AIRWORTHINESS LIMITATIONS SECTION P/N G150-1001-3

• Inspection methods of X-ray, ultrasonic and eddy current may be used in place of penetrant inspection methods NOTE: Inspection methods specified as ultrasonic or eddy current should not be substituted with X-ray as these methods have been determined as the best methods. Table 2: Alternate NDI Inspections - Accessible Locations LOCATION STATED METHOD ALTERNATE METHOD VISUAL PENETRANT HFEC (1) MAGNETIC PARTICLES Accessible Visual — Yes Yes No Penetrant No — Yes No HFEC No No — No Magnetic Particles No No Yes (1) — (1) High Frequency Eddy Current (HFEC). (2) Specific authorization is required. MAINTENANCE MANUAL 05-10-10 Page 4 September 15/25 Table 3: Alternate NDI Inspections - Inaccessible Locations LOCATION STATED METHOD ALTERNATE METHOD X-RAY ULTRASOUND LFEC (1) Inaccessible X-ray — Yes (2) Yes (2) Ultrasound Yes (2) — Yes (2) LFEC Yes (2) Yes (2) — (1) Low Frequency Eddy Current (LFEC). (2) Specific authorization is required. This Airworthiness Limitations Section is based on IAI engineering report 25G032/030367. Table 4 contains a list of structural inspections along with the specific description, initial threshold, repeat interval and Computerized Maintenance Program (CMP) Reference. See Figure 2 for ALS locations. Table 5 contains a requirement to visually inspect for external damage to the skin of unpainted aircraft. Table 6 contains a form for reporting inspection results. Table 7 contains a list of Safe Life Limited Components. Table 8 contains a list of all CMR tasks. Table 9 contains a list of fuel tank system inspections along with the specific description, initial threshold, repeat interval and CMP reference. Table 10 contains temporary limitations and inspection requirements. B. Airworthiness Limitations — Structural Inspections (1) ALS Inspections MAINTENANCE MANUAL 05-10-10 Page 5 September 15/25 Table 4: Airworthiness Limitations ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat ACF1.1 All fasteners along upper splice, skin / upper frames attachments Upper Skin Splice and Frame Attachment FS 282 - FS 343 (7172 - 8715 mm) - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-41-00 534101 ACF1.2 All fasteners along skin / intercostal attachments Upper Skin and Intercostal Attachment FS 282 - FS 343 (7172 - 8715 mm) - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-41-00 534102 ACF1.3 All fasteners along skin / upper longeron attachment Upper Skin and Longeron Attachment FS 282 - FS 343 (7172 - 8715 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-41-00 534103 ACF1.4 All fasteners along skin / aft pressure bulkhead attachment Upper Skin at Aft Pressure Bulkhead Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-41-00 534104 ACF2.1 All fasteners along skin, side splice / side frames attachments Side Skin Splice and Frame Attachment FS 282 - FS 343 (7172 - 8715 mm) - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-41-00 534105 MAINTENANCE MANUAL 05-10-10 Page 6 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat ACF2.2 All fasteners along skin / aft pressure bulkhead attachment Side Skin to Aft Pressure Bulkhead Attachment FS 343 (8715 mm) - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-41-00 534106 ACF2.3 All fasteners along skin / upper longeron attachment Side Skin and Longeron Attachment FS 282 - FS 343 (7172 - 8715 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-41-00 534107 ACF2.4 All fasteners of skin / emergency exit door doubler attachment Side Skin to Emergency Exit Door Doubler FS 282 - FS 320 (7172 - 8132 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-41-00 534108 ACF3.1 All fasteners along upper skin / upper frame attachment Aft Cabin Upper Skin to Frame and Longeron Attachment (Interior) FS 282 - FS 343 (7172 - 8715 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534301 ACF3.2 All fasteners on inner splice / upper frame attachment Upper Inner Splice to Upper Frame Attachment FS 282 - FS 343 (7172 - 8715 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534302 MAINTENANCE MANUAL 05-10-10 Page 7 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat ACF5.1 All fasteners along upper and side skin / upper and side frames attachments (on frames) Aft Cabin Upper and Side Frame to Skin Attachment FS 282 - FS 343 (7172 - 8715 mm) - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-43-00 534303 ACF5.2 All fasteners on inner splice / upper and side frames attachment (frames and splices) - Frame 28 Aft Cabin Inner Splice to Upper and Side Attachment at Frame 28 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534304 ACF5.3 All fasteners on inner splices / upper and side frames attachment (frames and splices) - Frame 29 - Frame 34 Aft Cabin Inner Splice Attachment to Upper and Side Frame 29 - Frame 34 - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-43-00 534305 ACF5.4 All fasteners on lower splice / side frame attachment (frames and splices) - Frame 28 Aft Cabin Lower Splice to Side Frame 28 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534306 MAINTENANCE MANUAL 05-10-10 Page 8 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat ACF5.5 All fasteners on lower splice / side frame attachment (frames and splices) - Frame 29, Frame 31 - Frame 34 Aft Cabin Lower Splice and Side Frame Attachments Frame 29, Frame 31 - Frame 34 - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-43-00 534307 ACF5.6 All fasteners on outer splice / skin attachment - Frame 28 Aft Cabin Outer Splice Skin at Frame 28 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534308 ACF9 Emergency exit door, window frame and door brackets Emergency Exit Window Frame and Door Brackets - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534309 ACF10 All fasteners on side skin / door doubler attachment - Frame 28 - Frame 32 Emergency Exit Side Skin and Door Doubler Attachment Frame 28 - Frame 32 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534310 ACF13 ACF14 Upper / lower sill and door stoppers Emergency Exit Upper and Lower Sill and Door Stoppers - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534311 ACF18 ACF19 ACF20 All fasteners on 3 splices of upper longeron Aft Cabin Longeron Splices at FS 282 (7172 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-43-00 534312 MAINTENANCE MANUAL 05-10-10 Page 9 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat Bulkhead 1.1 All fasteners along angle support / PI / forward web attachments (PI forward leg) Aft Pressure Bulkhead Hat Section Forward Web - NDT Inspection LFEC 10000 flight cycles 5000 flight cycles 53-42-03 534231 Bulkhead 1.2 All fasteners along angle support / PI / forward web attachments (angle support) Aft Pressure Bulkhead Hat Section Angle Support - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-42-03 534232 Bulkhead 1.3 All fasteners along skin / outer strap attachments Aft Pressure Bulkhead Hat Section Skin / Outer Strap Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-42-03 534233 Bulkhead 1.7.1 All integral stiffeners Aft Pressure Bulkhead Lower Base Integral Stiffeners - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-42-03 534234 Bulkhead 1.7.2 All fasteners along forward leg of PI channel / forward web attachment Aft Pressure Bulkhead Lower Base Channel Forward Web - NDT Inspection LFEC 10000 flight cycles 5000 flight cycles 53-42-03 534235 Bulkhead 1.7.3 All clips corner along forward leg of PI and Z channel / forward web attachment Aft Pressure Bulkhead Lower Base Channel Clips - Visual Inspection Visual 10000 flight cycles 5000 flight cycles 53-42-03 534230 MAINTENANCE MANUAL 05-10-10 Page 10 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat Bulkhead 1.8 All fasteners along forward web / omega and Z profiles and PI channel attachments (web side) Aft Pressure Bulkhead Forward Web Omega / Z Profiles and PI Channel Attachments - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-42-03 534236 Bulkhead 1.9 Aft web cutouts radii Aft Pressure Bulkhead Aft Web Cutouts Radii - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-42-03 534237 Bulkhead 1.10.1 All fasteners along forward web / omega and Z profiles attachments (omega and Z profiles) Aft Pressure Bulkhead Forward Web / Omega and Z Profiles Attachments - NDT Inspection LFEC 10000 flight cycles 5000 flight cycles 53-42-03 534238 Bulkhead 1.10.2 All fasteners along aft web / omega and Z profiles attachments (omega and Z profiles) Aft Pressure Bulkhead Aft Web / Omega and Z Profiles Attachment - NDT Inspection LFEC 10000 flight cycles 5000 flight cycles 53-42-03 534239 Bulkhead 1.11 Box casting Aft Pressure Bulkhead Box Casting - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-42-03 534240 MAINTENANCE MANUAL 05-10-10 Page 11 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat CTS1.1 All fasteners along rear spar / skin attachment CTS Lower Skin Rear Spar / Skin Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-00 533101 CTS1.2 All fasteners along front spar / skin attachment CTS Lower Skin Front Spar / Skin Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-00 533102 CTS1.3 All fasteners along lower skin / lower splice attachment CTS Lower Skin / Lower Splice Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-00 533103 CTS1.4 All access panel cutouts, along the perimeter CTS Lower Skin / Access Panel Cutouts Along the Perimeter - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-00 533104 CTS1.5 Around all drain holes CTS Lower Skin / Drain Holes - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-31-00 533105 CTS1.6 All fasteners along lower skin / ribs BL 330.2 attachment CTS Lower Skin / Ribs BL 330.2 Attachment - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-31-00 533106 MAINTENANCE MANUAL 05-10-10 Page 12 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat CTS2.1 All fasteners along front spar / lower skin attachment Front Spar / Lower Skin Attachment - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-32-00 533201 CTS2.2 All fasteners along front spar / upper skin attachment Front Spar / Upper Skin Attachment - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-32-00 533202 CTS2.3 All fasteners along front spar / web LBL 872 and RBL 872 attachment Front Spar / Web BL 872 Attachment - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-32-00 533203 CTS3.1 All fasteners along rear spar / lower skin attachment Rear Spar / Lower Skin Attachment - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-33-00 533301 CTS3.2 All fasteners along rear spar / upper skin attachment Rear Spar / Upper Skin Attachment - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-33-00 533302 CTS3.3 All fasteners along rear spar / web LBL 872 and RBL 872 attachments Rear Spar / Web LBL 872 and RBL 872 Attachments - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-33-00 533303 MAINTENANCE MANUAL 05-10-10 Page 13 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat CTS3.4 Web around access panel cutouts Rear Spar Access Panel Cutouts - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-33-00 533304 CTS4 CTS5 CTS6 All fasteners along lower skin / tee chord, along upper skin / cross chord, along cross chord / Web BL 872 and tee chord / web BL 872 attachments. Lower Skin Tee Chord and Upper Skin Cross Chord Attachments at Rib BL 872 - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-34-00 533401 533402 533403 CTS7.1 All fasteners on main fitting lower part, attachment to front spar Frame 28 Main Fitting Lower Front Spar Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533506 CTS7.2 Inner flange of the main fitting upper part Frame 28 Main Fitting Upper Inner Flange - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533507 CTS8 Frame 29 - lower fitting, inner flange and web Frame 29 Lower Fittings Inner Flange and Web - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-35-00 533501 CTS9 Frame 30 - Lower fitting, inner flange and web Frame 30 Lower Fittings Inner Flange and Web - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-35-00 533502 MAINTENANCE MANUAL 05-10-10 Page 14 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat CTS10 Frame 31 - Lower fitting, inner flange and web Frame 31 Lower Fittings Inner Flange and Web - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-35-00 533503 CTS11 Frame 32 - Lower fitting, inner flange and web Frame 32 Lower Fittings Inner Flange and Web - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-35-00 533504 CTS12 Frame 33 - Lower fitting, inner flange and web Frame 33 Lower Fittings Inner Flange and Web - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-35-00 533505 CTS13 Frame 29 - Upper fitting, fastener on the inner flange Frame 29 Upper Fitting Inner Flange Fasteners - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533510 CTS14 Frame 30 - Upper fitting, fastener on the inner flange Frame 30 Upper Fitting Inner Flange Fasteners - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533511 CTS15 Frame 31 - Upper fitting, fastener on the inner flange Frame 31 Upper Fitting Inner Flange Fasteners - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533512 MAINTENANCE MANUAL 05-10-10 Page 15 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat CTS16 Frame 32 - Upper fitting, fastener on the inner flange Frame 32 Upper Fitting Inner Flange Fasteners - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533513 CTS17 Frame 33 - Upper fitting, fastener on the inner flange Frame 33 Upper Fitting Inner Flange Fasteners - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533514 CTS18.1 All fasteners on main fitting lower part, attachment to rear spar Frame 34 Main Fitting Lower Part to Rear Spar Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533508 CTS18.2 Inner flange of the main fitting upper part Frame 34 Main Fitting Upper Inner Flange - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-35-00 533509 CTS19 All fasteners from the outer side of the cabin Upper Web LBL 872 / RBL 872 - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-36-00 533601 CTS20 All fastener holes along lower skin / rib BL 0.0 and upper skin / rib BL 0.0 attachments Lower Skin / Rib BL 0 and Upper Skin / Rib BL 0 Attachments - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-34-00 533404 MAINTENANCE MANUAL 05-10-10 Page 16 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat CTS21 All fastener holes along lower skin / rib BL 330.2 and upper skin / rib BL 330.2 attachments Lower Skin / Rib BL 330.2 and Upper Skin / Rib BL 330.2 Attachments - Detailed Inspection Visual Borescope 10000 flight cycles 5000 flight cycles 53-34-00 533405 F-AFT 2.1 Area around bolt holes with bushings at forward engine pickup fittings Forward Engine Beam - Engine Pickup Fitting - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-57-00 535721 535722 F-AFT 2.2 Upper channel - Front and rear brackets Forward Engine Beam - Engine Pickup Fitting - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-57-00 535701 535702 F-AFT 3.1 Engine support frame at FS 502 (12765.9 mm) - Top splice Frame 49 FS 502 (12765.9 mm) Upper Part - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-57-00 535703 F-AFT 3.2 All flanges and webs above the forward engine beam Frame 49 FS 502 (12765.9 mm) Upper Part - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-57-00 535723 F-AFT 4 Upper double lug of pickup fitting Aft Engine Beam - Engine Pickup Fitting - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-57-00 535705 535706 MAINTENANCE MANUAL 05-10-10 Page 17 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat F-AFT 5 All flanges, webs and top splice above aft engine beam. Frame 51 FS 532 (13528.6 mm) Upper Part - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-57-00 535707 F-AFT 6 Bolt attachments in forward pickup fitting with vertical stabilizer (lug holes). Lug roots of the forward pickup fitting Frame 54 Vertical Stabilizer Forward Pickup Fitting - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-66-00 536601 F-AFT 7.1 Skin / Frame 56 connecting fasteners on the left (thru 5L stringer) and right (thru 5R stringer) sides Frame 56 Empennage Aft Pickup Fitting - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-66-00 536602 F-AFT 7.2 Outer lugs at Z = 85.000 at HS attachment Frame 56 FS 620 (15770.8 mm) - Lug at Z = 85.000 at Horizontal Stabilizer Attachment - NDT Inspection Ultrasonic 10000 flight cycles 5000 flight cycles 53-66-00 536603 F-AFT 7.3 Vertical Stabilizer pick-up fitting lug hole and root. Vertical Stabilizer Pickup Fitting Lug - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553014 MAINTENANCE MANUAL 05-10-10 Page 18 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat F-AFT 8 Forward engine beam - upper / lower flanges and outer / inner straps. Forward Engine Beam - Upper / Lower Flanges and Outer / Inner Straps - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-57-00 535717 535718 F-AFT 9 Aft engine beam - upper / lower flanges and outer / inner straps. Aft Engine Beam - Upper / Lower Flanges and Outer / Inner Straps - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-57-00 535719 535720 FF1.1 Cockpit lower sill - Outer / inner flanges Cockpit Lower Sill Outer and Inner Flanges - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531702 FF1.3 FF1.4 FF1.5 Lower sill connection to center post, aft post, corner post and forward pressure bulkhead Cockpit Lower Sill Connection to Windshield Center, Corner and Aft Posts - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531710 FF2.1 Cockpit upper sill - Outer / inner flanges Cockpit Upper Sill Outer and Inner Flanges - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531711 MAINTENANCE MANUAL 05-10-10 Page 19 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat FF2.3 FF2.4 FF2.5 Upper sill connection to center, corner and aft posts Cockpit Upper Sill Connection to Windshield Center, Corner and Aft Posts - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531703 FF3.1 FF3.2 FF3.3 Center post to lower sill, upper sill and outer / inner flanges Cockpit Center Post Connections - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531704 FF4.1 FF4.2 FF4.3 Corner post to upper sill, lower sill and outer / inner flanges Cockpit Corner Windshield Posts Connections - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531705 FF5.1 FF5.2 FF5.3 Aft post to upper sill, lower sill and outer / inner flanges Cockpit Aft Post Connections - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531706 FF6.1 FF6.2 FF6.3 FF6.4 Vertical stiffeners without flange (BL ±295, ±496, ±680). Vertical stiffeners with flange (BL ±556). Horizontal stiffeners BL -480 at ring. Circumferential outer flange (aft side). Forward pressure bulkhead - Web cutouts. Cockpit Forward Pressure Bulkhead - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531707 MAINTENANCE MANUAL 05-10-10 Page 20 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat FF7.1 NLG trunnion fitting hole area. Fittings web for cracks at fastener holes. Nose Landing Gear Backup Structure Nose Landing Gear Trunnion Fitting - NDT Inspection NOTE: Ultrasonic bushing area. HFEC uncovered surface. HFEC / Ultrasonic 10000 flight cycles 5000 flight cycles 32-25-01 322507 FF7.2 NLG brace fitting hole area. Fittings web for cracks at fastener holes Nose Landing Gear Backup Structure Nose Landing Gear Brace Fitting - NDT Inspection NOTE: Ultrasonic bushing area. HFEC uncovered surface. HFEC / Ultrasonic 10000 flight cycles 5000 flight cycles 32-25-02 322508 FF7.3 Beam web. Fittings web for cracks at fastener holes Nose Landing Gear Backup Structure Nose Landing Gear Beam - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 32-25-02 322509 FF7.5 End pad around tension bolts Forward Pressure Bulkhead at Lower Longeron End Pad Connection - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531708 MAINTENANCE MANUAL 05-10-10 Page 21 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat FF8.1 Inside cabin: Upper longeron, outer flange, around fasteners. Outside cabin: Skin around fastener holes Forward Cabin Upper Longeron to J-beam Skin and Fastener Connection FS 178 - FS 282 (4518 - 7172 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-20-00 532001 FF8.2 Inside cabin: Left side upper longeron, its splices to forward and aft fittings. Forward fitting FS 3342 - 3549 left side, aft fitting FS 3549 left side. Outside cabin: Skin attachments to upper longeron and fittings Left Upper Longeron J-beam Splices to Forward and Aft Fittings from FS 139 - FS 169 (3549 - 4638 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-20-00 532002 FF8.3 Inside cabin: Upper longeron right side, splices at FS 3549 right side. Outside cabin: Skin attachments to upper longeron and fittings Right Upper Longeron J-beam Splices at FS 139 (3549 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-20-00 532003 FF9.1 FF9.2 Upper longeron attachment to splice angles, area around fastener holes and longeron edge. Upper Longeron J-beam Forward Splice Attachment FS 183 (4638 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-20-00 532004 MAINTENANCE MANUAL 05-10-10 Page 22 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat FF10.1 Outside cabin: Window frame inner flange, 15 - 20 degrees below middle of cutout circle. Skin at cutout radius and attachment to frame Cabin Window Frame and Skin Cutout - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-27-00 532701 FF11.1 Fuselage side skin cutout edges (left and right). Side Skin Cutouts, FS 178 - FS 282 (4518 - 7172 mm) - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-21-00 532115 FF12.1 Upper and lower corners of skin cutout and surrounding framing elements - Cracks at fastener holes and cutout edge Main Entrance Door Skin Cutout and Structure - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 52-11-00 521107 FF12.2.1 FF12.2.2 Main entrance door lower stops. Main Entrance Door Lower Door Stops - NDT Inspection Penetrant 10000 flight cycles 2500 flight cycles 52-11-00 521108 FF12.2.3 Backup fitting attachment to outer skin Main Entrance Door Backup Fitting Attachment - Detailed Inspection Visual 10000 flight cycles 2500 flight cycles 52-11-00 521112 FF12.2.4 Cabin door skin around edge of door handle cutout Main Entrance Door Handle Cutout - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 52-11-00 521113 MAINTENANCE MANUAL 05-10-10 Page 23 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat FF12.2.5 Inner flange of Z-beam lateral assembly Main Entrance Door Assembly Z-beam Inner Flange - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 52-11-00 521109 FF13.1 FF13.2 FF13.3 FF13.4 Frame inner flange at min radius (left / right). Upper segment inner flange and area around open holes. Door frame web cutouts (left / right) Main Entrance Doorframe Structure FS 139 (3549 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 52-11-01 521110 FF14.1 FF14.2 FF14.3 FF14.4 Frame inner flange at min radius (left / right). Frame inner flange with holes for seat track (right). Upper segment inner flange, area around open holes. Door frame web cutouts (left / right) Main Entrance Doorframe Structure FS 168 (4285 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 52-11-01 521111 FF15 Nose outer skin at access panels cutout corners and fastener holes along the rows of attachment to forward pressure bulkhead, nose landing gear beam, (left / right), forward side longerons Nose Landing Gear Bay - Lower Skin Cutouts - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-00-00 530015 FF16.1.1 FF16.1.2 Cockpit center lower frames FS 81 - FS 131 (2073 - 3342 mm) cutout radius and outer flange fillet radius. Cockpit Center Lower Frames FS 81 - FS 131 (2073 - 3342 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-12-00 531701 MAINTENANCE MANUAL 05-10-10 Page 24 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat FF16.2.1 FF16.2.2 FF16.2.3 FF16.2.4 Center lower frames STA 4757 - 6872 cutout radius, outer flange fillet radius, intermediate flange at nutplate attachments and attachments to side frame, longeron and all intermediate splice elements for cracks around the fasteners holes. Cabin Center Lower Frames FS 187 - FS 270 (4757 - 6872 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-22-00 532201 FF17.1 FF17.2 Side frames FS 81 - FS 131 (2073 - 3342 mm) inner flange and web, splice between side frame and lower longeron and lower frame. Cockpit Side Frames FS 81 - FS 131 (2073 - 3342 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-12-00 531712 FF17.3.1 FF17.3.2 FF17.3.3 Canopy frames attachments to center post, upper sill and open holes Cockpit Canopy Frames - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-17-00 531709 FF18.1 Cabin frame web open holes between FS 187 - FS 270 (4757 - 6872 mm). Cabin Frame Web FS 187 - FS 270 (4757 - 6872 mm) - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-22-00 532202 FF18.2 Cabin inner frame splice at upper longeron (left / right) between FS 187 - FS 270 (4757 - 6872 mm). Cabin Frame Splice at Upper Longeron FS 224 (5695 mm) - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-22-00 532203 MAINTENANCE MANUAL 05-10-10 Page 25 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat Fuel_T 1.1 Lugs and integral ribs. Fitting web for cracks at fastener holes Main Landing Gear Brace Fitting - NDT Inspection NOTE: Ultrasonic bushing area. HFEC uncovered surface. HFEC / Ultrasonic 10000 flight cycles 5000 flight cycles 53-50-00 532005 Fuel_T 1.2 All lugs on center Frame 35 Main Landing Gear Bay Frame 35 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-50-00 532006 Fuel_T 2.1 Drain hole and drain fitting attachment Fuel Tank Area Drain Hole and Drain Fitting Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 53-51-00 535101 Fuel_T 2.2 All fasteners along upper longeron attachments Fuel Tank Area Upper Longeron Attachments - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 53-51-00 535102 Fuel_T 2.3 Frame 36 flange to web outer radius Fuel T2.3 Fuel Tank Area Frame 36 to Web Outer Radius - Detailed Inspection NOTE: Visual with borescope on the inside. Visual Borescope 10000 flight cycles 5000 flight cycles 53-51-00 535103 T1 Overall vertical stabilizer skin and fasteners attachments Vertical Stabilizer Skin - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 55-30-00 553011 MAINTENANCE MANUAL 05-10-10 Page 26 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat T2 Lugs of the vertical stabilizer aft attachment fitting, lug hole and root Vertical Stabilizer Aft Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553012 T3 Lugs of the vertical stabilizer forward attachment fitting, lug hole, lug root and fastener hole Vertical Stabilizer Forward Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553013 T4 Upper skin area around the fastener holes at front spar attachment spanwise from Rib 14 - Rib 23 Horizontal Stabilizer Front Spar and Upper Skin Attachments at Rib 14 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-10-00 551011 Upper skin area around the fastener holes along front spar attachment from Rib 23 to tip Horizontal Stabilizer Front Spar and Upper Skin from Rib 23 to Tip - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 55-10-00 551017 T5.1 Horizontal stabilizer aft spar splice fitting outer lugs around lug hole and corner radii. Horizontal Stabilizer Aft Splice Fitting - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-15-00 551501 MAINTENANCE MANUAL 05-10-10 Page 27 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat T6.1 Horizontal stabilizers rear spar and upper skin aft attachment between ribs 14- 23 and area around fastener holes. Horizontal Stabilizer Rear Spar and Upper Skin Aft Attachment Between Ribs 14 - 23 - Visual / NDT Inspection HFEC / Visual 10000 flight cycles 5000 flight cycles 55-10-00 551013 T6.1a Horizontal stabilizers rear spar and upper skin aft attachment between Ribs 23 to tip rib and area around fastener holes. Horizontal Stabilizer Rear Spar and Upper Skin Aft Attachment from Rib 23 to Tip - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 55-10-00 551015 T6.2 Horizontal stabilizers splice fitting area, between Ribs 14-23, at rear spar upper flange , through the upper skin around fastener holes, rear spar upper flange at trailing edge area and at rear spar web splice fitting. Horizontal Stab Rear Spar Upper Flange (Splice Fitting Area) and Web, Ribs 14 - 23 - NDT Inspection HFEC 10000 flight cycles 1600 flight cycles 55-10-00 551016 T7.1 Horizontal stabilizers trim actuator fitting lugs. Horizontal Stabilizer Trim Actuator Fitting - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 55-15-00 551502 MAINTENANCE MANUAL 05-10-10 Page 28 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat T7.2 Horizontal stabilizer scissors attachment lugs and lug roots. Horizontal Stabilizer Trim Actuator Fitting Scissors Attachment Lugs and Lug Roots - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-15-00 551503 T8 Horizontal stabilizer scissors outer fittings. Horizontal Stabilizer Scissors - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-10-02 551014 T9 Elevator supporting fittings connection lugs. Elevator Supporting Fittings - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-23-00 552301 T10 Elevator fittings lugs. Elevator Fittings - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-23-00 552002 T11 All over connecting lugs Elevator Trim Tab Fittings - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 55-23-00 552003 T12 Rudder fittings attachments to vertical stabilizer aft spar flanges around fastener holes. Vertical Stabilizer Aft Spar Flanges - NDT Inspection NOTE: Aircraft 201 thru Aircraft 289. HFEC 8000 flight cycles 4000 flight cycles 55-30-00 553021 MAINTENANCE MANUAL 05-10-10 Page 29 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat T12 Rudder fittings attachments to vertical stabilizer aft spar flanges around fastener holes. Vertical Stabilizer Aft Spar Flanges - NDT Inspection NOTE: Aircraft 290 thru Aircraft 999. HFEC 10000 flight cycles 5000 flight cycles 55-30-00 553021 W1.1.1 Center spar to lower skin attachment fastener holes between Ribs 0 - 3. Wing Lower Skin Center Spar / Skin Attachment - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 57-15-00 571501 571502 W1.1.2 Front spar to lower skin attachment fastener holes between Ribs 0 - 4. Wing Lower Skin Front Spar / Skin Attachment - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 57-15-00 571503 571504 W1.1.3 Rib 0 to lower skin attachment fastener holes. Wing Lower Skin to Rib 0 Attachment - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 57-15-00 571505 571506 W1.1.4 Lower skin around drain valve hole and around valve attachment holes. Wing Lower Skin Drain Valve and Valve Attachment Holes - Detailed Inspection NOTE: Visual with borescope on the inside. Visual Borescope 10000 flight cycles 5000 flight cycles 57-15-00 571507 571508 MAINTENANCE MANUAL 05-10-10 Page 30 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat W1.1.5 Lower skin longitudinal splices fastener holes between Ribs 0 - 2. Wing Lower Skin Longitudinal Skin Splices - NDT Inspection NOTE: HFEC outside skin. LFEC inside skin. HFEC / LFEC 10000 flight cycles 5000 flight cycles 57-15-00 571509 571510 W1.1.6 Lower skin longitudinal splices fastener holes at Rib 2. Wing Lower Skin Splice at Rib 2 - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 57-15-00 571511 571512 W1.1.7 W1.1.9 W4.2.2 Lower skin / front spar attachment (fastener holes) between Ribs 5 - 23. Wing Lower Skin Front Spar / Skin Attachment - NDT Inspection NOTE: For Aircraft 201 thru Aircraft 300, 2500 flight cycles. For Aircraft 301 thru Aircraft 999, 5000 flight cycles. HFEC 10000 flight cycles Note 57-15-00 571513 571514 W1.1.8 W1.1.10 Lower skin / rear spar attachment (fastener holes) between Ribs 1 - 23. Wing Lower Skin Rear / Skin Attachment - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-15-00 571515 571516 W1.2 Lower skin access panel cutouts between Ribs 6 - 16. Wing Lower Skin Access Panel Cutouts - NDT Inspection HFEC 5000 flight cycles 5000 flight cycles 57-15-00 571517 571518 MAINTENANCE MANUAL 05-10-10 Page 31 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat W1.3 Access Panel Cutout between Ribs 2-3 and center to rear spars W1.3 Wing Lower Skin Access Panel Cutouts Between Rib 2 and Rib 3 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-15-00 571521 571522 W1.3.1 Rib 4 radius at the rear spar area W1.3.1 Wing Lower Skin at Rib 4 - Detailed Inspection NOTE: Visual with borescope on the inside. Visual Borescope 10000 flight cycles 5000 flight cycles 57-15-00 571523 571524 W2.1 W2.2 W9 All fasteners in inboard rear spar lower flange between Ribs 1 - 14. All fasteners in the rear spar splice fitting lower flange (16 fasteners) Rear Spar and Splice Lower Flange Between Ribs 1 - 14 - NDT Inspection HFEC / LFEC 10000 flight cycles 5000 flight cycles 57-12-00 571201 571202 W2.1.2 Wing rear spar trunnion attachment, pin hole area, web and integral ribs at MLG backup structure (MLG wheel well). Wing Rear Spar Main Landing Gear Trunnion Attachment - NDT Inspection NOTE: Ultrasonic bushing area. HFEC uncovered surface. HFEC / Ultrasonic 10000 flight cycles 5000 flight cycles 57-12-00 571205 571206 W3.1 All fasteners on wing center spar / splice lower flange between Rib 0 and Rib 3. Center Spar and Splice Lower Flange - NDT Inspection LFEC 10000 flight cycles 5000 flight cycles 57-13-00 571301 571302 MAINTENANCE MANUAL 05-10-10 Page 32 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat W3.1.2 Wing center spar trunnion attachment, pin hole area, web and integral ribs at MLG backup structure (MLG wheel well). Wing Center Spar Main Landing Gear Trunnion Attachment - NDT Inspection NOTE: Ultrasonic bushing area. HFEC uncovered surface. HFEC / Ultrasonic 10000 flight cycles 5000 flight cycles 57-13-00 571305 571306 W4.1 W4.2 All fasteners in inboard front spar lower flange between Ribs 0 - 13 Front Spar and Splices - NDT Inspection LFEC 10000 flight cycles 5000 flight cycles 57-11-00 571101 571102 W4.2.1 All cutouts in spar web between Ribs 6 - 22 Wing Front Spar Web Cutouts Between Rib 6 - Rib 22 - NDT Inspection NOTE: For Aircraft 201 thru Aircraft 288, 2500 flight cycles. For Aircraft 289 thru Aircraft 999, 5000 flight cycles. HFEC 10000 flight cycles Note 57-11-00 571107 571108 W6.1 All fasteners in the splice fitting lower flange between Ribs 0 - 1 (10 fasteners). Front Spar and Splice Lower Flange at Spar / CTS - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-11-00 571103 571104 W7 All fasteners in the splice fitting lower flange at Rib 6 (17 fasteners). Front Spar and Splice Flange - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-11-00 571105 571106 MAINTENANCE MANUAL 05-10-10 Page 33 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat W8.1 Wing center spar splice fitting lower flange fasteners at Rib 6 (14 fasteners). Center Spar and Splice Fitting Lower Flange - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 57-13-00 571303 571304 W10 Wing lower skin splice at Rib 2 lower flange fasteners. Wing Lower Skin Splice at Rib 2 - NDT Inspection LFEC 10000 flight cycles 5000 flight cycles 57-15-00 571519 571520 W11.1 Flap rails caps, webs and intersections. Flaps Rail Caps, Webs and Intersections - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 27-50-00 275009 275010 W11.2 Fastener holes at actuator access panel and at the Ribs 10 - 11 flanges connection to intermediate panel Flaps Fastener Holes at Actuator Access Panel - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 27-50-00 275011 275012 W11.3 Fasteners around edge of access panel and at panel free edges between Ribs 10 - 11 Flaps Fasteners Around Edge of Access Panel at Ribs 10 - 11 - NDT Inspection HFEC 10000 flight cycles 5000 flight cycles 27-50-00 275013 275014 W12.1 Rear spar flange, Rib 23 flange and internal splice plate Winglet Attachment - NDT Inspection X-ray 10000 flight cycles 5000 flight cycles 57-32-00 573201 573202 MAINTENANCE MANUAL 05-10-10 Page 34 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat W12.2 Lower skin at winglet attachment. Winglet Attachment Lower Skin - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 57-32-00 573203 573204 W13.1 All slat spar / skin and de-icing cutout fasteners. Slat Spar / Skin and De-Icing Cutout Fasteners - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 27-80-00 278007 278008 W13.2 Slat rails, caps, webs and the intersection between them Slats and Slat Rails - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 27-80-00 278009 278010 W15.1 Aileron main fitting, actuator lugs, hinge holes, actuator and hinge pins, fitting flanges attachment to composite structure aileron Aileron Main Fitting - Detailed Inspection Visual 10000 flight cycles 5000 flight cycles 27-10-00 271007 271008 W15.2 Aileron external structure. Aileron External Structure - Detailed / NDT Inspection NOTE: Areas that can not be effectively inspected by US method will be inspected by tapping. Ultrasonic / Visual / Tap Test 10000 flight cycles 5000 flight cycles 27-10-00 271009 271010 MAINTENANCE MANUAL 05-10-10 Page 35 September 15/25 ALS Number Description Aircraft Maintenance Manual Procedure NDI Type Inpection Interval ATA Ref CMP RefInitial Repeat W15.3 Actuator bracket, lug roots and holes Aileron Actuator Bracket - Visual / NDT Inspection NOTE: Visual for holes. HFEC for roots. HFEC / Visual 10000 flight cycles 5000 flight cycles 27-10-00 271011 271012 MAINTENANCE MANUAL 05-10-10 Page 36 September 15/25 (2) Unpainted Aircraft Table 5: 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 (3) ALS 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 airworthiness limitations inspection is accomplished. NOTE: Inspection results, both positive and negative, are to be reported to Gulfstream Maintainability Engineering, 912-965-3153, FAX 912-965-4704. Discrepancies are to be reported within 24 hours of their findings. Complete Table 6 with inspection results. Provide a digital photograph of the discrepancy. Table 6: ALS Inspection Results ALS NUMBER AIRCRAFT SERIAL NUMBER AIRCRAFT TAIL NUMBER Part Number(s) [if applicable] Aircraft Hours Aircraft Landings Date of Inspection Discrepancies Found No Yes If yes, complete the following information: Location FS BL WL Size Orientation MAINTENANCE MANUAL 05-10-10 Page 37 September 15/25 C. Safe Life Limited Components The Safe Life Limits addresses those items that have been defined as being life limited. See Table 7. Table 7: Life Limited Components Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref 2505-0300-000 Main Landing Gear Strut Assembly (Left) 1 20,000 flight cycles N/A 321223 2506-0300-000 Main Landing Gear Strut Assembly (Right) 1 20,000 flight cycles N/A 321224 2505-0100-00 Main Landing Gear Shock Absorber 2 20,000 flight cycles N/A 321203 321204 3537-0000-000 Main Landing Gear Brace Actuator (Left) 1 20,000 flight cycles N/A 321403 3538-0000-000 Main Landing Gear Brace Actuator (Right) 1 20,000 flight cycles N/A 321404 2505-0200-000 Trailing Link Assembly (Left / Right) 2 20,000 flight cycles N/A 321307 321308 2289-0500-000 Nose Landing Gear Shock Absorber Outer Body Assembly 1 20,000 flight cycles N/A 322005 2289-0100-00 Nose Landing Gear Shock Absorber Sliding Tube Assembly 1 20,000 flight cycles N/A 322006 2291-0000-000 Nose Landing Gear Brace Assembly 1 20,000 flight cycles N/A 322512 3468-0000-000 Nose Landing Gear Actuator 1 20,000 flight cycles N/A 322403 3462-0000-000 Steering Actuator 2 20,000 flight cycles N/A 325212 325213 2292-0000-000 Nose Wheel Steering Assembly 1 20,000 flight cycles N/A 325211 2289-0400-000 Nose Landing Gear Inner Cylinder 1 20,000 flight cycles N/A 322007 MAINTENANCE MANUAL 05-10-10 Page 38 September 15/25 Table 7: Life Limited Components Airworthiness Limitations Instructions Part Number Nomenclature Qty Discard ATA Ref CMP Ref 2247-0500-008 Nose Landing Gear Actuator to Nose Landing Gear Strut Attachment Pin NOTE: Aircraft beyond 5000 flight cycles, accomplish pin replacement or NDT inspection per SB 150-32- 200 within 200 flight cycles following date of Revision 29. 1 5200 flight cycles N/A 322009 D. Certification Maintenance Requirements (CMR) (1) Introduction The following presents a list of all Gulfstream 150 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: (a) One star CMRs (*) - The task and interval specified are mandatory and cannot be changed, escalated or deleted without the concurrence of the Civil Aviation Authority of Israel (CAAI). (b) Two star CMRs (**) - The task intervals may be adjusted in accordance with an 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 8. 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 Flight hours and flight cycles are tracked from first flight. C Checks and calendar items (monthly checks) are clocked from Entry Into Service (EIS) after completion of initial outfitting installation, unless EIS exceeds 12 months from Certificate of Airworthiness. If EIS exceeds 12 months from Certificate of Airworthiness, then C Checks and calendar items (monthly checks) are clocked from the aircraft Certificate of Airworthiness date plus 12 months. MAINTENANCE MANUAL 05-10-10 Page 39 September 15/25 Table 8: Certification Maintenance Requirements (CMR) ATA Ref Description Type CMP Ref Initial / Repeat 21-22-01 Ram Air Check Valve - Functional Check ** 212201 6A 21-31-00 Cabin Altitude High Warning - Functional Check ** 213105 2A 21-31-01 Cabin Pressure Controller Aneroid Switch - Functional Check MRB Ref: 21-30-00-03, Functional Check of aneroid switch NOTE: Task is applicable for Aircraft 201 thru Aircraft 295 Pre-SB 150-21-129 only. Perform at 1A following date of Revision 14, not to exceed 12 months from date of last accomplishment. ** 213112 1A 21-31-04 Safety Valve - Functional Check MRB Ref: 21-30-00-02, Functional Check of the safety valve NOTE: Interval is 1A for Aircraft 201 thru Aircraft 295 Pre-SB 150-21-129. Interval is 5A for Aircraft 296 and subsequent, and Aircraft 201 thru Aircraft 295 Post SB 150-21-129. Perform next due Functional Check from time of last accomplishment. * 213142 Note 24-30-00 Load Shedding - Operational Check ** 243010 2A 27-11-01 Aileron Input Lever Switch Circuit - Functional Check ** 271107 6A 27-11-01 Aileron Servo Actuator Pistons Differential Switch Circuit - Functional Check ** 271108 6A 27-11-23 Aileron Servo Actuator Compensator Volume and Damping - Functional Check * 271127 6A 28-21-00 Refuel Switch 77Q - Functional Check ** 282101 6A 52-70-00 Airstair Door Switch - Functional Test ** 521006 6A E. Fuel Tank System Airworthiness Limitations (1) Introduction The maintenance inspections presented below are necessary to maintain the design features required to preclude the existence or development of ignition sources within the fuel tank system throughout the operational life of the airplane. These inspections are the result of safety analysis performed to substantiate compliance with CFR / JAR 25.981 as presented in IAI Engineering Report 25G041/031584. (2) Maintenance Tasks MAINTENANCE MANUAL 05-10-10 Page 40 September 15/25