N691CA
Registered owner: DELTA AIR LINES INC, GA (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.
242 reports on file, 2007-11-11 – 2026-07-26.
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 41,469 hrs · 30,093 cycles
OVERHEAD EMERGENCY LIGHT INOP @ ROW 17. R/R BULB OPC GOOD IAW CRJ900 AMM 33-51-09
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 41,142 hrs · 29,809 cycles
MULTIPLE FWD GALLEY AREA AND FORWARD PASSENGER AREA EMERGENCY LIGHTS INOP. DURING TROUBLESHOOTING, BORROWED KNOWN GOOD BATTERY CHARGER ASSY FROM 15153. ONCE KNOWN GOOD BATTERY CHARGER ASSY WAS INSTALLED IN THE #1 POSITION (CRJ 900 AMM 33-51-17-400--802-A02), ALL EMERGENCY LIGHTS FOR BATTERY #1 WORKED. REMOVED BORROWED CHARGER ASSY (CRJ 900 AMM 33-51-17-000-802-A02) REPLACEMENT OF THE BATTERY CHARGER ASSY FOR BATTERY #1 POSITION REQUIRED. REMOVED FAULTY EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-17-000-802-A02 AND INSTALLED SERVICEABLE EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-17-400-802-A02. OPS TESTS PASSED. REMOVED FAULTY EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-17-- 000-802-A02 AND INSTALLED SERVICEABLE EMERGENCY POWER SUPPLY UNIT IAW AMM 33-51-17-400-802-A02.
Part: BEARING — DAMAGED (ZONE 600 AILERON) · airframe 41,142 hrs · 29,809 cycles
FOUND 1 EA. R/H AILERON SIDE BEARING LUG LABELED H TO BE PREVIOUSLY OVERSIZED REPAIRED IAW CRJ 900 MHIRJ REO 690-57-61-514 REV -- DATED 2026-05-08
Part: BUSHING — DAMAGED (AILERON) · airframe 41,142 hrs · 29,809 cycles
FOUND 4EA. R/H AILERON SIDE BUSHING LUGS LABELED B,C,F,AND G TO BE PREVIOSLY OVERSIZED REPAIRED IAW CRJ 900 MHIRJ REO 670-57-61-237 REV -- DATED 2017-07-25
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 41,142 hrs · 29,809 cycles
PAX FLOOR SEAT TRACK AT RBL9 CORRODED AT FS349. REPAIRED IAW MHI RJ REO 670-53-00-589 REV -D 2025-08-20.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 41,142 hrs · 29,809 cycles
PAX FLOOR SEAT TRACK AT LBL9 CORRODED AT FS379. REPAIRED IAW MHI RJ REO 670-53-00-589 REV -D 2025-08-20.
Part: BUSHING — DAMAGED (ZONE 600 AILERON) · airframe 41,142 hrs · 29,809 cycles
FOUND RT AILERON SIDE LUG LABELED -C- TO BE ABOVE 4TH OVER PER GREO 670-57-61-237 BY 0.0225, COMPLIED WITH REPAIR OF BUSHING LUG MARKED C IAW MHIRJ REO 690-57-61-518 REV -- DATED 2026-05-22.
Part: LUG — DAMAGED (ZONE 600) · airframe 41,142 hrs · 29,809 cycles
"R/H WING SIDE AILERON HINGE #3 (I/B) HAS A PREVIOUSLY O/S LUG LABELED ""E"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #3 IB LUG IAW MHIRJ REO 690-57-51-269 REV B DATED 2026-04-28."
Part: LUG — DAMAGED (ZONE 600) · airframe 41,142 hrs · 29,809 cycles
"R/H WING SIDE AILERON HINGE #2 (I/B) HAS A PREVIOUSLY O/S LUG LABELED ""C"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #2 IB LUG IAW MHIRJ REO 690-57-51-269 REV B DATED 2026-04-28."
Part: LUG — DAMAGED (ZONE 600) · airframe 41,142 hrs · 29,809 cycles
"R/H WING SIDE AILERON HINGE #3 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""F"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #3 OB LUG IAW MHIRJ REO 690-57-51-269 REV B DATED 2026-04-28."
Part: LUG — DAMAGED (ZONE 600) · airframe 41,142 hrs · 29,809 cycles
"R/H WING SIDE AILERON HINGE #2 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""D"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.8910""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED RH WING SIDE AILERON FITTING #2 OB LUG IAW MHIRJ REO 690-57-51-269 REV B DATED 2026-04-28."
Part: FITTING — CRACKED (ZONE 800) · airframe 41,142 hrs · 29,809 cycles
LEFT AFT OVERWING EMERGENCY EXIT DOOR THE UPPER FORWARD ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE IS CRACKED REPAIRED LH AFT OVERWING EMERGENCY EXIT IAW MHIRJ REO 690-52-21-228 REV -- DATED 2026-05-25 AND MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06.
Part: FITTING — CRACKED (ZONE 800) · airframe 41,142 hrs · 29,809 cycles
RIGHT FWD OVERWING EMERGENCY EXIT DOOR, THE UPPER AFT ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE, HAS EVIDENCE OF A CRACK. REPAIRED IAW REO 670-52-21-103 REV -- DATE 2024-11-06 AND CRJ 900 SRMS 51-26-01-001-001-A01 AND 51-42-21-001-001-A01. SEE MAINTENANCE TASK CARD FOR DETAILS OF WORK PERFORMED.
Part: LUG — DAMAGED (ZONE 500) · airframe 41,142 hrs · 29,809 cycles
"L/H WING SIDE AILERON HINGE #3 (I/B) HAS A PREVIOUSLY O/S LUG LABELED "E". CURRENT LUG INTERNAL DIAMETER MEASURES (0.9065""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED LH WING SIDE AILERON FITTING #3 IB LUG IAW MHIRJ REO 690-57-51-269 REV B DATED 2026-04-28."
Part: LUG — DAMAGED (ZONE 500) · airframe 41,142 hrs · 29,809 cycles
"L/H WING SIDE AILERON HINGE #3 (O/B) HAS A PREVIOUSLY O/S LUG LABELED ""F"". CURRENT LUG INTERNAL DIAMETER MEASURES (0.9065""). NOMINAL LUG INTERNAL DIAMETER IS (0.8750""). ENGINEERING IS REQUIRED. REPAIRED LH WING SIDE AILERON #3 FITTING OB LUG IAW MHIRJ REO 690-57-51-269 REV B DATED 2026-04-28."
Part: FITTING — CRACKED (ZONE 800) · airframe 41,142 hrs · 29,809 cycles
LEFT AFT OVERWING EMERGENCY EXIT DOOR THE UPPER FORWARD ALIGNMENT SPIGOT FITTING STRUCTURE NEAR THE BASE IS CRACKED. REPAIRED LH AFT OVERWING EMERGENCY EXIT IAW MHIRJ REO 690-52-21-228 REV -- DATED 2026-05-25 AND MHIRJ REO 670-52-21-103 REV -- DATED 2024-11-06.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,142 hrs · 29,809 cycles
L/H FS 280 CROSSBEAM HAS CORRODED PIT ON TOP CORNER EDGE OF THE BEAM. REMOVED FS 280 SACRIFICIAL TITANIUM PLATE FOR ACCESS IAW CRJ-900 SRM 51-42-13-001-001-A01. REMOVED DAMAGED LH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW LH FS 280.00 CROSSBEAM P/N:CC670-34094JP-1S IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW LH FS 280.00 CROSSBEAM P/N:CC670-34094JP-1S IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. APPLIED PAINT IAW CRJ 900 SRM 51-25-16-001-001-A01 TO FWD AND AFT SIDES OF LH FS 280.00 CROSSBEAM. APPLIED CIC IAW CRJ 900 SRM 51-21-11-001-001-A01 ON FWD AND AFT LH FS280.00 CROSSBEAM. INSTALLED FS 280 SACRIFICIAL TITANIUM PLATE IAW CRJ-900 SRM 51-42-06-001-001-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 41,142 hrs · 29,809 cycles
R/H FS 280 CORRODED ON BOTTOM CORNER EDGE OF THE BEAM. REMOVED DAMAGED RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW RH FS 280.00 CROSSBEAM P/N:CC670-34094JP-2S IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW RH FS 280.00 CROSSBEAM P/N: CC670-34094JP-2S IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. APPLIED PAINT TO RH FS 280.00 CROSSBEAM P/N:CC670-34094JP-2S IAW CRJ 900 SRM 51-25-16-001-001-A01 APPLIED CIC TO FWD AND AFT RH FS 280.00 CROSSBEAM P/N:CC670-34094JP-2S IAW CRJ 900 SRM 51-21-11-001-001-A01.
Earlier reports · 2007–2025 · 224 reports
2025
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 39,233 hrs · 28,146 cycles
RH AFT EXTERIOR EMERGENCY LIGHT INOP RELAMPED RH AFT EXTERIOR EMERGENCY LIGHT IAW CRJ 900 IPC 33-51-15. OPS TEST GOOD IAW AMM 33-51-15. P/N OFF/ON: 8GH002473-08
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 38,671 hrs · 27,679 cycles
FOUND EMERGENCY FLOOD LIGHT BULB IN-OP AFT OF GALLEY R/R EMERGENCY FLOOD LIGHT BULB IAW CRJ 900 AMM 33-51-09-960-801 OPS CHECK GOOD. P/N ON/OFF 1317 NSN
2024
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 37,857 hrs · 26,999 cycles
EMERGENCY LIGHT INOP ROW 3DC RELAMP EMERGENCY LIGHT PER AMM 33-51-09 P/N ON/OFF: 1317
Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,270 hrs · 25,623 cycles
LH AFT OVERWING EMERGENCY LIGHT INOP REMOVED AND REPLACED LH AFT OVERWING EMERGENCY LIGHT IAW CRJ 900 AMM 33-51-15. OP CHECKED GOOD.
2023
Part: RETAINER — CRACKED · airframe 34,541 hrs · 24,090 cycles
FOUND THE PAX DOOR CENTER BOTTOM SEAL RETAINER TO BE DAMAGED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-42-06-001-001-A01 AND 52-11-07-201-001-A01 REPAIR TYPE 2.
Part: INTERCOSTAL — CRACKED · airframe 34,541 hrs · 24,090 cycles
WHILE PERFORMING SB 670BA-53-044 REVISION G DATED JUL05/2022 FOUND INTERCOSTAL GC213-00021-7 TO BE BENT AND CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
2022
Part: FORMER — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR FWD FORMER IS CORRDED. REMOVED AND REPLACED FWD FORMER IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: SPLICE — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON SPLICE AT 23R AT F.S. 333. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
STRINGER 24L IS CORRODED BETWEEN FS 501.00 AND 517.00. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: FRAME — CORRODED · airframe 33,771 hrs · 23,462 cycles
FRAME IS CORRODED AT FS 485.00 BETWEEN STGR 24L AND 26R. REPAIRED IAW ENDEAVOR EA CRJ953-14201 ISSUE DATE 8/3/2022 REV IR
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
RH SIDE SEAT RAIL BETWEEN FS 469-483 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED IAW CRJ 900 SRM 53-00-49-201-002-A01 AND CRJ 900 AMM 53-00-49-400-801-A07.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON STGR 26R BETWEEN FS 1051.30-1069.75 REPAIRED IAW ENDEAVOR EA CRJ953-14233 REV. A DATED 8/8/2022.
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
L/H FLOOR SILL ANGLE IS CORRODED BETWEEN F.S.720 TO F.S.847. REPAIRED IAW ENDEAVOR EA CRJ953-14337 REV IR DATED 8/10/22.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON STRINGER 23R BETWEEN F.S. 280.00 TO F.S. 333.00. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON STGR 26R BETWEEN FS 1015-1031. REPAIRED IAW ENDEAVOR EA CRJ953-14232 REV. A DATED 8/8/2022.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON STRINGER 23R BETWEEN F.S. 333.00 TO F.S. 379.00. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01.
Part: STIFFENER — CRACKED · airframe 33,771 hrs · 23,462 cycles
LBL 27 FS 280 BULKHEAD STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW CRJ 900 SRMS
Part: ANGLE — CRACKED · airframe 33,771 hrs · 23,462 cycles
L/H VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED AND REPLACED IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
NOSE JACK PAD FITTING LH INTERCOSTAL CORRODED JUST FWD OF FS 280.00 REPAIRED IAW ENDEAVOR EA CRJ953-14244 REV IR DATED 8/3/22.
Part: WEB — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR FWD WEB STRUCTURE IS CORRODED. REPLACED FWD WEB STIFFNERS 6EA, TEE- STIFFNERS, GAS SPRING BEAM AND STOW CUP IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
NOSE JACK PAD FITTING RH INTERCOSTAL CORRODED JUST FWD OF FS 280.00 REPAIRED IAW ENDEAVOR EA CRJ953-14245 REV IR DATED 8/3/22.
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
LH SIDE SEAT RAIL STRUCTURE BETWEEN FS 661+8-670 HAS MULTIPLE SPOTS OF CORROSION INSTALLED NEW SIDE SEAT RAIL P/N SH 690-36283-1 ON L/H BETWEEN F.S661+8 TO F.S670 WL 85.25 IAW CRJ AMM 53-00-49-400-801-CONFIG A07
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
RH SIDE SEAT RAIL BETWEEN FS 677-720 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED SIDE SEAT RAIL SH690-36284-1 IAW CRJ 900 AMM 53-00-49-400-801-A07
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
RH SIDE SEAT RAIL BETWEEN FS 571-661+13 HAS MULTIPLE SPOTS OF CORROSION. REPLACED SEAT RAIL IAW CRJ900 AMM 53-00-49-400-801-A07 AND SRM 51-40-11-001-001-A01
Part: FRAME — CRACKED · airframe 33,771 hrs · 23,462 cycles
R/H AFT OVERWING EXIT DOOR (S/N SBO538) TOP EDGE MEMBER IS CRACKED. REPAIRED IAW EA CRJ952-14361 REV-IR DATED: 8/26/2022.
Part: ANGLE — WORN · airframe 33,771 hrs · 23,462 cycles
PAX DOOR AFT DRAG ANGLE HAS ELONGATED HOLES LOCATED, DRILLED AND INSTALLED PAX DOOR DRAG ANGLE TO AFT WEB IAW CRJ900 SRM 52-40-11-001-001-A01, SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
MULTIPLE AREAS OF CORROSION FOUND ON STRINGER 24R BETWEEN F.S. 295.00 TO F.S. 349.00. REMOVED AND REPLACED STGR 24R BTW FS 280-333 IAW CRJ900 SRM 51-42-06-0001-001-A01.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
STRINGER 25R IS CORRODED BETWEEN FS 581.00 AND 597.00. REPAIRED STRINGER 25R BETWEEN FS 581.00 AND 597.00IAW EA# CRJ953-14334 DATED 08/06/2022.
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
LH SIDE SEAT RAIL BETWEEN FS847+14-907 HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS847.00+14 TO FS907 WITH P/N SH670-37543-3, IAW CRJ900 AMM 53-00-49-400-801-A01
Part: CLEAT — CORRODED · airframe 33,771 hrs · 23,462 cycles
INTERCOSTAL DD6 AT AFT SIDE CLEAT FOUND TO BE CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE INTERCOSTAL DD6 CLEAT AT AFT SIDE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: PANEL — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR, TOP STEP CORRODED.. LOCATED AND DRILLED NEW TOP PANEL P/N 601R317075-3 IAW CRJ-900 SRM 51-40-11-001-001-A01.
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR, FWD WEB DRAG ANGLE IS CORRODED. LOCATED, DRILLED, AND INSTALLED A NEW SERVICEABLE FWD DRAG ANGLE IAW CRJ900 SRM 51-40-11-001-001-A01, AND 51-42-06-001-001-A01
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON STRINGER 27 AFT BETWEEN F.S. 310.00 TO F.S. 319.00. REMOVED AND REPLACED STRINGER 27 AFT BETWEEN F.S. 295.00 TO F.S. 333.00 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR ANGLE DD7A CORRODED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE ANGLE PN 601R317052-1 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
MULTIPLE AREAS OF CORROSION ON STRINGER 25R BETWEEN F.S. 308.00 TO F.S. 319.00. REMOVED STRINGER 25R FROM F.S. 280-F.S.333 IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED STGR 25R FROM FS280 TO FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: BEAM — CORRODED · airframe 33,771 hrs · 23,462 cycles
FLOOR BEAM AT LBL9 HAS MULTIPLE SPOTS OF CORROSION FROM FS1000 TO FS1088. REPAIRED FLOOR BEAM IAW CRJ900 SRM 53-00-41-201-001-A03.
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON LBL 9 SEAT TRACK BETWEEN FS 379-485. REMOVED AND REPLACED SEAT TRACK AT LBL 9 BETWEEN F.S.379 TO F.S.485
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
MID INTERCOSTAL AT DD6 FOUND TO BE CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
Part: FORMER — CORRODED · airframe 33,771 hrs · 23,462 cycles
AFT FORMER ON PASS DOOR FOUND TO HAVE CORROSION IN MULTIPLE LOCATIONS. LOCATED, DRILLED, AND INSTALLED SERVICEABLE AFT FORMER IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON LBL 27 SEAT TRACK BETWEEN FS 364-485. REMOVED AND REPLACED SEAT TRACK AT LBL 27 BETWEEN F.S.364 TO F.S.485
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
INTERCOSTAL DD6 AT AFT SIDE FOUND TO BE CORRODED. REMOVED AND REPLACED INTERCOSTAL DD6 AT AFT SIDE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: SKIN — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR INNER SKIN IS CORRODED. REMOVED AND REPLACED INNER SKIN IAW CRJ 900 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR CENTER INTERCOSTAL DD7 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: FRAME — CRACKED · airframe 33,771 hrs · 23,462 cycles
L/H FWD OVERWING EXIT DOOR (S/N SBO532) TOP EDGE MEMBER IS CRACKED. REPAIRED DAMAGE I.A.W. ENDEAVOR EA CRJ952-14342 REV.IR, DATED 08/26/2022
Part: FRAME — CRACKED · airframe 33,771 hrs · 23,462 cycles
L/H AFT OVERWING EXIT (S/N SBO539) TOP EDGE MEMBER IS CRACKED COMPLIED WITH ENDEAVOR EA CRJ952-14340 REV IR DATED 8/26/22
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
FRAME (ANGLE) CORRODED AT FS265.00 BETWEEN STGR 26L AND 27 REMOVED AND REPLACED ANGLE IAW BOMBARDIER CRJ900 SRM 51-42-06-001-001-A01
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
LH SIDE SEAT RAIL BETWEEN FS 670-720 HAS MULTIPLE SPOTS OF CORROSION INSTALLED NEW SIDE SEAT RAIL P/N SH690-36284-1 ON L/H BETWEEN FS670-FS720 WL 85.25 IAW CRJ 900 AMM 53-00-49-400-801-A01
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
SEAT TRACK LBL9 BETWEEN FS 661+32-681 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW SEAT TRACK @ LBL 9 BETWEEN FS 661.00+32 TO FS 681.00 IAW CRJ 900 AMM 53-00-49-400-801 (A07)
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
L/H FLOOR SILL DRIP TRAY IS CORRODED AT RIVETS BETWEEN F.S.693 TO F.S.847. REMOVED AND REPLACED L/H FLOOR SILL DRIP TRAYS BETWEEN F.S. 693 AND F.S. 847 WITH NEW SERVICEABLE P/N'S SH670-36175-3, SH670-36171-3 AND SH670-36172-3 IAW ENDEAVOR EA CRJ953-14502 REV A DATED 09/09/2022.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
STRINGER 22L IS CORRODED BETWEEN FS 501.00 AND 517.00. COMPLIED WITH ENDEAVOR EA CRJ953-14312 REV IR DATED 8/10/22
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
MULTIPLE AREAS OF CORROSION ON STRINGER 26L BETWEEN F.S. 310.00 TO F.S. 333.00. REMOVED CORRODED STGR 26L FROM FS 295 TO FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED STGR 26L FROM FS 280 TO FS 333 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
SEAT TRACK RBL 9 BETWEEN FS 681-836 HAS MULTIPLE SPOTS OF CORROSION. FABRICATED SEAT TRACK PART NUMBER BA690-30000-5979 OUT OF RAW STOCK PART NUMBER 20276-288-0-0A IAW CRJ900 SRM 53-00-49-201-002-A01, INSTALLED TRACK IAW CRJ900 AMM 53-00-49-000/400-801-A07.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
MULTIPLE AREAS OF CORROSION ON STRINGER 25L BETWEEN F.S.280 TO F.S.333 REMOVED AND REPLACED STRINGER 25L BETWEEN F.S.280 TO F.S.333.
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON RBL 9 SEAT TRACK BETWEEN FS 349-485. REMOVED CORRODED SEAT TRACK RBL 9 F.S.349 TO F.S.485 AND INSTALLED NEW SERVICEABLE SEAT TRACK RBL 9 F.S. 349-485 IAW CRJ-900 -AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
SEAT TRACK LBL9 BETWEEN FS 681-836 HAS MULTIPLE SPOTS OF CORROSION. REPLACED LBL9 SEAT TRACK BETWEEN FS681 AND FS836 IAW CRJ900 AMM 53-00-49-400-801-A07 AND SRM 51-40-11-001-001-A01
Part: SPLICE — CORRODED · airframe 33,771 hrs · 23,462 cycles
FWD BELLY FAIRING SUPPORT STRAP FOR PANEL 191AB IS CORRODED INSTALLED NEW SPLICE JOINT PLATE P/N SH670-39054-3 IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01.
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
LH SIDE SEAT RAIL BETWEEN FS 785.15-847+14 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS 785.15-847+14 CRJ 900 AMM 53-00-49-400-801-A07
Part: INTERCOSTAL — CRACKED · airframe 33,771 hrs · 23,462 cycles
INTERCOSTAL DD1 AT AFT SIDE FOUND TO BE CRACKED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL DD1 AT AFT SIDE IAW 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 PN:601R31902-318
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
FWD NUT PLATE ANGLE FOR PANEL 642AZ IN RH WHEEL WELL IS CORRODED. REPLACED ANGLE P/N CC670-10338-2 IAW CRJ 900 SRM 51-42-21-001-001-A01
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
SEAT TRACK LBL9 BETWEEN FS 581-661+32 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND INSTALLED NEW SERVICEABLE LBL9 SEAT TRACK P/N: SH690-33404-1 FROM FS581 TO FS661+32 IAW CRJ900 AMM 53-00-49-400-801-A07.
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
LH SIDE SEAT RAIL BETWEEN FS 744-752 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED LH SIDE SEAT RAIL BETWEEN FS 744.15 TO FS 761.85 WITH P/N SH690-36285-1 IAW CRJ900 AMM 53-00-49-400-801-A07
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
INTERCOSTAL DD2 AT FWD SIDE FOUND TO BE CORRODED ON PAX DOOR LOCATED, DRILLED AND INSTALLED INTERCOSTAL DD2 AT FWD SIDE ONTO PAX DOOR IAW CRJ900 SRM 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01 P/N 601R318051-1
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
RH SIDE SEAT RAIL AT FS 847+13-868 HAS MULTIPLE SPOTS OF CORROSION. REPLACED RH SIDE SEAT RAIL AT FS847+13-868 IAW CRJ900 AMM 53-41-49-400-801-A07
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
STRINGER 23R IS CORRODED BETWEEN FS 364.00 AND 379.00 REPLACED STGR23R FROM FS280 TO FS379 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
MID INTERCOSTAL AT DD4 FOUND TO BE CORRODED IN MULTIPLE LOCATIONS. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE MID DD4 INTERCOSTAL IAW CRJ 900 SRM 51-40-11-001-001-A01 51-42-21-001-001-A01 AND 51-42-06-001-001-A01 PN: 601R318081-1S
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
WHILE REMOVING INTERCOSTAL DD4 AT AFT SIDE FOUND THE CLEAT TO BE CORRODED IN MULTIPLE LOCATIONS. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL DD4 AT AFT SIDE CLEAT IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 PN: 600-31902-269
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
FWD NUT PLATE ANGLE FOR PANEL 542AZ IN WHEEL WELL IS CORRODED. REPLACED ANGLE P/N CC670-10338-1 IAW CRJ 900 SRM 51-42-21-001-001-A01
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
RH SIDE SEAT RAIL AT FS 868-969 HAS MULTIPLE SPOTS OF CORROSION. FABRICATED NEW SIDE SEAT RAIL FROM MAT. EXTRUSION P/N 20276-288-0-0A P/O:W000077329 IAW CRJ 900 SRM 53-00-49-201-002-A01 STEP 3 (A,B,C AND D) TABLE 1 PAGE 206. INSTALLED NEW SIDE SEAT RAIL ON APPROX R/H FS868 TO FS969 WL 85.25 IAW CRJ 900 AMM 53-00-49-400-801CONFIGA07
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
RH SIDE SEAT RAIL STRUCTURE AT FS 785.15-847+8 HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED RH SIDE SEAT RAIL STRUCTURE AT FS 785.15-847+8 CRJ 900 AMM 53-00-49-400-801-A07
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
RH SIDE SEAT RAIL AT FS 744-752 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW SIDE SEAT RAIL P/N SH690-36285-1 ON R/H FS 744 - FS 752 WL 85.25 IAW CRJ 900 AMM 53-00-49-400-801(CONFIG 07)
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
SEAT TRACK RBL9 BETWEEN F.S.661+32-681 HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED RBL9 SEAT TRACK SEGMENT
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
R/H SIDE SEAT TRACK IS CORRODED AT F.S.613 REMOVED, FABRICATED, AND INSTALLED NEW RIGHT SIDE SEAT TRACK SEGMENT
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
R/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S.549 AND F.S.565 REMOVED AND REPLACED RIGHT SIDE SEAT TRACK SEGMENT
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
AFT CARGO DOOR FLOOR SILL IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR FLOOR SILL
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
SEAT TRACK RBL9 BETWEEN F.S.485-581 HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED RBL9 SEAT TRACK SEGMENT
Part: NONE — CORRODED · airframe 33,771 hrs · 23,462 cycles
L/H SIDE SEAT TRACK IS CORRODED BETWEEN F.S.693 AND F.S.708 REMOVED AND REPLACED LEFT SIDE SEAT TRACK SEGMENT
Part: SEAT TRACK — CORRODED · airframe 33,771 hrs · 23,462 cycles
SEAT TRACK RBL9 BETWEEN F.S.581-661+32 HAS MULTIPLE SPOTS OF CORROSION REMOVED AND REPLACED RBL9 SEAT TRACK SEGMENT
Part: INTERCOSTAL — CORRODED · airframe 33,771 hrs · 23,462 cycles
PAX DOOR INTERCOSTAL DD4 AT AFT SIDE FOUND TO BE CORRODED LOCATED DRILLED AND INSTALLED NEW SERVICEABLE INTERCOSTAL DD4 AT AFT SIDE IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
Part: FRAME — CORRODED · airframe 33,771 hrs · 23,462 cycles
FRAME AT FS 927 CORRODED BETWEEN STRGR 24L AND 24R REMOVED AND REPLACED NEW FRAME P/N: SH690-37083-3 AT FS 927 BETWEEN STR 20L TO STR 23R IAW CRJ 900 SRM 53-00-06-201-001-A03
Part: CHANNEL — CRACKED · airframe 33,771 hrs · 23,462 cycles
AFT CARGO DOOR AFT TRACK LOWER FWD "U" CHANNEL IS CRACKED. REPLACEDâUâ CHANNEL P/N MM670-35552-005 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01.
Part: FRAME — CORRODED · airframe 33,771 hrs · 23,462 cycles
FRAME 379 IS CORRODED BETWEEN STRINGERS 20R TO 21R REPLACED FS379 FRAME BETWEEN STRINGERS 20R TO 25R IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01
Part: WEB — CORRODED · airframe 33,771 hrs · 23,462 cycles
F.S.280 L/H LOWER WEB AT DOOR POST IS CORRODED. INSTALLED NEW LOWER WEB REPAIR AND BUTTSTRAP AT F.S 280 L/H SIDE IAW CRJ-900 SRM 53-11-10-01-004-A01,51-42-06-001-001-A01AND 51-42-10-001-001-A01
Part: SPLICE — CORRODED · airframe 33,771 hrs · 23,462 cycles
STGR 21R SPLICED CORRODED AT FS 333 REPLACED STGR 21R FS 333 SPLICE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: SPLICE — CORRODED · airframe 33,771 hrs · 23,462 cycles
GUSSET AT FS 379 AND STRINGER 21R IS CORRODED. REPLACED JOINT PIECE AT STRINGER 21R BETWEEN FS 379 TO 394 IAW CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
F.S.280 BULKHEAD FWD "J" ANGLE IS CORRODED. REPLACED FS280 BULKHEAD FWD "J" ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
STGR 21R IS CORRODED BETWEEN FS 280 AND FS 333 REPLACED STGR 21R BTW FS 280 AND FS333 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: CHANNEL — CORRODED · airframe 33,771 hrs · 23,462 cycles
R/H #1 ATC ANTENNA CHANNEL IS CORRODED. REPLACED ANTENNA CHANNEL IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01
Part: ANGLE — CORRODED · airframe 33,771 hrs · 23,462 cycles
GALLEY DOOR LOWER SILL ANGLE IS CORRODED. REPLACED GALLEY DOOR LOWER SILL ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: WEB — CORRODED · airframe 33,771 hrs · 23,462 cycles
F.S.280 R/H BULKHEAD LOWER WEB AT DOOR POST IS CORRODED. INSTALLED NEW LOWER WEB REPAIR AND BUTTSTRAP AT F.S 280 R/H SIDE IAW CRJ-900 SRM 53-11-10-201-004-A01; 51-42-06-001-001-A01AND 51-42-10-001-001-A01.
Part: BEAM — CORRODED · airframe 33,771 hrs · 23,462 cycles
UPON REMOVING F.S 280 BULKHEAD FWD J ANGLE FOUND CORROSION AT CROSSBEAM. REPLACED THE FS280 CROSSBEAM IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-10-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON STGR 22R IN BETWEEN FS 333 TO FS 349 REPLACED STGR 22R BETWEEN FS333.00 TO FS349 IAW CRJ900 SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
STRINGER 21R BETWEEN F.S.333 TO F.S.349 IS CORRODED. REPLACED STGR 21R FROM FS 333 TO FS 379 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
Part: ANGLE — CRACKED · airframe 33,771 hrs · 23,462 cycles
FOUND CRACK ON ANGLE AT RBL 12 AND F.S 280 PN: CC670-34099-2SB. REPLACED ANGLE AT RBL 12 AND F.S 280 IAW CRJ-900 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
Part: CLEAT — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON CLEAT OF STGR 19L AT FS 295 REPLACED CLEAT AT STGR 19L AT FS 295 IAW CRJ900 SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED · airframe 33,771 hrs · 23,462 cycles
CORROSION FOUND ON STGR 22R IN BETWEEN FS 280 TO FS 295 REPLACED STGR 22R BETWEEN FS280.00 TO FS333.00 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
Part: FRAME — CORRODED · airframe 33,771 hrs · 23,462 cycles
FUSELAGE FRAME F.S.295 FROM STGR 26L TO STGR 26R IS CORRODED. REPAIRED FS295 FRAME SECTION 25L TO 25R IAW CRJ-900 SRM 53-00-06-201-001-A03.
Part: DOUBLER — CORRODED · airframe 33,771 hrs · 23,462 cycles
ANTENNA DOUBLER AT STRINGER 27 BETWEEN F.S.295 AND F.S.310 IS CORRODED REMOVED AND REPLACED ANTENNA DOUBLER AT STRINGER 27 BETWEEN F.S.295 AND F.S.310
Part: BUTTSTRAP — CORRODED · airframe 33,771 hrs · 23,462 cycles
CIRCUMFERENTIAL JOINT AT FS 333.00 IS CORRODED BETWEEN STGR 26L AND 26R. REMOVED (6) FASTENERS AT FS 333 C-JOINT BTW STGR 26L TO 26R FOR CORROSION REMOVAL IAW CRJ 900 SRM 51-42-06-001-001-A01 INSTALLED (6) FASTENERS AT FS 333 C-JOINT BTW STGR 26L TO 26R IAW CRJ 900 SRM 51-42-06-001-001-A01 CORROSION REMOVED IAW CRJ-900 SRM 51-21-06-001-001-A01.
2019
Part: PANEL — INOPERATIVE (NR 3) · airframe 28,050 hrs · 18,743 cycles
HYD 3 LOW PRESS CAUTION MSG FOLLOWED QRH DIVERTED TO JFK 0 PSI IN HYD 3 80% QUANTITY IN HYD 3 HAPPENED 20 MINS AFTER TAKE OFF. AN EMERGENCY WAS DECLARED. PERFORMED TROUBLESHOOTING IAW FIM 29-12-00. FOUND ACPC HYD 3A BREAKER POPPED + NOT RESETTING. AFTER DISCONNECTING ACMP B15, BREAKER REMAINS IN. CONFIRMED WIRING GOOD TO ACMP 3A. REMOVED + REPLACED ACMP 3A IAW CRJ900 AMM 29-12-03. OPS CHK & LEAK CHK OF #3 ACMP 3A + 3B GOOD IAW CRJ900 AMM 29-10-00. VERIFIED 3B PUMP FUNCTIONS IN AUTO MODE WITH 3A OFF + ONE AC-GEN ON-LINE WITH FLAPS OUT OF 0 DEGREES. A/C OK FOR SVC.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,991 hrs · 18,701 cycles
FA ADVISED OVERHEAD EMER LIGHTS INOP. R & R 3 CABIN CEILING EMERGENCY LIGHT IAW AMM 33-51-09. OPS TEST GOOD.
Part: CANISTER — CRACKED · airframe 27,640 hrs · 18,425 cycles
CRACK IN CANISTER, WELDED NO.3 IN STA WS148 AT LH MAIN FUEL TANK. CANISTER, NO.3 IN STA WS148 AT LH MAIN FUEL TANK.WAS REPAIRED PER REO 670-57-42-577 REV --
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,640 hrs · 18,425 cycles
INITIAL INSPECTION: CORROSION ON INTERCOSTAL BTW FS 349 AND FS 364 BTW STRNG 27-26R AT MAIN AVIONICS COMPARTMENT. (E/E). TCI: 100-09 COMPLETE: SUMMARYOF NRC 00141 CORROSION LEVEL 2 : INTERCOSTAL BTW FS 349 AND FS 364 BTW STRNG 27-26R AT MAIN AVIONICS COMPARTMENT. (E/E). WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR. 6
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 27,640 hrs · 18,425 cycles
INITIAL INSPECTION: CORROSION ON INTERCOSTAL BTW FS 349 AND FS 364 BTW STRNG 27-26L AT MAIN AVIONICS COMPARTMENT. (E/E). TCI: 100-09 COMPLETE: SUMMARY: CORROSION LEVEL-2, NEW INTERCOSTAL BTW FS 349 AND FS 364 BTW STRNG 27-26L AT MAIN AVIONICS COMPARTMENT. (E/E). WAS INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR.6.
Part: FRAME — CORRODED (BS 349) · airframe 27,640 hrs · 18,425 cycles
INITIAL INSPECTION: CORROSION ON FRAME FS 349 BTW STRNG 25L-25R AT MAIN AVIONICS COMPARTMENT. (E/E). TCI: 100-09. SUMMARY OF NRC 00140 CORROSION LEVEL 2:FRAME FS 349 BTW STRNG 25L-25R AT MAIN AVIONICS COMPARTMENT. (E/E) .WAS REPLACE PER CRJ 900, SRM 51-42-06,PAR6.C AND SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED (BS 285-349) · airframe 27,640 hrs · 18,425 cycles
INITIAL INSPECTION: CORROSION ON STRINGER 25RH BTW FS 285 AND FS 349 AT MAIN AVIONICS COMPARTMENT. (E/E). TCI: 100-09. SUMMARY OF NRC 00143 CORROSION LEVEL 2: STRINGER 25RH FS=285 TO FS=333, STRINGER 25RH BTW FS= 333 TO FS=364 AND SPLICE ON FS=328 TO FS=338 WERE INSTALLED PER CRJ-900 SRM 51-42-06-001-001-A01,51-42-21-001-001-A01
Part: DOOR FRAME — CORRODED (BS 310-349) · airframe 27,640 hrs · 18,425 cycles
HIDDEN DISCREPANCY: DURING REMOTION SUPPORT, CORROSION ON PASSENGER DOOR LOWER SURROUND STRUCTURE WAS FOUND BTW FS=310.00 / FS=349.00 AND LBL 42 IN REF NRC 00188 (CPAX) (SM). COMPLETE: SUMMARY OF NRC 00237: DUE CORROSION LEVEL 2 ON PASSENGER DOOR LOWER SURROUND STRUCTURE (KICKPLATE) BTW FS=310.00 / FS=349.00 AND LBL 42 WAS REPLACED PER CRJ/900 SRM 51-42-06-001-001-A01 PAR. 6
Part: INTERCOSTAL — CORRODED (BS 310-349) · airframe 27,640 hrs · 18,425 cycles
AWR HIDDEN DISCREPANCY: CORROSION ON INTERCOSTAL BTW FS=310.00 / FS=349.00 AND STGR 21 LH AT MAIN AVIONICS COMPARTMENT. (E/E) (SM). COMPLETE: SUMMARY OF NRC 00193 CORROSION LEVEL 2:2 INTERCOSTALS ON FS=310.00 TO FS=333.00 AND FS=333.00 TO FS=349.00 AND STGR 21 LH AT MAIN AVIONICS COMPARTMENT. E/E WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: INTERCOSTAL — CORRODED (BS 319.7-349) · airframe 27,640 hrs · 18,425 cycles
CORROSION ON INTERCOSTAL BTW FS=319.70 / FS=349.00 AND STGR 20 RH AT MAIN AVIONICS COMPARTMENT. (E/E) (SM). NEW INTERCOSTAL WAS DRILLED PER RM 51-40-11-001-001-A01. NEW INTERCOSTAL , SUPPORT ON LONG 20 RH FS= 319 TO FS= 349 , ANGLE ON FS=333 LONG 20, FRAME CLIP, FITTING WERE INSTALLED PER CRJ-900 SRM 51-42-21-001-001-A01 PAR. 6
Part: FLOORBEAM — CRACKED (BS 280) · airframe 27,640 hrs · 18,425 cycles
INITIAL INSPECTION: CRACKED BEAM AT RBL 9 AND FS 280. AT COCKPIT FLOOR STRUCTURE. COMPLETE: SUMMARY OF NRC 00125 :NEW BEAM AND REPAIR PARTS WERE INSTALLED PER CRJ-900 SRM 51-42-21-001-001-A01 PAR. 6 , SRM 51-42-06-001-001-A01 PAR 6 AND REO NUMBER A01 PAR 6 AND REO
Part: SUPPORT — CORRODED (BS 280-295) · airframe 27,640 hrs · 18,425 cycles
AWR INITIAL INSPECTION: CORROSION ON SUPPORT OF NUT AT FLOOR STRUCTURE BTW FS=280.00 / FS=295.00 AND RBL 17 (CPAX) (SM). COMPLETE: SUMMARY OF NRC : 00185 DUE CORROSION LEVEL 2 ON SUPPORT OF NUT AT FLOOR STRUCTURE BTW FS=280.00 / FS=295.00 AND LBL 17 WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 280-295) · airframe 27,640 hrs · 18,425 cycles
AWR INITIAL INSPECTION: CORROSION ON SUPPORT OF NUT AT FLOOR STRUCTURE BTW FS=280.00 / FS=295.00 AND LBL 21 (CPAX) (SM). COMPLETE: SUMMARY OF NRC : 00186 DUE CORROSION LEVEL 2 ON SUPPORT OF NUT AT FLOOR STRUCTURE BTW FS=280.00 / FS=295.00 AND LBL 21 WAS REPLACED PER CRJ-900 SRM 51-42-20-001-001-A01.
2018
Part: ACTUATOR — FAILED (RT WING TE FLAPS) · airframe 26,531 hrs · 17,602 cycles
FLAPS FAILED AT 8. AN EMERGENCY WAS DECLARED. REMOVED AND REPLACED THE RT MID FLAP ACTUATOR IAW AMM 27-52-09. OPS CHECKED GOOD.
Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 25,233 hrs · 16,628 cycles
ABOUT 80 MILES OUT, SMOKE AFT LAV WARNING RECEIVED. RAN ORH. AFTER ABOUT 5 MINUTES, RECEIVED A SMOKE FWD LAV WARNING. NO SMOKE DETECTED. PERFORMED AN OPS CHECK OF THE SMOKE DETECTION SYSTEM IAW AMM 26-16-00, OPS CHECKED GOOD.
2017
Part: PSEU — FAULT MESSAGE (ZONE 100) · airframe 22,914 hrs · 14,937 cycles
ON APPROACH RECEIVED GEAR DOWN DISAGREE WARNING MESSAGE. FOLLOWED QRH PULLED MANUAL RELEASE HANDLE, RECEIVED 3 GREEN DOWN & LOCKED INDICATION. LANDING NORMAL, NOSE WHEEL STEERING IN-OP. REMOVED AND REPLACED PSEU IAW AMM 32-61-01, OPS CHECKED GOOD.
2016
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 20,683 hrs · 13,337 cycles
CTR CARGO DOOR SEAL RETAINER DAMAGED. DRESSED BACK DENT IN CTR CARGO DOOR SEAL RETAINER IAW REO 690-52-35-013. REPAIR IS CLASSIFIED AS PERMANENT AND MAJOR IAW GMM 5-3.
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 20,683 hrs · 13,337 cycles
FWD CARGO DOOR SEAL RETAINER DAMAGED. DRESSED BACK DENT IN FWD CARGO DOOR SEAL RETAINER IAW REO 690-52-35-013. REPAIR IS CLASSIFIED PERMANENT AND MAJOR IAW GMM 5-3.
2015
Part: FLOOR SUPPORT — CORRODED (BS 985-1000) · airframe 19,970 hrs · 12,855 cycles
CORROSION ON LT FLOOR SILL IN AFT CARGO COMPARTMENT BETWEEN FS 985.00 AND FS 1000.00 IN SEVERAL LOCATIONS, MARKED 10/12/15. COMPLIED WITH EC/TC REO 670-53-00-390 AND REO 670-53-00-390, REV--DATED 1/22/2014 AS WRITTEN.
Part: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 19,970 hrs · 12,855 cycles
CORROSION ON LT FLOOR SUPPORT IN BAGGAGE BAY BETWEEN FS 1000.00 AND FS 1047.00 IN SEVERAL LOCATIONS. BLENDED CORROSION ON LT FLOOR SUPPORT AT FS 1000-1047 FOUND TO BE OUT OF LIMITS IAW REO 670-53-61-913, MEASURED MECHANICALLY WITH DEPTH GAUGE MCN-1235. REMOVED LT FLOOR SUPPORT AT FS 1000.00-FS 1047.00 IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. DRILLED FASTENER HOLES AND INSTALLED FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-15-001-001-A01 IAW DWG MM670-35655.
Part: SEAT TRACK — CORRODED (BS 913-969) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 913.00-FS 969 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 913-969 BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-51-49. R & R LT SIDE SEAT RAIL FS 913.00-969 IAW AMM 53-00-49-400-801-A01 CONFIG A07, AND 53-00-49-000-801, CONFIG A01. COMPLIED WITH EC/TC REO 670-53-00-343 & GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 847-865) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL, FS 847.00+16-FS 865.00 IS CORRODED IN MULTIPLE AREAS. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM SUP 53-31-49. R & R SEAT RAIL AT FS 847-465 RT SIDE IAW AMM 53-00-49-000-801, CONFIG A07 AND 53-00-49-400-801, CONFIG A07. FABRICATED NEW SEAT RAIL IAW ECTC REO 670-53-00-343. COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV "L" AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 661-683) · airframe 19,970 hrs · 12,855 cycles
RBL9, SEAT RAIL SEGMENT 661+16-683 CORRODED SEVERAL AREAS. CORROSION OF RBL 9 SEAT RAIL AT 661+16-683 IS BEYOND ALLOWABLE LIMITS OF SRM SUP: 53-41-49. R & R SET RAIL AT 661.00+16-683.00 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 19,970 hrs · 12,855 cycles
RBL 9, SEAT TRACK SEGMENT BS 847.62 - 977 CORRODED SEVERAL AREAS. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801 A07. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343. INSTALLED THE NEW SEAT TRACK IAW AMM 53-00-49-400-801 A07.
Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 379-485 IS CORRODED IN MULTIPLE AREAS. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM SUPPLEMENT. R & R SEAT RAIL IAW AMM 53-00-49-000-801-A07 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 847-977) · airframe 19,970 hrs · 12,855 cycles
LBL9 SEAT RAIL SEGMENT 847.62-977 CORRODED SEVERAL AREAS. REMOVED CORROSION FROM SEAT RAIL AT LBL9, FS 847.62-977 IAW SRM 51-21-06-001-001 A01, FOUND TO BE OUT OF LIMITS IAW SUPPLEMENT 53-41-49 & REO 670-53-00-013. REMOVED SEAT RAIL AT FS 847.62-977 AT LBL 9 IAW AMM 53-00-49-000-801 A01. COMPLIED WITH EC/TC REO & GREO 670-53-00-343, REV L. AS WRITTEN. INSTALLED NEW SEAT RAIL AT LBL 9, DS 847.62-977 IAW AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 677-FS 720.85 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 677-720.85IS BEYOND ALLOWABLE LIMITS IAW SRM SUPPLEMENT 53-41-49. R & R LT SIDE SEAT RAIL FS 677-FS720.85 IAW AMM 53-00-49-000-801-A07/ 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-373 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL FS 581-FS 661.00+16 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 581-661 IS BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-41-49. R & R SEAT RAIL AT FS 581.00-661.00+16 IAW AMM 53-00-49-000-801-A07/ 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-373 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 836-847) · airframe 19,970 hrs · 12,855 cycles
RBL9 SEAT RAIL SEGMENT 836.40-847.62 CORRODED SEVERAL AREAS. CORROSION OF RBL9, SEAT RAIL AT 836-847.62 IS BEYOND ALLOWABLE LIMITS OF SRM SUP: 53-41-49. REMOVED RBL9 SEAT RAIL FS 836.40-847.62 IAW AMM 53-00-49-000-801 A07 FABRICATED NEW SEAT RAIL AT RBL FS 836.40-847.62 IAW 670-53-00-343. INSTALLED NEW FABRICATED SEAT RAIL, RBL, FS 836.40-847.62 IAW AMM 53-00-49-400-801 A07. COMPLIED WITH ECTC REO 570-53-00-343 AND GREO 570-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 744.15-FS 761.85 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 744-761 IS BEYOND ALLOWABLE LIMITS IAW SRM SUP: 53-41-49. R & R SEAT RAIL AT FS 744.15-761.85 IAW AMM 53-00-49-000-801-A07/ 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-373 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 19,970 hrs · 12,855 cycles
RBL 9 SEAT RAIL SEGMENT 683-836.40 CORRODED SEVERAL AREAS. CORROSION OF RBL9 SEAT RAIL AT 683-836.40 IS BEYOND ALLOWABLE LIMITS OF SRM SUPPLEMENT 53-41-49. REMOVED RBL 9 SEAT RAIL FS 683-836.40 IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT RAIL AT RBL 9 F/S 683-FS 836340 REF: AMM 53-00-49-400-801-A07. FABRICATED NEW SEAT RAIL AT RBL9, FS 683-FS 836.40 IAW REO 670-53-00-343, REV L AND EC/TC REO 670-53-00-343, REV J. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN. RECEIVED ECTC REO 670-53-00-343, REV M COMPLIED WITH ECTC REO 670-53-00-343 & GREO 670-53-00-343, REV M AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL FS 677-FS 720.85 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 677-720.85 IS CORRODED BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-41-49. REMOVED RT SIDE SEAT RAIL AT FS 677-720 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED RT SIDE SEAT RAIL FS 677-720 IAW 53-00-49-400-801, CONFIG A07 AMM. FABRCIATED NEW SEAT RAIL IAW ECTC REP 670-53-00-3430 COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV "L" AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 19,970 hrs · 12,855 cycles
RBL9 SEAT RAIL SEQMENT FS 349-485 CORRODED SEVERAL AREAS. EVALUATED CORROSION SEAT RAIL CORRODED BEYOND REPAIR IAW SRM 53-21-49-101-001 A01 ALLOWABLE DAMAGE EXCEEDED IAW SUP: 53-21-49. REMOVED RBL9 SEAT RAIL, FS 349-485 IAW AMM 53-00-49-000-801. FABRICATED NEW SEAT RAIL RBL9, FS 349 485 IAW REO 670-53-00-343. INSTALLED NEW FABRICATED SEAT RAIL RBL9 FS 349-485 IAW AMM 53-00-49-400-801 A07. COMPLIED WITH EC/TC REO 570-53-00-313 AND GREO 570-53-00-313, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 785.15- 847.00+16 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 785-847 IS BEYOND ALLOWABLE LIMITS IAW SRM SUPPLEMENT 53-41-49. REMOVED LT SIDE RAIL AT FS 785-847 IAW AMM 53-00-49-000-801, CONFIG A07. INSTALLED NEW SEAT RAIL AT FS 785.15- FS 847.00+16 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 485-FS 581 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 485-581 IS BEYOND ALLOWABLE LIMITS OF SRM SUPPLEMENT 53-31-49. R & R SIDE SEAT RAIL AT FS 485-FS581 IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07. COMPLIED WITH ECTC REO 670-53-343 AND GREO 670-53-00-343, REV L AS WRITTEN. RECEIVED REO 670-53-00-343, REV M COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343, REV M AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 469-581) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL FS 469-FS 581 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 469-581 BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-31-49. R & R SEAT RAIL IAW AMM 53-00-49-000-801 A01, 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,970 hrs · 12,855 cycles
RBL 9 SEAT RAIL SEGMENT FS 581-661+16 CORRODED SEVERAL AREAS. CORROSION OF RBL 9 SEAT RAIL AT 581-661+16 IS BEYOND ALLOWABLE LIMITS OF SRM SUP 53-31-49. R & R SEAT RAIL AT RBL9 FS 581-00-661.00+16 IAW AMM 53-00-49-000-801 AND 53-00-49-400-801. COMPLIED WITH EC/TC REO 670-523-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL FS 744.15-FS 761.85 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 744-761 IS BEYOND ALLOWABLE LIMITS IAW SRM SUPPLEMENTS. REMOVED DISCREPANT SEAT RAIL IAW AMM 53-00-49-000-801-A7. INSTALLED NEW SEAT RAIL AT FS 744.15-FS 761.85 IAW AMM 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REF L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 661-683) · airframe 19,970 hrs · 12,855 cycles
LBL9 SEAT RAIL SEGMENT 661+16 -683 CORRODED SEVERAL AREAS. CORROSION OF LBL9 SEAT RAIL AT 661+16-683 IS BEYOND ALLOWABLE LIMITS OF SRM SUPPLEMENT 53-41-49. R & R SEAT RAIL AT FS 661.00+16-683.00 IAW AMM 53-00-49-400-801 AND 53-00-49-040-801. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 581-661 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 661-677 IS BEYOND ALLOWABLE LIMITS IAW SRM SUPPLEMENT XJET 53-41-49. REMOVED SEAT RAIL ON LT SIDE AT FS 661-FS 677 IAW AMM 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED NEW SEAT RAIL AT LT SIDE RAIL FS 661-FS 677 IAW AMM 53-00-49-400-801-A01.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL FS 581-661 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 581-661 IS BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-31-49. R & R SIDE SEAT RAIL AT FS 581-FS 661 IAW AMM 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO670-53-00-343 REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 836-847) · airframe 19,970 hrs · 12,855 cycles
LBL9 SEAT TRACK SEGMENT BS 836.40 - 847.62 CORRODED AT SEVERAL AREAS. CORROSION BEYOND ALLOWABLE LIMITS OF SRM SUPPLEMENT 53-41-49. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 379-469) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL, FS 379-FS 469 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 379-469 BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-21-49. R & R SEAT RAIL IAW AMM 53-00-49-400-801-A01 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 & GREO 670-53-00-343, REV L AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 847-913) · airframe 19,970 hrs · 12,855 cycles
LT SIDE SEAT RAIL BS 847+16- 913 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 847-913 IS BEYOND ALLOWABLE LIMITS IAW SRM SUP: 53-41-49. REMOVED LT SIDE RAIL AT FS 847.00+16-913 IAW AMM 53-00-49-000-801-A07. COMPLIED WITH EC/TC REO 670-53-00-373 AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED NEW SERIVCABLE LT SEAT RAIL AT FS 847.00+16-FS913, AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 683-836) · airframe 19,970 hrs · 12,855 cycles
LBL 9 SEAT RAIL SEGMENT 683-836,40 CORRODED SEVERAL AREAS. REMOVED CORROSION FROM SEAT RAIL AT LBL9, FS 683-836.40 IAW SRM 51-21-06-001-001 A01 FOUND TO BE OUT OF LIMITS IAW SRM SUP: 53-41-49 & REO 670-53-00-013. REMOVED SEAT TRACK FROM ACFT AT LBL9, FROM FS 683-836.10 IAW AMM 53-00-49-000-801. COMPLIED WITH EC/TC REO & GREO 670-53-00-343, REV L. INSTALLED SEAT RAIL AT LBL 9 AT FS 683-FS 836.40 IAW AMM 53-00-49-000-801.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL, FS 785.15-FS 847.00+16 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 785-847+16 IS CORRODED BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-41-49. REMOVED RT SIDE RAIL AT FS 785.15-FS847+16 IAW AMM 53-00-49-000-801 CONFIG A07. COMPLIED WITH ECTC REO AND GREO 670-53-00-343, REV L AS WRITTEN. INSTALLED NEW SEAT RAIL AT RT SIDE RAIL FROM FS 785.15-847.00+16 IAW AMM 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 19,970 hrs · 12,855 cycles
RT SIDE SEAT RAIL FS 661.00+16 -FS 661.00+90 IS CORRODED IN MULTIPLE AREAS. CORROSION ON SEAT RAIL AT 661+16-661+90 IS BEYOND ALLOWABLE LIMITS IAW SRM SUP 53-41-49. R & R SEAT RAIL AT FS 661.00+14-672.00 IAW AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L AS WRITTEN.
Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 19,970 hrs · 12,855 cycles
LEFT FLOOR SUPPORT BS 364 AND 349 IS CORRODED. COMPLIED WITH EC/TC REO 670-53-00-390 AND EO 670-53-00-390, REV.
Part: FLOOR SUPPORT — CORRODED (BS 349-364) · airframe 19,970 hrs · 12,855 cycles
RT FLOOR SUPPORT BETWEEN FS 349 AND FS 364 IS CORRODED. REMOVED CORROSION FROM RT FLOOR SUPPORT STRUCTURE BETWEEN FS 349 AND FS 353, RBL 40-RBL 43 IAW SRM 51-21-06-001-001-A01. BLEND DIMENSIONS ARE 2.5" WIDE BY 4" LONG. RECEIVED & COMPLIED WITH REO 670-53-21-783 & EC/TC REO 690-53-21-783 AS REQUIRED.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 19,970 hrs · 12,855 cycles
RIGHT SIDE FLOOR SILL AT FRAME 280 IS CORRODED. R & R FLOOR SILL DUE TO SEVERE CORROSION. REMOVED AND BEGAN INSTALLATION RT FLOOR SILL BETWEEN FS 280 AND FS 319 IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. RT FLOOR SILL BETWEEN FS 280 AND FS 319 FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-390. INSTALLED RIVETS COMMON TO FLOOR SILL AND SKIN IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 19,970 hrs · 12,855 cycles
RIGHT SIDE FLOOR SUPPORT BETWEEN FRAME 310 AND FRAME 319.7 IS CORRODED. R & R RT FLOOR SUPPORT BETWEEN FS 288 AND 319 IAW SRM 51-12-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01.
Part: ACCESS PANEL — CHAFED (RT AILERON) · airframe 19,970 hrs · 12,855 cycles
RT AILERON LOWER L/E ACCESS PANEL 699BB HAS CHAFE MARKS. REMOVED DAMAGE ON ACCESS PANEL 699BB IAW SRM 51-12-00-001-001-A01. RECEIVED AND COMPLIED WITH EA 26-2015-152. RECEIVED AND COMPLIED WITH ECTC EA26-2015-152. COMPLIED WITH PERMANENT OF EA26-2015-152.
Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 19,970 hrs · 12,855 cycles
FWD EQUIPMENT COMPARTMENT FLOOR IS CRACKED ON RT SIDE AT FRAME CUTOUT AT FS 193.00. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509, REV B, DATED 1-28-14 FOR RT SIDE.
Part: WIRE — BROKEN (PANEL) · airframe 19,970 hrs · 12,855 cycles
RIGHT AFT LIGHT ON PANEL 172CR HAS A BROKEN WIRE. INSTALLED SERVICEABLE CONTACT ON WIRE THAT WAS BROKEN OFF FROM CONTACT IAW ESPM 20-12-00 AND 20-26-00. REMOVED CONTACT/WIRE FROM POSITIVE CONNECTOR OF LIGHT, EM EXTERIOR. INSTALLED SERVICEABLE LIGHT EM EXTERIOR BY INSERTING CONTACTS IN CONNECTOR IAW ESPM 20-26-00. PERFORMED OPS TEST OF EMERGENCY LIGHT ON PANEL 172CR . OPS TEST GOOD. UPON PERFORMING OPS TEST OF EMERGENCY LIGHTS FOUND RT AFT OVER FLAP EMERGENCY LIGHT INOPERATIVE. LIGHT OVER RT FLAP. FOUND RT AFT OVER FLAP EMERGENCY LIGHT BULB TO BE INOPERATIVE. REPLACE BULB BY REMOVING LIGHT LENS, TURNING BULB CCW AND PULLING BULB FROM SOCKET THEN INSERTING SERVICEABLE BULB INTO SOCKET THEN TURNING BULB CW UNTIL LOCKED IN SOCKET THEN REINSTALLING LENS, OPS TEST GOOD.
Part: FLOOR PANEL — CRACKED (E/E BAY) · airframe 19,970 hrs · 12,855 cycles
FWD EQUIPMENT COMPARTMENT FLOOR IS CRACKED ON LT SIDE AT FRAME CUTOUT AT FS193.00. COMPLIED WITH EC/TC REO 670-53-11-509 AND GREO 670-53-11-509 REV B, DATED 01/28/2014 FOR LT SIDE.
Part: LIGHT — DETERIORATED (CABIN) · airframe 19,970 hrs · 12,855 cycles
SEVERAL PIECES OF EMERGENCY LIGHT TRACK WORN, STRAINED. REQUIRES REPLACEMENT CUT AS REQUIRED, RECEIVED SERIVCABLE LIGHT TRACKS AND CUT AS REQURIED IAW CMM 33-51-01.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,379 hrs · 11,696 cycles
NR 1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R THE EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
Part: DOOR — OUT OF RIG (MAIN PAX) · airframe 18,281 hrs · 11,634 cycles
MAIN CABIN DOOR WILL NOT OPEN, DOOR ACTUATOR HOLDING DOOR UP. REPOSITIONED DOOR CABLE ON PULLEY & OPS CHECKED SEVERAL TIMES. OPS CHECKED GOOD. IAW AMM 52-11-00. ACFT OK FOR SERVICE.
2014
Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,365 hrs · 11,044 cycles
RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R RT AFT OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-51-15. OPS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 17,195 hrs · 10,923 cycles
F/O FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT. OPS CHECKED GOOD.
Part: SKIN — BURNED (BS 645-661) · airframe 16,638 hrs · 10,548 cycles
TWO BURNS ON FASTENERS BETWEEN FS 645-661 AND S20R. REPAIRED IAW REO 670-53-00-045.
Part: SKIN — BURNED (BS 677-693) · airframe 16,638 hrs · 10,548 cycles
TWO BURNS ON FASTENERS AND ONE BURN ON FUSELAGE SKIN BETWEEN FS 677-693 ABOVE STR 20. REPAIRED IAW REO 670-53-00-045.
Part: SKIN — BURNED (FUSELAGE) · airframe 16,638 hrs · 10,548 cycles
ONE BURN ON FASTENER AT FS 20275 AND STGR 23R. REPAIRED IAW REO 670-53-00-045.
Part: SKIN — BURNED (BS 235-250) · airframe 16,638 hrs · 10,548 cycles
TWO BURNS ON FASTENERS BETWEEN F 235-250 AND S23R. REPAIRED IAW REO 670-53-00-045.
Part: SKIN — BURNED (BS 645) · airframe 16,638 hrs · 10,548 cycles
ONE BURN ON FASTENER AT FS 645 ABOVE S20R. REPAIRED IAW REO 670-53-00-045.
Part: SKIN — BURNED (BS 265) · airframe 16,638 hrs · 10,548 cycles
TWO BURNS ON FASTENERS AT FS 265 AND S22R. REPAIRED IAW REO 670-53-00-045.
Part: HANDLE — FROZEN (PAX DOOR) · airframe 15,808 hrs · 10,023 cycles
PAX DOOR HANDLE FROZEN. HEATED CABIN WITH THE APU AND REMOVED DEBRIS FROM DOOR JAM OPS CHECKED OK IAW AMM 52-11-00. ACFT OK FOR SERVICE.
Part: HANDLE — FROZEN (PAX DOOR) · airframe 15,729 hrs · 9,976 cycles
MAIN PAX DOOR HANDLE WILL NOT OPERATE TO LOCK, UNLOCK DOOR. RAN ACFT HEATING SYSTEM WITH PAX DOOR HELD IN CLOSED POSITION, PAX DOOR OPERATES NORMALLY IAW AMM 52-11-00. AIRCRAFT RETURNED TO SERVICE.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 15,627 hrs · 9,912 cycles
F/A REPORTED MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14. CHECKED GOOD.
2013
Part: GROUND WIRE — BROKEN (EMERGENCY LIGHT) · airframe 15,260 hrs · 9,694 cycles
LT AFT OVER WING EMERGENCY LIGHT INOP. FOUND BROKEN GROUND WIRE REPAIRED IAW ESPM 20-16-00. OPS CHECKED GOOD IAW AMM 33-51-00-710-801.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 15,260 hrs · 9,694 cycles
EMERGENCY LIGHT AT SERVICE DOOR ON GALLEY 2 AT FLOOR LEVEL HAS THREE BULBS INOPERATIVE. R & R BULBS, OPS CHECKED GOOD IAW AMM 33-51-00-710-801.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 15,260 hrs · 9,694 cycles
FLOORBEAM DAMAGED. REPAIRED CENTER COCKPIT FLOORBEAMS AT BL 12.00. FABRICATED IMBD UPPER ANGLE IAW REO 690-53-11-603 STEP G. LOCATED AND DRILLED -ANGLE IAW REO 690-53-11-603. COMPLETED ECTC REO 690-53-11-603 AND REO 690-53-11-603. MAJOR REPAIR.
Part: SKIN — DENTED (BS 196-202.75) · airframe 15,260 hrs · 9,694 cycles
DENT FOUND IN FUSELAGE SKIN BETWEEN BS 193-202.75 AND BETWEEN S12-13L. COUNTERSUNK DEBURRED TREATED AND PRIMED NWE SKIN PANEL IAW SRM 51-21-11-001-001-A01, 51-40-11-001-001-A01. INSTALLED NEW SKIN PANEL AND APPLIED FILLET SEALANT IAW SRM 51-42-06-001-001-A01 & 51-23-00-001-001-A01.
Part: HINGE — GOUGED (PAX DOOR) · airframe 15,260 hrs · 9,694 cycles
PAX DOOR HINGE GOUGED ON MULTIPLE HALF LUGS. REPAIRED IAW REO 670-52-11-511 REV DATED 6-29-10, REO 670-53-21-582 REV B.
Part: FLOOR SUPPORT — CORRODED (BS 280-295) · airframe 15,260 hrs · 9,694 cycles
FOUND LOGITUDINAL BEAM AT LBL 9 CORRODED ON UPPER FLANGE BETWEEN FS 280 AND 295. REMOVED CORROSION FROM UPPER SURFACE OF LONGITUDINAL BEAM AT LBL 9 FLANGE BETWEEN FS280 -FS 295 IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 15,260 hrs · 9,694 cycles
TWO DENTS ON LT INBD FLAP TOP SURFACE LOCATED BETWEEN FLS 30.00 AND 42.00 FWD T/E AND 6" FWD T/E. COMPLIED WITH NON FLASH REPAIR TO INBD FLAP IAW EO 900-57-0012 AND SRM 57-52-01-201-001-A01.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 15,260 hrs · 9,694 cycles
DENT IN HORIZONTAL STAB RT SIDE JUST BELOW CENTER LINE AND INBD OF RIB 3 DIMENSIONS ARE 1.9" LONG BY 1.2" WIDE AND HAS MAX DEPTH OF .053. REPAIRED IAW REO 690-55-12-872, REO 690-55-12-572, ECTC REO 690-55-12-072 AND REO 690-55-12-072. MAJOR REPAIR.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,260 hrs · 9,694 cycles
SERVICE DOOR ANGLE MOUNT CORRODED UNDER DOOR STOP. REMOVED SERVICE DOOR ANGLE MOUNT IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW ANGLE MOUNT. INSTALLED NEW ANGLE MOUNT IAW SRM 51-42-06-001-001-A01, 51-42-34-001-001-A01 AND DWG SH670-31996.
Part: SKIN — CORRODED (BS 295-310) · airframe 15,240 hrs · 9,682 cycles
SKIN ON OUTER SURFACE UNDER TCAS ANTENNA BS 295 & 310 CORRODED AT STRINGER 27. REPAIRED IAW REO 690-53-21-567.
Part: FRAME — CORRODED (BS 295) · airframe 15,260 hrs · 9,694 cycles
FRAME BS 295 HAS CORROSION BETWEEN S24-25R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.
Part: ATTACH ANGLE — CORRODED (BSA 349) · airframe 15,240 hrs · 9,682 cycles
FOUND ATTACH ANGLE CORRODED AT FS 349 RT SIDE. REMOVED CORRODED ATTACH ANGLE IAW REO 690-53-21-568. LOCATED DRILLED AND DEBURRED HOLES IN ANGLE IAW SRM 51-40-11-001-001-A01. INSTALLED ATTACH ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND REO 690-53-21-568. CLASSIFIED AS A MAJOR REPAIR.
Part: ATTACH ANGLE — CORRODED (COCKPIT DOOR) · airframe 15,260 hrs · 9,694 cycles
LEFT COCKPIT DOOR POST LOWER END ATTACH ANGLE CORRODED BEYOND LIMITS FS 280, LBL 11.00 REPLACED CORRODED ANGLE. REPAIRED IAW SRM 51-12-00-001-001 AND SRM 53-00-00-101-001.
Part: SILL — CORRODED (SERVICE DOOR) · airframe 15,240 hrs · 9,682 cycles
SERVICE DOOR LOWER SILL CORRODED AT FS 349. REMOVED SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SILL. INSTALLED NEW SILL IAW SRM 51-42-06-001-001-A01 AND DWG NR SH670-31950.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 15,240 hrs · 9,682 cycles
SIDE SEAT RAIL HAS CORROSION FS 785.15 TO 847 + 16 LT SIDE OF CABIN. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A07. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A07.
Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 15,240 hrs · 9,682 cycles
RT FLOOR SUPPORT CORRODED AT FS 349. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 15,240 hrs · 9,682 cycles
LBL 9 SEAT TRACK CORRODED AT FS 661+16. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
Part: SKIN — CORRODED (BS 280) · airframe 15,240 hrs · 9,682 cycles
CIRCUMFERENTIAL JOINT AT FS 280 INTERNAL SKIN CORRODED BETWEEN S25 LT AND 25 RT REMOVED CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-21-06-001-001-A01. CLASSIFIED AS A MAJOR REPAIR.
Part: SEAL DEPRESSOR — CORRODED (SERVICE DOOR) · airframe 15,240 hrs · 9,682 cycles
SERVICE DOOR STRIKER SEAL CORRODED. REPAIRED IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 661) · airframe 15,240 hrs · 9,682 cycles
LBL 9 SEAT TRACK CORRODED BS 661+40 AND 661+80. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801-A07. LOCATED DRILLED COUNTERSUNK DEBURRED HOLES IN NEW SEAT TRACK IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801. A MAJOR REPAIR.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 15,260 hrs · 9,694 cycles
MID CAP ANGLE CORRODED AT PAX DOOR FLOOR SUPPORT. R & R ANGLE IAW SRM 51-42-13-001-001-A01, SRM 51-41-02-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 349) · airframe 15,240 hrs · 9,682 cycles
RBL 9 SEAT TRACK CORRODED AT FS 349. R & R SEAT TRACK BS 349-485 IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
Part: FRAME — CORRODED (BS 319.7) · airframe 15,240 hrs · 9,682 cycles
FRAME BS 319.7 CORRODED BETWEEN S26LT AND 26RT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CLASSIFIED AS A MAJOR REPAIR.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,240 hrs · 9,682 cycles
INTERCOSTAL CORRODED AT STRINGER 27L BETWEEN BS 349 AND 364. REMOVED INTERCOSTAL, FOUND CORROSION AT ATTACHED FLANGE, NO DAMAGE IS ALLOWED IAW SRM 53-21-23-101-003-A01 & 51-42-06-001-001-A01. LOCATED DRILLED, DEBURRED AND INSTALLED INTERCOSTAL IAW SRM 51-40-11-001-001-A01 AND DWG SH 670-32075. MAJOR REPAIR.
Part: FRAME — CORRODED (BS 349) · airframe 15,260 hrs · 9,694 cycles
FRAME BS 349, CORRODED BETWEEN S26LT & 26 RT. REMOVED CORROSION FROM FRAME IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.
Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 15,240 hrs · 9,682 cycles
INTERCOSTAL CORRODED AT S27R BETWEEN BS 349 AND 364. REMOVED INTERCOSTAL AND FOUND CORROSION AT ATTACHED FLANGE. NO DAMAGE IS ALLOWED IAW SEM 53-21-23-101-003-A01 & 51-42-06-001-01-A01. NEW INTERCOSTAL LOCATED DRILLED AND DERURRED IAW SH670-32075. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01. CLASSIFIED AS MAJOR REPAIR.
Part: FLOOR SUPPORT — CRACKED (BS 278) · airframe 15,260 hrs · 9,694 cycles
RIGHT COCKPIT FLOOR SUPPORT ANGLE CRACKED AT APPROX FS 278. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SERVICEABLE ANGLE ASSY IAW SRM 51-42-06-001-001-A01 AND DWG CC670-33199 AND DWG CC670-33052. MAJOR REPAIR.
Part: FLOORBEAM — CRACKED (BS 274) · airframe 15,251 hrs · 9,688 cycles
LBL 12, FLOORBEAM CRACKED AT APPROX FS 274 . REPAIRED WITH REO 690-53-11-603.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,257 hrs · 9,692 cycles
RBL 12 FLOORBEAM CRACKED AT APPROX FS 274, FWD TOP CORNER OF BACKUP FITTING. COMPLIED WITH REO 690-53-11-603.
Part: FLOOR SUPPORT — CRACKED (BS 278) · airframe 15,260 hrs · 9,694 cycles
LEFT COCKPIT FLOOR SUPPORT ANGLE CRACKED AT APPROX FS 278. REMOVED FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW SUPPORT ANGLE IW SRM 51-42-06-001-001-A01 AND DWG CC670-33199-3CC670-33-199 AND DWG CC670-3-3052. MAJOR REPAIR.
Part: FRAME — CORRODED (BS 295) · airframe 15,240 hrs · 9,682 cycles
FRAME BS 295 CORRODED BETWEEN S26 & 27L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CLASSIFIED AS A MAJOR REPAIR.
Part: FRAME — CORRODED (BS 310) · airframe 15,240 hrs · 9,682 cycles
FRAME BS 310 CORRODED BETWEEN S26LT AND 26RT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. CLASSIFIED AS A MAJOR REPAIR.
Part: STRINGER SPLICE — CORRODED (BS 333-349) · airframe 15,240 hrs · 9,682 cycles
STRINGER SPLICE 25R CORRODED BETWEEN BS 333 AND 349. REMOVED STRINGER SPLICE IAW SRM 51-42-06. INSTALLED NEW STRINGER SPLICE IAW SRM 51-42-06-001-001-A01 & DWG SH670-32429. CLASSIFIED AS A MAJOR REPAIR.
Part: FRAME — CORRODED (BS 333) · airframe 15,260 hrs · 9,694 cycles
FRAME BS 333 CORRODED BETWEEN S26-27R. BLENDED AND REMOVED ALL CORROISON FROM FRAME IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.
Part: SKIN — GOUGED (BS 913-927) · airframe 15,240 hrs · 9,682 cycles
GOUGE ON EXTERNAL FUSELAGE SKIN ALONG STRINGER 27 BETWEEN FS 913 & 927. REPAIRED IAW EC/TC REO 670-53-00-290. CLASSIFIED AS A MAJOR REPAIR.
Part: DOUBLER — CORRODED (BS 295-310) · airframe 15,240 hrs · 9,682 cycles
DOUBLER CORRODED AT TCAS ANTENNA CUTOUT, STRINGER 27 BETWEEN BS 295 & 310. ANTENNA DOUBLER REMOVED. DRILLED NEW DOUBLER IAW SRM 51-40-11-001-001-A01. INSTALLED DOUBLER IAW SRM 51-42-06-001-001-A01. CLASSIFIED AS A MAJOR REPAIR.
Part: SKIN — CORRODED (BS 295-310) · airframe 15,240 hrs · 9,682 cycles
SKIN ON OUTER SURFACE UNDER TCAS ANTENNA, BS 295 & 310 IS CORRODED AT STR 27. BLENDED DAMAGE IAW SRM 51-21-06-001-001. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT INSPECTION PROCEDURE, FOUND OUT OF LIMITS IAW SRM 53-21-01-101-002-A02. NO DAMAGE ALLOWED. CLASSIFIED AS A MAJOR REPAIR.
Part: POST — CORRODED (COCKPIT DOOR) · airframe 15,251 hrs · 9,688 cycles
RT COCKPIT DOOR POST CORRODED WL 72.00 BS 280, RBL 11. REPAIRED IAW SRM 51-12-00-001-001 AND SRM 53-00-00-101-001-A01 AND REO 690-53-11-600. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,251 hrs · 9,688 cycles
COCKPIT FLOORBEAM AT FS 280 CORRODED. REMOVED IAW SRM 51-40-11-001-001-A01. INSTALLED NEW IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34010.
Part: WEB — CORRODED (BS 280) · airframe 15,251 hrs · 9,688 cycles
LEFT WEB CORRODED AT FS 280, LBL 11. REPAIRED IAW SRM 51-40-11-001-A01 AND REO 670-53-11-594. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,251 hrs · 9,688 cycles
LT FLOORBEAM AT FS 280 CORRODED AT LBL 13. REMOVED FLOORBEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & 51-42-22-001-001-A01. LOCATED AND DRILLED HOLES IN NEW FLOORBEAM IAW DWG CC670-34010.
Part: POST — CORRODED (COCKPIT DOOR) · airframe 15,251 hrs · 9,688 cycles
L COCKPIT DOOR POST CORRODED AT WL 72.00 LBL 11. REPAIRED IAW SRM 51-12-00-001-001 AND SRM 53-00-00-101-001. MAJOR REPAIR.
Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 15,240 hrs · 9,682 cycles
RT CABIN FLOOR SUPPORT CORRODED AT FS 280. REMOVED RT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 & 51-42-001-001-A01. LOCATED DRILLED AND DEBURED HOLES IAW SRM 51-40-11-001-01-A01. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-21-001-001-A01,51-42-06-001-001-A01 AND DWG SH670-32170. MAJOR REPAIR
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,251 hrs · 9,688 cycles
RT FLOORBEAM BS 280 CORRODED AT RBL 13. REMOVED FLOORBEAM SECTION IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. LOCATED FASTENER HOLES IN SERVICEABLE RT BEAM SECTION IAW SRM 51-42-00-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01 AND DWG CC670-34010. MAJOR REPAIR.
Part: WEB — CORRODED (BS 280) · airframe 15,251 hrs · 9,688 cycles
RT WEB CORRODED AT FS 280 RBL 11. COMPLIED WITH ECTC REO 670-53-11-594-01 AND GREO 670-53-11-594. MAJOR REPAIR.
Part: SKIN — DENTED (BS 193-202.75) · airframe 15,260 hrs · 9,694 cycles
DENT FOUND IN FUSELAGE SKIN BETWEEN BS 193-202.75 AND S12-13L. R & R FUSELAGE SKIN BETWEEN FS193-202 BETWEEN STRGS 12-13LT IAW SRM 51-42-06. DRILLED OF FUSELAGE SKIN PANEL CC670-33105-1 IAW SRM 51-42-06-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOP 5702. TRIMMED NEW SKIN IAW SRN 51-24-36-001-001-A01 AND DRILLED ALL HOLES IAW SRM 51-40-11-001-001-A01.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 15,260 hrs · 9,694 cycles
TWO DENTS ON LT INBD FLAP TOP SURFACE LOCATED BETWEEN FLS 30.00 AND 42.00 3" FWD T/E AND 6" FWD T/E. REPAIRED IAW EC/TC EO 900-57-0012. MAJOR REPAIR.
Part: PLATE — MISSING (RT WING SLAT) · airframe 15,260 hrs · 9,694 cycles
RT WING SLAT CLOSING PLATE MISSING. REPLACED RT WING SLAT CLOSING PLATE IAW AMM 57-41-05-400-809. MAJOR REPAIR.
Part: SKIN — DENTED (BS 193-202.75) · airframe 15,260 hrs · 9,694 cycles
SKIN DENTED AT 193-202.75. DENT DAMAGED SKIN AT FS 193.00-202.75 HAS BEEN REPLACED. P
Part: MEGAPHONE — CORRODED (CABIN) · airframe 15,052 hrs · 9,559 cycles
MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, IPC 256-14V, ITEM 5.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 15,052 hrs · 9,559 cycles
MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, IPC 25-61-14, ITEM 5.
2012
Part: CONNECTOR — DAMAGED · airframe 12,493 hrs · 7,889 cycles
EXPERIENCED FUMES IN THE COCKPIT. DECLARED AN EMERGENCY, RAN QRH, RETURNED TO DEPARTURE. FOUND ELECTRICAL DAMAGE TO PL116P1 AND PL116J1, SEE WO 267716, FOR DETAILS OF REPAIR, PERFORMED OPS CK OF DC PWR IAW AMM 24-61-00-710-806, NO FAULTS FOUND AT THIS TIME. R & R PL116P1 & PL116J1 IAW ESPM 20-26-31 AND 20-33-00.
Part: CANISTER — CRACKED (LE SLAT) · airframe 11,635 hrs · 7,323 cycles
RIGHT WING SLAT TRACK CANISTER AT INBOARD SLAT, NR 3 TRACK, CRACKED AT AFT SUPPORT TAB. REMOVED AND REPLACED SLAT TRACK CANISTER IAW SRM 51-42-21 AND AMM 51-23-00.
Part: CANISTER — CRACKED (LE SLAT) · airframe 11,635 hrs · 7,323 cycles
LEFT WING SLAT TRACK CANISTER AT INBOARD SLAT, NR 3 TRACK, CRACKED AT AFT SUPPORT TAB. REMOVED AND REPLACED SLAT TRACK CANISTER IAW SRM 51-42-21 AND AMM 51-23-00.
2010
Part: SAFETY VALVE — FAILED (CABIN PRESSURE) · airframe 7,900 hrs · 4,915 cycles
AT FL380 A/C PRESSURIZATION BEGAN TO CLIMB AT 1500 TO 2000 FT PER MIN. PERFORMED QRH FOR EMERGENCY DESCENT. RECEIVED CABIN ALT WARNING MSG. EMERGENCY DECLARED, A/C LANDED SAFELY IN SDF. REMOVED AND REPLACED LEFT SAFETY VALVE.
Part: UNKNOWN — ODOR (COCKPIT) · airframe 6,495 hrs · 4,010 cycles
ON CLIMBOUT FROM CVG RECEIVED SMOKE FWD LAV WARNING MSG, ACCOMPANIED BY BURNING ODOR IN COCKPIT. RAN QRH, EMERGENCY DECLARED. A/C RETURNED TO CVG LANDED SAFELY. INSPECTED A/C CHECKING FOR BAD ELECTRICAL COMPONENTS, NO DEFECTS NOTED. SUSPECT RESIDUAL FROM COMP WASH, RAN A/C FOR EXTENDED PERIOD AND SMELL HAS DISSIPATED.
2007
Part: PSEU — FAULTY (AVIONICS BAY) · airframe 99 hrs · 66 cycles
FLIGHT 5543 - ON CLIMBOUT FROM LGA TO CVG, RECEIVED GEAR DISAGREE MESSAGE DURING GEAR RETRACTION. AIRCRAFT DIVERTED TO JFK AND LANDED SAFELY. REMOVED AND REPLACED PSEU.