Gulfstream GVI (G650) Maintenance Program

05-20-00 Nose Wheel Steering Unit - Lubrication 122211 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. 05-20-00 Nose Wheel Steering Collar Assembly / Slave Gear - Lubrication 122212 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. 05-20-00 Flap Actuator Ball Nut - Lubrication 122328 122329 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. 05-20-00 Aileron Hinge Fitting - Lubrication 122333 122334 September 2013 - Gulfstream Maintainability Engineering added MRIP requirement to cover flight control hinge lubrication points. 05-20-00 Rudder Hinge Fitting - Lubrication 122335 September 2013 - Gulfstream Maintainability Engineering added MRIP requirement to cover flight control hinge lubrication points. 05-20-00 Elevator Hinge Fitting - Lubrication 122336 122337 September 2013 - Gulfstream Maintainability Engineering added MRIP requirement to cover flight control hinge lubrication points. 05-20-00 Flight Control System Electrical Backup Hydraulic Actuator Battery - Capacity Check 243607 November 2012 - G650 ISC Meeting - Added procedure, MRB to be updated after analysis approval @ 2013 ISC. 05-20-00 Ram Air Turbine Built-inTest Switch - Operational Check 242351 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. MAINTENANCE MANUAL 05-00-00 Page 3 September 30/13 Table 1: MRIP Table Chapter 5 Reference Description CMP Reference MRIP History 05-10-00 A Track Flap Roller - Discard 275058 275059 275060 275061 275062 275063 November 2011 - Gulfstream Fatigue and Damage Tolerance Engineering added requirement as a result of fatigue testing. 05-10-00 B Track Flap Roller - Discard 275064 275065 275066 275067 275068 275069 275070 275071 275072 275073 275074 275075 November 2011 - Gulfstream Fatigue and Damage Tolerance Engineering added requirement as a result of fatigue testing. 05-10-00 C Track Flap Roller- Discard 275076 275077 275078 275079 275080 275081 275082 275083 275084 275085 275086 275087 November 2011 - Gulfstream Fatigue and Damage Tolerance Engineering added requirement as a result of fatigue testing. 05-10-00 D Track Flap Roller - Discard 275088 275089 275090 275091 275092 275093 275094 275095 November 2011 - Gulfstream Fatigue and Damage Tolerance Engineering added requirement as a result of fatigue testing. 05-10-00 D Track Flap Down Load Catch Roller - Discard 275096 275097 275098 275099 November 2011 - Gulfstream Fatigue and Damage Tolerance Engineering added requirement as a result of fatigue testing. MAINTENANCE MANUAL 05-00-00 Page 4 September 30/13 Table 1: MRIP Table Chapter 5 Reference Description CMP Reference MRIP History 05-10-00 Left System Manifold Filter - Discard 291487 291488 291489 291490 291491 291492 2012 ISC - Gulfstream Engineering added requirement as a result of qualification testing. 05-10-00 Right System Manifold Filter - Discard 291525 291526 291527 2012 ISC - Gulfstream Engineering added requirement as a result of qualification testing. 05-10-00 Auxiliary Hydraulic Pump Manifold Filter - Discard 292511 2012 ISC - Gulfstream Engineering added requirement as a result of qualification testing. 05-20-00 Wing Anti-ice Temperature Switch - Temperature Trip Point Functional Check 301137 February 2011 - G650 ISC Meeting - Added to align task interval with other maintenance procedures in the same zones. 05-20-00 Windshield Surface Seal - Detailed Inspection 304118 304119 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. 05-10-00 Nose Landing Gear - Restore 322002 August 2012 - Gulfstream Engineering added requirement as a result of assembly modification status. 05-10-00 HP Stage 5 Air Nonreturn Valve - Restore 361110 361111 August 2013 - Requirement added to address valve corrosion. 05-10-00 Main Entrance Door Latching Actuator - Discard 521303 May 2012 - Gulfstream Mechanical Systems Engineering added requirement as a result of qualification testing. 05-20-00 Main Entrance Door Pressure Relief Valve - Detailed Inspection 521304 2012 ISC - Added Main Entrance Door Pressure Relief Valve - Detailed Inspection. 05-20-00 Radome to Structure Perimeter Steps - Detailed Inspection 531036 August 2012 - Gulfstream Maintainability Engineering added requirement to meet operator RVSM flight operations requirements. MAINTENANCE MANUAL 05-00-00 Page 5 September 30/13 Table 1: MRIP Table Chapter 5 Reference Description CMP Reference MRIP History 05-20-00 Main Landing Gear Wheel Well and Torque Box FS 671.411 - FS 739 - Enhanced Zonal Inspection 533002 533003 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. 05-20-00 Baggage Compartment Below Floor HIRF/L - Detailed Inspection 534001 June 2013 - Gulfstream Maintainability added 4C interval for task / calendar alignment. 05-20-00 Wing Tank (Internal) BL 0 - RBS 135 - Detailed Inspection 571027 571028 February 2011 - G650 ISC Meeting - Added to align task interval with other maintenance procedures in the same zones. 05-20-00 Wing Tank (Internal) RBS 135 - WS 551 - Detailed Inspection 571029 571030 February 2011 - G650 ISC Meeting - Added to align task interval with other maintenance procedures in the same zones. 05-20-00 Flap Upper Surface - Detailed Inspection 575301 575302 June 2012 - Gulfstream Fatigue and Damage Tolerance Engineering added requirement as a result of fatigue testing. 05-20-00 Nacelle, T/Rev and Exhaust External (Viewed From Platform) - Zonal Inspection 710035 710036 June 2012 - G650 ISC Meeting - Added to align task interval with other maintenance procedures in the same zones. 05-20-00 Engine Maintenance Program Declaration 710039 September 2013 - Gulfstream Maintainability added “One time inspection” task in 1A Check Scheduled Maintenance Table per review. 05-20-00 Engine Internal - Zonal Inspection 711002 711003 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. 05-20-00 Engine Lower Fan Cowl Door - Enhanced Zonal Inspection 711004 711005 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. MAINTENANCE MANUAL 05-00-00 Page 6 September 30/13 Table 1: MRIP Table Chapter 5 Reference Description CMP Reference MRIP History 05-20-00 Engine Bypass Duct Internal FS 894.6 - FS 950.3 - Zonal Inspection 727103 June 2012 - G650 ISC Meeting - Revised task interval to incorporate Low-Utilization Maintenance Program (LUMP) into the Aircraft Maintenance Manual (AMM) Chapter 5. 05-20-00 T/Rev and Exhaust Internal - Zonal Inspection 783112 783113 June 2012 - G650 ISC Meeting - Added to align task interval with other maintenance procedures in the same zones. 05-20-00 T/Rev HIRF/L - Detailed Inspection 783114 783115 June 2012 - G650 ISC Meeting - Added to align task interval with other maintenance procedures in the same zones. MAINTENANCE MANUAL 05-00-00 Page 7 September 30/13 MAINTENANCE MANUAL THIS PAGE IS INTENTIONALLY LEFT BLANK 05-00-00 Page 8 September 30/13 TIME LIMITS 1. Time Limits A. Introduction The time limits section provides manufacturer recommended time limits for inspections, maintenance and overhaul of aircraft, powerplant and systems. This section includes life limits of major components and other items designated critical. Subsections - Details • 1.A.(1) Manufacturer Recommended Restore / Discard Items Table 1 Chapter 23 - Communications Table 2 Chapter 24 - Electrical Power Table 3 Chapter 25 - Equipment / Furnishings Table 4 Chapter 26 - Fire Protection Table 5 Chapter 27 - Flight Controls Table 6 Chapter 29 - Hydraulic Power Table 7 Chapter 31 - Indicating / Recording Systems Table 8 Chapter 32 - Landing Gear Table 9 Chapter 33 - Lights Table 10 Chapter 35 - Oxygen Table 11 Chapter 38 - Water / Waste Table 12 Chapter 49 - Airborne Auxiliary Power Table 13 Chapter 52 - Doors • 1.A.(2) Hydrostatic Testing of Bottles (Charts and Notes) Table 14 Fire Extinguisher Bottle Maintenance Schedule Table 15 Emergency Blow Down Bottle Maintenance Schedule Table 16 Oxygen Bottle Maintenance Schedule (1) Manufacturer Recommended Restore / Discard Items The purpose of this section is to provide operators with a list of installed components having restoration and / or discard task intervals. Intervals have been recommended by product manufacturers. Operators are required to maintain this list, as appropriate, for their particular outfitting. MAINTENANCE MANUAL 05-10-00 Page 1 September 30/13 Table 1: Chapter 23 - Communications ATA Ref Component Manufacturer / Part Number Limits CMP Ref 23-72-11 Cockpit Voice Recorder Underwater Locator Beacon Battery - Discard MRB Ref: 23-72-00-03 Dukane DK120 6 years 237220 MAINTENANCE MANUAL 05-10-00 Page 2 September 30/13 Table 2: Chapter 24 - Electrical Power ATA Ref Component Manufacturer / Part Number Limits CMP Ref 24-35-02 Emergency Battery Pack - Discard MRB Ref: 24-20-00-08 NOTE: Clock for 48 month initial discard, starts at aircraft entry into service. For all recurring battery replacements, time starts with date of aircraft installation. Securaplane 100-0302-03 4 years 243508 243509 MAINTENANCE MANUAL 05-10-00 Page 3 September 30/13 Table 3: Chapter 25 - Equipment / Furnishings ATA Ref Component Manufacturer / Part Number Limits CMP Ref 25-61-01 Life Vest - Restore MRB Ref: 25-60-00-02 Hoover 3505-101CW 3505-101W 2 years 256070 thru 256099 25-61-01 Life Vest - Restore MRB Ref: 25-60-00-02 Air Cruisers (vacuum packed) 63600 120 months 256070 thru 256099 25-61-03 Life Raft - Restore MRB Ref: 25-60-00-04 Winslow 1320FAUL-630-1-100 3 years 256143 256144 256145 256146 25-61-04 Survival Kit - Restore MRB Ref: 25-60-00-12 NOTE: Per manufacturer recommendation. (If separate from life raft.) Winslow Note 256197 256198 256199 25-61-04 Survival Kit Time Limited Supplies - Discard MRB Ref: 25-60-00-13 NOTE: Per manufacturer recommendation. (If separate from life raft.) Winslow Note 256194 256195 256196 25-62-01 Smoke Hood - Discard MRB Ref: 35-10-00-08 Essex MR-10039N 10 years 256219 256220 256221 25-62-05 Emergency Vision Assurance System - Restore MRB Ref: 25-60-00-15 Vision Safe Products 107TC-049 107TC-050 120 months 256204 256205 25-62-05 Emergency Vision Assurance System Batteries - Discard MRB Ref: 25-60-00-16 Vision Safe Products 107TC-049 107TC-050 24 months 256206 256207 25-63-08 Emergency Locator Transmitter Battery Pack - Discard MRB Ref: 25-60-00-09 Artex 452-0133 5 years 256308 MAINTENANCE MANUAL 05-10-00 Page 4 September 30/13 Table 3: Chapter 25 - Equipment / Furnishings ATA Ref Component Manufacturer / Part Number Limits CMP Ref 25-64-01 First Aid Kit Time Limited Supplies - Discard MRB Ref: 25-60-00-11 MedAire AFAK 1 year 256406 256407 25-64-01 Medical Kit Time Limited Supplies - Discard MRB Ref: 25-60-00-11 MedAire EMK 1 year 256414 256415 25-64-03 Defibrillator Time Limited Supplies - Discard MRB Ref: 25-60-00-19 NOTE: Per manufacturer recommendation. Phillips Heartstart FRx 502861 Note 256419 MAINTENANCE MANUAL 05-10-00 Page 5 September 30/13 Table 4: Chapter 26 - Fire Protection ATA Ref Component Manufacturer / Part Number Limits CMP Ref 26-21-01 Engine Fire Bottle Cartridge (Squib) - Discard MRB Ref: 26-21-00-03 NOTE: 15 years total (shelf + service). Pacific Scientific 30903931 30903933 30903959 10 years Note 262132 262133 262134 262135 262136 262137 262138 262139 262140 262141 262142 262143 MAINTENANCE MANUAL 05-10-00 Page 6 September 30/13 Table 5: Chapter 27 - Flight Controls ATA Ref Component Manufacturer / Part Number Limits CMP Ref 27-03-03 Aileron and Elevator Control Module Assembly Rod (Pilot) - Discard 60P2711003Z001 4250 flight cycles 270310 27-03-03 Aileron and Elevator Control Module Assembly Rod (Copilot) - Discard 60P2711003Z001 4250 flight cycles 270311 27-03-03 Aileron and Elevator Control Module Assembly Rod (Pilot) - Discard 60P2711004Z001 4250 flight cycles 270312 27-03-03 Aileron and Elevator Control Module Assembly Rod (Copilot) - Discard 60P2711004Z001 4250 flight cycles 270313 27-03-03 Aileron and Elevator Control Module Assembly Rod (Pilot) - Discard 60P2711005Z001 4250 flight cycles 270314 27-03-03 Aileron and Elevator Control Module Assembly Rod (Copilot) - Discard 60P2711005Z001 4250 flight cycles 270315 27-03-03 Aileron and Elevator Control Module Assembly Interconnect Rod - Discard 60P2711006Z001 4250 flight cycles 270316 27-03-03 Aileron and Elevator Control Module Assembly (Pilot) - Discard 60P2711101Z004 4250 flight cycles 270317 27-03-03 Aileron and Elevator Control Module Assembly (Copilot) - Discard 60P2711201Z004 4250 flight cycles 270318 27-03-05 Rudder Control Module Assembly - Discard 60P2721300Z003 4250 flight cycles 272402 27-11-07 Aileron Control Cable Pulley Bracket - Discard 60P2711501Z001 4250 flight cycles 271170 27-11-07 Aileron Control Cable Pulley Bracket - Discard 60P2711502Z001 4250 flight cycles 271171 27-11-07 Aileron Control Cable Pulley Bracket - Discard 60P2711503Z001 4250 flight cycles 271172 27-11-07 Aileron Control Cable Pulley Bracket - Discard 60P2711504Z001 4250 flight cycles 271173 MAINTENANCE MANUAL 05-10-00 Page 7 September 30/13 Table 5: Chapter 27 - Flight Controls ATA Ref Component Manufacturer / Part Number Limits CMP Ref 27-11-09 Aileron Control Override Pushrod - Discard 60P2711310Z001 4250 flight cycles 271169 27-11-13 Aileron Trim Interconnect Pushrod - Discard 60P2711309Z001 4250 flight cycles 271168 27-13-05 Aileron EHSA Manifold - Discard 60P2713201Z004/ 005 8500 flight cycles 271362 271363 27-13-07 Aileron EB Manifold - Discard 60P2713301Z003 / 004 8500 flight cycles 271364 271365 27-13-09 Aileron HA Manifold - Discard 60P2713101Z005/ 006 8500 flight cycles 271360 271361 27-21-01 Rudder Pedal Assembly- Discard 60P2721100Z004 4250 flight cycles 272106 27-21-01 Rudder Pedal Assembly- Discard 60P2721200Z005 4250 flight cycles 272107 27-22-01 Rudder Force Sensor - Discard 60P2721101Z002 4250 flight cycles 272108 272109 27-23-01 Rudder EHSA Actuator - Discard 60P2723002Z003 8500 flight cycles 272313 27-23-03 Rudder EBHA Actuator - Discard 60P2723001Z004 8500 flight cycles 272312 27-23-05 Rudder EHSA Manifold - Discard 60P2723201Z002/ 003 8500 flight cycles 272315 27-23-07 Rudder EB Manifold - Discard 60P2713301Z003 / 004 8500 flight cycles 272316 27-23-09 Rudder HA Manifold - Discard 60P2723101Z003/ 004 8500 flight cycles 272314 27-31-01 Control Column and Control Wheel - Discard 60P2711100Z005 4250 flight cycles 273112 MAINTENANCE MANUAL 05-10-00 Page 8 September 30/13 Table 5: Chapter 27 - Flight Controls ATA Ref Component Manufacturer / Part Number Limits CMP Ref 27-31-01 Control Column and Control Wheel - Discard 60P2711200Z005 4250 flight cycles 273113 27-31-03 Elevator Control Override Pushrod - Discard 60P2731305Z002 4250 flight cycles 273129 27-32-01 Elevator Force Sensor - Discard 60P2731101Z002 4250 flight cycles 273212 273213 27-33-01 Elevator EHSA Actuator - Discard 60P2733002Z005 8500 flight cycles 273322 273323 27-33-03 Elevator EBHA Actuator - Discard 60P2733001Z004 8500 flight cycles 273320 273321 27-33-07 Elevator EB Manifold - Discard 60P2713301Z003 / 004 8500 flight cycles 273328 273329 27-33-09 Elevator HA Manifold - Discard 60P2723101Z003 / 004 8500 flight cycles 273324 273325 27-51-03 A Track Flap Roller - Discard MRIP 60P5755371Z005 Kamatics Corporation KRP505-04VT 2400 flight hours 275058 275059 275060 275061 275062 275063 27-51-03 B Track Flap Roller - Discard MRIP 60P5755371Z001 60P5755371Z002 60P5755371Z003 2400 flight hours 275064 275065 275066 275067 275068 275069 275070 275071 275072 275073 275074 275075 MAINTENANCE MANUAL 05-10-00 Page 9 September 30/13 Table 5: Chapter 27 - Flight Controls ATA Ref Component Manufacturer / Part Number Limits CMP Ref 27-51-03 C Track Flap Roller- Discard MRIP 60P5755371Z001 60P5755371Z003 60P5755371Z007 2400 flight hours 275076 275077 275078 275079 275080 275081 275082 275083 275084 275085 275086 275087 27-51-03 D Track Flap Roller - Discard MRIP 60P5755371Z004 60P5755371Z006 2400 flight hours 275088 275089 275090 275091 275092 275093 275094 275095 27-51-03 D Track Flap Down Load Catch Roller - Discard MRIP 60P5755371Z008 2400 flight hours 275096 275097 275098 275099 27-55-05 Flap Hydraulic Control Module - Discard 60P2756002Z006 4250 flight cycles 275507 27-63-05 Outboard Spoiler (Outboard Flight) EBHA Actuator - Discard 60P2763002Z100 / 200 60P2763002Z101 / 201 6800 flight cycles 276361 276362 27-63-09 Spoiler EB Manifold - Discard 60P2763301Z005 / 006 8500 flight cycles 276369 276370 MAINTENANCE MANUAL 05-10-00 Page 10 September 30/13 Table 5: Chapter 27 - Flight Controls ATA Ref Component Manufacturer / Part Number Limits CMP Ref 27-63-11 Spoiler HA Manifold - Discard 60P2763101Z004 8500 flight cycles 276363 276364 MAINTENANCE MANUAL 05-10-00 Page 11 September 30/13 Table 6: Chapter 29 - Hydraulic Power ATA Ref Component Manufacturer / Part Number Limits CMP Ref 29-14-19 Left System Manifold Filter - Discard MRIP Donaldson Company, Inc 339474 339482 339913 600 flight hours 291487 291488 291489 291490 291491 291492 29-14-20 Right System Manifold Filter - Discard MRIP Donaldson Company, Inc 339482 339913 600 flight hours 291525 291526 291527 29-25-03 Auxiliary Hydraulic Pump Manifold Filter - Discard MRIP Donaldson Company, Inc 339980 600 flight hours 292511 MAINTENANCE MANUAL 05-10-00 Page 12 September 30/13 Table 7: Chapter 31 - Indicating / Recording Systems ATA Ref Component Manufacturer / Part Number Limits CMP Ref 31-31-05 FDR Underwater Locator Beacon Battery - Discard MRB Ref: 31-31-00-04 Dukane DK120 6 years 313117 MAINTENANCE MANUAL 05-10-00 Page 13 September 30/13 Table 8: Chapter 32 - Landing Gear ATA Ref Component Manufacturer / Part Number Limits CMP Ref 32-10-00 Main Landing Gear - Restore MRB Ref: 32-10-00-03 Goodrich C1A4100LA002 C1A4100RA002 10,000 flight cycles 321008 321009 32-10-00 Main Landing Gear - Discard MRB Ref: 32-10-00-06 MRB Ref: 32-31-00-07 NOTE: In accordance with Airworthiness Limitations. Goodrich C1A4100LA002 C1A4100RA002 Note 321010 321011 32-20-00 Nose Landing Gear - Restore MRB Ref: 32-20-00-05 Goodrich C2A4100CA006 10,000 flight cycles 322002 32-20-00 Nose Landing Gear - Restore MRIP NOTE: 2500 flight cycles. Applicable to serial number GLG0005. 60E3222010A006 Note 322002 32-20-00 Nose Landing Gear - Restore MRIP NOTE: 2500 flight cycles. Applicable to serial number GLG0003. 60P3222010A003 Note 322002 32-20-00 Nose Landing Gear - Restore MRIP NOTE: 2500 flight cycles. Applicable to serial numbers GLG0009 thru GLG0011. 60P3222010A004 Note 322002 32-20-00 Nose Landing Gear - Restore MRIP NOTE: 2500 flight cycles. Applicable to serial numbers GLG0013 thru GLG0016. 60P3222010A006 Note 322002 MAINTENANCE MANUAL 05-10-00 Page 14 September 30/13 Table 8: Chapter 32 - Landing Gear ATA Ref Component Manufacturer / Part Number Limits CMP Ref 32-20-00 Nose Landing Gear - Restore MRIP NOTE: 2500 flight cycles. Applicable to serial numbers GLG0012 and GLG0017 thru GLG0022. 60P3222010A007 Note 322002 32-20-00 Nose Landing Gear - Restore MRIP NOTE: 2500 flight cycles. Applicable to serial numbers GLG0007, GLG0008, GLG0023 thru GLG0027, GLG0029, GLG0030, GLG0032 and GLG0033. 60P3222010A008 Note 322002 32-20-00 Nose Landing Gear - Discard MRB Ref: 32-20-00-06 NOTE: In accordance with Airworthiness Limitations. Goodrich C2A4100CA006 Note 322003 32-26-03 Nose Landing Gear Middle Electrical Harness - Discard Goodrich C2E4904CA002 15,400 flight cycles 322618 32-32-04 Main Landing Gear Door Actuator - Discard 60P5280901Z003 7200 flight cycles 323209 323210 MAINTENANCE MANUAL 05-10-00 Page 15 September 30/13 Table 9: Chapter 33 - Lights ATA Ref Component Manufacturer / Part Number Limits CMP Ref 33-42-01 Wing Anticollision / Navigation Light - Discard MRB Ref: 33-40-00-02 Whelen 01-0790453-01 01-0790453-02 20,000 flight hours 334207 334208 33-42-01 Tail Anticollision / Navigation Light - Discard MRB Ref: 33-40-00-02 D3 Technologies 1007-3342A011-001 20,000 flight hours 334215 MAINTENANCE MANUAL 05-10-00 Page 16 September 30/13 Table 10: Chapter 35 - Oxygen ATA Ref Component Manufacturer / Part Number Limits CMP Ref 35-11-01 Crew Oxygen Mask - Restore MRB Ref: 35-10-00-05 Zodiac / Intertechnique MLD20-564 6 years 351103 351104 351105 MAINTENANCE MANUAL 05-10-00 Page 17 September 30/13 Table 11: Chapter 38 - Water / Waste ATA Ref Component Manufacturer / Part Number Limits CMP Ref 38-12-01 Water Sterilizer Quartz Glass Sheath - Restore MRB Ref: 38-10-00-02 International Water-Guard NPS-A6 Sterilizer 3000 flight hours 381219 381220 38-12-01 Water Sterilizer Germicidal Lamp - Discard MRB Ref: 38-10-00-03 International Water-Guard 2-60001-01 3000 flight hours 381233 381234 38-12-01 Water Sterilizer Filter - Discard MRB Ref: 38-10-00-04 International Water-Guard 06-133802-XX 12 months 381237 381238 MAINTENANCE MANUAL 05-10-00 Page 18 September 30/13 Table 12: Chapter 49 - Airborne Auxiliary Power ATA Ref Component Manufacturer / Part Number Limits CMP Ref 49-23-00 Compressor Impeller - Discard MRB Ref: 49-22-00-01 NOTE: In accordance with Airworthiness Limitations. Honeywell WB3822573-1 Note 492300 49-23-00 Second Stage Turbine Rotor - Discard MRB Ref: 49-24-00-01 NOTE: In accordance with Airworthiness Limitations. Honeywell WE897994-3 Note 492302 49-23-00 First Stage Turbine Rotor Disc - Discard MRB Ref: 49-24-00-02 NOTE: In accordance with Airworthiness Limitations. Honeywell WK3840141-3 Note 492301 MAINTENANCE MANUAL 05-10-00 Page 19 September 30/13 Table 13: Chapter 52 - Doors ATA Ref Component Manufacturer / Part Number Limits CMP Ref 52-13-03 Main Entrance Door Latching Actuator - Discard MRIP 60P5210905Z002 5000 flight cycles 521303 52-14-00 Main Entrance Door Damper - Discard 60P5210904Z003 5000 flight cycles 521410 MAINTENANCE MANUAL 05-10-00 Page 20 September 30/13 (2) Hydrostatic Testing of Bottles (Charts and Notes) NOTE: Hydrostatic test and service life requirements of the following bottles are defined by Title 49 CFR § 180.205(c). All cylinders / spheres used as aircraft equipment must be maintained as follows (see Table 14, Table 15 and Table 16): • Department of Transportation (DOT) specification cylinders including spheres must be inspected and tested as required by Title 49 CFR § 180.205. • Cylinders including spheres manufactured under an exemption issued by RSPA must be inspected and tested as required by the terms of the exemption. • All other cylinders including spheres must be inspected and tested as required by Title 49 CFR § 180.205 as it applies to DOT 3HT cylinders, unless alternative testing and inspection procedures are specified by manufacturer or referenced authority. • Operators under Title 14 CFR, Parts 121 / 135 with heavy scheduled maintenance checks that are accomplished in phases or segments are required to have a procedure in place to check cylinders during that phase or segment of their heavy maintenance checks in which maintenance of high- pressure cylinders would normally occur. Refer to FAA Title 49 CFR § 180.205(c) (current revision) or National Airworthiness Authority for additional information. MAINTENANCE MANUAL 05-10-00 Page 21 September 30/13 Table 14: Fire Extinguisher Bottle Maintenance Schedule ATA Ref Component Vendor Name / Part Number Specification Limits CMP Ref Hydrostatic Test Service Life 26-21-03 Engine Fire Bottle - (Hydrostatic) Functional Check MRB Ref: 26-21-00-02 NOTE: Hydrostatic test per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. Pacific Scientific 33800100-1 DOT-E-7945-750 120 months On-condition 262106 262107 26-24-01 Portable Halon Fire Extinguisher - (Hydrostatic) Functional Check MRB Ref: 26-24-00-03 NOTE: Hydrostatic test per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. Kidde 898052 Vendor (Halon) 144 months On-condition 262404 262410 262416 262422 262428 262434 262440 262446 26-24-03 Portable Water Fire Extinguisher - (Hydrostatic) Functional Check MRB Ref: 26-24-00-05 NOTE: Hydrostatic test per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. Kidde 892480 Vendor (Water) 60 months On-condition 262452 MAINTENANCE MANUAL 05-10-00 Page 22 September 30/13 Table 15: Emergency Blow Down Bottle Maintenance Schedule ATA Ref Component Vendor Name / Part Number Specification Limits CMP Ref Hydrostatic Test Service Life 32-39-03 Landing Gear Emergency Extension Nitrogen Blow-down Bottle - (Hydrostatic) Functional Check MRB Ref: 32-39-00-03 NOTE: Hydrostatic test per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. Structural Composites Industries 60P2910072 (A001 / A002) DOT-E-10945 60 months 323912 323913 32-39-03 Landing Gear Emergency Extension Nitrogen Blow-down Bottle - Discard MRB Ref: 32-39-00-04 NOTE: Discard per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. Structural Composites Industries 60P2910072 (A001 / A002) DOT-E-10945 15 years 323910 323911 MAINTENANCE MANUAL 05-10-00 Page 23 September 30/13 Table 16: Oxygen Bottle Maintenance Schedule ATA Ref Component Vendor Name / Part Number Specification Limits CMP Ref Hydrostatic Test Service Life 35-12-01 Crew Oxygen Cylinder - (Hydrostatic) Functional Check MRB Ref: 35-10-00-02 NOTE: Hydrostatic test per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. AVOX 805983-15 DOT-E-10945 60 months 351203 35-12-01 Crew Oxygen Cylinder - Discard MRB Ref: 35-10-00-03 NOTE: Discard per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. AVOX 805983-15 DOT-E-10945 15 years 351202 35-23-01 Passenger Oxygen Cylinder - (Hydrostatic) Functional Check MRB Ref: 35-20-00-02 NOTE: Hydrostatic test per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. AVOX 805983-15 DOT-E-10945 60 months 352303 MAINTENANCE MANUAL 05-10-00 Page 24 September 30/13 Table 16: Oxygen Bottle Maintenance Schedule ATA Ref Component Vendor Name / Part Number Specification Limits CMP Ref Hydrostatic Test Service Life 35-23-01 Passenger Oxygen Cylinder - Discard MRB Ref: 35-20-00-03 NOTE: Discard per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. AVOX 805983-15 DOT-E-10945 15 years 352302 35-31-01 Portable Oxygen Bottle - (Hydrostatic) Functional Check MRB Ref: 35-30-00-02 NOTE: Hydrostatic test per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. AVOX 5600-9M6A-F30N DOT-3AA 60 months (1) 353102 353106 35-31-01 Portable Oxygen Bottle - Discard MRB Ref: 35-30-00-04 NOTE: Discard per Title 49 CFR § 180.205 or National Aviation Authority. If there is no national authority requirement, inspect per manufacturer requirements. AVOX 5600-9M6A-F30N DOT-3AA Note 353103 353107 (1) DOT 3AA cylinders inspection, testing and marking may be requalified every 10 years instead of every 5 years, provided the cylinders conform to Title 49 CFR § section 180.209. MAINTENANCE MANUAL 05-10-00 Page 25 September 30/13 MAINTENANCE MANUAL THIS PAGE IS INTENTIONALLY LEFT BLANK 05-10-00 Page 26 September 30/13 AIRWORTHINESS LIMITATIONS 1. Airworthiness Limitations A. Introduction The Gulftream GVI (G650) 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 2500 flight cycles until certification fatigue testing has been completed and Chapter 5-10-10 has been revised to remove this limitation. 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. As required by the time limited Exemption No. 10622 to 14 CFR Section 25.981(a)(3) cited in the Gulfstream G650 TCDS, operations of this aircraft after September 7, 2015, requires Gulfstream Aerospace demonstrate that the type design of this G650 airplane fully complies with the provisions of that rule at Amendment 25-102. When this demonstration has been completed, this Airworthiness Limitation will be removed. Subsections - Details • 1.B. Airworthiness Limitations 1.B.(1) Safe Life Limits - FAA • Table 1 Chapter 32 - Landing Gear • Table 2 Chapter 49 - Airborne Auxiliary Power 1.B.(2) Safe Life Limits - EASA 1.B.(3) Principal Structural Element Reporting Procedure • Table 3 Principal Structural Element Inspection Results 1.B.(4) Principal Structural Element Inspection Requirements • Table 4 Principal Structural Element Inspection Requirements • 1.C. Certification Maintenance Requirements Table 5 Certification Maintenance Requirements • 1.D. Fuel Tank System Airworthiness Limitations Table 6 Fuel Tank System Airworthiness Limitations • 1.E.Manufacturers Recommended Restoration / Discard Items Table 7 Chapter 36 - Pneumatic Systems B. Airworthiness Limitations Instructions The Airworthiness Limitations Instructions specifically address those items which have been identified, through the certification process, as being safe life (life limited) or damage tolerant and MAINTENANCE MANUAL 05-10-10 Page 1 September 30/13 meet the definition of a PSE. Aircraft without a record of the number of landings may calculate by using a ratio of one (1) flight cycle per two (2) flight hours. NOTE: Mandatory life limitations and inspections, applicable to aircraft certified under EASA Certification Basic Requirements, may differ from those approved by the FAA. Where these limitations or inspection requirements differ, EASA approved data is applicable. Where no supplemental EASA information is provided, FAA approved data is applicable. (1) Safe Life Limits - FAA Safe life limits address those items that have been defined as being life limited. Aircraft operating under the jurisdiction of the FAA shall reference Table 1 thru Table 2 for a listing of safe life limited components, including part number, nomenclature, quantity and mandatory discard times. Table 1:Life Limited Chapter 32 - Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref C1A4100LA002 Main Landing Gear - Discard (1) 1 2500 flight cycles (2) 32-10-00 321010 C1A4100RA002 Main Landing Gear - Discard (1) 1 2500 flight cycles (2) 32-10-00 321011 C1A4300LA002 Main Landing Gear Post Assembly - Discard (1) 1 2500 flight cycles (2) 32-10-00 322719 C1A4300RA002 Main Landing Gear Post Assembly - Discard (1) 1 2500 flight cycles (2) 32-10-00 322723 C1M5300LA001 Main Landing Gear Post Machining - Discard, 32-10-00, Servicing or Code 321013 1 2500 flight cycles (2) 32-10-00 321013 C1M5300RA001 Main Landing Gear Post Machining - Discard 1 2500 flight cycles (2) 32-10-00 321014 C1A4200CA001 Main Landing Gear Shock Absorber - Discard (1) 2 2500 flight cycles (2) 32-12-01 321236 321237 C1M5210CA001 Main Landing Gear Shock Absorber Cylinder Body - Discard 2 2500 flight cycles (2) 32-12-01 321238 321239 C1M5201CA001 Main Landing Gear Shock Absorber Piston Machining - Discard 2 2500 flight cycles (2) 32-12-01 321240 321241 C1M5221CA001 Main Landing Gear Shock Absorber Metering Pin Assembly - Discard 2 2500 flight cycles (2) 32-12-01 321242 321243 (1) Landing gear subassemblies may be tracked separately; however, this does not exclude interfacing and attaching parts, or subassemblies of a landing gear assembly, not listed here, from being subject to the same life limit requirements as the complete main or nose landing gear strut assembly. (2) Landing gear component safe life limit. Current testing and analysis show no life limits less than 2500 Landings. Final limitations will be established upon completion of fatigue tests. These are Airworthiness Limitations. MAINTENANCE MANUAL 05-10-10 Page 2 September 30/13 Table 1:Life Limited Chapter 32 - Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref C1M5205CA001 Main Landing Gear Shock Absorber Cap Machining - Discard 2 2500 flight cycles (2) 32-12-01 322703 322707 C1M5217CA001 Main Landing Gear Shock Absorber Cylinder Nut - Discard 2 2500 flight cycles (2) 32-12-01 322711 322715 C1M5415CA001 Main Landing Gear Shock Absorber Attach Pin - Discard 4 2500 flight cycles (2) 32-12-01 321244 321245 321246 321247 C1M5417CA001 Main Landing Gear Shock Absorber Attach Nut - Discard 4 2500 flight cycles (2) 32-12-01 322767 322771 322775 322779 C1M5310CA002 Main Landing Gear Forward Trunnion Pin - Discard 2 2500 flight cycles (2) 32-15-01 321508 321510 C1M5311CA002 Main Landing Gear Aft Trunnion Pin - Discard 2 2500 flight cycles (2) 32-15-01 321509 321511 C1M5315CA001 Main Landing Gear Spindle Pin - Discard 2 2500 flight cycles (2) 32-14-03 321433 321434 C1M5316CA002 Main Landing Gear Spindle Pin Nut - Discard 2 2500 flight cycles (2) 32-14-03 322727 322731 C1M5313CA001 Main Landing Gear Aft Pintle Pin Nut - Discard 2 2500 flight cycles (2) 32-15-01 322735 322739 C1M5319CA001 Main Landing Gear Forward Pintle Crossbolt - Discard 2 2500 flight cycles (2) 32-15-01 322743 322747 C1M5322CA001 Main Landing Gear Aft Pintle Crossbolt - Discard 2 2500 flight cycles (2) 32-15-01 322751 322755 C1A4400CA001 Main Landing Gear Axle Fitting - Discard (1) 2 2500 flight cycles (2) 32-13-01 321311 321312 C1M5400CA001 Main Landing Gear Trailing Arm Machining - Discard 2 2500 flight cycles (2) 32-13-01 322759 322763 C1M5425CA001 Main Landing Gear Knee Joint Pin - Discard 2 2500 flight cycles (2) 32-13-01 321313 321314 (1) Landing gear subassemblies may be tracked separately; however, this does not exclude interfacing and attaching parts, or subassemblies of a landing gear assembly, not listed here, from being subject to the same life limit requirements as the complete main or nose landing gear strut assembly. (2) Landing gear component safe life limit. Current testing and analysis show no life limits less than 2500 Landings. Final limitations will be established upon completion of fatigue tests. These are Airworthiness Limitations. MAINTENANCE MANUAL 05-10-10 Page 3 September 30/13 Table 1:Life Limited Chapter 32 - Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref C1M5426CA001 Main Landing Gear Knee Joint Retention Pin - Discard 2 2500 flight cycles (2) 32-13-01 322783 322787 C1M5420CA001 Main Landing Gear Brake Torque Takeout Pin - Discard 2 2500 flight cycles (2) 32-13-01 324312 324313 C1A4600CA004 Main Landing Gear Side Brace Actuator - Discard (1) 2 2500 flight cycles (2) 32-14-01 321435 321436 C1M5605CA001 Main Landing Gear Side Brace Actuator Cylinder Machining - Discard 2 2500 flight cycles (2) 32-14-01 322791 322795 C1M5651CA001 Main Landing Gear Side Brace Actuator Piston Machining - Discard 2 2500 flight cycles (2) 32-14-01 322799 322803 C1M5654CA001 Main Landing Gear Side Brace Actuator Lock Spool - Discard 2 2500 flight cycles (2) 32-14-01 322807 322811 C1M5655CA002 Main Landing Gear Side Brace Actuator Locking Segments - Discard 2 2500 flight cycles (2) 32-14-01 322815 322819 C1M5601CA001 Main Landing Gear Side Brace Actuator Cylinder End Cap - Discard 2 2500 flight cycles (2) 32-14-01 321248 321249 C1M5602CA001 Main Landing Gear Side Brace Actuator Cylinder Gland - Discard 2 2500 flight cycles (2) 32-14-01 322823 322827 C1M5670CA001 Main Landing Gear Side Brace Actuator Rod End Machining - Discard 2 2500 flight cycles (2) 32-14-01 322831 322835 C1M5640CA001 Main Landing Gear Side Brace Fitting Pin - Discard 2 2500 flight cycles (2) 32-14-03 321437 321438 C2A4200CA003 Nose Landing Gear Shock Absorber - Discard (1) 1 2500 flight cycles (2) 32-22-01 322203 C2M5200CA001 Nose Landing Gear Cylinder Machining - Discard 1 2500 flight cycles (2) 32-22-01 322507 C2M5206CA002 Nose Landing Gear Metering Pin - Discard 1 2500 flight cycles (2) 32-22-01 322523 C2M5201CA001 Nose Landing Gear Piston Machining - Discard 1 2500 flight cycles (2) 32-23-00 322511 (1) Landing gear subassemblies may be tracked separately; however, this does not exclude interfacing and attaching parts, or subassemblies of a landing gear assembly, not listed here, from being subject to the same life limit requirements as the complete main or nose landing gear strut assembly. (2) Landing gear component safe life limit. Current testing and analysis show no life limits less than 2500 Landings. Final limitations will be established upon completion of fatigue tests. These are Airworthiness Limitations. MAINTENANCE MANUAL 05-10-10 Page 4 September 30/13 Table 1:Life Limited Chapter 32 - Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref C2M5202CA001 Nose Landing Gear Upper Torque Arm - Discard 1 2500 flight cycles (2) 32-22-03 322515 C2M5203CA001 Nose Landing Gear Upper Torque Arm - Discard 1 2500 flight cycles (2) 32-22-05 322519 C2M5235CA001 Nose Landing Gear Lower Torque Arm Attach Pin - Discard 1 2500 flight cycles (2) 32-22-05 322531 C2M5250CA001 Nose Landing Gear Torque Arm Apex Pin - Discard 1 2500 flight cycles (2) 32-22-05 322535 C2E4800CA003 Nose Wheel Steering Equipment Assembly - Discard 1 2500 flight cycles (2) 32-52-03 325208 C2A4300CA001 Nose Landing Gear Trunnion - Discard (1) 1 2500 flight cycles (2) 32-24-01 322434 C2M5300CA001 Nose Landing Gear Trunnion Frame Machining - Discard 1 2500 flight cycles (2) 32-24-01 322539 C2M5310CA001 Nose Landing Gear Trunnion Pin - Discard 2 2500 flight cycles (2) 32-25-01 322588 322589 C2M5311CA001 Nose Landing Gear Retraction Actuator Attach Pin - Discard 1 2500 flight cycles (2) 32-24-01 323811 C2M5312CA001 Nose Landing Gear Cylinder / Trunnion Attach Pin - Discard 1 2500 flight cycles (2) 32-24-01 322428 C2M5314CA001 Nose Landing Gear Cylinder / Trunnion Pin Retaining Bolt - Discard 1 2500 flight cycles (2) 32-24-01 322543 C2A4400CA003 Nose Landing Gear Truss Brace - Discard (1) 1 2500 flight cycles (2) 32-24-05 322547 C2M5400CA001 Nose Landing Gear Truss Brace Forward Machining - Discard 1 2500 flight cycles (2) 32-24-05 322413 C2M5413CA001 Nose Landing Gear Truss Brace Aft Machining - Discard 1 2500 flight cycles (2) 32-24-05 322429 C2M5423CA001 Nose Landing Gear Truss Brace Apex Pin - Discard 2 2500 flight cycles (2) 32-24-05 322436 322551 (1) Landing gear subassemblies may be tracked separately; however, this does not exclude interfacing and attaching parts, or subassemblies of a landing gear assembly, not listed here, from being subject to the same life limit requirements as the complete main or nose landing gear strut assembly. (2) Landing gear component safe life limit. Current testing and analysis show no life limits less than 2500 Landings. Final limitations will be established upon completion of fatigue tests. These are Airworthiness Limitations. MAINTENANCE MANUAL 05-10-10 Page 5 September 30/13 Table 1:Life Limited Chapter 32 - Landing Gear Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref C2M5425CA001 Nose Landing Gear Downlock Apex Pin - Discard 1 2500 flight cycles (2) 32-24-05 322555 C2M5426CA001 Nose Landing Gear Aft Lock Link Pin - Discard 1 2500 flight cycles (2) 32-24-05 322559 C2M5404CA001 Nose Landing Gear Forward Lock Link Machining - Discard 1 2500 flight cycles (2) 32-24-05 322593 C2M5408CA001 Nose Landing Gear Aft Lock Link Machining - Discard 1 2500 flight cycles (2) 32-24-05 322563 C2M5424CA001 Nose Landing Gear Forward Lock Link Pin - Discard 1 2500 flight cycles (2) 32-24-05 322575 C2A4600CA002 Nose Landing Gear Drag Brace - Discard (1) 1 2500 flight cycles (2) 32-24-03 322433 C2M4601CA001 Nose Landing Gear Drag Brace Strut Body - Discard 1 2500 flight cycles (2) 32-24-03 322579 C2M4602CA002 Nose Landing Gear Drag Brace Rod End - Discard 1 2500 flight cycles (2) 32-24-03 322583 C2M4605CA001 Nose Landing Gear Drag Brace Nut - Discard 1 2500 flight cycles (2) 32-24-03 322587 C2M5234CA001 Nose Landing Gear Drag Brace Lower Attach Pin - Discard 1 2500 flight cycles (2) 32-24-03 322527 C2M5419CA001 Nose Landing Gear Drag Brace Attach Long Sleeve - Discard 1 2500 flight cycles (2) 32-24-03 322567 C2M5420CA001 Nose Landing Gear Drag Brace Attach Short Sleeve - Discard 1 2500 flight cycles (2) 32-24-03 322571 C2M5421CA001 Nose Landing Gear Drag Brace Upper Attach Pin - Discard 1 2500 flight cycles (2) 32-24-03 322432 60P3232030Z004 Main Landing Gear Uplock Hook / Latch Assembly - Discard 1 2500 flight cycles (2) 32-33-01 323305 60P3232031Z004 Main Landing Gear Uplock Hook / Latch Assembly - Discard 1 2500 flight cycles (2) 32-33-01 323306 (1) Landing gear subassemblies may be tracked separately; however, this does not exclude interfacing and attaching parts, or subassemblies of a landing gear assembly, not listed here, from being subject to the same life limit requirements as the complete main or nose landing gear strut assembly. (2) Landing gear component safe life limit. Current testing and analysis show no life limits less than 2500 Landings. Final limitations will be established upon completion of fatigue tests. These are Airworthiness Limitations. MAINTENANCE MANUAL 05-10-10 Page 6 September 30/13