Airworthiness Limitations Section P/N G200-1001-09 (Post SB 200-05-280)

repeat interval and Computerized Maintenance Program (CMP) Reference. Table 4 contains a requirement to visually inspect for external damage to the skin of unpainted aircraft. Table 5 contains a list of all CMR tasks. Table 6 contains temporary limitations and inspection requirements. Table 7 contains a list of life limited components. B. Log of Revisions REVISION DESCRIPTION DATE GALAXY 00 Basic Issue 12/15/98 01 Incorporation of SB Galaxy-52A-023. 09/20/99 02 Revision of CMR and addition of Table 8 (relocation of material) 06/30/00 GULFSTREAM 1 (1) Complete change of inspection requirements updated following revision C of report 4AS032/981049, approved with Mod 10021. (2) CMP Ref added in Tables 1 through 6. (3) Addition of CMP Ref in Appendix 1 instead of task numbers. (4) In Appendix 1, CMP 213015 - task name changed to Safety Valve Functional Check. (5) In Appendix 1, CMP 21320 - task name changed to Emergency Battery Capacity Test. (6) Table 7, Baggage Compartment Door, limitation removed SB Galaxy 52A-23, implemented on all affected aircraft. (7) Table 8 renamed to Table 7. 08/30/03 MAINTENANCE MANUAL 05-10-11 Page 4 August 15/25 REVISION DESCRIPTION DATE 2 ALS format changed in section 05-10-10 to become similar to standard Gulfstream Manual format. 08/17/06 3 Added Appendix to 05-10-10. Revision 10 of Appendix 2 Temporary Limitations and Inspection Requirements added to 05-10-10. All future revisions to the Temporary Limitations and Inspections Requirements will be documented on the 05-10-10 Log of Revisions. 10/15/06 4 Temporary Limitation AWL-9 extended to comply at 4800 flight hours. 12/18/07 4-1 ALS Temporary revision 4-1 released in AMM Temporary Revision 5-1. Added AWL-11. Changed Safety Valve Unpressurized - Functional Check from **CMR at 1200 flight hours to *CMR at 300 flight hours. Added Aneroid Switch - Functional Check as a *CMR at 12 months. 08/09/07 4-2 ALS Temporary revision 4-2 released in AMM Temporary Revision 5-2. Added notes to CMR table to clarify accomplishment requirements for Safety Valve and Aneroid Switch checks added in AMM Temp Rev 5-1. 09/20/07 5 (1) Added CAAI approval statement. (2) Editorial corrections to Table 2. (3) Editorial format changes. (4) Changed note to clarify accomplishment requirements for Safety Valve - Functional Test (5) Extended 8 Temporary Limitation AWLs from 3600 flight hours to 7200 flight hours. (6) Added SB 21-327 R1 changing 4 month compliance requirement to 7 months. 12/30/07 6 (1) Reformatted to CAAI requirements. (2) Updated to Continued Air Worthiness Document Revision E and F (approved by Mod G2-10159). (3) MLG Shock Strut Lower Union Bolt Replacement Analysis Revision New. 04/30/09 7 (1) Added ALS inspection reporting instructions. 02/28/2009 8 (1) Editorial changes. 10/31/2011 9 (1) Updated Safety Valve Functional Check and Aneroid Switch Functional Check requirements based on release of SB 200-21-378. 4/30/2012 10 (1) Added compliance statement. (2) Added paragraph for items overdue as a result of revision to ALS. (3) Changed interval for Emergency Battery — Capacity Test based on P/N. (4) Moved Emergency Brakes — Operational Check to 05-20-01. MRB 32-43-00/04 satisfies CCMR. (5) Added Discrete EICAS Display Outputs - Interface Test to CMR Table. 10/28/2012 11 (1) Reformatted tables. (2) Added CMP codes to Main Landing Gear Shock Absorber to Trailing Link Attachment Cross Bolt — Discard. (3) Corrected CMP codes for Main Landing Gear Actuator Attachment Bushing — Discard and FF10 J-Longeron at Aft Bulkhead — NDT Inspection. 10/31/2013 MAINTENANCE MANUAL 05-10-11 Page 5 August 15/25 REVISION DESCRIPTION DATE 12 (1) FF 47 Fuselage Skin Frame Attachment - NDT Inspection, added aircraft effectivity note “Aircraft 004 thru Aircraft 092”. (2) Emergency Battery - Capacity Test, for part number 276CH7 revised interval from “1A” to “1A or 1C whichever occurs. (3) Airworthiness Limitations Section Inspection Reporting Procedure, revised Note to correct FAX number and relocated reporting procedure above Airworthiness Limitations Section Inspections for clarity. 12/15/2014 13 (1) Updated Temporary Limitation and Inspection Requirements Table with the latest Service Bulletin revisions. 08/30/2015 14 (1) Corrected fuselage station for inspection points AF 1.3.2, 1.4.1, 1.4.2 and 1.4.3. (2) Added a visual inspection for E 1.4a Horizontal Stabilizer Aft Attachment Sleeves and Pins. 08/30/2016 15 (1) Clarified the Airworthiness Limitations inspections compliance tolerances. (2) Added illustration to show early inspection compliance tolerances. (3) AWL-10, changed data for SB 53-271 back to what they were prior to Airplane Maintenance Manual Revision 27, to correct error. 07/31/2017 16 (1) W 19, revised initial inspection interval. (2) W 21.1, revised PSE item title, type and repeat interval. (3) W 21.2, revised repeat interval. (4) W 21.3, deleted PSE item (3) W 22, added PSE item. 04/30/2025 C. Airworthiness Limitations — Structural Inspections (1) Airworthiness Limitations Section Inspection 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 (PSE) inspection is accomplished. All discrepancies must be accompanied by digital photograph(s). NOTE: Inspection results, both positive and negative, are to be reported to Gulfstream Maintainability Engineering. Complete Table 2 with inspection results. Return completed table to Gulfstream Maintainability Engineering, maintainability.engineering@gulfstream.com. Discrepancies must be reported within 24 hours. Discrepancies must be accompanied by digital photograph(s). MAINTENANCE MANUAL 05-10-11 Page 6 August 15/25 Table 2: PSE Inspection Results PSE NUMBER CMP 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 (2) Airworthiness Limitations Section Inspections MAINTENANCE MANUAL 05-10-11 Page 7 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat AF 1.1 AF 1.2 AF 1.1, AF 1.2 Fuel Tank Bulkhead FS 520.46 (13220 mm) and Stiffeners Attachment to Bulkhead Web - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 53-31-02 533106 AF 1.3.1 AF 1.3.1 Stiffener BL ±9.05 (±230 mm) at WL 82.06 (2085 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-01 533102 AF 1.3.2 AF 1.3.2 Fuel Tank Bulkhead FS 520.47 (13220 mm) Stiffeners - Visual Inspection NOTE: Aircraft 004 thru Aircraft 037, Aircraft 039. Visual 10000 flight cycles 5000 flight cycles 53-31-02 533110 AF 1.3.3 AF 1.3.3 Fuel Tank Bulkhead FS 520.47 (13220 mm) Stiffeners - Visual Inspection NOTE: Aircraft 038, Aircraft 040 thru Aircraft 999. Visual 10000 flight cycles 5000 flight cycles 53-31-02 533115 AF 1.4.1 AF 1.4.1 Fuel Tank Bulkhead FS 520.47 (13220 mm) for Aircraft 004 thru Aircraft 046 - NDT Inspection NOTE: Aircraft 004 thru Aircraft 046. HFEC 5000 flight cycles 5000 flight cycles 53-31-02 533107 AF 1.4.1 AF 1.4.1 Fuel Tank Bulkhead FS 520.47 (13220 mm) for Aircraft 047 thru Aircraft 999 - Visual Inspection NOTE: Aircraft 047 thru Aircraft 999. Visual 10000 flight cycles 5000 flight cycles 53-31-02 533101 AF 1.4.2 AF 1.4.2 Fuel Tank Bulkhead FS 520.47 (13220 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-02 533108 AF 1.4.3 AF 1.4.3 Fuel Tank Bulkhead FS 520.47 (13220 mm) - X-ray Inspection X-ray 10000 flight cycles 5000 flight cycles 53-31-02 533109 MAINTENANCE MANUAL 05-10-11 Page 8 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat AF 1.5 AF 1.5 Fuel Tank Bulkhead FS 520.46 (13220 mm) Upper and Lower Shroud Fittings - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-31-02 533103 AF 1.6.1 AF 1.6.1 Fuel Tank Bulkhead FS 520.47 (13220 mm) Upper Area - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-31-02 533120 AF 1.6.2 AF 1.6.2 Fuel Tank Bulkhead FS 520.47 (13220 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-31-02 533125 AF 2.1 AF 2.1 Upper Frame FS 530.70 - FS 567.91 (13480 - 14425 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-02 533202 AF 2.2 AF 2.2A AF 2.2, AF 2.2A Side Frames FS 530.70 - FS 567.91 (13480 - 14425 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-02 533203 AF 2.3 AF 2.3 Outer Skin Attachments to Right Side Frames FS 530.70 - FS 567.91 (13480 - 14425 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-01 533104 AF 2.4 AF 2.4 Baggage Compartment Side Frame Attachments - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-02 533204 AF 2.5 AF 2.5 Baggage Compartment Inner Skin to Frame Splice - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-01 533205 AF 2.6 AF 2.6 Baggage Compartment Left Side Frame to Upper Segment Attachments - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-02 533206 AF 2.7 AF 2.7 Baggage Compartment Left Side Frame Outer Flange Attachments - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-02 533207 MAINTENANCE MANUAL 05-10-11 Page 9 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat AF 2.8 AF 2.8 Inner Flange and Strap and Corner Fitting - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-02 533230 AF 3.1 AF 3.1 Baggage Compartment Inner Skin Attachment to Pressure Bulkhead - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 53-32-02 533602 AF 3.2 AF 3.2 Pressure Bulkhead FS 582 (14783 mm) Forward and Aft Webs Attachment to Upper and Lower Cap Crossbeams - NDT / Visual Inspection NOTE: Aircraft 004 thru Aircraft 083. HFEC / Visual 5000 flight cycles 5000 flight cycles 53-33-00 533603 AF 3.2 AF 3.2 Pressure Bulkhead FS 582 (14783 mm) Forward and Aft Webs Attachment to Upper and Lower Cap Crossbeams - NDT / Visual Inspection NOTE: Aircraft 084 thru Aircraft 999. HFEC / Visual 10000 flight cycles 5000 flight cycles 53-33-00 533603 AF 3.2.1 AF 3.2.1 Pressure Bulkhead FS 582 (14783 mm) Aft Crossbeam Fingerplate Attachments (Aircraft 004 thru Aircraft 021) - NDT Inspection NOTE: Aircraft 004 thru Aircraft 021. LFEC 10000 flight cycles 5000 flight cycles 53-33-00 533607 AF 3.2.1 AF 3.2.1 Pressure Bulkhead FS 582 (14783 mm) Aft Crossbeam Fingerplate Attachments (Aircraft 022 thru Aircraft 999) - Visual Inspection NOTE: Aircraft 022 thru Aircraft 999. Visual 10000 flight cycles 5000 flight cycles 53-33-00 533608 MAINTENANCE MANUAL 05-10-11 Page 10 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat AF 3.3.1 AF 3.3.1 Hat Section Stiffeners FS 583.97 (14833 mm) - NDT / Visual Inspection NOTE: Aircraft 004 thru Aircraft 019, Aircraft 021. HFEC / Visual 10000 flight cycles 5000 flight cycles 53-33-00 533604 AF 3.3.2 AF 3.3.2 Hat Section Stiffeners on Pressure Bulkhead at FS 583.96 (14833 mm) - Visual Inspection NOTE: Aircraft 020 and Aircraft 022 thru Aircraft 999. Visual 10000 flight cycles 5000 flight cycles 53-33-00 533605 AF 3.3.3 AF 3.3.3 Hat Section Stiffeners on Pressure Bulkhead at FS 583.96 (14833 mm) - NDT / Visual Inspection Visual Borescope / HFEC 10000 flight cycles 5000 flight cycles 53-33-00 533606 AF 3.4 AF 3.5 AF 3.6 AF 3.7 AF 3.8 AF 3.4, AF 3.5, AF 3.6, AF 3.7 and AF 3.8 Pressure Bulkhead at FS 582 (14783 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-33-00 533209 AF 4 AF 4 Baggage Door Cutout - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-00 533213 AF 5.1 AF 5.1 Forward Engine Support Adapter Plate - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-33-00 533215 AF 5.2 AF 5.2 Forward Engine Support Adapter Plate Walls and Ribs - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-33-00 533216 AF 5.3 AF 5.3 Adapter Plate Shear Pin Holes - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-33-00 533217 AF 5.4 AF 5.4 Forward Engine Support End Plate - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-33-00 533218 MAINTENANCE MANUAL 05-10-11 Page 11 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat AF 5.5 AF 5.5 Forward Beam to Fuselage Bulkhead Attachment - NDT Inspection NOTE: Except Aircraft 038. HFEC 10000 flight cycles 5000 flight cycles 53-33-00 533219 AF 5.5 AF 5.5 Forward Beam to Fuselage Bulkhead Attachment - NDT Inspection NOTE: Aircraft 038 only. HFEC / Visual 10000 flight cycles 5000 flight cycles 53-33-00 533219 AF 5.6 AF 5.6 Forward Beam Web - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-33-00 533221 AF 5.7 AF 5.7 Forward Engine Mount Adapter Plate Bolts and Shear Pins - NDT Inspection Magnetic Particle 10000 flight cycles 5000 flight cycles 53-33-00 533222 AF 6.1 AF 6.1 Aft Engine Support Fitting - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-33-00 533223 AF 6.2 AF 6.2 Aft Engine Support Fitting - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-33-00 533224 AF 7.1 AF 7.1 Baggage Door Hinges and Goosenecks - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-32-00 533240 AF 7.2 AF 7.2 Baggage Door Latch and Shaft - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-32-00 533241 AF 8 AF 8 Fuselage Skin Lower Cutout Corner - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 53-34-01 533105 AF 9 AF 9 Frame FS 664.83 (16887 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-34-02 533226 AF 10 AF 10 Frame FS 703.77 (17876 mm) Flange - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-34-02 533228 AF 11 AF 11 Frame FS 717.36 (18221 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-34-02 533229 MAINTENANCE MANUAL 05-10-11 Page 12 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat AF 12 AF 12 Aft Fuselage Diverter - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-30-00 533231 CTS 1 CTS 1 Spars Lower Flanges to Lower Skin Attachment - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-22-00 531202 CTS 2 CTS 2 Front Spar - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-22-00 531203 CTS 3 CTS 3 Aft and Rear Spar Webs - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-22-00 531204 CTS 4 CTS 4 Lower Skin to Wing Attachment - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 53-22-00 531205 CTS 5 CTS 5 Corner Beam - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-22-00 531206 CTS 6 CTS 6 Lower Skin Panels - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 53-22-00 531207 CTS 7 CTS 7 Shear Clips at CTS Rib 925, Left and Right Side - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-22-00 531208 E 1.1 E 1.1 Horizontal Stabilizer Aft Attachment Lug Fittings - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-10-00 551402 E 1.2 E 1.2 Horizontal Stabilizer Attachment Fittings - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-10-00 551403 E 1.3 E 1.3 Vertical Stabilizer Attachment Fittings - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 551404 MAINTENANCE MANUAL 05-10-11 Page 13 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat E 1.4a E 1.4a Horizontal Stabilizer Aft Attachment Sleeves and Pins - Visual Inspection NOTE: Accomplish a one-time inspection at 5000 flight cycles. For aircraft beyond 5000 flight cycles at publication date of Revision 28, accomplish at next due periodic inspection. Aircraft having incorporated SB 200-55-413 at 5000 or more flight cycles already comply with this requirement. For the “repeat” inspection for this location, see E 1.4. Visual Note Note 55-10-00 551020 E 1.4 E 1.4 Horizontal Stabilizer Aft Attachment Sleeves and Pins - NDT Inspection Magnetic Particle 10000 flight cycles 5000 flight cycles 55-10-00 551405 E 1.5 E 1.5 Horizontal Stabilizer Aft Spar - NDT Inspection (Aircraft 004 thru Aircraft 027) NOTE: Aircraft 004 thru Aircraft 027. HFEC / LFEC 7500 flight cycles 2500 flight cycles 55-10-00 551406 E 1.5a E 1.5a Horizontal Stabilizer Aft Spar - NDT Inspection (Aircraft 028 thru Aircraft 999) NOTE: Aircraft 028 thru Aircraft 999. HFEC / LFEC 10000 flight cycles 5000 flight cycles 55-10-00 551410 E 1.5b E 1.5b Horizontal Stabilizer Aft Spar - NDT Inspection HFEC / LFEC 10000 flight cycles 5000 flight cycles 55-10-00 551411 MAINTENANCE MANUAL 05-10-11 Page 14 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat E 1.6 E 1.6 Vertical Stabilizer Fitting Attachment Bolts - NDT / Visual Inspection LFEC / HFEC / Visual 10000 flight cycles 5000 flight cycles 55-30-00 551408 E 2 E 2 Horizontal Stabilizer Actuator, Upper Attachment - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-10-00 551407 E 3 E 3 Horizontal Stabilizer Skin / Spar Attachments - NDT / Visual Inspection LFEC / HFEC / Visual 10000 flight cycles 5000 flight cycles 55-10-00 551201 E 4 E 4 Horizontal Stabilizer Upper Skin Cutout - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-10-00 551101 E 5.1 E 5.1 Elevator Support Structure Hinge Support Fittings - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-20-00 552401 E 5.2 E 5.2 Elevator Support Structures, Actuator and Link Fittings - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-20-00 552405 E 6.1 E 6.1 Vertical Stabilizer Aft Spar Attachment at FS 704 (17876 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553402 E 6.2 E 6.2 Vertical Stabilizer Forward Spar Attachment at FS 665 (16886 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553403 E 6.3 E 6.3 Vertical Stabilizer Aft Spar Attachment at FS 704 (17876 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553404 E 6.4 E 6.4 Vertical Stabilizer Forward Spar Attachment at FS 665 (16886 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553405 MAINTENANCE MANUAL 05-10-11 Page 15 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat E 6.5 E 6.5 Vertical Stabilizer Aft Spar Attachment at FS 665 (16886 mm) and FS 704 (17876 mm) - NDT Inspection Magnetic Particle 10000 flight cycles 5000 flight cycles 55-30-00 553406 E 7 E 7 Vertical Stabilizer Rib No. 1 Cutouts - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-30-00 553201 E 8.1 E 8.1 Horizontal Stabilizer Actuator, Lower Attachment - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-10-00 551002 E 8.2 E 8.3 E 8.2 and E 8.3 Center U-fitting 3/8 and 5/16 inch Bolt Hole - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-10-00 551003 551004 E 9 E 9 Rudder Support Structures, Hinge Support Fittings - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-40-00 553005 E 10.1 E 10.1 Rudder Attachment Lugs - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-40-00 554402 E 10.2 E 10.2 Rudder External Structure - NDT / Visual Inspection Ultrasonic / Visual / Tap Test 10000 flight cycles 5000 flight cycles 55-40-00 554101 E 11.1 E 11.1 Elevator Attachment Lugs - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 55-20-00 552001 E 11.2 E 11.2 Elevator External Structure - NDT / Visual Inspection NOTE: Next inspections (not intervals) are due at 12500, 17500 and 20000 accumulated flight cycles. Ultrasonic / Visual / Tap Test 7500 flight cycles Note 55-20-00 552002 FF 1.1 FF 1a Forward Pressure Bulkhead - NDT / Visual Inspection HFEC / Visual 5000 flight cycles 5000 flight cycles 53-12-02 531001 MAINTENANCE MANUAL 05-10-11 Page 16 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat FF 1.2 FF 1b Forward Pressure Bulkhead - NDT / Visual Inspection HFEC / Visual 5000 flight cycles 5000 flight cycles 53-12-02 531007 FF 1.3 FF 1c Forward Pressure Bulkhead at FS 105.07 (2669 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-12-02 531008 FF 2.1 FF 2.1 Canopy Posts and Sills - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-12-03 531002 FF 2.2 FF 2.2 Cockpit Lower Sill Beam - NDT Inspection HFEC / LFEC 10000 flight cycles 5000 flight cycles 53-12-03 531009 FF 2.3 FF 2.3 Canopy Frame FS 156.8 (3982 mm) - NDT Inspection NOTE: Next inspection (not intervals). Operator may choose one of the proposed two options: • 10000, 15000, 20000 accumulated flight cycles • 12500, 17500, 20000 accumulated flight cycles HFEC / LFEC 7500 flight cycles Note 53-12-03 531010 FF 2.4 FF 2.4 Canopy Cockpit Lower Sill Beam - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-12-03 531011 FF 3 FF 3 Nose Landing Gear Wheel Well Cutout - NDT Inspection HFEC / LFEC 10000 flight cycles 5000 flight cycles 53-10-00 531003 FF 4 FF 4 Nose Landing Gear Lower Longerons - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-10-00 531004 FF 5 FF 5 Entrance Door Cutout - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-10-00 531005 FF 6 FF 6 Emergency Exit Cutout - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-21-00 531006 MAINTENANCE MANUAL 05-10-11 Page 17 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat FF 7 FF 7 Cabin Window Cutouts - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-13-03 532001 FF 9 FF 9 Upper J-Longeron Splices - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 53-13-01 532301 FF 10 FF 10 J-Longeron at Aft Bulkhead - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-21-02 532302 FF 11 FF 11 Cabin Frame Splices - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-21-02 532201 FF 12 FF 13 FF 12, FF 13 Fuselage Frame Fittings and Splices - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-20-00 532202 FF 14 FF 14 Side Frame Attachments - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-21-02 532503 FF 16a FF 16a Pressure Floor to Aft Pressure Bulkhead Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-21-02 532501 FF 16b FF 16b Pressure Floor Fitting Attachment - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-21-02 532504 FF 18 FF 18 Cabin Skin Longitudinal Splices - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-13-01 532102 FF 20.1 FF 20.1 Aft Pressure Bulkhead FS 482.67 (12260 mm) Circumferential Splice of Cabin Skin - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-31-02 533301 FF 20.2 FF 20.2 Aft Pressure Bulkhead at FS 482.67 (12260 mm) Upper Area - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-31-02 533303 MAINTENANCE MANUAL 05-10-11 Page 18 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat FF 20.2 FF 20.2 Aft Pressure Bulkhead at FS 482.67 (12260 mm) Upper Area - NDT Inspection NOTE: X-Ray is acceptable alternate NDI if HFEC cannot be applied. HFEC 5000 flight cycles 5000 flight cycles 53-31-02 533302 FF 20.3 FF 20.3 Aft Pressure Bulkhead at FS 482.67 (12260 mm) Upper Area - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-02 533304 FF 20.4 FF 20.4 Aft Pressure Bulkhead Upper Area - NDT / X-ray Inspection HFEC / X-ray 10000 flight cycles 5000 flight cycles 53-31-02 533305 FF 23 FF 23 Pressure Floor Beams and Skin FS 461.34 - FS 471.26 (11718 - 11970 mm) - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-21-04 532502 FF 30 FF 30 Flight Compartment Below Floor - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-12-04 531501 FF 31.1 FF 31.1 Side Frame FS 139 (3533 mm) - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-12-02 531211 FF 31.2 FF 31.2 Cockpit Side Frame at FS 113.03 - FS 177.87 (2871 mm - 4518 mm) - NDT Inspection HFEC 5000 flight cycles 2500 flight cycles 53-12-02 531210 FF 32a FF 32a Emergency Exit Door Stop Fittings Attachment - NDT Inspection NOTE: Aircraft 004 thru Aircraft 008, Aircraft 010. HFEC 3600 flight cycles 3600 flight cycles 52-20-00 522201 FF 32b FF 32b Emergency Exit Door Stop Fittings Attachment - Visual Inspection NOTE: Aircraft 009, Aircraft 011 thru Aircraft 999. Visual 10000 flight cycles 5000 flight cycles 52-20-00 522202 MAINTENANCE MANUAL 05-10-11 Page 19 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat FF 32c FF 32c Emergency Exit Door Stop Fittings - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 52-20-00 522203 FF 33 FF 33 Emergency Door Stoppers - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 52-20-00 522204 FF 40 FF 40 Upper Main Entrance Door Stop Fittings - NDT / Visual Inspection Magnetic Particle / Visual 5000 flight cycles 5000 flight cycles 53-10-00 532203 FF 42 FF 42 Cockpit Side Window Retainer - Visual Inspection Visual 5000 flight cycles 5000 flight cycles 53-12-03 532206 FF 44 FF 44 Nose Landing Gear Bay Bulkheads - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-10-00 532207 FF 45 FF 45 Nose Landing Gear Walls - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 53-10-00 532208 FF 47 FF 47 Fuselage Skin Frame Attachment - NDT Inspection NOTE: Aircraft 004 thru Aircraft 092. Next inspection (not intervals) is due at 10000, 15000, and 20000 accumulated flight cycles. HFEC 7500 flight cycles Note 53-13-00 532209 NLG 1 NLG 1 Nose Landing Gear Trunnion Attach Fittings - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 32-20-00 320101 NLG 2 NLG 2 Nose Landing Gear Drag Brace Attach Fittings - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 32-20-00 320102 MLG 1 MLG 1 Main Landing Gear Side Brace Supporting Structure - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 32-10-00 320103 MAINTENANCE MANUAL 05-10-11 Page 20 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat MLG 2 MLG 2 Main Landing Gear Trunnion Attach Fitting on Rear Spar - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 32-10-00 320104 MLG 3 MLG 3 Main Landing Gear Trunnion Attach Fitting on Center Spar - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 32-10-00 320105 W 1 W 1 Front Spar to CTS Attachment - NDT Inspection HFEC / X-ray 10000 flight cycles 5000 flight cycles 57-11-00 571601 W 2 W 2 Center Spar to CTS Attachment - NDT Inspection HFEC / X-ray 10000 flight cycles 5000 flight cycles 57-13-00 571602 W 3 W 3 Lower Skin Access Cutout Edges - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 57-15-00 571101 W 4.1 W 4.1 Lower Skin Splice at Rib 2 - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 57-15-00 571102 W 4.2 W 4.2 Lower Skin Splice near Rib 2 - Outboard Skin Panels - NDT Inspection NOTE: Aircraft 004 thru Aircraft 037. LFEC 7500 flight cycles 2500 flight cycles 57-15-00 571103 W 4.3 W 4.3 Lower Skin Splice near Rib No. 2 - Inboard Skin Panels - Visual Inspection NOTE: Aircraft 004 thru Aircraft 037. Visual 10000 flight cycles 5000 flight cycles 57-00-00 571104 W 4.4 W 4.4 Lower Skin Step Fillet near Rib 2 - NDT Inspection NOTE: Aircraft 004 thru Aircraft 037. HFEC 5000 flight cycles 5000 flight cycles 57-15-00 571105 W 4.5 W 4.5 Lower Skin Center Spar Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-15-00 571107 MAINTENANCE MANUAL 05-10-11 Page 21 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat W 4.6 W 4.6 Center Spar Lower Flange Aircraft 004 thru Aircraft 037 - NDT Inspection NOTE: Aircraft 004 thru Aircraft 037. LFEC 7500 flight cycles 2500 flight cycles 57-15-00 571108 W 4.6 W 4.6 Center Spar Lower Flange Aircraft 038 thru Aircraft 999 - NDT Inspection NOTE: Aircraft 038 thru Aircraft 999. LFEC 7500 flight cycles 5000 flight cycles 57-15-00 571109 W 5 W 5 Front Spar Splice at Rib 6 - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 57-11-00 571201 W 6 W 6 Rear Spar Splice at Rib 6 - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 57-12-00 571202 W 7 W 7 Wing, Lower Skin Panels - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-00-00 571106 W 8 W 8 Lower Skin at Front Spar Attachment between Rib 2 and Rib 18 - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 57-15-00 571203 W 9 W 9 Lower Skin at Rear Spar Attachment between Rib 2 and Rib 18 - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 57-15-00 571204 W 10 W 10 Lower Skin Longitudinal Splices - Visual Inspection NOTE: Aircraft 004 thru Aircraft 019. Visual 10000 flight cycles 5000 flight cycles 57-15-00 571205 W 11 W 11 Winglet Attachment - NDT / Visual Inspection Visual / X-ray 10000 flight cycles 5000 flight cycles 57-30-00 573401 W 12 W 12 Krueger Flap Attachment Fittings and Krueger Actuator Fitting - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-40-00 573402 MAINTENANCE MANUAL 05-10-11 Page 22 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat W 13.1 W 13.1 Flap Rails - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-50-00 573403 W 13.2 W 13.2 Flap Actuator Access Panels and Rib No. 10 and Rib No. 11 Flange Connect to Intermediate Panel - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-50-00 573404 W 13.3 W 13.3 Outboard Flap Upper Surface - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-30-00 573405 W 14.1 W 14.1 Slat Lower Spar, Flange / Skin Attachment - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-40-00 575101 W 14.2 W 14.2 Slat Rails - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-40-00 575102 W 15.1 W 15.1 Aileron Main Hinge Assembly - Visual Inspection NOTE: Aircraft 004 thru Aircraft 034. Visual 10000 flight cycles 5000 flight cycles 57-60-00 576001 W 15.1a W 15.1a Aileron Main Fitting of Actuator - Visual Inspection NOTE: Aircraft 035 thru Aircraft 999. Visual 10000 flight cycles 5000 flight cycles 57-60-00 576004 W 15.2 W 15.2 Aileron External Structure - NDT / Visual Inspection Ultrasonic / Visual / Tap Test / X-ray 10000 flight cycles 5000 flight cycles 57-60-00 576002 W 15.3 W 15.3 Aileron Actuator Bracket Lug - NDT / Visual Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 57-60-00 576003 W 16 W 16 Wing Lower Skin - Drain Hole Near Rib 0 - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-15-00 571501 MAINTENANCE MANUAL 05-10-11 Page 23 August 15/25 Table 3: Airworthiness Limitations PSE Number Description Aircraft Maintenance Manual Procedure NDI Type Inspection Interval ATA Ref CMP Ref Initial Repeat W 17 W 17 Open Holes in Rear Spar Web Between Rib No. 18 and No. Rib 19 - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-00-00 571206 W 18 W18 Cutouts in Front Spar Web Between Rib No. 18 and Rib No. 19 - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 57-00-00 571301 W 19 W 19 Wing Lower Skin Longitudinal Splices - NDT Inspection HFEC / LFEC 10000 flight cycles 5000 flight cycles 57-15-00 571302 W 20 W 20 Rear Spar Web - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 57-15-00 571303 W 21.1 W 21.1 Air Brakes Hinge - NDT Inspection HFEC 10000 flight cycles 2500 flight cycles 57-70-00 571304 W 21.2 W 21.2 Air Brakes Actuator Fitting - NDT Inspection HFEC 10000 flight cycles 2500 flight cycles 57-70-00 571305 W 21.3 Task Deleted. HFEC / Dye Penetrant 571306 W 22 W 22 Front Spar Web Cutouts Between Ribs 6 - 22 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-00-00 570050 MAINTENANCE MANUAL 05-10-11 Page 24 August 15/25 (3) Unpainted Aircraft Table 4: Unpainted Aircraft PS No. Inspection Description Inspection Interval PS25.2200 Visual inspection of external skin for finish treatment for lack of corrosion, weathering damage and abrasion (paragraph 8.3). Correct damage if found (paragraphs 10 through 14). 1 week or 40 Flight Hour, which ever occurs first D. Certification Maintenance Requirements (CMR) (1) Introduction The following presents a list of all Gulfstream G200 Certification Maintenance Requirements (CMR), based on safety analyses, performed to meet requirements of CFR / JAR 25.1529, Instructions for Continued Airworthiness and other relevant requirements and engineering judgement. (2) Types The Certification Maintenance Requirements (CMRs) are categorized into two types of CMR tasks as follows: • One Star CMR’s (*) - The tasks and intervals specified are mandatory and cannot be changed, escalated, or deleted without the concurrence of the responsible Aircraft Certification Authority (CAAI) • Two Star CMR’s (**) - Task intervals may be adjusted in accordance with operator’s approved escalation practices or an approved reliability program, but the task may not be changed or deleted without prior CAAI approval (3) Maintenance Tasks All CMR tasks are listed in Table 5. NOTE: Unless otherwise specified, task may be performed with a scheduling window as follows: • ±50 flight hours, not to exceed the task interval +50 flight hours between inspections • ±1 calendar month, not to exceed the task interval +1 calendar month between inspections • C checks or monthly inspections may be accomplished on any day of the calendar month that they are due MAINTENANCE MANUAL 05-10-11 Page 25 August 15/25 Table 5: Certification Maintenance Requirements (CMR) ATA Ref Description Type CMP Ref Initial / Repeat 21-30-00 Safety Valve - Functional Check MRB Ref: 21-30-00/02 NOTE: Interval is 1A for Aircraft 004 thru Aircraft 249 Pre-SB 200-21-378, and 5A for Aircraft 250 and Aircraft 004 thru Aircraft 249 Post SB 200-21-378. Perform next due Functional Check from time of last accomplishment. * 213052 Note 21-30-00 Discrete EICAS Display Outputs - Interface Test ** 213050 2A 21-30-07 Aneroid Switch - Functional Check MRB Ref: 21-30-00/07 NOTE: This requirement applies to Aircraft 004 thru Aircraft 249 Pre-SB 200-21-378 only. Perform at 1A following date of Revision 23, not to exceed 12 months from date of last accomplishment. ** 213302 1A 24-30-00 Load Shedding - Operational Test ** 243008 1A 24-30-20 Emergency Battery - Capacity Test MRB Ref: 24-30-00/01 NOTE: For part number 2778-18 accomplish is 300 flight hours or 6 months, whichever occurs first. For part number 276CH7 accomplish at 1A or 1C whichever occurs first. Perform next due Capacity Test from time of last accomplishment. ** 243020 Note 24-30-51 Contactor and Relay Boxes - Visual Inspection ** 243029 4C 27-10-00 Aileron Disconnect System - Operational Test MRB Ref: 27-10-00/02 * 271019 2A 27-10-75 Aileron Hydraulic System Volume and Dampener - Inspection * 271423 271424 6A 27-20-16 Rudder Trim Actuator Attach Points and Electrical Connectors - Inspection * 272046 2A 27-30-00 Elevator Pitch Disconnect Function - Operational Check MRB Ref: 27-30-00/03 * 273020 2A 27-30-55 Elevator Servo Actuator Compensator Volume and Dampener - Check * 273411 273412 6A MAINTENANCE MANUAL 05-10-11 Page 26 August 15/25 Table 5: Certification Maintenance Requirements (CMR) ATA Ref Description Type CMP Ref Initial / Repeat 32-30-00 Emergency Landing Gear System - Functional Check MRB Ref: 32-30-00/05 NOTE: Interval is 4A or 3C, whichever occurs first. Accomplish next due at Landing Gear Emergency Extension Bottle Hydrostatic Functional Check (CMP 323904), not to exceed 4A since last accomplishment. ** 323009 Note 78-30-00 Thrust Reverser Actuator Mechanism - Visual Inspection ** 783013 783014 1A 78-31-05 Thrust Reverser Actuator - Visual Inspection ** 783015 783016 1A 78-31-30 Hydraulic Control Unit - Visual Inspection ** 783017 783018 1A E. Temporary Limitation and Inspection Requirements Service Bulletins that are part of Gulfstream’s recommended inspection program are listed in Table 6: Temporary Limitation and Inspection Requirements. This table will be reviewed and updated periodically based on new requirements and compliance information received from the fleet. NOTE: If there are differences between required compliance times or recurring intervals in the individual Service Bulletins and the Temporary Limitation and Inspection Requirements section of the ALS, the ALS shall take precedence. MAINTENANCE MANUAL 05-10-11 Page 27 August 15/25 Table 6: Temporary Limitation and Inspection Requirements AWL NO. REPORT NO. (LATEST REVISION) CMP DESCRIPTION EFFECTIVITY INTERVAL TO COMPLY WITHIN LIFE LIMIT AWL-4 MOD 7147 SB 27 - 055 980550 Replace type of fasteners attaching pedal torque tube upper bracket to forward pressure bulkhead. Aircraft 004 thru Aircraft 022 — 1200 flight hours or 2A Inspection, whichever comes first — AWL-5 MOD 5013 SB 27 - 052 970520 Installation of additional idler pully at FS 480.7 (11210 mm). Aircraft 004 thru Aircraft 021 — 3500 flight hours not to exceed 3600 — AWL-5 MOD 5026 SB 27 - 057 970570 970571 (R1) Replace bolt in right tension regulator lower case guard. Aircraft 004 thru Aircraft 022 — 1200 flight hours or 2A Inspection, whichever comes first — AWL-5 MOD 7097, 7088 SB 53 - 039 970390 970391 Replace splice at bulkhead FS 520.5 (13220 mm) and add reinforcing stiffeners at bulkhead FS 582 (14783 mm). Aircraft 005 thru Aircraft 011 — 7000 flight hours not to exceed 7200 — AWL-5 MOD 7149 SB 52 - 040 970400 Rework brackets on emergency exit door. Aircraft 004, Aircraft 006 thru Aircraft 016 — 1000 flights — Aircraft 005 — 1500 flights — AWL-5 MOD 7153 SB 55 - 042 970420 Install passivated washers on vertical stabilizer attach fittings. Aircraft 004 thru Aircraft 023 — No later than December 31, 2001 — MAINTENANCE MANUAL 05-10-11 Page 28 August 15/25 AWL NO. REPORT NO. (LATEST REVISION) CMP DESCRIPTION EFFECTIVITY INTERVAL TO COMPLY WITHIN LIFE LIMIT AWL-6 MOD 7144 SB 21 - 079 970790 970791 Baggage compartment differential pressure reduction. Aircraft 004, Aircraft 006, Aircraft 008 thru Aircraft 033 — Next 1A or 2A Inspection, whichever comes first — Aircraft 005, Aircraft 007 — 1500 flights — AWL-6 MOD 7181 SB 53 - 084 970840 Rudder control arm installation redesigned at FS 591.5 (15025 mm). Aircraft 004 thru Aircraft 006, Aircraft 008 thru Aircraft 033 — Next 1A Inspection — AWL-7 MOD 5058 SB 52 - 100 981000 New drain holes in the inner frames of the entry door. Aircraft 004 thru Aircraft 043 — Next 2A Inspection — AWL-7 MOD 5061 SB 53 - 054 980540 Improvement of electrical grounding of power cables. Aircraft 004 thru Aircraft 045 — Part A: 50 flight hours Part B: 300 flight hours or next A Inspection whichever comes first — AWL-7 MOD 5022, 7101 SB 29 - 028 970280 FQMC software update. Aircraft 004 thru Aircraft 039 — Next 1A Inspection not to exceed 12 months — AWL- 7 MOD 7104 SB 53 - 081 970810 970811 Baggage compartment shroud installation change. Aircraft 004 thru Aircraft 029 — 7000 flight hours not to exceed 7200 — MAINTENANCE MANUAL 05-10-11 Page 29 August 15/25 AWL NO. REPORT NO. (LATEST REVISION) CMP DESCRIPTION EFFECTIVITY INTERVAL TO COMPLY WITHIN LIFE LIMIT AWL-7 MOD 7137 SB 53 - 061 970610 970611 Cockpit structure reinforcement - forward pressure bulkhead and lower sill. Aircraft 004 thru Aircraft 026 — 7000 flight hours not to exceed 7200 — AWL-7 MOD 7158 SB 53 - 075 970750 Aft cabin pressure bulkhead reinforcement FS 482.7 (12260 mm). Aircraft 004 thru Aircraft 031, Aircraft 033 — 7000 flight hours not to exceed 7200 — AWL-7 MOD 7178 SB 53 - 061 970610 970611 Reinforcement of forward pressure bulkhead stiffeners. Aircraft 004 thru Aircraft 034 — 7000 flight hours not to exceed 7200 — AWL-7 MOD 7179 SB 53 - 061 970610 970611 Reinforcement of frame at FS 156.8 (3982 mm) in the canopy left and right side. Aircraft 004 thru Aircraft 034 — 7000 flight hours not to exceed 7200 — AWL-8 MOD 5041 SB 53 - 108 971080 971081 Replacement of fasteners in cockpit floor. Aircraft 004 thru Aircraft 030 — 7000 flight hours not to exceed 7200 — AWL-8 MOD 5062 SB 53 - 105 981050 Surface finish of the edge radius of the nose landing gear by corner changed from 125 micro-inch to 63 micro-inch. Aircraft 004 thru Aircraft 044 — 1200 flight hours or next 2A Inspection — AWL-8 MOD 7169 SB 78 - 096 970960 Thrust Reverser - incorporation of time delay to prevent re-stow of thrust reverser on landing. Aircraft 004 thru Aircraft 036 — 300 flight hours or Next 1A Inspection whichever comes first — MAINTENANCE MANUAL 05-10-11 Page 30 August 15/25 AWL NO. REPORT NO. (LATEST REVISION) CMP DESCRIPTION EFFECTIVITY INTERVAL TO COMPLY WITHIN LIFE LIMIT AWL-8 MOD 7217 SB 53 - 116 971160 971161 Material change of upper longeron splice. Aircraft 004 thru Aircraft 052 — 7000 flight hours not to exceed 7200 — AWL- 9R1 MOD 7229 SB 53 - 121 971210 971211 Canopy lower sill reinforcement Aircraft 004 thru Aircraft 059 — 7000 flight hours not to exceed 7200 — AWL-10 SB 53A - 270 990300 Aft lower skin diverter - one-time inspection Aircraft 004 thru Aircraft 122 — Within 30 days after SB release — MOD G2 - 10126 SB 53 - 271 982710 Aft lower skin - reinforce diverter installation Aircraft 004 thru Aircraft 122 — 300 flight hours or next 1A — AWL-11 SB 200-21-327R1 983271 Test of Cabin Pressure Controller P/N 2119922-6 Series 1 and P/N 2119922-7 Series 1 for leakage. Aircraft 004 thru Aircraft 171 — Within next 7 months of Service Bulletin or at Aircraft completion prior to delivery — MAINTENANCE MANUAL 05-10-11 Page 31 August 15/25 F. Safe Life Limits The safe life limits section addresses those items that have been defined as being life limited. As shown in the life limited component table (Table 7) in this section, the item description, part number, mandatory replacement time and CMP codes are included. Table 7: Life Limited Components Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref 26100-000-01 26100-100-00 26105-000-00 27105-000-00 27100-000-01 27100-100-00 Main Landing Gear Shock Strut Assembly - Discard 2 17,500 flight cycles 32-10-05 321021 321022 26200-000-01 26200-100-00 Main Landing Gear Shock Absorber - Discard 2 17,500 flight cycles 32-10-25 321025 321026 26300-000-XX 27300-000-XX Main Landing Gear Actuator - Discard 2 17,500 flight cycles 32-10-20 321027 321028 26125-000-00 27125-000-00 Main Landing Gear Trailing Link Assembly - Discard 2 17,500 flight cycles 32-13-01 321303 321304 4AS2530005-001 Main Landing Gear Actuator Attachment Bushing - Discard 2 17,500 flight cycles 32-10-20 321029 321030 4AS2530004-001 Main Landing Gear Actuator Attachment Pin - Discard 2 17,500 flight cycles 32-10-20 321031 321032 26022-000-00 26021-000-00 Main Landing Gear Trunnion Pins - Discard 2 17,500 flight cycles 32-10-05 321033 321034 321035 321036 26023-000-00 Main Landing Gear Trailing Link Pin - Discard 2 17,500 flight cycles 32-13-01 321307 321308 NAS6204-34D 26179-000-00 Main Landing Gear Lower Shock Absorber Attachment Cross Bolt - Discard NOTE: Accomplish at 800 flights from installation or new. Aircraft beyond 800 cycles at publication of Rev 17, accomplish at next scheduled Main Landing Gear Assembly Lubrication. 2 800 flight cycles 32-10-25 321041 321042 MAINTENANCE MANUAL 05-10-11 Page 32 August 15/25 Table 7: Life Limited Components Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref 28100-000-01 28100-100-XX Nose Landing Gear Shock Absorber Assembly - Discard NOTE: The following life limited items are discarded as part of this assembly: • 28115-100-00 • 28190-000-00 • 23115-000-00 • 23343-000-00 1 20000 flight cycles 32-20-10 322018 28200-000-00 Nose Landing Gear Drag Brace Assembly - Discard NOTE: The following life limited items are discarded as part of this assembly: • 23325-300-1 • 23325-300-2 • 23245-300-00 • 23231-000-00 • 23233-000-00 1 20000 flight cycles 32-20-15 322021 28190-000-00 Nose Landing Gear Upper Torque Link - Discard 1 20000 flight cycles 32-20-12 322032 23115-000-00 Nose Landing Gear Lower Torque Link - Discard 1 20000 flight cycles 32-20-12 322034 23343-000-00 Nose Landing Gear Torque Link Pin - Discard 1 20000 flight cycles 32-20-12 322036 322030 23211-000-00 Nose Landing Gear Drag Brace Trunnion Pins - Discard 2 20000 flight cycles 32-20-15 322023 322024 28113-000-01 Nose Landing Gear Strut Trunnion Pins - Discard 2 20000 flight cycles 32-20-05 322057 322058 23202-000-00 Nose Landing Gear Drag Brace Strut Pin - Discard 1 20000 flight cycles 32-20-15 322052 MAINTENANCE MANUAL 05-10-11 Page 33 August 15/25 MAINTENANCE MANUAL THIS PAGE IS INTENTIONALLY LEFT BLANK 05-10-11 Page 34 August 15/25