N404LC

Part: FRAME — CRACKED (BS 814) · airframe 66,987 hrs · 39,219 cycles

DURING SCHEDULED B-3 CHECK, FOUND LT FUSELAGE FRAME AT FS 814 HAD CRACKED AT THE LONGERON CUTOUT LBL 62, WL256. REPAIRED IAW SMP583, SRM FIG 51-140-21.

Part: FITTING — CRACKED (BS 924) · airframe 66,987 hrs · 39,219 cycles

DURING SCHEDULED B-3 CHECK, FOUND FITTING HAD A CRACKED RADIUS; FS 924 61 WL 207. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM 51-70.

Part: BULKHEAD WEB — CRACKED (BS 924) · airframe 66,987 hrs · 39,219 cycles

DURING SCHEDULED B-3 CHECK, FOUND BULKHEAD WEB CRACKED, FS924 LBL62 WL270. REPAIRED IAW SMP583, SRM FIG 51-140-17.

Part: ATTACH ANGLE — CRACKED (BS 517) · airframe 66,987 hrs · 39,219 cycles

DURING SCHEDULED B-3 CHECK, FOUND NR 2 DRY BAY FWD INBD VERTICAL ATTACH ANGLE TOP END HAD APPROX 3" LONG VERTICAL CRACK, FS 517, WL270. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-70.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,734 hrs · 39,056 cycles

DURING SCHEDULED SSID INSPECTION FOR AD 2012-06-09 (SP189), A CRACK WAS FOUND ON NR 3L LONGERON. R & R LONGEORN ASSY.

Part: TEE FITTING — CRACKED (BS 477) · airframe 66,725 hrs · 39,054 cycles

DURING CRUISE FLIGHT VISUALLY OBSERVED CRACK AT FS 480. INSPECTION AFTER FLIGHT FOUND TEE FITTING CRACKED, FS 477, RBL 16.5 TO LBL 16.5, WL 285.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 66,291 hrs · 38,935 cycles

DURING SCHEDULED B-2 CHECK, FOUND FWD TOP EMERGENCY EXIT DOOR ASSY'S INNER FLANGE HAD 2 INCH LONG CRACK. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-19 WITH 2024-T3.

Part: BULKHEAD — CRACKED (BS 968) · airframe 66,291 hrs · 38,935 cycles

DURING SCHEDULED B-2 CHECK, FOUND AFT FUSELGAE INTERIOR FS 968, UPPER BULKHEAD CRACKED AT RBL 18, WL 285 VERTICAL FIN ATTACHMENT. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-06.

Part: FORMER — CRACKED (BS 834) · airframe 66,291 hrs · 38,935 cycles

DURING SCHEDULED B-2, , LT AFT FUSELAGE INTERIOR FORMER AT FS 834, LBL 66, WL 180 FOUND CRACKED. REPAIRED IAW SMP583 FIG 53-50-10.

Part: RING ASSEMBLY — CRACKED (BS 957) · airframe 66,291 hrs · 38,935 cycles

DURING SCHEDULED B-2 CHECK, FOUND RT AFT FUSELAGE INTERIOR FS 957 RING SEGMENT HAD 2.5" LONG CRACK AT WL 260, RBL 66. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-07.

Part: CONTROL UNIT — FAULTY (FIRE DETECTION) · airframe 65,596 hrs · 38,749 cycles

DURING CRUISE FLIGHT NR 1 ENGINE FIRE LIGHT ILLUMINATED, SHUTDOWN NR 1 ENGINE. INSPECTED ENGINE FOR EVIDENCE OF FIRE OR BLEED AIR LEAKAGE, REPLACED NR 1 FIRE CONTROL UNIT IAW SMP581 26-10, LP 34123.

Part: BULKHEAD — CRACKED (BS 902) · airframe 65,596 hrs · 38,749 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND LT AFT BULKHEAD CAP CRACK AT FS902, LBL63. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583, CH 51-6 AND 51-70.

Part: STRUCTURE — GOUGED (BS 859) · airframe 65,596 hrs · 38,749 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND LT SLOPING LONGERON GOUGED AT FS 859, LBL 61.62. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-12-088.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 65,596 hrs · 38,749 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND RT HORIZONTAL STABILZER UPPER SKIN CRACKED BETWEEN RIVETS FS 1041, HSS61, WL285. REPAIR ACCOMPLISHED IAW MEA 382-55-12-089.

Part: BULKHEAD WEB — CRACKED (BS 165) · airframe 65,596 hrs · 38,749 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND NLG WHEEL WELL BULKHEAD WEB CRACKED AT FS165, RBL70, WL171. REPAIR ACCOMPLISHED IAW SMP 583, FIG 51-140-17, NR 2-5-2.

Part: WEB — CRACKED (BS 880) · airframe 65,596 hrs · 38,749 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND RT AFT BULKHEAD WEB CRACKED AT FS 880, RBL 63. REPAIR ACCOMPLISHED BY REPLACEMENT IAW SMP583, 51-60 AND 51-70.

Part: JACKSCREW — SEIZED (TE FLAPS) · airframe 65,589 hrs · 38,747 cycles

FLAPS STUCK AT 15 PERCENT LANDING WAS UNEVENTFUL. R & R NR 7 JACKSCREW IAW SMP 581 27-50-11.

Part: BULKHEAD WEB — CRACKED (BS 188) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND NOSE WHEEL WELL LT BULKHEAD WEB CRACKED AT FS188, LBL30, WL154. REPAIRED IAW SMP583, FIG 51-140-17.

Part: STRUCTURE — CRACKED (BS 858 BULKHEAD) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND AFT FUSELAGE INTERIOR BULKHEAD INNER CAP CRACKED AT FS 858, WL 200, LBL 68. REPAIRED IAW SMP583 FIG 53-50-14.

Part: SKIN — DENTED (BS 777E) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND STONE MARKS AND WRINKLES BEYOND LIMITS ON FUSELAGE SKIN AT FS 777E, WL 140-158, LBL 60 TO RBL 60. REPAIRED BY REPLACEMENT IAW SMP583 51-60 & 51-70.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND CARGO DOOR FLOOR STIFFENER CRACKED AT FS 1012, LBL 26, WL 270. REPAIRED BY REPLACEMENT IAW SMP583, 51-60 & 51-70.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, UNDER JOB CARD HC5511 FOUND HORIZONTAL STABILIZER RT L/E LOWER RIB CRACKED AT HSS 197.5 AND 203.5. REPAIRED IAW SMP583 FIG 51-140-20.

Part: BULKHEAD — CORRODED (RT MLG WW) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD CORRODED AT FS 573 TO FS 577, WL 175, RBL 61.5. REPAIRED BY REPLACEMENT IAW SMP583 CHAPTER51-60 & 51-70.

Part: BEAM — CRACKED (BS 517) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND LT BEAM ASSY OTBD CAP CRACKED AT FS 517, LBL 64, WL 256. REPAIRED IAW LAC MEA 382-53-12-033.

Part: WEB — WARPED (CARGO DOOR) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND CARGO DOOR BULKHEAD WEB WARPED AT RS9, LBL15 TO LBL30. REPAIRED IAW SMP583 FIG 51-140-17.

Part: BEAM — CORRODED (WHEEL WELL) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, UNDER JOB CARD HC5324, FOUND MLG WHEEL WELL BEAM CORROSION UNDER REIMFORCEMENT PLATE AT FS577, WL160-163, RBL61. REPAIRED IAW LAC MEA 382-53-12-017.

Part: WINDOW FRAME — CRACKED (BS 156) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND RT SIDE WINDOW AFT FRAME LOWER CORNER CRACKED AT FS 156, WL 225, RBL 62. REPAIRED IAW SMP583, FIG 53-30-32.

Part: FLOOR SUPPORT — CRACKED (BS 477) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND CARGO BAY UNDERFLOOR SUPPORT CRACKED FS 477, WL 130, RBL 10. REPAIRED IAW SMP583, FIG 51-140-19.

Part: ATTACH ANGLE — CRACKED (BS 476) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND FUSELAGE TO WING FORWARD FAIRING ATTACH ANGLE CRACKED AT FS 476, LBL 59, WL 285. REPAIRED BY REPLACEMENT IAW SMP583 51-70.

Part: FLOORBEAM — CRACKED (BS 577) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND CABIN FLOORBEAM LOWER CAP CRACKED AT FS 577, WL 140, RBL 60. REPAIRED IAW SMP583 FIG 53-40-29.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND HORIZONTAL STAB LT L/E UPPER RIB CRACKED (COMPENSATOR MOUNTING POINT) AT HSS 156 & HSS 162. REPAIRED IAW SMP583, FIG 55-20-08.

Part: STRUCTURE — CRACKED (NR 4 NACELLE) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND NR 4 POSITION QEC SN LMG-1869-14 FWD BULKHEAD RT OUTER CAP TEE CRACKED AT FS 410.70. REPAIRED IAW MEA 382-54-07-081.

Part: BEAM — CORRODED (RT MLG WW) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND RT MAIN WHEEL WELL BOW BEAM OUTBD CAP CORROSION AT FS557, WL150, RBL64 / REPAIRED BY REPLACEMENT IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: POST — CRACKED (BS 134) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND LT WINDOW POST CRACKED AT FS 134, WL 251, LBL 62. REPAIRED IAW LAC MEA 382-53-12-015.

Part: BULKHEAD WEB — CRACKED (RT MLG WW) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT FS517, WL165, RBL61. REPAIRED BY REPLACEMENT IAW SMP583 CHAPTER 51-60 & 51-70, NR 2203.

Part: LONGERON — CORRODED (BS 473) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND NR 3 QEC RT LOWER LONGERON CORROSION AT INNER LOWER FLANGE AT FS 473. REPAIRED BY REPLACEMENT IAW SMP583 51-70 & 54-20, PAGES 2 THROUGH 4.

Part: DUCT — DAMAGED (NR 4 NACELLE) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND NR 4 QEC, SN LMG-1869-14 OIL COOLER DUCT FWD CHIN SCOOP ASSY WITH ELONGATED FASTENER HOLES AND CRACKS. REPAIRED IAW LAC MEA 382-54-12-018.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 64,899 hrs · 38,319 cycles

DURING SCHEDULED C-10 CHECK, FOUND HORIZONTAL STAB LT L/E UPPER RIBS CRACKED AT HSS138.5, 149.5 & 150.5 AND LOWER RIBS AT HSS93, 99,N 111, 144, 168.6, & 278. REPAIRED IAW SMP 583, FIG 51-140-20.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 64,208 hrs · 37,692 cycles

DURING SCHEDULED B-3, CHECK IAW JOB CARD HB2703 FOUND LT INBD FLAP UPPER SKIN CRACKED AT CWS120 BUMPER PAD AREA. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-12.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 64,208 hrs · 37,692 cycles

DURING SCHEDULED B-3 CHECK IAW JOB CARD HB5301, FOUND RAMP DOOR EXTERNAL SKIN CRACK AT RS1 TO RS1.6, BL0. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-12.

Part: WEB — CRACKED (BS 497) · airframe 64,208 hrs · 37,692 cycles

DURING SCHEDULED B-3 CHECK IAW JOB CARD HB3200, FOUND LT MAIN WHEEL WELL BOW BEAM INBD WEB CRACKED AT FS497, LBL63, WL158. REPAIR ACCOMPLISHED IAW SMP583, FIG 53-40-12.

Part: STRUCTURE — CRACKED (BULKHEAD) · airframe 64,208 hrs · 37,692 cycles

DURING SCHEDULED B-3 CHECK IAW FOUND AFT FUSELAGE RT BULKHEAD INNER CAP REPAIR MEMBER CRACKED AT FS814, RBL70, WL175. REPAIR ACCOMPLISHED BY REPLACING DOUBLER IAW SMP583, FIG 53-40-14.

Part: SKIN — CRACKED (BS 196-204) · airframe 64,002 hrs · 37,548 cycles

DURING REGULAR A-CHECK, FOUND FUSELAGE SKIN CRACK AT FS 196 TO 204, WL 126, LBL 27. MX FERRY TO FOR REPAIR. LOG PAGE NR 37654 M1.

Part: WEB — CRACKED (FUSELAGE) · airframe 63,498 hrs · 37,367 cycles

DURING SCHEDULED B-2 CHECK PER JOBCARD HB5302 FOUND CRACKED WEB AT FS 880, RBL 62, WL 250. REPAIRED IAW LOCKHEED SRM SMP583 CH 51-60 AND FIG 51-140-17.

Part: FLOOR PANEL — CRACKED (CARGO DOOR) · airframe 63,498 hrs · 37,367 cycles

DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND AFT CARGO DOOR FLOOR PANEL CRACKED AT FS 880 RBL 58. REPAIRED IAW LOCKHEED SRM SMP583 FIG 51-140-17.

Part: WEB — DENTED (CARGO DOOR) · airframe 63,498 hrs · 37,367 cycles

DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND AFT CARGO DOOR WEB DENTED AT FS 902, BL 0. REPAIRED IAW LOCKHEED SRM SMP583CH 51-140, FIG 51-140-17.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,498 hrs · 37,367 cycles

DURING SCHEDULED B-2 CHECK PER JOB CARD HB5305 FOUND CRACK ON HORIZONTAL FLANGE OF LONGERON AT FS 248E, LBL 66, WL 195. REPAIRED BY REPLACING LONGERON IAW LOCKHEED SRM SMP583 CH 51-60, 51-70, FIG 51-140-21.

Part: MOUNT — SCORED (NR 2 TRUSS) · airframe 63,498 hrs · 37,367 cycles

DURING SCHEDULED B-2 CHECK PER JOBCARD HB7251 FOUND NR 2 ENGINE UPPER INBOARD AND OUTBOARD AND LOWER OUTBOARD TRUSS MOUNT BORES WITH SCORING DAMAGE AT CWS178L & 213L. REPAIRED IAW LAC MEA 382-54-11-003 R0.

Part: MOUNT — SCORED (NR 1 TRUSS) · airframe 63,498 hrs · 37,367 cycles

DURING SCHEDULED B-2 CHECK PER JOB CARD HB7251 FOUND NR 1 ENGINE UPPER INBOARD AND OUTBOARD TRUSS MOUNT BORES WITH SCORING DAMAGE AT OWS 162L & 197L. REPAIRED IAW LAC MEA 382-54-11-003 R0.

Part: WEB — DENTED (CARGO DOOR) · airframe 63,498 hrs · 37,367 cycles

DURING SCHEDULED B-2 CHECK PER JOB CARD HB5302 FOUND AFT CARGO DOOR WEB DENTED FS 880, BL 0. REPAIRED IAW LOCKHEED SRM SMP583 FIG 51-140-17.

Part: SKIN — DENTED (BS 713) · airframe 62,995 hrs · 37,069 cycles

DURING SNOW REMOVAL OPS DAMAGE OCCURRED TO LT AFT FUSELAGE SKIN, FS713, WL175, LBL82. REQUIRING MAJOR REPAIR. REPAIRED IAW LAC MEA382-53-10-055.

Part: SKIN — DENTED (CARGO DOOR) · airframe 62,527 hrs · 36,762 cycles

DURING AIRCRAFT LOADING CARGO DOOR OUTER SKIN DENTED AT FS 890, WL 270, LBL 12. REPAIRED BY INSTALLING DOUBLER IAW LOCKHEED SMP583 FIG 51-140-12.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 62,384 hrs · 36,675 cycles

DURING SCHEDULED A CHECK FOUND LT HORIZONTAL STABILIZER LEADING EDGE CRACK AT HSS156-162. REPAIRED IAW LAC MEA 382-55-10-37.

Part: DUCT — CRACKED (CARGO BAY) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313 FOUND CARGO COMPT MIXING CHAMBER INLET SCOOP WITH CRACKS. REPAIRED IAW LAC MEA 382-21-10-013.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC4912 FOUND APU COMPT UPPER LONGERON EXFOLIATION CORROSION AT FS 457, WL 180, LBL 65. REPLACED LONGERON IAW SMP583 CHAPTER 51-60 & 51-70.

Part: GUSSET — CRACKED (CARGO DOOR) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5315 FOUND CARGO DOOR INTERIOR LT GUSSET CRACKED AT FS 880, LBL 50. REPLACED GUSSET IAW SMP583 CHAPTER 51-60 & 51-70.

Part: FAIRING — WARPED (FUSELAGE) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5321 FOUND RAMP DOOR PEDESTAL FWD FAIRING WARPED AT RAMP STA 5-6, BL 15L/R, WL 146. REPLACED FWD FAIRING ASSY IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5321 FOUND AFT FUSELAGE EXTERIOR SKIN WRINKLE AT FS 797 TO FS 836, LBL 62, WL 170. REPAIRED IAW LAC MEA 382-53-10-012.

Part: FITTING — CORRODED (NLG) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5321 FOUND NOSE WHEEL BRACE FITTINGS CORROSION BEYOND LIMITS AT FS 196, WL 146, LBL 4 & RBL 4. REPLACED LT & RT BRACE FITTINGS IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CRACKED (WING) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK WHILE REPLACING LT RAINBOW FITTINGS FOUND LOWER CTR WING PLANK & STRINGER 15 SWORD FITTING LAYERS WITH FASTENER HOLE CRACKS AT CWS 220, WL 256.5. REPAIRED IAW LAC MEA 382-57-10-014.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5315 FOUND RAMP DOOR INTERIOR INTERCOSTAL BEAM WEB CRACKED AT RAMP STATION 6.1, BL 0, WL 150. REPLACED BEAM WEB IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CRACKED (WING) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK WHILE REPLACING LT RAINBOW FITTINGS FOUND LOWER CTR WING NR 2 PLANK LAYERS AT STRINGER 16 AND BETWEEN STRINGER 16 & 17, & STRINGER 12 SWORD FITTING LAYERS WITH FASTENER HOLES CRACKED AT CWS 220, WL 256.5. REPAIRED IAW LAC MEA 382-57-10-014.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5321 FOUND RT MAIN WHEEL WELL BHD WEB CRACKED AT FS 520, RBL 61.6, WL 184. REPAIRED IAW LAC MEA 382-53-10-015.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC2411 FOUND UNDER DECK LT BHD SUPPORT CRACKED AT FS 180, LBL 20, WL 170. REPLACED SUPPORT IAW SMP583 CHAPTER 51-60 & 51-70 & LOCKHEED SB A382-53-51.

Part: WEB — CRACKED (CARGO DOOR) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5315 FOUND RAMP DOOR INTERIOR BHD WEB & UPPER 'L' ANGLE CRACKED AT RAMP STATION 6 LBL 5. REPLACED WEB AND 'L' ANGLE IAW SMP583 CHAPTER 51-60 & 51-70.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 62,203 hrs · 36,556 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5321 FOUND UPPER AFT FUSELAGE REINFORCE U-CHANNEL CRACKED AT FS 1038, BL 0, WL 285. REPLACED CHANNEL IAW LOCKHEED DRAWING 341749-3.

Part: GASKET — LEAKING (NR 4 PROPELLER) · airframe 61,737 hrs · 36,425 cycles

DURING CRUISE FLIGHT NR 4 PROP LOW OIL LIGHT ILLUMINATED DUE TO LOW OIL AND SUBSEQUENT PROP FEATHERING FAILURE RESULTING IN THE FLIGHT CREW PERFORMING AN ENGINE SHUT-DOWN IAW QRH. REPLACED FAILED STANDBY FILTER COVER GASKET P/N 69494R223.

Part: ARM — CORRODED (RUDDER) · airframe 61,500 hrs · 36,376 cycles

DURING SCHEDULED B3 CHECK PER JOB CARD HB1204 FOUND RUDDER TORQUE ARM TO RUDDER TORQUE TUBE ATTACH HARDWARE LOOSE AND ROD-END AT INPUT OF TORQUE ARM WORN BEYOND LIMITS. FOUND TORQUE ARM CORROSION UPON DISASSEMBLY. REPAIR ACCOMPLISHED BY REPLACING RUDDER TORQUE ARM AND HARDWARE, AND RUDDER PUSH-ROD AFT ROD-END BEARING IAW LOCKHEED MARTIN L382 MM CH 27-20.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 60,239 hrs · 36,038 cycles

DURING SCHEDULED B-1 CHECK, FOLLOWING REMOVAL TO FACILITATE OTHER MAINTENANCE, FOUND CARGO DOOR INTERIOR INTERCOSTAL ANGLE EXFOLIATION CORROSION AT FS 858-880, RBL 44. REPAIRED BY REPLACING ANGLE IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 60,239 hrs · 36,038 cycles

DURING SCHEDULED B-1 CHECK PER JOB CARD HB3200, FOUND LT MWW BULKHEAD WEB RISER CRACKED AT FS 617, LBL 71, WL 185. REPAIRED BY REPLACING WEB IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: RIB — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57119, FOUND RT CENTER WING AUX TANK COMPT RIB FOOT CAP CRACKED AT FS597, CWS100R, WL256.5. REPAIRED IAW LAC MEA 382-57-09-003.

Part: SKIN — CRACKED (BS 139) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5301, FOUND FUSELAGE EXTERIOR SKIN WITH MULTIPLE CRACKS AT FS 139, LBL59, WL208 TO WL216. REPAIRED IAW SMP583 FIG 51-140-12.

Part: INTERCOSTAL — CRACKED (CARGO DOOR) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND CARGO DOOR INTERCOSTAL SUPPORT CRACKED AT FS 883, LBL 50 TO RBL 50 (2 PLACES). REPAIRED IAW SMP583 FIG 51-140-19.

Part: FLOORBEAM — CORRODED (BS 242) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5301, FOUND UNDER DECK FLOORBEAM UPPER CAP TIE DOWN POINT EXFOLIATION CORROSION AT FS 242, WL 146, LBL 56. REPLACED IAW DRAWING 389183.

Part: BULKHEAD — CRACKED (BS 968) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE UPPER BULKHEAD FWD FLANGE CRACKED AT VERTICAL FIN ATTACHMENT AT FS 968, RBL18, WL286. REPAIRED IAW SMP583 FIG 53-50-06.

Part: BULKHEAD — CRACKED (BS 968) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE UPPER BULKHEAD CRACKED AT FS 968, WL286, LBL18. REPAIRED IAW SMP583 FIG 53-50-06.

Part: RIB — CRACKED (CENTER WING) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57119, FOUND RT CENTER WING AUX TANK COMPT RIB FOOT CAP CRACKED AT FS 522, CWS139R, WL256.5. REPAIRED IAW LAC MEA 382-57-09-008.

Part: STRINGER — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57217, FOUND CRACK ON RT CENTER WING UPPER CHANNEL STRINGER NR 5. REPAIRED IAW LAC MEA 382-57-09-006.

Part: FITTING — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57257, FOUND CRACK AT LT FWD LOWER CENTER WING JOINT CORNER FITTING BOLT HOLE FS 517, CWS220L, WL256.5. REPLACED IAW DRAWING 390604.

Part: BULKHEAD — CRACKED (BS 477) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5316, FOUND BULKHEAD CRACKED AT FS477, RBL30, WL282. FABRICATED AND INSTALLED REPLACEMENT IAW DRAWING 340043.

Part: PANEL — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57217, FOUND CRACK ON RT CENTER WING UPPER SURFACE PANEL AT FS 574.25, CWS213.6R, WL285. REPAIRED IAW LAC MEA 382-57-09-005.

Part: BULKHEAD — CRACKED (BS 477) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5316, FOUND BULKHEAD CRACKED AT FS 477, LBL30, WL282. FABRICATED AND INSTALLED REPLACEMENT IAW DRAWING 340043.

Part: FITTING — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57257, FOUND CRACK AT RT FWD LOWER CENTER WING JOINT CORNER FITTING BOLT HOLE FS 517, CWS 220R, WL 256.5. REPLACED IAW DRAWING 390604.

Part: RIB — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57119, FOUND RT CENTER WING AUX TANK COMPT RIB FOOT CAP CRACKED AT FS 521, CWS100R, WL256.5. REPAIRED IAW LAC MEA 382-57-09-003.

Part: BEAM — CRACKED · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC3212, FOUND RT MLG WHEEL WELL UPPER END BOW BEAM REPAIR DOUBLER CRACKED AT FS 537, RBL61.1, WL198. REPLACED REPAIRED DOUBLER IAW SMP583 FIG 53-40-14.

Part: FLOOR SUPPORT — CORRODED (BS 196-220) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND FLIGHT DECK FLOOR SUPPORT UPPER CAP EXFOLIATION CORROSION. REPAIRED IAW SMP583 FIG 51-140-23.

Part: FLOORBEAM — CORRODED (BS 180) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND COCKPIT FLOORBEAM UPPER CAP EXFOLIATION CORROSION AT FS 180, WL195, RBL12. FABRICATED AND INSTALLED UPPER CAP IAW SMP583 FIG 53-30-05 AND CHAP 51-70.

Part: RIB — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57119, FOUND RT CENTER WING AUX TANK COMPT RIB FOOT CAP CRACKED AT FS 527, CWS100R, WL256.5. REPAIRED IAW LAC MEA 382-57-09-003.

Part: PANEL — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57256, FOUND CRACK ON LT CENTER WING LOWER PANEL NR 2 AT FS 554, CWS213.6L, WL256.5. REPAIRED IAW LAC MEA 382-57-09-004.

Part: FITTING — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57217, FOUND CRACK ON RT LOWER CENTER WING RAINBOW FITTING CUTOUT NR 5. REPLACED RAINBOW FITTING IAW SB 382-57-82 REV 3.

Part: RIB — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57119, FOUND RT CENTER WING AUX TANK COMPT RIB FOOT CAP CRACKED AT FS 527, CWS139R, WL256.5. REPAIRED IAW LAC MEA 382-57-09-009.

Part: RIB — CRACKED (WING BOX) · airframe 59,606 hrs · 35,803 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HSP57119, FOUND LT CENTER WING AUX TANK COMPT RIB FOOT CAP CRACKED AT FS 517, WL256.5, CWS100L. REPAIRED IAW LAC MEA 382-57-09-007.

Part: BRUSH BLOCK — WORN (PROP DEICE SYS) · airframe 59,583 hrs · 35,800 cycles

FLAME OUT NR 1 ENGINE DURING HEAVY ICING. COMPLIED IAW AOM, SHUTDOWN ENGINE 0100Z. INSPECTED AIR INTAKE, COMPRESSOR BLADES, 5TH AND 10TH STAGE COMPRESSOR BLEEDS, TURBINE SECTION BLADES, AND MAG PLUGS, NO DEFECTS NOTED. OPS CHECK NR 1 ENGINE REF SMP581 CH 71-00. OPS CHECK GOOD. SUSPECT BRUSH BLOCK, CREW REPORTED NR 1 BLADE DE-ICING 55 AMPS. REMOVED AND REPLACED NR 1 BRUSH BLOCK ASSY REF HAM STANDARD P5059 PAG I-798.1-I-798.8, OPS CHECK GOOD.

Part: SKIN — CRACKED (FAIRING) · airframe 58,958 hrs · 35,666 cycles

DURING SCHEDULED B-3 CHECK, PER HB5301 JOB CARD FOUND LT MLG BOTTOM SKIN FAIRING CRACKED AT FS 597, LBL40, WL129 ATTACHMENT TO BELLY AREA. REPAIRED IAW SMP583 FIG 51-140-12.

Part: FITTING — CRACKED (FS 858) · airframe 58,958 hrs · 35,666 cycles

DURING SCHEDULED B-3 CHECK, PER HB5302 JOB CARD, FOUND AFT FUSELAGE INTERIOR STRUT TO SLOPING LONGERON TEE FITTING CRACKED AT FS 858. REPLACED FITTING IAW SMP583 CHAP 51-70.

Part: SKIN — PUNCTURED (CARGO DOOR) · airframe 58,958 hrs · 35,666 cycles

EN ROUTE TO SCHEDULED B-3 CHECK, FOUND 1/4 INCH HOLE IN CARGO DOOR SKIN AT FS 877, LBL 10, WL 201. AIRCRAFT FERRIED TO WSSL FOR B CHECK AND REPAIR. REPAIRED IAW SMP583 FIG 51-140-10.

Part: VALVE — DAMAGED (NR 3 PROP) · airframe 58,317 hrs · 35,190 cycles

DURING CRUISE FLIGHT, CREW REPORTED NR 3 PROPELLER RPM OUT OF LIMITS. PERFORMED ENGINE SHUT DOWN IAW ESP. NR 3 PROPELLER VALVE HOUSING REPLACED IAW LAC JOB CARD HN61135, OPS CHECK GOOD.

Part: ANGLE — CRACKED (FS 557) · airframe 58,246 hrs · 35,131 cycles

DURING SCHEDULED B-2 CHECK, PER JOB CARD HB3200, FOUND RT MLG WHEEL WELL CHINE ANGLE CRACKED AT FS557 WL141. REPAIR IAW SMP583 FIG 51-140-19.

Part: BEAM — CRACKED (ELEVATOR TAB) · airframe 58,246 hrs · 35,131 cycles

DURING SCHEDULED B-2 CHECK, PER JOB CARD HB2703, FOUND RT ELEVATOR TRIM TAB INBD FRONT BEAM CRACK AT HSS72. REPAIR ACCOMPLISHED IAW SMP583 FIG 55-30-04 .

Part: BULKHEAD — CRACKED (FS 880) · airframe 58,246 hrs · 35,131 cycles

DURING SCHEDULED B-2 CHECK, PER JOB CARD HB5302, FOUND LT AFT FUSELAGE INTERIOR LOWER BULKHEAD WEB CRACKED THROUGH FASTENER HOLE AT FS 880L, WL200. REPAIR IAW DRAWING 342582 BY FABRICATING AND INSTALLING WEB.

Part: LONGERON — CRACKED (PAX DOOR) · airframe 58,246 hrs · 35,131 cycles

DURING SCHEDULED B-2 CHECK, PER JOB CARD HB5305, FOUND CREW DOOR LONGERON CRACKED THRU RIVET HOLE ADJACENT TO MICROSWITCH AT FS 241 WL195. REPAIR IAW SMP583 FIG 51-140-19.

Part: BRACKET — CRACKED (ELEVATOR TAB) · airframe 58,246 hrs · 35,131 cycles

DURING SCHEDULED B-2 CHECK, PER JOB CARD HB2703, FOUND ELEVATOR BRACKETS IN TRIM TAB WELL CRACKED AT HSS77R AND HSS113R. REPAIR BY BRACKET FABRICATION AND INSTALLATION IAW SMP583 CH 51-60 AND 70 AND DRAWING 353948-4R.

Part: BULKHEAD — CRACKED (FS 880) · airframe 58,246 hrs · 35,131 cycles

DURING SCHEDULED B-2 CHECK, PER JOB CARD HB5302, FOUND RT AFT FUSELAGE INTERIOR LOWER BULKHEAD WEB CRACKED THROUGH FASTENER HOLE AT FS 880R, WL 200. REPAIR IAW DRAWING 342582 BY FABRICATING AND INSTALLING WEB.

Part: FRAME — CRACKED (FS 814) · airframe 57,611 hrs · 34,996 cycles

DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302, FOUND CABIN BULKHEAD INBD FRAME CRACKED AT FS 814, WL176, RBL 67. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-14.

Part: BULKHEAD — CRACKED (FS 846) · airframe 57,611 hrs · 34,996 cycles

DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302, FOUND CABIN BHD CRACKED AT FS 846, WL170, RBL73. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-10.

Part: BRACKET — CRACKED (CARGO BAY) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC2111 FOUND CARGO AIR COND AUX VENT DUCT ASSY UPPER & LOWER MOUNTING BRACKET CRACKED. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-21-07-066.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321 FOUND BELLY EXTERIOR SKIN DENTS / SCRATCHES WITH EXISTING PATCHES AT FS 377 TO 417 BL 61L TO 61R. REPAIR ACCOMPLISHED BY REPLACING BELLY SKIN IAW SMP583 CHAPTER 51-60 & 51-70 USING 2024T3 .071".

Part: RIB — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5311 FOUND COCKPIT RIB CRACKED AT FS 132 WL 207 TO 215 LBL 61. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70 USING 2024T3 .050".

Part: BEAM — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RIGHT UPPER MWW BOW BEAM CRACKED AT FS 557 WL 202 RBL 64. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-14 USING 7075T6, .100".

Part: BEAM — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RT UPPER MWW BOW BEAM CRACKED AT FS 537 WL 202 RBL 64. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-14 USING 7075T6 .100".

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND UPPER MWW ATTACH ANGLE WITH MULTIPLE CRACKS AT FS 477 TO 517 WL 280 RBL 62.5. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70 USING 7075T6 .050".

Part: MANIFOLD — CRACKED (RT MLG WW) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RIGHT MWW MANIFOLD CRACKED AT FS 607 WL 146 RBL 62. REPAIR ACCOMPLISHED BY REPLACING MANIFOLD IAW SMP583 CHAPTER 51-60 & 51-70.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RIGHT MLG FRAME INNER CAP CRACKED AT FS 528 WL 232-240 RBL 66. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-53-07-063.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321 FOUND BELLY EXTERIOR SKIN CRACKED AT FS 477 WL 128 BL 3R. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 CHAPTER 51-70 USING 2024T3 .080".

Part: BRACKET — CRACKED (APU EXHAUST) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC4912 FOUND APU EXHAUST DUCT ASSY BRACKET CRACKS. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-49-07-065.

Part: LONGERON — CRACKED (VERTICAL STAB) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5511 FOUND LT & RT DORSAL FIN LOWER LONGERON REPAIR DOUBLER FOUND CRACKED AT FS 850. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA382-53-00-087 AND MEA382-53-00-088.

Part: MANIFOLD — CRACKED (LT MLG WW) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5323 FOUND LT MWW MANIFOLD CRACKED AT FS 507, 542 & 567 WL 146 BL 62. REPAIR ACCOMPLISHED BY REPLACING IAW SMP583 CHAPTER 51-60 & 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5313 FOUND AFT FUSELAGE INTERIOR BULKHEAD WEB CRACK AT HI-LOK PIN HOLE FS 880 WL 210 RBL 73. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17 USING 7075T6 .040".

Part: SPLICE — CRACKED (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5317 FOUND CABIN OVERHEAD RING SEGMENT SPLICER CRACKED AT FS 477 WL 285 RBL 20. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: ATTACH ANGLE — CRACKED (FS477WL284RBL32) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5316 FOUND RT AERODYNAMIC FAIRING ATTACH ANGLE CRACKED, DURING SP-126 INSPECTION AT FS 417 WL 284 RBL 32-60. REPAIR ACCOMPLISHED BY REPLACING ATTACH ANGLE IAW AD92-10-14, SB 382-53-27 R1, SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5212 FOUND AFT CARGO DOOR AFT BULKHEAD SKIN CRACKS AT FASTENER HOLES FS 1040 WL 268 LBL 44 RBL 44. REPAIR ACCOMPLISHED BY REPLACING SKIN IAW SMP583 CHAPTER 51-60 & 51-70 USING 7075T6 .025".

Part: FRAME — BROKEN (FUSELAGE) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324 FOUND RT MLG FRAME OUTBOARD CAP BROKEN AT FS 528 WL 209 & 232 RBL 66. REPAIR ACCOMPLISHED IAW LYNDEN AIR CARGO MEA 382-53-07-063.

Part: CHANNEL — CRACKED (NLG WW) · airframe 56,958 hrs · 34,806 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC3215 FOUND NOSE WW BULKHEAD U-CHANNEL CRACKED AT FS 196 WL 145 BL 0. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: BULKHEAD — CRACKED (FS 836, LBL 83) · airframe 56,701 hrs · 34,614 cycles

DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND LEFT BULKHEAD WEB CRACKED AT FS 836, LBL 83, WL 212-223. REPAIRED BULKHEAD WEB IAW LAC MEA 382-53-07-053.

Part: BULKHEAD — CRACKED (FS 836 RBL 83) · airframe 56,701 hrs · 34,614 cycles

DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND RIGHT BULKHEAD WEB CRACKED AT FS 836, RBL 83, WL 212-222. REPAIRED BULKHEAD WEB IAW LAC MEA 382-53-07-053.

Part: CHECK VALVE — LEAKING (FUEL SYSTEM) · airframe 46,407 hrs · 34,375 cycles

FLIGHT CREW REPORTED VISUAL FLUID LEAK BEHIND NR 3 ENGINE ON CLIMBOUT FROM TIN. PERFORMED PRECAUTIONARY SHUT DOWN ON ENGINE NR 3 IAW WITH PROCEDURES AND DIVERTED TO ANC FOR MAINTENANCE. FOUND FUEL LEAKAGE INTO PREVIOUSLY DE-ACTIVATED AUXILARY TANK BLADDER DURING REFUELING, DUE TO DEFECTIVE CHECK VALVE. REPLACED CHECK VALVE, LOG PAGE 26636 GMM133 ITEM M14. REPLACED RIGHT AUXILARY FUEL TANK BLADDERS, LOG PAGE 26636 ITEM 1.

Part: BULKHEAD — CRACKED (FS 990) · airframe 56,382 hrs · 34,367 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT BULKHEAD UPPER FUSELAGE TO SIDE BULKHEAD ATTACHMENT GUSSET PLATE CRACKED AT FS 990, RBL 61, WL 256. REPLACED PLATE IAW SMP583 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (FS 968) · airframe 56,382 hrs · 34,367 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE UPPER BULKHEAD CRACKED AT FS 968, RBL 18, WL 285. REPAIRED BULKHEAD IAW SMP583 53-50-06.

Part: BEAM — BROKEN (FS 497) · airframe 56,382 hrs · 34,367 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB3200, FOUND LT MWW BOW BEAM INBD CAP BROKEN AT FS 497, LBL63, WL158. REPLACED CAP IAW SMP 583 51-60 AND 51-70.

Part: WEB — CRACKED (FS 750) · airframe 56,050 hrs · 34,027 cycles

DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND LT SIDE RAMP WEB SKIN GOUGED AND CRACKED BETWEEN RAMP STN 0 AND STN 2 AT FS750, WL146, BL61. REPAIRED RAMP WEB SKIN IAW SMP583 FIG 51-140-12, LOG PAGE 26257 ITEM M1.

Part: WINDOW FRAME — CRACKED (FS 124 WL 251) · airframe 55,674 hrs · 33,688 cycles

DURING SCHEDULED B 2 CHECK PER JOB CARD HB5301, FOUND RT DV WINDOW FRAME CRACKED AT FS 124, WL 251. REPAIRED FRAME IAW SMP583 53-30-25 AND LAC MEA 382-53-07-007.

Part: FITTING — DAMAGED (RT WING) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B 1 CHECK PER JOB CARD HSP5785, FOUND NR 4 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP INBOARD FITTING BOLT HOLES OVERSIZED AT RT OWS162.8. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-086.

Part: FITTING — DAMAGED (LT WING) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE OUTBOARD TRUSS MOUNT UPPER RIB CAP OUTBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS197.2. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-086.

Part: FITTING — DAMAGED (LT WING) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE OUTBOARD TRUSS MOUNT UPPER RIB CAP INBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS197.2. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-086.

Part: FITTING — DAMAGED (LT WING) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP INBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS162.8. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-042.

Part: FITTING — DAMAGED (LT WING) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HSP5785, FOUND NR 1 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP OUTBOARD FITTING BOLT HOLES OVERSIZED AT LT OWS162.8. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-042. NR 1101.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB5301, FOUND RAMP SKIN CRACKED AT RS4-RS8, BL 0. REPAIRED SKIN IAW SMP 583 FIG 51-140-12.

Part: FITTING — DAMAGED (RT WING) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B 1 CHECK PER JOB CARD HSP5785, FOUND NR 4 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP OUTBOARD FITTING BOLT HOLES OVERSIZED AT RT OWS162.8. REPLACED FITTING IAW LOCKHEED DWG 3325557 AND LAC MEA 382-57-06-086.

Part: FITTING — CRACKED (WING) · airframe 55,004 hrs · 33,543 cycles

DURING SCHEDULED B 1 CHECK PER JOB CARD HSP57131, FOUND NR 3 ENGINE INBOARD TRUSS MOUNT UPPER RIB CAP OUTBOARD FITTING CRACKED AT CWS178.8. REPLACED FITTING IAW LOCKHEED DWG 371232 AND LAC MEA 382-57-06-087. NR 1105

Part: ATTACH FITTING — DAMAGED (LT WING) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK, FOUND NR 1 INBD TOP TRUSS MOUNT ATTACH FITTING TO HAVE OVERSIZED HOLE AT FS 517, LT OWS 162, WL 280. REPLACED FITTING IAW LOCKHEED DWG 3308216.

Part: DOUBLER — CRACKED (CARGO RAMP) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5211 FOUND CARGO RAMP AFT LT SIDE BEAM ATTACHMENT DOUBLER CRACKED AT RAMP STA 10, LBL 61. REPLACED ANGLE IAW SMP583 51-140-19.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5315, FOUND RT SIDE BULKHEAD WEB CRACKED AT FS 902, RBL 61, WL 200. REPAIRED WEB IAW LOCKHEED SMP583 51-140-12.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK, FOUND PRESSURE BULKHEAD WEB CRACKED AT FS 617, LBL 61.62, WL 250. REPLACED WEB IAW SMP583 CHAP 51.

Part: CAP — CRACKED (MLG WW) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC3213 FOUND MLG BEAM INNER CAP CRACKED AT FS 517 RT, WL 256. REPAIRED BEAM IAW LAC MEA 382-53-06-036.

Part: BEAM — CRACKED (CARGO RAMP) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5211, FOUND CARGO RAMP AFT RT SIDE BEAM WEB CRACKED AT RAMP STA 10, RBL 61. REPAIRED WEB IAW LAC MEA 382-52-06-020.

Part: WEB — DAMAGED (CARGO DOOR) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5212 FOUND CARGO DOOR FWD WEB DAMAGED AT FS 869 LBL 61-RBL 61. REPLACED WEB IAW LAC MEA 382-52-06-032.

Part: SPAR CAP — CORRODED (T/E FLAP) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5712 FOUND RT OUTBOARD FLAP LWR SPAR CAP CORRODED AT FLAP STATION 163-208. REPAIRED CAP IAW LAC MEA 382-27-06-027.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5313 FOUND LT AND RT FRAME SPLICES CRACKED AT FS 617, LBL 20 AND RBL 20, WL 260. REPLACED FITTINGS IAW LOCKHEED DWG 343067.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5321 FOUND RT CHINE ANGLE CRACKED AT FS 245-377, LBL 61.62, WL 146. REPLACED ANGLE IAW LOCKHEED DRAWING 372321 AND LAC MEA 382-53-06-034.

Part: CAP — CRACKED (CARGO RAMP) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5211, FOUND CARGO RAMP LT UPPER SIDE BEAM CAP CRACKED AT RAMP STA 8, LBL 61. REPAIRED CAP IAW SMP583 51-140-23.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HSP53297 FOUND ANGLE CRACKED AT FS 132, RBL 58, WL 200-231. REPLACED ANGLE IAW LOCKHEED DWG 362011 AND 339010.

Part: ATTACH FITTING — DAMAGED (LOWER TRUSS) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK FOUND NR 4 I/B LWR TRUSS MOUNT ATTACH FITTING TO HAVE OVERSIZED HOLE AT FS 517, RT OWS 162, WL 260. REPAIRED FITTING IAW LAC MEA 382-57-06-022.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC3213 FOUND MLG WHEEL WELL FORMER DAMAGED AT FS 491 RT, RBL 70, WL 130. REPAIRED FORMER IAW LAC MEA 382-53-06-028.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC3214, FOUND SIDE SKIN CORRODED AT FS 477, LBL 80, WL 155. REPLACED SKIN IAW LOCKHEED DWG 370790.

Part: BEAM — CRACKED (CARGO RAMP) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5211, FOUND CARGO RAMP AFT LT SIDE BEAM WEB CRACKED AT RAMP STA 10, LBL 61. REPLACED WEB IAW LOCKHEED DWG 353614.

Part: REPAIR — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HHC3214 FOUND BEAM REPAIR PLATE CRACKED AT FS 597, RBL 64, WL 140. REPAIRED BEAM IAW SMP583 53-40-30.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5321 FOUND LOWER BELLY SKIN PANEL FRAME CRACKED AT FS 340, RBL 50, WL 132. REPAIRED FRAME IAW SMP583 51-140-21.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5212 FOUND CARGO DOOR FWD BULHEAD SUPPORT STIFFENER CRACKED AT FS 869, LBL 15. REPAIRED STIFFENER IAW SMP583 51-140-23.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC53125, FOUND RING FRAME CRACKED AT FS 968, RBL 20, WL 285. REPLACED RING FRAME ASSY IAW LOCKHEED DWG 368198.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5212, FOUND AFT CARGO DOOR LT LWR SIDE BEAM CRACKED AT FS 1041, LBL 60, WL 268. REPAIRED BEAM IAW LAC MEA 382-52-06-018.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5321, FOUND LOWER BELLY BEAM CAP CORRODED AT FS 277, RBL 61 TO LBL 61, WL 126. REPLACED LOWER CAP IAW LOCKHEED DWG 388019.

Part: BRACE — DAMAGED (RT FLAP TRACK) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5712 FOUND RT INBOARD FLAP TRACK BRACE DAMAGED AT CWS 108 RT. REPLACED BRACE IAW LAC MEA 382-57-06-038.

Part: COVER — DAMAGED (NR 3) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5701 FOUND NR 3 DRY BAY COVER DAMAGED. REPAIRED COVER IAW LAC MEA 382-57-06-031.

Part: SKIN — CRACKED (RT WING) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER SB3825785/2 FOUND NR 2 LWR RT WING PLANK CRACKED AT FS 542, CWS 62R, WL 256. REPAIRED PLANK IAW LAC MEA 382-57-06-016.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC3214 FOUND ANGLE CORRODED AT FS 557, LBL 70, WL 200. REPLACED ANGLE IAW LOCKHEED DRAWING 371610 AND LAC MEA 382-53-06-040.

Part: SKIN — SCORED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5321, FOUND LOWER BELLY SKIN SCORED AND IMPACT DAMAGED AT FS 337 TO FS 377, RBL 62 TO LBL 62, WL 126 TO WL 146. REPLACED SKIN IAW LOCKHEED DWG 375256.

Part: ANGLE — DAMAGED (CARGO RAMP) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5211 FOUND CARGO RAMP AFT SHELF PANELS AND SUPPORT BEAMS DAMAGED AT RAMP STN 10, RBL 30-61. REPLACED ANGLE IAW LOCKHEED DRAWING 353612.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5313 FOUND CARGO BAY LT AND RT OVERHEAD WEB LWR CHANNELS CRACKED AT FS 617, LBL 25 AND RBL 25, WL 277. REPLACED LT AND RT CHANNELS IAW LOCKHEED DWG 343067.

Part: ANGLE — CRACKED (CARGO RAMP) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5211, FOUND CARGO RAMP LT STRIKER ANGLE CRACKED AT RAMP STA 0 THRU 6, LBL 61. REPLACED ANGLE IAW LOCKHEED DWG 353614.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5321, FOUND LOWER BELLY BEAM CAP CORRODED AT FS 317, RBL 61 TO LBL 61, WL 126. REPLACED LOWER CAP IAW LOCKHEED DWG 388019.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5315, FOUND RING FRAME CRACKED AT FS 858, LBL 61, WL 265. REPAIRED RING FRAME IAW LOCKHEED SMP 583 51-140-19.

Part: WEB — CRACKED (CENTER WING) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER SB 382-57-85 FOUND RT CNTR WING REAR WEB CRACKED AT RT CWS 84.3-140. REPAIRED WEB IAW SMP583 57-30-22.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC3213 FOUND MLG WHEEL WELL LONGERON CORRODED AT FS 491RT, WL 170. REPAIRED LONGERON IAW LAC MEA 382-53-06-026.

Part: SPAR — CRACKED (CENTER WING) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HSP57119/L FOUND CENTER WING FWD SPAR WEB CRACKED AT CWS 20.5, FS 517, WL 287. REPAIRED WEB IAW LAC MEA 382-57-06-017.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5315, FOUND RING FRAME CRACKED AT FS 803, LBL 61, WL 265. REPAIRED RING FRAME IAW LOCKHEED SMP 583 51-140-19.

Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HSP53297 FOUND FUSELAGE RIB TO SILL ATTACHMENT ANGLE DAMAGED AT FS 132, WL 231. REPAIRED ANGLE IAW LAC MEA 382-53-06-037.

Part: FITTING — OVERSIZED (RT WING) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK, FOUND NR 4 OB TOP TRUSS MOUNT ATTACH FITTING TO HAVE OVERSIZED HOLE AT FS 517, RT OWS 197, WL 280. REPLACED FITTING IAW LOCKHEED DWG 3308216.

Part: RIB — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HSP53297 FOUND RIB CRACKED AT FS 132, RBL 58, WL 200-231. REPLACED RIB IAW LOCKHEED DWG 362011 AND 339010.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC5321, FOUND LOWER BELLY SKIN SCORED AND IMPACT DAMAGED AT FS 297 TO FS 337, RBL 62 TO LBL 62, WL 126 TO WL 146. REPLACED SKIN IAW LOCKHEED DWG 375256.

Part: PRESSURE PANEL — CORRODED (LT MLG WW) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC3214 FOUND LT MLG WHEEL WELL WEB CORRODED AT FS 515-596, WL 200. REPLACED WEB IAW LOCKHEED DWG 371610 AND LAC MEA 382-53-06-029.

Part: STRINGER — CRACKED (CENTER WING) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER SB3825785/2 FOUND NR 12 STRINGER LWR FWD TOP HAT SECTION CRACKED AT FS 525, CWS 9R, WL 257. REPAIRED STRINGER IAW SMP583 57-30-13 AND LAC MEA 382-57-06-023.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 54,297 hrs · 32,936 cycles

DURING SCHEDULED C6 CHECK PER JOB CARD HC3214 FOUND SPLICE ANGLE CRACKED AT FS 477, BL 61-75, WL 154. REPAIRED ANGLE IAW SMP583 51-140-22.

Part: CAP — CRACKED (BULKHEAD) · airframe 53,646 hrs · 32,810 cycles

DURING 'B-3' CHECK PER HB5302, FOUND LOWER FLANGE OF BULKHEAD CAP CRACKED 3 INCHES AT FS902, WL195, RBL64. REPAIRED CAP IAW SMP583 FIG. 53-50-17. N/R NO. 0078.

Part: ENGINE — FLAMED OUT (NR 4) · airframe 53,052 hrs · 32,618 cycles

FLIGHT CREW REPORTED DURING APPROACH, NR 4 ENGINE FLAMED OUT ON SHORT FINAL AFTER WAKE TURBULENCE ENCOUNTER. ENGINE WAS AT FLIGHT IDLE. DURING MAINTENANCE EVALUATION GROUND RUN NR 4 RRM AT 105 PERCENT AT FLIGHT IDLE. REPLACED PROPELLER ASSY IAW HN6101 AND 61135. OPS CHECK NORMAL IAW HN7101.

Part: FAIRING — LIGHTNING STRIKE (FS 1128) · airframe 52,996 hrs · 32,587 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB2703 FOUND EVIDENCE OF LIGHTNING STRIKE AT RUDDER FAIRING TIP, FS 1128, VSS 277. REPAIRED IAW LAC MEA 382-53-05-062.

Part: SKIN — CRACKED (FS 900) · airframe 52,996 hrs · 32,587 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND FS 900 FUSELAGE SKIN CRACKED AT RBL 59, WL 215. REPAIRED IAW SRM SMP 583 51-140-12.

Part: SKIN — CRACKED (FS 105) · airframe 52,996 hrs · 32,587 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5303 FOUND FS 105 FUSELAGE SKIN CRACKED AT CO-PILOTS DV WINDOW APERTURE, RBL 60, WL 231. REPAIRED IAW LAC MEA 382-53-05-065.

Part: SKIN — DENTED (FS 440) · airframe 52,996 hrs · 32,587 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND DENT IN FS 440 FUSELAGE SKIN AT WL 200, RBL 70. REPAIRED IAW SRM SMP 583 51-140-10.

Part: TEE FITTING — CORRODED (FS 588-596) · airframe 52,996 hrs · 32,587 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WHEEL WELL TEE AND WEB CORRODED AT FS 588 TO 596, LBL 65, WL 138. REPLACED TEE AND WEB IAW SRM SMP 583 51-60 AND 70.

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,399 hrs · 32,385 cycles

DURING SCHEDULED B-1 CHECK INSPECTION PER JOB CARD HB5303 FOUND FS 792 RT SUPPORT BEAM TO SLOPING LONGERON LOWER ATTACHMENT T FITTING CRACKED. FITTING REPLACED IAW DRW 342590 AND SMP583 51-60 & 51-70. FS 792, RBL 62.5, WL 160.5-162.

Part: FITTING — CRACKED (FUSELAGE) · airframe 52,399 hrs · 32,385 cycles

DURING SCHEDULED B-1 CHECK INSPECTION PER JOB CARD HB5303 FOUND FS 858 RT SUPPORT BEAM TO SLOPING LONGERON LOWER ATTACHMENT T FITTING CRACKED. FITTING REPLACED IAW DRW 342593 AND SMP583 51-60 & 51-70, FS 858, RBL 62.5, WL 190-192.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 323, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FRAME — MISDRILLED (FUSLEAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 762E, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 444, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 324E, WL 147, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 283, WL 148, LBL 65 & RBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 657, WL 175, LBL 77. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 667, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 782E, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE CARGO COMP STIFFENER EDGE CRACKED AT LT FS 940 WL 280 LBL 16-18. REPLACED STIFFENER IAW SRM SMP 583 CHP 51-60 & 51-70.

Part: BEAM — CRACKED (FUSLEAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND CRACK ON RT BOW BEAM FS 557, WL 197, RBL 63. REPAIRED IAW SRM SMP 583 FIG 53-40-14.

Part: FRAME — MISDRILLED (FS) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 291, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE CARGO COMP BULKHEAD CRACKED AT RT FS 970, WL 280, RBL 15. REPAIRED IAW SRM SMP 583 FIG 53-50-06.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 702, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE RT BULKHEAD INBOARD CAP & WEB CRACKED AT FS 1012, WL 260, RBL 62. WEB & CAP REPLACED IAW SRM SMP 583 CHP 51-60 & 51-70.

Part: BEAM — CRACKED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND CW REAR BEAM WEB CRACKED AT FS 597, WL 276, CWS 52L. REPAIRED IAW LAC MEA 382-57-05-025.

Part: FRAME — CRACKED (WING TO BODY) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5324 FOUND RT UPPER MLG WW WING TO FUSELAGE FAIRING FORMER CRACKED AT FS 522-528, WL 236, RBL 72. REPAIRED IAW LAC MEA 382-57-05-025.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 768E, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSLEAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 687, WL 148, RBL 65 AND LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 732, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FITTING — GOUGED (HORIZONTAL STAB) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5511 FOUND VERTICAL STAB ATTACH TO HORIZONTAL STAB FITTING MAIN BOLT HOLE WITH THREAD TYPE GOUGES AT FS 1043, WL 287, LBL 15. REPLACED FITTING IAW SRM SMP583 CHP 51-60 & 51-70.

Part: FITTING — CRACKED (NLG) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HST5301 FOUND CRACK ON NLG FWD DOOR ASSY LT HINGE FITTING AT FS 165. REPAIRED IAW LAC MEA 382-53-05-027.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 384, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED, MIS-DRILLED FUSELAGE LINER HOLES AT FS 637, WL 176, LBL 77. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 647, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 767, WL 152, RBL 66. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND AFT FUSELAGE INTERIOR BULKHEAD CRACKED AT FS 1020, WL 280 LBL 15. REPAIRED IAW SRM SMP 583 FIG 53-50-7.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 787 WL 178 AND 205, RBL 77. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 707, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: SKIN — DENTED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5321 FOUND BELLY SKIN SCRATCHED AND DENTED AT FS 297E - 345E, BL 40L - 40R. SKIN REPLACED FS 297E - 245E, BL 61L/R IAW SMP583 CHP 51-60 & 51-70.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 364, WL 148, LBL 65. REPAIRED IAW LAC MEA 382-53-04-074 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 807E WL 148 LBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: FRAME — MISDRILLED (FUSELAGE) · airframe 51,745 hrs · 32,248 cycles

DURING SCHEDULED C5 INSPECTION PER JOB CARD HC5313 FOUND ELONGATED / MIS-DRILLED FUSELAGE LINER HOLES AT FS 747, WL 148, RBL 65. REPAIRED IAW LAC MEA 382-53-04-073 R1.

Part: DOOR — DETACHED (EMERGENCY EXIT) · airframe 51,218 hrs · 32,107 cycles

FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO YFB. AT YFB FOUND RT SIDE EMERGENCY EXIT LAYING ON FREIGHT. INSPECTED DOOR ASSY, AIRCRAFT FRAME AND LATCHING MECHANISM. NO DEFECTS NOTED PER MM SMP 581 52-20. REINSTALLED DOOR. OPS CHECK NORMAL.

Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 51,069 hrs · 32,078 cycles

DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND RT MLG BAY FS 575 SIDEWALL SKIN CORRODED AT WL 161, RBL 62. REPAIRED IAW LAC MEA 382-53-04-084.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,069 hrs · 32,078 cycles

DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND LOWER LBL 60 CHINE ANGLE CRACKED AT FS 617, WL 142. REPAIRED IAW ARM SMP 583 53-40-26.

Part: BEAM — CRACKED (MLG) · airframe 51,069 hrs · 32,078 cycles

DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND LT MLG BAY FS 557 LOWER BOW BEAM TEE CAP CRACKED AT WL 171, LBL 66. REPLACED BOW BEAM IAW DWG 372330 AND SRM SMP 583 51-70 AND 53-40-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,069 hrs · 32,078 cycles

DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND RT MLG BAY LOWER SKIN SPLICE STIFFENER FLANGE CRACKED AT FS 537, WL 175, RBL 62. REPLACED SKIN SPLICE FS 537 - 557 IAW SRM SMP 583 51-70.

Part: PROPELLER — OVERSPEED (NR 1 ENGINE) · airframe 50,419 hrs · 31,655 cycles

NR 1 ENGINE OVERSPEED TO 106 PERCENT IN BOTH MECHANICAL AND NORMAL GOVERNING ON FINAL APPROACH. SHUTDOWN IAW QRH. THREE ENGINE FERRY FLIGHT TO ANC FOR REPAIR. AT ANC REPLACED NR 1 PROP ASSY PER JOB CARD HN6101 AND ENGINE RUN PER HN7101.

Part: SKIN — DENTED (FUSELAGE) · airframe 50,350 hrs · 31,608 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB5301 FOUND FS 420 LOWER FUSELAGE SKIN DENTED AT LBL 30, WL 127. REPAIRED IAW SRM SMP 583 51-140-12. NR 0008.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,350 hrs · 31,608 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG FS 497 BOW BEAM CRACKED APPROX. 1.0 INCH AT LBL 64, WL 156. REPAIRED IAW SRM SMP 583 53-40-12.

Part: BEAM — CRACKED (FUSELAGE) · airframe 50,350 hrs · 31,608 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3200 FOUND LT MLG FS 557 BOW BEAM CRACKED APPROX. 1.0 INCH AT LBL 64, WL 156. REPAIRED IAW SRM SMP 583 53-40-12.

Part: WEB — CRACKED (FUSELAGE) · airframe 49,738 hrs · 31,420 cycles

DURING CARGO RAMP CLOSURE, CARGO DOOR LEADING EDGE WEB CRACKED AND STIFFENER ANGLE BROKEN BY CONTACT WITH RAMP SUPPORT STOOL AT FS 869, LBL 15 AND 32, WL 200. REPAIRED IAW LAC MEA 382-52-04-036.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 49,593 hrs · 31,369 cycles

DURING SCHEDULED B1 INSPECTION PER JOB CARD HB2703 FOUND LT FLAPWELL CWS 192 REAR BEAM STIFFENER CRACKED, FS 517, WL 259. REPLACED STIFFENER IAW SRM SMP583 51-60 & 51-70.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 49,233 hrs · 31,204 cycles

DURING SCHEDULED A1 INSPECTION, FOUND FS 1070 HORIZONTAL STAB LOWER SKIN CRACKED AT RBL 50, WL 265. REPAIRED IAW SRM SMP 583 55-20-06. LP 19339, M2.

Part: STATIC INVERTER — FAILED (COCKPIT) · airframe 49,132 hrs · 31,151 cycles

INVERTER FAILED DURING START. ON ENGINE START THE FLIGHT DECK FILLED WITH SMOKE. PROBLEM WAS ISOLATED TO A FAILED STATIC INVERTER. REPLACED ENGINE INSTRUMENT (2500 VA) INVERTER PER SMP581 24-20.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND LT FWD FUSELAGE SKIN CRACKED FS 160, LBL 50, WL 236. REPAIRED IAW SRM SMP 51-140-10. NR 2022.

Part: SKIN — LOOSE (ELEVATOR) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND RT ELEVATOR LOWER SKIN REPAIR WITH LOOSE FASTENERS AT HSS 67. REPLACED ELEVATOR SKIN FROM HSS 51 -90 IAW SMP 583 51-60 & 51-70. NR 2241.

Part: RING — DEFORMED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND RT CENTER FUSELAGE RING SEGMENT DEFORMED AT FS 747E, 752E & 762E, RBL 60, WL 142-148. REPAIRED IAW SRM SMP 583 51-140-23. NR 2238.

Part: SKIN — WARPED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND RT AFT FUSELAGE SKIN WRINKLED FS 737-761, RBL 60, WL 170-186. REPLACED RT FUSELAGE SKIN FS 737-773 IAW SRM SMP 583 51-60 & 51-70. NR 2043.

Part: SKIN — WARPED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND CENTER FUSELAGE SKIN WARPED FS 697-737, RBL 60, WL 140-180. REPLACED RT FUSELAGE SKIN FS 697-737E IAW SRM SMP 583 51-60 & 51-70. NR 2020.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND FS 476 AERODYNAMIC FAIRINGS CRACKED AT LBL 30 AND RBL 30, WL 283. REPAIRED IAW SRM SMP 583 51-140-12. NR 2060.

Part: FASTENER — LOOSE · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND LOOSE FASTENERS FS 345E-245 FUSELAGE SKIN, LBL 30, WL 230-285. REPLACED 60 EA RIVETS IAW AC 43.13-1B AND SB 382-53-42. NR 2067.

Part: RING — CORRODED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND LT CENTER FUSELAGE RING SEGMENT CORRODED AND CRACKED AT FS 762E, 767E AND 772E, LBL 60, WL 142-148. REPAIRED IAW SRM SMP 583 51-140-23. NR 2240.

Part: FLOORBEAM — SCHEDULED MAINT (FS 737E-817E) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND RT CENTER FUSELAGE FS 737E-817E CHINE ANGLE WITH NUMEROUS REPAIRS, RBL 61, WL 142. REPLACED CHINE ANGLE FS 737E-817E IAW SRM SMP 583 51-60 & 51-70.

Part: REPAIR — NONE · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 NOTED LT AILERON UPPER SURFACE NON-FLUSH REPAIR AT AS 40-55. REPLACED AILERON UPPER SURFACE SKIN IAW SRM SMP 583 51-60 & 51-70.

Part: REPAIR — NONE (RT ELEVATOR) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5511 NOTED RT ELEVATOR NON-FLUSH REPAIR AT HSS 164. REPAIRED IAW SRM SMP 583 51-140-10.

Part: SKIN — LOOSE (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND LOOSE FASTENERS FS 245-245E FUSELAGE SKIN, LBL 60-RBL 60, WL 230. REPLACED 400 EA RIVETS IAW AC 43.13-1B AND SB 382-53-42. NR 2068.

Part: REPAIR — NONE (FS 528-577) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC3213 NOTED LMLG WHEEL WELL BULKHEAD WEB PREVIOUS REPAIR IN WEB AREA OF FS 528 - 577, WL 142 - 150, LBL 62. SCHEDULE REPLACEMENT TO ELIMINATE REPAIR. REPLACED WEB FS 528 - 577 IAW SRM SMP 583 51-60 & 51-70.

Part: SKIN — CANNING (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND AFT FUSELAGE SKIN WARPED AND OIL CANNED FS 737E-777E, LBL 60, WL 147-200. REPLACED LT AFT FUSELAGE SKIN FS 737E-777E IAW SRM SMP 583 51-60 & 51-70. NR 2021.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND LT AFT FUSELAGE SKIN WRINKLED FS 737-814, LBL 60, WL 142-170. REPLACED FUSELAGE SKIN FS 737-814 IAW SRM SMP 583 51-60 & 51-70. NR 2075.

Part: BEAM — CORRODED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND LT MLG FS 517 VERTICAL BEAM CORRODED AT TRACK ATTACHMENT, LBL 60, WL 151 & 185. REPAIRED IAW LAC MEA 382-25-03-074 R1. NR 2225.

Part: SKIN — WRINKLED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND LT CENTER FUSELAGE SKIN WRINKLED FS 737E-777E, LBL 60, WL 142-175. REPLACED FUSELAGE SKIN FS 737E-777E IAW SRM SMP 583 51-60 & 51-70. NR 2074.

Part: PLATE — GOUGED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND FLOOR END SCUFF PLATE GOUGED AT FS 817E, WL 146, LBL 60 - RBL 60. REPLACED SCUFF PLATE IAW SMP 583 51-60 & 51-70. NR 2243.

Part: FLOORBEAM — MISDRILLED (FS 517-597) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION CARRY OVER NR 0220 DUE FOR ACCOMPLISHMENT - LT CHINE CAP MISDRILLED HOLES FS 557, LBL, 61, WL 146. REPLACED LT CHINE CAP FS 517- 597 IAW SRM SMP 583 51-60 & 51-70.

Part: FLOORBEAM — SCHEDULED MAINT (FS 737E-817E) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION PER JOBCARD HC5321 FOUND LT CENTER FUSELAGE FS 737E-817E CHINE ANGLE WITH NUMEROUS REPAIRS, LBL 61, WL 142. REPLACED CHINE ANGLE FS 737E-817E IAW SRM SMP 583 51-60 & 51-70.

Part: SKIN — WARPED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND CENTER FUSELAGE SKIN WARPED FS 697-737E, LBL 60, WL 142-185. REPLACED LT FUSELAGE SKIN FS 697-737E IAW SRM SMP 583 51-60 & 51-70. NR 2039.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION FOUND RT MLG FS 477 INTERCOSTAL BEAM INBOARD AND OUTBOARD CAPS CRACKED AT RBL 63, WL 200. REPLACED BEAM IAW SRM SMP 583 51-60 & 51-70. NR 2141.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 48,895 hrs · 31,021 cycles

DURING SCHEDULED C4 INSPECTION, FOUND LT CENTER FUSELAGE SKIN SCRATCHED FS 777E-817E, LBL 60, WL 142-170. REPLACED FUSELAGE SKIN FS 777E-817E IAW SRM SMP 583 51-60 & 51-70. NR 2073.

Part: SPLICE — CRACKED (BULKHEAD) · airframe 48,249 hrs · 30,730 cycles

DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND LT MLG WW FS 617 AFT BULKHEAD LOWER PANEL SPLICE CRACKED AT OUTBD END, LBL 80, WL 150. REPLACED LOWER SPLICE IAW LOCKHEED DWG 339149. NR 0031.

Part: STRUT — BROKEN (FS 858) · airframe 47,888 hrs · 30,621 cycles

DURING SCHEDULED A CHECK INSPECTION PER JOB CARD HA1200 FOUND LH FS 858 STRUT CRACKED AND BROKEN AT LBL 61, WL 190. INSPECTED FOR SECONDARY DAMAGE, NONE NOTED. AIRCRAFT FERRIED UNPRESSURIZED TO EGSC FOR REPAIR.AT EGSC REPAIRED STRUT IAW SRM SMP 583 53-50-25. MARSHALL NR 0001.

Part: SKIN PANEL — CRACKED (FS 617) · airframe 47,625 hrs · 30,533 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB3202 FOUND RMLG WHEEL WELL FS 617 AFT BULKHEAD SKIN CRACKED .5 IN. AT CENTER OF PANEL RBL 69, WL 184.REPLACED SKIN PANEL IAW SRM SMP 583 53-40-02 AND DWG 339149. NR 0040.

Part: DOUBLER — MISSING (FS 902) · airframe 47,625 hrs · 30,533 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0504 FOUND PREVIOUS FRAME REPAIR REQUIRING REWORK TO CONFORM TO SRM SMP 583 53-50-17, DUE 1 EA. MISSING DOUBLER FS 902, LBL 62, WL 200. CAUSE LIKELY MISINTERPRETATION AND APPLICATION OF 53-50-16 REPAIR - NO OUTBD DOUBLER REQUIRED.INSTALLED DOUBLER ON OUTBOARD SURFACE OF INNER TEE IAW SRM SMP 583 53-50-17. NR 0071.

Part: ANGLE — CRACKED (FS617) · airframe 47,043 hrs · 30,839 cycles

DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND RH MLG BAY AFT PRESSURE BULKHEAD PANEL SLICE ANGLE CRACKED. FS617, RBL60, WL170.REPLACED ANGLE IAW SRM SMP 583 51-70 AND DWG 339149. NR0067.

Part: RISER — CRACKED (FS517) · airframe 47,043 hrs · 30,839 cycles

DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND LH MLG BAY SKIN RISER CRACKED ADJACENT TO EXISTING REPAIR. FS517-497, LBL60, WL150-175.REPAIRED SKIN RISER IAW SRM SMP 583 FIG 53-40-02, AND 51-70. NR0059.

Part: TRACK — CRACKED (FS577) · airframe 47,043 hrs · 30,839 cycles

DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND ON REMOVAL OF RH FS577 MLG BEAM, RH AFT FWD MLG TRACK CRACKED AT LOWER NUT HOLE. FS577, RBL60, WL160.REPLACED RH AFT MLG TRACKS IAW SRM SMP 51-70 AND DWG 388997. NR0098.

Part: TRACK — WORN (FS159) · airframe 47,043 hrs · 30,839 cycles

DURING SCHEDULED B1 INSPECTION PER HB0509 FOUND FLIGHT ENGINEERS SEAT TRACKS WORN. FS159, BL0, WL200.REPLACED TRACKS IAW SRM SMP 583-51-60-00, DWGS 371094, AND 371095. NR0047.

Part: BEAM — CORRODED (FS577) · airframe 47,043 hrs · 30,839 cycles

DURING SCHEDULED B1 INSPECTION PER HB0506 FOUND RH MLG BAY TRACK SUPPORT BEAM CORRODED. FS577, RBL60, WL160.REPLACED BEAM AND CAP IAW SRM SMP 583 51-70 AND DWG 388482. NR0065.

Part: FITTING — CRACKED (FS 557) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG FS 557 LOWER BOW BEAM FITTING CRACKED AT RBL 63, WL 150.REPLACED FITTING IAW SRM SMP 583 51-70. NR 0076.

Part: BEAM — CRACKED (FS 528) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG BAY FS 528 SUPPORT BEAM CRACKED FROM UPPER ATTACHMENT BOLT HOLE AT LBL 64, WL 250.REPAIRED IAW LAC MEA 382-53-02-030. NR 0289.

Part: FITTING — MISALIGNED (FS 557) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION LH FS 557 FLOOR END FITTING REPLACEMENT FOUND NEW FITTING PILOT HOLES NOT ALIGNED WITH STRUCTURE.REWORKED FITTING IAW LAC MEA 382-53-02-035. NR 0375.

Part: SKIN — CORRODED (AS 55) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND LH AILERON UPPER SKIN CORRODED AT AS 55, FS 595.REPAIRED SKIN IAW SRM SMP 583 51-140-10. NR 0139.

Part: BEAM — CRACKED (FUSELAGE) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION FOUND LT FS 557 LOWER BOW BEAM CRACKED AT LOWER END AT LBL 63, WL 146. REPAIRED IAW LAC MEA 382-53-02-034.

Part: STIFFENER — CRACKED (FS 600) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG WHEEL WELL FS 600 WALL SKIN RISER CRACKED AT RBL 62, WL 163.REPAIRED IAW SRM SMP 583 53-40-10. NR 0023.

Part: STIFFENER — CRACKED (OWS 241) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC2704 FOUND RH OWS 241 FLAP TRACK STIFFENER CRACKED.REPLACED STIFFENER IAW SRM SMP 583 57-50-03. NR 0106.

Part: FITTING — CRACKED (FS 497) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5369 FOUND LH FS 497 UPPER BOW BEAM FITTING CRACKED AT LBL 63, WL 258.REPAIRED IAW SRM SMP 583 51-70 AND DWG 341973. NR 0037.

Part: FITTING — CRACKED (FS 557) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG FS 557 LOWER BOW BEAM FITTING CRACKED AT LBL 63, WL 150.REPLACED FITTING IAW SRM SMP 583 51-70. NR 0075.

Part: ANGLE — CRACKED (FS 946) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC05297 FOUND FS 946 FRAME UPPER BEAM CAP ANGLE CRACKED AT RBL 14, WL 285.REPAIRED IAW SRM SMP 583 51-140-23. NR 0250.

Part: FITTING — CRACKED (FS 497) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3209 FOUND RMLG FS 497 LOWER BOW BEAM FITTING CRACKED AT RBL 63, WL 150.REPLACED FITTING IAW SRM SMP 583 51-70. NR 0077.

Part: DOUBLER — CUT (FS 573-597) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION CUT EXISITING FS 573 - 597 SKIN DOUBLER AT LBL 62, WL 144 TO PROVIDE ACCESS FOR CHINE ANGLE REPLACEMENT (NR 0033).REPAIRED IAW LAC MEA 382-53-02-032. NR 0070.

Part: FITTING — CRACKED (FS 497) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HSP5369 FOUND RH FS 497 UPPER BOW BEAM FITTING CRACKED AT RBL 63, WL 258.REPAIRED IAW SRM SMP 583 51-70 AND DWG 341973. NR 0038.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION FOUND LBL 62 CHINE ANGLE CRACKED AT FS 573 TO 597, WL 144. REPLACED CHINE ANGLE IAW SRM SMP 583 51-70 AND DWG 386681.

Part: BEAM — CRACKED (FUSELAGE) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION FOUND LT FS 557 UPPER BOW BEAM LOWER END CRACKED AND EXISTING REPAIR NOT PER SRM AT LBL 63, WL 150. REPAIRED IAW SRM SMP 583 53-40-14.

Part: FITTING — CRACKED (FS 497) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG FS 497 LOWER BOW BEAM FITTING CRACKED AT LBL 63, WL 150.REPLACED FITTING IAW SRM SMP 583 51-70. NR 0073.

Part: FITTING — CRACKED (FS 537) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3208 FOUND LMLG FS 537 LOWER BOW BEAM FITTING CRACKED AT LBL 63, WL 150.REPLACED FITTING IAW SRM SMP 583 51-70. NR 0074.

Part: FRAME — CRACKED (FS 140) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION PER JOB CARD HC3207 FOUND FS 140 BATTERY BAY SUPPORT FRAME CRACKED ADJACENT TO LOWER CORNER AT LBL 46, WL 158.REPAIRED IAW SRM SMP 583 51-140-19. NR 0041.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 46,439 hrs · 30,207 cycles

DURING SCHEDULED C3 INSPECTION FOUND RBL 62 CHINE ANGLE CRACKED AT FS 588 TO 597, WL 144. REPLACED CHINE ANGLE IAW SRM SMP 583 51-70 AND DWG 386681.

Part: HORN — CRACKED (ELEVATOR TAB) · airframe 45,831 hrs · 30,084 cycles

DURING SCHEDULED B3 INSPECTION, FOUND LT ELEVATOR TRIM TAB INBOARD AFT HORN BRACKET CRACKED AT HSS 99, FS 1153, WL 277. REPLACED HORN ASSY IAW SMP 581 91-00. OPERATIONAL CHECK AND RIGGING COMPLIED WITH IAW SMP 581 27-31 PG 218 AND 201.

Part: STUD — LOOSE (NR. 3 PUMP HSG) · airframe 45,401 hrs · 29,927 cycles

AFTER TAKEOFF FROM DNA, FLIGHT CREW NOTED NR. 3 PROP LOW OIL LIGHT ON. RPM INCREASED TO 106%. SHUTDOWN ACCOMPLISHED IAW QRH. CONTINUED TO OKO AND LANDED WITHOUT INCIDENT.FOUND NR. 3 PROPELLER 1 EA. VALVE HOUSING HOLD DOWN STUD LOOSE IN PUMP HOUSING CAUSING FLUID LOSS. REPLACED STUD IAW HAMILTON SUNSTRAND P5606 CH 3, 2-7, HN61135 AND HN7101.

Part: WEB — CRACKED (FS 924) · airframe 45,223 hrs · 29,869 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0505 FOUND RH FS 924 BULKHEAD WEB CRACKED AT RBL 60, WL 250.REPAIRED IAW SRM SMP 51-140-17. NR 2009.

Part: WEB — CRACKED (FS 902) · airframe 45,223 hrs · 29,869 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HB0505 FOUND LH FS 902 BULKHEAD WEB CRACKED AT LBL 60, WL 238.REPAIRED IAW SRM SMP 51-140-17. NR 2023.

Part: PANEL — CORRODED (RH CWS 202-207) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION SCHEDULED REPAIR FOR TIME LIMITED LMAS ENGINEERING DISPOSITON FOR RH CENTER WING LOWER SURFACE, AFT PANEL CORROSION BLENDOUT AT CWS 202-207, FS 575-590.ACCOMPLISHED REPAIR IAW LAC MEA 382-57-01-032. NR 2001.

Part: FRAME — ELONGATED (FS 677 & 807E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 677 AND 807E LOWER RING SEGMENTS WITH ELONGATED HOLES AT LBL 64, WL 151.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166.

Part: FLOOR PANEL — WARPED (FS 245-345E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 245 - 345E RH FLOOR PANEL WARPED AND CORRODED AT LBL 16 - 42, WL 146.REPLACED FLOOR PANEL IAW SRM SMP 583-53-40-05. NR 2143.

Part: FRAME — CRACKED (FS 277) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 277 LH RING SEGMENT CRACKED AT LBL 63, WL 146.REPAIRED IAW SRM SMP 583-51-140-21. NR 2083.

Part: CAP — CRACKED (FS 537) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC3209 FOUND LH FS 537 BOW BEAM CAP CRACKED AT LBL 61, WL 206.REPAIRED IAW SRM SMP 583-53-40-14. NR 2134.

Part: BEAM — CRACKED (FS 577-597) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC3209 FOUND FS 577 - 597 RMLG UPPER WHEEL WELL BEAM CRACKED AT RBL 70 , WL 236.REPLACED BEAM IAW SRM SMP 583 57-20-02 (12). NR 2007.

Part: SKIN — DENTED (FS 777E-817E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND FS 777E -817E BELLY SKIN DENTED AND SCRATCHED LBL 61 TO RBL 61.REPLACED BELLY SKIN IAW SRM SMP 583-53-10 PG 2. NR 2055.

Part: FRAME — ELONGATED (FS 757E-801E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 757E,777E, 797E & 801E LOWER RING SEGMENTS WITH ELONGATED HOLES AT RBL 64, WL 154.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166.

Part: FRAME — CRACKED (FS 970) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HSP5330 FOUND FS 970 LH UPPER RING SEGMENT CRACKED AT LBL 61, WL 256.REPAIRED IAW SRM SMP 583-51-140-19. NR 2077.

Part: FRAME — MISDRILLED (FS 336-807E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 336, 702, 707, 711, 716, 722, 727, 732, 737, 757E, 777E, 781E, 797E, 801E AND 807E LOWER RING SEGMENTS WITH MISDRILLED HOLES AT RBL 64, WL 152.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166.

Part: FLOOR PANEL — WARPED (FS 737E-817E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 737E - 817E CENTER FLOOR PANEL WARPED AND CORRODED AT BL 0, WL 146.REPLACED FLOOR PANEL IAW SRM SMP 583-53-40-05. NR 2121.

Part: SKIN — DENTED (FS 777E-817E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND LH FS 777E - 817E FUSELAGE SKIN DENTED IN SEVERAL LOCATIONS LBL 65, WL 146 - 160.REPAIRED IAW LAC MEA 382-53-01-046. NR 2174.

Part: SKIN — DENTED (FS 697-737) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND FS 697 - 737 BELLY SKIN WITH SEVERAL DENTS AT LBL 61 TO RBL 61.REPLACED BELLY SKIN IAW SRM SMP 583-53-10 PG 4. NR 2056.

Part: SKIN — CRACKED (FS 869-1001) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND LH FS 869 - 1001 FUSELAGE SKIN CRACKED AT LBL 61, WL 194-270 AND HIGH DENSITY OF PREVIOUS REPAIRS.REPAIRED IAW LAC MEA 382-53-01-047. NR 2051.

Part: SKIN — DENTED (FS 737E-817E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND RH FS 737E - 817E FUSELAGE SKIN DENTED IN SEVERAL LOCATIONS RBL 65, WL 146 - 166REPAIRED IAW LAC MEA 382-53-01-045. NR 2173.

Part: FLOOR PANEL — WARPED (FS 245-345E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND FS 245 - 345E RH FLOOR PANEL WARPED AND CORRODED AT RBL 16 - 52, WL 146.REPLACED FLOOR PANEL IAW SRM SMP 583-53-40-05. NR 2119.

Part: SKIN — GOUGED (FS 840) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC05297 FOUND LH FS 840 RAMP ACTUATOR CUTOUT AREA GOUGED AT LBL 63, WL 180.REPAIRED IAW LAC MEA 382-53-01-034 NR 2133.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION PER JOB CARD HC5303 FOUND RT FS 869 - 935 FUSELAGE SKIN WITH A HIGH DENSITY OF PREVIOUS REPAIRS AT RBL 61, WL 194-254. REPAIRED IAW LAC MEA 382-53-01-048.

Part: FRAME — ELONGATED (FS 762E-772E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 762E, 767E AND 772E LOWER RING SEGMENTS WITH ELONGATED HOLES AT LBL 64, WL 154.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166.

Part: FRAME — ELONGATED (FS 277 & 317) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 277 AND FS 317 LOWER RING SEGMENTS WITH ELONGATED HOLES AT LBL 64, WL 152.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166.

Part: FRAME — MISDRILLED (FS 341E-807E) · airframe 44,117 hrs · 29,359 cycles

DURING SCHEDULED C2 INSPECTION NR 2098 ACCOMLISHMENT (CURB PANEL REPLACEMENT) FOUND FS 341E, 677, 762E, 767E, 772E & 807E LOWER RING SEGMENTS WITH MISDRILLED HOLES AT LBL 64, WL 152.REPAIRED IAW LAC MEA 382-53-01-052. NR 2166.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 43,531 hrs · 28,933 cycles

DURING SCHEDULED B3 CHECK PER JOB CARD HB0506, FOUND FS 608 LT WW BULKHEAD CRACKED AT RBL 62, WL 192 INSULATION MOUNT STUD. REPAIRED IAW SRM SMP 583-53-40-10.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,531 hrs · 28,933 cycles

DURING SCHEDULED B3 CHECK PER JOB CARD HB0505, FOUND FS 902 RT WEB CRACKED AT RBL 62, WL 220. REPAIRED IAW SRM SMP 583-51-140-17.

Part: RETAINER — CRACKED (FUSELAGE) · airframe 43,531 hrs · 28,933 cycles

DURING SCHEDULED B3 CHECK PER JOB CARD HB0505, FOUND FS 838 SEAL RETAINER BENT AND CRACKED AT RLB 62, WL 160. REPAIRED IAW SRM SMP 583-51-140-19.

Part: BRACKET — OUT OF ADJ (NR 2 ENGINE) · airframe 43,476 hrs · 28,916 cycles

NR 2 PROP FLUCUATING OUT OF LIMITS. ENGINE SHUTDOWN ON SHORT FINAL. RPM FLUCTUATING +/- 1 PERCENT. DATE: 2FEB01 TIME: 1047Z. ADJUSTED NR 2 NTS BRACKET IAW HAM STD MM P5059 PARA 4-1, PG I-405 AND I-406.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 43,148 hrs · 28,790 cycles

DURING SCHEDULED A-CHECK INSPECTION PER JOB CARD HA1200, FOUND FS 561.75 LT MLG WHEEL WELL PRESSURE BULKHEAD WEB CRACKED 3.625 INCH AT LBL 61, WL 175. REPAIRED PER SRM SMP 583-53-40-09.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 43,006 hrs · 28,744 cycles

DURING SCHEDULED B-CHECK, THE AUX LONGERON AT RT BL 76 WL 175 FS 773 WAS DISCOVERED CRACKED 2.0 INCHES. REPAIRED PER MEA 382-53-00-119 AND LYNDEN DRAWING R00-0024-2.

Part: CAP — CRACKED (BULKHEAD) · airframe 43,006 hrs · 28,744 cycles

DURING SCHEDULED B-CHECK, THE RT FS 1012 BULKHEAD CAP WAS DISCOVERED CRACKED 6.0 INCHES IN LENGTH. REPAIRED PER MEA 382-53-00-121 R1 AND LYNDEN DRAWING R00-0024-4 REV A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,006 hrs · 28,744 cycles

DURING SCHEDULED B-CHECK, A 2.5 INCH CRACK WAS DISCOVERED IN THE FS 968 OVERHEAD FORMER DOUBLER. REPAIRED FRAME CRACK PER MEA 382-53-00-120, SMP 583-50-06 AND LYNDEN DRAWING R00-0024-3.

Part: LONGERON — CRACKED (HORIZONTAL STAB) · airframe 43,006 hrs · 28,744 cycles

DURING SCHEDULED B-CHECK, THE DORSAL FIN ATTACH ANGLE WAS DISCOVERED CRACKED IN THE RADIUS AT FS 902 LBL 13 WL 285. REPAIRED PER MEA 382-53-00-115 AND LYNDEN DRAWING R00-0024-1.

Part: RISER — CRACKED (RT MLG WW) · airframe 43,006 hrs · 28,744 cycles

DURING SCHEDULED B-2 INSPECTION PER JOB CARD HB0506, FOUND FS 607 RT MLG WHEEL WELL BULKHEAD EXTRUDED RISER CRACKED AT RBL 62, WL 166. REPAIRED PER SRM SMP 583-53-40-10. NR 21618.

Part: CAP — CRACKED (CARGO DOOR) · airframe 42,902 hrs · 28,708 cycles

DURING CRUISE AT FL 200 FLIGHT CREW REPORTED UNUSUAL SOUND FOLLOWED BY CABIN PRESSURE LOSS WITHIN 3O SECONDS. MAINTAINED ALTITUDE, UTILIZED CREW OXYGEN SYSTEM AND INSPECTED AIRCRAFT INTERIOR. NO DEFECTS NOTED. DESCENDED TO FL 100, RETURNED TO NSY PRECAUTIONARY AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED CARGO DOOR LBL 61 SIDE BEAM LOWER CAP CRACKED 60.0 INCHES AT FS 946. A/C FERRIED UNPRESSURIZED TO CBG FOR REPAIR. REPLACED CARGO DOOR PER SMP 581 52-30 PG 238-248.

Part: STRUT — CRACKED (FUSELAGE) · airframe 42,622 hrs · 28,604 cycles

DURING SCHEDULED A-CHECK PER JOB CARD HA1200, FOUND FS 858 RT TUBE STRUT (STANCHION) CRACKED AT BASE FITTING ATTACH. REPLACED TUBE STRUT IAW SRM SMP 583-53-50, PG 38, FIGURE 53-50-25.

Part: MANIFOLD — CRACKED (RT MLG WHEEL) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0506, FOUND RT MLG WHEEL WELL 3 HEAT TRANSFER MANIFOLDS CRACKED AT FS 535, 540 AND 565, WL 145, RBL 61. REPAIRED PER DWG 339482. NR 39922.

Part: BEAM — CRACKED (FUSELAGE) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0506, FOUND RT MLG WHEEL WELL FS 557 BOW BEAM CRACKED AT WL 159. REPLACED BEAM CAP AND WEB PER SRM SMP 583-51-70. NR 39286.

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0505, FOUND CREW DOOR EXTERNAL DOUBLER CRACKED AT FS 207, WL 195. REPLACED DOUBLER PER SRM SMP 583-53-30-30. NR 31571.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0502, FOUND RT FS 902 DORSAL FIN ATTACH ANGLE CRACKED IN RADIUS AT RBL 13, WL 285. REPAIRED PER LAC MEA 382-53-00-089. NR 44276.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0502, FOUND LT FS 840 DORSAL FIN ATTACH ANGLE CRACKED APPROX 1 INCH IN RADIUS, RBL 15, WL 280. REPAIRED PER LAC MEA 382-53-00-088. NR 39925.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0505, FOUND FS 836 RING SEGMENT CRACKED AT WL 277, RBL 18. REPAIRED PER SRM SMP 583-53-50-06. NR 39950.

Part: ATTACH ANGLE — CRACKED (DORSAL FIN) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0502, FOUND RT FS 840 DORSAL FIN ATTACH ANGLE CRACKED APPROX 2 INCHES IN RADIUS, RBL 15, WL 280. REPAIRED PER LAC MEA 382-53-00-087. NR 39912.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,546 hrs · 28,576 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB0506, FOUND LT MLG WHEEL WELL FS 458 MAIN BEAM INTERCOSTAL CRACKED AT WL 200, LBL 61. REPAIRED PER SRM SMP 583-53-40-36. NR 44243.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,236 hrs · 28,333 cycles

DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND FS 792 RT LOWER RAMP SUPPORT TEE FITTING CRACKED. REPLACED FITTING IAW SRM SMP 583-53-10-00 D&C 10.

Part: STIFFENER — CRACKED (TE FLAP TRACK) · airframe 42,183 hrs · 28,285 cycles

DURING SCHEDULED A-CHECK PER HA1200, FOUND LT OWS 28 FLAP TRACK RIB STIFFENER FITTING CRACKED AND BROKEN AT LOWER FLANGE.REPLACED FITTING IAW SRM SMP 583-57-10 (3) AND LAC MEA 382-57-00-072. D&C 1.

Part: BRACE — CRACKED (FUSELAGE) · airframe 42,107 hrs · 28,212 cycles

DURING SCHEDULED A-CHECK PER HA1200, FOUND FS 547 RT MLG FAIRING SUPPORT BRACE CRACKED AT WL 200. REPLACED BRACE IAW LAC MEA 382-53-00-071 AND SRM SMP 583-51-10, PG 4, PARA G, D & C 1.

Part: SKIN — GOUGED (FUSELAGE) · airframe 42,013 hrs · 28,133 cycles

DURING SCHEDULED A CHECK PER HA1200, FOUND FS 777 SKIN GOUGED AT RBL 57, WL 142. REPAIRED IAW SRM SMP 583-51-140-12. D&C 6.

Part: SKIN — GOUGED (FUSELAGE) · airframe 42,013 hrs · 28,133 cycles

DURING SCHEDULED -A- CHECK PER HA1200. FOUND LT FS 748 SKIN GOUGED AT WL 146. REPAIRED IAW SRM SMP 583-51-00-02 AND 51-140-12 FOR TEMP REPAIR. ENTERED IN C/O008. D&C 4.

Part: DOOR — BENT (NLG) · airframe 41,983 hrs · 28,116 cycles

DURING SCHEDULED A CHECK PER HA1200, FOUND AFT NLG DOOR TRAILING EDGE SKIN BENT AND TORN. REPAIRED IAW LAC MEA 382-53-00-039. D&C 2.

Part: SKIN — TORN (FUSELAGE) · airframe 41,983 hrs · 28,116 cycles

DURING SCHEDULED A CHECK PER HA1200, FOUND FS 196 FUSELAGE SKIN BENT AND TORN BY NLG AFT DOOR AT RBL 9 TO 13. REPAIRED IAW SRM SMP 583-51-140-12 AND 51-70-22E. LAC MEA 382-53-00-040. D&C 8.

Part: PLATE — CRACKED (FUSELAGE) · airframe 41,950 hrs · 28,105 cycles

DURING SCHEDULED C1 INSPECTION ACCOMPLISHED SCHEDULED REPLACEMENT OF TIME LIMITED FS 766.75 TEMP REPAIR OF CHINE PLATE. REPLACED FS 737 TO 817 RT AFT CHINE PLATE IAW LAC MEA 382-53-00-035 AND SRM SMP 583-51-10 PG 4, PARA G. DRC 2003.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 41,950 hrs · 28,105 cycles

DURING SCHEDULED C1 INSPECTION PER JOB CARD HSP57110, FOUND FS 844 RT DORSAL FIN LONGERON CRACKED (INTERNAL). REPAIRED IAW SRM SMP 583-51-140-23. DRC 2016.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,950 hrs · 28,105 cycles

DURING SCHEDULED C1 INSPECTION PER JOB CARD HSP53121, FOUND LT FS 577 CARGO FLOOR BULKHEAD END FITTING CRACKED AT LBL 59. REPLACED END FITTING IAW LAC MEA 382-53-00-028 AND SRM SMP 583-51-10 PG 4, PARA G. DRC 2063 AND 2064.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,950 hrs · 28,105 cycles

DURING SCHEDULED C1 INSPECTION PER JOB CARD HSP53121, FOUND RT FS 577 CARGO FLOOR BULKHEAD END FITTING CRACKED AT RBL 59. REPLACED END FITTING IAW LAC MEA 382-53-00-028 AND SRM SMP 583-51-10 PG 4, PARA G. DRC 2066 AND 2067.

Part: CLAMP — LOOSE (BS 467)

CARGO COMPARTMENT AIR CONDITIONING OVERHEAT LIGHT CAME ON IN-FLIGHT. SHUTDOWN CARGO COMPARTMENT AIR CONDITIONING SYSTEM IAW AFM EMERGENCY PROCEDURES AND ISOLATED WING. DEFERRED CARGO COMPARTMENT AIR CONDITIONING SYSTEM PER MEL 21-1, DMI LOG NR 00082. SPECIAL PROCEDURE NR 1 C/W, CARGO COMPARTMENT FLOW CONTROL AND SHUT OFF VALVE SECURED CLOSED IAW SMP 581 21A-50, PG 208. CLEARED DMI 00082 5/4/99, TAT: 39998. TIGHTENED CLAMPS NEAR TURBINE BYPASS AREA CARGO COMPARTMENT AIR CONDITIONING. LEAK AND OPS CHECK PER SMP 581 21A-50-201.

Part: GUSSET — BROKEN (BS 858)

DURING ACCESS FOR FS 858 STRUT REPLACEMENT, FOUND FS 858 UPPER GUSSET BROKEN AT UPPER STRUT ATTACH BOLT HOLE, WL 256, RBL 61. REPLACED GUSSET IAW SMP 583 51-10, PG 4.

Part: STRUT — CRACKED (BS 858)

ON ARRIVAL ANC, FOUND FS 858 STRUT CRACKED AT UPPER GUSSET ATTACH, WL 256, RBL 61. REPLACED STRUT IAW SMP 583 51-10, PG 4.

Part: SUPPORT — CORRODED (BS 657)

DURING C CHECK/BRIDGING INSPECTION, FOUND FS 657 FLOOR SUPPORT UPPER CAP CORRODED AT BL 20R. REPAIRED BY FILLER AND REPAIR ANGLES IAW SPAR MPP L100-404-99-019, DWG R99-0002-10. LAC MEA 382-53-99-020.

Part: CAP — CORRODED (BS 357-517)

DURING C CHECK/BRIDGING INSPECTION - PER HC05297, FOUND RT CHINE CAP CORRODED AND CRACKED IN 10K TIE DOWN WELLS, FS 357 TO 517. REPLACED CHINE CAP PER SMP 538 51-70 AND DWG 372349.

Part: CAP — CORRODED (BS 760-844)

DURING C CHECK/BRIDGING INSPECTION - PER HC05297, FOUND RAMP RT CHINE CAP CORRODED AND CRACKED. REPLACED CHINE CAP IAW SMP 583 52-60 AND DWG 354104.

Part: TRUNNION — CRACKED (NLG)

DURING C CHECK/BRIDGING INSPECTION - PER HSP5368, FOUND LT NOSE GEAR TRUNNION CRACKED. REPLACED LT NOSE GEAR TRUNNION IAW SMP 581-53-40 AND DWG 360587.

Part: PANEL — CORRODED (BS 617)

DURING C-CHECK/BRIDGING INSPECTION, FOUND FS 617 AFT RT CENTER WING PRESSURE PANEL CORRODED. REPAIRED BY CORROSION BLEND OUT AND DOUBLER INSTALLATION PER SPAR MPP L100-404-99-056. LAC MEA 382-57-99-054.

Part: SPAR CAP — CORRODED (CENTER WING)

DURING C-CHECK/BRIDGING INSPECTION, FOUND CENTER WING, REAR BEAM, UPPER CAP CORRODED AT RBL 57 TO 62. REPAIRED WITH FILLER AND DOUBLER INSTALL IAW SPAR MPP L100-404-99-060. LAC MEA 382-53-9-058.

Part: WEB — CRACKED (VERT STAB)

DURING C CHECK/BRIDGING INSPECTION, FOUND FS 1095 VERTICAL STABILIZER WEB CRACKED FROM VSS 9 TO 12. REPAIRED BY DOUBLER INSTALL IAW SPAR MPP L100-404-99-061, DWG R99-0002-08. LAC MEA 382-53-99-027.

Part: SKIN — MISDRILLED (BS 777)

DURING C-CHECK/BRIDGING INSPECTION, FOUND 2 MISDRILLED HOLES AT FS 777.0E FUSELAGE SKIN. REPAIRED BY INSTALLING DOUBLERS IAW SPAR MPP L100-404-99-057, DWG R99-0002-03. LAC MEA 382-53-99-055.

Part: CAP — CORRODED (BS 245-345)

DURING C CHECK/BRIDGING INSPECTION PER HC05397, FOUND LT FWD CHINE CAP CORRODED FS 245 TO 345E. REPLACED LT FWD CHINE CAP IAW SMP 583 AND DWG 3305020. NR 188.

Part: FRAME — CRACKED (BS 817)

DURING C CHECK/BRIDGING INSPECTION, FOUND FS 817E LT LOWER RING SEGMENT CRACKED AT WL 156. REPAIRED IAW SMP 583 53-40-38, 39.

Part: PANEL — MISDRILLED (BS 497-517)

DURING C CHECK/BRIDGING INSPECTION, FOUND NEW REPLACEMENT FS 497 TO 517 RT FWD PRESSURE PANEL WITH MISDRILLED HOLES, BELOW MINIMUM EDGE DISTANCE. REPAIRED BY TRIMMING OUT DAMAGED AREA AND INSTALLING REPAIR DOUBLER IAW SPAR MPP L100-404-9-069. LAC MEA 382-57-99-79.

Part: PANEL — DAMAGED (BS 477)

DURING C CHECK/BRIDGING INSPECTION, FOUND NEW REPLACEMENT FS 477 RT FWD PRESSURE PANEL SUB STRUCTURE ATTACH REQUIRES INSTALLATION OF HL37PB6 PINS AND KFN542-3 COLLARS IN LIEU OF STANDARD MS90353-06 BLIND BOLTS DUE PANEL PRELOAD. INSTALLED PINS AND COLLARS IAW SPAR MPP L100-404-99-071. LAC MEA 382-57-99-80.

Part: FITTING — CRACKED (BS 617)

DURING C CHECK/BRIDGING INSPECTION PER HSP53262, FOUND FS 617 LT AFT END FITTING CRACKED AT WL 145, LBL 61. REPAIRED PER SMP 583 53-40-40.

Part: CAP — BENT (CARGO DOOR)

DURING C CHECK/BRIDGING INSPECTION - PER HSP53131, FOUND RAMP BEAM CAP BENT AT RAMP STA 10. REPLACED BEAM CAP IAW SMP 583 AND DWG 353608.

Part: ANGLE — CRACKED (BS 574.7-576)

DURING C-CHECK/BRIDGING INSPECTION, FOUND LT CHINE ANGLE, CENTER FUSELAGE CRACKED AT FS 574.7 TO 576, RBL 61.6, WL 143. REPAIRED BY STOP DRILLING CRACK AND INSTALLING REPAIR ANGLE AND FILLER IAW SPAR MPP L100-404-99-059. LAC MEA 382-53-99-057.

Part: CAP — CORRODED (BS 760-844)

DURING C CHECK/BRIDGING INSPECTION - PER HC05297, FOUND RAMP LT CHINE CAP CORRODED AND CRACKED. REPLACED CHINE CAP IAW SMP 583-52-60 AND DWG 354104.

Part: CAP — CORRODED (BS 357-517)

DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND FS 357 TO 517 LT CHINE CAP CORRODED. REPLACED CHINE CAP IAW SMP 583 52-60 AND DWG 372342. NR 190.

Part: CAP — CORRODED (BS 597-737)

DURING C CHECK/BRIDGING INSPECTION PER HC 0529,7 FOUND TH AFT FS 597 TO 737 CHINE CAP CORRODED. REPLACED CHINE CAP PER SMP 583 53-40-01. NR 189.

Part: SPLICE — CRACKED (BS 766.75)

DURING C-CHECK/BRIDGING INSPECTION, FOUND FS 737E TO 817E RT AFT CHINE PLATE SPLICE CRACKED. ACCOMPLISHED TEMPORARY REPAIR BY STOP DRILLING CHINE ANGLE CRACK AND INSTALLING NEW REPAIR ANGLES IAW SPAR MPP L100-404-99-058, DWG R99-0002-11. LAC MEA 382-53-99-056. CHINE PLATE DUE REPLACEMENT BY 42301.5 TAT.

Part: FRAME — UNSERVICEABLE (BS 817)

DURING C CHECK/BRIDGING INSPECTION, FOUND FS 817E RT LOWER RING SEGMENT PREVIOUS REPAIR AT WL 156 NOT PER SRM. REPAIRED IAW SMP 583 53-40-38, 39.

Part: FRAME — CRACKED (BS 817)

DURING C-CHECK/BRIDGING INSPECTION, FOUND LT LOWER RING SEGMENT CRACKED AT FS 817E, WL 156. REPAIRED RING SEGMENT IAW SMP 583 53-40-38, 39.

Part: FITTING — CRACKED (BS 474)

DURING C CHECK/BRIDGING INSPECTION PER HSP53262, FOUND FS 477 LT FWD END FITTING CRACKED AT WL 145, LBL 61. REPAIRED PER SMP 583 53-40-40. NR 183.

Part: SKIN — WRINKLED (BS 577-617)

DURING C-CHECK/BRIDGING INSPECTION PER HC5303, FOUND FS 577 TO 617 BELLY SKIN WRINKLED BEYOND LIMITS. REPLACED SKIN PANEL IAW SMP 583-40-06.

Part: PANEL — CRACKED (BS 140.5-160)

DURING C CHECK/BRIDGING INSPECTION, FOUND BATTERY COMPARTMENT UPPER PANEL CRACKED AND GOUGED FS 140.5 TO 165. REPAIRED BY FABRICATING AND INSTALLING A REPAIR PANEL IAW SPAR MPP L100-404-99-065. LAC MEA 382-24-99-071.

Part: WEB — BUCKLED (BS 677)

DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUNDFS 677 CARGO FLOOR BULKHEAD WEB BUCKLED, STIFFENER BENT AND CHANNEL CRACKED. REPLACED WEB, STIFFENER AND CHANNEL PER DWG 356245. NR 441.

Part: FITTING — CRACKED (BS 880)

DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 880 BULKHEAD END FITTING CAP CRACKED AT LBL 61. REPLACED CAP IAW SMP 583-51-70 AND DWG 342582. NR 365.

Part: CHANNEL — CRACKED (BS 512.64)

DURING C CHECK BRIDGING INSPECTION, FOUND NR 2 UPPER AFT NACELLE LOWER LT CHANNEL CRACKED AT FS 512.64, PP WL -5.38. REPAIRED BY INSTALLING REPAIR DOUBLER IAW SPAR MPP L100-404-99-004. LAC MEA 382-53-99-006.

Part: ANGLE — CRACKED (BS 597 - 737)

DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND CARGO COMPARTMENT CHINE ANGLE CORRODED AND CRACKED FS 597 TO 737. REPLACED CHINE ANGLE IAW SMP 583 AND DWG 372326. NR 458.

Part: WEB — BUCKLED (BS 657)

DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND FS 657 CARGO FLOOR BULKHEAD WEB BUCKLED AND CHANNEL CRACKED. REPLACED WEB AND CHANNEL IAW DWG 356119. NR 440.

Part: BULKHEAD CAP — MISDRILLED (BS 657)

DURING C CHECK BRIDGING INSPECTION, FOUND 2 EA HOLES MISDRILLED IN FS 657 UNDER FLOOR BULKHEAD LOWER BEAM CAP. REPAIRED BY BUSHING, REPAIR ANGLE, AND DOUBLER INSTALL IAW SPAR MPP L100-404-99-015. LAC MEA 382-53-99-016.

Part: BULKHEAD WEB — CRACKED (BS 477)

DURING C CHECK BRIDGING INSPECTION, FOUND FS 477 RT MLG FWD BULKHEAD ASSY CRACKED AT RISERS WL 230, 234 AND 240. REPLACED BULKHEAD ASSY IAW SPAR MPP L100-404-99-018. LAC MEA 382-53-99-019.

Part: FRAME — CORRODED (BS 297)

DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND FS 297 RT RING SEGMENT CORRODED AT WL 166 TO 190. REPAIRED IAW SMP 583 51-70 AND MPP L100-404-99-005. NR 500.

Part: WEB — BUCKLED (BS 717)

DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND FS 717 CARGO FLOOR BULKHEAD WEB BUCKLED AND CHANNEL BENT. REPLACED WEB AND CHANNEL PER DWG 356250. NR 443.

Part: PRESS PANEL — DENTED (BS 593)

DURING C CHECK/BRIDGING INSPECTION PER HC3208, FOUND RMLG FS 593 SIDE PRESSURE PANEL DENTED BEYOND LIMITS AT WL 150. REPLACED PANEL IAW SMP 583-51-70 AND DWG 3311015. NR 360.

Part: FITTING — CORRODED (BS 697 - 817)

DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND RT LONGERON FITTING CORRODED AND DRILLED FS 697 TO 817. REPLACED FITTING IAW DWG 3305049 AND SMP 583-51-70. NR 393.

Part: FITTING — CRACKED (BS 617 - 717)

DURING C CHECK/BRIDGING INSPECTION PER HSP5297, FOUND FS 617 RT AND FS 717 RT 25K TIE DOWN END FITTINGS CRACKED. REPLACED FITTINGS IAW SMP 583-51-70. NR 323.

Part: FITTING — CRACKED (BS 196)

DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND NLG DRAG BRACE ATTACH FITTING CRACKED AT FS 196. REPLACED FITTING IAW SMP 583-51-70. NR 398.

Part: WEB — CRACKED (VERTICAL STAB)

DURING C CHECK/BRIDGING INSPECTION PER HST5505, FOUND FS 1095 VERTICAL STAB WEB CRACKED AT VSS 9 TO 12. REPAIRED IAW DWG R99-0002-8 AND MPP L100-404-99-061. NR 545.

Part: CAP — CRACKED (BS 946)

DURING C CHECK/BRIDGING INSPECTION, FOUND FS 946 LT INBD CAP CRACKED BEHIND SLOPING LONGERON. REPLACED CAP IAW DWG 342585. NR 1011.

Part: FLOORBEAM — CORRODED (BS 597)

DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND CARGO LOWER STRUCTURE FS 597 UPPER BEAM CAP CORRODED AT RBL 40. REPLACED CAP IAW SMP 583 53-40. NR 924.

Part: CAP — CRACKED (BS 777)

DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 777 CARGO COMPARTMENT LOWER CAP CRACKED. REPLACED CAP IAW DWG 376954, 356250 AND MPP L100-404-99-057. DRC 386.

Part: BULKHEAD — DAMAGED (BS 617)

DURING C CHECK BRIDGING INSPECTION, FOUND FS 617 RT AFT MLG BULKHEAD ASSY DAMAGED BEYOND 2.5 IN LIMIT AT BL 61.62R, WL 200. REPLACED BULKHEAD ASSY IAW SPAR MPP L100-404-99-008. LAC MEA 382-53-99-010.

Part: CAP — CRACKED (BS 797)

DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 797 CARGO COMPARTMENT LOWER BEAM CAP CRACKED BETWEEN LBL 11.0 AND RBL 5.0. REPAIRED IAW MPP L100-404-99-017. NR 387.

Part: WEB — BUCKLED (BS 697)

DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND FS 697 CARGO FLOOR BULKHEAD WEB BUCKLED AND CHANNEL BENT. REPLACED WEB AND CHANNEL PER DWG 356250. NR 442.

Part: ANGLE — CRACKED (BS 576)

DURING C CHECK/BRIDGING INSPECTION PER HC3208, FOUND LOWER CHINE ANGLE CRACK AT FS 576, LBL 61.6. REPAIRED IAW SMP 583 53-40-27 AND MPP L100-404-99-059. NR 478.

Part: BEAM — CORRODED (WING BOX)

DURING C CHECK/BRIDGING INSPECTION NR 420 WORK, FOUND CENTER WING BOX BEAM UPPER REAR CAP CORRODED AT CWS 61R. REPAIRED IAW SMP S83 AND MPP L100-404-99-060. NR 981.

Part: WEB — CRACKED (BS 477)

DURING C CHECK/BRIDGING INSPECTION PER HSP53224, FOUND FS 477 UPPER BULKHEAD WEB CRACKED AT RBL 20 TO RBL 61. REPAIRED IAW SRM 583 53-40-33A. NR 585

Part: WEB — CRACKED (BS 200)

DURING C CHECK/BRIDGING INSPECTION, FOUND FS 200 NWW AFT PRESSURE WEB CRACKED AT WL 126, LBL 9 TO RBL 9. REPAIRED IAW MPP L100-404-99-016. NR 400.

Part: FITTING — CRACKED (BS 617)

DURING C CHECK/BRIDGING INSPECTION PER HST5302, FOUND FS 617 BULKHEAD SIDE SUPPORT FITTING CRACKED AT RBL 61. REPLACED FITTING IAW SMP 583-51-70, NR 350.

Part: LONGERON — CORRODED (NACELLE)

DURING C CHECK/BRIDGING INSPECTION PER HSP7180 FOUND NR 3 QEC RT UPPER SLOPING LONGERON CORRODED. REPLACED LONGERON IAW SRM 583-54-20-08 AND SB 382-71-12, REV 92. NR 349 AND 959.

Part: PANEL — DENTED (BS 593)

DURING C CHECK/BRIDGING INSPECTION PER HC3209, FOUND LMLG FS 593 PRESSURE PANEL DENTED BEYOND LIMITS AT WL 150. REPLACED PRESSURE PANEL IAW SMP 583-51-70 AND DWG 3311015. NR 362.

Part: FITTING — CORRODED (BS 817)

DURING C CHECK/BRIDGING INSPECTION, FOUND LT SLOPING LONGERON FWD ATTACH FITTING CORRODED AT FS 817. REPLACED FITTING IAW SMP 583-53-10-10. NR 381.

Part: CHANNEL — CRACKED (BS 517)

DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND FS 517 4 VERTICAL BULKHEAD CHANNELS CRACKED AT TOP END AT RBL 7, LBL 7, RBL 9 AND LBL 9. REPLACED VERTICAL CHANNELS IAW DWG R99-0002-2 REV A AND MPP L100-404-99-012. NR410.

Part: BEAM — CORRODED (BS 597)

DURING C CHECK/BRIDGING INSPECTION PER HST5319, FOUND FS 597R VERTICAL BEAM SHEARED DUE CORROSION AT WL 200. REPLACED BEAM IAW SMP 583-53-30. NR 390.

Part: DOUBLER — CORRODED (BS 817)

DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND RT SLOPING LONGERON DOUBLER CORRODED, CHIPPED AND HOLED AT FS 817. REPLACED DOUBLER IAW SMP 583-51-70 AND DWG 340033. NR 403.

Part: FLOORBEAM — CORRODED (BS 657)

DURING C CHECK/BRIDGING INSPECTION PER HC05297, FOUND CARGO COMPARTMENT FLOOR FS 657 UPPER BEAM CAP CORRODED AT RLB 20. REPAIRED BEAM CAP IAW MPP L100 404-99-019. NR 921

Part: WEB — DENTED (BS 583)

DURING C CHECK/BRIDGING INSPECTION PER HSP57108, FOUND RMLG FS 583 ACCESS PANEL OPENING DENTED BEYOND LIMITS AT WL 155. REPAIRED IAW SMP 583 51-140-17.

Part: LONGERON — CORRODED (NR 2 NACELLE)

DURING C CHECK/BRIDGING INSPECTION PER HSP7180, FOUND NR 2 ENGINE QEC S/N 3769-24 LOWER RT LONGERON CRACKED AND CORRODED AT FWD INNERFLANGE FIRESHIELD HOLE. REPLACED LONGERON IAW DWG 362501 AND SB 382-71-12. NR 944.

Part: LONGERON — CORRODED (NR 3 NACELLE)

DURING C CHECK/BRIDGING INSPECTION PER HSP7180, FOUND NR 3 QEC S/N LMG 1369-31 UPPER RT SLOPING LONGERON CORRODED. REPLACED LONGERON IAW SMP 583 54-20-03, HSPO7180, AND SB 382-71-12, REV 92. NR 959.

Part: BEAM — CORRODED (BS 597)

DURING C CHECK/BRIDGING INSPECTION PER HST5319, FOUND FS 597L VERTICAL BEAM CORRODED AT WL 144. REPLACED BEAM IAW SMP 583-53-30. NR 389.

Part: FRAME — CORRODED (BS 797)

DURING C CHECK BRIDGING INSPECTION, FOUND FS 797 RING FRAME CORRODED AT FROM BL 5.0L TO BL 10.0R. REPAIRED WITH ANGLE INSTALL IAW SPAR MPP L100-404-99-017. LAC MEA 382-53-9-018.

Part: CHANNEL — DAMAGED (BS 517)

DURING C CHECK BRIDGING INSPECTION, FOUND FS 517 VERTICAL CHANNELS DAMAGED AT BL 40L AND 40R. REPAIRED BY INSTALLING REPAIR DOUBLERS IAW SPAR MPP L100-404-99-012. LAC MEA 382-53-99-014.

Part: WEB — CRACKED (BS 200)

DURING C CHECK BRIDGING INSPECTION, FOUND FS 200 NOSE WHEEL WELL AFT PRESSURE WEB CRACKED CORRODED AT WL 126, BL 9L TO 9R REPLACED IAW SPAR MPP L100-404-99-016. LAC MEA 382-53-99-017.

Part: FRAME — CORRODED (BS 297)

DURING C CHECK BRIDGING INSPECTION, FOUND CENTER FUSELAGE RT FS 297 RING SEGMENT CORRODED FROM WL 166 - 190. REPAIRED IAW SPAR MPP L100-404-99-005. LAC MEA 382-53-99-007.

Part: FITTING — CRACKED (BS 817)

DURING C CHECK/BRIDGING INSPECTION PER HSP53161, FOUND RT SLOPING LONGERON FITTING CRACKED AT FS 817. REPLACED FITTING IAW SMP 583-51-70 AND DWG 356198. NR 402.

Part: BULKHEAD — DAMAGED (BS 617)

DURING C CHECK BRIDGING INSPECTION, FOUND FS 617 LT AFT MLG BULKHEAD ASSY DAMAGED BEYOND 2.5 IN LIMIT AT BL 61.62L, WL 200. REPLACED BULKHEAD ASSY IAW SPAR MPP L100-404-99-009. LAC MEA 382-53-99-011.

Part: BEAM — CRACKED (BS 528)

DURING C CHECK BRIDGING INSPECTION, FOUND FS 528 RT MLG BEAM, INNER BEAM CRACKED AT BL62R, WL 256. REPAIRED BY CUTTING OUT CRACK AND INSTALL FILLER, STRAPS AND ANGLES IAW SPAR MPP L100-404-99-001. LAC MEA 382-53-99-004.

Part: CAP — CRACKED (BS 817)

DURING C CHECK/BRIDGING INSPECTION PER HSP5336, FOUND FS 817 CARGO COMPARTMENT LOWER CAP CRACKED. REPLACED CAP IAW SMP 583-51-70 AND DWG 356251. NR 388

Part: ANGLE — CORRODED (BS 687)

DURING C CHECK/BRIDGING INSPECTION, FOUND FS 687 LT CHINE ANGLE CORRODED. REPAIRED IAW SMP 583-53-40-26. NR 382.