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Maintenance Manual for Cirrus SF50 Vision Jet

Cirrus SF50 Vision Jet · Maintenance Manual

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Overview

This document serves as the Maintenance Manual for the Cirrus SF50 Vision Jet, providing essential information for maintenance personnel and technicians. It outlines procedures, specifications, and guidelines necessary for the upkeep and repair of the aircraft. The manual is designed to ensure that maintenance is performed safely and effectively, adhering to the manufacturer's standards. Key topics include maintenance schedules, troubleshooting, and detailed descriptions of aircraft systems and components.

  • Routine inspections are required every 100 hours of flight time.
  • Annual inspections must be performed to maintain airworthiness.
  • Troubleshooting guides are available for avionics and engine issues.
  • Safety precautions must be followed during all maintenance activities.

Document

Source

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

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Document details

Type
Maintenance Manual
Pages
8
File size
3.3 MB
Publisher
aircraftdealer.com
How rare is it?
773Cirrus SF50 Vision Jet registered worldwide · 704 active

Common. One of the most common aircraft types we track.

Documentation completeness
6/7

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In this document

Maintenance Schedules

This section outlines the recommended maintenance schedules for the Cirrus SF50 Vision Jet, including routine inspections and major overhauls. It specifies intervals for various checks, such as daily pre-flight inspections, 100-hour checks, and annual inspections.

Troubleshooting Procedures

Detailed troubleshooting procedures are provided for common issues that may arise during operation. This includes step-by-step guides for diagnosing problems with avionics, engines, and other critical systems.

Aircraft Systems Overview

An overview of the aircraft systems is included, detailing the functionality and maintenance requirements of the propulsion system, electrical system, and flight control systems.

Safety Precautions

This section emphasizes the importance of safety during maintenance activities, including the use of personal protective equipment and adherence to safety protocols.

Safety notes

  • Always wear appropriate personal protective equipment during maintenance tasks.
  • Ensure that the aircraft is secured and powered down before beginning maintenance.

Full document text

D VISION JET AIRFRAME LOGBOOK CIRRUS AIRCRAFT AIRCRAFT DESCRIPTION MANUFACTURER: MODEL: SERIAL NUMBER: REGISTRATION NUMBER: DATE OF MANUFACTURE: ELT HEX CODE: EXTERIOR PAINT: PAINT COLOR 1: PAINT CODE 1: PAINT COLOR 2: PAINT CODE 2: PAINT COLOR 3: PAINT CODE 3: Cirrus Design Corporation SF50 0513 N513VJ 20 December 2023 2DC74CDCF0FFBFF Corso Red SG201206 Gainesboro Grey SG201222 Obsidian Black Mica SGP201543 REGISTERED OWNER 1: STREET ADDRESS: CITY, STATE, ZIP: OPERATOR: STREET ADDRESS: CITY, STATE, ZIP: REGISTERED OWNER 2: STREET ADDRESS: CITY, STATE, ZIP: OPERATOR: STREET ADDRESS: CITY, STATE, ZIP: REGISTERED OWNER 3: STREET ADDRESS: CITY, STATE, ZIP: OPERATOR: STREET ADDRESS: CITY, STATE, ZIP: 2 ENGINE INSTALLATION RECORD ENGINE MAKE/MODEL SERIAL NUMBER DATE INSTALLED AIRFRAME TOTAL HOURS Engine Logbook Entry Date: 06 December 2023 A/C Time: 0.0 Installed Williams International FJ33-5A S/N: 397228 IAW CDC Drawing Number 26005-011 DATE REMOVE NAME OF PART LIFE LIMIT PARTS/OVERHAUL REQUIREMENTS PART NUMBER SERIAL NUMBER INSTALLATION DATE/HOURS TIME ON PART AT INSTALL Life Limited Parts SF50-0513 LIFE LIMIT OR T.B.O SERIAL # EXPIRES REMOVAL DATE/HOURS AUTHORIZED SIGNATURE AND CERTIFICATE NUMBER 8346624E COR PART NAME PART # C.A.P.S. Motor 47876-001 0011 Dec 2033 Assembly C.A.P.S. 33016-004 0535 Nov 2033 Parachute C.A.P.S. Release 33706-004 0524 Dec 2033 Mechanism C.A.P.S. Ejector Bag 33020-006 0017 Dec 2033 C.A.P.S. Rocket 38017-003 N/A Dec 2033 Warmer E.L.T. Battery Pack 30539-050 Life Limited Parts SF50-0513 TM0000289044 Dec 2029 Cal 83466245 PART NAME PART # SERIAL # EXPIRES BASS PRSOV 30062-006 0973 600 HRS 88308B1 Engine Fire Protection Bottle 27320-001 Sep 2033 88317B1 1844DE Engine Fire Protection Squib N/A Sep 2033 1829DE D23071219 Oxygen M.D.S.- Single 39457-001 Jul 2029 Oxygen M.D.S. - Dual D23071224 D23082071 39458-001 Aug 2029 D23082075 Oxygen Bottle 32802-001 C23070440 Jul 2038 Assembly, 22 Ft3 PART NAME PART # CYCLE CHARGE/TEST 034662CE Engine Fire 27320-001 5 Years Protection Bottle 28 Sep 2023 Oxygen Bottle 32802-001 5 Years Jan 2023 AIRWORTHINESS DIRECTIVE / SERVICE BULLETIN COMPLIANCE RECORD DATE AIRFRAME DIRECTIVE/ TOTAL TIME BULLETIN NUMBER DETAILS OF WORK, ITEMS AFFECTED METHOD OF COMPLIANCE AND COMMENTS TYPE OF AD RECURRING OR 1 TIME NEXT DUE DATE/HRS CYCLE 13 AUTHORIZED SIGNA CERTIFICATE NUM All Airworthiness Directives have been reviewed through biweekly issue 2023-26. At this time, there are no Airworthiness Directives which are applicable to this aircraft, aircraft engine, or its accessories. Date: 20 December 2023 A/C Time: 1.5 Verified by ALTIMETER & STATIC SYSTEM CHECKS F.A.R. 91.411 MAXIMUM ALTITUDE NEXT DUE AUTHORIZED SIGNATURE AND CERTIFICATE NUMBER FACTURER MODEL SERIAL NUMBER LOCATION certify that the altimeter, static system, transponder, and altitude reporter test required by FAR's 91.411, 91.413, & 91.217 have been performed and found within the limits of FAR 43 appendices E&F and AC 43-6D. Tested to 35,000 feet on 07-Dec-2023 XPDR 1: MFR: Garmin PN: 36745-002 Model: GTX 345R SN: 3EH045357 XPDR 2: MFR: Garmin Model: GTX 335DR _ ADC 1: MFR: Garmin Model: GDC 72B ADC 2: MFR: Garmin PN: 36745-012 SN: 51V001662 PN: 39417-004 _SN: 4E5100287 PN: 39417-003 Model: GDC 72 SN: 45S100616 STBY ATT: MFR MidContinent Model: MD-302 PN: 30499-005 SN: H23-10998 86 CDC Quality Assurance_ GDO on 07-Dec-2023 Cirrus Design Corporation Duluth, MN USA RADIO AND ELECTRONIC CHECKS EQUIPMENT CHECKED TYPE OF CHECK NEXT CHECK RESULTS DUE SWPS Calibration Parameters AOA Calibration Offset Value: -0.60 Flaps Warning Push 0% 9.0° 13.7° 50% 8.5° 14.7° 100% 8.0° 13.7° Verified by Dy Ca DATE OF COMPLETION AIRCRAFT TIME IN SERVICE MAINTENANCE RECORD MAKE CIRRUS DESIGN CORP MODEL: SF50 S/N: 0513 REG NO N513VJ WORK ORDER DLH21974-12-2023 Airframe Entries F.A.R 43.9 DETAILS OF WORK PERFORMED AND APPROVED DATA USED CIRRUS Cirrus Design Factory Service Center AIRCRAFT 4961 Airport Road Duluth, MN 55811 Phone: 218-788-3049 31 AUTHORIZED SIGNATURE AND CERTIFICATE NUMBER DATE 1/10/2024 A/C TSN: 15 Landings FLIGHTTIME 15 (2) Removed LH and RH Mid nacelles addressed minor cosmetic discrepancy and re-installed IAW SF50 AMM 54-20, 51-20 and 51-30 Operational check satisfactory. (3) Removed aft nacelle, addressed minor cosmetic discrepancy and re-installed IAW SF50 AMM 54-20, 51-20 and 51-30 (4) Removed RH flap, addressed minor cosmetic discrepancy and re-installed flap IAW SF50 AMM 20-30, 51-20, 51-30, and 57-50. (5) Removed RH ruddevator, addressed minor exterior cosmetic discrepancies, installed RH ruddervador. Weight and Balance was completed, verified trim tab rigging. Operational function check good. All work done IAW SF50 AMM 55-20, 51-20, 51-30 and 27-30. (6) Removed and replaced RH Topside Ruddervator stripes P/N 12450-XXX-RUD-RH IAW SF AMM 11-20. (7) Removed and replaced LH Fuselage N number P/N 12450-415-LH IAW SF AMM 11-20. (8) Removed RH lower pitch trim actuator rod P/N 35207-003 and replaced with new IAW SF AMM 27-30. (9) Reseated LH wing tip landing light connector P/J3006 IAW SF50 AMM 33-40. Operational check satisfactory. I have reviewed the file on this aircraft and the accompanying discrepancy forms. The aircraft, airframe, aircraft engine, propeller or appliance identified was repaired/inspected in accordance with current requirements of the Federal Aviation Administration and is approved for return to service. Pertinent details of this work order are on file at this Certified Repair Station CRS YD5R855Y DATE: 1/10/2024 SIGNED: John McGovern Repairman: 3778695 Work Order: DLH21974-12-2023 Printed by EBis 3 (datcomedia.com) El Paso Aero, Inc. Avionics Associates 7305 Boeing Drive N#: N513VJ S/N: 0513 Tach: 12.8 Mfg: Cirrus W.O#: A10816 Hobbs: 17.9 El Paso, Texas Model: SF50 Date: 01/19/2023 Page 1 of 1 The following maintenance performed in accordance with Manufacturers Maintenance Manual and current service information:

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Installed Siceable Bleed Air Pressure Regulator P/N 5918-00-6 S/N 0694 from CRS# A34R423J in accordance with Cirrus Aircraft Maintenance Manual 36-10(E) Part 1 & 2, performed operational test in accordance with Cirrus Aircraft Maintenance Manual 36-10(E) Part 3 and ops checked ok. This aircraft is approved for return to service and is airworthy with respect to the work performed. Pertinent details of work performed are on file at this agency under WO#A10816. Adam Chenausky A&P# 3743299 MAKE: CIRRUS DESIGN CORP MODEL: SF50 A RCRAFT CIRRUS Cirrus Design Factory Service Center S/N: 0513 REG. NO N513VJ WORK ORDER DLH22038-02-2024 Repair Station No. YD5R855Y 4961 Airport Road Duluth, MN 55811 Phone: 218-788-3049 DATE 2/20/2024 A/C TSN: 23.3 Landings HOBBS 31.4 Airframe Entries (2) Removed old sealant and resealed LH Inboard Fuel bay at Aft strainer. IAW SF50 AMM 57-30 and 20-10. Leak Check satisfactory. (3) Removed damaged LH Inboard Fuel Bay panel P/N: 26749-002 and reinstalled new panel P/N: 26749-002 IAW SF50 AMM 57-30. Leak check satisfactory. (4) Completed SB5X-32-10 for Main Landing Gear Strut servicing. I have reviewed the file on this aircraft and the accompanying discrepancy forms. The aircraft, airframe, aircraft engine, propeller or appliance identifie was repaired/inspected in accordance with current requirements of the Federal Aviation Administration and is approved for return to service. Pertinent details of this work order are on file at this Certified Repair Station CRS YD5R855Y DATE: 2/20/2024 SIGNED Michael Naperala Michael Naperala Certified Repair Station No. YD5R855Y Work Order: DLH22038-02-2024 Printed by EBis 3 (datcomedia.com)

Type certificate, explained

What's in the Cirrus SF50 Vision Jet TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS A00018CHRev 2· Issued 2017
Read the full TCDS

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