N403LC

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 70,704 hrs · 36,034 cycles

CLIMBING THROUGH 22000 FEET, A LOUD BANG WAS HEARD AND THE AIRPLANE BEGAN RAPIDLY DEPRESSURIZING. DURING INSPECTION AFTER LANDING, FOUND A 14.5 INCH CRACK ON RADOME PRESSURE CANTED BULKHEAD @ BUTTLINE 0, FUSELAGE STATION 93 & WATERLINE 200-214 REQUIRING MAJOR REPAIR. / REPAIRED CRACKED BULKHEAD IAW ERO 5320D3827 & REF MEA 382-53-24-123 R1. LOG PAGE# 51252 ITEM #1

Part: BRACE — CRACKED (ZONE 500) · airframe 70,222 hrs · 35,621 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HSP57165, FOUND LH OUTERWING BRACE CRACKED AT OWS56L, FS535. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 436632. / PSE# 57-50-14, AD 2012-06-09

Part: BRACE — CRACKED (ZONE 500) · airframe 70,222 hrs · 35,621 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HSP57165, FOUND RH OUTERWING #4 MAIN TANK BRACE CRACKED AT OWS248R. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 436630. / PSE# 57-50-14, AD 2012-06-09

Part: BRACE — CRACKED (ZONE 500) · airframe 70,222 hrs · 35,621 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HSP57165, FOUND LH OUTERWING BRACE CRACKED AT OWS108L, FS535. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 436631. / PSE# 57-50-14, AD 2012-06-09

Part: STRINGER — CRACKED (ZONE 500) · airframe 70,222 hrs · 35,621 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HSP57165, FOUND RH OUTERWING STRINGER TO LWR RIB CAP H. CLIP CRACKED AT OWS108R, FS535. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 436633. / PSE# 57-50-14, AD 2012-06-09

Part: LONGERON — CRACKED (ZONE 200) · airframe 70,222 hrs · 35,621 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND LH SLOPING LONGERON VERTICAL TAPE CRACKED AT FS858, LBL61, WL190. / REPAIRED IAW LAC MEA 382-53-24-150. NR# 435680. / PSE# 53-50-13, AD 2012-06-09

Part: JACKSCREW — FAILED (TE FLAPS) · airframe 70,025 hrs · 35,493 cycles

DURING CLIMB FOR A SCHEDULED FLIGHT: FLAPS STUCK AT APPROXIMATELY 10% ON RETRACTION / REMOVED AND REPLACE RH FLAP JACK SCREWS IAW SMP581 CH.27 FIG.27-50-11 & HN2751. . MAJOR REPAIR TO RH INBOARD AND OUTBOARD FLAPS RIG AND OPS CHECK IAW SMP581 27-50-14. / LOG PAGE #55759

Part: FAIRING — CRACKED (CW UPR RH) · airframe 69,525 hrs · 35,134 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND CENTER WING FUSELAGE FAIRING CRACKED AT FS598, WL282, RBL18. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001002070.

Part: SKIN — DENTED (LH FWD) · airframe 69,525 hrs · 35,134 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND FORWARD FUSELAGE DENTED AT FS195, WL166, LBL73. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001001877.

Part: BEAM — CRACKED (LT MLG) · airframe 69,525 hrs · 35,134 cycles

DURING SCHEDULED B-1 CHECK UNDER SP-309, FOUND LH MLG BEAM BOLT HOLES COMMON TO SHELF BLOCK CRACKED AT FS517, WL140-145, LBL63-66. / REPAIRED IAW LAC MEA 382-53-23-054. NR# 1001011319. / PSE# 53-40-15, AD 2012-06-09

Part: STIFFENER — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB LH RIB STIFFENER FOUND CORRODED AT HSS238L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0621. / PSE# 55-10-10, AD 2012-06-09

Part: SKIN — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5712, FOUND RH OUTER FLAP UPPER SKIN CRACKED AT OWFS63R. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0609. / PSE# 57-50-16, AD 2012-06-09

Part: CHINE — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND RH CHINE CAP FS777.0E AND FS797.0E 10,000LBS TIEDOWNS ATTACHMENT AREA CORRODED AT WL146. RBL50.5-61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0363. / PSE# 53-40-10, AD 2012-06-09

Part: CAP — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC53-15, FOUND FS946 BULKHEAD INBOARD CAP CRACKED AT, WL230-270. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0367. / PSE# 53-50-07, AD 2012-06-09

Part: CAP — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS677 UNDERFLOOR BULKHEAD LOWER CAP CORRODED AT LBL60 TO RBL60, WL126-145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0359. / PSE# 53-40-11, AD 2012-06-09

Part: SKIN — DENTED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5321, FOUND LH AFT FUSELAGE SKIN DENTED AT FS903-928, LBL62, WL210-220. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR#0620. / PSE# 53-50-06, AD 2012-06-09

Part: FITTING — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FS777.0E 25000LBS TIE DOWN FITTING CRACKED AT RBL61, WL141-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0506. / PSE# 53-40-11, AD 2012-06-09

Part: WINDOW FRAME — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND WINDSHIELD FRAME CRACKED AT FS93-165, RBL35, WL250. / REPAIRED IAW LAC MEA 382-53-11-060. NR# 0631. / PSE# 53-30-01, AD 2012-06-09

Part: WEB — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH AILERON ASSY WEIGHT SUPPORT ASSY WEB CRACKED AT AS29.17L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0730. / PSE# 57-50-21, AD 2012-06-09

Part: CHINE — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND RH CHINE CAP FS597, FS617, FS637, AND FS657 10,000LBS TIEDOWNS ATTACHMENT AREA CORRODED AT WL146. RBL50.5-61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0364. / PSE# 53-40-10, AD 2012-06-09

Part: CAP — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS737/737.0E UNDERFLOOR BULKHEAD LOWER CAP CORRODED AT LBL60 TO RBL60, WL126-145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0358. / PSE# 53-40-11, AD 2012-06-09

Part: SKIN — DENTED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH INBOARD FLAP LOWER SKIN DENTED AT CWS213-221. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0629. / PSE# 57-30-22, AD 2012-06-09

Part: CAP — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS697 UNDERFLOOR BULKHEAD LOWER CAP CORRODED AT LBL60 TO RBL 60, WL126-145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0360. / PSE# 53-40-11, AD 2012-06-09

Part: RIB — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB LH RIB CAP CRACKED AT HSS219L, FS1070, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 55-20-24. NR# 0623.

Part: RIB — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB LH RIB CAP CRACKED AT HSS199L, FS1070, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 55-20-24. NR#0622.

Part: FITTING — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FS797.0E UNDERFLOOR BULKHEAD TO RING SEGMENT FITTING CRACKED AT RBL61, WL141-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0507. / PSE# 53-40-11, AD 2012-06-09

Part: BULKHEAD WEB — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FUSELAGE AFT OVERHEAD BULKHEAD WEB CRACKED AT FS946, RBL16.5-40, WL272-285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR#0628. / PSE# 53-50-09, AD 2012-06-09

Part: BULKHEAD WEB — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HCHC5315, FOUND FS902 BULKHEAD WEB CRACKED THROUGH RIVET HOLES AND EXISTING REPAIR AT WL210-270. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0366. / PSE# 53-50-07, AD 2012-06-09

Part: CHINE — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS245.0E TO FS345.0E CHINE CAP TIEDOWN RING AREA CORRODED AT LBL50.5-61, WL146.. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR#0362. / PSE# 53-40-10, AD 2012-06-09

Part: STIFFENER — CRACKED · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STABILIZER FRONT BEAM STIFFENER CRACKED AT HSS217L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0624. / PSE# 55-10-10, AD 2012-06-09

Part: CHINE — CORRODED · corrosion level 2 · airframe 68,898 hrs · 34,728 cycles

DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5314, FOUND FS737.0E TO FS817.0E CHINE CAP TIEDOWN RING AREA CORRODED AT LBL50.5-61, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0361. / PSE# 53-40-10, AD 2012-06-09

Part: SKIN — WORN · airframe 68,248 hrs · 34,426 cycles

DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB2703, FOUND RH OUTBOARD FLAP TRAILING EDGE UPPER SKIN WITH WORN SPOTS AT OWFS310-320R; REQUIRING MAJOR REPAIR. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR#1000641124.

Part: BEAM — CRACKED (LT MLG WW) · airframe 67,572 hrs · 34,017 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB3200, FOUND THE LH MLG WHEEL WELL FS497 LOWER BOW BEAM FITTING WITH CRACKED FASTENER HOLE; WL155, LBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0202 / PSE# 53-40-14, AD 2012-06-09

Part: FLOORBEAM — CORRODED (BS 497) · airframe 67,572 hrs · 34,017 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND THE FS497 UNDERFLOOR BULKHEAD LOWER CAP CORRODED, RBL7.5 TO RBL14. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0118 / PSE# 53-40-11, AD 2012-06-09

Part: CAP — CORRODED (LT FLOOR CHINE) · airframe 67,572 hrs · 34,017 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND THE CARGO COMPARTMENT FLOOR LH CHINE CAP FS517 TIEDOWN WELL AREA CORRODED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0084 / PSE# 53-40-10, AD 2012-06-09

Part: FLOOR SUPPORT — CORRODED (BS 597-737) · airframe 67,572 hrs · 34,017 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND THE CARGO COMPARTMENT FLOOR LH CHINE CAP FS617 25,000 LBS TIEDOWN RING AREA CORRODED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0117 / PSE# 53-40-10, AD 2012-06-09

Part: FITTING — CRACKED (LT MLG WW) · airframe 67,572 hrs · 34,017 cycles

DURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH FS537 BULKHEAD TO WHEEL WELL FITTING (PN 355673-201) WITH CRACKS THROUGH ANCHOR NUT HOLES. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0123

Part: BEAM — CRACKED (RT MLG WW) · airframe 67,572 hrs · 34,017 cycles

DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB3200, FOUND THE RH MLG WHEEL WELL FS497 LOWER BOW BEAM FITTING WITH CRACKED FASTENER HOLE; WL155, RBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0203 / PSE# 53-40-14, AD 2012-06-09

Part: HOUSING — OUT OF LIMITS (PROP PUMP) · airframe 67,254 hrs · 33,927 cycles

DURING SCHEDULED FLIGHT, NR 2 ENGINE LOW PROP FLUX OUT OF LIMITS. ENGINE SHUT DOWN, FUEL DUMPED. REPLACED NR 2 PROP PUMP HOUSING.

Part: CONTROL BOX — MALFUNCTIONED (FIRE DETECTION) · airframe 67,061 hrs · 33,804 cycles

APU FIRE INDICATION ON CLIMB OUT. APU WAS NOT RUNNING. PULLED 'T' HANDLE, ISOLATED BLEED AIR, DISCHARGED BOTH FIRE BOTTLES. INDICATION PERSISTED; DECLARED EMERGENCY AND RETURNED TO PABR. REMOVED AND REPLACED FIRE DETECTION CONTROL BOX, IAW SMP581 CHAPTER 26-10. OPERATION CHECK GOOD.

Part: UPLOCK — BROKEN (NLG) · airframe 66,994 hrs · 33,748 cycles

DURING LANDING ON SCHEDULED FLIGHT, NLG UNSAFE INDICATION. VERIFIED VISUALLY DOWN AND LOCKED. FOUND WIRE NR 2 ON UPLOCK SWITCH BROKEN. REMOVED AND REPLACED UPLOCK SWITCH FOR BROKEN WIRES AND PHYSICAL DAMAGE. LEAK CHECKS, ADJUSTMENTS, RETRACTION/EXTENSION CHECKS GOOD. EMERGENCY EXTENSION CHECKS GOOD, IAW SMP581 CH 32-30.

Part: FITTING — CRACKED (BS 858) · airframe 66,923 hrs · 33,706 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS858 AFT FUSELAGE VERTICAL STRUT WITH CRACKED LOWER ATTACHMENT FITTING, RBL62, WL190. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 AND 51-70. NR# 282454.

Part: SKIN — DENTED (BS 865) · airframe 66,923 hrs · 33,706 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND FS865 FUSELAGE SKIN DENTED AT LBL61, WL193. / REPAIRED IAW SMP583 SRM, FIG. 51-140-12. NR# 281590.

Part: STIFFENER — CRACKED (BS 497) · airframe 66,923 hrs · 33,706 cycles

DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND FS497 OVERHEAD BULKHEAD WITH CRACKED STIFFENER AT LBL58, WL264. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 AND 51-70. NR# 282387. / PSE# 53-40-19, AD 2012-06-09.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND ELEVATOR RIB CRACKED HSS61.18R, WL272, FS1125.5 FS1130.5 / REPAIR ACCOMPLISHED IAW SRM, 51-140-20.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND ELEVATOR RIB CRACKED HSS61.98 HSS88.0L. REPAIR ACCOMPLISHED IAW SRM, 51-140-20.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND ELEVATOR RIB CRACKED HSS80.63L, WL272, FS1117.5 FS1133.5 / REPAIR ACCOMPLISHED IAW LOCKHEED SMP583 SRM, 51-140-20. NR# 1000245682.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND ELEVATOR RIB CRACKED HSS76.08R, REPAIR ACCOMPLISHED IAW SRM, 51-140-20.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND RT ELEVATOR RIB CRACKED HSS71.54R. REPAIR ACCOMPLISHED IAW SRM, 51-140-20.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND ELEVATOR RIB CRACKED HSS67.0L, REPAIR ACCOMPLISHED IAW SRM, 51-140-20.

Part: RIB — CRACKED (LT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND ELEVATOR RIB CRACKED HSS71.54L, REPAIR ACCOMPLISHED IAW SRM, 51-140-20.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 66,890 hrs · 33,675 cycles

DURING SCHEDULED MAINTENANCE FOR SKIN REPLACEMENT FOUND ELEVATOR RIB CRACKED HSS67.0R, REPAIR ACCOMPLISHED IAW SRM, 51-140-20.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 66,883 hrs · 33,674 cycles

DURING A CHECK UNDER JOB CARD HA1200 FOUND LT ELEVATOR LOWER SKIN CRACKED AT FS1127, HSS80L AND ALSO CRACKED AT FS1130 AND HSS80L, REQUIRING MAJOR REPAIR. STOP DRILLED CRACKS, FABRICATED AND INSTALLED PATCH IAW SMP583 SRM FIG 51-140-12 AND MEA 382-55-20-048.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 66,865 hrs · 33,670 cycles

DURING A CHECK UNDER JOB CARD HA1200, FOUND RT ELEVATOR LOWER SKIN PUNCTURED AND CRACKED AT FS1126, HSS63.5R AND ALSO CRACKED AT FS1123, HSS70.5R; REQUIRING MAJOR REPAIR. CLEANED DAMAGE AND STOP DRILLED CRACKS, FABRICATED AND INSTALLED PATCH IAW SMP583 SRM FIG 51-140-12 AND MEA 382-55-20-044.

Part: FASTENER — LOOSE (LT TE FLAP SKIN) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH OUTBOARD FLAP TRAILING EDGE UPPER SURFACE WITH LOOSE RIVETS AT OWFS84L, 5" FROM THE TRAILING EDGE. / REPAIRED IAW SRM FIG. 51-140-12.

Part: BULKHEAD WEB — BUCKLED (BS 537) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS537 UNDERFLOOR BULKHEAD WEB BUCKLED AT LBL15, WL138. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: STIFFENER — BUCKLED (BS 657-697) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND UNDERFLOOR STIFFENERS BUCKLED AT FS657, FS667, FS697 AT RBL11, WL145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: ANGLE — CORRODED (BS 537) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5323, FOUND THE LH MLG FS537 BEAM UPPER ANGLE CORRODED, WL250, LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: TEE FITTING — CORRODED (BS 196-236) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE TEE SECTION BETWEEN FS196-236 CORRODED, AT LBL23, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1975502.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5511, FOUND THE LH ELEVATOR LOWER SKIN DENTED BEYOND LIMITS AT HSS285L, FS1126, WL284. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1974177.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5712, FOUND THE RH INBOARD FLAP LOWER SKIN DENTED AT CWS126R, 9" FROM THE TRAILING EDGE. / REPAIRED IAW SRM FIG. 51-140-12.

Part: FLOORBEAM — CORRODED (BS 228) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5312, FOUND THE FS228 FLOOR SUPPORT BEAM UPPER CAP (TEE) CORRODED UNDER ANCHOR NUTS AT RBL20-52, WL146. REPAIRED IAW SRM FIG. 53-30-20.

Part: FASTENER — LOOSE (RT FLAP SKIN) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH OUTBOARD FLAP LEADING EDGE UPPER SURFACE WITH FASTENERS PULLED THROUGH SKIN AT OWFS305R. REPAIRED IAW SRM FIG. 51-140-12.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTBOARD FLAP TRAILING EDGE LOWER SURFACE DENTED AT OWFS45L, 7" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1973852.

Part: BULKHEAD — CORRODED (BS 257) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS257.0E UNDERFLOOR BULKHEAD UPPER CAP CORRODED ON UNDERNEATH SIDE AT LBL32 AND LBL40, WL145. REPAIRED IAW MEA 382-53-19-067.

Part: FRAME — CORRODED (BS 245) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS245.0E FRAME AFT SIDE CORRODED, LBL12, WL126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: DOOR SILL — CRACKED (BS 236) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CREW DOOR SILL CRACKED AT FS236.83, WL195, LBL60. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1973555. / PSE# 53-30-12, AD 2012-06-09.

Part: LONGERON FITTING — CORRODED (BS 245) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245.0E LH LONGERON FITTING CORRODED AT LBL60, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH INBOARD FLAP LOWER SKIN DENTED AT CWS208L, 8" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1000003012.

Part: SKIN — CORRODED (BS 477-490) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE BELLY SKIN CORRODED AT FS477-490, BL0, WL126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: FLOORBEAM — CRACKED (BS 245) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245.0E FLOORBEAM CORRODED AT LBL23, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5511, FOUND THE TAIL CONE (HORIZONTAL STABILIZER) RIB END CRACKED AT FS1107, LBL15, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: SKIN — WORN (LT ELEVATOR) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5511, FOUND THE LH ELEVATOR LEADING EDGE LOWER SKIN WITH WEAR MARK AT HSS53L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: LATCH — DAMAGED (DOOR LATCH) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FUSELAGE DOOR LATCH FITTING DAMAGED AT FS210, LBL60, WL190. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: STIFFENER — BUCKLED (BS 677-717) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FLOORBOARD STIFFENERS BUCKLED AT FS677, FS697 AND FS717; RBL10-15. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1947587.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH OUTBOARD FLAP LEADING EDGE SURFACE CRACKED AT OWFS238R AT CARRIAGE CUTOUT. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR#1979865.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH INBOARD FLAP LEADING EDGE LOWER SURFACE DENTED AT CWS120L, 5" TO 9" FROM LEADING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1974327.

Part: STRUCTURE — CRACKED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH INBOARD FLAP LEADING EDGE LOWER SURFACE CRACKED AT CWS135L, 1.5" FROM THE LEADING EDGE. REPAIRED IAW SRM 51-140-12.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTBOARD FLAP LEADING EDGE LOWER SURFACE CRACKED AT OWFS241L CARRIAGE CUTOUT. REPAIRED IAW SRM FIG. 51-140-12.

Part: CAP — CORRODED (BS 195) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5312, FOUND THE FS195 UNDERFLOOR BULKHEAD UPPER CAP CORRODED UNDER ANCHOR NUTS, LBL10-61, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: BULKHEAD — CORRODED (BS 537) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS537 UNDERFLOOR BULKHEAD LOWER CAP CORRODED AT LBL15, WL126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: CAP — CORRODED (BS 250) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE LH CHINE CAP CORRODED UNDERNEATH ANCHOR NUTS AT FS250.0E, LBL55, WL146. REPAIRED IAW SRM FIG. 53-40-28.

Part: BULKHEAD — DAMAGED (BS 345) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5302, FOUND THE FS345.0E/FS245 UNDERFLOOR BULKHEAD UPPER CAP DAMAGED AT RBL33, WL146. / REPAIRED IAW MEA 382-53-19-079.

Part: FRAME — CRACKED (BS 477) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5316, FOUND THE FS477 FRAME CRACKED AT RBL38, WL278. REPAIRED IAW 53-50 (82-636) REPAIR B, SK382-53-184 REVISION 1.

Part: STIFFENER — CRACKED (BS 497) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5316, FOUND THE FS497 STIFFENING CHANNEL AT LBL7.5, WL258 CRACKED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: BULKHEAD — DAMAGED (BS 345) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS345.0E/FS245 UNDERFLOOR BULKHEAD UPPER CAP TOP SURFACE DAMAGED AT LBL25, WL146. REPAIRED IAW MEA 382-53-19-088.

Part: SUPPORT — CRACKED (BS 180) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS180 BULKHEAD FORWARD LH VERTICAL SUPPORT CRACKED, LBL17 WL170. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, 51-60 & 51-70.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTBOARD FLAP LOWER SKIN DENTED AT OWFS52L, 15" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1973853.

Part: SKIN — CRACKED (RUDDER) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5501, FOUND THE RUDDER LH SKIN CRACKED AT PANEL 291 OPENING, FS1138, VSS121-125. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1946896.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5712, FOUND THE RH OUTBOARD FLAP TRAILING EDGE LOWER SURFACE DENTED AT OWFS130.5R, 5" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1971289.

Part: ANGLE — CORRODED (BS 277) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH FS277.0E CHINE ANGLE CORRODED AT LBL61, WL141 WITH BLENDOUT EXCEEDING SRM LIMITS. REPAIRED IAW MEA 382-53-19-053.

Part: FITTING — CRACKED (LT WING) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTER WING OWS241.6L FLAP TRACK-TO-AFT SPAR LOWER ATTACHED FITTING CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: BULKHEAD — CORRODED (BS 337) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS337 UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT RBL40, WL145./ REPAIRED IAW MEA 382-53-19-068.

Part: FLOORBEAM — CORRODED (BS 228) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5312, FOUND THE FS228 FLOOR SUPPORT BEAM UPPER CAP (TEE) CORRODED UNDER ANCHOR NUTS AT LBL2-LBL40, WL146. REPAIRED IAW SRM FIG. 53-30-20.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTBOARD FLAP TRAILING EDGE LOWER SURFACE DENTED AT OWFS270L, 1" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1973855.

Part: ANGLE — CORRODED (BS 246-257) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH FS246.0E-FS251.0E AND FS257.0E CHINE ANGLE CORRODED AT LBL61.5, WL142 WITH BLENDOUT EXCEEDING LIMITS. REPAIRED IAW MEA 382-53-19-054.

Part: ANGLE — CORRODED (BS 246-251) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH CHINE ANGLE CORRODED AT FS246.0E TO FS251.0E, LBL61, WL141. REPAIRED IAW MEA 382-53-19-054.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LH LEADING EDGE CORRODED AT HSS181L, FS1041. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 55-20-05. NR# 1973880.

Part: INTERCOSTAL — CRACKED (HORIZONTAL STAB) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5511, FOUND THE TAIL CONE (HORIZONTAL STABILIZER) INTERCOSTAL END CRACKED, FS1138, RBL25, WL285. REPAIRED IAW SRM FIG. 51-140-20.

Part: TIE DOWN — CRACKED (BS 245) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND 25,000 LB TIEDOWN FITTING CRACKED AT FS245.0E, LBL56, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: FAIRING — CRACKED (WIND TO BODY) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5321, FOUND THE RH WING-TO-BODY FAIRING UPPER SKIN CRACKED AT FS667, RBL49, WL275. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1946487.

Part: ANGLE — CORRODED (BS 337) · corrosion level 2 · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5321, FOUND THE RH CHINE ANGLE CORRODED AT FS337, WL146, RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH OUTBOARD FLAP LOWER SKIN DENTED AT OWFS225L, 16" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 51-140-12. NR# 1973854.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5511, FOUND THE TAIL CONE (HORIZONTAL STABILIZER) RIB END CRACKED AT FS1107, RBL15, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: FITTING — CORRODED (BS 245) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245.0E BULKHEAD WITH CORRODED LH FITTING, LBL60, WL146.CHECK. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: CAP — CORRODED (BS 817) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5313, FOUND THE RH CHINE CAP CORRODED AT FS817.0E, RBL60, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1946468. / PSE# 53-40-10, AD 2012-06-09.

Part: SPLICE — CRACKED (BS 345) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5317, FOUND THE FS345.0E EXTENSION PLUG SPLICE FITTING CORRODED AT RBL20, WL282.5. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: DUCT — CRACKED (HORIZONTAL STAB) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE HORIZONTAL STABILIZER ANTI-ICE LH EJECTOR DUCT CRACKED. / REPAIRED IAW LAC MEA 382-30-19-084. NR# 1000011914.

Part: BEAM — CRACKED (LT MLG) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS497 LH MLG BOW BEAM CRACKED WL243, LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.

Part: ATTACH FITTING — WORN (MLG) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC3215, FOUND THE NLG RETRACT/EXTEND ACTUATOR AFT ATTACH LUGS (LH & RH) WITH WORN FACES, FS196 BULKHEAD. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1948748.

Part: CAP — CORRODED (BS 497) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS497 UNDERFLOOR BULKHEAD LOWER CAP CORRODED AT LBL6-RBL2, WL126.5. REPAIRED IAW MEA 382-53-19-069.

Part: SKIN — DENTED (LT WING FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE LH INBOARD FLAP LOWER SKIN DENTED AT CWS130L, 8"-14" FROM THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM FIG. 57-70-10. NR# 1973845.

Part: CAP — CORRODED (BS 245) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245 UNDERFLOOR BULKHEAD LOWER CAP CORRODED AT LBL12-RBL12, WL126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: SKIN — CORRODED (BS 277-287) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC3401, FOUND THE BELLY SKIN CORRODED AT FS277.0E TO FS287.0E, BL0, WL126. REPAIRED IAW MEA 382-53-19-065.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5712, FOUND THE RH WING OUTBOARD FLAP TRAILING EDGE UPPER SURFACE CRACKED AT OWFS17R, 7" FROM THE TRAILING EDGE. REPAIRED IAW SRM FIG. 51-140-12.

Part: BULKHEAD WEB — BUCKLED (BS 537) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5314, FOUND THE FS537 UNDERFLOOR BULKHEAD WEB BUCKLED AT RBL15, WL138. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.

Part: SKIN — NICKED (HORIZONTAL STAB) · airframe 66,552 hrs · 33,465 cycles

DURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LH LOWER SKIN WITH MULTIPLE NICKS AT HSS100L, FS1075-FS1090, WL260. / REPAIRED IAW SRM FIG. 55-20-06.

Part: BRACKET — BROKEN (FUSELAGE) · airframe 66,010 hrs · 33,168 cycles

DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5305, FOUND CREW ENTRANCE ABOVE INTERIOR AT FS204 WL200 WITH BROKEN BRACKET, LBL85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH 51-60 & 51-70.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 65,643 hrs · 32,968 cycles

DURING SCHEDULED FLIGHT, THE NR 1 HYDRAULIC PUMP FAILED. REPLACED THE HYDRAULIC PUMP IAW SWP 581 29-11

Part: PANEL — CORRODED (BS 574) · corrosion level 2 · airframe 65,540 hrs · 32,908 cycles

DURING SCHEDULED B-2 CHECK, FOUND THE RT MAIN LANDING GEAR EXTRUDED RISER PANEL CORRODED, BS 574, WL 175, RBL 62. REPLACED IAW SRM 51-60, AND 51-70.

Part: SUPPORT BEAM — CORRODED (BS 577) · corrosion level 2 · airframe 65,540 hrs · 32,908 cycles

DURING SCHEDULED B-2 CHECK, FOUND THE RT BS 577 TRACK SUPPORT BEAM CORRODED AT WL 150, RBL 61. REPLACED IAW SRM 51-60, AND 51-70.

Part: BEAM — CRACKED (BS 588) · airframe 65,540 hrs · 32,908 cycles

DURING SCHEDULED B-2 CHECK, FOUND THE RT BS 588 MAIN LANDING GEAR BEAM OUTBOARD CAP CRACKED, RBL 61, WL 243. REPAIRED IAW MEA 382-53-17-150.

Part: BULKHEAD WEB — CRACKED (BS 902) · airframe 65,540 hrs · 32,908 cycles

DURING SCHEDULED B-2 CHECK, FOUND THE BS 902 OVERHEAD BULKHEAD WEB CRACKED AT RBL 36, WL280. REPAIRED IAW SMP 583, SRM 51-140-17.

Part: BEAM — CORRODED (BS 557) · corrosion level 2 · airframe 65,540 hrs · 32,908 cycles

DURING A SCHEDULED B-2 CHECK, FOUND THE RT BS 557 LOWER BOW BEAM LOWER END FITTING CORRODED AT WL 150, RBL 63. REPAIRED IAW SRM 53-40-13.

Part: PANEL — CORRODED (BS 574) · corrosion level 2 · airframe 65,540 hrs · 32,908 cycles

DURING SCHEDULED B-2 CHECK, FOUND THE RT MAIN LANDING GEAR EXTRUDED RISER PANEL CORRODED AT BS 574, WL 177, RBL 62. REPLACED IAW SRM 51-60, AND 51-70.

Part: HOUSING — FAILED (VALVE) · airframe 64,955 hrs · 32,435 cycles

DURING SCHEDULED FLIGHT, THE NR 3 ENGINE FLAMED OUT ON SHORT FINAL. REPLACED THE VALVE HOUSING IAW CARD HN61135.

Part: BULKHEAD — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR RS8 BULKHEAD UPPER CAP WITH STRESS CORROSION CRACKING, RBL17. REPAIRED IAW SMP 583, SRM FIG 51-140-22.

Part: SKIN — DENTED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING A SCHEDULED C-12 CHECK, FOUND THE CARGO DOOR EXTERIOR SKIN DENTED AT BS 895 RBL 36. REPAIRED IAW SMP 583 SRM 51-140-12.

Part: BULKHEAD — CORRODED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP RS2 BULKHEAD UPPER CAP WITH EXFOLIATION CORROSION, RBL15. SPLICED AT RBL38-RBL46, WL146. REPAIRED IAW SMP 583, SRM FIG 51-140-22.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE CARGO DOOR FS 1012 BULKHEAD WEB WITH MULTIPLE CRACKS AT BL0 TO LBL45. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: GUSSET — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5212, FOUND THE CARGO DOOR INTERIOR, FS990 BULKHEAD TO LOWER SKIN REAR GUSSET CRACKED, LBL50-LBL61. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH 51-70.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 1034, LT & RT ANGLE & DOUBLER CRACKED AT BL59R. ANGLES & DOUBLER REPLACED USING 7075-T6, 0.063" & 0.090". REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SRM CH51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR STA 5.8 & 6.2 LT BULKHEAD WEB CRACKED. REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (BS 880) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE LT AFT FUSELAGE BS 880 BULKEAD WEB INBOARD CAP CRACKED AT WL 225 LBL 63.5. REPAIRED IAW SRM 53-50-17.

Part: BULKHEAD — CORRODED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP RS 4 BULKHEAD UPPER CAP WITH EXFOLIATION CORROSION, RBL 15. SPLICED AT RBL 8 - 21, WL 146. REPAIRED IAW SRM FIG. 51-140-22.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE RT UPPER HORIZONTAL STABILIZER SKIN CRACKED AT FS 1078, HSS59R, WL285. REPAIRED IAW SMP 583, SRM, FIG 55-20-06.

Part: BULKHEAD — CRACKED (BS 968) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RT AFT FUSELAGE INTERIOR BS 968 UPPER BULKHEAD CRACKED RBL 62, WL 278 - 285. REPAIRED IAW SRM 53-50-06.

Part: WEB — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 902 LT & RT LOWER CAP & WEB FOUND CRACKED AT LBL59, RBL59. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: HINGE FITTING — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE RAMP DOOR HINGE FITTING CRACKED AT RS0, LBL32. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583, SRM CH51-60 AND 51-70.

Part: BULKHEAD WEB — DAMAGED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR FWD BULKHEAD WEB RS 0, LBL 34 TO RBL 34 WITH MULTIPLE ELONGATED HOLES. REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE NOSE WHEEL WELL, FS93, BULKHEAD LOWER CAP WITH MULTIPLE CRACKS AT HINGE BRACKET ATTACHMENT LBL21, WL150-WL160. REPAIRED IAW SMP583, SRM FIG 53-30-10.

Part: PLATE — CORRODED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5314, FOUND THE RAMP DOOR RT CHINE PLATE WITH EXFOLIATION CORROSION AT RS1.6 AND RS7.6 AT 2 PLACES; RBL50 & RBL60. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: STRIP — WORN (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE RAMP DOOR L/E STRIP, STEEL, WORN AND ATTACHMENT WITH EXFOLIATION CORROSION; RS0, LBL60-RBL60. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583 SRM CH51-60 AND 51-70, NR 2059.

Part: BULKHEAD — CRACKED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12, FOUND THE RAMP DOOR STA10.2 BULKHEAD UPPER CAP CRACKED AT LBL 58 & RBL 58. REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5314, FOUND THE FS 597 BULKHEAD LOWER CAP WITH 2" LONG CRACK AT LBL 58 TO LBL 61; WL126-WL140. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BEAM — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR RT BEAM WEB CRACKED AT RS10 HOOK FITTING CUTOUT ACCESS AREA, RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD WEB — CRACKED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR STA 3.8 & 4.2 BULKHEAD WEB CRACKED. REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5511, FOUND THE LT HORIZONTAL STABILIZER L/E LOWER RIB CRACKED AT HSS191, LOWER, FS1041, WL260. REPAIRED IAW SMP583, SRM FIG 51-140-20.

Part: FRAME — CRACKED (BS 475) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE CARGO AIR COND COMPT FWD UPPER SKIN ATTACHMENT FRAME WITH A 3 INCH LONG CRACK AT FS 475 WL 200 RBL 85. REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: WEB — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR, RS9.8, BL58L, INTERCOSTAL BULKHEAD WEB CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5511, FOUND LT HORIZONTAL STABILIZER L/E RIB CRACKED AT HSS85L, FS 1020, WL 260. REPAIRED IAW SMP 583, SRM FIG 51-140-20.

Part: SKIN — WARPED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE BELLY FS 196 SKIN WARPED & SCRATCHED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JOB CARD HC5313, FOUND THE RT AFT FUSELAGE FS880, RT BULKHEAD WEB CRACKED AT WL195 RBL66. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 SRM CH51-60 AND 51-70.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC 5313, FOUND THE CARGO COMPARTMENT RT CHINE CAP REPAIR DOUBLER CORRODED; FS 250E TO FS 284E, BL50R, WL146. REPAIRED IAW SMP 583, SRM FIG 53-40-28.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5314, FOUND THE CABIN FS 607 BELLY SKIN STIFFENER CRACKED AT LBL 60, WL 130. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE BELLY, UNDERDECK, FS196 BULKHEAD LOWER CAP WITH STRESS CORROSION CRACK AT BL25L, WL130. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND CH51-70.

Part: STIFFENER — CRACKED (NLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE NOSE WHEEL WELL RT STIFFENER CRACKED AT FS 100, WL 195, BL 80R. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: CHINE — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5314, FOUND THE RT CHINE CAP WITH STRESS CORROSION CRACKING AT FS 733 TIEDOWN WELL, BL60R WL146. REPAIRED IAW MEA 382-55-16-062.

Part: SKIN — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE RAMP DOOR FWD L/E SKIN CRACKED AT RS0, RBL30 TO RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND 51-70.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC 5313, FOUND LT AFT FUSELAGE, FS 968 UPPER BULKHEAD FRAME CRACKED AT BL 61L, WL 280. REPAIRED IAW SMP 583, SRM FIG 53-50-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE NOSE RADOME BULKHEAD WEB WITH MULTIPLE CRACKS AT FS 93, LBL 80, WL 190. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5511, FOUND LT HORIZONTAL STABILIZER L/E RIB CRACKED AT HSS90L, FS 1020, WL 260. REPAIRED IAW SMP 583, SRM FIG 51-140-20.

Part: BULKHEAD — CORRODED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP RS2 BULKHEAD UPPER CAP WITH EXFOLIATION CORROSION, LBL17. SPLICED AT LBL38-LBL46, WL146. REPAIRED IAW SMP 583, SRM FIG 51-140-22.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 1012, BULKHEAD RT LOWER CAP & DOUBLER CRACKED AT BL 69R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE AFT FUSELAGE INTERIOR FS 814, LT BULKHEAD TO SLOPING LONGERON TEE FITTING CRACKED AT WL170, BL62L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR RS 6 BULKHEAD WEB WITH MULTIPLE CRACKS AT LBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC 5313, FOUND CARGO DOOR FS 1012, BULKHEAD STIFFENER CRACKED AT LBL45 & LBL55. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: FITTING — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR LATCH, ACTUATOR FITTING ASSY CRACKED, RS8, BL0. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH 51-70.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR FS 924 BULKHEAD RT DOUBLER CRACKED AT BL 59R. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5323, FOUND THE LT MAIN WHEEL WELL FS 477 BULKHEAD WEB CRACKED AT WL190, LBL85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND 51-70.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5324, FOUND THE RT MAIN WHEEL WELL FS 477 BULKHEAD WEB CRACKED, WL175, RBL85. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5312, FOUND THE UNDERDECK FLOOR SUPPORT L-ANGLE WITH STRESS CORROSION CRACKING AT FS 196 WL146, LBL61 TO RBL61 AROUND ANCHOR NUT HOLES. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: RIB — WARPED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR, STA 10.5, RBL34 T/E RIB WEB, WARPED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: SPAR CAP — CORRODED (RT HORIZ STAB) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE RT HORIZONTAL STABILIZER FRONT SPAR UPPER CAP WITH EXFOLIATION CORROSION AT HSS 140R, FS 1041, WL 282. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: STIFFENER — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR STA 10.2, BULKHEAD STIFFENER, HOOK FITTING SUPPORT. CRACKED AT LBL41. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: FRAME — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211 FOUND THE RAMP DOOR PEDESTAL FRAME WARPED & CRACKED; RS9. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5323, FOUND THE LT MAIN WHEEL WELL FS572, WL160 TO WL165, LBL62 BULKHEAD WEB WITH STRESS CORROSION CRACKING. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: STIFFENER — CRACKED (NLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JOB CARD HC3215, FOUND THE NOSE WHEEL WELL FS 93 BULKHEAD FWD STIFFENER, LOWER, CRACKED AT LBL20, WL159. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH51-60 AND 51-70.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC 5313, FOUND THE RT AFT FUSELAGE INTERIOR FS990 BULKHEAD INBD CAP FOUND CRACKED, RBL61-RBL80, WL250-WL270. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BAND — BENT (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JOB CARD HC5313, FOUND THE CARGO RAMP FAIRING, BELLY BAND, BENT AT APPROXIMATELY BL45R-BL55R, RS10.2-RS10.8. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: BULKHEAD — DAMAGED (RT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5324, FOUND THE RT MAIN WHEEL WELL CABIN FS 477 BULKHEAD OTBD CAP WITH DEEP CUTTING MARK AT RBL85, WL185. REPAIRED IAW SMP 583, SRM FIG 51-140-22.

Part: STRUCTURE — CRACKED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR STA 9 BULKHEAD-TO-RT BEAM GUSSET WITH MULTIPLE CRACKS RBL 40 - 50. REPAIRED BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: BRACE — CRACKED (LT WING) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JC HC2811, FOUND NR 2 TANK OWS108 RIB BRACE CRACKED AT FS550 OWS108L WL260-WL285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JOB CARD HC5324, FOUND THE RT MAIN WHEEL WELL FS 617 BULKHEAD WEB CRACKED AT WL175, RBL83. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM CH51-60 AND 51-70.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 968 BULKHEAD RT DOUBLER CRACKED AT BL 59R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: BEAM — CRACKED (RT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5324, FOUND THE RT MAIN WHEEL WELL FS 537 BOW BEAM WITH STRESS CORROSION CRACK AT WL254, RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND 51-70.

Part: SHIELD — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE RAMP DOOR T/E SHIELD WITH MULTIPLE CORROSION AREAS & CRACKS AT RS10, BL60L TO BL60R, 2024T3 0.063, 7075-T6 0.071. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH 51-60 AND 51-70, NR 2058, 7075-T6 0.071.

Part: BEAM — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR RS 9 BEAM WEB CRACKED AT BL30R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: STIFFENER — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR STA 10.2 BULKHEAD STIFFENER, HOOK FITTING SUPPORT. CRACKED AT LBL49. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 880 BULKHEAD RT DOUBLER CRACKED AT RBL59. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: CAP — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 968 BULKHEAD LT & RT LOWER CAP CRACKED AT LBL59 & RBL59. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND 51-70.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5511, FOUND LT HORIZONTAL STABILIZER L/E RIB CRACKED AT HSS 95L, FS020, WL 260. REPAIRED IAW SMP 583, SRM FIG 51-140-20.

Part: STRUCTURE — CRACKED (PUMP SHIELD) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE CARGO BAYBS 797E LT PUMP SHIELD (BOX) CRACKED AT LBL 62, WL 146 - 171. REPAIRED IAW SRM FIG. 51-140-12.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 990 BULKHEAD LT LOWER CAP & DOUBLER CRACKED AT LBL59, AND THE RT DOUBLER CRACKED AT RBL 59. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: FRAME — CORRODED (BULKHEAD) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR STA 10.2 BULKHEAD LOWER CAP WITH MULTIPLE EXFOLIATION CORROSION AREAS & ELONGATED HOLES, LBL 60 & RBL 60. REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5323, FOUND THE LT MAIN WHEEL WELL REAR BULKHEAD WEB CRACKED AT FS617, WL175, LBL85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND 51-70.

Part: BEAM — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS1034 RT BEAM WEB CRACKED, FS 1022 TO FS 1034. REPAIRED IAW SMP583, SRM FIG 51-140-17.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 946 BULKHEAD RT LOWER CAP, WEB & DOUBLER CRACKED AT BL 59R. REPLACED WITH LS 2242-3, 7075T6-0.071" & 0.125". REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5321, FOUND THE FORWARD FUSELAGE EXTERIOR SKIN CRACKED AT FS 240, WL 193, LBL 61 & MULTIPLE ELONGATED HOLES. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD WEB — CRACKED (BS 93) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE BS 93 BULKHEAD WEB WITH A 1 INCH LONG CRACK AT WL 190 RBL 50. REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE FWD FUSELAGE INTERIOR FS 160, WL 138, BL 30L, SKIN DOUBLER WITH STRESS CORROSION CRACKING. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE FWD FUSELAGE INTERIOR FS 186, WL 130, RBL 40, SKIN DOUBLER WITH EXFOLIATION CORROSION. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583, SRM CH51-60 AND CH51-70.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5313, FOUND THE CARGO COMPARTMENT FS 577, FLOORBEAM LT & RT WEB FOUND CRACKED AT WL 138 BL 51L, BL 51R AT 2 PLACES. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: BULKHEAD — WARPED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5212, FOUND THE CARGO DOOR INTERIOR FS 902, BULKHEAD WEB WARPED & DENTED AT BL20L TO BL20R & BL20 TO BL40 LT, RT 3 PIECE WEB. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC 5313, FOUND THE CARGO COMPARTMENT FS 577 FLOORBEAM UPPER CAP CRACKED AT RBL 56, WL 243. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: INTERCOSTAL — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC 5211, FOUND THE RAMP DOOR INTERIOR RS 6 TO RS 8, INTERCOSTAL BEAM CRACKED AT BL3L, BL3R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: BULKHEAD — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR LT BULKHEAD WEB BEAM CRACKED AT RS10 HOOK FITTING ACCESS CUTOUT, LBL60. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: ANGLE — CORRODED (RT MLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5324, FOUND THE RT MAIN WHEEL WELL LOWER CHINE ANGLE BULGED, FROM CORROSION, AT FS587, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND 51-70.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5511, FOUND THE LT HORIZONTAL STABILIZER L/E RIB CRACKED AT HSS 296L, FS 1020, WL 260. REPAIRED IAW SMP 583, SRM FIG 55-20-11.

Part: ATTACH ANGLE — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR RS8.6 TO RS9 ATTACH ANGLE CRACKED, RBL60. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: SUPPORT FITTING — CORRODED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JOB CARD HC5313, FOUND THE RAMP DOOR RT SUPPORT FITTING WITH PITTING CORROSION AROUND BUSHING HOLE; RS0, RBL32. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND 51-70.

Part: FLOOR SUPPORT — CORRODED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR FLOOR SUPPORT WITH CORROSION AT RS 4 RBL 17. REPAIRED BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: WEB — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5212, FOUND THE FS 924 CARGO DOOR LOWER CAP ATTACHMENT WEB CRACKED; RBL20 TO RBL40. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: CAP — CRACKED (CARGO DOOR) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS 924 BULKHEAD LT LOWER CAP CRACKED AT BL59L. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583 SRM CH51-60 AND 51-70.

Part: TIE DOWN — CRACKED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5314, FOUND THE FS 677, TIE DOWN 25,000 LB FITTING WITH 2" LONG CRACK, WL146, LBL60. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD WEB — CRACKED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR STA 7.8 & 8.2 BULKHEAD WEB CRACKED. REPAIRED BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: STRUCTURE — CRACKED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR STA 8.6 BULKHEAD TO RT BEAM GUSSET CRACKED RBL 40 - 50. REPAIRED BY REPLACEMENT IAW SRM CH51-60 AND 51-70.

Part: BULKHEAD — CORRODED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR STA 6, BULKHEAD UPPER CAP WITH EXFOLIATION CORROSION, RBL16. REPAIRED IAW SMP 583, SRM FIG 51-140-22.

Part: BULKHEAD — CORRODED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP RS 4 BULKHEAD UPPER CAP WITH CORROSION, LBL 15. SPLICED AT LBL 8 - 21, WL 146. REPAIRED IAW SRM FIG. 51-140-22.

Part: BULKHEAD — WARPED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR STA 9 BULKHEAD WEB WARPED AT RBL18 TO RBL24. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM CH51-60 AND CH51-70.

Part: STIFFENER — CRACKED (CARGO RAMP) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5211, FOUND THE RAMP DOOR INTERIOR STA 10.2 BULKHEAD STIFFENER, HOOK FITTING SUPPORT, CRACKED AT RBL41. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH51-60 AND CH51-70.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK UNDER JOB CARD HC5321, FOUND NOSE WHEEL WELL FS 93 BULKHEAD LOWER CAP WITH MULTIPLE CRACKS AT HINGE BRACKET ATTACHMENT RBL 21, WL 150-160. REPAIRED IAW SMP 583, SRM FIG 53-30-10.

Part: BULKHEAD WEB — CORRODED · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR FWD BULKHEAD WEB CORRODED WITH MULTIPLE ELONGATED HOLES AT RS 0, LBL 34 TO LBL 59. / REPAIR BY REPLACEMENT IAW SRM 51-60 AND 51-70.

Part: BEAM — CORRODED (FUSELAGE) · airframe 64,217 hrs · 32,021 cycles

DURING SCHEDULED C-12 CHECK, UNDER JOB CARD HC5323, FOUND THE LT MAIN WHEEL WELL, FS 557 BOW BEAM INBD CAP WITH EXFOLIATION CORROSION AT WL155 TO WL160, LBL 63 SPLICE JOINT AREA. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP 583, SRM CH 51-60 AND CH 51-70.

Part: INTERCOSTAL — CORRODED (BS 307) · airframe 63,595 hrs · 31,479 cycles

DURING SCHEDULED B-3 CHECK, FOUND 9G NET LT INTERCOSTAL NR 2 CORRODED FS307, LBL85, WL195. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SRM CH 51-70 & LM DWG 3305014.

Part: STRUT — PUNCTURED (BS 814) · airframe 63,595 hrs · 31,479 cycles

DURING SCHEDULED B-3 CHECK, UNDER JOB CARD HB5302, FOUND PUNCTURED VERTICAL STRUT TUBE LOWER END AT FS814 LT SIDE, STANCHION, LBL62, WL175. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 581, MM 91-00 & SMP 583, SRM 51-70.

Part: INTERCOSTAL — GOUGED (BS 307) · airframe 63,595 hrs · 31,479 cycles

DURING SCHEDULED B-3 CHECK, FOUND THE 9G NET NR 9 INTERCOSTAL GOUGED AND PIN WORN, FS307, LBL75, WL225. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM CH 51-70 AND LM DWG 3305014.

Part: INTERCOSTAL — CORRODED (BS 307) · airframe 63,595 hrs · 31,479 cycles

DURING SCHEDULED B-3 CHECK, FOUND 9G NET LT INETRCOSTAL NR 1 CORRODED FS307, LBL75 WL165. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM CH 51-70 & LM DWG 3305014.

Part: HOUSING — FAILED (VALVE) · airframe 63,313 hrs · 31,313 cycles

DURING CRUISE, NR 4 ENGINE FLAMED OUT. SHUTDOWN IAW QRH PROCEDURES. R & R VALVE HOUSING ASSY IAW HN61135.

Part: HOUSING — DAMAGED (VALVE) · airframe 63,274 hrs · 31,292 cycles

DURING DESCENT, NR 4 ENGINE FLAMED OUT. SHUTDOWN IAW QRH PROCEDURES. R & R VALVE HOUSING ASSY.

Part: STRAP — CORRODED (BS 200-236) · airframe 62,947 hrs · 31,001 cycles

DURING SCHEDULED B-2 CHECK UNDER FOUND BELT FRAME STRAP CORRODED AT BS 200 - 236, LBL 60 AT FORWARD LOWER CORNER OF ENTRY DOORWAY. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-70.

Part: BULKHEAD WEB — CRACKED (BS 946) · airframe 62,947 hrs · 31,001 cycles

DURING SCHEDULED B-2 CHECK, FOUND CARGO DOOR BS 4 BULKHEAD WEB HAD 3 CRACKS AT FS 946, LBL 30 TO LBL 37. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP583 SRM 51-60 & 51-70, AND DWG 372552.

Part: WEB — WORN (CARGO DOOR) · airframe 62,947 hrs · 31,001 cycles

DURING SCHEDULED B-2 CHECK UNDER JC HB5302, FOUND THE CARGO DOOR WEB WORN THROUGH AT STA 1, FS 880, LBL 33. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70, AND DWG 342582.

Part: BULKHEAD — CRACKED (BS 880) · airframe 62,947 hrs · 31,001 cycles

DURING SCHEDULED B-2 CHECK, FOUND BS 880 RT SIDE BULKHEAD INBD CAP CRACKED, RBL 62, WL 199. REPAIRED IAW SRM FIG 53-50-17.

Part: BULKHEAD WEB — CRACKED (BS 924) · airframe 62,947 hrs · 31,001 cycles

DURING SCHEDULED B-2 CHECK, FOUND FS 924 BULKHEAD WEB CRACKED, RBL 62, WL 254. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM 51-60 & 51-70, AND DWG 359091. NR N-14, WO 1391418.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 62,947 hrs · 31,001 cycles

DURING SCHEDULED B-2 CHECK, FOUND HORIZONTAL STABILZER LOWER SKIN FS1066, RBL36 HAD CRACK & CORROSION. REPAIRED IAW SRM, 51-60 & 51-70, AND DWG 370372.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 62,947 hrs · 31,001 cycles

DURING SCHEDULED B-2 CHECK, FOUND HORIZONTAL STABILZER LOWER SKIN CRACKED & CORRODED. REPAIRED IAW SRM 51-60 & 51-70, AND DWG 370247.

Part: FORMER — CRACKED (RT WING TE FLAP) · airframe 62,364 hrs · 30,559 cycles

DURING SCHEDULED A-1 CHECK, UNDER JC HA120, FOUND THE RT OTBD WING FLAPWELL HAD A CRACKED FORMER. FORMER LOCATED AT OTBD FLAP. REPAIRED IAW SRM 57-60-10.

Part: SKIN — DAMAGED (LT AILERON) · airframe 62,364 hrs · 30,559 cycles

DURING SCHEDULED A-1 CHECK, FOUND THE LT AILERON LOWER SKIN WAS DAMAGED. REPAIRED IAW SRM FIG 51-140-12.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 62,364 hrs · 30,559 cycles

DURING SCHEDULED A-1 CHECK, FOUND THE RT OTBD FLAP LOWER SURFACE WAS PUNCTURED AT FLAP STATION 141R, 35 INCHES FORWARD FROM THE T/E, AT WL256. REPAIRED IAW SRM 57-70-10.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 62,364 hrs · 30,559 cycles

DURING SCHEDULED A-1 CHECK, FOUND THE HORIZONTAL STABILIZER BOX STRUCTURE'S LOWER SKIN WAS CRACKED. REPAIRED IAW SRM 51-140-12.

Part: ANGLE — CRACKED · airframe 62,185 hrs · 30,253 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND LT UPPER MAIN WHEEL WELL ARMPIT PANEL ATTACH BEAM ASSY ZEE ANGLE CRACKED AT BS 561, LBL 72.6, WL 237. REPAIR ACCOMPLISHED IAW MEA 382-57-14-025.

Part: CHANNEL — CRACKED (BULKHEAD) · airframe 62,185 hrs · 30,253 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND RIGHT AFT BS 836 BULKHEAD CHANNEL CRACKED AT WL 195, RBL 82. REPAIRED IAW SMP 583, FIGURE 51-140-19, NR 2010.

Part: ANGLE — CRACKED (BS 770) · airframe 62,185 hrs · 30,253 cycles

DURING SCHEDULED B-1 INSPECTION, FOUND RIGHT AFT FUSELAGE INTERIOR BS 770 BULKHEAD-TO-SLOPING-LONGERON TEE ANGLE WAS CRACKED, RBL66 WL150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: CONTROL BOX — UNKNOWN (CARGO TEMP) · airframe 61,691 hrs · 30,014 cycles

DURING SCHEDULED FLIGHT, CREW EXPERIENCED SMOKE AND FUMES ON FLIGHT DECK. BOTH CARGO AND FLIGHT DECK AIR CONDITIONING PACKS WERE SECURED AS A PRECAUTION AND AN AIR RETURN WAS EXECUTED. AFTER LANDING, A VISUAL INSPECTION OF THE CARGO COMPARTMENT AIR CONDITIONING PACK AND FLIGHT DECK AIR CONDITIONING PACK WAS PERFORMED. CARGO BAY TEMP CONTROL VALVE WAS DISCOVERED TO BE IN THE "FULL HOT" POSITION. CARGO COMPARTMENT TEMP CONTROL BOX WAS REPLACED AS A PRECAUTION. A TEST FLIGHT WAS PERFORMED AND A FULL OPS CHECK OF THE AIRCONDITIONING SYS WAS CARRIED OUT. NO DEFECTS WERE NOTED DURING THE TEST FLIGHT.

Part: COOLING TURBINE — FAILED (A/C SYSTEM) · airframe 61,686 hrs · 30,012 cycles

DURING SCHEDULED FLIGHT, THE CREW EXPERIENCED SMOKE AND FUMES ACCOMPANIED BY A HIGH PITCHED SQUEAL. THE FLIGHT DECK AIR CONDITIONING SYS WAS SECURED AND AIR TURNED BACK. POST LANDING INSP DETERMINED THE FLIGHT DECK STATION COOLING TURBINE TO HAVE FAILED. DEFERRED THE FLIGHT STATION AIR CONDITIONING SYS IAW MEL 21-1A, LP 33737.

Part: SUPPORT BRACKET — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11, CHECK WHILE PERFORMING NR 2148, FOUND LT HORIZONTAL STABILIZER L/E EJECTOR INTERIOR STRINGER SKIN SUPPORT BRACKET HAD CRACKED; HSS276.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW 51-60 AND 51-70.

Part: SUPPORT BRACKET — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2148, FOUND LT HORIZONTAL STABILIZER L/E EJECTOR INTERIOR STRINGER SKIN SUPPORT BRACKET HAD CRACKED; HSS257, REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: STIFFENER — CRACKED (BS 607) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2080, FOUND BELLY STIFFENER CRACKED BS 607, LBL 34, WL 126. REPAIRED IAW SMP 583, FIG 51-140-21.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11, CHECK IAW JOB CARD HC5321, FOUND RT HORIZONTAL STABILIZER L/E UPPER SKIN CRACKED AT HSS162. 2024-T3 0.040" AND 20245-T3 0.050". REPAIRED IAW SMP 583, FIGURE 51-140-14. NR 2046 /PSE 55-10-02/ AD 2012-06-09.

Part: STIFFENER — CRACKED (BS 607) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2080, FOUND BELLY STIFFENER CRACKED BS 607, RBL 1, WL 126. REPAIRED IAW SMP 583, FIG 51-140-21.

Part: STRINGER — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER L/E INTERIOR STRINGER HAD CRACKED AT WL 278, HSS 261. REPAIRED IAW SMP 583, FIG 55-20-08.

Part: ATTACH FITTING — BROKEN (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER'S LT INTERIOR RIB-TO-FRONT SPAR CLIPS BROKEN AT HSS 277 LOWER. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: SUPPORT BRACKET — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2148, FOUND LT HORIZONTAL STABILIZER LEADING EDGE EJECTOR INTERIOR STRINGER SKIN SUPPORT BRACKET HAD CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2164 PSE 55-10-10 AD 2012-06-09.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT UPPER HORIZONTAL STABILIZER SKIN CRACKED, HSS61. REPAIRED IAW SMP 583, FIGURE 55-20-06.

Part: RIB — CRACKED (BS 830) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2009, FOUND RIB CRACKED BS 830, WL 165-180, RBL 67. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: SPAR CAP — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER FRONT SPAR'S LOWER OTBD CAP'S TIP ASSY MOUNTING POINT CRACKED, HSS296. REPAIRED IAW SMP 583, FIG 55-20-30. NR 2075, PSE 55-10-04, AD 2012-06-09.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2153, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER FRONT SPAR WEB, FOUND UPPER SKIN INNER HAT SECTION, CORRUGATED SKIN CRACKED; FS1070, HSS199, WL278. REPAIRED IAW SMP 583, FIG 55-20-07. NR 2172 / PSE 55-10-02, AD 2012-06-09.

Part: PLATE — WARPED (BS 205-236) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND UPPER DECK CREW DOOR SILL WARPED FS 205 TO 236, WL 146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW MEA 382-53-05-018.

Part: LONGERON — CRACKED (BS 858) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT AFT SLOPING LONGERON TANG CRACKED AT BS 858, BULKHEAD STRUT ATTACHMENT, BS 858, RBL 62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: STIFFENER — CRACKED (CARGO DOOR BLKHD) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT CARGO DOOR BULKHEAD STIFFENER CRACKED, BS 1012, RBL 10 AND 20. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: ANGLE — CRACKED (BS 418) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT CHINE ANGLE CRACKED, BS 418 WL 140 LBL 61.5. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: FLOORBEAM — CORRODED (BS 577) · corrosion level 2 · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND FLOORBEAM LOWER CAP HAD EXFOLIATION CORROSION BS 577, LBL 10 TO RBL 10, WL 126. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT MAIN WHEEL WELL BULKHEAD WEB CRACKED BS 615, WL 230 AND 235, LBL 61.5. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: BEAM — CRACKED (BS 577) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 4415, FOUND RT MLG BEAM AT FS 577 PREVIOUSLY STOP-DRILLED MEMBER HAD THE CRACK CONTINUE PAST THE STOP-DRILL. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-13-103.

Part: ANGLE — CUT (BS 491) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL CHINE ANGLE HAD DEEP CUT MARK, BS 491 WL 140, FROM CHAFING AGAINST MUD GUARD PANEL. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: CAP — CORRODED (BS 577) · corrosion level 2 · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT CHINE CAP EXFOLIATION CORROSION AT PORK CHOP FITTING ATTACHMENT, BS 577, LBL 50 TO 61, WL 146. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: BULKHEAD WEB — CRACKED (BS 605) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK PER, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT BS 605 WL 165 RBL 62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT STABILZER L/E UPPER SKIN CRACKED AT HSS 162. REPAIRED IAW SMP 583, FIG 51-140-14.

Part: BULKHEAD WEB — CORRODED (LT MLG WW) · corrosion level 2 · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2070, FOUND LT MAIN WHEEL WELL WEB HAD PITTING AND CORROSION FS 472 TO 517, WL 144 TO 150 AND INSUFFICIENT EDGE DISTANCE AT FS 497. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, DURING LT ELEVATOR REMOVAL FOUND HORIZONTAL STABILIZER T/E RIB CRACKED; FS 1095, HSS 156, WL 265 TO WL 272. REPAIRED IAW SMP583, SRM FIG 51-140-20.

Part: BULKHEAD WEB — CRACKED (BS 617) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT BS 617, WL 200 RBL 72. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: SUPPORT BRACKET — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2148, FOUND LT HORIZONTAL STABILIZER L/E EJECTOR INTERIOR STRINGER SKIN SUPPORT BRACKET HAD CRACKED; HSS218.5, REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2164 / PSE55-10-10, AD 2012-06-09.

Part: SKIN — CRACKED · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2153, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER FRONT SPAR WEB, FOUND LOWER SKIN INNER HAT SECTION CORRUGATED SKIN CRACKED; FS1090, HSS199, WL260. REPAIRED IAW SMP 583, FIG 55-20-07.

Part: CAP — CRACKED (BULKHEAD) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND AFT FUSELAGE INTERIOR UPPER BULKHEAD'S LOWER CAP CRACKED, BS 946 WL 260 RBL 56. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: STRINGER — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER L/E INTERIOR STRINGER HAD CRACKED AT WL 278, HSS 156 UPPER. REPAIRED IAW SMP 583, FIG 55-20-08.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11, CHECK WHILE PERFORMING NR 2153, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER FRONT SPAR WEB, FOUND LOWER SKIN INNER HAT SECTION CORRUGATED SKIN CRACKED; FS 1065, HSS 199, WL 260. REPAIRED IAW SMP 583, FIG 55-20-07.

Part: RIB — CRACKED (BS 918) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2009, FOUND RIB CRACKED; FS 918, WL 190-210, RBL 67. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: CAP — CRACKED (BULKHEAD) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, IAW JOB CARD HC5315, FOUND LT AFT FUSELAGE INTERIOR BULKHEAD INBD CAP CRACKED AT BS 902, WL 230, LBL 64. REPAIRED IAW SMP 583, FIG 53-50-17.

Part: MANIFOLD — CRACKED (BS 607) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL MANIFOLD CRACKED AT BS 607, RBL 62, WL 142. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: STIFFENER — BROKEN (CARGO DOOR BLKHD) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT CARGO DOOR REAR BULKHEAD STIFFENER BROKEN, FS 1038, LBL 25. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2153, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER FRONT SPAR WEB, FOUND UPPER SKIN INNER HAT SECTION CORRUGATED SKIN CRACKED; FS1065, HSS219, WL278. REPAIRED IAW SMP 583, FIG 55-20-07.

Part: ANGLE — BROKEN (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER'S LT INTERIOR RIB-TO-FRONT SPAR CLIPS BROKEN AT HSS277 UPPER. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: STRINGER — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER L/E INTERIOR STRINGER HAD CRACKED AT WL 278, HSS 268. REPAIRED IAW SMP 583, FIG 55-20-08.

Part: SKIN — CRACKED (HORIZONAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, LT UPPER HORIZONTAL STABILIZER SKIN CRACKED AT HSS 256. REPAIRED IAW SMP 583, FIG 55-20-06.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, IAW JOB CARD HC5321, FOUND LT HORIZONTAL STABILIZER UPPER SKIN INNER HAT SECTION HAD 3 CRACKS AT HSS277, WL278. REPAIRED IAW SMP 583, FIG 55-20-07.

Part: CAP — WORN (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER TIP INNER LOWER CAP WORN AT FWD AND AFT MOINTING POINTS, HSS298. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CRACKED · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, WHILE PERFORMING NR 2153, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER FRONT SPAR WEB, FOUND UPPER SKIN INNER HAT SECTION CORRUGATED SKIN CRACKED; FS1089, HSS199, WL278. REPAIRED IAW SMP 583, FIGURE 55-20-07.

Part: BULKHEAD WEB — CRACKED (BS 477) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT UPPER MAIN WHEEL WELL BULKHEAD WEB CRACKED, BS 477 WL 120 RBL 85. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: TEE FITTING — CRACKED (BS 858) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11, CHECK WHILE PERFORMING NR 2009, FOUND TEE FITTING CRACKED AT BS 858, RBL 63 NEAR SLOPING LONGERON. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: STIFFENER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2153, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER'S FRONT SPAR WEB, FOUND BULKHEAD STIFFENER HAD EXFOLIATION CORROSION AT FS 1075, HSS180. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: CAP — CRACKED (BULKHEAD) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK IAW JOB CARD HC5315, FOUND RT AFT FUSELAGE INTERIOR BULKHEAD INBD CAP CRACKED AT BS 902, WL 203, RBL 63. REPAIRED IAW SMP 583, FIG 53-50-17, NR 2013, PSE 53-50-07, AD 2012-06-09.

Part: MANIFOLD — CRACKED (BS 567) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL MANIFOLD CRACKED AT BS 567, RBL 62, WL 142. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CRACKED (BS 1076) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2153, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER FRONT SPAR WEB, FOUND UPPER SKIN INNER HAT SECTION CORRUGATED SKIN CRACKED; FS1076, HSS199, WL278. REPAIRED IAW SMP 583, FIG 55-20-07. NR 2172, PSE 55-10-02, AD 2012-06-09.

Part: TEE FITTING — CRACKED (BS 824) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2009, FOUND TEE FITTING CRACKED AT BS 824, RBL 63. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: SKIN — CUT (RT ELEVATOR) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT ELEVATOR L/E SKIN HAD DEEP CUTS (AGAINST BRUSH STRIP); BS 1110, HSS 51 TO HSS 61, WL 270. REPAIRED IAW SMP 583 FIGURE 51-140-10.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER UPPER SKIN INNER HAT SECTION HAD TWO CRACKS AT HSS 257, WL 278. REPAIRED IAW SMP 583, FIG 55-20-07.

Part: FLOORBEAM — CORRODED (BS 617) · corrosion level 2 · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND UNDERFLOOR BEAM LOWER CAP HAD EXFOLIATION CORROSION BS 617, LBL10 TO RBL10. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: DOUBLER — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND RT HORIZONTAL STABILIZER L/E INNER DOUBLER HAD TWO CRACKS AT INTERIOR SURFACE SKIN AND COMPENSATOR SUPPORT, HSS162. REPAIRED IAW SMP583, FIG 55-20-08.

Part: TEE FITTING — CRACKED (BS 836 BULKHEAD) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK, FOUND AFT FUSELAGE INTERIOR BULKHEAD'S RT TEE FITTING CRACKED. BS 836, RBL 63. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583 51-60 AND 51-70.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 61,630 hrs · 29,994 cycles

DURING SCHEDULED C-11 CHECK WHILE PERFORMING NR 2030, DURING THE PEELING UP OF THE LT HORIZONTAL STABILIZER'S FRONT SPAR WEB, FOUND CLIPS CRACKED AT HSS199 UPPER AND HSS199 LOWER. REPAIRED BY REPLACEMENT ACCOMPLISHED IAW SMP583, 51-60 AND 51-70.

Part: ANGLE — CRACKED (NR 4 NACELLE) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND NR 4 NACELLE FIREWALL ASSY INBD SIDE WITH A CRACKED ATTACH ANGLE AND WEB AT CLAMSHELL DOOR AFT HINGE ATTACH POINTS. REPAIR TO WEB AND ANGLE ACCOMPLISHED IAW MEA 382-54-13-045.

Part: FRAME — CRACKED (BS 814) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3, FOUND CRACKED FRAME AT FS 814, LBL 61, WL 278. REPAIRED IAW SRM 51-70 AND FIG 51-140-21.

Part: SKIN — CRACKED (BS 245) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND CRACKED LONGERON AND SKIN ABOVE CREW DOOR, FS 245 WL 200, LBL 75. LONGERON REPLACED IAW SMP583, 51-70. SKIN REPAIRED IAW SMP583, FIG 51-140-12.

Part: BULKHEAD — CRACKED (BS 165) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND CRACKS IN PRESSURE BULKHEAD BS 165, LBL 70, WL 165 TO WL 170 . REPAIRED IAW SRM FIG 53-30-17.

Part: FRAME — CRACKED (BS 814) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3, FOUND FRAME CRACKED AT FS 814, WL 278, RBL 61. REPAIRED IAW SRM 51-70 AND FIG 51-140-21.

Part: FRAME — CRACKED (BS 814) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND FRAME CRACKED AT FS 814, WL 278, RBL 61. REPAIRED IAW SRM 51-70 AND FIG 51-140-21.

Part: SKIN — CRACKED (TAILCONE) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND TAILCONE LOWER SKIN PANEL CRACKED AT FS 1163, RBL 12, WL 278. REPAIRED IAW SRM FIG 51-140-12.

Part: FRAME — CRACKED (BS 814) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND CRACKED FRAME AT FS 814, LBL 61, WL 278. REPAIRED IAW SRM 51-70 AND FIG 51-140-21.

Part: SKIN — CRACKED (TAILCONE) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND TAIL CONE LOWER SKIN PANEL CRACKED AT FS 1163, RBL 12, WL 278. REPAIRED IAW SRM FIG 51-140-12.

Part: LONGERON — CRACKED (BS 245) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND CRACKED LONGERON AND SKIN ABOVE CREW DOOR, FS 245 WL 200, LBL 75. LONGERON REPAIRED IAW SRM 51-70. SKIN REPAIRED IAW SMP583, FIG 51-140-12.

Part: BULKHEAD — CRACKED (BS 165) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND CRACKS IN FUSELAGE PRESSURE BULKHEAD AT FS 165, LBL 70, WL 165 TO 170, INT BATTERY BOX AREA. REPAIRED IAW SRM FIG 53-30-17.

Part: ANGLE — CRACKED (NR 4 NACELLE) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3, FOUND NR 4 ENGINE AFT NACELLE FIREWALL ASSY INBD SIDE HAD CRACKED ATTACH ANGLE AND WEB AT CLAMSHELL DOOR AFT HINGE ATTACH POINTS. REPAIRED TO WEB AND ANGLE ACCOMPLISHED IAW MEA 382-54-13-045.

Part: FRAME — CRACKED (BS 968) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND FRAME CRACKED AT FS 968, WL 278, LBL 61. REPAIRED IAW SRM 51-60 AND FIG 53-50-06.

Part: FRAME — CRACKED (BS 968) · airframe 61,065 hrs · 29,602 cycles

DURING SCHEDULED B-3 CHECK, FOUND FRAME CRACKED AT FS 968, WL 278, LBL 61. REPAIRED IAW SRM 51-60 AND FIG 53-50-06.

Part: SWITCH — DEFECTIVE (RT MLG) · airframe 60,890 hrs · 29,475 cycles

DURING SCHEDULED FLIGHT, AFTER T/O, GEAR HANDLE RAISED, RT MLG INDICATED IN-TRANSIT, HANDLE LIGHT ON, LT MAIN AND NOSE GEAR INDICATED GEAR UP. REPLACED RT HAND MLG UPPER LIMIT SWITCH IAW CHAP. 32-33 / LP 38142.

Part: GUSSET — CRACKED (BS 858) · airframe 60,846 hrs · 29,441 cycles

DURING SCHEDULED A-CHECK, FOUND UPPER RT STANTION GUSSET FS 858, WL 256.5, BL 61.62R CRACKED. R & R RT STANTION GUSSET FITTING IAW SMP583, FIG 51-70-04 AND DWG 343194/LP 38246.

Part: HOUSING — FAILED (NR 1) · airframe 60,512 hrs · 29,154 cycles

DURING DESCENT, NR 1 ENGINE FLAMED OUT, THEN RELIT, FOLLOWED BY 105 PERCENT RPM SHUTDOWN IAW QRH PROCEEDURES. R & R VALVE HOUSING ASSY IAW HN61135 LP 38080.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 60,371 hrs · 29,019 cycles

DURING SCHEDULED B-2 CHECK, FOUND CRACKS IN FWD PRESSURE BULKHEAD IN NLG WHEEL WELL RBL 70, WL 171, FS 165 JUST BELOW NLG JACK PAD FITTINGS. REPAIR ACCOMPLISHED IAW SMP 583 51-71 AND FIG 51-140-17.

Part: SKIN — DENTED (BS 737) · airframe 60,371 hrs · 29,019 cycles

DURING SCHEDULED B-2 CHECK, FOUND FUSELAGE SKIN DENTED FS 737 RBL 60 WL 126. REPAIR ACCOMPLISHED IAW SMP 583, FIG 51-140-12.

Part: SKIN — GOUGED (BS 297) · airframe 60,371 hrs · 29,019 cycles

DURING SCHEDULED B-2 CHECK, FOUND FUSELAGE BELLY SKIN GOUGED FS 297, WL 126, LBL 20. REPAIR ACCOMPLISHED IAW SMP 583 FIG 51-140-12.

Part: SKIN — DAMAGED (RUDDER) · airframe 60,371 hrs · 29,019 cycles

DURING SCHEDULED B-2 CHECK, FOUND HOLE IN T/E OF RUDDER SKIN DUE TO LIGHTNING STRIKE AT RUDDER STA 223. REPAIR ACCOMPLISHED IAW SMP 583 FIG 51-140-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,371 hrs · 29,019 cycles

DURING SCHEDULED B-2 CHECK, CONCURRENT WITH WINDOW REPLACEMENT, FOUND PILOT'S SIDE WINDSHIELD UPPER AFT CORNER AREA OF AIRFRAME SKIN HAS CRACKED BETWEEN FASTENER HOLES. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-12-113.

Part: SKIN — DENTED (BS 800) · airframe 59,932 hrs · 28,693 cycles

DENT RT AFT FUSELAGE, FS 800, WL 146, RBL 64. REPAIRED RT AFT FUSELAGE SKIN IAW SMP 583, FIGURE 51-140-12.

Part: BULKHEAD — CRACKED (BS 902) · airframe 59,675 hrs · 28,492 cycles

DURING SCHEDULED B1 INSPECTION, FOUND INTERIOR FUSELAGE BULKHEAD INBD CAP CRACKED AT FS 902, WL 200, LBL 63. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-22.

Part: BULKHEAD — CRACKED (BS 847) · airframe 59,675 hrs · 28,492 cycles

DURING SCHEDULED B1 INSPECTION, FOUND INTERIOR FUSELAGE BULKHEAD FLANGE CRACKED AT FS 847, WL 200, LBL 72. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-19.

Part: ANGLE — PUNCTURED (PAX DOOR) · airframe 59,356 hrs · 28,156 cycles

A .2500 INCH PUNCTURE IN CREW DOOR FRAME SEAL ANGLE AT FS 205 WL 159, LBL 72. REPAIRED IAW MEA 382-53-12-035, LP 31902.

Part: SKIN — CRACKED (BS 630) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND RT CABIN SKIN CRACKED AT SPLICE BAR FITTING ATTACHMENT BOLT HOLE FS630, WL256, RBL63. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-11-053.

Part: STIFFENER — CRACKED (BS 935) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT UNDER, FOUND LT AFT FUSELAGE INTERIOR OVERHEAD STIFFENER CRACKED AT FS 935 LBL 15. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-07.

Part: BRACKET — CRACKED (WATER SEP) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CARGO AIR COND DUCT ASSY WATER SEPARATOR AIR EXIT MOUNTING BRACKET CRACKED. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-21-11-046.

Part: SKIN — CRACKED (RT WING) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT OTBD WING LOWER FWD PLANK NR 3 CRACKED AT FS522-533, ROWS 3.7. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-11-056.

Part: SKIN — DENTED (BS 837-869) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT AFT FUSELAGE EXTERIOR SKIN DENTED AND SCRATCHED BEYOND LIMITS FS837-869, WL175-200, LBL65. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 & 51-70.

Part: FRAME — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN OVERHEAD RING SEGMENT AT FS 477, LBL 18, WL 282. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-70.

Part: ATTACH ANGLE — CRACKED (BS 1041) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT AFT FUSELAGE BULKHEAD TO HORIZONTAL STABILIZER ATTACH ANGLE CRACKED FS1041, WL256, RBL64. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583, CHAPTER 51-70.

Part: SKIN — CRACKED (BS 677) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT FUSELAGE SKIN CRACKED AT FS 677, WL 200, RBL 85. REPAIR ACCOMPLISHED IAW LKHEED SMP583 FIG 51-140-12.

Part: INTERCOSTAL — WARPED (BS 797E-817E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND BELLY INTERCOSTAL BEAM ASSY WARP FS 797E TO FS 817E, WL 125-146, LBL 10 TO RBL 10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CHAPTER 51-60 & 51-70.

Part: FRAME — DAMAGED (BS 437) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT CABIN RING FRAME CRACKED EXCESS DOUBLER HOLES AT FS437, WL283, RBL20. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-21.

Part: BULKHEAD WEB — CRACKED (BS 770) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND AFT FUSELAGE INTERIOR RT STRUT BULKHEAD REPAIR DOUBLER CRACKED FS770, WL170-178, RBL72 / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 FIG 53-50-14 & CHAP 51-60, 51-70.

Part: DOUBLER — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND CRACK ON LT DOUBLER CONNON TO LONGERON AT FS 477, BL 20, WL 285, HOLE Q. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CH 51-60 & 51-70.

Part: DOUBLER — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND CRACK ON RT DOUBLER COMMON TO LONGERON AT FS 477, RBL 20, WL 285 HOLE E. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAP 51-60 & 51-70.

Part: SKIN — DAMAGED (CENTER WING) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT OTBD WING LOWER NR 3 PLANK TO RAINBOW FITTING NEXT OVERSIZE PIN RIVET FS 572, LOWS 5, WL 256. REPAIR ACCOMPLISHED IAW MEA 382-57-11-044.

Part: FRAME — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACK IN CABIN OVERHEAD LT RING SEGMENT FS 477, LBL 22, WL 282. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CH 51-60 & 51-70.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT MAIN WHEEL WELL BULKHEAD WEB CRACKED FS 597-617, WL 175-200, LBL 62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CHAP 51-60 & 51-70.

Part: FLOORBEAM — CORRODED (BS 277) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND BELLY FLOORBEAM LOWER CAP CORROSION EXCEEDING LIMITS FS 277, WL 126, BL 0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-60 & 51-70.

Part: TENSION TIE — CRACKED (BS 617) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACK ON LT TENSION TIE FITTING FS 617, WL 256, LBL 61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-70.

Part: ANGLE — CRACKED (BS 515) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT MWW CHINE ANGLE CRACKED FS 515, WL 140, RBL 61. REPAIR ACCOMPLISHED IAW SMP583, FIG 53-40-27.

Part: FORMER — DAMAGED (BS 477-517) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN OVERHEAD FORMER (X4) WITH CORROSION AND ELONGATED HOLES FS 477-517 AREAS, LBL 25-RBL 25, WL 285. REPAIR BY REPLACMENT ACCOMPLISHED IAW SMP583 CHAP 51-60 & 51-70.

Part: BULKHEAD WEB — CRACKED (BS 880) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT AFT FUSELAGE INTERIOR BULKHEAD WEB CRACKED AT FS 880, RBL 68, WL 190. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAP 51-60 & 51-70.

Part: ANGLE — DENTED (BS 630) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND SHARP DENT BEYOND LIMITS AT LT CHINE CAP FS 630, LBL 55, WL 146. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-28.

Part: BRACKET — CRACKED (BS 93) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT NLG FWD DOOR HINGE BRACKET CRACKED AT FS 93, WL 150, LBL 20. REPAIR ACCOMPLISHED IAW SMP583 CHAPTER 51-70.

Part: BEAM — CRACKED (BS 517) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACKED LT UPPER MWW ARMPIT PANEL ATTACH BEAM (WING TO FAIRING FORMER) AT FS 517, LBL 85, WL 236. REPAIR ACCOMPLISHED IAW MEA 382-57-051.

Part: ANGLE — CORRODED (BS 800E-817E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN UNDERFLOOR RT CHINE ANGLE FITTING WITH EXFOLIATION CORROSION & MULTIPLE ELONGATED FASTENER HOLES FS800E-817E, WL142, RBL61. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583 CHAP 51-70.

Part: ATTACH ANGLE — CRACKED (BS 517) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT MWW OVERHEAD BULKHEAD TO BEAM ATTACH ANGLE CRACKED AT FS 517, WL 202, LBL 69. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: LONGERON — DAMAGED (BS 436) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT FUSELAGE UPPER LONGERON WITH MIS-DRILLED DOUBLER HOLES AT FS436, WL257, RBL62. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-11-065.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT UPPER INBD FLAP SKIN DENTED AND OIL CANNING WS108 TO 192. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: FRAME — CRACKED (BS 817E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT AFT FUSELAGE INTERIOR RING SEGMENT CRACKED FS 817E, WL 158, LBL 63. REPAIR ACCOMPLISHED IAW SMP583, FIG 53-40-46.

Part: INTERCOSTAL — DAMAGED (BS 777E-797E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND BELLY INTERCOSTAL CAP THICKNESS BEYOND LIMITS FS777E-797E, WL140, RBL10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: DUCT — CRACKED (BS 183) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND AIR COND AIR INTAKE DUCT FLANGE CRACK AT FS 183, WL 175. REPAIR WELD ACCOMPLISHED IAW MEA 382-21-11-057.

Part: PANEL — CRACKED (LT WING) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND LT OUTER WING UPPER NR 2 & NR 3 PANELS CRACKED AT ROW 5. REPAIR ACCOMPLISHED IAW MEA 382-57-11-039.

Part: BULKHEAD WEB — DAMAGED · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT CABIN UPPER BULKHEAD PRESSURE WEB WITH EXCESS WIRE LINE ACCESS HOLES AT FS 597-617, WL 270-286, RBL 61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CRACKED (RT WING) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND RT OUTER WING LOWER NR1 PLANK CRACKS AT OWS3, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-11-056.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT INBD FLAP LOWER L/E SKIN CRACKED AT FS 612 TO FS 617, LCWS 104 TO LCWS 112, WL 258. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12.

Part: ANGLE — CORRODED (RT MLG WW) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT CHINE ANGLE CORROSION BEYOND LIMITS FS797E-817E, WL144, RBL61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LKHEED SMP583, CHAPTER 51-60 & 51-70.

Part: INTERCOSTAL — CORRODED (BS 807E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND BELLY INTERCOSTAL BEAM LOWER CAP WITH EXFOLIATION CORROSION AT FS807E, LBL10, WL125. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — DENTED (CARGO DOOR) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CARGO DOOR LOWER SURFACE WITH DENTS BEYOND LIMITS ON EXISTING PATCHES FS 1001 TO 1012.5 RBL 5 TO RBL 16.5. REPAIR ACCOMPLISHED IAW SMP 583 FIG 51-140-12.

Part: SKIN — GOUGED (BELLY) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND BELLY SKIN PITTING CORROSION AND DEEP SCRATCHES WITH RIVET HEAD DAMAGE AT FS 777E TO FS 817E LBL 61 TO RBL 61, WL 126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-60 & 51-70.

Part: BULKHEAD WEB — CRACKED (BS 594-602) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT UPPER MAIN WW BULKHEAD WEB WITH CRACKS AT FASTENER HOLES FS 594-602, RBL 61.5, WL 263. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CHAPTER 51-60 & 51-70.

Part: STIFFENER — DAMAGED (BS 477-517) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN OVERHEAD STIFFENERS (X8) WITH ELONGATED HOLES FS477-497 & FS497-517 AREAS, LBL34-RBL34 & LBL46-RBL46, WL285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: BRACKET — CRACKED (BS 93) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT NLG FWD DOOR HINGE BRACKET CRACKED AT FS 93, RBL 20, WL 150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-70.

Part: BULKHEAD WEB — CRACKED (LT MLG WW) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN LT MAIN WHEEL WELL BULKHEAD WEB CRACKED AT FS 516 TO FS 529, WL 144 TO WL 250, LBL 61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: TENSION TIE — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACK ON RT TENSION TIE FITTING FS 477, RBL 61, WL 256. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-70.

Part: PLATE — CRACKED (CARGO DOOR) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RAMP DOOR REAR BULKHEAD (FAIRING) RUBBING PLATE DENTED SCRATCHED AND CRACKED AT RS8 TO 8.3, LBL61 TO RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-70.

Part: FLOORBEAM — CORRODED (BS 217) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND EXFOLIATION CORROSION AT FLT DECK FLOORBEAM CAP FS 217, WL 200, LBL 61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-70.

Part: CAP — CRACKED · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RAMP DOOR BULKHEAD UPPER CAP CRACKED RS10.0, LBL58. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 & 51-70.

Part: SKIN — WARPED (BS 869-902) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND AFT FUSELAGE EXTERIOR SKIN WARP WITH EXISTING REPAIR PATCHES AT FS 869 TO FS 902, WL 190 TO WL 205, RBL 62. REPAIR ACCOMPLISHED IAW SMP 583, CHAPTER 51-70.

Part: SKIN — DENTED (BS 245-291) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT FUSELAGE EXTERIOR SKIN WITH DENTS & SCRATCHES BEYOND LIMITS AND PITTING CORROSION AT FS 245 TO 291, WL 160 TO WL 240. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CH 51-70.

Part: SKIN — GOUGED (BS 902-935) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT AFT FUSELAGE EXTERIOR SKIN WITH MULTIPLE EXISTING PATCHES AND DEEP SCRATCHES AT FS 902 TO FS 935, WL 180 TO WL 200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — DAMAGED (BS 437-457) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT FUSELAGE SKIN SPLICE WITH MISDRILLED HOLES FS437-457, WL246, RBL63.5. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-11-081.

Part: FRAME SPLICE — CORRODED (BS 617) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN RING SEGMENT SPLICE CORROSION FS617, WL283, RBL20. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583 CHAPTER 51-70.

Part: FORMER — DAMAGED (BS 497-517) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN OVERHEAD FORMER (X2) WITH SURFACE CORROSION, ELONGATED HOLES, AND WARPED FS 497-517, LBL 18-RBL 18, WL 185. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-60 & 51-70.

Part: SKIN — CORRODED (ZONE 100) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT FUSELAGE EXTERIOR SKIN WITH MULTIPLE EXISTING PATCHES, PITTING CORROSION, AND OUT OF LIMIT DENTS AND SCRATCHES AT FS 777E TO FS 817E, WL 140 TO WL 245, LBL 74. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-11-062.

Part: ANGLE — CRACKED (BS 737E-817E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT CHINE ANGLE CRACKED AND CORRODED AT FS 813E-817E, WL140, LBL62. REPAIR BY REPLACEMENT. ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND CRACK IN LEFT SKIN COMMON TO LONGERON FS 477, LBL 20, WL 285 HOLES P & V. REPAIR ACCOMPLISHED IAW MEA 283-53-11-052.

Part: DOUBLER — CRACKED (BS 168) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT FWD SKIN INNER DOUBLER CRACKED FS168, WL175, RBL70. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LKHEED SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — WARPED (BS 902-936) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT. FOUND RT AFT FUSELAGE EXTERIOR SKIN WARP WITH MULTIPLE PATCHES AT FS902 TO FS936, WL178 TO WL224, RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-60 & 51-70.

Part: BEAM — CRACKED (BS 588) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT MAIN WHEEL WELL BEAM CRACKED FS588, WL198-200, LBL61. REPAIR ACCOMPLISHED IAW LKHEED SMP583, FIG 53-40-51.

Part: FLOORBEAM — CORRODED (BS 257) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND EXFOLIATION CORROSION OF CABIN FLOORBEAM UPPER CAP AT FS 257, LBL 20 & LBL 30, WL 146 TIE-DOWN POINT. REPAIR ACCOMPLISHED IAW SMP583, FIG 51-140-22.

Part: ATTACH ANGLE — CORRODED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND ATTACH ANGLE CORROSION AND FASTENER HOLE ELONGATED FS 477, LBL 24-60, WL 280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-60 & 51-70.

Part: BULKHEAD WEB — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT UPPER MWW FWD BULKHEAD WEB CRACKED AT FS 477, WL 234, LBL 76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CH 51-60 & 51-70.

Part: FLOORBEAM — CRACKED (BS 817E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND FLOORBEAM WEB CRACKED AND WITH EXFOLIATION CORROSION, FS817E, WL125-146, LBL26 TO RBL26. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT MAIN WHEEL WELL CHINE ANGLE CRACKED AT FS597 BEAM ATTACHMENT FS598, WL140, LBL61.5. REPAIR ACCOMPLISHED IAW LKHEED SMP583, FIG 53-40-27.

Part: CAP — CORRODED (BS 817E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND FLOOR END BULKHEAD LOWER CAP DEEP PITTING CORROSION FS 817E, WL 141, LBL 61.5 TO RBL 61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-70.

Part: BRACKET — CRACKED (AIR DUCT) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10, CHECK AND CENTER WING REPLACEMENT, FOUND CARGO AIR COND RECIRCULATING AIR UPPER DUCT ASSY MOUNTING BRACKET CRACKED. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-21-11-045.

Part: BRACKET — CRACKED (CABIN AIR) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CARGO COMPARTMENT AIR COND AUX VENT INLET DUCT ASSY BRACKET CRACKED. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-21-11-047.

Part: SKIN — CORRODED (BS 165-196) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT FWD FUSELAGE SKIN SURFACE CORROSION AND SCRATCH MARKS FS 165 TO FS 196, WL 139 TO WL 195. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-60 & 51-70.

Part: BEAM — CRACKED (BS 577) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACKS ON RT MLG BEAM FS 577, WL258, RBL61, HOLE F. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-11-064.

Part: SKIN — CRACKED (BS 618) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT FUSELAGE SKIN CRACKED AT LONGERON & RING SEGMENT SPLICER ATTACHMENT AREA FS 618, LBL 21, WL 285. REPAIR ACCOMPLISHED IAW MEA 382-53-11-048.

Part: BULKHEAD — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN OVERHEAD LT UPPER BULKHEAD FLANGE WITH A CRACK AT FS 477, LBL 24, WL 285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CH 51-60 & 51-70.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT MAIN WHEEL WELL CHINE ANGLE WARP AND PITTING CORROSION FS588-597, WL144, LBL61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, FIG 53-40-27.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT INBD FLAP UPPER SKIN CENTER PANEL SURFACE CORROSION, AND CRACK WS108-192. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, FIG 57-70-01.

Part: DOUBLER — CRACKED (BS 439-477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN UPPER SKIN RT REINFORCE DOUBLER CRACKED AT SPLICE BAR FITTING ATTACHMENT BOLT HOLES FS465-466, WL256, RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LKHEED SMP583, CHAPTER 51-60 & 51-70.

Part: SEAT TRACK — WORN (BS 165-185) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND FLT DECK FE SEAT TRACKS (LT & RT) FWD & AFT TRAVEL METERING HOLES WORN BEYOND LIMITS. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CHAPTER 51-70.

Part: ATTACH ANGLE — CRACKED (BS 617) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN OVERHEAD PRESSURE FAIRING ATTACH ANGLE CRACKED AT FS 617, RBL 61, WL 285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: BEAM — CRACKED (BS 588) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND RT MLG BEAM CRACK FS 588, RBL 61, WL 258, HOLE F. REPAIR ACCOMPLISHED IAW MEA 382-53-11-049.

Part: BULKHEAD — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACKED CABIN RT UPPER BULKHEAD FLANGE FS 477, RBL 24, WL 285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: FITTING — CORRODED (CENTER WING) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT OTBD REAR LOWER CORNER FITTING DEEP PITTING CORROSION AT MAIN HOLE & NODE FACE, FS 597, WL 258, OWS0-10R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-60 & 51-70.

Part: FLOOR SUPPORT — CORRODED (BS 181-196) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND FLT DECK FLOOR SUPPORT TEE ANGLE EXFOLIATION CORROSION AT FS 181 TO FS 196, RBL 40, WL 200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-70.

Part: PANEL — CRACKED (RT WING) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND RT OUTER WING UPPER NR 2 PANEL CRACKS AT OWS5R, WL285. REPAIR ACCOMPLISHED IAW MEA 382-57-11-038.

Part: MANIFOLD — CRACKED (MLG WW) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT & RT MWW MANIFOLDS (X3) CRACKED AT FS 507, LBL 61.5 & RBL 61.5, WL 142-148 AND FS 532, RBL 61.5, WL 142-148. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAP 51-70.

Part: BULKHEAD — CORRODED (BS 1038) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND AFT FUSELAGE CARGO DOOR SEAL BUMPER VERTICAL BULKHEAD SKIN WITH PITTING CORROSION AT FS 1038, LBL 60 TO RBL 60, WL 256. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — GOUGED (BS 297E-345E) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT UNDER, FOUND BELLY SKIN WITH DEEP STONE GOUGES, DENTS, AND SURFACE CORROSION AT FS 297E TO FS 345E, LBL 61.5 TO RBL 61.5, WL 126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-60 & 51-70.

Part: SKIN — CRACKED (BS 477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACKS ON RT SKIN, COMMON TO LONGERON FS 477 RBL 20, WL 285 HOLES F, G, & H. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CH 51-60, 51-70.

Part: BULKHEAD WEB — CRACKED (BS 1138) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACKED HORIZONTAL STABILIZER T/E BULKHEAD WEB FS1138, WL256, LBL40-RBL40. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAP 51-60 & 51-70.

Part: TENSION TIE — CRACKED (BS 617) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CRACK ON RT TENSION TIE FITTING FS 617, WL 256, LBL 61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-70.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CARGO DOOR REAR BULKHEAD STIFFENER CRACKED AT FS1041, LBL30, WL268-275. REPAIR BY REPLACEMENT ACCOMPLISHED IAW CHAPTER 51-60 & 51-70.

Part: FITTING — DAMAGED (BS 497) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND CABIN UPPER BULKHEAD TO ATTACH ANGLE FITTING WITH ELONGATED RIVET HOLES FS 497, WL 256, RBL 61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-70.

Part: SKIN — DAMAGED (BS 418-477) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND FUSELAGE UPPER SKIN DRILLED WITH EXCESS DOUBLER HOLES FS436, WL257, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 & 51-70.

Part: SKIN — DENTED (BS 291-337) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT FUSELAGE EXTERIOR SKIN WITH DENTS & SCRATCHES BEYOND LIMITS AT FS 291 TO 337, WL 160 TO WL 236. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CH 51-70.

Part: SKIN — DENTED (BS 617-657) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RT AFT MWW LOWER FAIRING SKIN WITH DENTS AND SCRATCHES BEYOND LIMITS AND CORROSION AT FS 617 TO FS 657, RBL 40 TO RBL 95, WL 135 TO WL 141. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: SKIN — CRACKED (BS 627) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT FOUND CRACK ON RT SKIN COMMON TO LONGERON AT FS 627, WL258, RBL61, HOLE GG. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-11-053.

Part: SKIN — DENTED · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND RAMP DOOR PEDESTAL FWD FAIRING WITH DENTS AND MULTIPLE EXISTING REPAIR PATCHES. REPAIR ACCOMPLISHED IAW SMP583, CHAP 51-70.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT HORIZONTAL STABILIZER L/E LOWER SKIN CRACKED, HSS 220L, WL 258. REPAIR ACCOMPLISHED IAW MEA 382-55-11-069.

Part: SKIN — GOUGED (BS 337-377) · airframe 58,982 hrs · 27,812 cycles

DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND BELLY SKIN WITH MULTIPLE DEEP CUTTING MARKS, RIVET HEAD DAMAGE, DENTS, AND SURFACE CORROSION AT FS 337 TO FS 377, LBL 61 TO RBL 61, WL 126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CHAP 51-60 & 51-70.

Part: PLATE — GOUGED (LT WING TE FLAP) · airframe 58,401 hrs · 27,496 cycles

DURING SCHEDULED B-3 CHECK, FOUND LT INBD FLAP INBD END PLATE GOUGED FLAP STA 1, HSS45L, CWS81L. REPAIR ACCOMPLISHED IAW MFG SMP 583, FIG 51-140-20.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 58,401 hrs · 27,496 cycles

DURING SCHEDULED B-3 CHECK, FOUND HORIZONTAL STABILIZER WEB CRACKED AT FS 1125, HSS 45L, WL 277. REPAIR ACCOMPLISHED IAW MFG SMP 583, FIG 51-140-17.

Part: WINDOW FRAME — CRACKED (BS 117) · airframe 58,401 hrs · 27,496 cycles

DURING SCHEDULED B-3 CHECK IAW FOUND LT CLEAR VISION WINDOW TOP FRAME CRACKED AT FS 117, LBL 35, WL 251.5. REPAIR ACCOMPLISHED IAW SMP 583 FIG 53-30-25. NR 2-5-3.

Part: SKIN — DENTED (FUSELAGE) · airframe 57,724 hrs · 27,106 cycles

DURING SCHEDULED B-2 CHECK PER JOB CARD HB5301, FOUND DENT IN FUSELAGE LOWER SKIN AT FS 302, WL 127, RBL 21.5. REPAIRED IAW LOCKHEED SMP583 FIG 51-140-10.

Part: PANEL — CORRODED (RT MLG WW) · airframe 57,724 hrs · 27,106 cycles

DURING SCHEDULED B-2 CHECK PER JOB CARD HB3200, FOUND RT MLG WHEEL WELL PANEL CORRODED AT FS 557, WL 206, RBL 61. REPAIRED IAW LAC MEA 382-53-10-050.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 57,517 hrs · 27,059 cycles

DURING SCHEDULED A CHECK FOUND CRACK ON PRESSURE SEAL PANEL AFT OF CARGO DOOR HINGE FS 1038, LBL 5-26, WL 271.5. REPLACED PRESSURE PANEL IAW LOCKHEED SMP583 CHAP 51-10 PAGE 3 PARA G (DWG 339776).

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 57,034 hrs · 26,903 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB5301 FOUND CENTER FUSELAGE ATTACH FITTING CRACKED AT FS 617, WL 260, LBL 61. REPAIR ACCOMPLISHED BY REPLACING FITTING IAW LOCKHEED SRM SMP583 CH 51-60 & 51-70.

Part: FORMER — CRACKED (FUSELAGE) · airframe 57,034 hrs · 26,903 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB5302 FOUND FORMER CRACKED IN CENTER CARGO COMPARTMENT AT FS 617, WL 272, RBL 40. REPAIR ACCOMPLISHED IAW LOCKHEED SRM SMP583 FIG 51-140-20.

Part: ANGLE — CRACKED (CARGO BAY) · airframe 57,034 hrs · 26,903 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB5302 FOUND CENTER CARGO COMPT AFT PRESSURE FAIRING ANGLE CRACKED AT FS 597, WL 265, BL 0. REPAIR ACCOMPLISHED IAW LOCKHEED SRM SMP583 FIG 51-140-23.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 57,034 hrs · 26,903 cycles

DURING SCHEDULED B1 CHECK PER JOB CARD HB5302 FOUND U-CHANNEL CRACKED IN CARGO COMPARTMENT AT FS 617, WL 280. RBL 20. REPAIR ACCOMPLISHED IAW LOCKHEED SRM SMP583 FIG 51-140-20.

Part: SKIN — WARPED (BS 832) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND AFT FUSELAGE EXTERIOR SKIN WARPED AT FS 832, WL 180, LBL 85. / REPAIRED IAW SRM SMP583 FIG 51-140-10.

Part: FITTING — CRACKED (BS 245) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313, FOUND UNDERDECK SNATCH-BLOCK FITTING CRACKED AT FS 245, WL 146, LBL 22. REPLACED FITTING IAW SRM SMP583 51-60 & 51-70.

Part: FRAME — CRACKED (BS 588) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5314, FOUND UNDERFLOOR FRAME STRUCTURE CRACKED AT FS 588, WL 130, RBL 20. REPAIRED IAW SRM SMP583 FIG 51-140-21.

Part: PLENUM — CRACKED (NR 2 NACELLE) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC7204, FOUND NR 2 ENGINE AFT NACELLE PLENUM CRACK AT FS 535, WL 250.5, PP LBL9.5. REPAIRED IAW LAC MEA 382-54-09-027.

Part: FITTING — CRACKED (RAMP DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD H5211, FOUND RAMP DOOR LATCH ACTUATOR FITTING CRACKED AT DOOR STATION 6, BL0. REPLACED FITTING IAW SRM SMP583 51-60.

Part: WEB — CRACKED (CARGO RAMP) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR INTERCOSTAL LOWER BEAM WEBS (2EA) & CAPS (2EA), CRACKED AT RS6.1, WL 152, BL 0. FABRICATED AND REPLACED CAPS & WEBS IAW SRM SMP583 51-60 & 51-70.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5301, FOUND LT FUSELAGE EXTERIOR CHINE ANGLE EXFOIATION CORROSION AT FS 297E, WL 141, LBL 61 / REPAIRED IAW LAC MEA 382-53-09-025.

Part: INTERCOSTAL — BROKEN (RAMP DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR INTERCOSTAL UPPER BEAM BROKEN AT RS6, BL 0. FABRICATED AND REPLACED BEAM WEB AND ANGLE IAW SRM SMP583 51-60 & 51-70.

Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313, FOUND CARGO DOOR INTERIOR BULKHEAD STIFFENER CRACKED AT FS 1012, RBL 20. REPAIRED BY FABRICATING AND PREPLACING STIFFENER IAW SRM SMP583 51-60 & 51-70.

Part: GUSSET — CRACKED (CARGO DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313, FOUND CARGO DOOR INTERIOR GUSSET PLATE (DOUBLER) CRACKED AT FS 990, RBL 60. FABRICATED AND REPLACED GUSSET PLATE IAW SRM SMP583 CHAPTER 51-60 & 51-70.

Part: FRAME — WARPED (CARGO RAMP) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR PEDESTAL INNER FRAME LOWER CAP WARP AT RS8.5 TO RS10, LBL 12 TO RBL 12. FABRICATED AND REPLACED CAPS IAW SRM SMP583 51-60 & 51-70.

Part: GUSSET — CRACKED (CARGO DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5212, FOUND CARGO DOOR INTERIOR BULKHEAD TO LOWER SKIN GUSSET PLATES CRACKED AT FS 880, LBL 60 AND FS 880, RBL 60. FABRICATED AND REPLACED GUSSET PLATES IAW SRM SMP583 51-60 & 51-70.

Part: ANGLE — BROKEN (CARGO DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND CARGO DOOR INTERIOR BULKHEAD LOWER ANGLE BROKEN AT FS 880, RBL 58. REPAIRED IAW SRM SMP583 FIG 51-140-23.

Part: SKIN — WARPED (CARGO DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND CARGO DOOR BOTTOM SKIN WARP AT FS 942, RBL 3. REPAIRED IAW SRM SMP583 FIG 51-140-12.

Part: BEAM — CRACKED (CARGO RAMP) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR TRANSVERSE BEAM CRACKED AT RS10, LBL 22. FABRICATED AND REPLACED BEAM IAW SRM SMP583 51-60 & 51-70.

Part: RIB — CRACKED (BS 743) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR RIB CRACKED AT FS 743, WL 145, RBL 66. REPAIRED BY FABRICATING AND REPLACING RIB IAW SRM SMP583 51-60 & 51-70.

Part: MANIFOLD — CRACKED (HYD SYSTEM) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5323, FOUND LT MAIN WHEEL WELL MANIFOLD CRACKED AT FS 492, WL 146, LBL 62. REPLACED MANIFOLD IAW SRM SMP583 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND CARGO DOOR INTERIOR BULKHEAD WEB CRACKED AT FS 880, RBL 61. FABRICATED AND REPLACED WEB IAW LOCKHEED SRM SMP583 CHAPTER 51-60 & 51-70.

Part: BULKHEAD — CRACKED (BS 497) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5315, FOUND LH CARGO COMPARTMENT BULKHEAD CAP CRACKED AT FS 946, WL 200, RBL 64. REPAIRED BY FABRICATING AND REPLACING CAP IAW SRM SMP583 51-60 & 51-70 .

Part: BULKHEAD — PUNCTURED (RT MLG WW) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313, FOUND RT WHEEL WELL BULKHEAD PUNCTURED AT FS 499, WL 157, RBL 61.5. / REPAIRED IAW LOCKHEED SRM SMP583 FIG 53-40-09.

Part: ANGLE — CORRODED (BS 297E) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5301, FOUND RH FUSELAGE EXTERIOR CHINE ANGLE STRESS CORROSION AT FS 297E, WL 141, RBL 61. REPAIRED IAW LAC MEA 382-53-09-026.

Part: SKIN — CORRODED (MLG POD) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HHC5321, FOUND RT MLG POD CENTER FAIRING CORROSION AT FS 617, WL 160-169, FABRICATED AND REPLACED SKIN IAW LAC MEA 382-53-06-045 R1.

Part: BULKHEAD — CRACKED (BS 836) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR BULKHEAD CRACKED AT FS 836, WL 185, RBL 66. REPAIRED IAW SRM SMP583 FIG 53-50-10.

Part: SKIN — DENTED (BS 717) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5301, FOUND AFT FUSELAGE SKIN DENTED AT FS717, WL146, LBL63. / REPAIRED IAW SRM SMP583 FIG 51-140-12.

Part: FRAME — CRACKED (BS 968) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5315, FOUND AFT FUSELAGE INTERIOR UPPER BULKHEAD FORMER CRACKED AT FS 968, WL 280, RBL 60. REPAIRED IAW SRM SMP583 FIG 51-140-21.

Part: SKIN — DENTED (BS 737E-777E) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5301, FOUND BELLY SKIN WITH MULTIBLE SCRATCHES / DENTS EXCEEDING LIMITS AT FS737E TO FS77E, LBL 61 TO RBL 61. REPLACED SKIN IAW SRM SMP583 51-60 & 51-70.

Part: PLENUM — CRACKED (NR 3 NACELLE) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC7204, FOUND NR 3 ENGINE AFT NACELLE PLENUM CRACKED AT FS 535, WL 255, PPBL0. REPAIRED IAW LAC MEA 382-54-09-028.

Part: BEAM — CRACKED (BS 497) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5324, FOUND RH UPPER W/W BOW BEAM O/B CAP CRACKED AT FS 497, WL 260, RBL 64. REPAIRED IAW SRM SMP583 FIG 53-10-12.

Part: WEB — CRACKED (RAMP DOOR) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR BULKHEAD WEB AND STIFFENER CRACKED AT DOOR STATION 6. FABRICATED AND REPLACED WEB AND STIFFENER IAW SRM SMP583 51-60 & 51-70.

Part: MANIFOLD — CRACKED · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5323, FOUND LT MAIN WHEEL WELL MANIFOLD CRACKED AT FS 607, WL 146, LBL 62. REPLACED MANIFOLD IAW SRM SMP583 FIG 51-70.

Part: ANGLE — DENTED (BS 380-386) · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD HC5313, FOUND LT CHINE CAP DENTED BEYOND LIMITS AT FS 380 TO FS 386, WL146, LBL 55. REPAIRED IAW SRM SMP583 FIG 53-40-28.

Part: MANIFOLD — CRACKED · airframe 56,382 hrs · 26,566 cycles

DURING SCHEDULED C-9 CHECK PER JOB CARD H5312, FOUND RT MAIN WW MANIFOLD CRACKED AT FS 492, WL 146, RBL 62. REPLACED MANIFOLD IAW SRM SMP583 51-70.

Part: STIFFENER — BENT (BS 792-803) · airframe 56,069 hrs · 26,503 cycles

DURING LOADING OF THE CARGO BAY, 3 FORE & AFT HORIZONTAL TUBULAR STIFFENERS AND 5 VERTICAL STIFFENERS WERE DAMAGED IN THE AREA OF FS 792-803, WL 249, RBL 0.0-38. REPAIRED BY REPLACING ALL DAMAGED STIFFENERS IAW SMP583 CHAPTER 51-10 PARAGRAPH G.

Part: CONTROL UNIT — FALSE ACTIVATION (NR 3 NACELLE) · airframe 55,831 hrs · 26,395 cycles

DURING DESCENT, CREW NOTED NUMBER 3 ENGINE FIRE WARNING LIGHT ANNUNCIATOR FLASHED. PRECAUTIONARY ENGINE SHUT DOWN PERFORMED. FIRE DETECTION CONTROL UNIT CHANGED FOR PRECAUTIONARY PURPOSE.

Part: HYDRAULIC LINE — LEAKING (NLG) · airframe 55,497 hrs · 26,238 cycles

DURING LANDING GEAR EXTENSION LOST THE UTILITY HYDRAULIC SYSTEM. REMOVED AND REPLACED LEAKING GEAR DOWN HOSE ON NLG RETRACTION CYLINDER, GEAR RETRACTIONS CARRIED OUT IAW SMP581 32-30, OPS AND LEAK CHECK GOOD.

Part: STANCHION — SCRATCHED (FS 770 WL 175) · airframe 55,006 hrs · 26,091 cycles

DURING POST FLIGHT INSPECTION, CREW NOTED A SCRATCHED STANCHION AT FS 770, WL 175. SCRATCH DETERMINED TO BE BEYOND SERVICEABLE LIMITS, REPAIRED STANCHION IAW SMP583 53-50-24.

Part: HOUSING — UNKNOWN (PROP VALVE) · airframe 54,498 hrs · 25,738 cycles

DURING CRUISE FLIGHT, CREW REPORTED NR 4 PROPELLER RPM OUT OF LIMITS. PERFORMED ENGINE SHUT DOWN IAW ESP. NR 4 PROPELLER VALVE HOUSING REPLACED IAW LACE JOB CARD HN61135, OPS CHECK GOOD.

Part: CONNECTOR — CORRODED (CROSSFEED VALVE) · airframe 54,057 hrs · 25,613 cycles

DURING CRUISE FLIGHT, NR 2 CROSSFEED VALVE FAILED IN THE CLOSED POSITION. NR 2 CROSSFEED VALVE SUBSEQUENTLY DEFERRED IAW MEL 28-4 CAT "C" DEFERRAL SP NR 2 COMPLIED WITH. CROSSFEED VALVE ELECTRICAL PLUG REMOVED AND BAGGED. VALVE OPENED MANUALLY AND LOCKWIRED IN THE OPEN POSITION ON LOG PAGE 27022, ITEM 2. WILL UPDATE COMPONENT INFORMATION WHEN IT BECOMES AVAILABLE. UPDATED INFORMATION IS AS FOLLOWS, FOUND CORRODED WIRE EYE TERMINAL AT POSITION "9" TB42B. REPAIR AND OPS CHECK IAW SMP581 28-22, LOG PAGE 28526 ITEM M1.

Part: MOUNT BRACKET — CRACKED (RT WING) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5712, FOUND RT OW LEADING EDGE DIFFUSER MOUNTING BRACKET P/N 351783 CRACKED OWS205-255R. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-029.

Part: MOUNT — CRACKED (NR 3 NACELLE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK, FOUND NR 3 ENGINE INBD TRUSS MOUNT DIAGONAL BRACE ATTACHMENT LUG CRACK. REPAIR ACCOMPLISHED BY REPLACING NR 3 ENGINE INBD TRUSS MOUNT IAW RELEVANT PARAGRAPHS OF SMP583 CHAP 54-30 AND FIG 54-30-06 SHEET 1, 2, 3, AND 5.

Part: MOUNT BRACKET — CRACKED (CARGO BAY) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC2111, FOUND CARGO AIR CONDITION AUX VENT DUCT MOUNTING BRACKET CRACKED. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-21-08-032.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND RT CABIN BULKHEAD CRACKED AT FS 597, WL280, RBL61.5. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-04-071 R1.

Part: FIRE SEAL — CRACKED (NR 2 ENGINE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC7201, FOUND NR 2 ENGINE FIRESEAL COLLAR ASSEMBLY FLANGE CRACKED. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-54-08-028.

Part: STRIKER — CORRODED (CARGO DOOR) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR FWD LEADING EDGE SEAL STRIKER EXFOLIATION CORROSION RS0, LBL50 TO RBL50. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING STRIKER IAW LAC MEA 382-52-08-034 AND DWG 353607.

Part: BULKHEAD — CRACKED (HORIZ STAB) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK, FOUND HORIZ STABILIZER REAR BHD CRACKED AT FS 1138, RBL 27. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17.

Part: RIB — CRACKED (RT WING) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC2811, FOUND RT AUX TANK OBD COMPARTMENT FWD LOWER RIB CAP CRACK AT RADIUS CWS141. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-08-027.

Part: SUPPORT — CORRODED (CARGO DOOR) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR LEADING EDGE WELL INTERGRANULAR CORROSION AT RS0.0, LBL62-RBL62, WL144. REPAIR ACCOMPLISHED BY REMOVING CORROSION AND REPLACING SUPPORTS P/N 353607-51, -52L, -53R IAW SMP583 CHAP 51-60 AND 51-70 AND DWG 353607.

Part: BULKHEAD — BUCKLED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND LT AFT FUSELAGE INTERIOR SIDE BHD BUCKLED AT FS 880, WL200, LBL66. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5324, FOUND RT MWW BULKHEAD FRAME CHAFED AT FS 477, WL176-200, RBL61.62-76. REPAIR ACCOMPLISHED BY REPLACING BULKHEAD IAW SMP583 CHAP 51-60 AND 51-70 AND DWG 370784.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK, FOUND COCKPIT FLOORBEAM EXFOLIATION CORROSION AT FS 196-216, WL196, LBL30. REPAIR ACCOMPLISHED BY CUTTING OUT CORROSION AREA AND SPLICED IAW SMP583 FIG 51-140-22.

Part: RIB — CRACKED (T/E FLAP) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5713, FOUND RT OBD FLAP RIB CRACKED AT ROWS 30. REPAIR ACCOMPLISHED IAW LAC MEA 382-27-08-024.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5711, FOUND LT OW LEADING EDGE DIFFUSER P/N 370911-11 SUPPORT BRACKET CRACKED AT OWS54. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-025.

Part: BEAM — CRACKED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5324, FOUND RT UPPER MWW ARMPIT PANEL BEAM CRACKED AT FS 522. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-021 AND MEA 382-53-08-022.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR UPPER BHD WEB CRACKED AT FS 1012, WL280, RBL6. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-71.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK, FOUND RT ELEVATOR INBD TRAILING EDGE SKIN CRACKED AT HSS52R. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12.

Part: FITTING — CORRODED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND RT CABIN TIE DOWN WELL CHINE CAP EXFOLIATION CORROSION AT FS 516, WL146, RBL59.5. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-54.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND FUSELAGE EXTERIOR UPPER SKIN STIFFENER CRACKED AT FS 1039, WL286, BL0.0. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING STIFFENER IAW SMP583 CHAP 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR FWD BHD WEB CRACKED AT RS0.0, WL143, BL0.0. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17.

Part: WEB — CRACKED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK, FOUND WEB CRACKED AT BOLT HOLE UPON REMOVAL OF RT WING ATTACH ANGLE AT FS 596, WL250, RBL61.5. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-026.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND RT MWW BHD STIFFENER CRACK AT FS 597-617, WL150, RBL62. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING STIFFENER IAW SMP583 CHAPTER 51-60 AND 51-70 AND DWG 345367.

Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5711, FOUND LT OW LEADING EDGE ANTI-ICING DIFFUSER SUPPORT BRACKET CRACKED P/N 351783 OWS205-255. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-029.

Part: CAP — CRACKED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR BULKHEAD INBD CAP CRACKED AT FS792, WL160, LBL66. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-019.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK, FOUND COCKPIT FLOORBEAM EXFOLIATION CORROSION AT FS 196, WL196, RBL30. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING SPLICE CAP IAW SMP583 FIG 51-60 AND 51-70 AND DWG 393863-1.

Part: SUPPORT — CRACKED (HORIZ STAB) · airframe 53,961 hrs · 25,591 cycles

DURING SCHEDULED C-8 CHECK PER JOB CARD HC5511, FOUND LT HORIZ STAB LE ANTI-ICING COMPENSATOR TANG SUPPORT CRACKED, P/N10265-12. WELDING REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-031.

Part: SKIN — DENTED (FS 142) · airframe 53,799 hrs · 25,487 cycles

DURING MAINTENANCE REVIEW A 4 INCH LONG DENT WAS NOTED IN NOSE WHEEL WELL SKIN AT FS 142, WL156, RBL66, REQUIRING MAJOR REPAIR. AIRCRAFT FERRIED TO ANC, REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-016.

Part: SKIN — CRACKED (FS 826) · airframe 53,653 hrs · 25,387 cycles

DURING SCHEDULED A-1 CHECK, PER JOB CARD HA1200, FOUND CRACKED SKIN AT FS 826, WL178, RBL64.5. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 ON LOG PAGE 28130 ITEM M4.

Part: WINDOW FRAME — CRACKED (FS 150) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND LT SIDE WINDOW FRAME CRACKED AT AFT LOWER CORNER (POST 5) FS150, WL233, LBL52. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-30-32.

Part: FITTING — CRACKED (FS 770) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND CABIN BHD TO SLOPING LONGERON TEE FITTING CRACKED AT FS 770, WL152, LBL62. REPAIR ACCOMPLISHED BY REPLACING TEE FITTING IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (FS 902) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR RT BULKHEAD WEB CRACKED AT FS902, WL260, RBL66. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-1.

Part: BULKHEAD — CRACKED (FS 617) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND LT MWW BHD WEB CRACKED AT FS 617, WL190, LBL73. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-10.

Part: BULKHEAD — CRACKED (FS 1012) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR LT BULKHEAD UPPER WEB CRACKED AT FS 1012, WL275, LBL80. REPAIR ACCOMPLISHED BY REPLACING WEB IAW SMP583 CHAPTER 51-60 AND 51-70.

Part: FRAME — CRACKED (FS 1012) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR LT SIDE BULKHEAD OUTBD CAP CRACKED AT FS 1012, WL275, LBL80. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-003.

Part: BEAM — CRACKED (FS577) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB5301, FOUND RT UPPER WHEEL WELL MLG FRAME OUTBD CAP CRACKED AT FS 577, WL230, RBL66. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-002.

Part: BEAM — CRACKED (FS 577) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK PER JOB CARD HB5301, FOUND RT UPPER WHEEL WELL MLG BEAM CRACKED AT FS 577, WL236, RBL64. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-001.

Part: BULKHEAD — CRACKED (FS 880) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND CABIN BULKHEAD WEB CRACKED AT FS 880, WL200, RBL66. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17.

Part: WINDOW FRAME — CRACKED (FS 150) · airframe 53,319 hrs · 25,151 cycles

DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND RT WINDOW FRAME CRACKED AT AFT LOWER CORNER (POST5) FS 150, WL233, RBL 52. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-30-32.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE DETECTION) · airframe 52,766 hrs · 24,842 cycles

DURING CRUISE, FLIGHT CREW REPORTED NR 2 ENGINE FIRE WARNING INDICATION, AND PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AND FIRE BOTTLE DISCHARGE. MAINTENANCE FOUND MALFUNCTIONING FIRE DETECTION CONTROL UNIT AND REPLACED WITH SERVICEABLE UNIT, NR 1.

Part: WIRE — BROKEN (OVERHEAT SWITCH) · airframe 52,718 hrs · 24,788 cycles

DURING CRUISE, FLIGHT CREW REPORTED NR 4 ENGINE TURBINE OVERHEAT LIGHT CAME ON, RETARDED THROTTLES AND LIGHT WENT OUT AT 900 DEGREES AT 1856Z. MAINTENANCE REPAIRED WIRE AT TURBINE OVERHEAT SWITCH AND REPORTED OPERATIONAL CHECK SATISFACTORY. LOG PAGE 25371 ITEM 1.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 52,697 hrs · 24,785 cycles

DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5301, FOUND RAMP DOOR FLOORBEAM SUPPORT BROKEN AT RS6 BL 0. SUPPORT FABRICATED & REPLACED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: RIB — CRACKED (FS 132 RBL 55) · airframe 52,697 hrs · 24,785 cycles

DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5303, FOUND COCKPIT RIGHT SIDE RIB CRACKED AT FS 132 WL 204 TO 216 RBL 55. RIB REPLACED IAW SMP583 CHAPTER 51-60 & 51-70.

Part: FITTING — CRACKED (FS 477 RBL 71) · airframe 52,697 hrs · 24,785 cycles

DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5301, FOUND CENTER FUSELAGE EXTERIOR STRUT UPPER FITTING CRACKED AT FS 477 WL 150 RBL 71. FITTING REPLACED IAW SMP583 FIG 51-60 & 51-70. P/N:339394-3.

Part: SKIN — CRACKED (RAMP DOOR) · airframe 52,697 hrs · 24,785 cycles

DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5301, FOUND RAMP DOOR BOTTOM EXTERIOR SKIN CRACKED FROM RS0.3 TO 1.7, BL 0. REPAIR CARRIED OUT USING 2024T3 .071" IAW SMP583 FIG 51-140-12.

Part: BULKHEAD — CRACKED (FS 880 RBL 62) · airframe 52,697 hrs · 24,785 cycles

DURING SCHEDULED B-2 CHECK, PER JOBCARD HB5302 FOUND AFT FUSELAGE INTERIOR UPPER BHD WEB CRACKED AT FS 880, WL 260, RBL 62. REPAIR CARRIED OUT IAW SMP583 FIG 53-50-05. P/N:7075T6 .063".

Part: SKIN — DENTED (FS 815E, LBL 63) · airframe 52,377 hrs · 24,513 cycles

DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND EXTERIOR FUSELAGE SKIN DENTED AT FS 815E, LBL 63, WL 144. REPAIRED SKIN IAW LAC MEA 382-53-07-051.

Part: SKIN — DENTED (BS 807E, RBL 63) · airframe 52,377 hrs · 24,513 cycles

DURING SCHEDULED A-1 CHECK PER JOB CARD HA1201, FOUND EXTERIOR FUSELAGE SKIN DENTED AT FS 807E, RBL 63, WL 144. REPAIRED SKIN IAW LAC MEA 382-53-07-051.

Part: BOLT — SHEARED (DRIVE BRACKET) · airframe 52,233 hrs · 24,409 cycles

NR 4 ENGINE FLAMED OUT DURING DESCENT. FOUND CONTROL DRIVE BRACKET (ANTI-ROTATION) BOLTS SHEARED, AND EXCESSIVE PLAY ON PUMP HOUSING GEAR. REPLACED DRIVE BRACKET BOLTS IAW HAMILTON STANDARD P5059 PG 1-402, REPLACED NR 4 PUMP HOUSING IAW HAMILTON STANDARD MM P5059 PG 1-338 - 1-340, REPLACED NR 4 VALVE HOUSING PRECAUTIONARY IAW LAC JC 61135, GROUND RUNS AND LEAK CHECKS SATISFACTORY.

Part: ENGINE — FLAMED OUT (NR 4) · airframe 52,078 hrs · 24,362 cycles

FLIGHT CREW REPORTED, THE NR 4 ENGINE FLAMED OUT AND WENT INTO FEATHER ON DESCENT TO LICZ. MAINTENANCE REMOVED AND REPLACED NR 4 PROPELLER VALVE HOUSING ON FLIGHT LOG PAGE 26683 WITH UNSATISFACTORY RESULTS. AIRCRAFT FERRIED FROM LICZ TO ETAR, LOG PAGE 26684. ENGINE CHANGE ACCOMPLISHED BY MAINTENANCE IN ETAR ON LOG PAGE 26685. SUSPECT FAULTY NTS PLUNGER IN REDUCTION GEARBOX. FAILURE ANALYISIS UNDER INVESTIGATION.

Part: SKIN — DAMAGED (FS 902) · airframe 51,796 hrs · 24,055 cycles

DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND FUSELAGE DAMAGED RT SIDE APPROX 4 INCHES LONG 2 INCHES WIDE AT FS 902, WL198, RBL 61.62. REPAIRED DAMAGE IAW MEA 382-53-07-036, LOG PAGE 26514 ITEM M1.

Part: STRUT — DENTED (FS770) · airframe 51,697 hrs · 23,980 cycles

DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND TUBE STRUT DENTED AT FS 770, WL 164, RBL 61. REPLACED TUBE STRUT IAW SMP583 51-10 PG 3G & 51-70, LOG PAGE 26232 ITEM M5.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324, FOUND RT MWW REAR BULKHEAD WEB CRACKED AT FS 617, RBL 73, WL 185. REPLACED WEB IAW SMP583 51-60.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5313, FOUND RT OUTBOARD BULKHEAD CAP CRACKED AT FS 1012, RBL67, WL270. REPAIRED BULKHEAD IAW MEA 382-53-07-011.

Part: SKIN — CRACKED (ESCAPE DOOR) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321, FOUND LT AFT AFT ESCAPE HATCH DOOR EXTERIOR SKIN CRACKED AT FS 935, LBL12, WL238. REPLACED SKIN IAW SMP583 51-60 AND 51-70.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5313, FOUND LT AFT FUSELAGE BULKHEAD TO LONGERON TEE FITTING CRACKED AT FS 858, LBL62, WL192. REPLACED FITTING IAW SMP 583 51-60 AND 51-70.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321, FOUND LT "ELEPHANT EAR" SKIN CRACKED AT FS847, LBL65, WL180. REPAIRED SKIN IAW SMP583 51-140-12.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HSP53300, FOUND NLG PRESSURE SKIN CRACKED AT FS 204, RBL2, WL134. REPAIRED SKIN IAW SMP 583 53-30-17.

Part: SKIN — CHAFED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC2111, FOUND FUSELAGE EXTERIOR SKIN CHAFED AT FS477, RBL80, WL180. REPAIRED SKIN IAW SMP583 51-140-12.

Part: CAP — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5315, FOUND RT AFT FUSELAGE BULKHEAD INNER CAP CRACKED AT FS 770, RBL67, WL162. REPAIRED CAP IAW SMP583 53-50-14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5321, FOUND RT "ELEPHANT EAR" SKIN CRACKED AT FS 847, RBL65, WL180. REPAIRED SKIN IAW SMP583 51-140-12.

Part: HINGE BRACKET — CRACKED (NLG DOOR) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HSP32302, FOUND FWD RT NLG DOOR HINGE BRACKET CRACKED AT FS 93, RBL20.5, WL153. REPLACED BRACKET IAW SMP583 51-60 AND 51-70.

Part: HINGE BRACKET — CRACKED (NLG DOOR) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HSP32302, FOUND FWD LT NLG DOOR HINGE BRACKET CRACKED AT FS93, LBL20.5, WL153. REPLACED BRACKET IAW SMP583 51-60 AND 51-70.

Part: SKIN — CRACKED (FUSELAGE) · airframe 51,359 hrs · 23,550 cycles

DURING SCHEDULED C-7 CHECK PER JOB CARD HC5324, FOUND RT BOTTOM MWW SKIN CRACKED AND WARPED AT FS 477 - 621, RBL33 - 64, WL132. REPLACED SKIN IAW SMP 583 51-60 AND 51-70.

Part: WEB — CRACKED (FS 880) · airframe 50,654 hrs · 23,082 cycles

DURING SCHEDULED B3 CHECK PER JOB CARD HB5302, FOUND RT AFT FUSELAGE INTERIOR WEB CRACKED AT FS 880, WL216, RBL71. REPAIRED WEB IAW SMP583 51-140-17.

Part: SKIN — CRACKED (FS 595) · airframe 50,654 hrs · 23,082 cycles

DURING SCHEDULED B 3 CHECK PER JOB CARD HB5301, FOUND RT MAIN WHEEL WELL EXTERIOR SKIN CRACKED AT FS 595, WL190. REPLACED SKIN IAW LAC MEA 382-53-04-013 R1.

Part: BEAM — CRACKED (FS 557) · airframe 50,654 hrs · 23,082 cycles

DURING SCHEDULED B3 CHECK PER JOB CARD HB5301, FOUND RT UPPER WHEEL WELL BOW BEAM CRACKED AT FS 557, WL202, RBL62. REPAIRED BOW BEAM IAW SMP 583 53-40-14.

Part: FRAME — CRACKED (FS 116) · airframe 50,654 hrs · 23,082 cycles

DURING SCHEDULED B3 CHECK PER JOB CARD HB5301, FOUND RT CLEAR VISION WINDOW REAR FRAME CRACKED AT FS 116. REPAIRED FRAME IAW LAC MEA 382-53-06-095.

Part: FITTING — CRACKED (FS 946) · airframe 50,654 hrs · 23,082 cycles

DURING SCHEDULED B 3 CHECK PER JOB CARD HB5302, FOUND LT AFT FUSELAGE GUSSET FITTING CRACKED AT FS 946, WL256, BL61. REPLACED FITTING IAW SMP583 51-60 AND 51-70.

Part: BULKHEAD — CRACKED (FS 617) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB5301 FOUND RT MWW REAR BULKHEAD CRACKED AT FS 617, RBL 70, WL 188. REPAIRED BULKHEAD IAW SMP583 FIG 53-40-10.

Part: TEE FITTING — CRACKED (FS 858) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB5302 FOUND RT AFT FUSELAGE TEE FITTING CRACKED AT FS 858, RBL 64, WL 160. FABRICATED AND INSTALLED FITTING IAW SMP583 51-60, 51-70 AND LOCKHEED DWG 342593.

Part: BULKHEAD — CRACKED (FS 946) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB5302 FOUND AFT FUSELAGE UPPER BULKHEAD WEB CRACKED AT FS 946, LBL 50, WL 260. REPAIRED WEB IAW SMP583 FIG 51-140-17.

Part: FITTING — CRACKED (FS 497) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB5301 FOUND LT BOW BEAM FITTING CRACKED AT FS 497, LBL 62, WL 250. REPLACED FITTING IAW SMP583 51-60, 51-70 AND LOCKHEED DWG 3338353.

Part: FRAME SPLICE — CRACKED (FS 477) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB5302 FOUND RING SEGMENT SPLICE CRACKED AT FS 477, RBL 20, WL 285. FABRICATED AND REPLACED SPLICE IAW SMP583 51-60, 51-70 AND LOCKHEED DWG 375943.

Part: BULKHEAD — CRACKED (FS 880) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB5302 FOUND RT AFT FUSELAGE BULKHEAD WEB CRACKED AT FS 880, RBL 65, WL 195. FABRICATED AND INSTALLED WEB DOUBLER IAW SMP583 51-60, 51-70 AND FIG 51-140-17.

Part: STIFFENER — CRACKED (FS 597) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB2702 FOUND RT OUTBOARD FLAP TRACK STIFFENER CRACKED AT FS 597, OWS 173 RT. REPLACED STIFFENER IAW SMP583 51-60, 51-70 AND LOCKHEED DWG 348626.

Part: BEAM — CRACKED (FS 497) · airframe 50,041 hrs · 22,834 cycles

DURING SCHEDULED B2 CHECK PER JOB CARD HB5301 FOUND LT BOW BEAM CRACKED AT FS 497, LBL 62, WL 250. REPAIRED BEAM IAW LAC MEA 382-53-06-055.

Part: SPRING — BROKEN (THROTTLE) · airframe 49,811 hrs · 22,664 cycles

NR 4 THROTTLE JAMMED FORWARD OF FLIGHT IDLE. ENGINE SHUT DOWN ON SHORT FINAL AT 01:08 Z IAW QRH. FOUND THROTTLE DETENT SPRING BROKEN IN QUADRANT. REMOVED AND REPLACED THROTTLE DETENT SPRING, INSPECTED AND CLEANED AREA PER SMP581 CHAP 76-10, SYSTEM OPS CHECK GOOD PER HN7101.

Part: MOUNT — CRACKED (WS 197.2 LT) · airframe 49,332 hrs · 22,521 cycles

DURING 'B-1' CHECK PER HN7101, FOUND NR 1 ENGINE OUTBOARD TRUSS MOUNT CRACKED AT FS 598, WL 280-284, OWS197.2. REPLACED TRUSS MOUNT IAW SMP583 54-30-05 AND 54-30-06 AND SB 382-71-13, N/R 0009.

Part: BULKHEAD — CRACKED (BS 946) · airframe 49,332 hrs · 22,521 cycles

DURING 'B-1' CHECK PER HB5302, FOUND OVERHEAD BULKHEAD WEB CRACKED AT FS946, WL275, RBL50. REPAIRED IAW SMP583 51-140-17, N/R 0068.

Part: FRAME — CRACKED (BS 957) · airframe 49,332 hrs · 22,521 cycles

DURING 'B-1' CHECK PER HB5302, FOUND RINGFRAME CRACKED AT FS957, WL270, LBL66. REPAIRED IAW SMP583 53-50-07, N/R 0069.

Part: BULKHEAD — CRACKED (BS 902) · airframe 49,332 hrs · 22,521 cycles

DURING 'B-1' CHECK PER HB5302, FOUND SIDE BULKHEAD WEB CRACKED AT FS902, WL200, RBL68. REPAIRED IAW SMP583 51-140-17, N/R 0070.

Part: CAP — CORRODED (WS 171 R) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5711, FOUND RIGHT HAND INBOARD FLAP CENTER LOWER SPAR CAP CORROSION, 7-05-074, NR 0407.

Part: SKIN — DAMAGED (FS 757E-777E) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5321, FOUND BELLY SKIN DAMAGED, FS 757E TO FS 777E, BL0. REPAIRED DAMAGED BELLY SKIN PER SRM 51-104-12, NR 0250.

Part: BULKHEAD — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB CRACKED LBL40. REPAIRED IAW SRM SMP 583 FIGURE 51-140-17, NR 0086.

Part: SKIN — CRACKED (FUSELAGE) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5211, FOUND RAMP REAR SILL UPPER RIGHT HAND SKIN PANEL SPLIT. REPLACED SKIN PANEL PER DRAWING 353612 AND SRM 51-70, NR 0296.

Part: SKIN — DAMAGED (FS 317E) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5321, FOUND STONE DAMAGE, FS 317E.0E, LBL2 WL126. REPAIRED BELLY SKIN PER SRM 51-140-10, NR 0352.

Part: BRACKET — CRACKED (FS 1001) · airframe 48,745 hrs · 22,385 cycles

,DURING C-6 CHECK PER HC5212 FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, RBL10. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081.

Part: FRAME — MISDRILLED (FS 626) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT SIDE, FS626, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: FLOORBEAM — CORRODED (FS 200) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE LOWER FORWARD UNDERDECK FLOOR SUPPORT ANGLE, FS 200, RBL9 WL146. REPLACED FLOOR SUPPORT ANGLE IAW SRM SMP 583 51-70 AND ED05-025-02, NR 0307.

Part: FRAME — MISDRILLED (FS 697) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS697, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: STIFFENER — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS1023, LBL20. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43.13-1B PARA 4-57, NR 0106.

Part: FRAME — MISDRILLED (FS 727) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS727, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: BRACKET — CRACKED (FS 1001) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS1001, RBL30. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081.

Part: BRACKET — CRACKED (FS 1001) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS1001, BL0. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081.

Part: BRACKET — CRACKED (FS 1001) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, RBL40. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B PARA 4-57, NR 0081.

Part: SKIN — DAMAGED (FS 277) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5321, FOUND STONE DAMAGE FS 277, LBL30 WL126. REPAIRED BELLY SKIN PER SRM 51-140-12, NR 0351.

Part: STIFFENER — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C -6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL20. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43.13-1B PARA 4-57, NR 0106.

Part: CAP — MISDRILLED (FS597) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC3212, FOUND TWO FASTENER HOLES WERE MISTAKENLY DRILLED DURING RIGHT HAND MLG BEAM CAP REPAIR, FS 597. REPAIRED IAW SRM SMP 583 53-40-3 AND ED05-025-1, NR 0373.

Part: ANGLE — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL37. REPAIRED STIFFENER ANGLES PER SRM 51-140-19, NR 0107.

Part: FRAME — MISDRILLED (FS 647) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT SIDE, FS 647, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: FRAME — MISDRILLED (FS 457) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT SIDE, FS 457, WL158. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414.

Part: STIFFENER — CRACKED (FS1023) · airframe 48,745 hrs · 22,385 cycles

DURING C -6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED FS 1023, RBL0. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43.13-1B PARA 4-57 NR 0106.

Part: DOUBLER — CORRODED (FS 197) · airframe 48,748 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE IN LOWER FORWARD UNDERDECK SKIN FS 197, LBL36 WL139 - WL146. INSTALLED DOUBLER PER SRM SMP 583 51-70, NR 0307.

Part: BRACKET — CRACKED (FS 1001) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, RBL20. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B, PARA 4-57 NR 0081.

Part: FLANGE — CRACKED (FS 847) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5315, FOUND CANTED SKIN ATTACH FLANGE CRACKED, FS 847, LBL 65 WL 187. REPAIRED PER LAC MEA 382-53-01-080 (ED01-058-01) NR 0175.

Part: FRAME — MISDRILLED (FS 742) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT HAND SIDE, FS 742, WL151. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414.

Part: STIFFENER — CRACKED (FS1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED FS 1023, RBL10. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43, 13-1B PARA 4-57 NR 0106.

Part: FRAME — MISDRILLED (FS 377) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE RIGHT HAND SIDE, FS 377 WL151. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414.

Part: ANGLE — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL34. REPAIRED STIFFENER ANGLES PER SRM 51-140-19, NR 0107.

Part: SKIN — CRACKED (FS 870) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5211, FOUND RAMP REAR SILL UPPER CENTER SKIN PANEL CRACKED, FS 870. REPLACED SKIN PANEL IAW SRM SMP 583 FIGURE 51-70 AND AC43, 13-1B PARA 4-57, NR 0202.

Part: ANGLE — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL25. REPAIRED STIFFENER ANGLES IAW SRM 51-140-19, NR 0107.

Part: FRAME — MISDRILLED (FS657) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313 FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE. FS657, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070. NR 0413.

Part: BRACKET — CRACKED (FS 1001) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD STIFFENER/TUBE STRUT ATTACH BRACKET CRACKED, FS 1001, LBL20. REPLACED ATTACH BRACKET IAW SRM SMP 583 51-70 AND AC43.13-1B PARA 4-57 NR 0081.

Part: ANGLE — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, LBL33. REPAIRED STIFFENER ANGLES IAW SRM 51-140-19, NR 0107.

Part: CAP — CORRODED (WS 163 RT) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5711, FOUND RIGHT HAND OUTBOARD FLAP CENTER LOWER SPAR CAP CORROSION. REPAIRED IAW DRAWING R05-025-03 PER LAC MEA382-57-05-073. NR 0404.

Part: FRAME — MISDRILLED (FS 667) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS 667, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: FRAME — MISDRILLED (FS 757) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS757, WL151. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: CHANNEL — CRACKED (FS 1030) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5315, FOUND REAR FUSELAGE RIGHT HAND SIDE CHANNEL CRACKED, FS 1030. REPLACED CHANNEL IAW SRM SMP 583 51-70-00, LEAK CHECKED IAW SMP 581 36-10, NR 0178.

Part: DOUBLER — DAMAGED (CARGO DOOR) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5211, FOUND REAR RAMP SHELF DAMAGED RS10 LBL 60-RBL 60. INSTALLED PROTECTIVE PADS IAW DRAWING 105-025-01 PER LAC MEA382-53-05-080, NR 0376.

Part: SKIN — DAMAGED (BS 764) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5321, FOUND STONE DAMAGE FS 764.0E, LBL64 WL146. REPAIRED FUSELAGE SKIN PER SRM 51-140-10, NR 0356.

Part: PANEL — CRACKED (FS 597) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER SB 382-57-85, FOUND CRACKS IN NR 3 CENTER WING LOWER SURFACE PANEL, FS 597, LBL 60. REPAIRED IAW LOCKHEED REPAIR TASK 39 UNDER GLD 1720 (SK382-57-296) PER LAC MEA382-57-05-086, NR 0459.

Part: FLOORBEAM — CORRODED (FS 210) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE IN LOWER FORWARD UNDERDECK FLOOR SUPPORT CHANNEL FS 210, BL 0 WL146. REPLACED FLOOR SUPPORT CHANNEL IAW SRM SMP 583 51-70, NR 0307.

Part: FRAME — MISDRILLED (FS 457) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT HAND SIDE, FS457, WL162. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414.

Part: STIFFENER — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C -6 CHECK IAW HC5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS1023, RBL30. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43 13-1B PARA 4-57, NR 0106.

Part: FLOORBEAM — CORRODED (FS 200) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE LOWER FORWARD UNDERDECK FLOOR SUPPORT ANGLE, FS 200, LBL9 WL146. REPLACED FLOOR SUPPORT ANGLE IAW SRM SMP 583 51-70 AND ED05-025-02, NR 0307.

Part: FRAME — MISDRILLED (FS 707) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE LEFT HAND SIDE, FS707, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: FRAME — MISDRILLED (FS 732) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS4010-8) MISDRILLED LINER HOLE LEFT HAND SIDE, FS732, WL151. REPAIRED IAW DRAWING R05-025-07 PER LAC MEA382-53-05-071, NR 0414.

Part: FLOOR SUPPORT — CORRODED (FS 197-225) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5312, FOUND CORROSION DAMAGE IN LOWER FORWARD UNDERDECK FLOOR SUPPORT TEE SECTION FS 197 TO FS 225. REPLACED FLOOR SUPPORT TEE SECTION IAW SRM SMP 583 51-70, NR 0307.

Part: SKIN PANEL — CORRODED (CWS 171) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5711, FOUND LEFT HAND CENTER WING LOWER PLANK CORROSION CWS171-213. REPAIRED IAW DRAWING R05-025-05 PER LAC MEA382-57-05-077, NR 0416.

Part: BULKHEAD — CRACKED (FS 617) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER 02SB-382-5785-2, FOUND PRESSURE BULKHEAD WEB CRACKED. FS617 LBL61, WL240. REPLACED WEB IAW SRM SMP 583 51-60/70 AND AC43.13-1B, NR 0429.

Part: DOUBLER — DAMAGED (FS 847) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5315, FOUND ELEPHANT EAR DAMAGE, FS847, LBL64 WL185. REPLACED ELEPHANT EAR DOUBLER PER SRM 51-70, NR 0224.

Part: BULKHEAD — CRACKED (NR 3 NACELLE) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5711, FOUND NR 3 NACELLE OUTBOARD BULKHEAD CRACKED. REPAIRED IAW DRAWING R05-025-06 PER LAC MEA382-54-05-078, NR 0387.

Part: FRAME — MISDRILLED (FS 626) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5313, FOUND FUSELAGE FRAME (LS5408-2) MISDRILLED LINER HOLE RIGHT HAND SIDE, FS 626, WL158. REPAIRED IAW DRAWING R05-025-08 PER LAC MEA382-53-05-070, NR 0413.

Part: ANGLE — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C-6 CHECK IAW HC5212, FOUND CARGO DOOR BULKHEAD WEB STIFFENERS CRACKED, FS 1023, LBL36. REPAIRED STIFFENER ANGLES IAW SRM 51-140-19, NR 0107.

Part: GUSSET — CRACKED (FS 980) · airframe 48,475 hrs · 22,385 cycles

DURING C-6 CHECK PER HC5212, FOUND CARGO DOOR BULKHEAD LOWER ANGLE GUSSET CRACKED FS 980. REPLACED LOWER ANGLE GUSSETT PLATE ASSEMBLY IAW SRM SMP 583 51-70 AND AC43.13-1B PARA 4-52, NR 0193.

Part: STIFFENER — CRACKED (FS 1023) · airframe 48,745 hrs · 22,385 cycles

DURING C -6 CHECK IAW HC 5212, FOUND CARGO DOOR AFT BULKHEAD WEB STIFFENERS CRACKED, FS 1023, RBL40. REPLACED WEB STIFFENERS IAW SRM SMP 583 FIGURE 51-70 AND AC43 13-1B PARA 4-57, NR 0106.

Part: COOLING TURBINE — FAILED (AIR CON SYS) · airframe 48,625 hrs · 22,346 cycles

FLIGHT CREW REPORTED, FLIGHT STATION AIR CONDITIONING SYSTEM HOWLING AND SMELL BAD. SHUT DOWN AIR CONDITIONING SYSTEM. FOUND FLIGHT STATION COOLING TURBINE FAILED. REPLACED COOLING TURBINE IAW MM SMP 581 21-50. OPS AND LEAK CK NORMAL. LP 18732, ITEM 1.

Part: CARGO TRACK — CRACKED (FUSELAGE) · airframe 47,606 hrs · 21,901 cycles

DURING SCHEDULED B2 INSPECTION PER JOB CARD HSP53262 FOUND LT FS 617 25000 LB TIE DOWN FITTING CRACKED APPROX .25 INCH AT LBL 61, WL 143. REPLACED FITTING IAW SRM SMP 583 51-70. NR 2004.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 47,332 hrs · 21,740 cycles

DURING SCHEDULED A CHECK PER JOB CARD HA1200 FOUND FS 1078 HORIZONTAL STAB LOWER SKIN CRACKED 1.5 INCH SPANWISE AT RBL 46, WL 223. REPAIRED IAW SRM SMP 583 55-20-06. LP 15658, GMM133 ITEM M3.

Part: SPAR — CRACKED (CENTER WING) · airframe 46,948 hrs · 21,579 cycles

DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5302, FOUND CENTER WING FRONT SPAR WEB CRACKED AT FS 517, CWS 20.5R, WL 273. REPAIRED IAW EA 382-53-04-088. NR 0017.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,948 hrs · 21,579 cycles

DURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5301, FOUND RT FS 407 EXTERNAL ESCAPE HATCH FWD UPPER CORNER CUTOUT CRACKED AT WL 226, RBL 80. REPAIRED IAW SRM SMP 583 53-40-50. NR 0027.

Part: BOOT — DISLODGED (RUDDER) · airframe 46,299 hrs · 21,437 cycles

HEARD A LOUD NOISE IN THE CARGO COMP, PRESSURIZATION WENT TO ZERO, AT 5000 FT IAW MINUTE NOTICE LIGHT COMING IN ON BOTH SIDE OF AFT DOOR. DECENDED TO 11,000 FT DUMPED APPROX 7000 LBS ALTITUDE AT TIME OF INCIDENT 20,000 FT, DID NOT GET A DOOR WARNING LIGHT. PRESSURE OF 13IN. TROUBLESHOOTING CARRIED OUT FOUND RUDDER BOOT ASSY DISLODGED FROM HOUSING ON A/C STRUCTURE SIDE. BOOT ASSY. REMOVED AND REPLACED IAW SMP 581-27-20 PG 210B. P/N 377304-1 (1 EA). PRESS LEAK CHECK C/OUT IAW SMP 581-21-30 PG 217/218 FIG 21-30-07 FOUND SATISFACTORY.

Part: FLOOR PANEL — WARPED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5211 FOUND RAMP DOOR FS 762 - 857, RBL 40, RT FLOOR PANEL WARPED. FLOOR PANEL REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2231.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321 FOUND LMLG WHEEL WELL SKIN CRACKED AT FS 597, LBL 35, WL 130. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2036.

Part: SKIN — DELAMINATED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321 FOUND 4 IN. X 10 IN. AREA OF HONEYCOMB PANEL DELAMINATED AT LT MLG WHEEL WELL FS 520 - 530, WL 200. AND LT MLG POD CENTER FAIRING FS 512 - 596, WL 180-200. SKIN PANEL REPLACED IAW LAC MEA 382-53-04-046. DRC 2054.

Part: PANEL — CRACKED (CENTER WING) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW SB382-57-55R1 PARA 1.B.3. HFEC FOUND FS 564 RT CENTER WING NR 2 PANEL LOWER SURFACE CRACKED APPROX .280 IN. AT CWS 63R. REPAIRED IAW LAC MEA 382-57-04-050 AND LOCKHEED SES GLD-1720 TN 0033, DWG SK382-57-278. DRC 2189.

Part: SKIN — WARPED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND LT SIDE FUSELAGE SKIN WITH NUMEROUS DEEP CUTTING MARKS, WARPED, AND SUNKEN RIVETS. FS 777E-817E, LBL 80, WL140 - 160. REPLACED SKIN LT FS 777E - 817E, WL 140 - 195 IAW SRM SMP 583 CHP 51-60 AND 51-70. DRC 2039.

Part: SKIN — CRACKED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND BELLY TO RT MLG WHEEL WELL SKIN CRACKED AT FS 537, RBL 43, WL 135. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2037.

Part: FLOOR PANEL — WARPED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5211, FOUND RAMP DOOR CENTER ACCESS FLOOR PANEL WARPED AT FS 809 - 856. CENTER FLOOR PANELS AT FS 809-832 AND FS 832-856 REPLACED IAW SRM SMP 583 CHP 51-60 & 51-70. DRC 2042.

Part: WEB — CRACKED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5324 FOUND RT MLG WHEEL WELL INTERCOASTAL BEAM OUTER CAP AND WEB CRACKED AT FS 493, RBL 68, WL 200. CAP AND WEB REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2210.

Part: FITTING — CORRODED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5321 FOUND NLG ATTACH FITTINGS WITH PITTING CORROSION. FS196, BL 5 L/R, WL146. FITTINGS REPLACED IAW SRM SMP 583 CHP51-60 AND 51-70. DRC 2064.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION DRC 2210 ACCOMPLISHMENT FOUND INTERCOSTAL INBD CAP CRACKED CLOSE TO EXISTING REPAIR AT FS 494, RBL 62, WL 200. CAP REPLACED IAW SRM SMP 583 CHP51-60 & 51-70. DRC 2222.

Part: PANEL — CRACKED (CENTER WING) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION IAW HSP57141 FOUND RT CTR WING LOWER SURFACE NR 3 PANEL CRACKED APPROX. 3.0 IN. AT FS 597, CWS 62R AND NR 24 CW STRINGER CRACKED APPROX 14 IN. SAME LOCATION. REPAIRED IAW LAC MEA 382-57-04-051 AND LOCKHEED SES GLD-1720 TN 0034, DWG SK382-57-279. DRC 2191.

Part: SKIN — DENTED (CARGO DOOR) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION PER IAW CARD HC5321 FOUND CARGO DOOR EXTERIOR SKIN DENTED AT FS 900 - 930, WL 195 - 210, LBL 15 - RBL 15 AND FS 930 - 960, WL195 - 210, LBL 15 - RBL 15. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2132.

Part: SKIN — DEFORMED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION IAW JOB CARD HC5321 FOUND RAMP DOOR REAR TE BOTTOM EXTERIOR SKIN DEFORMED/NICKED AT FS 857, RBL 50. REPAIRED IAW SRM SMP 583 FIG 51-140-12. DRC 2073.

Part: FLOOR PANEL — WARPED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5211, FOUND RAMP DOOR LT FLOOR PANEL WARPED AT FS 809. FLOOR PANEL REPLACED IAW SRM SMP 583, CHP 51-60 AND 51-70. DRC 2043.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION DRC 2191 ACCOMPLISHMENT FOUND RBL 61 BULKHEAD WEB CRACKED AT FS 614 - 617, WL260. REPLACED WEB AT FS 577 - 617, WL 252 - 270 IAW SMP583 CHP51-60 AND 51-70 AND LAC MEA 382-53-04-053. DRC 2245.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND WINDSHIELD FRAME CRACKED AT FS 130, LBL 60, WL 251. REPAIRED IAW SRM SMP 583 FIG 53-30-25. DRC 2013.

Part: BEAM — CRACKED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION DRC 2191 ACCOMPLISHMENT FOUND FS 597 MLG BEAM IB CAP CRACKED AT RBL 62, WL 257. REPAIRED IAW LAC MEA 382-53-04-055. DRC 4422.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 46,295 hrs · 21,435 cycles

DURING SCHEDULED C-5 INSPECTION, IAW JOB CARD HC5321, FOUND BELLY ANTENNA FLANGE WITH DENTS AND DEEP SCRATCHES AT FS 265 - 278 BL18 L/R, WL126. RADIO ALTIMETER ANTENNA DOUBLERS FABRICATED AND INSTALLED IAW DWG 3304217. DRC 2034.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 45,668 hrs · 21,234 cycles

DURING SCHEDULED B3 INSPECTION PER JOB CARD HB5301 FOUND RT AFT DV WINDOW POST CRACKED. REPAIR CARRIED OUT IAW SMP583 CH 53-30-25, FS 116 WL 255 RBL 40.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 45,668 hrs · 21,234 cycles

DURING SCHEDULED B3 INSPECTION PER JOB CARD HB3200 FOUND FS 617 BULKHEAD AT WL 210 EXISTING REPAIR CRACKED AT LBL 60. REPAIRED IAW SMP583 FIG 53-40-10, FS 617 WL 200 - 210 LBL 63-73.

Part: FITTING — CRACKED (FLOORBEAM) · airframe 44,900 hrs · 20,974 cycles

DURING SCHEDULED B2 INSPECTION IAW JOB CARD HB5302 FOUND RT FS 477 FLOORBEAM END FITTING CRACKED AT RBL 60, WL 146. REPLACED FITTING IAW DWG 356245-19 AND SRM SMP 583 51-70. NR 0027.

Part: BEAM — CRACKED (FUSELAGE) · airframe 44,207 hrs · 20,351 cycles

DURING SCHEDULED B1 INSPECTION PER JOB CARD HB3201 FOUND LT FS 517 MLG BEAM OUTER CAP CRACKED AT WL 215, LBL 62. REPLACED OUTER CAP IAW DWG 388394 AND SRM SMP 583 51-70. NR 0014.

Part: BOOSTER — BINDING (RUDDER ACTUATOR) · airframe 44,103 hrs · 20,267 cycles

DURING APPROACH TO BET FLT CREW REPORTED RUDDER WOULD NOT MOVE PAST NEUTRAL TO THE RT. INITIATED GO AROUND. ON SECOND APPROACH SOME RT RUDDER CONTROL WAS REGAINED WITH FLAPS AT 50 PERCENT AND IAS 150 KTS. FLEW ABNORMAL PATTERN AND USED DIFFERENTIAL POWER TO MAINTAIN RUNWAY ALIGNMENT. ON ROLL OUT RUDDER REACTED NORMALLY BELOW 60 KTS. INSPECTED RUDDER CONTROL SYSTEM FOR FREEDOM OF MOVEMENT. NO DEFECTS NOTED. NOTED INTERNAL POPPING SOUND FROM RUDDER BOOSTER ASSY DURING MOVEMENT. REPLACED RUDDER BOOSTER ASSY IAW SMP 581 27-20 PG 217-219, LEAK AND OPS CHECK NORMAL. AIRCRAFT RELEASED FOR TEST FLIGHT TO CONFIRM CORRECTIVE ACTION. TEST FLIGHT SATISFACTORY. LP 12179, ITEM 1.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC3212 RT WING-TO-FUSELAGE FAIRING CHANNEL CRACKED AT FS 532, RBL 86, WL 237. REPAIRED IAW LAC MEA 382-53-03-010. NR 2209.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5511 FOUND LT HORIZONTAL STAB UPPER TRAILING EDGE SKIN CRACKED AT HSS 180 & 210. REPAIRED IAW SRM SMP 583 55-20-06. NR 2038.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB HC5324 FOUND RT MLG WHEEL WELL BOW BEAM CRACKED AT FS 557, RBL 61, WL 200. REPAIRED IAW SRM SMP 583 53-40-14. NR 2076.

Part: STIFFENER — CRACKED (BULKHEAD) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5711 FOUND LT WING FLAP WELL BULKHEAD WEB BRACE/ STIFFENER CRACKED AT OWS 241. REPLACED STIFFENER IAW SRM SMP 583 51-60 AND 51-70. NR 2033.

Part: STRAP — BROKEN (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5321 FOUND LT FUSELAGE SKIN INNER STRAP BROKEN AT FS 787E, LBL 70, WL 250. REPAIRED IAW LAC MEA 382-53-03-012. NR 2264.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND FS 814 RING SEGMENT WEB CRACKED AT LBL 67, WL 150. REPAIRED IAW SRM SMP 583 51-140-17. NR 2158.

Part: SKIN — CRACKED (LT & RT WING) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5711 FOUND UPPER SURFACE OWS 173-241 T/E PANELS CRACKED LT AND RT. SKIN PANELS REPLACED IAW LAC MEA 382-57-03-020. NR 2232.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WL 140 CHINE ANGLE CRACKED AT FS 520, LBL 61. REPAIR IAW SRM SMP 583 53-40-27. NR 2079.

Part: RIB — CRACKED (BULKHEAD) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND FS 1023 UPPER BULKHEAD RIB CRACKED BEYOND PREVIOUS REPAIR AT LBL 20, WL 283. REPLACED RIB IAW SRM SMP 583 51-70 & 51-60. NR 2156.

Part: BEAM — CRACKED (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5323 FOUND FS 577 LT MLG BEAM ASSY CRACKED AT LBL 64, WL 240. PREVIOUS REPAIRS AT WL 225 & 245. BEAM ASSY REPLACED IAW SRM SMP 583 51-60 & 51-70 AND DWG 388482. NR 2316.

Part: SUPPORT FITTING — BROKEN (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND RT AFT SLOPING LONGERON FS 1041 SUPPORT FITTING CRACKED AT RBL 61, WL 190. FITTING REPLACED IAW SRM SMP 583 51-10 PG 4. NR 2227.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5324 FOUND RT MLG WHEEL WELL CHINE ANGLE CRACKED AT FS 617, RBL 61, WL 180. REPAIRED IAW SRM SMP 583 53-40-27. NR 2167.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5315 FOUND FS 924 BULKHEAD UPPER WEB CRACKED AT LBL 61, WL 256. REPAIRED IAW SRM SMP 583 51-140-17. NR 2159.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 43,629 hrs · 19,912 cycles

DURING SCHEDULED C4 INSPECTION PER JOB CARD HC5323 FOUND LT MLG WHEEL WELL WEB CRACKED AT FS 585 LBL 61, WL 180. REPAIRED IAW LAC MEA 382-53-03-014. NR 2263.