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AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2

Gulfstream Aerospace G280 · Maintenance Manual

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Overview

The Airworthiness Limitations Section for the Gulfstream G280 outlines mandatory maintenance actions required to ensure the aircraft's continued airworthiness. It specifies inspection procedures and intervals for various structural components based on damage tolerance analysis and FAA regulations.

  • The G280 is limited to 10,000 flight cycles until certification fatigue testing is completed.
  • Mandatory inspections are based on flight cycles, not flight hours.
  • The document includes detailed inspection procedures for six major aircraft components.
  • Inspections must comply with life limits and maximum interval limits.
  • Early compliance with inspection intervals is allowed within specified limits.
  • The aircraft is not authorized for operations beyond 10,000 flights until further testing is approved.
  • Cracks detected during inspections must be reported immediately.
  • Alternative inspection programs may be established for non-standard operations.

Document

Source

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

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Document details

Type
·
Maintenance Manual
Year
·
2019
File size
·
668 KB
Publisher
·
regulations.gov
Language
·
en
About this document
What is the AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2?

The AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2 is a maintenance manual for the Gulfstream Aerospace G280, dated 2019.

Where does the AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2 come from?

This copy of the AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2 was originally published by regulations.gov and is hosted on Sprinkle as a free, searchable reference copy.

What year was the AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2 published?

The AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2 — the Gulfstream Aerospace G280 maintenance manual on file — is dated 2019.

Documentation completeness
2/7

Most owners only have the POH. Here's the essential set for the Gulfstream Aerospace G280.

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

More Gulfstream Aerospace G280manuals & documents

In this document

Introduction

The introduction outlines the airworthiness limitations and the need for compliance with FAA regulations until certification fatigue testing is completed.

Inspection Procedures

This section details the mandatory inspection procedures for major aircraft components, including the forward fuselage, center fuselage, aft fuselage, empennage, wing, and landing gears.

Inspection Intervals

Inspection intervals are specified based on flight cycles, with initial and repeat intervals clearly defined for each inspection point.

Reporting Cracks

Procedures for reporting detected cracks during inspections are outlined, emphasizing immediate notification to relevant authorities.

Limitations on Operations

The document specifies operational limitations, including the prohibition of flights beyond 10,000 cycles until further testing is approved.

Alternative Inspection Programs

Guidance is provided for establishing special inspection programs for aircraft used in non-standard operations.

Safety notes

  • No aircraft may be operated beyond 10,000 flight cycles until certification fatigue testing is completed.
  • Compliance with inspection intervals greater than the REPEAT Interval +5% is not allowed.
  • If cracks are detected, they must be reported immediately to IAI and Gulfstream Aerospace LP.
  • Inspections are not appropriate for aircraft used in missions other than intended design.
  • The aircraft is prohibited from operation after specified dates unless certain modifications are incorporated.

Full document text

AIRWORTHINESS LIMITATIONS SECTION P/N G280-1001-3-2 1. Airworthiness Limitations Section A. Introduction The Gulfstream G280 is a newly developed aircraft which is currently undergoing extensive fatigue testing of the structural components. Current FAA regulations require a limitation on operation of the aircraft until all certification fatigue tests have been completed. Therefore, no aircraft may be operated beyond 10,000 flight cycles until certification fatigue testing has been completed and Chapter 05-10-10 has been revised to remove this limitation. This Airworthiness Limitations Section is Civil Aviation Authority of Israel (CAAI) approved and specifies maintenance required under Israeli Air Navigation Regulations (ANR) Chapter 7 Section 126 (equivalent to Sections 43.16 and 91.403 of the Federal Aviation Regulations) unless an alternative program has been CAAI approved. The signed CAAI approval form is kept on file with Gulfstream Aerospace Publications. These Airworthiness Limitations are mandatory actions derived from the certification activities, namely, the Damage Tolerance Analysis, structural inspections in the ALS are the results of damage tolerance analysis performed to substantiate compliance with 14 CFR Part 25.571 as presented in certification engineering report 30P032/061977. This section presents the maintenance actions established in order to fully comply with the requirements of Title 14 CFR 25.571 and 25.1529 and 14 CFR Part 25 Subpart H, and therefore, are required to be accomplished in strict compliance with the life limits, maximum intervals limits, inspection methods and PSE location established herein. The Airworthiness Limitations are a result of the Engineering Certification analysis and have been approved by CAAI. The Airworthiness Limitations may only be revised with the approval of the Civil Aviation Authority of Israel (CAAI). Damage tolerance analysis of the Gulfstream G280 shows that the aircraft structure can safely sustain damage in the form of cracks permitting timely detection and repair of cracks. The Airworthiness Limitations Section provides a set of procedures for inspection points of the following six major aircraft components: • Forward fuselage • Center fuselage • Aft fuselage (including engine supports) • Empennage • Wing • Landing gears For each of these sections, a summary table of the inspection points is presented below. See Table 3. These tables give, for each major aircraft structural component, a list of structural points where inspections are to be carried out. For each inspection point the following are given: • The structural part and location to be inspected • The inspection method to be used • The number of flights before the first inspection (initial inspection threshold) MAINTENANCE MANUAL 05-10-10 Page 1 September 15/19 • The number of flights between all further inspections (repeat inspection intervals) • Effectivity The Airworthiness Limitations Section (ALS) stipulates, by means of Continued Airworthiness Inspection Tables, explicit inspection procedures and intervals for the detection of structural cracks throughout the life of the aircraft. This is facilitated by the information presented in this Airworthiness Limitations Section. Airworthiness Limitations inspections (see Table 3) are specified on the basis of flights and not of flight hours. Airframe inspection items will reflect the total flight cycles of the aircraft. Inspections conducted on removable structural parts or assemblies that can be exchanged from one airplane to another such as door assemblies and flight control surfaces are to be tracked by the total flights of the part or assembly itself, and not by total aircraft flights, being these parts may have accumulated flight cycles on (an) other airplane(s) prior to installation on the current aircraft. To allow the scheduling of structural inspections to coincide with a general maintenance check, an inspection overfly tolerance of +5% is allowed. For an inspection accomplishment at a time earlier than the published interval, subsequent inspections are to be scheduled at the specified REPEAT inspection interval, see Figure 1 for examples, and may be accomplished at no later than +5% of the REPEAT interval. Compliance of the inspection greater than the REPEAT Interval +5% is not allowed. The inspection schedule, determined in this document, identifies the inspection areas, initial inspection periods, recurring inspection intervals and component replacement items. It may be emphasized that this schedule is based on airplane utilization, operation and maintenance for which the airplane was originally designed; specifically, a pressurized executive or corporate transportation vehicle wherein the majority of cruise is above 25,000 feet altitude and flight duration is more than one hour. Should the aircraft be used for missions other than that intended by design, such as an air taxi, commuter air service, extraordinary service at low altitude or unusually short duration flights (less than 30 minutes), the inspections specified in this document are not appropriate for continued airworthiness of the airplane structure. In such cases, promptly notify Gulfstream Customer Support and a special inspection program will be established to address the unique requirements of the airplane’s mission. The aircraft is not authorized to fly more than 10,000 flights. This number will be raised to the design goal of 20,000 flights as soon as the full scale fatigue testing results have been analyzed and approved by the Civil Aviation Administration of Israel. As required by the time-limited Exemption No. 10612 to 14 CFR Section 25.981(a)(3) cited in the Gulfstream G280 TCDS, operation of an aircraft after June 30, 2014 is prohibited unless production modification G25-10706 or its associated Service Bulletin 280-57-036 and production modification G25-20047 or its associated Service Bulletin 280-57-071 are incorporated.

Show full text

As required by the Partial Time-limited Exemption No. 10613A from certain engine installation, operational limitation and engine indication provisions of Title 14, Code of Federal Regulations (14 CFR) cited in the Gulfstream G280 TCDS, operation of an aircraft after December 31, 2015 is prohibited unless production modification G25-10022 or associated service bulletin 280-30-017, and production modification G25-20061 or associated service bulletin 280-76-111 are incorporated. If cracks are detected in any of the specified inspections, this information must be reported immediately to Israel Aerospace Industries (IAI) and Gulfstream Aerospace LP. Customer Service will then advise on the procedure to be followed. A form for reporting inspection results is provided in Table 1 of this section. MAINTENANCE MANUAL 05-10-10 Page 2 September 15/19 Table 1: ALS Inspection Results ALS NUMBER AIRCRAFT SERIAL NUMBER AIRCRAFT TAIL NUMBER Part Number(s) [if applicable] Aircraft Hours Aircraft Landings Date of Inspection Discrepancies Found No Yes If yes, complete the following information: Location FS BL WL Size Orientation MAINTENANCE MANUAL 05-10-10 Page 3 September 15/19 0 3000 10,000 12,000 14,000 0 8500 10,500 12,500 14,500 (EARLY COMPLIANCE = 7000) 10,000 INITIAL 2000 RECURRING (EARLY COMPLIANCE = 1500) 10,000 INITIAL 2000 RECURRING TIL-035311 the next inspection due is at the original initial due time. If time remaining after early compliance is greater than the recurring interval, the next inspection due is at the recurring interval from the actual accomplished point. If time remaining after early compliance is less than the recurring interval, 2000 cycles. threshold interval, the next requirement is at the original 10,000 cycles then recurring at For initial compliance early at 3000 cycles having 7000 cycles remaining until the original recurring at 2000 cycles. due time, the next requirement is at 10,500 cycles and all subsequent requirements are For initial compliance early at 8500 cycles having less than 2000 cycles remaining until the original Early Inspection Compliance Figure 1 MAINTENANCE MANUAL 05-10-10 Page 4 September 15/19 For abbreviations used in the airworthiness limitations inspections, see Table 2. Table 2: Airworthiness Limitations Inspection Abbreviations AF - Aft Fuselage LG - Landing Gear BHEC - Bolt Hole Eddy Current (High Frequency) LHS - Left Hand Side CF - Center Fuselage MLG - Main Landing Gear E - Empennage NLG - Nose Landing Gear FF - Forward Fuselage RHS - Right Hand Side HFEC - High Frequency Eddy Current TE - Trailing Edge HS - Horizontal stabilizer US - Ultrasound LE - Leading Edge VS - Vertical stabilizer LFEC - Low Frequency Eddy Current W - Wing Table 3 contains a list of structural inspections along with the specific description, initial threshold, repeat interval and Computerized Maintenance Program (CMP) Reference. Table 4 and Table 5 contains a list of life limited components. Table 6 contains a list of all CMR tasks and fuel tank system airworthiness limitation inspections. Table 7 contains Critical Design Configuration Control Limitations (CDCCL). Table 9 contains temporary limitations and inspection requirements. Table 10 contains LRU and associated failure modes for reportable maintenance events. MAINTENANCE MANUAL 05-10-10 Page 5 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF1.5 Left Connector Plate FF1.5 Forward Pressure Bulkhead Left Connector Plate - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-10-02 531025 FF1.6 Right Connector Plate FF1.6 Forward Pressure Bulkhead Right Connector Plate - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-10-02 531026 FF1.7 Stiffeners at BL 8.3 (210 mm) FF1.7 Forward Pressure Bulkhead Stiffeners, FS 105.1 (2669 mm) at BL 8.3 (210 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-10-02 531038 FF1.8 Stiffeners at BL 12.2 (310 mm) FF1.8 Forward Pressure Bulkhead Stiffeners, FS 105.1 (2669 mm) at BL 12.2 (310 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-10-02 531039 FF2.7 FF2.8 Left / Right Lower Canopy Sill FF2.7, FF2.8 Canopy Lower Sills - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531231 531232 FF2.9 Splice Upper Sill and Central Post FF2.9 Canopy Splice Upper Sill and Central Post - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531233 FF2.10 Lower Sills Doubler FF2.10 Canopy Lower Sills Doubler - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531234 MAINTENANCE MANUAL 05-10-10 Page 6 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF2.11 Lower Sills Splice FF2.11 Canopy Lower Sills Splice - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531235 FF2.12 Left / Right Lower Sill Fitting Reinforcement , FS 139.09 - FS 148.35 (3533 - 3768 mm) FF2.12 Canopy Fitting Lower Sill Reinforcement FS 139.09 - FS 148.35 (3533 - 3768 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531236 FF2.13 Center Post Attach Fitting, FS 105.1 (2669 mm) FF2.13 Canopy Center Post Attachment Fitting FS 105.1 (2669 mm) - NDT Inspection, 53-12-02, Inspection / Check or Code 531237 HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531237 FF2.14 Lower Sill Lightning Holes FF2.14 Canopy Lower Sill Lightning Holes - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531241 FF2.15 Lower Sill Forward Integral Rib FF2.15 Canopy Lower Sill Forward Integral Rib - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531242 FF2.16 Lower Sill Fastener Holes FF2.16 Canopy Lower Sill Fastener Holes - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531243 MAINTENANCE MANUAL 05-10-10 Page 7 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF3.4 Left / Right NLG Trunnion Fitting FF3.4 Nose Landing Gear Trunnion Fittings - NDT Inspection, 53-16-00, Inspection / Check or Code 531604 HFEC 10,000 flight cycles 5000 flight cycles 53-16-00 531604 FF3.5 Left NLG Bay Brace Fitting, FS 148.07 (3761 mm) FF3.5 Nose Landing Gear Brace Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-16-00 531605 FF3.6 NLG Bay Ceiling FF3.6 Nose Landing Gear Bay Ceiling - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-16-00 531606 FF3.8 Doubler, FS 122.16 (3103 mm) FF3.8 Nose Landing Gear Bay Doubler FS 122.16 (3103 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-16-00 531607 FF3.9 Doubler, FS 177.87 (4518 mm) FF3.9 Nose Landing Gear Bay Doubler FS 177.87 (4518 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-16-00 531608 FF3.10 NLG Bay Intergral Intercostal FF3.10 Nose Landing Gear Bay Intercostal Splices - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-16-00 531609 FF3.11 NLG Vertical Stiffener, Left Side FF3.11 Nose Landing Gear Bay Vertical Stiffener, FS 158.19 (4018 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-16-00 531610 MAINTENANCE MANUAL 05-10-10 Page 8 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF4.3 Left Skin Panel, FS 177.87 - FS 229.21 (4518 - 5822 mm) FF4.3 Forward Fuselage Skin Left Side FS 177.87 - FS 229.21 (4518 - 5822 mm) - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-10-01 531004 FF5.3 Upper Skin Panel, FS 229.21 - FS 346.38 (5822 - 8798 mm) FF5.3 Forward Fuselage Skin Upper Panel FS 229.21 - FS 346.38 (5822 - 8798 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-10-01 531009 FF7.1 Forward Window Frame FF7.1 Forward Fuselage Window Frames - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-10-02 531027 FF7.2 Cockpit Side Window Retainer, Left / Right FF7.2 Cockpit Side Windows Retainer - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-02 531223 FF8.2 Upper Panel, Right Longeron, FS 177.87 - FS 229.21 (4518 - 5822 mm) FF8.2 Forward Fuselage Upper Panel Right Longeron FS 177.87 - FS 229.21 (4518 - 5822 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-10-02 531029 FF10.1 Left Frame, FS 185.94 (4723 mm) FF10.1 Forward Cabin Left Frame at FS 185.94 (4723 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531317 MAINTENANCE MANUAL 05-10-10 Page 9 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF10.2A MED Jamb Assembly, Frame 14, FS 221.77 (5663 mm) FF10.2A Forward Cabin Frame 14 MED Jamb Assembly FS 221.77 (5633 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531330 FF10.3 Lower Left Fitting, FS 185.94 (4723 mm) FF10.3 Forward Cabin Lower Fitting at FS 185.94 (4723 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531319 FF10.4 Door Stop Fitting FF10.4 Main Entrance Door Support Stopper - NDT Inspection NOTE: Applies to Aircraft 2001 thru Aircraft 2020 Pre-Mod G25- 20026. HFEC 5000 flight cycles 5000 flight cycles 53-13-02 531329 FF10.4 Door Stop Fitting FF10.4 Main Entrance Door Support Stopper - NDT Inspection NOTE: Applies to Aircraft 2001 thru Aircraft 2020 Post Mod G25- 20026 and Aircraft 2021 thru Aircraft 9999. HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531329 FF10.5 Entry Door Stopper FF10.5 Main Entrance Door Assembly Stopper - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 52-13-03 521312 MAINTENANCE MANUAL 05-10-10 Page 10 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF10.6 Frame 10, Left Side, FS 177.87 (4518 mm) FF10.6 Frame 10, Left Side, FS 177.87 (4518 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531331 FF11.1 Upper Sill, FS 185.94 - FS 221.77 (4723 - 5633 mm) FF11.1 Forward Cabin Upper Sill FS 185.94 - FS 221.77 (4723 - 5633 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531320 FF12.1 Fitting, FS 185.94 (4723 mm), BL 22.24 (565 mm) FF12.1 Forward Cabin Fitting FS 185.94 (4723 mm) BL 22.24 (565 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531322 FF12.2 Fitting, FS 221.77 (5633 mm), BL 22.24 (565 mm) FF12.2 Forward Cabin Fitting FS 221.77 (5633 mm) BL 22.24 (565 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-13-02 531323 FF13.1 Lower Left Intercostal, FS 177.87 - FS 185.94 (4518 - 4723 mm), BL 330 FF13.1 Forward Cabin Lower Left Intercostal FS 177.87 - FS 185.94 (4518 - 4723 mm) BL330 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-13-01 531316 MAINTENANCE MANUAL 05-10-10 Page 11 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF14.1 Left / Right Frame, FS 346.38 (8798 mm) FF14.1 Forward Cabin Frames FS 346.38 (8798 mm) - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-13-02 531324 FF14.2 Upper Frame, FS 346.38 (8798 mm) FF14.2 Forward Cabin Upper Frame FS 346.38 (8798 mm) - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-13-02 531325 FF14.3 Lower Frame, FS 346.38 (8798 mm) FF14.3 Forward Cabin Lower Frame FS 346.38 (8798 mm) - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-13-02 531326 FF15.1 Lower Frame, FS 221.77 (5633 mm) FF15.1 Forward Cabin Lower Frame FS 221.77 (5633 mm) - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-13-02 531327 FF15.2 Lower Frame, FS 185.94 (4723 mm) FF15.2 Forward Cabin Lower Frame FS 185.94 (4723 mm) - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-13-02 531328 FF17.1 Left / Right Frame 5, FS 128.93 (3275 mm) FF17.1 Cockpit Frame 5 FS 128.93 (3275 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-01 531238 FF17.2 Left / Right Frame 6, FS 139.09 (3533 mm) FF17.2 Cockpit Frame 6 FS 139.09 (3533 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-01 531239 MAINTENANCE MANUAL 05-10-10 Page 12 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat FF17.3 Left / Right Frame 7, FS 148.35 (3768 mm) FF17.3 Cockpit Frame 7 FS 148.35 (3768 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-12-01 531240 CF1.1 Center Fuselage Right Side Skin, Frame 27 - Frame 41 CF1.1 Center Fuselage Right Skin Frame 27 - Frame 41 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532019 CF1.2 Center Fuselage Left Side Skin, Frame 27 - Frame 41 CF1.2 Center Fuselage Left Skin Frame 27 - Frame 41 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532020 CF1.3 Center Fuselage Right Side Skin, Frame 41 - Frame 50 CF1.3 Center Fuselage Right Skin Frame 41 - Frame 50 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532021 CF1.4 Center Fuselage Left Side Skin, Frame 41 - Frame 50 CF1.4 Center Fuselage Left Skin Frame 41 - Frame 50 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532022 CF2.1 Center Fuselage Upper Skin, Frame 27 - Frame 41 CF2.1 Center Fuselage Upper Skin Frame 27 - Frame 41 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532023 MAINTENANCE MANUAL 05-10-10 Page 13 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF2.2 Center Fuselage Upper Skin, Frame 41 - Frame 50 CF2.2 Center Fuselage Upper Skin Frame 41 - Frame 50 - NDT Inspection, 53-20-01, Inspection / Check or Code 532024 HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532024 CF3.1 Center Fuselage Lower Skin, Frame 27 - Frame 41 CF3.1 Center Fuselage Lower Skin Frame 27 - Frame 41 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532025 CF3.2 Center Fuselage Lower Skin, Frame 41 - Frame 50 CF3.2 Center Fuselage Lower Skin Frame 41 - Frame 50 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532026 CF4.1 - CF4.20 Center Fuselage Lower Frame 27 - Frame 50 CF4.1 - CF4.20 Center Fuselage Lower Frames - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-20-02 532030 thru 532049 CF4.21 - CF4.39 Center Fuselage Side Splices, Frame 27 - Frame 50 CF4.21 - CF4.39 Center Fuselage Side Splice - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532079 thru 532097 MAINTENANCE MANUAL 05-10-10 Page 14 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF5.1 Center Fuselage Window Frame CF5.1 Center Fuselage Window Frame Between Frame 27 - Frame 41 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-03 532098 CF6.1 Emergency Exit Frame 32 CF6.1 Emergency Exit Frame 32 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532008 CF6.2 Emergency Exit Frame 33 CF6.2 Emergency Exit Frame 33 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532009 CF6.3 Emergency Exit Frame 34 CF6.3 Emergency Exit Frame 34 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532010 CF6.4 Emergency Exit Frame 35 CF6.4 Emergency Exit Frame 35 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532013 CF6.5 Emergency Exit Frame 36 CF6.5 Emergency Exit Frame 36 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532014 CF7.1 Emergency Exit Doubler CF7.1 Emergency Exit Doubler - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-01 532027 MAINTENANCE MANUAL 05-10-10 Page 15 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF9.1 Emergency Exit Window Cut Out CF9.1 Emergency Exit Window Cut Out Perimeter - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 52-21-00 522111 CF10.1 Baggage Compartment Exit Doubler, Frame 45 - Frame 49 CF10.1 Baggage Compartment Exit Doubler Between Frame 45 and Frame 49 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-22-01 532208 CF11.1 Baggage Compartment Exit Side Frame 45 CF11.1 Baggage Compartment Exit Frame 45 - NDT / Visual Inspection LFEC / Visual 10,000 flight cycles 5000 flight cycles 53-22-02 532211 CF11.2 Baggage Compartment Exit Side Frame 49 CF11.2 Baggage Compartment Exit Frame 49 - NDT / Visual Inspection LFEC / Visual 10,000 flight cycles 5000 flight cycles 53-22-02 532212 CF11.3 Baggage Compartment Exit Side Frame 45 and Side Frame 49 CF11.3 Baggage Compartment Exit Frame 45 and Frame 49 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-22-02 532209 CF12.1 Baggage Compartment Exit Upper Sill, Frame 45 - Frame 49 CF12.1 Baggage Compartment Exit Upper Sill - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-22-02 532213 MAINTENANCE MANUAL 05-10-10 Page 16 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF14.1 Wing Pickup Fitting, Frame 29 CF14.1 Wing Pickup Fitting Left and Right Frame 29 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532052 532053 CF14.2 Center Fuselage Upper Frame 29 and Frame 38 CF14.2 Center Fuselage Upper Frame 29 and Frame 38 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532054 532055 CF15.1 Wing Pickup Fitting, Frame 38 CF15.1 Wing Pickup Fitting Left and Right Frame 38 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532056 532057 CF16.1 Wing-to-Fuselage Left Fitting, Frame 29 CF16.1 Wing Attachment Fitting Left Frame 29 - NDT Inspection HFEC / Ultrasonic 10,000 flight cycles 5000 flight cycles 57-16-00 571625 CF16.2 Wing-to-Fuselage Right Fitting, Frame 29 CF16.2 Wing Attachment Fitting Right Frame 29 - NDT Inspection HFEC / Ultrasonic 10,000 flight cycles 5000 flight cycles 57-16-00 571626 CF16.3 Wing-to-Fuselage Right Fitting, Frame 38 CF16.3 Wing Attachment Fitting Vertical Frame 38 - NDT Inspection HFEC / Ultrasonic 10,000 flight cycles 5000 flight cycles 57-16-00 571627 CF16.4 Wing-to-Fuselage Left Fitting, Frame 38 CF16.4 Wing Attachment Fitting Horizontal Frame 38 - NDT Inspection HFEC / Ultrasonic 10,000 flight cycles 5000 flight cycles 57-16-00 571628 MAINTENANCE MANUAL 05-10-10 Page 17 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF18.1 Wing-to-Fuselage Connection Forward Drag Link, Frame 28 - Frame 29 CF18.1 Wing to Fuselage Attachment Forward Drag Link Between Frame 28 and Frame 29 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 57-16-00 571629 CF18.2 Wing-to-Fuselage Connection Forward Right Link, Frame 29 CF18.2 Wing to Fuselage Attachment Forward Link Right Frame 29 - NDT Inspection HFEC / Ultrasonic 10,000 flight cycles 5000 flight cycles 57-16-00 571630 CF18.3 CF18.4 CF18.7 - CF18.10 Forward and Aft Horizontal Wing-to- Fuselage Connection Link, Frame 38 CF18.3, CF18.4, CF18.7 - CF18.10 Wing to Fuselage Attachment Rear Horizontal Link Frame 38 - NDT Inspection HFEC / Ultrasonic 10,000 flight cycles 5000 flight cycles 57-16-00 571632 thru 571637 CF18.5 Rear Vertical Wing-to-Fuselage Connection Link, Frame 38 CF18.5 Wing to Fuselage Attachment Rear Vertical Link Frame 38 - NDT Inspection HFEC / Ultrasonic 10,000 flight cycles 5000 flight cycles 57-16-00 571631 CF19.1 Center Fuselage Side Frame 34, Lower Left / Right CF19.1 Center Fuselage Side Frame 34 Lower Left and Right - NDT Inspection LFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532067 532068 MAINTENANCE MANUAL 05-10-10 Page 18 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF19.2 Center Fuselage Side Frame 37, Lower Left / Right CF19.2 Center Fuselage Side Frame 37 Lower Left and Right - NDT Inspection LFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532069 532070 CF19.3 Center Fuselage Side Frame 39, Left / Right CF19.3 Center Fuselage Side Frame 39 Left and Right - NDT Inspection LFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532071 532072 CF19.4 Center Fuselage Side Frame 41, Left / Right CF19.4 Center Fuselage Side Frame 41 Left and Right - NDT Inspection LFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532073 532074 CF19.5 Center Fuselage Side Frame 50, Left / Right CF19.5 Center Fuselage Side Frame 50 Left and Right - NDT Inspection LFEC 10,000 flight cycles 5000 flight cycles 53-20-02 532075 532076 CF19.6 Center Fuselage Upper Frame 41 CF19.6 Center Fuselage Upper Frame 41 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-20-02 532077 CF19.7 Center Fuselage Upper Frame 50 CF19.7 Center Fuselage Upper Frame 50 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-20-02 532078 MAINTENANCE MANUAL 05-10-10 Page 19 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF21.1 - CF21.6 Pressure Bulkhead Shear Ties, Frame 50 - Frame 51 CF21.1 - CF21.6 Aft Fuselage Pressure Bulkhead Shear Ties Between Frames 50 and Frame 51 - NDT / Visual Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 53-34-00 533411 thru 533422 CF22.1 Emergency Door Bracket, Frame 33 and Frame 35 CF22.1 Emergency Door Brackets at Frame 33 and Frame 35 - NDT Inspection HFEC / MFEC 10,000 flight cycles 5000 flight cycles 52-21-00 522112 CF22.2 Emergency Door Bracket, Upper Sill CF22.2 Emergency Door Brackets Upper Sill - NDT Inspection HFEC / MFEC 10,000 flight cycles 5000 flight cycles 52-21-00 522113 CF22.3 Emergency Door Bracket, Lower Sill CF22.3 Emergency Door Bracket Lower Sill - NDT Inspection HFEC / MFEC 10,000 flight cycles 5000 flight cycles 52-21-00 522114 CF22.4 - CF22.12 Baggage Door Brackets CF22.4 - CF22.12 Baggage Door Brackets - NDT Inspection HFEC 10,000 flight cycles 2500 flight cycles 52-31-00 523121 thru 523129 MAINTENANCE MANUAL 05-10-10 Page 20 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CF23.1 CF23.2 Center Fuselage Longeron Fitting, Auxiliary Bulkhead, BL 12.99 (330 mm) CF23.1, CF23.2 Auxiliary Bulkhead Forward Inboard Longeron Fitting, Left and Right Side, BL 12.99 (330 mm) - NDT Inspection HFEC 10,000 flight cycles 2500 flight cycles 53-21-02 532122 532123 AF1.7 Aft Fuselage Lower Right Angle Support, FS 578.27 (14,688 mm) AF1.7 Aft Pressure Bulkhead Lower Right Angle Support FS 578.27 (14688 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533346 AF1.8 Aft Fuselage Lower Left Angle Support, FS 578.27 (14,688 mm) AF1.8 Aft Pressure Bulkhead Lower Left Angle Support FS 578.27 (14688 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533347 AF1.13 Aft Fuselage Lower Frame, FS 582.2 (14,788 mm) AF1.13 Aft Pressure Bulkhead Lower Frame Inner Flanges at Corner Radius - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533352 AF1.20 Aft Pressure Bulkhead Omega Channel 4, WL 35.43 (WL 900 mm) AF1.20 Aft Pressure Bulkhead Omega Channel 4 WL35.43 (WL900 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533359 MAINTENANCE MANUAL 05-10-10 Page 21 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat AF1.21 Aft Pressure Bulkhead Omega Channel 5, WL 27.95 (WL 710 mm) AF1.21 Aft Pressure Bulkhead Omega Channel 5 WL27.95 (WL710 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533360 AF1.25 Aft Pressure Bulkhead Web, FS 577.48 (14,668 mm) AF1.25 Aft Pressure Bulkhead Web - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533362 AF1.29 Aft Pressure Bulkhead Doubler, Aperture 4 AF1.29 Aft Pressure Bulkhead Doubler Aperture 4 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533364 AF1.30 Aft Pressure Bulkhead Doubler, Aperture 1 AF1.30 Aft Pressure Bulkhead Doubler Aperture 1 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533365 AF1.31 Aft Pressure Bulkhead Doubler, Aperture 3 AF1.31 Aft Pressure Bulkhead Doubler Aperture 3 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533366 AF1.32 Aft Pressure Bulkhead Doubler, Aperture 2 AF1.32 Aft Pressure Bulkhead Doubler Aperture 2 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533367 MAINTENANCE MANUAL 05-10-10 Page 22 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat AF1.33 Aft Pressure Bulkhead Right Doubler Adaptor, FS 577.64 (14,672 mm), WL 32.28 (WL 820 mm) AF1.33 Aft Pressure Bulkhead Doubler Adaptor Right FS 577.64 (14672 mm) WL32.28 (WL820 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533368 AF1.47 Aft Pressure Bulkhead Right Longeron Bath Tab Fitting AF1.47 Aft Pressure Bulkhead Bathtub Fitting Right Longeron - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533393 AF1.48 Aft Pressure Bulkhead Left Longeron Bath Tab Fitting AF1.48 Aft Pressure Bulkhead Bathtub Fitting Top Left Longeron - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-03 533394 AF2.1 Forward Engine Mount Lugs, Left / Right AF2.1 Forward Engine Mount Lugs - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-34-00 533425 533426 AF2.9 Engine Yoke Connection Bolt, Left / Right AF2.9 Forward Engine Mount Bolt Yoke Connection - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-34-00 533433 533434 AF3.2 Engine Pylon Rib 6, Left / Right AF3.2 Engine Pylon Rib 6 Upper and Lower Lugs / Flange - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 54-50-00 545009 545010 MAINTENANCE MANUAL 05-10-10 Page 23 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat AF3.2.1 Aft Engine Mount Strut Connection Bolt, Left / Right AF3.2.1 Aft Engine Mount Strut Connection 1/2 Inch Bolts - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 54-50-00 545011 545012 AF3.3 Engine Thrust Link, Left / Right AF3.3 Engine Thrust Link - NDT Inspection Ultrasonic 10,000 flight cycles 5000 flight cycles 54-50-00 545013 545014 AF3.4 Engine Thrust Link Fitting, Left / Right AF3.4 Aft Engine Mount Thrust Link Fitting - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-34-00 533445 533446 AF3.5 AF3.6 Aft Engine Mount Frame 55, Left / Right AF3.5, AF3.6 Aft Engine Mount Frame 55 to Rib 6 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-34-00 533447 533448 AF4.4 Upper Longeron, Frame 56 - Frame 60, Left AF4.4 Aft Fuselage Left Upper Longeron Frame 56 - Frame 60 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-02 533306 AF4.5 Upper Longeron, Frame 56 - Frame 60, Right AF4.5 Aft Fuselage Right Upper Longeron Frame 56 - Frame 60 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-02 533307 MAINTENANCE MANUAL 05-10-10 Page 24 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat AF6.1 Aft Fuselage Upper Joint Splice, Frame 56, FS 639.41 (16,241 mm) AF6.1 Aft Fuselage Joint Splice Frame 56 FS 639.41 (16,241 mm) - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-02 533316 AF8.1 Aft Fuselage Upper Skin, Frame 50 - Frame 64 AF8.1 Aft Fuselage Upper Skin - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-01 533301 AF10.1 Aft Fuselage Upper Skin Doubler, Frame 56 AF10.1 Aft Fuselage Upper Skin Doubler Frame 56 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 53-33-01 533302 AF11.1 Aft Fuselage, Frame 56 at Boomerang Attachment AF11.1 Aft Fuselage Upper Frame 56 at Boomerang Attachment - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-33-02 533324 AF11.5 Aft Fuselage, Frame 60 at Boomerang Attachment AF11.5 Aft Fuselage Upper Frame 60 at Boomerang Attachment - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-33-02 533328 MAINTENANCE MANUAL 05-10-10 Page 25 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat AF11.6 Aft Fuselage, Frame 63 at Boomerang Attachment AF11.6 Aft Fuselage Upper Frame 63 at Boomerang Attachment - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 53-33-02 533329 E1.1 Vertical Stabilizer Front Spar E1.1 Vertical Stabilizer Front Spar - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553021 E1.2 Vertical Stabilizer Front Boomerang Fittings 1 and 2 E1.2 Vertical Stabilizer to Aft Fuselage Front Boomerang Attach Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553022 E1.4 Vertical Stabilizer Front Drag Fitting E1.4 Vertical Stabilizer to Aft Fuselage Front Drag Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553023 E1.6 E1.7 Vertical Stabilizer Front Attach Strap E1.6, E1.7 Vertical Stabilizer Fuselage Front Attach Strap - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553025 553026 E2.1 Vertical Stabilizer Mid Spar E2.1 Vertical Stabilizer Mid Spar - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553027 MAINTENANCE MANUAL 05-10-10 Page 26 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E2.2 Vertical Stabilizer Mid Boomerang Fittings 1 and 2 E2.2 Vertical Stabilizer to Aft Fuselage Mid Boomerang Attach Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553028 E2.6 E2.7 Vertical Stabilizer Mid Attach Angle E2.6, E2.7 Vertical Stabilizer Fuselage Mid Attach Angle - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553029 553030 E2.11 Vertical Stabilizer Mid Drag Fitting E2.11 Vertical Stabilizer to Aft Fuselage Mid Drag Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553031 E3.1 Vertical Stabilizer Rear Spar E3.1 Vertical Stabilizer Rear Spar - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553032 E3.2 Vertical Stabilizer Rear Boomerang Fittings 1 and 2 E3.2 Vertical Stabilizer to Aft Fuselage Rear Boomerang Attach Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553033 E3.3 Vertical Stabilizer Rear Drag Fitting E3.3 Vertical Stabilizer to Aft Fuselage Rear Drag Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553034 MAINTENANCE MANUAL 05-10-10 Page 27 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E3.7 Vertical Stabilizer Rear Attach Angle E3.7 Vertical Stabilizer Fuselage Rear Attach Angle - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553035 E3.13 Upper Rudder Hinge Fittings 1 and 2 E3.13 Vertical Stabilizer Rear Spar Upper Rudder Hinge Fitting 1 and Fitting 2 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-31-01 553121 E3.14 Mid Rudder Hinge Fittings 1 and 2 E3.14 Vertical Stabilizer Rear Spar Mid Rudder Hinge Fitting 1 and Fitting 2 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-31-01 553122 E3.15 Lower Rudder Hinge Fittings 1 and 2 E3.15 Vertical Stabilizer Rear Spar Lower Rudder Hinge Fitting 1 and Fitting 2 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-31-01 553123 E4.1 E4.2 Vertical Stabilizer Shear Deck, Front and Rear Lower, Rib 0 E4.1, E4.2 Vertical Stabilizer Front and Rear Lower Shear Deck Rib 0 - NDT / Visual Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553037 553038 E4.3 Vertical Stabilizer Shear Deck, Front, Rib 1 E4.3 Vertical Stabilizer Front Rib 1 - NDT / Visual Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553039 MAINTENANCE MANUAL 05-10-10 Page 28 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E4.4 Vertical Stabilizer Shear Deck, Rear, Rib 2 E4.4 Vertical Stabilizer Rear Rib 2 - NDT / Visual Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553040 E4.5 Vertical Stabilizer Rear Rib 6 E4.6 Vertical Stabilizer Rear Rib 10 - NDT / Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553041 E4.6 Vertical Stabilizer Rear Rib 10 E4.6 Vertical Stabilizer Rear Rib 10 - NDT / Visual Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553042 E4.7 Vertical Stabilizer Fitting, Rear Rib 10 E4.7 Vertical Stabilizer Rear Rib 10 Fitting - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553043 E4.8 Vertical Stabilizer Shear Deck, Upper, Rib 12 E4.8 Vertical Stabilizer Upper Shear Deck Rib 12 - NDT / Visual Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553044 E5.1 E5.2 Horizontal Stabilizer Trim Actuator Fittings E5.1, E5.2 Vertical Stabilizer Lower Horizontal Stabilizer Trim Actuator Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553045 553046 MAINTENANCE MANUAL 05-10-10 Page 29 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E5.3 E5.4 Vertical Stabilizer Mid Spar Flight Control Fittings E5.3, E5.4 Vertical Stabilizer Upper and Lower Flight Control Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553047 553048 E5.5 Front Rudder Actuator Fittings 1 and 2 E5.5 Vertical Stabilizer Mid Spar Forward Rudder Actuator Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553049 E5.6 Rear Rudder Actuator Fittings 1 and 2 E5.6 Vertical Stabilizer Rear Spar Rudder Actuator Fittings - NDT Inspecton HFEC 10,000 flight cycles 5000 flight cycles 55-30-00 553050 E5.7 Vertical Stabilizer Pivot Fittings E5.7 Vertical Stabilizer Pivot Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-31-01 553124 E6.3 E6.4 Left / Right Primary Sleeve Pivot E6.3, E6.4 Horizontal to Vertical Stabilizer Primary Sleeve Pivot - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-31-01 553125 553126 E6.5 Secondary Sleeve Pivot E6.5 Horizontal to Vertical Stabilizer Secondary Sleeve Pivot - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-31-01 553127 MAINTENANCE MANUAL 05-10-10 Page 30 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E7.1 E7.2 Vertical Stabilizer Composite Skins E7.1, E7.2 Vertical Stabilizer Composite Skin - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-30-00 553051 553052 E8.1 Horizontal Stabilizer Scissors, Lower Brace Fitting E8.1 Horizontal Stabilizer Scissors Lower Brace Fitting - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-11-01 551177 E8.2 Horizontal Stabilizer Scissors, Upper Brace E8.2 Horizontal Stabilizer Scissors Upper Brace - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-11-01 551178 E8.3 Horizontal Stabilizer Scissors, Lower Brace E8.3 Horizontal Stabilizer Scissors Lower Brace - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-11-01 551179 E8.4 E8.5 Horizontal Stabilizer Scissors, Upper Brace Fitting E8.4, E8.5 Horizontal Stabilizer Scissors Upper Brace Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-11-01 551180 551181 E8.6 Horizontal Stabilizer Brace Backup Fitting E8.6 Horizontal Stabilizer Backup Brace Fitting - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-11-01 551182 MAINTENANCE MANUAL 05-10-10 Page 31 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E10.1 Horizontal Stabilizer Upper Center Skin E10.1 Horizontal Stabilizer Upper Center Skin - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-10-01 551131 E10.2 Horizontal Stabilizer Upper Outer Skin, Left / Right E10.2 Horizontal Stabilizer Upper Outer Skin - Visual / NDT Inspection Visual / Tap Test 10,000 flight cycles 5000 flight cycles 55-10-01 551133 551134 E10.3 Horizontal Stabilizer Lower Center Skin E10.3 Horizontal Stabilizer Lower Center Skin - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-10-01 551135 551136 E10.4 Horizontal Stabilizer Lower Outer Skin, Left / Right E10.4 Horizontal Stabilizer Lower Outer Skin - Visual / NDT Inspection Visual / Tap Test 10,000 flight cycles 5000 flight cycles 55-10-01 551137 551138 E11.1 Horizontal Stabilizer Center Front Spar E11.1 Horizontal Stabilizer Center Front Spar - Visual / NDT Inspection LFEC / HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551139 E11.2 Horizontal Stabilizer Outer Front Spar, Left / Right E11.2 Horizontal Stabilizer Outer Front Spar - Visual / NDT Inspection Visual / Tap Test 10,000 flight cycles 5000 flight cycles 55-10-02 551141 551142 MAINTENANCE MANUAL 05-10-10 Page 32 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E11.3 Horizontal Stabilizer Front Spar Splice Fitting, Left / Right E11.3 Horizontal Stabilizer Front Spar Splice Fitting - NDT Inspection LFEC / X-ray 10,000 flight cycles 5000 flight cycles 55-10-02 551143 551144 E11.4 Horizontal Stabilizer Center Rear Spar E11.4 Horizontal Stabilizer Center Rear Spar - Visual / NDT Inspection LFEC / HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551145 E11.5 Horizontal Stabilizer Outer Aft Spar, Left / Right E11.5 Horizontal Stabilizer Outer Rear Spar - Visual / NDT Inspection Visual / Tap Test 10,000 flight cycles 5000 flight cycles 55-10-02 551147 551148 E11.7 Horizontal Stabilizer Rear Spar Splice, Left / Right E11.7 Horizontal Stabilizer Rear Spar Splice - NDT Inspection LFEC / X-ray 10,000 flight cycles 5000 flight cycles 55-10-02 551149 551150 E12.1 - E12.3 Horizontal Stabilizer Upper Attachment E12.1, E12.2, E12.3 Horizontal Stabilizer Forward Attachment Fitting - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-11-01 551183 551184 551185 E13.1 Horizontal Stabilizer Rib 0 E13.1 Horizontal Stabilizer Rib 0 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-10-02 551151 MAINTENANCE MANUAL 05-10-10 Page 33 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E13.2 Horizontal Stabilizer Rib 1, Left / Right E13.2 Horizontal Stabilizer Left and Right Rib 1 - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-10-02 551152 E13.3 - E13.5 Horizontal Stabilizer Rib 2 - Rib 4, Left / Right E13.3, E13.4, E13.5 Horizontal Stabilizer Rib 2, Rib 3 and Rib 4 - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551153 551154 551155 E13.6 Horizontal Stabilizer Rib 1-1 Intercostal, Left / Right E13.6 Horizontal Stabilizer Rib 1-1 Intercostal - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-10-02 551168 E14.1 Horizontal Stabilizer Pivot Fitting E14.1 Horizontal Stabilizer Pivot Fitting - NDT Inspection HFEC / Ultrasonic / Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551156 E14.2 Horizontal Stabilizer Rib 2 - Rib 3 Intercostal E14.2 Horizontal Stabilizer Rib 2 and Rib 3 Intercostal - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551157 551158 E14.3 Horizontal Stabilizer Actuator Backup Intercostal E14.3 Horizontal Stabilizer Actuator Backup Intercostal - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551159 MAINTENANCE MANUAL 05-10-10 Page 34 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E14.4 Elevator Actuator Rear Fitting E14.4 Elevator Actuator Rear Fitting - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551161 551162 E14.5 Elevator Actuator Front Fitting E14.5 Elevator Actuator Front Fitting - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551163 551164 E14.7 E14.8 Horizontal Stabilizer Flight Control Fittings 1 and 2 E14.7, E14.8 Horizontal Stabilizer Flight Control Fittings - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551165 551166 E14.9 Elevator Stop Fitting E14.9 Elevator Stop Fitting - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-10-02 551167 E15.1 - E15.6 Elevator Hinge Fittings E15.1, E15.2, E15.3, E15.4, E15.5, E15.6 Elevator To Horizontal Stabilizer Attachment Fittings - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-21-01 552105 thru 552116 E16.1 - E16.4 Elevator Fittings E16.1, E16.2, E16.3, E16.4 Elevator Fittings - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-21-01 552121 thru 552128 E16.6 Elevator Torsion Box Skins E16.6 Elevator Torsion Box Skins - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-20-00 552007 552008 MAINTENANCE MANUAL 05-10-10 Page 35 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat E17.1 - E17.3 Rudder Fittings E17.1, E17.2, E17.3 Rudder Fittings - Visual or NDT Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 55-41-01 554111 554112 554113 E17.4 E17.5 Rudder Actuator Fittings E17.4, E17.5 Rudder Actuator Fittings - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 55-41-01 554114 554115 E17.6 Rudder Torsion Box E17.6 Rudder Torsion Box - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 55-40-00 554011 CP1 Location W1.1 W1.2 W1.3 W4.1 Front Spar Splice CP1 Front Spar Splice - NDT Inspection HFEC / LFEC 10,000 flight cycles 5000 flight cycles 57-02-00 570221 570222 CP2 Location W1.1 W1.2 Front Spar Web Penetrations CP2 Front Spar Web Penetrations - Visual / NDT Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 57-02-00 570223 570224 CP3 Location W2.1 W2.2 W2.3 W4.3 Rear Spar Splice CP3 Rear Spar Splice - NDT Inspection HFEC / LFEC 10,000 flight cycles 5000 flight cycles 57-02-00 570225 570226 MAINTENANCE MANUAL 05-10-10 Page 36 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CP4 Location W2.1 W2.2 Rear Spar Web Penetrations CP4 Rear Spar Web Penetrations - Visual / NDT Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 57-02-00 570227 570228 CP5 Location W1.1 W4.1 W4.4 Lower Skin Splice at Front Spar, BL 0 CP5 Lower Skin Splice at Front Spar BL 0 - NDT Inspection HFEC / X-ray 10,000 flight cycles 5000 flight cycles 57-02-00 570229 570230 CP6 Location W2.1 W4.3 W4.4 Lower Skin Splice at Rear Spar, BL 0 CP6 Lower Skin Splice at Rear Spar BL 0 - NDT Inspection HFEC / X-ray 10,000 flight cycles 5000 flight cycles 57-02-00 570231 570232 CP7 CP12 Location W4.1 W4.2 W4.3 W4.4 W5 W7.1 Lower Skin Splice, Stringer Runouts, and Drain Holes at BL 0 CP7, CP12 BL 0 Lower Skin Splice, Stringer Runouts and Drain Holes - NDT / Visual Inspection HFEC / X-ray / Visual 10,000 flight cycles 5000 flight cycles 57-10-00 571003 571004 CP8 Location W1.1 W1.2 W2.1 W2.2 W4.1 W4.2 W4.3 Lower Spar Caps and Stiffeners CP8 Front and Rear Lower Spar Caps and Stiffeners - Visual / NDT Inspection LFEC / HFEC / Visual 10,000 flight cycles 5000 flight cycles 57-02-00 570233 570234 MAINTENANCE MANUAL 05-10-10 Page 37 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CP9 Location W5.1 W5.2 W5.3 Lower Skin and Lower Stringers CP9 Lower Skin and Lower Stringer - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 57-02-00 570235 570236 CP9 Location W5.3 Stringer 3 Aft Skin at Fuel Partition Brackets CP9 Stinger 3 Aft Skin at Fuel Partition Brackets - Visual Inspection NOTE: Applies to Aircraft 2001 and Aircraft 2003 through Aircraft 2079 Pre-Mod G25-20726. Visual 5000 flight cycles 5000 flight cycles 57-02-00 570241 570242 CP10 Location W4.1 W4.2 W4.3 W5.1 W5.2 W5.3 Lower Skin Stringer Runouts CP10 Lower Skin and Lower Stringer Runouts - Visual / NDT Inspection HFEC / Visual 10,000 flight cycles 5000 flight cycles 57-02-00 570237 570238 CP11 Location W4.2 Lower Skin Access Cutouts CP11 Lower Skin Access Cutouts - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 57-02-00 570239 570240 CP13 CP14 Location W1.1 W6.1 W6.2 Wing-to-Fuselage Forward Attachments CP13, CP14 Wing To Fuselage Forward Attachments - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 57-16-00 571638 571639 571640 MAINTENANCE MANUAL 05-10-10 Page 38 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CP15 CP16 Location W2.1 W6.3 W6.4 Wing-to-Fuselage Aft Fittings CP15, CP16 Wing To Fuselage Aft Fittings - Visual Inspection Visual 10,000 flight cycles 5000 flight cycles 57-16-00 571641 571642 571643 CP17 Location W1.1 W6.5 Wing-to-Fuselage Drag Link Fitting CP17 Wing Drag Link Fitting - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 57-16-00 571645 571646 CP18 Location W2.1 W4.3 W8.1 W8.2 Main Landing Gear Sponson CP18 Main Landing Gear Sponson and Attachments To Torsion Box - NDT Inspection HFEC / LFEC 10,000 flight cycles 5000 flight cycles 57-51-00 575109 575110 CP19 Location W2.1 W4.3 W8.4 W8.5 W8.6 Main Landing Gear Actuator and Side Brace Attachments and Backup Structure CP19 Main Landing Gear Actuator and Side Brace Fittings - Visual / NDT Inspection LFEC / HFEC / Visual 10,000 flight cycles 5000 flight cycles 57-10-00 571011 571012 MAINTENANCE MANUAL 05-10-10 Page 39 September 15/19 Table 3: Airworthiness Inspection Section PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP Ref Initial Repeat CP20 Location W9.6 W9.7 Flap Track A Roller Fitting CP20 Flap Track A Roller Fittings - NDT Inspection NOTE: Applies to Aircraft 2001 and Aircraft 2003 thru Aircraft 2054 Pre-SB 280-57-133 (Pre-Mod G25-10710) having the following flap assembly part numbers: • 30P191000002-501 / -502 • 30P191000003-501 / -502 • 30P191000004-501 / -502 • 30P191000005-501 / -502 • 30P191000006-501 / -502 • 30P191000007-501 / -502 • 30P191000008-501 / -502 • 30P191000009-501 / -502 HFEC 1000 flight cycles 225 flight cycles 57-50-00 575033 575034 CP20 Location W9.1 W9.2 W9.4 W9.8 W9.9 Flap Track A Support and Ribs CP20 Flap Track A Support and Ribs - NDT Inspection HFEC 10,000 flight cycles 5000 flight cycles 57-50-00 575035 575036 MAINTENANCE MANUAL 05-10-10 Page 40 September 15/19