N409LC
Registered owner: LYNDEN AIR CARGO LLC, AK (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
662 reports on file, 2019-06-24 – 2026-06-19.
Part: SKIN — CRACKED (ZONE 300 ELEV) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND LH ELEVATOR LEADING EDGE SKIN CRACKED AT FS1106, HSS213L, WL280. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0771.
Part: SPAR CAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB FRONT SPAR UPPER CAP FLANGE CORRODED AT FS1041, HSS62-64.75R, WL283. / REPAIRED IAW LAC MEA 382-55-25-064. NR# 0767.
Part: SPAR CAP — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB LOWER SPAR CAP CRACKED AT FS1041, HSS54R. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0766.
Part: DOUBLER — CRACKED (ZONE 300 ELEV) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5313, FOUND LH ELEVATOR UPPER SKIN INNER DOUBLER CRACKED AT HSS296L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0758.
Part: SPAR CAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC 5511, FOUND HORIZONTAL STAB FRONT SPAR LOWER CAP TEE FLANGE CORRODED AT FS 1041, LBL 61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SPAR CAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC 5511, FOUND HORIZONTAL STAB LOWER CAP TEE FLANGE CORRODED AT FS 1041, RBL 61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: STIFFENER — CRACKED (ZONE 800) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5211, FOUND CARGO DOOR BS 1017 BULKHEAD WEB VERTICAL STIFFENERS LOWER SCREW HOLE CRACKED AT RBL 21. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: RIB — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STAB RT LEADING EDGE RIBS CRACKED AT HHS 255R, HSS 262R, HSS 267R, AND HSS 284R. REPAIRED IAW SRM 51-140-20.
Part: RIB — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STAB RT LEADING EDGE RIBS CRACKED AT HHS 203R, HSS 209R, AND HSS 214R. REPAIRED IAW SRM 51-140-20.
Part: FORMER — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STAB LT LEADING EDGE LOWER FORMER CRACKED AT HSS 162L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FORMER — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STAB LT LEADING EDGE LOWER FORMER CRACKED AT HSS 156L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, 51-60 & 51-70.
Part: FORMER — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STAB LT LEADING EDGE LOWER FORMER CRACKED AT HSS 168L. REPAIRED IAW SRM 51-140-20.
Part: SKIN — DENTED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND LT ELEVATOR UPPER SKIN DENTED AT HSS 238-296L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CRACKED (ZONE 500 FLAP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT OTBD FLAP UPPER CENTER SKIN CRACKED UNDER BUMPER PAD AT OWFS207L. REPAIRED IAW SRM 51-14-12.
Part: SKIN — DENTED (ZONE 300 ELEV) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND LT ELEVATOR UPPER SKIN DENTED AT HSS 180-238L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FAIRING — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RADOME FAIRING CRACKED AT RIVET EDGE AT FS 80, LBL 12, WL 200 . REPAIRED IAW SRM 51-140-11.
Part: BRACKET — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC3211, FOUND LT MLG WHEEL WELL FS 491 UPPER SUPPORT BRACKET CRACKED AT LBL 61, WL 200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: TRIM TAB — CRACKED (ZONE 600 AILERON) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5712, FOUND RT AILERON TRIM TAB TRAILING EDGE CRACKED AT AS62R AND AS66R. REPAIRED IAW SRM 51-140-12.
Part: BULKHEAD WEB — CRACKED · airframe 43,251 hrs · 26,493 cycles
DURING ULTRASONIC SPECIAL NDI INSP IAW SERVICE FLO CS1370999, FOUND FS 93 CANTED. BULKHEAD CRACKING IN THE WEB. DOCUMENTED ON NDT RPT PLA-066-2025. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND VERTICAL STAB RH AFT SKIN CORRODED AT FS 1115, VSS 30, RBL 11. REPAIRED IAW LOCKHEED SRM 51-140-12.
Part: ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC 5511, FOUND HORIZONTAL STAB LT VERTICAL ANGLE CORRODED AT FS 1077, HSS 238L, WL 285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (WING TIP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT OUTER WING TIP COVER ATTACHMENT FITTING CRACKED AT OWS 563L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SPAR CAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB FRONT SPAR UPPER CAP CORRODED AT FS 1041, HSS 62-64R, WL 283. REPAIRED IAW MEA 382-55-25-064.
Part: SKIN — CRACKED (ZONE 500 FLAP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT OTBD FLAP UPPER CENTER SKIN CRACKED UNDER CHAFE PAD AT OWFS0L. REPAIRED IAW LOCKHEED SRM 51-140-12.
Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC3211, FOUND MLG WHEEL WELL UPPER WL 200 SUPPORT CLIP CRACKED AT FS 517, LBL 85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FLANGE — CRACKED (CARGO RAMP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5211, FOUND CARGO RAMP BULKHEAD FORWARD SUPPORT FLANGE CRACKED AT RS0, LBL 44-48, WL 141. / REPAIRED IAW SRM 51-140-19.
Part: SKIN — CHAFED (ZONE 600 FLAP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5712, FOUND LT INBOARD FLAP LEADING EDGE SKIN CHAFED AT CWS82R. REPAIRED IAW LOCKHEED SRM 51-140-12.
Part: SKIN — CHAFED (ZONE 500 FLAP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT INBD FLAP LEADING EDGE SKIN CHAFED AT CWS82L. REPAIRED IAW LOCKHEED SRM 51-140-12.
Part: FORMER — CRACKED (ZONE 200) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5315, FOUND FS 922 OVERHEAD FORMER CRACKED AT LBL 13 SCREW HOLE AND LBL17 FLANGE. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB INTERIOR FITTING CORRODED AT FS 1049, LBL 13, WL 278. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: RIB — CRACKED (ZONE 500 FLAP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT OUTBOARD FLAP RIB CRACKED AT OWFS336L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FRAME — MISREPAIRED (ZONE 200) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS 777.0E RING SEGMENT WITH INCORRECT REPAIR AT RBL 70, WL 246. REPAIRED IAW SRM 53-40-11.
Part: BEAM — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5324, FOUND RT MLG UPPER WHEEL WELL BEAM ASSY WEB CRACKED AT FS 523, RBL 61, WL 237. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BEAM — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5324, FOUND RT UPPER WHEEL WELL BEAM ASSY WEB CRACKED AT FS 532, RBL 61, WL 237. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FASTENER — LOOSE (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC551, FOUND HORIZONTAL STAB UPPER SKIN PATCH WITH SMOKING RIVETS AT FS 1097, HSS 161L WL 282. REPAIRED IAW SRM 55-20-01.
Part: SKIN — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB UPPER SKIN PANEL CRACKED IN 3 AREAS AT FS 1041-FS 1063, HSS 59R, WL 284. REPAIRED IAW LAC MEA 382-55-25-044.
Part: SKIN — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL UPPER SKIN PANEL CRACKED AT FS 1063 HSS 59L, WL 284. REPAIRED IAW LAC MEA 382-55-25-043.
Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB LOWER SKIN PANEL INTERIOR MATTING SURFACE TO THE BULKHEAD CAP CORRODED AT FS 1066, RBL 30 TO RBL 33. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND HORIZONTAL STAB INTERIOR FITTING CORRODED AT FS 1047, LBL 6, WL 278. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BULKHEAD WEB — CRACKED (ZONE 200) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5315, FOUND BS 946 RT UPPER BULKHEAD WEB CRACKED AT RBL 19, WL 278. REPAIRED IAW SRM 51-140-17.
Part: BULKHEAD WEB — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5315, FOUND BS 880 LT BULKHEAD LOWER LIGHTENING HOLE CRACKED AT LBL61, WL190. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5315, FOUND FS 814 LT LOWER ATTACHMENT TEE FITTING CRACKED AT LBL 62, WL 170. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5313, FOUND RT CARGO FLOOR END FITTING UNDER CHINE CAP CRACKED AT FS 717, RBL 61, WL 140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (ZONE) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5313, FOUND LT CARGO FLOOR END FITTING UNDER CHINE CAP CRACKED AT FS 717, LBL 61, WL 140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (ZONE 500 AILERON) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LT AILERON LOWER FORWARD SKIN CORRODED AT AS55.4L TO AS143.6L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (ZOEN 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5313, FOUND RH CARGO FLOOR END FITTING UNDER CHINE CAP CRACKED AT FS 797.0E, RBL 61, WL 140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: PLATE — CHAFED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5211, FOUND CARGO FLOOR RAMP END PLATE CHAFED AT BS 817.0E, LBL 48 TO RBL 36, WL 145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CRACKED (ZONE 600 FLAP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5712, FOUND RT INBOARD FLAP UPPER CENTER SKIN CRACKED AT CWS121R. REPAIRED IAW SMP583 SRM, FIGURE 51-140-12.
Part: SKIN — CRACKED (ZONE 600 FLAP) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5712, FOUND RT INBOARD FLAP UPPER SKIN TRAILING EDGE CRACKED AT CWS150R. REPAIRED IAW SMP583 SRM, FIGURE 51-140-12.
Part: LUG — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5323, FOUND LT MLG UPPER BULKHEAD BOW BEAM LOWER LUG CRACKED AT FS 537, LBL 62, WL 201. REPAIRED IAW SMP583 SRM, FIGURE 53-40-14.
Part: RISER PANEL — CRACKED (ZONE 100) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5323, FOUND LT MLG WHEEL WELL UPPER BULKHEAD RAISER PANEL CRACKED AT BS 487, LBL 61, WL 216. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.
Part: SKIN — CORRODED (ZONE 500 AILERON) · corrosion level 2 · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5711, FOUND LH AILERON LOWER FORWARD SKIN CORRODED AS143.6L TO AS214L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0778.
Part: FORMER — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STAB LT LEADING EDGE FORMER CRACKED AT FS1045, HSS90L, WL285. REPAIRED IAW SMP583 SRM, FIGURE 51-140-20. NR# 0774.
Part: SKIN — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND LH ELEVATOR LEADING EDGE SKIN CRACKED AT FS1106, HSS258L WL280. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0772.
Part: SKIN — CRACKED (ZONE 300) · airframe 43,251 hrs · 26,493 cycles
DURING SCHEDULED C-3 CHECK UNDER JOB CARD HC5511, FOUND LH ELEVATOR LEADING EDGE SKIN CRACKED AT FS1106, HSS223L, WL280. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 0771.
Earlier reports · 2019–2025 · 607 reports
2025
Part: STIFFENER — CRACKED (ZONE 800) · airframe 42,801 hrs · 26,206 cycles
DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5302, FOUND CREW ENTRY DOOR STIFFENER CRACKED ON THE THIRD STEP. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001224104.
Part: ATTACH FITTING — BROKEN (ZONE 200) · airframe 42,801 hrs · 26,206 cycles
DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5302, FOUND VERTICAL STRUT ATTACH FITTING BROKEN AT FS813, LBL61, WL263. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001224171.
Part: STEP — CRACKED (ZONE 800) · airframe 42,801 hrs · 26,206 cycles
DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5302, FOUND CREW ENTRY DOOR STEP CRACKED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001224102.
Part: FORMER — CORRODED (ZONE 800) · corrosion level 2 · airframe 42,801 hrs · 26,206 cycles
DURING SCHEDULED B-3 CHECK UNDER JOB CARD HB5302, FOUND CENTER OVERHEAD EMERGENCY EXIT DOOR FORMER CORRODED AT FS637-657, BL0-LBL20, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001224122.
2024
Part: BULKHEAD — CRACKED (ZONE 100) · airframe 42,663 hrs · 26,129 cycles
DURING PREFLIGHT FOR SCHEDULED FLIGHT LYC130, FOUND FS1012 RH BULKHEAD CRACKED. LP #57821. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. LOGPAGE 57821 ITEM #1.
Part: GENERATOR — FAILED (NR 3) · airframe 42,663 hrs · 26,126 cycles
DURING SCHEDULED FLIGHT LYC2156, #3 GENERATOR BEARING FAILURE LIGHT ILLUMINATED. SHUTDOWN #3 ENGINE @2354 IAW QRH. EMERGENCY DECLARED. LP #57820. / REMOVED AND REPLACED #3 ENGINE GENERATOR. OPS CHECK GOOD. REF: SMP581 CH24-20 & HN7101B
Part: FORMER — CRACKED (ZONE 500) · airframe 42,624 hrs · 26,099 cycles
DURING SCHEDULED INSPECTION 24 INCH HORIZONTAL CRACK IN LEFT HAND WING TRAILING EDGE FORMER FLAP STATION 118. VERTICAL CRACKS IN FORMER AT 45.5, 49.5 AND 54 INCHES AFT OF REAR BEAM. / REPLACED FORMER SMP583 51-10 AND 57-60-03. / LP 57802
Part: BULKHEAD WEB — CRACKED (BS 943) · airframe 42,102 hrs · 25,756 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND FS946 UPPER BULKHEAD ASSEMBLY WEB CRACKED AT RBL18, WL280. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR# 1001116294. / PSE# 53-50-09, AD 2012-06-09
Part: BULKHEAD — CRACKED (BS 990) · airframe 42,102 hrs · 25,756 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND FS990 RH BULKHEAD ASSEMBLY TEE CRACKED AT RBL69, WL250. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-16. NR# 1001128506. / PSE# 53-50-07, AD 2012-06-09
Part: FRAME — CRACKED (BS 1023) · airframe 42,102 hrs · 25,726 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FS1023 UPPER RING SEGMENT CRACKED AT LBL20, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1001124830. / PSE# 53-50-09, AD 2012-06-09
2023
Part: RING — CRACKED (RH AFT) · airframe 41,456 hrs · 25,504 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB 5302, FOUND FS979 RH RING SEGMENT CRACKED AT RBL66, WL265. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-07. NR# 1000939823.
2022
Part: BULKHEAD WEB — CRACKED (BS 880 LBL62-75) · airframe 41,228 hrs · 25,440 cycles
DURING SCHEDULED INSPECTION FOUND CRACK IN WEBBING AND BULKHEAD LEFT SIDE FUSELAGE FS880 LBL62-75 WL213 / REPAIR ACCOMPLISHED IAW SMP583 SRM 51-140-17.
Part: DOUBLER — CORRODED (BS 202) · corrosion level 2 · airframe 41,004 hrs · 25,353 cycles
DURING N409LC NOSE WHEEL WELL STRUCTURAL REPAIR, FOUND CORROSION ON THE DOUBLER ABOVE THE CREW DOOR AT FS202, LBL85, WL195. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-30-30. NR# 0036 / PSE# 53-30-08, AD 2012-06-09
Part: BEAM — CRACKED (NLG WW) · airframe 41,004 hrs · 25,353 cycles
DURING N409LC NOSE WHEEL WELL STRUCTURAL REPAIR, FOUND NLG WHEEL WELL WL195 BEAM CRACKED AT FS165, LBL70. / REPAIRED IAW LAC MEA 382-53-22-101. NR# 0034.
Part: SKIN — CORRODED (BS 165-205) · corrosion level 2 · airframe 41,004 hrs · 25,353 cycles
DURING N409LC NOSE WHEEL WELL STRUCTURAL REPAIR, FOUND FUSELAGE SKIN INNER SURFACE CORRODED AT FS165-205. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0037.
Part: ANGLE — CRACKED (NLG WW) · airframe 41,004 hrs · 25,353 cycles
DURING N409LC NOSE WHEEL WELL STRUCTURAL REPAIR, FOUND FS196 BULKHEAD ANGLE CRACKED AT LBL73, WL185. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-23. NR#0035 / PSE# 53-30-11, AD 2012-06-09
Part: BULKHEAD — CRACKED (NLG WW) · airframe 41,004 hrs · 25,353 cycles
DURING N409LC NOSE WHEEL WELL STRUCTURAL REPAIR, FOUND NLG WHEEL WELL LH FS165 BULKHEAD CRACKED THROUGH FASTENER HOLE WITH CORROSION AT WL171. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC#0013
Part: FRAME SPLICE — DENTED · airframe 40,989 hrs · 25,349 cycles
DURING SCHEDULED FLIGHT DURING ENGINE START AIRCRAFT ROLLED FORWARD STRIKING A TRUCK ON THE LEFT FORWARD SIDE OF THE AIRCRAFT / AIRCRAFT FERRIED TO MAINTENANCE FACILITY. LP 36212
Part: FRAME — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC3215, FOUND NLG WHEEL WELL FS157 FRAME CRACKED AT LBL47, WL157. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-19. NR# 0096. / PSE# 53-30-08, AD 2012-06-09
Part: BULKHEAD WEB — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5316, FOUND FS477 OVERHEAD BULKHEAD WEB CRACKED AT LBL33, WL260-285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0079. / PSE# 53-40-19, AD 2012-06-09
Part: CARGO TRACK — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5314, FOUND CARGO FLOOR RH FS677.0E 25,000LBS TIE DOWN FITTING CRACKED AT RBL61, WL141-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0063. / PSE# 53-40-11, AD 2012-06-09
Part: CARGO TRACK — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5314, FOUND CARGO FLOOR RH FS397 25,000LBS TIE DOWN FITTING CRACKED AT RBL61, WL141-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0064. / PSE# 53-40-11, AD 2012-06-09
Part: CARGO TRACK — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5314, FOUND CARGO FLOOR RH FS777.0E 25,000LBS TIE DOWN FITTING CRACKED AT RBL61, WL141-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0062. / PSE# 53-40-11, AD 2012-06-09
Part: CARGO TRACK — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5314, FOUND CARGO FLOOR LH FS337.0E 25,000LBS TIE DOWN FITTING CRACKED AT LBL61, WL141-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0066. / PSE# 53-40-11, AD 2012-06-09
Part: CAP — CORRODED (BULKHEAD) · corrosion level 2 · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5314, FOUND FS497 BULKHEAD UPPER CAP ANCHOR NUTS CORRODED AT LBL60 TO RBL60, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0099. / PSE# 53-40-11, AD 2012-06-09
Part: SHROUD — CRACKED (LT AILERON) · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5711, FOUND LH AILERON LEADING EDGE SHROUD WITH MULTIPLE CRACKED AND DENTS AT AS0L TO AS562L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0193.
Part: BULKHEAD WEB — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5315, FOUND FS880 BULKHEAD WEB CRACKED AT LBL68, WL220. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR# 0067. / PSE# 53-50-07, AD 2012-06-09
Part: SKIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5711, FOUND LH AILERON UPPER SKIN PANEL BULGING AT AS55.4L TO AS143.6L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0194.
Part: CARGO TRACK — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5314, FOUND CARGO FLOOR LH FS397 25,000LBS TIE DOWN FITTING CRACKED AT LBL61, WL141-143. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0065. / PSE# 53-40-11, AD 2012-06-09
Part: CAP — CORRODED (BULKHEAD) · corrosion level 2 · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5314, FOUND FS437 BULKHEAD UPPER CAP ANCHOR NUTS CORRODED AT LBL60 TO RBL60, WL145. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0098. / PSE# 53-40-11, AD 2012-06-09
Part: RING — CRACKED (FUSELAGE) · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5317, FOUND FS817.0E RING SEGMENT CRACKED AT LBL72, WL157. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-40-46. NR# 0201. / PSE# 53-40-01, AD 2012-06-09
Part: FITTING — CRACKED (ZONE 200) · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC3215, FOUND NLG ATTACHMENT FITTING ASSY CRACKED AT FS196, LBL3, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0053
Part: FRAME — CRACKED · airframe 40,794 hrs · 25,223 cycles
DURING SCHEDULED C-2 CHECK UNDER JOB CARD HC3215, FOUND NLG WHEEL WELL FS140 FRAME EXISTING REPAIR CRACKED AT LBL45, WL157. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-19. NR# 0097. / PSE# 53-30-08, AD 2012-06-09
2021
Part: RISER — CRACKED (BS 477 RBL 61-85) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB3200, FOUND FS477 RH BULKHEAD WEB HAS MULTIPLE CRACKS IN THE NUTPLATE HOLES AT WL219, RBL78. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0101. / PSE# 53-40-19, AD 2012-06-09
Part: CAP — CRACKED (BS 902 BLKHD) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND FS902 RH BULKHEAD INBD LOWER CAP CRACKED AT WL210-270, RBL63. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0132. / PSE# 53-50-07, AD 2012-06-09
Part: WEB — CRACKED (BS 560-597) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB3200, FOUND FS573 & FS589 LH MLG WHEEL WELL LONGERON SHELF WEB RADIUS CRACKED AT WL200, LBL73 . / REPAIRED IAW LAC MEA 382-53-06-029 R2. NR# 0106. / PSE# 53-40-16, AD 2012-06-09
Part: FITTING — CRACKED (LT MLG WW) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB3200, FOUND LH MLG WHEEL WELL FS557 BOW BEAM LOWER FITTING CRACKED AT WL143.5, LBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0131. / PSE# 53-40-14, AD 2012-06-09
Part: TIE DOWN — CRACKED (BS 477 RBL 61) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS477 RH FWD LOWER STRUT ATTACH FITTING (25K LBS. TIEDOWN FITTING) CRACKED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0092 / PSE# 53-40-23, AD 2012-06-09
Part: FITTING — CRACKED (BULKHEAD) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND THE FS990 LH SIDE BULKHEAD LOWER FORWARD FITTING CRACKED; WL250, LBL63. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0087. / PSE# 53-50-07, AD 2012-06-09
Part: FITTING — CRACKED (BS 557 RT MLG WW) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB3200, FOUND RH MLG WHEEL WELL FS557 BOW BEAM LOWER FITTING CRACKED AT WL143.5, RBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0130. / PSE# 53-40-14, AD 2012-06-09
Part: BEAM — CRACKED (BS 497 LT MLG WW) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB3200, FOUND LH MLG WHEEL WELL FS497 BOW BEAM LOWER FITTING CRACKED AT WL143.5, LBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0128. / PSE# 53-40-14, AD 2012-06-09
Part: SKIN — CORRODED (LT AILERON) · corrosion level 3 · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND LH AILERON AS143 TO AS214 LOWER FORWARD SKIN PANEL CORRODED IN SEVERAL PLACES. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0089. / PSE# 57-50-21, AD 2012-06-09
Part: RISER — CRACKED (BS 477 LBL 71) · airframe 40,218 hrs · 24,861 cycles
DURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5302, FOUND THE FS477 LH SIDE BULKHEAD WEB RISER PANEL CRACKED AT WL220, LBL71. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0082. / PSE# 53-40-19, AD 2012-06-09
2020
Part: HINGE — BROKEN (RT MLG DOOR) · airframe 39,830 hrs · 24,700 cycles
RT MLG DOOR CAME UNSECURED IN FLIGHT. INSPECTED RT MLG DOOR IDENTIFIED 3 BROKEN HINGE LOBES ON CENTER HINGE. DAMAGE CLASSIFIED AS SECONDARY STRUCTURE, IAW SRM 583 53-10. FUSELAGE STA APPROXIMATELY 547, INSPECT FREQUENTLY. THIS ITEM IS PLACED ON CARRY OVER 01011.
Part: PUMP — FAULTY (HYDRAULIC SYS) · airframe 39,659 hrs · 24,659 cycles
DURING SCHEDULED FLIGHT SHORTLY AFTER TAKE OFF UTILITY SUCTION BOOST PUMP LIGHT ILLUMINATED. RESEVOIR FOUND EMPTY. EMERGENCY LANDING / RESEALED #1 ENGINE HYDRAULIC PUMP PRESSURE SIDE ELBOW. IAW LOCKHEED SMP581, 29-00. LP 46548.
Part: FITTING — CRACKED (DOOR LOCK) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND CRACKED DOOR LOCK FITTING AT RAMP CUTOUT, FS792, WL162, LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000150040.
Part: TEE FITTING — CRACKED (BS 858 BULKHEAD) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS858 LH SIDE BULKHEAD TEE (INBOARD CAP) CRACKED AT WL198, LBL69. / REPAIRED IAW LAC MEA 382-53-20-018. NR# 1000151181. / AD 2012-06-09, PSE# 53-50-07.
Part: BULKHEAD WEB — CRACKED (BS 902) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS902 RH SIDE BULKHEAD WEB CRACKED AT WL230, RBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000151719.
Part: BULKHEAD WEB — CRACKED (BS 935) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS935 LH SIDE BULKHEAD J-SECTION (WEB) CRACKED AT WL256, LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000151720.
Part: TEE FITTING — CRACKED (BS 792 BULKHEAD) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS792 RH BULKHEAD INBOARD CAP (TEE) CRACKED AT WL166, RBL65. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-14. NR# 1000151183. / AD 2012-06-09, PSE# 53-50-07.
Part: FITTING — CRACKED (DOOR LOCK) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND CRACKED DOOR LOCK FITTING AT RAMP CUTOUT, FS858, WL176, RBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000150036.
Part: RIB — CRACKED (LT ELEVATOR) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH ELEVATOR HSS89L RIB LOWER FLANGE WITH CRACKED FASTENER HOLE AT FS1117. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-20. NR# 1000153065.
Part: FITTING — CRACKED (DOOR LOCK) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND CRACKED DOOR LOCK FITTING AT RAMP CUTOUT, FS770, WL156, LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000150044.
Part: SPAR — CORRODED (RT ELEVATOR) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH ELEVATOR FORWARD SPAR WEB CORRODED AT THE LOWER INBOARD SPAR RAIL, HSS51-56R, FS1108. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-17. NR# 1000151823.
Part: RIB — CRACKED (LT ELEVATOR) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH ELEVATOR HSS89L RIB LOWER FLANGE WITH CRACKED FASTENER HOLE AT FS1145. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-20. NR# 1000153064.
Part: TEE FITTING — CRACKED (BS 814 BULKHEAD) · airframe 39,575 hrs · 24,634 cycles
DURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5302, FOUND THE FS814 RH BULKHEAD INBOARD CAP (TEE) CRACKED AT WL170, RBL65. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 53-50-14. NR# 1000151182. / AD 2012-06-09, PSE# 53-50-07.
2019
Part: BULKHEAD WEB — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING IRAN ON REPLACEMENT RAMP (REF WO# SV 26611), FOUND RAMP DOOR REAR BHD WEB WARPED WITH INCORRECT REPAIR AT RS10.6 AND LBL27-RBL27. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: CONTROL UNIT — FAILED (FIRE WARNING) · airframe 38,910 hrs · 24,094 cycles
DURING SCHEDULED FLIGHT WHILE IN DESCENT #2 FIRE LIGHT ILLUMINATED. FALSE FIRE INDICATION. REPLACED #2 FIRE DETECTION CONTROL UNIT IAW SMP 581 26-10 LP #42909
Part: SPAR — CRACKED (LT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT OUTER WING FRONT SPAR WEB WITH CRACKS AT PIN RIVET HOLES OWS69. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6659.
Part: STRUT — CORRODED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5323 FOUND EXFOLIATION CORROSION ON LH MLG WHEEL WELL FS617 SIDE BULKHEAD STRUT ASSY FS617 LBL62 WL140 TO WL150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FORMER — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CTR PRESSURIZE SKIN PANEL ATTACHMENT FORMER WITH 2-4" CRACKS AT FS597-617, WL284, LBL17, AND RBL17. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6105.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LBL30 & RBL30 FWD LONGERONS CORRODED AT FS196, WL130. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2852.
Part: GUSSET — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR HINGE FITTING TO REAR BHD GUSSET LT/RT CRACKED AT FS1034 LBL45-60, AND RBL45-60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6087
Part: GUSSET — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR BHD TO LOWER SKIN GUSSET LT REAR CRACKED AT FS990 AND LBL45-60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6083.
Part: SKIN — WRINKLED (BS 491-617) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BOTTOM LH MAIN WHEEL WELL FAIRING WRINKLED, AND CRACKED WITH MULTIPLE REPAIR AT FS491 TO FS617, WL135, AND LBL45 TO LBL85. / REPAIRED IAW LAC MEA 382-53-06-097.
Part: STRAP — CORRODED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING CWS56L AND CWS56R DRAIN TROUGH INTERIOR DOUBLERS (STRAPS) CORRODED; FS597, WL256. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6164.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS397 RT RING SEGMENT WITH ELONGATED HOLES, WL156. REPAIRED IAW SRM FIG. 51-140-21. NR# 6245.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RH FS357 RING SEGMENT WITH ELONGATED HOLES AT WL160, RBL75. REPAIRED IAW SRM FIG. 51-140-21. NR# 2716.
Part: SKIN — DAMAGED (BS 889-902) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH AFT FUSELAGE RIVET MISSING WITH MULTIPLE REPAIR DOUBLERS AT FS889 TO FS902, WL180 TO WL230, AND RBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.
Part: SKIN — CHAFED (LT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE LT ELEVATOR LEADING EDGE SKIN CHAFED AND WITH MULTIPLE CRACKS AT HSS51-180L. FS1095. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6287.
Part: STIFFENER — DAMAGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND THE LT OUTBOARD WING OWFS28L FLAP TRACK FORWARD STIFFENER LOWER BOLT HOLE ELONGATED; FS597. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6254.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC2485, FOUND THE FS836 BULKHEAD UPPER FLANGE (ZEE) CRACKED IN RADIUS, LBL20 & RBL20, WL282. REPAIRED IAW SRM FIG. 53-50-06. NR# 2485.
Part: FRAME — ELONGATED (BS 370) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS370 RH RING SEGMENT WITH ELONGATED HOLES AT WL160, RBL75. REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-21.
Part: SKIN — CRACKED (BS 160) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE LH FWD FUSELAGE EXTERIOR SKIN CRACKED AT FS160, WL236, LBL65. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2097. / PSE# 53-30-08, AD 2012-06-09
Part: RISER PANEL — CRACKED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT UPPER MAIN WHEEL WELL BULKHEAD RISER PANEL CRACKED AT FS617, WL250, LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6313.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND THE UNDERDECK FS196 LBL28 WL146 FLOOR SUPPORT CORRODED, LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2493.
Part: SKIN — DENTED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR EXTERIOR SKIN DENTED WITH SCRATCH MARKS 36" AND PRESSURE VALVE DOUBLER CRACKED AT FS990 AND LBL30-RBL10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6086.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS337 RT RING SEGMENT WITH ELONGATED HOLES AT WL150-161, RBL63-82. REPAIRED IAW SRM FIG. 51-140-21. NR# 2721.
Part: WINDOW FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT SIDE WINDOW FRAME FWD POST #3 WITH MULTIPLE ELONGATED HOLES; FS116-127, LBL35-42, WL231-251. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2850.
Part: FITTING — CRACKED (BS 739) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314 FOUND STRESS CORROSION CRACKING ON SKIN FITTING FS 739 WL140 RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP UPPER SKIN CORRODED WITH INCORRECT REPAIR PATCHES AT OWS176-228. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6492.
Part: STRUT — ELONGATED (BS 858 BULKHEAD) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE RH AFT FUSELAGE FS858 BULKHEAD STRUT WITH ELONGATED HOLES; RBL62, WL200-270. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: DOUBLER — CORRODED (BS 597 BULKHEAD) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE FS597 UNDERFLOOR BULKHEAD RH PORK CHOP FITTING DOUBLER CORRODED, RBL50-60, WL140. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2879.
Part: SKIN — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE LT FWD FUSELAGE SKIN CRACKED NEAR EXTERNAL POWER RECEPTACLE FORWARD EDGE, FS156-158, LBL45, WL150. REPAIRED IAW SRM FIG. 51-140-12. NR# 6069.
Part: SUPPORT — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND BELLY TEE SUPPORT WITH TOO MANY ELONGATED HOLES AT FS257-277 AN RBL10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6569.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS777.0E RT RING SEGMENT CRACKED AT WL265, RBL61. REPAIRED IAW SRM FIG. 53-40-11. NR# 2478.
Part: SKIN — CANNING (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER TRAILING EDGE SKIN CANNING WITH MULTIPLE ELONGATED HOLES AT OWS0-8. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6584.
Part: CAP — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS277.0E UNDERFLOOR BULKHEAD LOWER CAP CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2583.
Part: RETAINER — CORRODED (HATCH SEAL) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE AFT HATCH SEAL RETAINER CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT OUTBD FLAP UPPER TRAILING EDGE SKIN CORRODED AT OWS30-97. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6578.
Part: SKIN — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT INBD FLAP LOWER SKIN CRACKED IN 3 PLACES AT FS212-220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6475.
Part: SKIN — CRACKED (BS 235) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FORWARD FUSELAGE RH SKIN WITH REDUNDANT HOLE AT FS235, WL206, RBL85. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-10. NR# 2902.
Part: SKIN — BULGED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTERWING BOX REAR LOWER PLANK BULGED SKIN SURFACE BEHIND #3 ENGINE EXHAUST . REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CANNING (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RT OUTBOARD FLAP LOWER TRAILING EDGE SKIN DRESS UP DENTS WITH CANNING AND INCORRECT REPAIR AT OWS103-164. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6701.
Part: ANGLE — CORRODED · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RH FWD CHINE ANGLE CORRODED AT FS245.0E TO FS345.0E, RBL61, WL141. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2099.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND EXT BELLY SKIN WARPED WITH DEEP PITTING CORROSION AT FS245-297, WL126, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2191.
Part: FRAME — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RT FS384 RING SEGMENT CORRODED AND CRACKED AT WL142, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2722.
Part: SKIN — BENT (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND THE LT INBOARD FLAP UPPER TRAILING EDGE SKIN BENT AND WITH ELONGATED RIVET HOLES. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6457.
Part: RIB — DAMAGED (HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LT LEADING EDGE HSS75L RIB LOWER END WITH ELONGATED HOLES. FS1040, WL260. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6456.
Part: LONGERON — CORRODED (BS 477-580) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RH MAIN WHEEL WELL WL200 SHELF LONGERON CORRODED, FS553-561, RBL83. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: INTERCOSTAL — DAMAGED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN LANDING GEAR WHEEL WELL FS477-517 WL200 INTERCOSTAL BEAM OUTBOARD CAP WITH ELONGATED HOLES. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6449.
Part: BEAM — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS497 RT LOWER BOW BEAM OUTBOARD CAP WITH ELONGATED HOLES, RBL65. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6259.
Part: ACCESS PANEL — CRACKED (LT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE LT ELEVATOR LEADING EDGE ACCESS PANELS CORRODED AND CRACKED. FS1095. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6286.
Part: FITTING — DAMAGED (NR 3 ENGINE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT AUX TANK #3 ENGINE TRUSS UPPER TANK DRAG FITTING HOLE ELONGATED AT CWS176. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6151.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CABIN LT BHD TO CTR WING FITTING CRACKED AT FS517, WL287, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6119.
Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR BHD WEB CRACKED AT FS990 AND LBL20-40. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6149.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS657 RT RING SEGMENT WITH ELONGATED HOLES AT WL158-161, RBL73-76. REPAIRED IAW SRM FIG. 51-140-23. NR# 2734.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND THE FS202 UNDERDECK LBL28 LOWER LONGERON CORRODED; WL128. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2492.
Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR LT REAR BHD RT DOUBLER CRACKED AT FS1034 AND RBL50-60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6075.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND UNDERFLOOR BEAM LOWER CAP CORRODED AT FS337.0E, WL126-140, AND RBL3-6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2320.
Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND LT HOR STAB LEADING EDGE EXT SKIN WITH MULTIPLE CRACK AFTER DRESSED UP DEFORMED EDGES AT HSS296. REPAIRED IAW SRM FIG. 51-140-14. NR# 6579.
Part: FITTING — CRACKED (BS 817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS 817 RH HOCKEY STICK FITTING CRACKED, RBL58, WL140-150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — DAMAGED (NR 3 ENGINE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND #3 ENGINE TRUSS INBD MOUNT OUTBD DRAG FITTING WITH 2 ELONGATED HOLES AT CWS178.8. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6128.
Part: SPAR WEB — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CTR WING REAR SPAR WEB 3" CRACK CLOSE TO PREVIOUSLY REPAIR PATCH BEAM ATTACHMENT AREA AT FS597, WL255-285, AND RBL61-157. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6113.
Part: SKIN — CORRODED (RAMP DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR EXTERIOR SKIN CORRODED & WARPED, RAMP STATION 6 TO RAMP STATION 10, LBL4-RBL4. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RH FS437 RING SEGMENT WITH ELONGATED HOLES AT WL185, RBL83. REPAIRED IAW SRM FIG. 51-140-21. NR# 2725.
Part: ATTACH ANGLE — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT FS617 OVERHEAD BULKHEAD TO LBL61 VERTICAL ATTACH ANGLE WITH ELONGATED HOLES; WL265-285, LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6243.
Part: WINDOW FRAME — CRACKED (BS 427) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO COMPARTMENT LH FS 427 WINDOW FLANGE CORRODED, WL200, LBL82. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT UPPER FLOOR BEAM UPPER SURFACE WITH MINOR CORROSION AT FS737 AND LBL50-RBL50. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2439.
Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND VERTICAL ATTACH ANGLE CRACKED BOTH UPPER AND LOWER END AT LT CWS220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6723.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS924 RT BULKHEAD INBOARD CAP CORRODED AT WL195, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2476.
Part: INTERCOSTAL — CRACKED (RT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT MAIN WHEEL WELL INTERCOSTAL BEAM OUTBD CAP AND WEB CRACKED AND CORRODED AT FS497-517 AND WL215-230. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6586.
Part: CAP — CORRODED (RAMP DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RAMP DOOR LT FLOOR PLATE (CHINE CAP) CORRODED BEYOND LIMITS AT MULTIPLE PLACES. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6211.
Part: CAP — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR BHD LOWER CAP LT AND RT DOUBLER CRACKED AT FS902, RBL61, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6071.
Part: SUPPORT — DEFORMED (BS 777) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS777.0E UNDERFLOOR BULKHEAD WEB LBL20 & RBL2 SUPPORTS AND BL0 BRACE WERE DEFORMED & CRACKED, WITH ELONGATED HOLES; WL130-145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WARPED AND WITH MULTIPLE REPAIR DOUBLERS AT FS497-537, WL126, AND RBL61-LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2156.
Part: ATTACH FITTING — CRACKED (BS 497) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND INBOARD CAP ATTACHMENT FITTING CRACKED ON FS497 BOW BEAM. FS497 WL205. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: DOUBLER — CORRODED (BS 205 BULKHEAD) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE UNDERDECK FS205 BULKHEAD REINFORCE DOUBLER CORRODED, LBL56, WL145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS667 RING SEGMENT WITH ELONGATED HOLES AT WL150-161, LBL68-75. REPAIRED IAW SRM FIG. 51-140-23. NR# 2737.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245.0E UNDERFLOOR BULKHEAD RH END FITTING CORRODED; RBL61, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2719.
Part: RIB — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND THE LT INBD FLAP OUTBOARD RIB CRACKED AT CWS213L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6460.
Part: CAP — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND LT CHINE CAP WITH 2.5" CRACK AND REPAIR DOUBLER AT FS737.0E-817.0E. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2313. / PSE# 53-40-10, AD 2012-06-09
Part: RISER PANEL — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO AIR CONDITIONING COMPARTMENT FS477-497 RBL61 BULKHEAD WEB (EXTRUDED RISER PANEL) WARPED, WITH TEMPORARY REPAIR AT WL201, FS482. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6266.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WITH MULTIPLE SCRATCHES AND CORROSION AT FS245.0E-297.0E, WL126, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2190.
Part: FLOORBOARD — WARPED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR FLOORBOARD WARPED, CORRODED AND STIFFENER BENT AT C1, C2 AND C-3. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2071.
Part: FORMER — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND TRAILING EDGE FORMER CRACKED AT LH CWS220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6724.
Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT SIDE WINDOW FRAME FWD POST #3 WITH MULTIPLE ELONGATED HOLES; FS116-127, RBL35-42, WL231-251. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2848.
Part: STIFFENER — CRACKED (HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STABILIZER LOWER SKIN INNER STIFFENER CRACKED AT FS1075-1095. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6093.
Part: FRAME — CORRODED (BS 257) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314 FOUND EXFOLIATION CORROSION ON RING SEGMENT FS257 LBL62 TO LBL85 WL140 TO WL200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BULKHEAD — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP DOOR REAR BHD WEB WARPED WITH INCORRECT REPAIR AT RS10.6 AND LBL27-RBL27. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2018.
Part: RETAINER — CORRODED (HATCH SEAL) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER HATCH SEAL RETAINER AND INNER FLANGE CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: STRINGER — DAMAGED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING STRINGER #14 (FS532.5) FORWARD FLANGE WITH AN ELONGATED HOLE AT CWS60L. WL257. REPAIRED IAW MEA 382-57-18-196. NR# 6349.
Part: RIB — CORRODED (LT AILERON) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT AILERON INTERIOR RIB LOWER CAP CORRODED AT AS117. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6570.
Part: ANGLE — CORRODED (MLG FAIRING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT MAIN WHEEL WELL REAR FAIRING INNER RIB REINFORCE ANGLE CORROSION EXCEEDED LIMITS FS637 WL165. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6434.
Part: DOUBLER — CRACKED (MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CABIN FS577-588 MAIN LANDING GEAR SHAFT BRACKET MOUNTING POINT DOUBLERS CRACKED AT WL126, LBL65 AND RBL65. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6443.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WITH MULTIPLE STONE MARKS AND SURFACE CORROSION WITH TEMPORARY REPAIR AT FS457-497, WL126, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2188.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245.0E-FS250.0E WL236 LBL74 INTERCOSTAL BEAM CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6229.
Part: SKIN — CORRODED (RAMP DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP DOOR LEADING EXTERIOR SKIN WARPED AND CORRODED; RAMP STA 0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2500.
Part: CAP — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR LT BEAM LOWER CAP CRACKED AT FS1034 AND LBL0-60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6072.
Part: SKIN — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP UPPER SKIN CRACKED AT OWS267. REPAIRED IAW SRM FIG. 51-140-12. NR# 6583.
Part: BEAM — CORRODED (RT MLG) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT MLG BEAM CORRODED WITH MULTIPLE ELONGATED HOLES AT FS517 AND WL160-200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6584.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT FS880 BULKHEAD WEB REPLACEMENT NECESSARY FOR EXISTING TEMPORARY REPAIR. FS880 RBL61 TO RBL85 WL200 TO WL265. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6379.
Part: RIB — WARPED (RT AILERON) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND THE RT AILERON STATION 143R RIB TO REAR SPAR CLIP WARPED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6160.
Part: SKIN — WARPED (LT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD SKIN WARPED WITH MULTIPLE DENTS AND I9NCORRECT REPAIR AT OWS103-170. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6503.
Part: RAMP — CORRODED · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR STATION 10.6 REAR BULKHEAD UPPER CAP CORRODED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2070.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS397 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2753.
Part: BEAM — CRACKED (LT MLG) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HAIRLINE CRACK ON LT MAIN LANDING GEAR BEAM FS517 WL265 LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6416.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT LOWER CAP CORRODED AT FS657, WL126-140, AND BL0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2428
Part: RIB — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RH OUTBOARD FLAP LEADING EDGE RIB CRACKED WITH MULTIPLE ELONGATED HOLES AT OWS183-192. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6662.
Part: RIB — CORRODED (BS 337-357) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313 FOUND WINDOW RIB INTERCOSTAL SUPPORT CORRODED FS337 TO FS357 LBL82 AND RBL62 WL185. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BEAM — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR RT BEAM WEB CRACKED, FS1014-1020, RBL60. REPAIRED IAW SRM FIG. 51-140-17. NR# 6166.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT UPPER FLOORBEAM CAP AT INTERIOR CHINE CAP CORRODED AT FS517, WL146, AND RBL56. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2404.
Part: FITTING — CRACKED (RT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT MAIN WHEEL WELL RING SEGMENT SPLICE FITTING WITH EXFOLIATION CORROSION FS627 RBL61 WL256. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6424.
Part: RISER PANEL — DAMAGED (LT M LG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN WHEEL WELL FS477-517 BULKHEAD WEB (EXTRUDED RISER PANEL) WITH ELONGATED HOLES, WL175-200. LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6451.
Part: SKIN — CORRODED (RT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD WING LOWER TRAILING EDGE SKIN SURFACE BULGED WITH SUNKEN RIVETS AND CORROSION AT FS597-617, WL560, AND OWS0-84, REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2235.
Part: DOUBLER — DAMAGED (LT M LG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN WHEEL WELL FS517-528 WL148 AND WL218 REINFORCE DOUBLERS WITH ELONGATED HOLES AND CHAFED. LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6442.
Part: TEE FITTING — CORRODED (FLAP TRACK) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD WING REAR BEAM FLAP TRACK ATTACHMENT TEE FITTING UPPER AREA CORRODED AT OWS100. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2311.
Part: SKIN — DAMAGED (RUDDER) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND RUDDER SKIN WITH TEMPORARY REPAIR AT FS1128-1140 AND VSS251-270. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2330.
Part: TEE FITTING — CORRODED (FLAP TRACK) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD WING REAR BEAM FLAP TRACK ATTACHMENT TEE FITTING UPPER AREA CORRODED AT OWS100. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2310.
Part: STIFFENER — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING FRONT SPAR WEB CWS178L VERTICAL STIFFENER CRACKED. FS517, WL263-285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6374.
Part: STRINGER — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTER WING FS538 STRINGER #15 LAYER CRACKED, CWS52L, WL257. REPAIRED IAW MEA 382-53-18-199. NR# 6224.
Part: CHANNEL — DAMAGED (RT AILERON) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT AILERON U CHANNEL WARPED WITH MULTIPLE ELONGATED HOLES. AS90 TO AS562 REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6399
Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT UPPER MAIN WHEEL WELL FS497-517, WL215 AND WL230 INTERCOSTAL BEAM WEB CORRODED BEYOND LIMITS; LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6294.
Part: RIB — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT INBD FLAP LOWER SKIN INNER RIB WITH MULTIPLE CRACKS AND WARPS AT CWS178. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6619.
Part: BULKHEAD WEB — CRACKED (BS 245) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245.0E UNDERFLOOR BULKHEAD WEB CRACKED AT LBL54, WL126-142. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2884.
Part: BULKHEAD — CRACKED (NLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE NOSE WHEEL WELL AFT BULKHEAD WARPED/CRACKED AT FS180, LBL28. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2093. / PSE# 53-30-10, AD 2012-06-09
Part: STRUCTURE — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR TRAILING EDGE SHELF CORRODED AND WARPED; RAMP STATION 10 TO RAMP STATION 10.6, LBL60-RBL60. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2078.
Part: HINGE FITTING — CORRODED (BS 817) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE FS817.0E FUSELAGE AFT BULKHEAD RAMP LH HINGE FITTING CORRODED AT LBL31, WL140-150. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2105.
Part: BEAM — CRACKED (BS 597) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND THE LT AUX TANK INBOARD COMPARTMENT CENTER WING REAR BEAM WEB HAD A 2 INCH CRACK AT CWS73L, FS597, WL265. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE HORIZONTAL STABILIZER RH LOWER SKIN TRAILING EDGE CORRODED BEYOND LIMITS, FS1099, HSS256-262R, WL270. REPAIRED IAW SRM FIG. 55-20-06. NR# 2815.
Part: SKIN — WARPED (BS 777-817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE EXTERIOR SKIN WARPED AT FS777.0E TO FS817.0E, AND WL140 TO WL236, RBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: PLATE — CRACKED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT MLG BEAM REINFORCE PLATE CRACKED AT FS577 AND WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6596.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS657 RING SEGMENT WITH INCORRECT REPAIR AND ELONGATED HOLES AT WL142-165, LBL62-77. REPAIRED IAW SRM FIG. 53-40-11. NR# 2739.
Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE AIRFRAME'S CARGO DOOR SEAL BUMPER FS1041 LBL61 SPLICE PLATE CORRODED, WL270. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2473.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT & RT FS627 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76 AND RBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2742.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS677 RING SEGMENT HAD ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-23. NR# 2738.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND LT AFT FUSELAGE INT BHD WEB WITH TEMPORARY REPAIR AT FS847, WL178, AND LBL72. REPAIRED IAW SMP583 SRM FIG. 53-50-10. NR# 2232.
Part: CAP — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS938 OVERHEAD BULKHEAD UPPER CAP CRACKED AT LBL17 & RBL17 RADIUS AND BL0 LOWER FLANGE; WL280. REPAIRED IAW SRM FIG. 53-50-06. NR# 2487.
Part: BULKHEAD — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RT MAIN WHEEL WELL BHD WEB WARPED WITH TEMPORARY REPAIR AT FS588-597, WL146-170, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2365.
Part: SKIN — WARPED (BS 657-697) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE EXTERIOR SKIN AT FS657 TO FS697, WL140 TO WL240, AND RBL85 WARPED WITH TEMPORARY REPAIR AT WL200. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: DOUBLER — CRACKED (BS 406-428) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CRACKED SKIN DOUBLERS FS406 TO FS428 RBL85 WL190 TO WL224. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND RT OUTBOARD FLAP LOWER TRAILING EDGE SKIN CORRODED AT OWS241-303. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6681.
Part: BULKHEAD WEB — MISALIGNED (BS 245) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS 245 UNDERLOOR BULKHEAD WEB WITH HOLES MISALIGNED TO THE NEW TIE DOWN FITTING RBL30 PILOT HOLES; WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BEAM — CORRODED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT MAIN WHEEL WELL BEAM CORRODED AND CRACKING AT FS588 AND WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6479.
Part: BULKHEAD — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR BHD WEB CORRODED AND WARPED AT FS880 AND LBL40-RBL40. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6078.
Part: BUMPER — DAMAGED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE CARGO DOOR LH SEAL BUMPER REPAIR DOUBLES WITHOUT SPACE DISTANCE AT FS946, TEMPORARY REPAIR AT FS888-FS910, AND FORWARD END WORN AT FS866. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: RIB — WARPED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT OUTBD FLAP TRAILING EDGE RIB WARPED AND CRACKED AT OWS316-323. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6593.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND DEEP PITTING CORROSION ON LONGERON FS245 TO FS477 WL260 LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6395.
Part: SEAT TRACK — DAMAGED (BS 165-180) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5311, FOUND THE FLIGHT ENGINEER SEAT TRACK LH/RH LOCATE PIN HOLE ELONGATED, FS165-FS180, LBL27-RBL11, WL202 / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2102.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT INBD FLAP LOWER SKIN CORRODED WITH MULTIPLE ELONGATED HOLES AND DENTS AT CWS84-178. REPAIRED IAW SRM FIG. 51-140-20. NR# 6465.
Part: BEAM — CORRODED (MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3212, FOUND RT UPPER WHEEL WELL BEAM OTBD CAP WITH CORROSION AT FS597, WL280, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2206.
Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND BHD STIFFENER REPLACEMENT WITH MULTIPLE ELONGATED HOLES AT FS817.0E, WL135-145, AND RBL10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2443.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND MULTIPLE DENTS, STONE MARKS, AND REPAIR DOUBLERS ON BELLY SKIN AT FS697-737, WL126, AND RBL61-LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2154.
Part: SKIN — CRACKED (RT MLG FAIRING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RT MAIN WHEEL WELL BOTTOM FAIRING WRINKLED WITH MULTIPLE CRACKS AT FS491-617, WL140-180, AND RBL45-85. REPAIRED IAW LAC MEA 382-53-06-097
Part: CAP — CORRODED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS880 BULKHEAD UPPER CAP CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6345.
Part: ACCESS PANEL — CRACKED (LT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT WING RAINBOW FITTING ACCESS PANEL CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6402.
Part: BULKHEAD — CORRODED (CARGO DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR BHD WEB CORRODED WITH MULTIPLE DENTS AT FS902 AND LBL40-RBL40. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6079.
Part: SPLICE PLATE — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE AIRFRAME'S CARGO DOOR SEAL BUMPER FS1041 RBL61 SPLICE PLATE CORRODED, WL260. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2475.
Part: DOUBLER — DAMAGED (BS 491-677) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH MAIN WHEEL WELL POD-TO-BELLY SKIN DOUBLER WITH ELONGATED HOLES, FS491-677, WL136, RBL50-73. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: STRUT — DENTED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT AFT FUSELAGE FS792 STRUT WITH MULTIPLE DENTS AT WL200, LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6246.
Part: TEE FITTING — CORRODED (BS 588) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH MAIN WHEEL WELL FS588 BEAM-TO-WL200 BULKHEAD TEE CLIP CORRODED, LBL63. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SPAR WEB — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CTR WING FRONT SPAR WEB 1" CRACK AT BEAM ATTACHMENT AREA AT FS517, WL256-285, AND RCWS61-101. REPAIRED IAW SRM FIG. 57-030-22. NR# 6117.
Part: STRUCTURE — DAMAGED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTERWING LOWER FWD #1 PLANK REQUIRES REPLACEMENT. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: GUSSET — CORRODED (CARGO DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR LT AND RT BHD TO LOWER REAR SKIN GUSSET CORRODED WITH ELONGATED HOLES AT FS880, LBL45-60, AND RBL45-60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6082.
Part: SKIN — WARPED (BS 869-902) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH AFT FUSELAGE EXTERIOR SKIN WARPED AT FS869, WL180 TO WL230, A DENT AT FS902 WL178, AND REPAIR DOUBLER AT WL182. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2147.
Part: SKIN — CORRODED (LT AILERON) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT AILERON UPPER SKIN CORRODED AT AS55-143. REPAIRED IAW SMP583 SRM FIG. 51-140-12. NR# 2323.
Part: SKIN — CORRODED (RT AILERON) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND THE RT AILERON LOWER SKIN CORRODED AT AS143-214R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6159.
Part: INTERCOSTAL — ELONGATED (BS 727-767) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CABIN FS727-737 LBL4 WL282 INTERCOSTAL BEAM WITH ELONGATED HOLES. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: ATTACH ANGLE — CORRODED (BS 617) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION CORROSION ON FITTING TO BELLY SKIN ATTACH ANGLE FS617 LBL40 TO LBL62 WL135 TO WL140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND THE HORIZONTAL STABILIZER LOWER SKIN CORRODED BEYOND LIMITS AT FS1067, RBL30, WL265. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2921.
Part: PLATE — MISSING (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND SKID BAR BASE PLATE MISSING AT FS797.0E-817.0E, WL130, AND LBL11-RBL11. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6099.
Part: SKIN — CORRODED (BS 617-657) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS617-657 BELLY SKIN CORRODED; LBL45-61 & RBL45-61, WL130-140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND THE RH WINDOW RETAINER (FRAME) POST #3 UPPER FWD CORNER AT FS127, WL251, RBL35 WITH TEMP REPAIR AND LOWER FWD CORNER CRACKED AT FS116, WL231, RBL42. / REPAIRED IAW LAC MEA 38253-18-038. NR# 2111. / PSE# 53-30-01, AD 2012-06-09
Part: SKIN — CRACKED (LT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT ELEVATOR HSS51-89L UPPER SKIN DENTED, CRACKED AND CORRODED. WL265. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6337.
Part: GUSSET — SCRATCHED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH AFT FUSELAGE FS797 & FS814 STRUT-TO-SLOPING LONGERON GUSSET PLATE DEEPLY SCRATCHED; LBL62. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SRM 51-60 & 51-70.
Part: WEB — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR WEB CRACKED FS924 RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND CABIN OHD RING SEGMENT WITH CORROSION REMOVAL OUT OF LIMIT (0.045"DEPTH X 4.5" LENGTH) AT FS737. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6628.
Part: CAP — CORRODED (BS 417) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS417 UNDERFLOOR BULKHEAD UPPER CAP CORRODED BEYOND LIMITS AT TIE DOWN POINT, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND CABIN LONGERON CORRODED AT BAR-FITTING ATTACHMENT AT FS627, WL260, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2448.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP UPPER SKIN WITH INNER SKIN CORROSION AT OWS303. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6611.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH FS277 RING SEGMENT WITH ELONGATED HOLES AT WL150 AND WL161, RBL63-82. REPAIRED IAW SRM FIG. 51-140-21. NR# 2718.
Part: FRAME — CRACKED (BULKHEAD) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS196 UNDERFLOOR BULKHEAD LOWER CAP CRACKED AT LBL29, WL131. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: BEAM — CRACKED (BS 557) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE LH MAIN WHEEL WELL FS557 BOW BEAM CRACKED & TEMP REPAIRS AT WL150 & WL198, LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE CARGO DOOR EXTERIOR SKIN FS968-990 CORRODED AND DENTED/BULGED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2061.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND UNDERDECK INTERCOSTAL RIB CRACKED AT FS236, WL195, AND LBL58. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2278.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT ATTACHMENT WEB CORRODED WITH MULTIPLE ELONGATED HOLES AT FS477-617, WL250, AND LBL61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6566.
Part: BRACKET — CRACKED (RT HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND RT HORIZONTAL LEADING EDGE INTERIOR COMPENSATOR BRACKET CRACKED HSS156.2 TO HSS162.6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6432.
Part: SKIN — CORRODED (LT ELEVATOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE LT ELEVATOR LOWER SKIN CORRODED BEYOND LIMITS AT HSS51L-89L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2489.
Part: INTERCOSTAL — TORN (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP INTERCOSTAL WEB TORN AT OWS256-262. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6496.
Part: BULKHEAD — CORRODED (RT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT MAIN LANDING GEAR WHEEL WELL BULKHEAD WEB CORRODED AT FS517, WL146-200, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6446.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND FLOORBEAM UPPER CAP CORRODED IN SEVERAL AREAS AT FS537, WL 146, LBL61-RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6652.
Part: CAP — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR LOWER CAP CRACKED FS968 LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — DAMAGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT INBD FLAP UPPER TRAILING EDGE SKIN WITH MULTIPLE ELONGATED HOLES, CORROSION, AND INCORRECT REPAIR AT CWS84-220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6557.
Part: ANGLE — DAMAGED (BS 588-597) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH FS588-FS597 CHINE ANGLE WITH ELONGATED HOLES, LBL62, WL140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SRM 51-60 & 51-70. 2907.
Part: STIFFENER — CORRODED (RAMP DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP DOOR PEDESTAL ATTACHMENT STIFFENERS CORRODED & WITH ELONGATED HOLES, RAMP STATION 9, LBL10-32L, RBL10R-32R, WL130. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2499.
Part: FORMER — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT INBD FLAP RIB FORMER WARPED AND CRACKED IN 3 PLACES AT FS220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6476.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT UPPER MAIN WHEEL WELL FILLET PANEL ATTACH ANGLE CRACKED AT FS477, WL283, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2238.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND FUSELAGE TO WING FWD FILLET ATTACH ANGLE CORRODED AT FS517, WL280, AND RBL20-63. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2334.
Part: STIFFENER — DAMAGED (BS 777-797) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND BELLY SKIN STIFFENERS WITH ELONGATED HOLES FS777E TO FS797E LBL30 W126 / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BULKHEAD WEB — DAMAGED (RT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH MAIN WHEEL WELL BULKHEAD LOWER WEB WITH ELONGATED HOLES, FS528-577, WL142-150, RBL61. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — DAMAGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP UPPER TRAILING EDGE SKIN WITH DEEP CUTTING MARKS AND INCORRECT REPAIR AT FLAP STA.0-28. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6509.
Part: SKIN — DENTED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR EXTERIOR SKIN DENTED, BULGED & CORRODED; RAMP STATION 0 TO RAMP STATION 10.6, RBL30-RBL60. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2077.
Part: SKIN — CORRODED (LT HORIZ STAB) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LT LEADING EDGE SKIN CORRODED AND WITH ELONGATED HOLES; HSS71L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2637.
Part: SKIN — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP TRAILING EDGE SKIN WITH 7 WARPED CRACK AND ELONGATED HOLES AT OWS28-100. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6582.
Part: FITTING — OUT OF ALIGNMENT (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT REAR UPPER CORNER FITTING OUT OF ALIGNMENT 0.045" AT FS597 AND CWS220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6722.
Part: SKIN — DENTED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WITH MULTIPLE DENTS, STONE MARKS, AND REPAIR PATCHES AT FS777.0E-817.0E, WL126, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2197.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS817.0E UNDERFLOOR BULKHEAD UPPER CAP CORRODED AT LBL52 SUPPORT FITTING, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2791.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RH FS751.0E RING SEGMENT WITH ELONGATED HOLES AT WL158-161, RBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2729.
Part: RISER PANEL — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3211, FOUND THE LT UPPER MAIN WHEEL WELL FS477 BULKHEAD WEB (EXTRUDED RISER PANEL) CRACKED AT WL240, LBL78. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6250.
Part: LONGERON — CRACKED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LT UPPER MAIN WHEEL WELL LONGERON CORRODED AND REPAIRED AT FS477-577, WL204, AND LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2245.
Part: MANIFOLD — DENTED (RT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5324, FOUND THE RT MLG WHEEL WELL MANIFOLD WITH QTY 4 EACH DEEP DENTS; RBL61, WL150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2579.
Part: STRINGER — WARPED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING RT LOWER PLANK #21 STRINGER CWS165-218R SECTION WARPED. REPAIRED IAW MEA 382-57-18-151. NR# 6214.
Part: INTERCOSTAL — DAMAGED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN LANDING GEAR WHEEL WELL FS477-517 WL200 INTERCOSTAL BEAM INBOARD CAP WITH ELONGATED HOLES AT FS517. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6448.
Part: SKIN — DENTED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR EXTERIOR SKIN DENTED; RAMP STATION 0 TO RAMP STATION 10, BL0-LBL30. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.
Part: LONGERON — CORRODED (BS 245-477) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION ON LONGERON FS245 TO FS477 RBL20 WL280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND CARGO AIRCOND COMPT LOWER SKIN WARPED AT FS397-457, WL136, AND LBL50-70. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2162.
Part: SKIN — CRACKED (LT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND LT OUTBD UPPER TRAILING EDGE SKIN OF AILERON WELL BULGED, SUNKEN RIVETS, CRACKS, AND INTERGRANULAR CORROSION AT FS597-617, WL580, AND AS73-106. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2258.
Part: BULKHEAD WEB — CRACKED (BS 902) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND AFT FUSELAGE LH BULKHEAD WEB MULTIPLE CRACKS FS902 LBL32 WL200 TO WL265. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BULKHEAD WEB — CRACKED (BS 93) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FORWARD FUSELAGE FS93 BULKHEAD WEB CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BEAM — CORRODED (BS 517) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3212, FOUND THE RH FS517 MLG BEAM CORRODED AT WL190-195, RBL66. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2855.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RT FS647 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, RBL73-76. REPAIRED IAW SRM FIG. 51-140-23. NR# 2733.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND WEB STRESS CORROSION CRACKLING AT FS477 AND WL225-250. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2300.
Part: DOUBLER — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP TRAILING EDGE DOUBLER CORRODED AT OWS173. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6616
Part: SKIN — CORRODED (VERTICAL STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE VERTICAL STABILIZER TRAILING EDGE LT SKIN CORRODED BEYOND LIMITS, VSS4, FS1096-1099, LBL85. REPAIRED IAW SRM FIG. 51-140-12. NR# 2582.
Part: SKIN — DENTED (LT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT ELEVATOR UPPER SKIN WITH MULTIPLE DENTS & SCRATCHED, HSS122L-180L; FS1100-1130, WL265. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6336.
Part: FITTING — CRACKED (BS 577) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS577 UNDERFLOOR BULKHEAD LH PORK CHOP FITTING CRACKED, LBL59, WL140. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2905.
Part: CAP — CRACKED (WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING REAR SPAR WEB CWS192R FLAP ATTACHMENT VERTICAL CAP CRACKED; FS597. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6248.
Part: ACCESS PANEL — CRACKED (RT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT WING RAINBOW FITTING ACCESS PANEL CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6403.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RH FS457 RING SEGMENT WITH ELONGATED HOLES AT WL161, RBL75. REPAIRED IAW SRM FIG. 51-140-21. NR# 2724.
Part: SKIN — WARPED (BS 537-577) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WARPED AT FS537 TO FS577, LBL60 TO RBL60, AND WL126. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS880 BULKHEAD LOWER CAP AND WEB CRACKED, LT SIDE. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6070.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT UPPER FLOORBEAM SURFACE TIE DOWN RING NUTPLATE HOLES CORRODED AT FS637, WL146, AND RBL0-20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2436.
Part: CAP — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER HSS61L BULKHEAD REAR LOWER CAP CORRODED AT F1093, WL256. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2778.
Part: CAP — CORRODED (BS 457) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS457 UNDERFLOOR BULKHEAD UPPER CAP CORRODED BEYOND LIMITS AT TIED DOWN POINTS, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BEAM — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND ATTACHMENT BEAM INBD CAP HAIRLINE CRACK AND TEMPORARY REPAIR AT FS528-577, WL205-256, AND LBL61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6597.
Part: SPLICE — CRACKED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT MAIN WHEEL WELL WEB SPLICE TEE CRACKED AT FS477-497, WL175, AND LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6484.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, THE RT MAIN WHEEL WELL FS477-517, WL200 INTERCOSTAL BULKHEAD WEB FOUND WITH ELONGATED HOLES AND CRACKS; RBL61-68. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6265.
Part: ANGLE — CORRODED (BS 737-817) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RH CHINE ANGLE CORRODED AT FS737.0E TO FS817.0E, WL140-150, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPARTMENT LOWER CAP CORRODED AT FS257.0E, WL126-140, AND RBL38-48. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2397.
Part: RAMP — CORRODED · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR STATION 10.6 REAR BULKHEAD LOWER CAP CORRODED & WITH MULTIPLE REPAIRS. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2069.
Part: ANGLE — WORN (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5323, FOUND LH MAIN WHEEL WELL CHINE ANGLE SCREW HOLES WORN AT FS516, WL142, AND LBL61. REPAIRED IAW SRM FIG. 53-040-27. NR# 2408.
Part: CAP — CRACKED (BS 577) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LOWER CAP CRACKED FS577 RBL59 TO RBL61 WL126 TO WL140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — DENTED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LT AFT FUSELAGE EXT SKIN WITH MULTIPLE DENTS AND REPAIR DOUBLERS AT FS902-935, WL170-180, AND LBL61-70. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2177.
Part: BEAM — CRACKED (RT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND STRESS CORROSION IN LOWER BEAM INSIDE RT MAIN WHEEL WELL AT FS557, WL150-500, AND RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2151.
Part: CHANNEL — CRACKED (RT AILERON) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT AILERON FORWARD CHANNEL MULTIPLE CRACKS. FS635 AS21 REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6398.
Part: SPAR CAP — WORN (RT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBOARD FRONT SPAR LOWER CAP WORN. OWS255 REPAIRED IAW MEA 382-57-18-054 NR #6388
Part: STIFFENER — CORRODED (RT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD WING REAR BEAM WEB VERT SUPPORT STIFFENER UPPER AREA CORRODED AT FS597, OWS73, AND WL256-280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2350.
Part: RISER PANEL — CORRODED (RT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5324, FOUND THE RT MLG WHEEL WELL STRESSED RISER PANEL CORRODED, FS597-617, WL170-200, RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2643.
Part: CAP — CORRODED (BS 617 BULKHEAD) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS617 UNDERFLOOR BULKHEAD LOWER CAP CORRODED AT RBL5-10, WL126-140. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: STRINGER — DAMAGED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND ATTACHMENT STRINGER / STRAP WITH MULTIPLE ELONGATED HOLES AT CWS108-192. REPAIRED IAW SRM FIG. 57-070-05. NR# 6501.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RT UPPER MAIN WHEEL WELL FILLET PANEL ATTACH ANGLE CORRODED AT FS477-517, WL283, AND RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2236.
Part: RIB — WARPED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, LT OUTBD FLAP LOWER TRAILING EDGE SKIN FOUND ATTACHMENT RIB WARPED WITH MULTIPLE ELONGATED HOLES AT OWS164-210. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6613.
Part: ICE SHIELD — CORRODED (BS 367-397) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH FS367-397 ICE SHIELD SKIN DOUBLER CORRODED, WL140-143, RBL85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: RIB — DAMAGED (RT AILERON) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT AILERON LOWER SKIN ATTACHMENT RIB MULTIPLE ELONGATED HOLES. AS178 AND AS562 REPAIRED IAW SRM FIG. 57-80-03 NR# 6406.
Part: BUMPER — DAMAGED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE CARGO DOOR RH SEAL BUMPER WITH MULTIPLE REPAIR DOUBLERS AND ELONGATED HOLES (QTY 10. EA), FS1026-FS1033. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND ATTACHMENT WEB CORRODED WITH ELONGATED HOLES BY DRAG ANGLE AT FS447-617, WL250, AND RBL61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6567.
Part: SKIN — WARPED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR EXTERIOR SKIN WARPED WITH TEMP REPAIR AT FS902 AND LBL5-46. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6077.
Part: RIB — WARPED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT OUTBD FLAP TRAILING EDGE RIB FOUND WARPED WITH MULTIPLE OVERSIZED HOLES AT OWS267-276. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6486.
Part: RIB — WARPED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND RT ATTACHMENT RIB WARPED AND EXCEEDED CUT OUT AT OWS255. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6610.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WITH MULTIPLE STONE MARKS, PITTING, CORROSION, AND MULTIPLE REPAIR DOUBLERS AT FS297-337, WL126, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2192.
Part: STRAP — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP DOOR LEADING EDGE SCRAPER STRAP WARPED AND WITH TEMPORARY REPAIR; RAMP STATION 0, LBL61-RBKL61, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2501.
Part: WEB — CRACKED (NR 1 ENGINE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND #1 ENGINE INBD TRUSS MOUNT ATTACHMENT WEB 5/8" LONG CRACK AT UPPER TANG CUTOUT ACCESS HOLE AT FS517, WL265-280, AND OWS158-201. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6140.
Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CENTERWING LEADING EDGE TO OUTBOARD WING JOINT ATTACH ANGLE CRACKED CWS84.3 TO CWS178.8 FS497 WL272. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6381.
Part: SKIN — BULGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RT AFT FUSELAGE SKIN BULGED AT FS737-747, WL170-230, AND RBL85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2150.
Part: TEE FITTING — CORRODED (FLAP TRACK) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD WING REAR BEAM FLAP TRACK ATTACHMENT TEE FITTING UPPER AREA CORRODED AT OWS162. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2311.
Part: ANGLE — DEFORMED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RAMP DOOR SIDE FAIRING SUPPORT TEE ANGLES DEFORMED, CRACKED AND WITH ELONGATED HOLES; RAMP STATION 9-10, LBL12 & BL0 & RBL12. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2869.
Part: BULKHEAD WEB — CORRODED (BS 528-577) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND EXFOLIATION CORROSION ON BHD WEB IN LH MAIN WHEEL WELL BETWEEN L/G BEAM AND REINFORCE DOUBLER AT FS528 TO FS577, LBL61.6, AND WL150 TO WL175. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: SKIN — DAMAGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER LEADING EDGE SKIN WITH MULTIPLE ELONGATED HOLES AND A TEMPORARY REPAIR AT OWS164-200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6607.
Part: SKIN — CORRODED (RT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD WING UPPER TRAILING EDGE SKIN OF AILERON WELL SURFACE BULGED, SUNKEN RIVETS, CRACK AND INTERGRANULAR CORROSION AT FS597-617, WL580, AND AS125-161. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2262.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RT FS687 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, RBL73-76. REPAIRED IAW SRM FIG. 51-140-23. NR# 2732.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RT FS637 RING SEGMENT WITH ELONGATED HOLES, WL158-161, LBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2740.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WITH MULTIPLE STONE MARKS, PITTING CORROSION, AND MULTIPLE DOUBLER REPAIRS AT FS337-377, WL126, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2193.
Part: ATTACH ANGLE — CORRODED (VERTICAL STAB) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND VERT STAB LT / RT LOWER ATTACH ANGLE CORRODED AT FWD AND REAR LOCATED AT FS946-1128, VSS0, WL285, LBL20, AND RBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# XXXX.
Part: SKIN — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND BELLY SKIN WITH MULTIPLE WARPED AREAS, PITTING CORROSION, AND REPAIR DOUBLER AT FS737.0E-777.0E, WL126, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2196.
Part: SPAR — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND THE CENTER WING REAR SPAR WEB WITH MULTIPLE CRACKS AT CWS157R-206R; FS597, WL255-285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6262.
Part: SPAR CAP — DAMAGED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, REPLACED RT CTR WING FRONT SPAR UPPER CAP AS PER LAC TASK 0150 REV A (BEYOND 2ND/3RD OVERSIZE FASTENER HOLES) DUE TO FRONT SPAR WEB RENEW AT CWS154.5-220. REPAIRED IAW SRM FIG. 57-030-15. NR# 6639.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP UPPER SKIN CORRODED WITH MULTIPLE INCORRECT REPAIRS AT OWS103-170. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6491.
Part: BEAM — CRACKED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3211, FOUND LT UPPER WHEEL WELL BOW BEAM CRACKED AT FS497, WL202, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2207.
Part: STIFFENER — CORRODED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT UPPER MAIN WHEEL WELL BHD STIFFENER CORRODED AT FS537, WL201, AND LBL62-84. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6511.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT RING SEGMENT CORRODED WITH MULTIPLE ELONGATED HOLES AT FS742 AND WL140-200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6482.
Part: BULKHEAD — NOT REPORTED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP DOOR FORWARD BULKHEAD WEB WITH TEMPORARY REPAIR AT RBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2584.
Part: SKIN — WARPED (BS 737-817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH AFT FUSELAGE SKIN OIL-CANNED (WARPED) AFTER CORROSION REMOVAL, FS737-817, WL140-170. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SPLICE — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND CABIN OHD RING SEGMENT SPLICE CRACKED AT FS477, WL283, AND LBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2449
Part: FITTING — ELONGATED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP DOOR STATION 6 ACTUATOR FITTING BOLT SEIZED AND THE FITTING BOLT HOLES ELONGATED; BL0, WL132. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2503.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LH FS357 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2752.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT CTR FUSELAGE SKIN CORRODED AT FS677-737, WL265-285, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6599.
Part: SEAT TRACK — CORRODED (BS 212-226) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5311, FOUND THE NAVIGATOR SEAT TRACKS CORRODED. FS212 & FS226, RBL8-RBL39, WL195. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: SKIN — DENTED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER SKIN WITH MULTIPLE DENTS, ELONGATED HOLE AND TEMP REPAIR DOUBLER AT OWS197-330. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6604.
Part: BULKHEAD — CRACKED (NLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND NOSE WHEEL WELL RT BHD WEB CRACKED AT FS196, WL130-180, AND RBL3-33. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2182. / PSE# 53-30-10, AD 2012-06-09
Part: SKIN — CHAFED (RUDDER) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LEADING EDGE SKIN WITH DEEP CHAFED MARKS AT VSS15-149, RT SIDE. FS1128. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6271.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT UPPER FLOORBEAM, CAP CORRODED AT TIE DOWN RING NUTPLATE HOLES AT FS617, WL146, AND LBL19-RBL19. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2431.
Part: CAP — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT LOWER CAP CORRODED WITH MULTIPLE EXCESS HOLES AT FS757.0E, WL126-140, AND LBL6-RBL15. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2429
Part: SKIN — CRACKED (LT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD UPPER SURFACE TRAILING EDGE SKIN FWD AND AFT PANEL WITH SURFACE CORROSION, BULGING, SUNKEN AND SHEARED RIVETS, CRACKS, AND INTERGRANULAR CORROSION WITH LOWER BEADED SKIN DEBONDED AND CORRODED AT OWS303-339. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2275.
Part: BRACKET — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CWS191 TO CWS200 BRACKET CRACKED DURING REMOVAL OF SPAR WEB REPLACEMENT ACCESS. CWS191R TO CWS200R WL272 FS517. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6380.
Part: LONGERON — CORRODED (BS 148-196) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH FS148-TO-FS196 RBL27 WL130 LONGERON CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SRM 51-60 & 51-70.
Part: STRINGER — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CENTERWING #19 STRINGER AT LOWER CENTER PLANK ATTACHMENT CRACKED. CWS103R REPAIRED IAW MEA 382-57-18-192 NR #6390
Part: FAIRING — CHAFED (BS 837-852) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE AFT FUSELAGE RH ELEPHANT EAR FAIRING CUTOUT AREA CHAFED BY RAMP HARDWARE, AT FS837-840 AND FS848-852, WL185, RBL65. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2115.
Part: SPAR — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING REAR SPAR WEB CRACKED AT CWS158L LOWER CAP ATTACHMENT; FS597, WL255. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6239.
Part: SKIN — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND EXT BELLY SKIN WARPED WITH DEEP STONE MARKS, CORROSION, AND TEMPORARY REPAIR AT FS617-657, WL126, AND LBL48-RBL48. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2194.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5316, FOUND THE FS497 OVERHEAD BULKHEAD LOWER CAP CRACKED. RBL40-60, WL258-262. REPAIRED IAW SRM FIG. 53-40-05. NR# 6171.
Part: FLOORBEAM — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND REDUNDANT DUCT ACCESS OPENING FLOORBEAM WEB WARPED AT FS797.0E, WL137, AND LBL12-RBL12. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6095
Part: CAP — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT CENTER WING FRONT WEB UPPER CAP CORROSION AND OVERSIZED HOLES CWS157.5 TO 209.5L FS517 WL257. REPAIRED IAW MEA 382-57-18-193 DWG #5730LH2527 NR #6377
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT L-ANGLE ATTACH TO UPPER FLOORBEAM CORRODED AT FS597, WL142-145, AND RBL50. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2435.
Part: FITTING — CORRODED (LT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD WING TIP ATTACHMENT POINT, AFT ATTACHMENT POINT UPPER AND LOWER FITTING CORRODED AT FS580, OWS563, AND WL256-280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2355.
Part: FITTING — CORRODED (BS 800-817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND PITTING ON CHINE ANGLE WITH ELONGATED HOLES. RH FS800E TO FS817E WL140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: RIB — DEFORMED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT INBD FLAP INNER RIB DEFORMED WITH MULTIPLE ELONGATED HOLES AND CRACK AT CWS178. REPAIRED IAW SRM FIG. 51-140-20. NR# 6470.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LH FS370 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2751.
Part: CHANNEL — BROKEN (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT MAIN WHEEL WELL ATTACHMENT U CHANNEL BROKEN WITH TEMP REPAIR AT FS497, WL200, AND RBL85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6097.
Part: RISER PANEL — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN WHEEL WELL BULKHEAD WEB (EXTRUDED RISER PANEL) CRACKED AT FS516, WL165, LBL61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6247.
Part: SKIN — CORRODED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP UPPER TRAILING EDGE SKIN CORRODED WITH MULTIPLE INCORRECT REPAIRS AT OWS244-300. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6493.
Part: DOUBLER — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND HORIZONTAL STAB LOWER SKIN ATTACHMENT DOUBLER CORRODED AT FS1075-1095, HSS61L-61R, AND WL270. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6094.
Part: SKIN — WARPED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RT OUTBOARD FLAP INNER RIB WARPED WITH INCORRECT REPAIR ON UPPER SKIN AT OWS222-225. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6702.
Part: SPAR — CORRODED (CENTER WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CTR WING REAR SPAR UPPER CAP DEEP CUTTING MARK AND CORRODED AT FS597, WL285, AND RCWS73. REPAIRED IAW SRM FIG. 57-0320-14. NR# 6122.
Part: RIB — CORRODED (BS 830) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH AFT FUSELAGE ATTACHMENT RIB CORRODED AND WITH ELONGATED HOLES, FS830, WL170-185, LBL63-LBL68. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: CAP — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR BULKHEAD LOWER CAP CRACKED FS1012 LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: CAP — CORRODED (LT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5324, FOUND THE LT MAIN WHEEL WELL FS497 LOWER BOW BEAM OUTBOARD CAP CORRODED AND WITH ELONGATED HOLES, WL150-200, LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2796.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RT FS404 RING SEGMENT CORRODED AND WITH ELONGATED HOLES, WL142, RBL61. REPAIRED IAW SRM FIG. 51-140-21. NR# 2723.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LT FUSELAGE TO WING FWD FILLET ATTACH ANGLE WITH INTERGRANULAR CORROSION AT FS477, WL280, AND LBL20-63. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2308.
Part: FRAME — WORN (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5312, FOUND CREW DOOR SIDE FRAME WORN AT REAR SUPPORT CABLE ATTACHMENT AT FS235, WL192, AND LBL71. REPAIRED IAW SRM FIG. 51-140-19. NR# 6740.
Part: SPAR — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT FORWARD SPAR WEB EYE BOLT HOLE CRACKED CWS143L. EPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6396.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT UPPER FLOORBEAM CAP CORRODED AT FS597, WL146, AND RBL28-RBL50. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2433.
Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND MULTIPLE ELONGATED HOLES IN LT HORIZONTAL LEADING EDGE INNER SKIN HSS69. FS1012 TO FS1041 WL285 TO WL268 REPAIRED IAW SRM FIG. 51-140-14. NR# 6412.
Part: ACCESS PANEL — CORRODED (LT AILERON) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT AILERON LOWER ACCESS PANEL FLANGE CORRODED AT AS45. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6570.
Part: SUPPORT ANGLE — CRACKED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RAMP DOOR PEDESTAL INTERIOR SUPPORT ANGLES CORRODED, CRACKED AND WITH ELONGATED HOLES; RS9, LBL30-RBL30. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: RISER PANEL — WARPED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT MAIN WHEEL WELL FS517 BULKHEAD WEB (EXTRUDED RISER PANEL) WARPED OVER A 5" BY 10" AREA; WL195-220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6195.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS687 RING SEGMENT WITH ELONGATED HOLES AT WL150-161, LBL68-75. REPAIRED IAW SRM FIG. 51-140-23. NR# 2736.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3212, FOUND RT CHINE ANGLE CORRODED WITH 3" CRACK AT FS617-697, WL140-146, AND RBL61-64. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2411.
Part: BULKHEAD WEB — ELONGATED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5323, FOUND THE LH MAIN WHEEL WELL FS528-577 LBL61 BULKHEAD WEB AND CHINE ANGLE WITH ELONGATED HOLES AND PITTING CORROSION, WL145-WL150. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2104.
Part: BULKHEAD WEB — CORRODED (BS 577) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH MAIN WHEEL WELL BULKHEAD WEB (EXTRUDED RISER PANEL) CORRODED BEYOND LIMITS BEHIND THE FS577 BEAM CAP, WL175-200, LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: ATTACH ANGLE — CORRODED (LT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE LT UPPER MAIN WHEEL WELL FS597-617 BULKHEAD LBL62 WL287 ATTACH ANGLE CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6315.
Part: RIB — DAMAGED (HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LT LEADING EDGE HSS80L RIB UPPER END WITH ELONGATED HOLES. FS1040, WL285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6454.
Part: SKIN — CORRODED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR LOWER SKIN CORRODED. FS902-924, LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6217.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND THE FS202 UNDERDECK RBL28 LOWER LONGERON CORRODED; WL128. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2491.
Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5323, FOUND LT MAIN WHEEL WELL BHD MANIFOLD WITH 5 CRACKS AT LBL61.5. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2418.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND FUSELAGE TO WING REAR FILLET FAIRING ATTACH ANGLE CORRODED AT FS617, WL285, LBL20-63, AND RBL20-63. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2335.
Part: CAP — CRACKED (WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING REAR SPAR WEB CWS192L FLAP ATTACHMENT VERTICAL CAP CRACKED; FS597. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6249.
Part: FORMER — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH PRESSURIZED SKIN PANEL ATTACHMENT FORMER WITH 6" CRACK AT FS597-617, WL285, AND LBL23. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6106.
Part: FRAME — WARPED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LT MAIN WHEEL WELL STEP AND FRAME WARPED AT FS491-510, WL138, AND LBL60-70. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2379.
Part: SPLICE — CORRODED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CORROSION AT LT MAIN WHEEL WELL BULKHEAD WEB SPLICE FS617 WL220 LBL61.62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6397.
Part: SUPPORT ANGLE — CORRODED (BS 178-196) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH UNDERDECK SUPPORT ANGLES (QTY 2) CORRODED, FS 178-196 RBL45 WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BRACE — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND AFT FUSELAGE LT STRUT BRACE WARPED AT FS792-817, WL195, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2304.
Part: STIFFENER — CORRODED (BS 491) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND STIFFENER FOR CHINE ANGLE ACCESS IN RH WITH CORROSION AT FS491, RBL66. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: CAP — CRACKED (BS 990 BULKHEAD) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LH FS990 SIDE BULKHEAD OUTBOARD CAP CRACKED 2" LONG, LBL75, WL275. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION CORROSION ON LONGERON BAR FITTING ATTACHMENT. FS245 TO FS477 RBL61 REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6400.
Part: SKIN — BULGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER SURFACE BULGED, SUSPECT INNER SPAR LOWER CAP CORRODED AT OWS164-173. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6561.
Part: BULKHEAD WEB — DAMAGED (BS 228) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS228 UNDERFLOOR BULKHEAD WEB WITH ELONGATED HOLES AT LBL35-48 & RBL35-56. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SPAR — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT CTR WING FWD SPAR WEB WITH 1" CRACK AROUND #2 ENGINE TRUSS UPPER TANG CUT OUT ACCESS HOLE AT CWS178. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6142.
Part: SKIN — CANNING (RT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, THE RT ELEVATOR TRAILING EDGE SKIN INBOARD UPPER & LOWER SKIN FOUND CANNING (WARPED). FS1150-1160, HSS51-67R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6288.
Part: SKIN — CORRODED (LT AILERON) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT AILERON UPPER SKIN CORRODED AT AS55-143. REPAIRED IAW SMP583 SRM FIG. 51-140-12. NR# 2324.
Part: ANGLE — CORRODED (BS 517-597) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE RH CHINE CAP CORRODED IN BETWEEN PORK CHOP FITTING; FS517-597, RBL50-60, WL146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2984.
Part: BULKHEAD — WARPED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR BHD WEB WARPED WITH TEMP REPAIR AT FS924 AND LBL40-RBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6081.
Part: SPAR CAP — DAMAGED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING FRONT SPAR (FS517) RT WEB LOWER CAP WITH OVERSIZED HOLES AT CWS174R-180R; WL257. REPAIRED IAW MEA 382-57-18-211. NR# 6375.
Part: WEB — CRACKED (BS 924) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315 FOUND RH BULKHEAD ATTACHMENT WEB CRACKED FS924 RBL62 TO RBL70 WL210 TO WL215. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BULKHEAD WEB — DAMAGED (NLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE NOSE WHEEL WELL FWD BULKHEAD WITH TEMP REPAIR AT BOTH LH & RH HINGE FITTINGS. FS93, LBL23 & RBL23. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2088.
Part: FITTING — CORRODED (BS 245 BULKHEAD) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE FS245 UNDERFLOOR BULKHEAD RT END FITTING CORRODED AT MAIN BOLT HOLE FOR CHINE ANGLE ATTACHMENT, WL 140-145, RBL 61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: WEB — CRACKED (BS 617) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH MAIN WHEEL WELL BULKHEAD WEB STRESS CORROSION CRACKING FS617 RBL84 WL180. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — WARPED (BS 777-817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH FUSELAGE EXTERIOR SKIN AT FS777.0E TO FS 817.0E, WL140 TO WL 236, AND LBL85 WARPED. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS457 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2758.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPARTMENT FLOORBEAM CAP NUTPLATE HOLE CORRODED AT FS257.0E, WL146, AND RBL18-38. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2395.
Part: TEE FITTING — CORRODED (FLAP TRACK) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD WING REAR BEAM FLAP TRACK ATTACHMENT TEE FITTING UPPER AREA WITH CORROSION AT OWS293. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2309.
Part: FAIRING — CORRODED (RAMP DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND THE RAMP DOOR RT ACTUATOR FITTING EXTERNAL FAIRING CORRODED AND WITH TEMPORARY REPAIRS; RAMP STATION 8, RBL60-75, WL150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2502.
Part: FRAME — CORRODED (BS 384) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH RING SEGMENTS AT FS384 & FS391 CORRODED, WL140-195, RBL62-85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RT FS771.0E RING SEGMENT WITH ELONGATED HOLES AT WL158, RBL74. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2728.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS324.0E RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2744.
Part: SKIN — CORRODED (TE FLAP) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND THE LT INBOARD FLAP OUTBOARD LEADING EDGE INNER SKIN DOUBLER CORRODED, CWS213L-220L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6458.
Part: SPLICE — CORRODED (LT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5323, FOUND LT MAIN WHEEL WELL BHD SPLICE CORRODED AT FS 537-557, WL150, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2415.
Part: RIB — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP OUTBD RIB CRACKED AT FLAP STA.336. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6506.
Part: FORMER — CORRODED (TE FLAP) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP RIB FORMER CORRODED WITH CUT MARKS AND CRACKS AT FLAP STA.0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6508.
Part: TRACK — CORRODED (LT MLG) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3211, FOUND THE LT FS517 & FS528 MAIN LANDING GEAR TRACKS CORRODED AT WL150-185. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6371.
Part: SKIN — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND RAMP DOOR EXT SKIN WARPED WITH SCRATCH MARKS AND TEMP REPAIR AT RS0-8 AND LBL6-RBL6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2005.
Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND UPPER FUSELAGE PRESSURE FAIRING WITH MULTIPLE REPAIR DOUBLERS OVERLAPPED AND WITH CORROSION AND WATER LEAKING AT FS477-517, AND RBL24-61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2170.
Part: BULKHEAD WEB — DAMAGED (BS 477) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS477 UNDERFLOOR BULKHEAD LBL18-40 WEB, AND STIFFENERS AT LBL25, LBL36 AND LBL40 WITH ELONGATED HOLES. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212 FOUND CARGO DOOR FITTING WITH DEEP CUTTING MARKS FS990 LBL0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3211, FOUND THE RT MAIN WHEEL WELL FS477 INTERCOSTAL BEAM CAP CRACKED AT WL200, RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6252.
Part: STRINGER — CRACKED (BS 120) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FUSELAGE LH SKYLIGHT FWD RIB CRACKED AT FS120, WL252, LBL25. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS677 RT RING SEGMENT WITH ELONGATED HOLES AT WL158, RBL73. REPAIRED IAW SRM FIG. 51-140-23. NR# 2731.
Part: WEB — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC212, FOUND CARGO DOOR RH SIDE BEAM WEB CRACKED FS878 RBL60. / REPAIRED IAW SRM, FIG. 510-140-17 .
Part: SKIN — BULGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CENTER WING BOX LOWER PLANK #2 BULGED SKIN SURFACE BEHIND #3 ENGINE EXHAUST AREA. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.
Part: SPAR WEB — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CTR WING REAR SPAR WEB 3" AT BEAM ATTACHMENT AT FS597, WL265-285, AND LBL61-157. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6113.
Part: RISER PANEL — CORRODED (RT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5324, FOUND THE RT MLG WHEEL WELL STRESSED RISER PANEL CORRODED BEYOND LIMITS, FS528-577, WL151-176, RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2628.
Part: CAP — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR BHD LOWER CAP LT/RT, DOUBLER LT/RT, AND WEB LT CRACKED AT FS990, LBL40-60, AND RBL 50-6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6074.
Part: FITTING — BROKEN (BS 557) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE LT MAIN WHEEL WELL FS557 BOW BEAM LOWER FITTING BROKEN, WL155, LBL62. REPAIRED IAW SRM 53-40-13.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS771.0E RING SEGMENT WITH ELONGATED HOLES AT WL150-161, LBL68-75. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2743.
Part: BULKHEAD — CORRODED (RT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3212, FOUND THE RH MAIN WHEEL WELL RBL61 BULKHEAD CORRODED AT SEVERAL AREAS, FS528-577, WL175-WL220. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2857.
Part: SKIN — DENTED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER SKIN DENTED WITH INCORRECT REPAIR AT OWS209-225. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6552.
Part: FITTING — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND CABIN TENSION TIE FITTING CRACKED AT FS617, WL260, AND RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2421.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS257.0E UNDERFLOOR BULKHEAD WEB CRACKED AND WITH ELONGATED HOLE(S), RBL38-50, WL130-145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2790.
Part: FLOORBOARD — WARPED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HCH5321, FOUND THE RAMP DOOR LH AND RH FLOORBOARD WARPED, LBL18-50 AND RBL18-50, RAMP STATION 8 TO RAMP STATION 10 / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2072.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE RT CHINE ANGLE CORRODED AT FS498-517, WL146, RBL64. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2629.
Part: INTERCOSTAL — DAMAGED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN LANDING GEAR WHEEL WELL FS477-517 WL200 INTERCOSTAL BEAM WEB WITH ELONGATED HOLES. LBL65. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6447.
Part: ANGLE — CORRODED (BS 737-817) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH CHINE ANGLE CORRODED WITH MULTIPLE ELONGATED HOLES AT FS737.0E TO FS817.0E, WL140 TO WL146, AND LBL64. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: DOUBLER — CRACKED (PYLON) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CRACK EVIDENT AT PYLON FITTING LAYER AT FS517, WL257, AND LH OWS572. REPAIRED IAW MEA 382-57-19-004 NR#6658.
Part: CAP — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR BULKHEAD LOWER CAP CRACKED. FS946 RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: WEB — BROKEN (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND RAMP DOOR INTERIOR BHD WEB BROKEN AT RAMP STA.6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2392.
Part: CHANNEL — CORRODED (BS 424-480) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION CORROSION ON U CHANNEL FS 424 TO FS480 RBL85 WL200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND UNDER FLIGHT DECK FLOOR BHD UPPER CAP CORRODED AT FS228, WL195, AND LBL75-RBL75. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2426.
Part: CAP — CORRODED (BS 297) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS297 UNDERFLOOR BULKHEAD UPPER CAP CORRODED BEYOND LIMITS AT BL0 TIEDOWN POINT, WL146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS880 BULKHEAD LBL9 & RBL9 STIFFENERS CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6216.
Part: LONGERON — CORRODED (BS 245-477) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION CORROSION ON LONGERON FS245 TO FS477 RBL20 WL265. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (BS 817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS 817 LH HOCKEY STICK FITTING CRACKED AT LBL61, WL140-150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: STRUCTURE — CORRODED (RUDDER) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND RUDDER TIP ASSEMBLY WITH CORROSION AT FS1128 AND VSS272. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2332.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPARTMENT UPPER FLOORBEAM NUTPLATE HOLE CORRODED AT FS245.0E, WL146, AND LBL61-RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2396.
Part: SKIN — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER LEADING EDGE SKIN WITH MULTIPLE ELONGATED HOLES, LOOSE RIVETS, CRACKS, CORROSION, AND INCORRECT REPAIR AT OWS227-OWS330. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6609.
Part: FAIRING — CRACKED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND RAMP DOOR PEDESTAL FWD FAIRING CRACKED WITH MULTIPLE DENTS AT RS9 AND LBL13-RBL34. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2001.
Part: RIB — CORRODED (TE FLAP) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP RIB CORRODED AND CRACKED IN SEVERAL AREAS AT OWS0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# XXXX.
Part: BULKHEAD — CRACKED (LTLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN WHEEL WELL FS517 BULKHEAD WEB CRACKED AT WL185, LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6445.
Part: SPAR — DAMAGED (RT AILERON) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT AILERON SPAR HAS MULTIPLE ELONGATED HOLES AS117 TO AS134. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6410.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5323, FOUND LH MAIN WHEEL WELL UNDER PORK CHOP FITTING SPLICE DOUBLER CORRODED AT FS594, WL138, AND LBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2419.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS337.0E RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2745.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS410 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2754.
Part: DOUBLER — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS880 RT BULKHEAD REINFORCEMENT DOUBLER WITH 1" LONG CRACK AT WL200; RBL62-70. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6193.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT BEAM UPPER CAP TIE DOWN POINT CORRODED AT FS277.0E, AND RBL33-40. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2398.
Part: TRUSS FITTING — DAMAGED (NR 3 ENGINE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND #3 ENGINE INBD TRUSS MOUNT UPPER LUG MAIN HOLE ELONGATED AT CWS178.8. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6131
Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER TRAILING EDGE SKIN CORRODED AT OWS106-164. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6620.
Part: BULKHEAD — CORRODED (BS 357) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS537 UNDERFLOOR BULKHEAD LOWER CAP CORRODED BEYOND LIMITS AT LBL5-RBL5. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2878.
Part: STRINGER — DAMAGED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING STRINGER #13 (FS530.25) AFT FLANGE WITH AN ELONGATED HOLE (#9C) AT CWS60L. REPAIRED IAW MEA 382-57-18-195. NR# 6348.
Part: FITTING — CRACKED (BS 377) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS377 UNDERFLOOR BULKHEAD RH END FITTING CORRODED/CRACKED; RBL61, WL140. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND CORROSION ON RH CHINE ANGLE AT FS245-382, WL140-146, AND RBL61-64. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2149.
Part: SKIN — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC53221, FOUND FWD FUSELAGE EXTERIOR SKIN CANNING AND WARPED AT FS83-93, WL210-231, AND LBL30-RBL30. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6139.
Part: SKIN PANEL — CORRODED (RT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD WING TRAILING EDGE LOWER SURFACE SKIN PANEL EXT WITH SURFACE CORROSION, BULGED, AND CRACKED AT RIVET HOLES AT OWS293-339. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2460.
Part: RIB — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT TRAILING EDGE ATTACH RIB QTY 5EA WARPED, CRACKED, WITH ELONGATED HOLES AT OWS164-200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6605.
Part: BEAM — CORRODED · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3212, FOUND THE RH FS577 MLG BEAM CORRODED AT WL173 AND TEMPORARY REPAIR AT WL193-223, RBL61-67. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT CTR FUSELAGE EXT SKIN CORRODED AT FS617-677 AND WL265-285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6598.
Part: BULKHEAD WEB — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS864-880 LBL6 BULKHEAD WEB CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6209.
Part: ATTACH ANGLE — CORRODED (LT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT OUTER WING FLAPWELL L-ANGLE ATTACH TO REAR WEB CORRODED ON TOP POSITION, OWS142L, FS597, WL260-280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6208.
Part: STRUCTURE — CRACKED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE RAMP DOOR REAR BULKHEAD SHELF PANEL CRACKED AT RAMP STATION 10 TO RAMP STATION 10.6, LBL40-RBL40. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2080.
Part: GUSSET — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS968 RT BULKHEAD GUSSET (INBOARD CAP) CORRODED, RBL62, WL240-270. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2474.
Part: CAP — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT AUX TANK BHD LOWER CAP CRACKED AT FS592 AND LCWS140. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6252.
Part: BEAM — CORRODED (RT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3212, FOUND RT UPPER WHEEL WELL BEAM INBD AND OTBD CAP WITH CORROSION AT FS597, WL280, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2206.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPARTMENT BHD SKIN ATTACH TO AIRCON MIXING CHAMBER WITH 2" CRACK AT FS477-497, WL258, AND RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6104.
Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND THE CENTER WING REAR SPAR UPPER CAP (PRESSURE FAIRING ATTACH ANGLE) CRACKED AT LBL22. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6219.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPT INT RT BHD SKIN CORRODED AT FS617, WL285, AND RBL20-61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6108.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FLOORBEAM LOWER CAP CORRODED AT FS517, WL126-140, AND LBL18-RBL18. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6110.
Part: CAP — NOT REPORTED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT LOWER CAP WITH TEMPORARY REPAIR AT FS477, WL126-140, AND LBL26. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2399.
Part: FITTING — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE AFT FUSELAGE FS968 UPPER BULKHEAD TO FORWARD INTERCOSTAL BEAM FITTING CRACKED. BL0, WL285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6353.
Part: SKIN — CHAFED (LT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE LT ELEVATOR LEADING EDGE SKIN WITH DEEP CHAFE MARKS AT HSS51-81L AND HSS192-238L. FS1106, WL265-275. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6319.
Part: SPAR WEB — CORRODED (CENTER WING) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT OUTER WING REAR SPAR WEB CORRODED BENEATH UPPER CORNER FITTING AT FS597, WL255-285, AND ROWS6. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6123.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE LH HORIZONTAL STABILIZER LEADING EDGE STRINGER (RIB UPPER FORMER) CRACKED, HSS192L, FS1041, WL285. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-20. NR# 2887.
Part: RETAINER — CORRODED (HATCH SEAL) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FORWARD HATCH SEAL RETAINER CORRODED & ELONGATED HOLES, AND DOOR FLANGE WITH 3" CRACK. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: CHANNEL — CRACKED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT ELEPHANT EAR ATTACH FRAME C CHANNEL CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6404.
Part: RISER PANEL — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN WHEEL WELL FS477 BULKHEAD WEB (EXTRUDED RISER PANEL) CRACKED AT LBL84, WL180 AND WL185. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6202.
Part: BULKHEAD — CORRODED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND RAMP DOOR REAR BHD WEB WITH CORROSION AND MULTIPLE TEMPORARY REPAIR DOUBLERS AT RS10, WL130-146, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2199.
Part: RIB — DAMAGED (LT HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND MULTIPLE ELONGATED HOLES IN LT HORIZONTAL STABILIZER LEADING EDGE RIB CAP. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6411.
Part: BULKHEAD — CRACKED (HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, THE HORIZONTAL STABILIZER FSS1138 BULKHEAD WEB FOUND CRACKED AT LBL5 AND RBL3 LIGHTENING HOLE EDGE; WL285. REPAIRED IAW SRM FIG. 51-140-17. NR# 2804.
Part: STRINGER — DAMAGED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING STRINGER #12 (FS524.5) AFT FLANGE WITH AN ELONGATED HOLE AT CWS60L. WL257. REPAIRED IAW MEA 382-57-18-194. NR# 6347.
Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND UPPER FUSELAGE PRESSURE FAIRING WITH MULTIPLE REPAIR DOUBLERS OVERLAPPED AND WITH CORROSION AND WATER LEAKING AT FS477-517, AND RBL24-61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2170.
Part: WEB — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT AFT FUSELAGE WEB WITH 8" CRACK FORMER AT FS836, WL192-200, AND LBL85. REPAIRED IAW SMP583 SRM FIG. 51-140-17. NR# 2180.
Part: BULKHEAD — WARPED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LT MAIN WHEEL WELL BHD WEB WARPED WITH TEMPORARY REPAIR AT FS588-5974, WL140-160, AND LBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2189.
Part: STRUCTURE — MISSING (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND ATTACHMENT STRINGER MISSING AT FS807.0E, WL126, AND LBL10-RBL10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR#2248.
Part: SKIN — CRACKED (LT WING) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD WING UPPER SURFACE TRAILING EDGE SKIN FWD AND AFT PANEL WITH SURFACE CORROSION, BULGING, SUNKEN AND SHEARED RIVETS, CRACKS, INTERGRANULAR CORROSION, 9 PATCH REPAIRS, AND WITH LOWER SURFACE BEADED SKIN DEBONDED AND HAVING 3 CRACKS AT FS597-617, WL560, AND OWS173-241. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2273.
Part: CAP — CRACKED (VERTICAL STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND VERT STABILIZER LT FRONT BEAM CAP WITH 6" CRACK. REPAIRED IAW SMP583 SRM FIG. 55-040-12. NR# 2336.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT SLOPING LONGERON CRACKED AT FS861, WL202, LBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2567.
Part: RISER PANEL — CORRODED (RT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE RT MLG WHEEL WELL STRESSED RISER PANEL CORRODED BEYOND LIMITS, FS597-617, WL151-176, RBL62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2625.
Part: ATTACH FITTING — CORRODED (NLG) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND THE FS196 NOSE LANDING GEAR ATTACHMENT (FITTING) ASSEMBLY CORRODED, LBL3 AND RBL3, WL126-146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2636.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS257 RING SEGMENT WITH ELONGATED HOLES AT WL150 AND WL161, LBL63-82. REPAIRED IAW SRM FIG. 51-140-21. NR# 2717.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RH FS627 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, RBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2726.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RH FS762.0E RING SEGMENT WITH ELONGATED HOLES, WL158-161, RBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2727.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS637 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2741.
Part: RIB — CORRODED (LT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND LT ELEVATOR INBOARD RIB LOWER CAP CORROSION FS1096. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6387.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE FS697 RT RING SEGMENT WITH ELONGATED HOLES AT WL158-WL161, RBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2730.
Part: SKIN — WARPED (BS 657-697) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH FUSELAGE EXTERIOR SKIN FS657 TO FS697, WL140 TO WL250, AND LBL85 WARPED WITH TEMPORARY REPAIR. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: SKIN — WARPED (BS 337) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RH FUSELAGE SKIN WARPED AT FS337 TO FS377, WL140 TO WL250, AND RBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: SKIN — DAMAGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP TITANIUM SKIN (LOWER SURFACE) BEHIND ENGINE #1 EXHAUST AREA WITH 1/2 RIVETS LOOSE AND ELONGATED HOLE AT OWS164-200. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6606.
Part: SKIN — DAMAGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LOWER LEADING EDGE SKIN WITH MULTIPLE LOOSE RIVETS AND ELONGATED HOLES AND REPAIR DOUBLER AT OWS197-227. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6608.
Part: STRIP — CORRODED (TE FLAP) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP TRAILING EDGE STRIP CORRODED AT OWS170-240. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6617.
Part: BULKHEAD WEB — CORRODED (BS 914) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE FOUND LH BULKHEAD WEB CORRODED WITH ELONGATED HOLE AT FS914, WL220, AND LBL75. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-17.
Part: SKIN — WARPED (BS 737-770) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND LH AFT FUSELAGE EXTERIOR SKIN WARPED AT FS737 TO FS770, WL170 TO WL230, AND LBL85. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: CARGO TRACK — CRACKED (BS 245) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS245.0E UNDERFLOOR BULKHEAD RH TIEDOWN FITTING CRACKED AT RBL20 (RBL36), WL140-146. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 2898.
Part: BRACE — CRACKED (BS 814) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC3315, FOUND THE AFT FUSELAGE INTERIOR LH FS814 WL200 BRACE CRACKED, LBL63. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: BEAM — DAMAGED (BS 588) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH FS588 MAIN LANDING GEAR BEAM ASSEMBLY WITH ELONGATED HOLES AT WL200, RBL65. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FITTING — CRACKED (BS 246) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH FS246 CHINE ANGLE FITTING CORRODED & CRACKED RBL 61, WL142. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: FRAME — CORRODED (BS 477) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5316, FOUND THE FS477 OVERHEAD FRAME CORRODED, LBL18-RBL18, WL282. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: LONGERON — CORRODED (BS 617-737) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION CORROSION ON LONGERON FS617 TO FS737 RBL20 WL280. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: WINDOW FRAME — CORRODED · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313 FOUND CABIN WINDOW FLANGE EXFOLIATION CORROSION AT FS447, WL170 LBL82 AND RBL82. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS417 RING SEGMENT WITH ELONGATED HOLES AT WL150-161, LBL63-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2755.
Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT SIDE CENTER AND AFT LOWER WINDOWS WITH CRACKED UPPER FRAME (WL251), AT 2 LOCATIONS NEAR POTS #3; FS135, LBL42. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2851.
Part: SKIN — WARPED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR EXTERIOR SKIN WARPED AT FS864 AND LBL36-46. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6076.
Part: SKIN — DENTED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5212, FOUND CARGO DOOR EXTERIOR SKIN DENTED WITH MULTIPLE SCRATCHES AT FS1012-1034 AND LBL36-RBL10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6085.
Part: STIFFENER — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC52125, FOUND CARGO DOOR BHD STIFFENER CRACKED AT FS1012 LBL30, LBL20, LBL0, AND RBL10. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6088.
Part: ATTACH FITTING — CORRODED (RAMP DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP DOOR EDGE SCRAPER ATTACHMENT LEADING EDGE CORRODED AT RS0, LBL60, AND RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6101.
Part: BULKHEAD — CORRODED (LT MLG WW) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT UPPER MAIN WHEEL WELL BHD WEB CORRODED AND CRACKLING AT FS577 AND WL230. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6102.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO COMPT INT LT BHD SKIN WITH OLD PATCH REPAIRED AND CORRODED AT FS617, WL280-285, AND RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6109.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND ATTACHMENT UPPER CAP WITH PITTING CORROSION AT FS597, WL285, AND CWS108. REPAIRED IAW MEA 382-57-18-152. NR# 6112.
Part: RIB — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP DOOR BOTTOM PEDESTAL ATTACHMENT RIB WARPED AND CRACKED AT RS10, LBL12-22 AND RBL12-22. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2019.
Part: WEB — CRACKED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP DOOR LT SIDE BEAM WEB CRACK AT RS4, WL138-146, AND LBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6136.
Part: SPAR — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RT CTR WING FWD SPAR WEB CRACK 1" LONG AROUND #3 ENGINE TRUSS UPPER TANG CUT OUT ACCESS AREA AT CWS176-220. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6143.
Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT MAIN WHEEL WELL FS617 BULKHEAD PRESSURE WEB CRACKED AT WL190, BL84. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6189.
Part: BUMPER — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE AFT FUSELAGE FS1038 CARGO DOOR SEAL BUMPER BENT AND CRACKED AT LBL55 AND RBL55. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6190.
Part: RING ASSEMBLY — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS344.0E LT RING SEGMENT CRACKED AT WL140 CHINE ANGLE ATTACHMENT FITTING; LBL61. REPAIRED IAW MEA 382-53-18-157. NR# 6206
Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND THE UNDERDECK SUPPORT ANGLE CORRODED BEYOND LIMITS AT FS218-244, LBL60, WL195. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6215.
Part: STRINGER — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING #15 (FS538) HOLE A19 CRACKED AT CWS178R, WL257. REPAIRED IAW MEA 382-57-18-200. NR# 6225.
Part: SKIN — CORRODED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LOWER BELLY SKIN CORRODED IN SEVERAL AREAS; FS577-617, WL126-142, LBL61-RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6242.
Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT MAIN WHEEL WELL FS477-TO-517 WL200 INTERCOSTAL BEAM OUTBOARD CAP WITH ELONGATED HOLES; RBL61-68. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6260.
Part: FRAME — CORRODED (RUDDER) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER FRAME WEB CORRODED BEYOND LIMITS AT SEVERAL PLACES. FS1128-1200, LBL12-RBL12, WL286. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6270.
Part: CAP — CORRODED (CARGO DOOR) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FS924 BULKHEAD UPPER CAP CORRODED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6344.
Part: SPAR — CRACKED (LT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT OUTER WING FRONT SPAR WEB WITH 2 CRACKS AT OWS58 AND WL259-287. REPAIRED IAW SRM FIG. 57-030-22. NR# 6658.
Part: SKIN — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP DOOR EXT SKIN IN NEED OF REPLACEMENT DUE TO A PREVIOUSLY REPAIR BEING WARPED AT RS0-10 AND RBL2-LBL32. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2013.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5313, FOUND FLOORBEAM UPPER CAP CORRODED AT FS257.0E. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6622.
Part: WEB — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT CTR WING FRONT SPAR 2" CRACK AND MISDRILLED AT FS517, WL256-285, AND LCWS71. REPAIRED IAW SRM FIG. XX-YYY-ZZ. NR# 6118.
Part: SKIN — BULGED (TE FLAP) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT OUTBD FLAP LOWER SKIN BEHIND ENGINE #4 EXHAUST AREA BULGED - SUSPECT CORRODED LOWER CAP. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6549.
Part: STIFFENER — DAMAGED (BS 777-817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND ELONGATED HOLES IN BELLY SKIN INNER STIFFENER FS777E TO FS817E LBL5 TO LBL10 WL126. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: WEB — WARPED (BS 817) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND WARPED INTERCOSTAL RIB FS817E LBL10 TO RBL 10 WL130 TO WL140 / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, 51-60 & 51-70.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5324, FOUND THE LT MAIN WHEEL WELL FS617 CHINE ANGLE WITH 3" CRACK, AND CORRODED AT FS697 EXTERIOR SURFACE; LBL61, WL141. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2795.
Part: SPLICE — CRACKED (LT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, THE LT UPPER MAIN WHEEL WELL FS477 BULKHEAD WEB SPLICE TEE FOUND CRACKED AT WL225. LBL61-85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6324.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT UPPER FLOORBEAM CAP CORRODED AT 2 PLACES AT FS577, WL146, AND LBL30. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2432.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS430 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2756.
Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE RT ELEVATOR LEADING EDGE SKIN WITH MULTIPLE CUT MARKS AT HSS51-79R, HSS107-122R, AND HSS165-180R LOWER SKIN. FS1101, WL275. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6318.
Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND AFT FUSELAGE OH STIFFENER WITH TEMPORARY REPAIR AT FS928, WL285, AND LBL20-RBL20. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2231.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND FLOOR END BHD LOWER CAP CORRODED WITH TEMPORARY REPAIR AT FS817.0E, WL130-140, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2314.
Part: INTERCOSTAL — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND RAMP DOOR INTERIOR INTERCOSTAL BEAM WARPED AND CRACKED AT RAMP STA.6-8. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2391.
Part: FAIRING — DAMAGED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RAMP DOOR PEDESTAL LT FAIRING WITH ELONGATED HOLE AND TEMP REPAIR. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2014.
Part: RIB — CORRODED (TE FLAP) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP LEADING EDGE RIB CORRODED AND CRACKED AT OWS183-201. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6621.
Part: RIB — CRACKED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OUTBD FLAP RIB FORMER WITH MULTIPLE CRACKS AND CORROSION AT FLAP STA.0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6546.
Part: SKIN — WARPED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND EXT BELLY SKIN WARPED WITH MULTIPLE REPAIR PATCHES, DENTS, AND STONE MARKS AT FS657-697, WL126, AND LBL61-RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 1692.
Part: ADAPTER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE UPPER FUSELAGE FS303 BL0 ANTENNA ADAPTER CORRODED BEYOND LIMITS, WL285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6163.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE FUSELAGE LOWER SKIN CORRODED AND WITH LOOSE RIVETS; FS180-196, LBL61-RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT LOWER CAP CORRODED AT FS597, WL126-140, AND RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2427.
Part: STRINGER — WARPED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING RT LOWER PLANK #20 STRINGER CWS165-218R SECTION WARPED. REPAIRED IAW MEA 382-57-18-150. NR# 6213.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FLOOR BEAM LOWER CAP WITH TEMPORARY REPAIR AT FS737, WL126-140, AND LBL61-RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2181.
Part: SKIN — BULGED (TE FLAP) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND RT INBD FLAP LOWER SKIN BULGED AT CWS128-206. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6466.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS284 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2747.
Part: SKIN — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND CARGO DOOR REAR BUMPER ASSY LOWER SKIN AND RIB, ANGLE FLANGE WITH MULTIPLE CRACKS AND DEFORMATION AT FS1034-1041, WL265-280, AND LBL60-RBL60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2220.
Part: TEE FITTING — CORRODED (BS 588 BULKHEAD) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RH MAIN WHEEL WELL FS588 LANDING GEAR BEAM TO WL200 HORIZONTAL BULKHEAD TEE CLIP CORRODED; RBL65. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE LH WINDOW RETAINER (FRAME) CRACKED AT POST #3 LOWER FWD END AT FS116, WL231, LBL42.6; AND TEMP REPAIRS AT POST #3 FWD UPPER END AT FS156 WL257 AND FS156 WL231. / REPAIRED IAW LAC MEA 382-53-18-037.
Part: RIB — CRACKED (BS 537-557) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321 FOUND EXFOLIATION CORROSION AND WARPED INTERCOSTAL RIB. FS537 TO FS557 LBL62 WL162. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS761.0E RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2736.
Part: SKIN — WARPED (RAMP DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5211, FOUND RAMP DOOR RT EXT SKIN WARPED WITH MULTIPLE SCRATCH MARKS AT RS6-10 AND RBL30-60. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2003.
Part: SKIN PANEL — CRACKED (LT WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND LT OTBD WING TRAILING EDGE LOWER SURFACE SKIN PANEL EXT CORRODED, BULGED, CRACKED, WITH INNER BEADED SKIN DEBONDED AND 4 PATCHES EXISTING AT FS597-617, WL560, AND OWS0-82. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2453
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS343 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2749.
Part: BULKHEAD WEB — CORRODED (BS 196) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND FS196 BULKHEAD RBL26-TO-RBL50 WEB SECTION WITH CORRODED WHERE IT MATES WITH REINFORCEMENT DOUBLER. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SKIN — CORRODED (BS 377-417) · corrosion level 2 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE FS377-417 BELLY SKIN WITH STONE MARKS AND CORRODED; LBL61-RBL61, WL126-146. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.
Part: STRINGER — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER WING CWS103R STRINGER #19 CRACKED; WL257. REPAIRED IAW MEA 382-57-18-192. NR# 6368.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS437 RING SEGMENT WITH ELONGATED HOLES AT WL158-161, LBL73-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2757.
Part: SKIN — DENTED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND THE FS297.0E-345.0E BELLY SKIN DENTED AND CORRODED, LBL60-RBL60, WL126-141. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2709.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND CARGO COMPT UPPER FLOORBEAM TIE DOWN RING NUTPLATE HOLES CORRODED AT FS717, WL146, AND RBL20-LBL40. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2438.
Part: RIB — DAMAGED (HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE HORIZONTAL STABILIZER LT LEADING EDGE HSS75L RIB UPPER END WITH ELONGATED HOLES. FS1040, WL285. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6453.
Part: RING ASSEMBLY — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE LT FS250 RING SEGMENT WITH ELONGATED HOLES AT WL150-161, LBL63-76. REPAIRED IAW SRM FIG. 51-140-21. NR# 2746.
Part: STIFFENER — DAMAGED (BS 677-697) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5312, FOUND THE FS677-697 BELLY SKIN STIFFENER AT LBL18 WITH ELONGATED HOLES; WL130. REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SRM 51-60 & 51-70.
Part: BULKHEAD — CRACKED (BS 165) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5312, FOUND THE NOSE WHEEL WELL FS165 LBL28 BULKHEAD TEE CAP CORRODED & CRACKED; WL130. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70.
Part: SEAT TRACK — DAMAGED (BS 131-157) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5311, FOUND THE COPILOT'S SEAT TRACKS WORN, WITH ELONGATED LOCATING HOLES. FS131-FS157, RBL13 & RBL27, WL202. / REPAIRED IAW LAC MEA 382-53-99-164 R5. NR# 2101.
Part: CAP — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CWS178R VERTICAL ATTACH TEE CAP CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6376.
Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5314, FOUND FLOOR END BHD CORRODED WITH EXCESS HOLES AND REDUNDANT DRAIN TUBE HOLES AT FS817.0E, WL130-146, AND LBL56-RBL56. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2386.
Part: STIFFENER — CORRODED (RT MLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION ON RT UPPER MAIN WHEEL WELL U STIFFENER FS590 WL201 RBL61 TO RBL85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6433.
Part: SPAR CAP — CORRODED (HORIZ STAB) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER FWD BEAM (SPAR) UPPER CAP CORRODED BETWEEN HSS63L-70L. FS1041, WL280. REPAIRED IAW MEA 382-55-18-080. NR# 6312.
Part: RIB — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT AFT FUSELAGE INT RIB CRACKED WITH MULTIPLE ELONGATED HOLES AT FS808, AND WL170-185. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6148.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND THE RT FS364 RING SEGMENT WITH ELONGATED HOLES AT WL158, RBL73. REPAIRED IAW SRM FIG. 51-140-21. NR# 2720.
Part: BULKHEAD WEB — CORRODED (BS 597) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND EXFOLIATION CORROSION ON FS597 UNDERFLOOR BULKHEAD WEB, LBL40 TO RBL50, WL125 TO WL145. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM. 51-60 & 51-70.
Part: LONGERON — CORRODED (FUSELAGE) · corrosion level 3 · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5321, FOUND RT UPPER MAIN WHEEL WELL LONGERON CORRODED AND WITH TEMPORARY REPAIR AT FS617-737 AND RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70. NR# 2222.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5315, FOUND BHD LT AFT FUSELAGE INTERIOR INBD CAP WITH TEMPORARY REPAIR AT FS834, WL180, AND LBL61-66. REPAIRED IAW SMP583 SRM FIG. 51-140-23. NR# 2234.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE FS817.0E RT RING SEGMENT WITH RIVET DAMAGE, WL240-252, RBL69-75. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2715.
Part: ATTACH ANGLE — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND CTR WING LT FWD BEAM WING ATTACH ANGLE TO LEADING EDGE RIB CRACKED AT LOWER BEND RADIUS 1.5" AT FS517, WL260-285, AND CWS174. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2469.
Part: SPAR — CRACKED (CENTER WING) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5711, FOUND THE CENTER WING REAR SPAR WEB CRACKED AT CWS18R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6223.
Part: BULKHEAD — CRACKED (CARGO DOOR) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO DOOR INT BHD WEB WITH MULTIPLE ELONGATED HOLES AND CRACK AT FS1012 AND LBL40. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6138.
Part: BULKHEAD — CRACKED (NLG WW) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE NOSE WHEEL WELL AFT BULKHEAD (WHEEL CUTOUT) FS201 LOWER WEB CORRODED & CRACKED, LBL10-RBL10, WL130. REPAIRED IAW SRM FIG. XX-YYY-ZZ. NR# 2713.
Part: FORMER — CRACKED (FUSELAGE) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LT PRESSURIZED SKIN PANEL ATTACHMENT FORMER WITH 6" CRACK AT FS597-617, WL285, AND RBL23. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6107.
Part: RIB — DAMAGED (HORIZ STAB) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE HORIZONTAL STABILIZER LT LEADING EDGE HSS80L RIB LOWER END WITH ELONGATED HOLES. FS1040, WL260. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6455.
Part: SKIN — CRACKED (RT AILERON) · airframe 38,886 hrs · 24,089 cycles
DURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5712, FOUND THE RT AILERON LEADING EDGE DEFORMED AND CRACKED AT AS0R AND AS86R. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6158.