With PCW logbook #3 Mos 21-Oct-2005 Hrs 464.1 Ldg ASB 427-08-22 Hydraulic Pump Driveshaft Assembly P/N 406-040-072-105, One Time Inspection of RE (-) Alert Service Bulletin 29 A/F Eff: 26-Jun-2008 Not Applicable by P/N Mos 03-Sep-2008 Hrs 884.8 Ldg ASB 427-09-28 Hydraulic Servoactuator P/N 206-076-062-11 1, Inspection of RE (-) Alert Service Bulletin 29 A/F Eff: 07-Oct-2009 Complied With Found PCW Mos 30-Apr-2010 Hrs 1,035.6 Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 15/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ASB 427-09-28 Part 1 Hydraulic Servoactuator P/N 206-076-062-11 1, Inspection of RE (-) Alert Service Bulletin 29 A/F Eff: 07-Oct-2009 Complied With Found PCW Mos 30-Apr-2010 Hrs 1,035.6 Ldg ASB 427-09-28 Part 2 Hydraulic Servoactuator P/N 206-076-062-11 1, Inspection of RE (-) Alert Service Bulletin 29 A/F Eff: 07-Oct-2009 Complied With Found PCW Mos 30-Apr-2010 Hrs 1,035.6 Ldg ASB 427-11-35 Rev B Clevis Assembly - Hydraulic Servo Assemblies, P/N 206-076-062-109 and 206-076-062-111 RE (-) Alert Service Bulletin 29 A/F Eff: 29-Aug-2011 Complied With Found PCW Mos 17-Aug-2011 Hrs 1,129.1 Ldg TB 427-05-19 Hydraulic Pump Input Shaft 407-340-107-101 and Adapter 407-340-108-101, Introduction of RE (-) Optional, Technical Bulletin 29 A/F Eff: 07-Jan-2005 Mos Hrs Ldg TB 427-05-19 Part 1 Hydraulic Pump Input Shaft 407-340-107-101 and Adapter 407-340-108-101, Introduction of RE (-) Optional, Technical Bulletin 29 A/F Eff: 07-Jan-2005 (NOTE: Helicopters Serial Number 56048 and subsequent and 58003 and subsequent will have the intent of this bulletin completed before delivery.) Mos Hrs Ldg TB 427-05-19 Part 2 Hydraulic Pump Input Shaft 407-340-107-101 and Adapter 407-340-108-101, Introduction of RE (-) Technical Bulletin 29 A/F Eff: 07-Jan-2005 (NOTE: Helicopters Serial Number 56048 and subsequent and 58003 and subsequent will have the intent of this bulletin completed before delivery.) Mos Hrs Ldg TB 427-16-34 Rev A Hydraulic Pressure Switch 205-076-044- 007, Inspection and Addition of Safety Wire T (-) Recommended 29 A/F Eff: 22-Nov-2016 Mos Hrs Ldg TB 427-16-34 Rev B Hydraulic Pressure Switch 205-076-044- 007, Inspection and Addition of Safety Wire RE (-) Recommended 29 A/F Eff: 10-Jan-2018 Mos Hrs Ldg ▼ 31 - INDICATING / RECORDING SYSTEM IL GEN-21-151 Defective Pitot/Static Elbow Fitting 50-012-13N402 T (A/R) Information Letter 31 A/F Eff: 12-May-2021 Mos Hrs Ldg TB 427-02-07 Instrument Cooling Fans, Installation of RE (-) Recommended, Technical Bulletin 31 A/F Eff: 02-Oct-2002 (NOTE: Model 427 helicopters serial number 56032 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery.) Mos Hrs Ldg TB 427-03-09 Integrated Instrument Display System (IIDS). Data Acquisition Unit (DAU) 427-375-001-101 and 427-375-001-113, and Display Unit (DU) 427-375-001-103 and 427-375-001-115, Replacement of RE (-) Recommended, Technical Bulletin 31 A/F Eff: 16-Jan-2003 (NOTE: Model 427 helicopters serial number 56036 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 16/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ▼ 32 - LANDING GEAR 321100-0101 Forward Crosstube Low RE 04-00-00, Life Limit ≈16-Apr-2178 32 A/F 427-036-103-117 AT 12 (SOURCE: BHT-427-MM) Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 0 RIN(2) 0 60,000 60,000 55,632 RIN(2) 321200-0101 Aft Crosstube Low RE 04-00-00, Life Limit ≈05-Oct-2189 32 A/F 427-036-104-121 AT 214 New (SOURCE: BHT-427-MM) Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 0 RIN(3) 0 70,000 70,000 65,632 RIN(3) 321300-0101 Forward Crosstube High RE (O/C) 04-00-00, Life Limit 32 A/F Not Type Installed Not Type Installed (SOURCE: BHT-427-MM) Mos Hrs Ldg 321400-0101 Forward Crosstube High RE (O/C) 04-00-00, Life Limit 32 A/F Not Type Installed Not Type Installed (SOURCE: BHT-427-MM) Mos Hrs Ldg 321500-0101 Aft Crosstube High RE (O/C) 04-00-00, Life Limit 32 A/F Not Type Installed Not Type Installed (SOURCE: BHT-427-MM) Mos Hrs Ldg 321600-0101 Forward Crosstube Low RE (O/C) 04-00-00, Life Limit 32 A/F Not Type Installed Not Type Installed (SOURCE: BHT-427-MM) Mos Hrs Ldg 321700-0101 Aft Crosstube Low RE (O/C) 04-00-00, Life Limit 32 A/F Not Type Installed Not Type Installed (SOURCE: BHT-427-MM) Mos Hrs Ldg 321800-0101 Forward Crosstube High RE (O/C) 04-00-00, Life Limit 32 A/F Not Type Installed Not Type Installed (SOURCE: BHT-427-MM) Mos Hrs Ldg 321900-0101 Aft Crosstube High RE (O/C) 04-00-00, Life Limit 32 A/F Not Type Installed Not Type Installed (SOURCE: BHT-427-MM) Mos Hrs Ldg 322600-0101 Emergency Floatation System Cartidge RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 17/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 323100-0101 Float Bag Assembly RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Left Fwd Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 323100-0102 Float Bag Assembly RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Right Fwd Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 323100-0201 Float Bag Assembly RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Left Middle Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 323100-0202 Float Bag Assembly RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Right Middle Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 323100-0301 Float Bag Assembly RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Left Aft Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 323100-0302 Float Bag Assembly RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Right Aft Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 323200-0101 Float Reservoir Assembly RE (O/C) 04-00-00, Floats, Life Limit 32 A/F Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 5-15-007 Examine the landing gear forward crosstube for damage and security. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 32 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-15-008 Examine the landing gear aft crosstube for damage and security. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 32 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-15-009 Examine the landing gear aft crosstube, support beam, pivot bolt and wear strips for damage and security. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 32 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 18/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-15-010 Examine the landing gear assembly for proper installation and security to helicopter fuselage. Ensure the electrical bonding straps are attached. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 32 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-15-011 Examine the landing gear skid tubes, skid saddles and skid shoes for condition and security. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 32 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg ASB 427-07-17 Disc Assembly 407-340-340-103, Inspection of RE (-) Alert Service Bulletin 32 A/F Eff: 28-Mar-2007 Complied With Mos 15-Apr-2007 Hrs 642.8 Ldg ASB 427-07-17 Part 2 Disc Assembly 407-340-340-103, Inspection of RE (-) Alert Service Bulletin 32 A/F Eff: 28-Mar-2007 Complied With Mos 15-Apr-2007 Hrs 642.8 Ldg TB 427-04-18 Emergency Flotation System, Modification of RE (-) Recommended, Technical Bulletin 32 A/F Eff: 13-Oct-2004 (NOTE: Model 427 helicopters serial number 56037 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg ▼ 34 - NAVIGATION Garmin GI-205 Indicator RE (O/C) 34 A/F 013-02121-00 1175 New Mos 21-Jul-2023 Hrs 2,145.3 Ldg Garmin GRA 55 Rad Alt RE (O/C) 34 A/F 011-02537-05 3RC009042 New Mos 21-Jul-2023 Hrs 2,145.3 Ldg Sensor Systems Alt Antenna - Co Pilot Side RE (O/C) 34 A/F S67-2002 543-112231 New Mos 21-Jul-2023 Hrs 2,145.3 Ldg Sensor Systems Alt Antenna - Pilot Side RE (O/C) 34 A/F S67-2002 542-112217 New Mos 21-Jul-2023 Hrs 2,145.3 Ldg True Blue Power Inverter RE (O/C) 34 A/F MD50 B23-10856 New Mos 21-Jul-2023 Hrs 2,145.3 Ldg 341000-0101 Altimeter RE (O/C) 34 A/F Unknown Unknown Mos 21-Oct-2000 Hrs 0 Ldg 0 [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 19/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 342000-0101 Transponder RE (O/C) 34 A/F Unknown Unknown Mos 21-Oct-2000 Hrs 0 Ldg 0 FAR 91.413 ATC Transponder test and inspections per FAR 91.413 Appendix F of Part 43. RE FAR91, FAR 91 34 A/F Unknown Unknown Inspected Date 02-May-2023 Mos 02-May-2023 24 02-May-2025 1.4 Years Hrs Ldg OSN GEN-22-51 Potential 5G C-Band Wireless Broadband Interference with Radio (Radar) Altimeter Equipment T (A/R) Operation Safety Notice 34 A/F Eff: 20-Jan-2022 Mos Hrs Ldg TB 427-03-15 Artificial Horizon Indicator, Replacement of RE (-) Technical Bulletin 34 A/F Eff: 27-Jun-2003 (NOTE: Model 427 helicopters serial number 56032 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg TB 427-10-30 Encoding Altimeter P/N 214-175-278-101, Replacement of RE (-) Technical Bulletin 34 A/F Eff: 04-Jun-2010 (NOTE: Model 427 helicopters serial number 56067 and subsequent and serial number 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg ▼ 39 - ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS IL 427-20-05 New DU and DAU Replacement Units T (A/R) Information Letter 39 A/F Eff: 29-Jan-2020 Mos Hrs Ldg ▼ 52 - DOORS 5-17-020 DOORS AND WINDOWS - Examine the crew, passenger, baggage compartment and battery doors for condition, security and correct operation. RE 5-00-00, Scheduled Inspections 52 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-021 DOORS AND WINDOWS - Examine the passenger door restraint strap for condition, security and correct operation. RE 5-00-00, Scheduled Inspections 52 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-022 DOORS AND WINDOWS - Examine all windows and windshields for condition and security. RE 5-00-00, Scheduled Inspections 52 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg TB 427-09-28 New Improved Door Seals RE (-) Optional, Technical Bulletin 52 A/F Eff: 30-Nov-2009 (NOTE: Model 427 helicopters serial number 56066 and subsequent and 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 20/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ▼ 53 - FUSELAGE 2003-04-12 Auxiliary Fin Assemblies, P/N 427-035-836-101, -102, -105, or -106 - Modification/ RFM Revision RE (-) Mandatory 53 A/F Eff: 04-Apr-2003 Complied With Found PCW byt Bell Helicopters Logbook#1 Mos 30-Apr-2002 Hrs Ldg 2003-04-12 Par. 2(a) Auxiliary Fin Assemblies, P/N 427-035-836-101, -102, -105, or -106 - Modification RE (-) Mandatory 53 A/F Eff: 04-Apr-2003 Complied With Found PCW byt Bell Helicopters Logbook#1 Days 30-Apr-2002 Hrs Ldg 2003-04-12 Par. 2(b) Auxiliary Fin Assemblies, P/N 427-035-836-101, -102, -105, or -106 - RFM Revision RE (-) Mandatory 53 A/F Eff: 04-Apr-2003 Complied With Found PCW byt Bell Helicopters Logbook#1 Mos 30-Apr-2002 Hrs Ldg 2012-10-01 Tailboom Attachment Bolt - Over-Torque - Replace/ Inspect RE (-) Mandatory 53 A/F Eff: 29-Jun-2012 Complied With Found PCW Performed ASB 427-10-31 on 04-09-2010, replacement of tail boom attachment hardware Mos 13-Jun-2011 Hrs 1,127.8 Ldg 2012-10-01 Par. 2(e)(1) Tailboom Attachment Bolt - Over-Torque - Replace RE (-) Mandatory 53 A/F Eff: 29-Jun-2012 Complied With Found PCW Performed ASB 427-10-31 on 04-09-2010, replacement of tail boom attachment hardware Days 13-Jun-2011 Hrs 1,127.8 Ldg 2012-10-01 Par. 2(e)(2) Tailboom Attachment Bolt - Over-Torque - Inspect RE Mandatory ≈01-Aug-2024 53 A/F Eff: 29-Jun-2012 Complied With Accomplished as part of the BHT 427 MM 300 hour inspection Mos Hrs 2,051.3 300 2,351.3 257.5 Hrs Ldg 5-16-099 Perform a torque check of the vertical fin attachment hardware. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 53 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16A-001 Examine the tailboom skins around the edge of the horizontal stabilizer support for cracks using 10X magnification. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-002 Do a visual inspection of the horizontal stabilizer supports for security and loose fasteners. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-003 Examine the aft tailboom skins around the rivets heads for cracks using 10X magnification. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 21/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-16A-004 Examine the mid tailboom skins around the rivet heads for cracks using 10X magnification. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-005 Examine the forward tailboom skin around the rivet heads for cracks using 10X magnification. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-006 Examine the doubler area of the tailboom skin around the rivet heads for cracks using 10X magnification. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-007 Do a visual inspection of the tailboom skins and horizontal stabilizer supports for loose fasteners. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-008 Examine the longeron and intercostal around the rivet heads for visual cracks. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-009 Do a visual inspection of the longeron and intercostal for security and loose fasteners. RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-16A-011 Perform torque check of tailboom attachment hardware RE 5-00-00, Scheduled Inspections 53 A/F 5-16A (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 300 +10% (2,351.3) 257.5 Hrs (+30) Ldg 5-17-023 FUSELAGE - Examine the fuselage structure for condition, security and corrosion damage. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-024 FUSELAGE - Examine the roof and beam assembly for corrosion damage, rivet attachment and condition. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-025 FUSELAGE - Examine all structural access panels for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 22/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-17-026 FUSELAGE - Examine cowlings for condition. Ensure all inspection panels, hinges and latches operate correctly. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-027 FUSELAGE - Examine the floor and the walls of the baggage compartment for damage and condition. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-028 FUSELAGE - Examine the tailboom attachment fittings and hardware on the fuselage for condition, security and loose fasteners. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-029 TAILBOOM - Examine the tail rotor driveshaft covers for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-030 TAILBOOM - Examine the tailboom assembly for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-031 TAILBOOM - Examine the tailboom attachment fittings and hardware for condition, security and loose fasteners. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-032 TAILBOOM - Examine the tailboom skins for chafing damage from the tail rotor driveshaft covers. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-033 TAILBOOM - Examine the horizontal stabilizer for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-034 TAILBOOM - Examine the upper and lower skin surfaces of the horizontal stabilizer for condition RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-035 TAILBOOM - Examine the auxiliary fins for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 23/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-17-036 TAILBOOM - Examine the vertical fin for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-037 TAILBOOM - Examine the tail skid for condition and security. Tail skid movement is not allowed. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-038 TAILBOOM - Examine the tail rotor gearbox support where it attaches to the tailboom for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 5-17-039 TAILBOOM - Examine the tail rotor gearbox where it attaches to the gearbox support for condition and security. RE 5-00-00, Scheduled Inspections 53 A/F 5-17 (SOURCE: BHT-427-MM) Mos 03-May-2023 12 +30d (03-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 600 +10% (2,651.3) 557.5 Hrs (+60) Ldg 531000 Inspect Tailboom Assembly RE 04-00-00, Inspection Time Limits ≈01-Aug-2024 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-4 for inspection details. Contact Product Support Engineering for changes or modifications to the structure in area where a mandatory airworthiness inspection is specified.) Mos Hrs 2,051.3 300 +10% 2,351.3 257.5 Hrs (+30) Ldg 531000-0101 Tailboom Assembly RE (O/C) On Condition 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) Mos 21-Oct-2000 Hrs 0 Ldg 0 531100 Inspect Tailboom Horizontal Stabilizer Cutout RE 04-00-00, Inspection Time Limits ≈01-Mar-2024 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-2 for inspection details.) Mos Hrs 2,051.3 150 +10% 2,201.3 107.5 Hrs (+15) Ldg 532000 Inspect Tailboom Assembly RE (N/A) 04-00-00, Inspection Time Limits 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-4 for inspection details. Contact Product Support Engineering for changes or modifications to the structure in area where a mandatory airworthiness inspection is specified.) Mos Hrs Ldg 532100 Inspect Tailboom Horizontal Stabilizer Cutout RE (N/A) 04-00-00, Inspection Time Limits 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-2 for inspection details.) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 24/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 533100 Inspect Vertical Fin Assembly RE 04-00-00, Inspection Time Limits ≈12-Jan-2024 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) (NOTE: This inspection only applies to vertical fin assemblies in service with 1500 flight hours or more, or with total time unknown. Refer to Figure 4-6 for inspection details.) Mos Hrs 2,051.3 100 +10% 2,151.3 57.5 Hrs (+10) Ldg 533100-0101 Vertical Fin Assembly RE (O/C) On Condition 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) Mos 21-Oct-2000 Hrs 0 Ldg 0 533200 Inspect Intercostal RE 04-00-00, Inspection Time Limits ≈01-Mar-2024 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-3 for inspection details. Contact Product Support Engineering for changes or modifications to the structure in area where a mandatory airworthiness inspection is specified.) Mos Hrs 2,051.3 150 +10% 2,201.3 107.5 Hrs (+15) Ldg 533200-0101 Intercostal RE (O/C) On Condition 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) Mos 21-Oct-2000 Hrs 0 Ldg 0 533300 Inspect Longeron / Upper Aft LH Fuselage RE 04-00-00, Inspection Time Limits ≈01-Mar-2024 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-3 for inspection details. Contact Product Support Engineering for changes or modifications to the structure in area where a mandatory airworthiness inspection is specified.) Mos Hrs 2,051.3 150 +10% 2,201.3 107.5 Hrs (+15) Ldg 533300-0101 Longeron RE (O/C) On Condition 53 A/F Unknown Unknown (SOURCE: BHT-427-MM) Mos 21-Oct-2000 Hrs 0 Ldg 0 5-42-006 After Initial Installation - Tailboom Attachment hardware Torque Check RE (A/R) 5-00-00, Special Inspections 53 A/F (SOURCE: BHT-427-MM) (NOTE: Torque check must be repeated every 1 to 5 hours until torque is stabilized.) Mos Hrs Ldg 5-42-008 After Initial Installation - Vertical Fin Attachment Hardware Torque Check RE (A/R) 5-00-00, Special Inspections 53 A/F (SOURCE: BHT-427-MM) (NOTE: Torque check must be repeated every 1 to 5 hours until torque is stabilized.) Mos Hrs Ldg ASB 427-01-1 Auxiliary Fin Upper Tuning Weight 407-023-003-145, Relocation of RE (-) Alert Service Bulletin 53 A/F Eff: 19-Apr-2001 Complied With PCW logbook #1 Mos 30-Apr-2001 Hrs Ldg ASB 427-01-7 Auxiliary Fin P/N 427-035-836-101/-102/-105 and -106, Height Reduction of RE (-) Alert Service Bulletin 53 A/F Eff: 16-Nov-2001 Complied With PCW logbook#1 Mos 03-Jul-2002 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 25/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ASB 427-06-15 Rev A Vertical Fin to Tail Rotor Gearbox Support Attachment Hardware Replacement of RE (-) Alert Service Bulletin 53 A/F Eff: 18-Dec-2009 Complied With PCW logbook #4 Mos 17-Feb-2010 Hrs 1,014.4 Ldg ASB 427-06-15 Rev A Part 1 Vertical Fin to Tail Rotor Gearbox Support Attachment Hardware Replacement of RE (-) Alert Service Bulletin 53 A/F Eff: 18-Dec-2009 Complied With PCW logbook #4 Mos 17-Feb-2010 Hrs 1,014.4 Ldg ASB 427-06-15 Rev A Part 2 Vertical Fin to Tail Rotor Gearbox Support Attachment Hardware Replacement of RE (-) Alert Service Bulletin 53 A/F Eff: 18-Dec-2009 Complied With PCW logbook #4 Mos 17-Feb-2010 Hrs 1,014.4 Ldg ASB 427-09-25 Staked Bearings, One Time Inspection of RE (-) Alert Service Bulletin 53 A/F Eff: 07-Apr-2009 Complied With Found PCW Days 28-Apr-2009 Hrs 939.9 Ldg ASB 427-10-31 Tailboom Attachment Hardware, Replacement of RE (-) 53 A/F Complied With Found PCW Days 09-Apr-2010 Hrs 1,034.7 Ldg ASB 427-15-38 Rev A Vertical Fin 427-035-840-105 and 427-035-840-109, Inspection of RE (-) Alert Service Bulletin 53 A/F Eff: 14-Nov-2016 Complied With Found PCW Mos 26-Apr-2023 Hrs 2,051.3 Ldg ASB 427-15-38 Rev A Part 1 Vertical Fin 427-035-840-105 and 427-035-840-109, Inspection of RE (-) Alert Service Bulletin 53 A/F Eff: 14-Nov-2016 Complied With Found PCW Days 26-Apr-2023 Hrs 2,051.3 Ldg ASB 427-15-38 Rev A Part 2 Vertical Fin 427-035-840-105 and 427-035-840-109, Inspection of RE Alert Service Bulletin ≈12-Jan-2024 53 A/F Eff: 14-Nov-2016 Complied With Recurring Mos 26-Apr-2023 Hrs 2,051.3 100 2,151.3 57.5 Hrs Ldg TB 427-07-23 Tailboom Assembly P/N: 427-034-801-ALL, Configuration Check RE (-) Optional, Technical Bulletin 53 A/F Eff: 27-Feb-2007 (NOTE: Model 427 helicopters serial number 56060 and subsequent will have the intent of this bulletin accomplished prior to delivery) Mos Hrs Ldg TB 427-11-31 Input Driveshaft P/N 206-340-300-105. Removal of Airworthiness Limitation and Introduction of Overhaul Requirement T (A/R) Technical Bulletin 53 A/F Eff: 02-Jun-2011 Mos Hrs Ldg TB 427-11-32 Transmission Beam Pylon Mount Holes, Inspection of RE (-) Technical Bulletin 53 A/F Eff: 08-Jun-2011 (NOTE: Serial numbers 56066 and 56068 and subsequent with 58003 and subsequent will have the intent of this bulletin accomplished prior to delivery.) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 26/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining TB 427-14-33 Rotor Brake Limit Switch P/N D0413-1, Introduction of T (A/R) Optional 53 A/F Eff: 21-Aug-2014 Mos Hrs Ldg ▼ 55 - STABILIZERS 2009-15-15 Vertical Stabilizer, Attach Fittings - Inspect/ Repair/ Replace RE (-) Mandatory 55 A/F Eff: 08-Sep-2009 Complied With Found PCW Bell logbook #4. Replaced hardware. Mos 17-Feb-2010 Hrs 1,014.4 Ldg 2009-15-15 Par. 2(e)(1)(2) Vertical Stabilizer, Attach Fittings - Inspect RE (-) Mandatory 55 A/F Eff: 08-Sep-2009 Complied With Found PCW Bell logbook #4. Replaced hardware. Mos 17-Feb-2010 Hrs 1,014.4 Ldg 2009-15-15 Par. 2(f)(g) Vertical Stabilizer, Attach Fittings - Repair/ Replace RE (-) Mandatory 55 A/F Eff: 08-Sep-2009 Complied With Found PCW Bell logbook #4. Replaced hardware. Mos 17-Feb-2010 Hrs 1,014.4 Ldg 2019-23-09 Empennage Structure - Vertical Fin, P/N 427-035-840-105 or P/N 427-035-840-109 - Inspection RE Mandatory ≈12-Jan-2024 55 A/F Eff: 10-Jan-2020 Complied With (NOTE: COMPLIANCE: Within 25 hours, time-in-service (TIS) and thereafter at intervals not to exceed 100 hours TIS.) Mos Hrs 2,051.3 100 2,151.3 57.5 Hrs Ldg ▼ 56 - WINDOWS IL GEN-15-133 Clearfix Aerospace Acrylic Plastic Window Restoration RE (-) Information Letter 56 A/F Eff: 11-May-2015 Mos Hrs Ldg IL GEN-15-133 Rev A Clearfix Aerospace Acrylic Plastic Window Restoration T (A/R) Information Letter 56 A/F Eff: 24-Sep-2020 Mos Hrs Ldg ▼ 62 - ROTOR/S 2007-19-52 Emergency AD - To Prevent Loss of the Blade Tip Weight Loss of the Blade and Subsequnet Loss of Control RE (-) Mandatory 62 A/F Eff: 20-Nov-2007 Mos Hrs Ldg 2009-22-11 Swashplate link assembly bearing RE (-) Mandatory 62 A/F Eff: 16-Nov-2009 Complied With Found PCW Mos 16-Feb-2010 Hrs 1,014.4 Ldg 5-15-012 Clean the main rotor blades with a cloth wet with aliphatic naphtha (C-305) or drycleaning solvent (C-304), as an alternate, cleaning compound (C-318) or detergent (C-355) may be used. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 62 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 27/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-15-013 Examine the main rotor blades for condition and security. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 62 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-15-014 Protect the blades from corrosion by applying preservative oil (C-125) to the top and bottom leading edge surfaces of the main rotor blade leading edge. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 62 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-15-015 Examine the main rotor yoke assembly flexures for condition. RE 5-00-00, Scheduled Inspections ≈22-Nov-2023 62 A/F 5-15 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 50 +10% (2,101.3) 7.5 Hrs (+5) Ldg 5-16-016 Examine the main rotor hub assembly for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-017 Examine the main rotor yoke for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-018 Examine the upper and lower hub plates condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-019 Examine the mast nut for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-020 Examine the main rotor blade grips for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-021 Examine the pitch horns for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-022 Examine the up and down stops for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 28/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-16-023 Examine the elastomeric shear bearings for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-024 Examine the elastomeric lead lag bearings for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-025 Examine the elastomeric dampers for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-026 Examine the nose Frahm assembly for condition and security. Ensure that the coil springs are not damaged. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-027 Examine the forward fuel cell Frahm assembly for condition and security. Ensure that the coil springs are not damaged. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-029 Examine the swashplate assembly for corrosion, damage, condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-030 Examine the swashplate assembly for signs of too much grease leakage from the internal seals. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-031 Examine the swashplate assembly boot for tears and condition. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 62 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-34-001 MAIN ROTOR BLADE - Perform detailed visual inspection for evidence of skin cracks or crazing. RE 5-00-00, Component Maintenance Req. ≈15-Apr-2024 62 A/F 5-34 (SOURCE: BHT-427-MM) Mos Hrs 1,945.4 300 +10% (2,245.4) 151.6 Hrs (+30) Ldg 5-34-002 SWASHPLATE CONTROLS - Examine the swashplate assembly and rotating controls. RE 5-00-00, Component Maintenance Req. ≈15-Apr-2024 62 A/F 5-34 (SOURCE: BHT-427-MM) Mos Hrs 1,945.4 300 +10% (2,245.4) 151.6 Hrs (+30) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 29/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-42-001 After Initial Installation - Main Rotor Hub Mast Nut Torque Check RE (A/R) 5-00-00, Special Inspections 62 A/F (SOURCE: BHT-427-MM) (NOTE: Torque check must be repeated every 1 to 5 hours until torque is stabilized.) Mos Hrs Ldg 5-42-002 After Initial Installation - Main Rotor Hub through Bolt Torque Check RE (A/R) 5-00-00, Special Inspections 62 A/F (SOURCE: BHT-427-MM) (NOTE: Torque check must be repeated every 1 to 5 hours until torque is stabilized.) Mos Hrs Ldg 5-42-003 After Initial Installation - Main Rotor Hub Lower Cone Bolt Torque Check RE (A/R) 5-00-00, Special Inspections 62 A/F (SOURCE: BHT-427-MM) (NOTE: Torque check must be repeated every 1 to 5 hours until torque is stabilized.) Mos Hrs Ldg 5-42-007 After Initial Installation - Swashplate Tilt Friction RE (A/R) 5-00-00, Special Inspections 62 A/F (SOURCE: BHT-427-MM) (NOTE: Torque check must be repeated every 10 to 25 hours until torque is stabilized.) Mos Hrs Ldg 621000-0101 Grip RE 04-00-00, Life Limit ≈17-Apr-2026 62 A/F Red 406-010-108-135 TI 1662 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 1,467.6 1,500 2,967.6 873.8 Hrs 0 Ldg 621000-0102 Grip RE 04-00-00, Life Limit ≈17-Apr-2026 62 A/F Orange 406-010-108-135 TI 1780 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 1,467.6 1,500 2,967.6 873.8 Hrs 0 Ldg 621000-0103 Grip RE 04-00-00, Life Limit ≈17-Apr-2026 62 A/F Blue 406-010-108-135 TI 1838 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 1,467.6 1,500 2,967.6 873.8 Hrs 0 Ldg 621000-0104 Grip RE 04-00-00, Life Limit ≈17-Apr-2026 62 A/F Green 406-010-108-135 TI 1861 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 1,467.6 1,500 2,967.6 873.8 Hrs 0 Ldg 622000-0101 Upper Plate Assembly RE 04-00-00, Life Limit ≈31-Dec-2024 62 A/F 406-010-115-123 A-1385 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 2,500 2,500 406.2 Hrs 0 Ldg 0 622000-0102 Lower Plate Assembly RE 04-00-00, Life Limit ≈31-Dec-2024 62 A/F 406-010-117-121 A-1614 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 2,500 2,500 406.2 Hrs 0 Ldg 0 623000-0101 Main Rotor Blade RE (O/C) On Condition 62 A/F Red 427-015-001-135 A-624 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 30/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 623000-0102 Main Rotor Blade RE (O/C) On Condition 62 A/F Orange 427-015-001-135 A-633 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 623000-0103 Main Rotor Blade RE (O/C) On Condition 62 A/F Blue 427-015-001-135 A628 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 623000-0104 Main Rotor Blade RE (O/C) On Condition 62 A/F Green 427-015-001-135 A-629 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 623500-0101 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Red - Fwd 406-010-120-105 A-FS6392 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 623500-0102 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Orange - Fwd 406-010-120-105 A-FS6079 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 623500-0103 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Blue - Fwd 406-010-120-105 A-FS6344 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 623500-0104 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Green - Fwd 406-010-120-105 A-FS6364 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 623500-0201 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Red - Aft 406-010-120-105 A-FS6369 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 623500-0202 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Orange - Aft 406-010-120-105 A-FS6350 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 623500-0203 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Blue - Aft 406-010-120-105 A-FS6383 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 31/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 623500-0204 Main Rotor Blade Bolt RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F Green - Aft 406-010-120-105 A-FS6417 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 623550-0101 Expandable Blade Bolt RE (O/C) 04-00-00, Life Limit 62 A/F Red Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 623550-0102 Expandable Blade Bolt RE (O/C) 04-00-00, Life Limit 62 A/F Orange Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 623550-0103 Expandable Blade Bolt RE (O/C) 04-00-00, Life Limit 62 A/F Blue Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 623550-0104 Expandable Blade Bolt RE (O/C) 04-00-00, Life Limit 62 A/F Green Unknown Unknown (SOURCE: BHT-427-MM) Mos Hrs Ldg 624000-0101 Pitch Horn RE 04-00-00, Life Limit ≈31-Dec-2024 62 A/F Red 407-010-103-105 A-2016 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 2,500 2,500 406.2 Hrs 0 Ldg 0 624000-0102 Pitch Horn RE 04-00-00, Life Limit ≈27-Jan-2029 62 A/F Orange 407-010-103-115 RE54 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 1,467.6 2,500 3,967.6 1,873.8 Hrs 0 Ldg 624000-0103 Pitch Horn RE 04-00-00, Life Limit ≈31-Dec-2024 62 A/F Blue 407-010-103-105 RE184 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 2,500 2,500 406.2 Hrs 0 Ldg 0 624000-0104 Pitch Horn RE 04-00-00, Life Limit ≈31-Dec-2024 62 A/F Green 407-010-103-105 RE162 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 2,500 2,500 406.2 Hrs 0 Ldg 0 625000-0101 Main Rotor Blade Hub Shear Bearing RE 04-00-00, Life Limit ≈08-Feb-2047 62 A/F Red 407-301-101-103 7594 New (SOURCE: BHT-427-MM) Mos 06-Sep-2021 0 Hrs 464.1 10,000 10,464.1 8,370.3 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 32/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 625000-0102 Main Rotor Blade Hub Shear Bearing RE 04-00-00, Life Limit ≈08-Feb-2047 62 A/F Orange 407-301-101-103 7629 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 464.1 10,000 10,464.1 8,370.3 Hrs 0 Ldg 625000-0103 Main Rotor Blade Hub Shear Bearing RE 04-00-00, Life Limit ≈08-Feb-2047 62 A/F Blue 407-301-101-103 7667 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 464.1 10,000 10,464.1 8,370.3 Hrs 0 Ldg 625000-0104 Main Rotor Blade Hub Shear Bearing RE 04-00-00, Life Limit ≈06-Mar-2048 62 A/F Green 407-301-101-103 LK9503 New (SOURCE: BHT-427-MM) 0 Mos 06-Sep-2021 0 Hrs 852.4 10,000 10,852.4 8,758.6 Hrs 0 Ldg 626000-0101 Lower Cone Seat RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F 427-010-103-105 A-137 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 627000-0101 Drive Ring Set RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F 427-010-105-101 A-54 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628000-0101 Swashplate Drive Assembly Drive Link RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.1 427-010-410-101 TI-48 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628000-0102 Swashplate Drive Assembly Drive Link RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.2 427-010-410-101 TI-51 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628100-0101 Swashplate Drive Assembly Drive Lever RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.1 427-010-408-101 TI-79 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628100-0102 Swashplate Drive Assembly Drive Lever RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.2 427-010-408-101 TI-86 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628200-0101 Swashplate Drive Assembly Bearing and Liner Assembly RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.1 406-010-417-109 A-2402 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 33/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 628200-0102 Swashplate Drive Assembly Bearing and Liner Assembly RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.2 406-010-417-109 A-2408 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628300-0101 Swashplate Drive Assembly Inner Ring RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F 406-010-410-125 A-1686 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628400-0101 Swashplate Drive Assembly Cap Assembly RE 04-00-00, Life Limit ≈31-Dec-2024 62 A/F 406-010-419-117 A-2 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 2,500 2,500 406.2 Hrs 0 Ldg 0 628500-0101 Swashplate Drive Assembly Anti-drive Lever RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F 427-010-418-105 A-68 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 628600-0101 Swashplate Drive Assembly Anti-drive Link RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F 406-010-432-101 A-FS119 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628700-0101 Swashplate Drive Assembly Swashplate Support RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F 427-010-405-101 A-26 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 628800-0101 Swashplate Drive Assembly Swashplate Sleeve RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F 427-010-403-101 A-59 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 628900-0101 Swashplate Drive Assembly Collective Lever RE 04-00-00, Life Limit ≈25-Oct-2045 62 A/F 427-010-407-101 A-47 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 628950-0101 Swashplate Drive Assembly Collective Lever Pin RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.1 206-010-408-103 MW21 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 628950-0102 Swashplate Drive Assembly Collective Lever Pin RE 04-00-00, Life Limit ≈09-Dec-2031 62 A/F No.2 206-010-408-103 MW6 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 34/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 629100 Inspect Main Rotor Yoke Assembly RE 04-00-00, Inspection Time Limits ≈04-Jan-2024 62 A/F 407-101-101-100 A-1185 (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-1 for inspection details.) Mos 04-Nov-2023 Hrs 2,092.8 50 +10% 2,142.8 49 Hrs (+5) Ldg 4,362 629100-0101 Main Rotor Yoke Assembly RE (O/C) On Condition 62 A/F 407-101-101-100 A-1185 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 629150-0101 Swashplate and Support Assembly RE (O/C) On Condition 62 A/F 427-010-401-101 A-34 Overhauled (SOURCE: BHT-427-MM) Mos 06-Sep-2021 Hrs Ldg 629150-0101-OH OVERHAUL - Swashplate and Support Assembly RE 5-00-00, Overhaul ≈31-Dec-2024 62 A/F 427-010-401-101 A-34 (SOURCE: BHT-427-MM) Mos 06-Sep-2021 0 Hrs 0 2,500 +100 2,500 406.2 Hrs (+100) Ldg 629200-0101 Main Rotor Hub Assembly RE (O/C) On Condition 62 A/F 427-010-100-103 A-41 Overhauled (SOURCE: BHT-427-MM) Mos 06-Sep-2021 852.4 852.4 Hrs 852.4 Ldg 629200-0101-OH OVERHAUL - Main Rotor Hub Assembly RE 5-00-00, Overhaul ≈31-Dec-2024 62 A/F 427-010-100-103 A-41 (SOURCE: BHT-427-MM) Mos 06-Sep-2021 852.4 Hrs 852.4 2,500 +100 2,500 406.2 Hrs (+100) Ldg 629201 Inspect Main Rotor Blade RE (N/A) 04-00-00, Inspection Time Limits 62 A/F Red 427-015-001-135 A-624 (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-5 for inspection details.) Mos Hrs Ldg 629202 Inspect Main Rotor Blade RE (N/A) 04-00-00, Inspection Time Limits 62 A/F Orange 427-015-001-135 A-633 (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-5 for inspection details.) Mos Hrs Ldg 629203 Inspect Main Rotor Blade RE (N/A) 04-00-00, Inspection Time Limits 62 A/F Blue 427-015-001-135 A628 (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-5 for inspection details.) Mos Hrs Ldg 629204 Inspect Main Rotor Blade RE (N/A) 04-00-00, Inspection Time Limits 62 A/F Green 427-015-001-135 A-629 (SOURCE: BHT-427-MM) (NOTE: Refer to Figure 4-5 for inspection details.) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 35/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 62-CUS-01 Perform 50 Hour Main Rotor Blade Sta 197 Visual RE ≈22-Nov-2023 62 A/F Mos Hrs 2,051.3 50 2,101.3 7.5 Hrs Ldg 62-CUS-02 Perform 100 Hour Main Rotor Blade Sta 197 Visual Inspection RE ≈12-Jan-2024 62 A/F Mos Hrs 2,051.3 100 2,151.3 57.5 Hrs Ldg ASB 427-17-41 Main Rotor Expandable Blade Bolt 406-310-103-101/-103, Inspection of RE (-) Alert Service Bulletin 62 A/F Eff: 05-Aug-2016 Not Applicable Not installed Mos 18-Apr-2022 Hrs 1,974.5 Ldg ASB 427-17-41 Part 1 Main Rotor Expandable Blade Bolt 406-310-103-101/-103, Inspection of RE (-) Alert Service Bulletin 62 A/F Eff: 05-Aug-2016 Not Applicable Not installed Mos 18-Apr-2022 Hrs 1,974.5 Ldg ASB 427-17-41 Part 2 Main Rotor Expandable Blade Bolt 406-310-103-101/-103, Inspection of RE (-) Alert Service Bulletin 62 A/F Eff: 05-Aug-2016 Not Applicable Not installed Mos 18-Apr-2022 Hrs 1,974.5 Ldg ASB 427-21-45 Inspection and Application of Torque Seal Lacquer Main Rotor Pitch Link Assembly 406-010- 413-125/-141 RE (-) Alert Service Bulletin 62 A/F Eff: 08-Feb-2021 Complied With Mos 26-Apr-2023 Hrs 2,051.3 Ldg ASB 427-21-45 Part I Inspection and Application of Torque Seal Lacquer Main Rotor Pitch Link Assembly 406-010- 413-125/-141 - One-Time Inspection and Application of Torque Seal Lacquer RE (-) Alert Service Bulletin 62 A/F Eff: 08-Feb-2021 Complied With (AVG MAN HRS: 1) Mos 26-Apr-2023 Hrs 2,051.3 Ldg ASB 427-21-45 Part II Inspection and Application of Torque Seal Lacquer Main Rotor Pitch Link Assembly 406-010- 413-125/-141 - Recurring Inspection RE Alert Service Bulletin 62 A/F Complied With (AVG MAN HRS: 0.25) (NOTE: COMPLIANCE: Within 300 flight hours or 12 months whichever comes first after accomplishment of PART I and every 300 flight hours or 12 months thereafter.) Mos 26-Apr-2023 12 26-Apr-2024 4.3 Months Hrs 2,051.3 300 2,351.3 257.5 Hrs Ldg GEN-17-49 Main Rotor Pitch Link Assembly T (A/R) Operation Safety Notice 62 A/F Eff: 12-Oct-2017 Mos Hrs Ldg TB 427-02-05 Main Rotor Blade Abrasion Strip, Rework of T (A/R) Recommended, Technical Bulletin 62 A/F Eff: 24-May-2002 Mos Hrs Ldg TB 427-10-29 New Main Rotor Blades 427-015-001-133, /-135, Product Balance Adjustment Capability, Introduction of RE (-) Optional, Technical Bulletin 62 A/F Eff: 11-Feb-2010 (NOTE: Model 427 helicopters serial number 56042 and subsequent will have the intent of this bulletin accomplished prior to delivery.) Mos Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 36/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining ▼ 63 - ROTOR DRIVE/S 2015-17-02 Main Rotor Drive System - To Prevent Failure of a Driveshaft, Loss of Drive to the Main Rotor System, and a Subsequent Emergency Landing. (This AD Supersedes AD 2001-13-51) RE (-) Mandatory 63 A/F Driveshafts Never installed on Bell 407 (AVG MAN HRS: 3.25) Mos 14-Sep-2015 Hrs 1,552.5 Ldg 5-16-028 Examine the mast assembly for condition, mechanical damage and cleanliness. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-036 Examine the transmission assembly for correct fluid level, leaks, corrosion and mechanical damage. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-037 Examine the three transmission chip detectors for metal particles. Examine the electrical circuits for continuity. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-038 Examine the filter for impending bypass indication. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-039 Examine the fluid flexible hoses (shrouded and non-shrouded areas) and rigid lines for condition, security and leaks. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-040 Examine the transmission oil cooling system for condition, leaks and security. Ensure that the cooler is clean and free of any obstruction. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-041 Examine the pylon beam assemblies for corrosion and damage. Inspect for proper installation and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-042 Examine the left and right pylon vertical LIVE mounts for proper servicing, corrosion and damage. Inspect for proper installation and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-043 Examine both left and right pylon pitch restraint spring assemblies for condition, corrosion and damage. Inspect for proper installation and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 37/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 5-16-044 Examine the pylon adapters for condition, corrosion and damage. Inspect for proper installation and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-045 Examine the driveshaft assemblies for condition and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-046 Examine the driveshaft tubes for corrosion and surface damage. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-047 Examine the flexframe adapters and bolts for condition and signs of fretting or cracking. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-048 Examine the transmission oil cooler for obstruction, cleanliness, condition and oil leaks. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-16-049 Examine the oil filter assembly and oil lines for leaks, corrosion, rubbing and wear. Inspect for proper installation and security. RE 5-00-00, Scheduled Inspections ≈01-Mar-2024 63 A/F 5-16 (SOURCE: BHT-427-MM) Mos 02-May-2023 12 +30d (02-May-2024) 4.5 Months (+31 Days) Hrs 2,051.3 150 +10% (2,201.3) 107.5 Hrs (+15) Ldg 5-36-004 600 Hour Mast Assembly Inspection RE 5-00-00, Component Maintenance Req. ≈15-Aug-2024 63 A/F 5-36 427-040-011-101 56016 (SOURCE: BHT-427-MM) Mos Hrs 1,764.9 600 +10% (2,364.9) 271.1 Hrs (+60) Ldg 5-36-005 RELAY BOXES 4270WA4 AND 4270WA5 Inspection RE 5-00-00, Component Maintenance Req. ≈15-Aug-2024 63 A/F 5-36 (SOURCE: BHT-427-MM) Mos Hrs 1,764.9 600 +10% (2,364.9) 271.1 Hrs (+60) Ldg 5-39-001 24 Month Main Rotor Mast Inspection RE 5-00-00, Component Maintenance Req. 63 A/F 5-39 427-040-040-101 a79 (SOURCE: BHT-427-MM) Mos 03-Oct-2022 24 +30d (03-Oct-2024) 9.6 Months (+30 Days) Hrs Ldg 631000-0101 Main Rotor Mast RE 04-00-00, Life Limit ≈01-Jan-2037 63 A/F 427-040-040-101 a79 New (SOURCE: BHT-427-MM) Mos 13-Feb-2019 0 Hrs 1,824.3 5,000 6,824.3 4,730.5 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 38/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 632000-0101 Pylon Support Structure Beam Assembly RE 04-00-00, Life Limit ≈09-Dec-2031 63 A/F Left 427-010-201-107 T1100 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 632000-0102 Pylon Support Structure Beam Assembly RE 04-00-00, Life Limit ≈09-Dec-2031 63 A/F Right 427-010-201-108 T186 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 5,000 5,000 2,906.2 Hrs 0 Ldg 0 632100-0101 Pylon Support Structure Pitch Restraint Spring RE 04-00-00, Life Limit ≈25-Oct-2045 63 A/F Left 427-010-204-101 LK-0123 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 632100-0102 Pylon Support Structure Pitch Restraint Spring RE 04-00-00, Life Limit ≈25-Oct-2045 63 A/F Right 427-010-204-101 LK-0133 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 10,000 10,000 7,906.2 Hrs 0 Ldg 0 632200-0101 Pylon Support Structure Stop Fitting Assembly RE 04-00-00, Life Limit ≈31-Dec-2024 63 A/F Left 427-010-207-101 RE16 New (SOURCE: BHT-427-MM) Mos 06-Sep-2021 0 Hrs 0 2,500 2,500 406.2 Hrs Ldg 632200-0102 Pylon Support Structure Stop Fitting Assembly RE 04-00-00, Life Limit ≈12-Dec-2027 63 A/F Right 427-010-209-101 RD7191 New (APX COST: 7,836.55) (SOURCE: BHT-427-MM) Mos 23-Aug-2023 0 Hrs 2,061.6 1,500 3,561.6 1,467.8 Hrs Ldg 4,224 633100-0101 Input Driveshaft RE (O/C) On Condition 63 A/F Left 206-340-300-105 KC1594 Overhauled (APX COST: 9,995) (SOURCE: BHT-427-MM) Mos 27-Oct-2023 Hrs 2,082.7 Ldg 4,319 633100-0101-OH OVERHAUL - Input Driveshaft RE 5-00-00, Overhaul ≈12-Oct-2030 63 A/F Left 206-340-300-105 KC1594 (SOURCE: BHT-427-MM) (NOTE: Input driveshaft 206-340-300-105 must be overhauled at 5000 hours of operation and every 2500 hours of operation thereafter. Overhaul is to be accomplished by Kamatics Corporation only. Return driveshaft to Bell Helicopter Textron (BHT) per Information Letter (IL) GEN-04-98.) Mos 27-Oct-2023 Hrs 2,082.7 2,500 +100 4,582.7 2,488.9 Hrs (+100) Ldg 4,319 633100-0102 Input Driveshaft RE (O/C) On Condition 63 A/F Right 206-340-300-105 KC 871 New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 633100-0102-OH OVERHAUL - Input Driveshaft T 5-00-00, Overhaul ≈09-Dec-2031 63 A/F Right 206-340-300-105 KC 871 (SOURCE: BHT-427-MM) (NOTE: Input driveshaft 206-340-300-105 must be overhauled at 5000 hours of operation and every 2500 hours of operation thereafter. Overhaul is to be accomplished by Kamatics Corporation only. Return driveshaft to Bell Helicopter Textron (BHT) per Information Letter (IL) GEN-04-98.) Mos Hrs 5,000 +100 5,000 2,906.2 Hrs (+100) Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 39/146 Generated: 20-Dec-2023 3:50 PM N427PG STATUS REPORT BELL HELICOPTER TEXTRON CANADA LIMITED Owner/Operator: Helicopter Flight Services, Inc Bell 427 N427PG,SN 56019 Task No Description Categories Time SEQ PN/SN MOC Note or Component Condition TSNI TSOI TSRI TSI CW REQ TOL DUE Remaining 634100-0101 Transmission Assembly RE (O/C) 5-00-00, Overhaul 63 A/F 427-040-006-117 A-40 Overhauled (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 634100-0101-OH OVERHAUL - Transmission Assembly RE 5-00-00, Overhaul ≈09-Dec-2031 63 A/F 427-040-006-117 A-40 (SOURCE: BHT-427-MM) (NOTE: It is recommended to replace the left hand and right hand input clutches 406-040-580-103, clutch roller bearings 406-040-530-103, and clutch ball bearings 427-340-110-101 (or subsequent dash numbers), during the 5000 hour transmission assembly overhaul.) Mos Hrs 5,000 +100 5,000 2,906.2 Hrs (+100) Ldg 634200-0101 Transmission Mast Assembly RE (O/C) On Condition 63 A/F 427-040-011-101 56016 Overhauled (SOURCE: BHT-427-MM) Mos 13-Feb-2019 1,035.6 1,035.6 Hrs 1,035.6 Ldg 634200-0101-OH OVERHAUL - Transmission Mast Assembly RE 5-00-00, Overhaul ≈20-May-2026 63 A/F 427-040-011-101 56016 (SOURCE: BHT-427-MM) Mos 13-Feb-2019 1,035.6 Hrs 1,035.6 3,000 +100 3,000 906.2 Hrs (+100) Ldg 634300-0101 Fan Shaft Assembly RE (O/C) On Condition 63 A/F 427-044-200-105 Unknown New (SOURCE: BHT-427-MM) 0 Mos 21-Oct-2000 0 Hrs 0 0 Ldg 0 634300-0101-OH OVERHAUL - Fan Shaft Assembly RE 5-00-00, Overhaul ≈20-May-2026 63 A/F 427-044-200-105 Unknown (SOURCE: BHT-427-MM) (NOTE: Fan shaft assemblies 407-044-200-105/-107 and subsequent require a complete overhaul including bearing replacement only upon reaching 3000 hours of operation. Bearings 407-340-339-101 and subsequent must be replaced upon reaching 3 years of service, regardless of the number of hours flown. Bearing replacement may be accomplished without performing the complete overhaul procedure of the fan shaft assembly.) Mos Hrs 3,000 +100 3,000 906.2 Hrs (+100) Ldg 634310-0101 Fan Shaft Assembly - Bearings RE (O/C) On Condition 63 A/F Fwd 407-340-339-107 ZS-32415 New (SOURCE: BHT-427-MM) 0 Mos 06-Apr-2021 Hrs Ldg 634310-0101-OH OVERHAUL - Fan Shaft Assembly - Bearings RE 5-00-00, Overhaul 63 A/F Fwd 407-340-339-107 ZS-32415 (SOURCE: BHT-427-MM) (NOTE: Fan shaft assemblies 407-044-200-105/-107 and subsequent require a complete overhaul including bearing replacement only upon reaching 3000 hours of operation. Bearings 407-340-339-101 and subsequent must be replaced upon reaching 3 years of service, regardless of the number of hours flown. Bearing replacement may be accomplished without performing the complete overhaul procedure of the fan shaft assembly.) Yrs 06-Apr-2021 3 +30d 06-Apr-2024 3.6 Months (+30 Days) Hrs Ldg 634310-0102 Fan Shaft Assembly - Bearings RE (O/C) On Condition 63 A/F Aft 407-340-339-107 ZS-32431 New (SOURCE: BHT-427-MM) 0 Mos 06-Apr-2021 Hrs Ldg [ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance 40/146 Generated: 20-Dec-2023 3:50 PM

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