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AIRWORTHINESS LIMITATIONS
1. Airworthiness Limitations Section A. Introduction The Airworthiness Limitations Section is Federal Aviation Administration approved and specifies maintenance required under Sections 43.16 and 91.403 of the Federal Aviation Regulations, unless an alternative program has been FAA approved.
(1) Subsections - Details
• Section 1.B. Safe Life Limited Items
• Section 1.C. Principal Structural Element (PSE) Reporting Procedures
• Section 1.D. Principal Structural Element (PSE) Inspections
• Section 1.E. Certification Maintenance Requirements (CMR)
(2) Airworthiness Limitations Each new model of Gulfstream aircraft, will have its own Airworthiness Limitations (AL). The AL speci fically addresses those items which have been identi fied through the certi fication process as being safe life (life limited) or damage tolerant and meet the de finition of a PSE.
Aircraft without a record of the number of landings may calculate by using a ratio of one (1) landing per two (2) flying hours.
(3) MRB Report MSG-3 structural inspection tasks which satisfy ALI requirements for accidental and environmental (corrosion) damage are listed in AMM Chapter 05-22-00 (Maintenance Review Board Report). The operator must consider both AMM Chapter 05-22-00 and Chapter 05-10-10 requirements when developing and maintaining a maintenance program.
B. Safe-Life Limits The Safe Life Limits addresses those items that have been de fined as being life limited. The part number, quantity, item description and mandatory replacement times for these parts are included as shown in the following Life Limited Components Tables.
Table 1: Life Limited Components Chapter 27 Flight Controls Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159SCC474-1 Control Column Sensor Assembly - Discard NOTE: Elevator force senor.
FAR Part 135 operators with ASC 428.
1 1000 flight hours 27-31-13 273051 1159SCC474-5 Control Wheel Sensor Assembly - Discard NOTE: Aileron force senor.
FAR Part 135 operators with ASC 428.
2 1000 flight hours 27-11-17 271073 271074
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Table 1: Life Limited Components Chapter 27 Flight Controls Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159SCC474-9 Rudder Pedal Sensor Assembly - Discard NOTE: Rudder force senor.
FAR Part 135 operators with ASC 428.
11 0 0 0 flight hours 27-21-09 272004 Table 2: Life Limited Components Chapter 30 Ice and Rain Protection Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159P41632-51 1159P41632-53 Nose Cowl Anti-ice Duct - Discard 2 20,000 flight hours 30-02-00 302033 302034 Table 3: Life Limited Components Chapter 32 Nose Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159HM40120-1, -7 Nose Landing Gear Retract Actuator Rod End - Discard 16 4 7 0 flight cycles 32-38-03 322032 1159SCL567-3 Nose Landing Gear Retract Actuator Rod End - Discard NOTE: Covers spares and replacements for all GIV aircraft including GIV series CB 183 / 183A.
1 25, 000 flight cycles 32-38-03 322032 1159L40004 Nose Gear Strut Assembly - Discard (1) 1 20,000 flight cycles 32-20-00 322031 1159LM40700 Nose Landing Gear Shock Strut Cylinder Assembly - Discard (1) 1 20,000 flight cycles 32-22-01 322007 1159LM40520 Nose Landing Gear Shock Strut Piston Assembly - Discard (1) 1 20,000 flight cycles 32-22-01 322003 1159LM40585 Nose Landing Gear Drag Brace - Discard (1) 1 20,000 flight cycles 32-24-00 322055
(1) Landing Gear Assemblies are life limited and may be tracked as an assembly, or Landing Gear Components within the assembly may be tracked separately; however, this does not exclude interfacing and attaching parts or the landing gear assembly not listed here from being subject to the same life limit requirements as the complete Main or Nose Landing Gear Assembly.
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Table 3: Life Limited Components Chapter 32 Nose Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159LM40544 Nose Landing Gear Axle Fitting - Discard (1) 1 20,000 flight cycles 32-23-00 322034 1159LM30548 Nose Gear Upper Torque Arm Assembly - Discard (1) 1 20,000 flight cycles 32-23-00 322013 1159LM30553 Nose Gear Lower Torque Arm Assembly - Discard (1) 1 32,750 flight cycles 32-23-00 322014 1159LM40690 Nose Gear Trunnion Assembly - Discard (1) 1 20,000 flight cycles 32-24-01 322065 1159L40801 Nose Gear Truss Brace Assembly - Discard (1) 1 20,000 flight cycles 32-24-00 322060
(1) Landing Gear Assemblies are life limited and may be tracked as an assembly, or Landing Gear Components within the assembly may be tracked separately; however, this does not exclude interfacing and attaching parts or the landing gear assembly not listed here from being subject to the same life limit requirements as the complete Main or Nose Landing Gear Assembly.
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Table 4: Life Limited Components Chapter 32 Main Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159HM20178 Main Gear Door Actuator End Cap Fitting - Discard NOTE: For aircraft with landing gear door actuator that has more than 9500 flight cycles since new or which the flight cycles since new cannot be determined, comply with initial discard within 12 months from original issue date of CB 235 and discard of landing gear door actuator end cap every 9500 flight cycles thereafter.
For aircraft with landing gear door actuator that has less than 9500 flight cycles since new comply with landing gear door actuator end cap discard at 9500 flight cycles and every 9500 flight cycles thereafter.
For main gear door actuator end cap fittings that are not serialized, the end cap fitting must be tracked by the main gear door actuator part number and serial number until end cap is replaced with a serialized part.
2 Note 32-32-04 323093 323094 1159L40001 Main Landing Gear Assembly - Discard (1) 2 20,000 flight cycles 32-10-00 321077 321078 1159LM40126 Main Landing Gear Structural Post Assembly - Discard (1) 2 20,000 flight cycles 32-12-01 321065 321066 1159LM40110 Main Landing Gear Shock Absorber Cylinder Assembly - Discard (1) 2 20,000 flight cycles 32-12-01 321043 321044
(1) Landing Gear Assemblies are life limited and may be tracked as an assembly, or Landing Gear Components within the assembly may be tracked separately; however, this does not exclude interfacing and attaching parts or the landing gear assembly not listed here from being subject to the same life limit requirements as the complete Main or Nose Landing Gear Assembly.
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Table 4: Life Limited Components Chapter 32 Main Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159LM30114 Main Landing Gear Shock Absorber Piston Assembly - Discard (1) 2 20,000 flight cycles 32-12-01 321045 321046 1159LM40140 Main Landing Gear Axle Fitting - Discard (1) 2 20,000 flight cycles 32-13-01 321062 321063 1159LM40175 Main Landing Gear Aft Trunnion Pin - Discard 2 16,500 flight cycles 32-15-01 321023 321024 1159LM40147 Main Landing Gear Shock Absorber Attach Pin - Discard NOTE: Three strut pins per gear.
6 20,000 flight cycles 32-12-01 321092 321093 321094 321095 321096 321097
(1) Landing Gear Assemblies are life limited and may be tracked as an assembly, or Landing Gear Components within the assembly may be tracked separately; however, this does not exclude interfacing and attaching parts or the landing gear assembly not listed here from being subject to the same life limit requirements as the complete Main or Nose Landing Gear Assembly.
Table 5: Life Limited Components Chapter 56 Windows Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref NAS1580 Side Window Fasteners - Discard NOTE: Reference PSE 53-17-106.
Perform within 5000 flight cycles from last accomplishment.
5000 flight cycles 56-12-00 561021 561022 Table 6: Life Limited Components Chapter 57 Wings Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 1159WM20023 Sponson Rib Assembly - Discard NOTE: Reference PSE 57-14-200.
Covers spares and replacements for all aircraft.
2 20,000 flight cycles 57-10-00 571035 571036
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Table 7: Life Limited Components Chapter 71 Power Plant Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATARef CMP Ref 94756-06 94756-07 Engine Isolator Mount Bolt Assembly - Discard NOTE: Reference PSE 71-22-101.
At scheduled engine overhaul. Not to exceed 8500 hours between replacement.
4 Note 71-01-00 712084 712085 712086 712087 C. Principal Structural Elements Reporting Procedure Reporting of inspection results is required to ensure continued airworthiness of the fleet is maintained. This procedure contains the necessary reporting information which is to be used whenever a principal structural element inspection is accomplished.
NOTE: Inspection results, both positive and negative, are to be reported to Gulfstream Maintainability Engineering. Complete Table 8 with inspection results. Return completed table to Gulfstream Maintainability Engineering, FAX 912-965-4704. Discrepancies must be reported within 24 hours. Discrepancies must be accompanied by digital photograph(s).
Table 8: PSE Inspection Results PSE Number A/C Serial Number A/C Tail Number Part Number(s) [if applicable] A/C Hours A/C Landings Date of Inspection Discrepancies Found Yes (If yes information below must be completed.) No Location
FS BL WL Size Orientation
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D. Principal Structural Element Inspection Requirements Table 10 contain a list of PSE along with the specific description, initial threshold, repeat interval and Computerized Maintenance Program (CMP) reference.
NOTE: For PSE inspections with an MRB reference listed as inspection interval, see Scheduled Maintenance Checks, 05-20-00, Scheduled Maintenance Checks inspection table with same MRB reference to determine frequency.
For inspections with a reduced recurring interval (i.e., 10,000 initial / 2,000 recurring) the next due inspection is dependent upon the initial inspection accomplishment. See Figure 1.
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0 3000 10,000 12,000 14,000 For initial compliance early at 3000 hours having 7000 hours remaining until the original threshold interval, the next requirement is at the original 10,000 hours then recurring at 2000 hours.
0 8500 10,500 12,500 14,500 NOTE:
NOTE:
10,000 INITIAL 2000 RECURRING (EARLY COMPLIANCE = 7000) 10,000 INITIAL 2000 RECURRING (EARLY COMPLIANCE = 1500) For initial compliance early at 8500 hours having less than 2000 hours remaining until the original due time, the next requirement is at 10,500 hours and all subsequent requirements are recurring at 2000 hours.
If time remaining after early compliance is greater than the recurring interval, the next inspection due is at the original initial due time.
If time remaining after early compliance is less than the recurring interval, the next inspection due is at the recurring interval from the actual accomplished point.
TIL-78178B Early Inspection Compliance Figure 1
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Table 10: Principal Structural Elements PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat 32-25-100 Nose Landing Gear Retraction Fitting Lug Nose Landing Gear Retraction Fitting Lug - NDT Inspection Eddy current 15,000 flight cycles 4100 flight cycles 32-25-00 322502 32-25-200 Nose Landing Gear Drag Brace Fitting Nose Landing Gear Drag Brace Fitting - NDT Inspection Eddy current 15,000 flight cycles 4100 flight cycles 32-25-00 322056 32-25-300 Nose Landing Gear Trunnion Fitting Nose Landing Gear Trunnion Fitting - NDT Inspection Eddy current 15,000 flight cycles 11,200 flight cycles 32-24-01 322066 52-10-101 Passenger Door Structure Main Entrance Door Structure - Inspection Visual 13,600 flight cycles 13,600 flight cycles 52-11-00 521031 52-10-102 Passenger Door Pin Bearing Plates Main Entrance Door Pin Bearing Plates
- Inspection Visual 13,600 flight cycles 13,600 flight cycles 52-10-00 521023 52-10-103 Passenger Door Hinges Main Entrance Door Structure - Inspection Visual 13,600 flight cycles 13,600 flight cycles 52-11-00 521031 52-30-101 Baggage Door Stop Fittings Baggage Compartment Door Stop Fittings and Internal Structure - Detailed Inspection Visual 15,000 flight cycles 3400 flight cycles 52-30-00 523050
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Table 10: Principal Structural Elements PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat 52-30-102 Baggage Door Structure Baggage Compartment Door Stop Fittings and Internal Structure - Detailed Inspection Visual 15,000 flight cycles 3400 flight cycles 52-30-00 523050 53-11-101 Cockpit Skin Splices Fuselage Skins and Stringers - General Visual Inspection NOTE: See PSE 53-31-104.
Visual Note Note 53-00-06 533101 53-11-102 Nose Landing Gear Well Skin Cutout Nose Gear Wheel Well FS 44 - FS 119 - Zonal Inspection Visual MRB No. 53-100-03 53-10-20 534021 53-12-100 FS 63 Bulkhead Bulkhead Installation FS 63 - Detailed Inspection Visual 15,000 flight cycles 1600 flight cycles 53-12-01 531201 53-12-110 FS 85 Bulkhead Bulkhead Installation FS 85 - Detailed Inspection Visual 15,000 flight cycles 15,000 flight cycles 53-12-01 531202 53-12-120 FS 119 Bulkhead Bulkhead Installation FS 119 - Inspection Eddy current 15,000 flight cycles 3300 flight cycles 53-12-01 531203 53-12-130 FS 133 Bulkhead Bulkhead Installation FS 133 - Detailed Inspection Visual 15,000 flight cycles 15,000 flight cycles 53-12-01 531204
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Table 10: Principal Structural Elements PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat 53-12-150 Cockpit Stub Frames Cockpit Stub Frames - Detailed Inspection Visual 15,000 flight cycles 15,000 flight cycles 53-12-02 531205 53-12-170 Access Panel Surround Structure Cockpit Access Panel Surround Structure - Detailed Inspection Visual 15,000 flight cycles 6700 flight cycles 53-14-00 531206 53-15-100 Pressure Floor Structure Cockpit Pressure Floor Structure - Detailed Inspection Visual 15,000 flight cycles 1600 flight cycles 53-15-00 531501 53-17-101 Lower Rail Cockpit Lower Rail Attachment - General Visual Inspection Visual 15,000 flight cycles 1600 flight cycles 53-17-00 531701 53-17-102 Upper Sill Cockpit Upper Sill - General Visual Inspection Visual 15,000 flight cycles 1600 flight cycles 53-17-00 531702 53-17-103 Center Windshield Post Windshield Center Post - NDT Inspection Eddy current 15,000 flight cycles 8100 flight cycles 53-17-10 531703 53-17-104 Side Windshield Post Cockpit Side Windshield Post - NDT Inspection Eddy current 8000 flight cycles 2300 flight cycles 53-17-20 539502
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Table 10: Principal Structural Elements PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat 53-17-105 Aft Windshield Post Cockpit Aft Windshield Post - NDT Inspection Eddy current 13,700 flight cycles 11,300 flight cycles 53-17-30 539503 53-17-106 Windshield Fasteners Side Window Fasteners - Discard NOTE: See Table 5 Life Limited Components Chapter 56 Windows.
Discard Note Note 56-12-00 561021 561022 53-22-100 FS 169 Bulkhead FS 169 Bulkhead - Detailed Inspection Visual 15,000 flight cycles 15,000 flight hours
(1) 15,000 flight cycles 15,000 flight hours
(1) 53-22-00 532201 53-29-101 Passenger Door Surround Structure - Longeron 6 Main Entrance Door Surround Structure Longeron 6 - NDT Inspection Eddy current 15,000 flight cycles 5000 flight cycles 53-21-00 532901 53-29-102 Passenger Door Cutout Corner Main Entrance Door Corner Cutout - NDT Inspection X-ray 15,000 flight cycles 15,000 flight hours
(1) 5000 flight cycles 53-21-00 532902 53-31-101 Longitudinal Skin Splices Fuselage Skins and Stringers - General Visual Inspection NOTE: See PSE 53-31-104.
Visual Note Note 53-00-06 533101
(1) Whichever occurs first.
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