N195PQ
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.
153 reports on file, 2010-11-02 – 2023-08-24.
Part: ANGLE — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR ANGLE C AT INTERCOSTAL DD7A FOUND TO BE CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW CRJ-900 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR INTERCOSTAL DD2 MID FOUND TO BE CORRODED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD2 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01AND 51-40-11-001-001-A01 PN 601R318053-3.
Part: FORMER — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR FORMER CORRODED AT FS 329.41 BETWEEN DD4 AND DD5. REMOVED CORRODED FORMER AND INSTALLED A NEW FORMER IAW CRJ900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR FWD INTERCOSTAL AT DD2 IS CORRODED. REMOVED CORRODED INTERCOSTAL AND INSTALLED A NEW INTERCOSTAL IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR INTERCOSTAL DD5 ON THE AFT SIDE FOUND TO BE CORRODED.. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR AFT SIDE INTERCOSTAL DD5 IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01 PN 601R31902-317A.
Part: FORMER — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR FORMER CORRODED AT FS 329.21 AND BETWEEN DD5 AND DD6. REMOVED CORRODED FORMER AND INSTALLED A NEW FORMER IAW CRJ 900 SRM 51-42-06-400-001-A01.
Part: FRAME — CORRODED (BS 847 S27) · airframe 33,234 hrs · 24,322 cycles
CORROSION FOUND ON FORWARD FACE OF FRAME AT F.S 847+16 AND STRG 27. REPAIRED FRAME FS847+16 IAW CRJ900 SRM REPAIR 53-00-06-201-001-A03.
Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 33,234 hrs · 24,322 cycles
AFT BAGGAGE BAY DOOR SURROUND STRUCTURE, LOWER SILL CORRODED BETWEEN FS1000 TO FS1047 INSTALLED MIDDLE INNER CHORD P/N MM670-35669-001 IAW CRJ-900 SRM 51-42-21-001-001-A01
Part: DOOR SILL — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
AFT BAGGAGE BAY DOOR SURROUND STRUCTURE, LOWER SILL CORRODED BETWEEN FS1000 TO FS1047 INSTALLED AFT CARGO DOOR SILL PN: MM670-35655-003 IAW CRJ-900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01.
Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 33,234 hrs · 24,322 cycles
AFT BAGGAGE BAY DOOR SURROUND STRUCTURE, LOWER SILL CORRODED BETWEEN FS1000 TO FS1047 INSTALLED NEW SERVICEABLE AFT INNER CHORD P/N MM670-35670-003 PER CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
STGR 18R FOUND TO BE CORRODED BETWEEN FS 295 - FS 310. LOCATED AND DRILLED NEW STRINGER #18R P/N: SH670-31631-1. IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER #18R P/N SH670-31631-1 IAW CRJ900 SRM 51-42-06-001-001-A01
Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
R/H SIDE SEAT RAIL CORRODED BETWEEN F.S. 744.15 TO F.S. 761.85. REPLACED R/H SIDE SEAT RAIL PN SH690-36285-1 IAW CRJ900 SRM 53-00-49-400-801-A07 AND BOMBARDIER MODSUM NO: IS67053000195 REV A DATED 2016/02/07
Part: FLOORBEAM — CRACKED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
RBL9 COCKPIT FLOOR BEAM FWD SIDE OF F.S 280 IS CRACKED. INSTALLED NEW SERVICEABLE RH FLOORBOARD ANGLE (P/N CC670-33199-4) IAW CRJ 900 SRM 53-11-43-201-003-A01
Part: ANGLE — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR LOWER SILL ANGLE IS CORRODED. RECEIVED, LOCATED, DRILLED AND DEBURRED NEW ANGLE KICKPLATE P/N SH670-31875-7S IN SURROUND STRUCTURE PAX DOOR, IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE KICKPLATE P/N SH670-31875-7 ON SURROUND STRUCTURE PAX DOOR, IAW CRJ900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01
Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 677 TO F.S. 720. REMOVED SEAT TRACK FROM FS.677-FS.720 IAW CRJ900 AMM 53-00-49-000-801 (A07) INSTALLED NEW SEAT TRACK FROM FS 677-FS 720 IAW CRJ 900 AMM 53-00-49-400-801(A07)
Part: ANGLE — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
GALLEY DOOR LOWER SILL ANGLE AND FITTING ANGLES ARE CORRODED. REMOVED AND REPLACES GALLEY DOOR LOWER SILL ANGLE AND FITTING ANGLES IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
L/H SIDE SEAT RAIL CHANNEL IS CORRODED BETWEEN F.S. 744 TO F.S. 761.85 FABRICATED NEW LH SIDE SEAT RAIL AT FS 744 TO FS 761'85 PN: SH690-36258-1 USING MATERIAL 670-53-00-692-1 PER MHIRJ REO 670-53-00-587 DATE 2023-02-08.
Part: ANGLE — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PAX DOOR CAP ANGLE IS CORRODED FROM FS 319.00 TO FS 333.00. RECEIVED, LOCATED, DRILLED AND DEBURRED NEW ANGLE MID CAP P/N SH670-31825-9S IN SURROUND STRUCTURE PAX DOOR, IAW CRJ900 SRM 51-40-11-001-001-A01. INSTALLED NEW ANGLE MID CAP P/N SH670-31825-9 ON SURROUND STRUCTURE PAX DOOR, IAW CRJ900 SRM 51-41-02-001-001-A01 & 51-42-06-001-001-A01
Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 379 TO F.S. 485. INSTALLED R/H SIDE SEAT RAIL BETWEEN F.S. 379 TO F.S. 485 IAW CRJ900 AMM 53-00-49-400-801 (CONFIG A07)
Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
SEAT TRACK AT FS375 LBL 9 IS CORRODED REPLACED SEAT TRACK AT F.S.375 LBL 9 P/N SH670-32249-3 IAW CRJ 900 AMM 53-00-49-400-801(A07)
Part: SEAT TRACK — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
SEAT TRACK AT FS 349 RBL 9 IS CORRODED REPLACED SEAT TRACK AT F.S. 349 RBL 9 P/N SH670-32159-1 IAW CRJ 900 AMM 53-00-49-400-801(A07)
Part: CHANNEL — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
F.S. 581 TO F.S. 597 ANTENNA DOUBLER IS CORRODED. REPAIRED DOUBLER IAW ENDEAVOR EA CRJ953-15388 REV IR DATED 07/29/2023
Part: FRAME — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
FWD AND AFT SIDE OF F.S. 533 FRAME IS CORRODED AT STGR 18L. REMOVED FS 533 FROM STGR 16L-18L IAW CRJ 900 SRM 51-42-06-001-001-A01 INSTALLED FS 533 FROM STGR 16L-18L IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: FRAME — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
FWD AND AFT SIDE OF FRAME IS CORRODED AT F.S. 549 STGR 18L. FABRICATED, LOCATED AND DRILLED FRAME SPLICE REPAIR AND REINFORCEMENT ANGLE REPAIR FROM S1710-4 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND CRJ 900 53-00-06-201-001-A03 STEP 6E(D) LOCATED AND DRILLED NEW FRAME SECTOR PN:SH690-33122-3S AND REINFORCEMENT ANGLE PN: SH690-33164-3 IAW CRJ 900 SRM 51-40-11-001-001-A01 INSTALLED FS549 AND REINFORCEMENT ANGLE FROM STGR 18L-14L IAW CRJ 900 SRM 51-42-06-001-001-A01
Part: INTERCOSTAL — CRACKED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
F.S. 333.0 CRACKED AT TOP CENTER BETWEEN STGR #0 AND STGR #1. REPAIRED FS 333 FRAME STRINGER 0-1R IAW ENDEAVOR AIR EA CRJ953-15423 REV IR DATED 8/2/23
Part: FRAME — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
"F.S. 597 FRAME IS CORRODED AT STGR 19L. REMOVED CORROSION ON FS 597 AT STGR 19L IAW CRJ 900 SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS OF FRAME FS597 REWORKED AREA IAW CRJ 900 NDTM PART 1 51-20-004-270-A01 REV 36 DATED 2/8/22. FOUND LOWEST REMAINING THICKNESS TO BE 0.063"" OR GREATER."
Part: INTERCOSTAL — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
INTERCOSTAL 27R BETWEEN FS 394 AND FS 421 IS CORRODED LOCATED AND DRILLED NEW SERVICEABLE INTERCOSTAL P/N SH670-32075-3S, LOCATED AT STR 27R BETWEEN FS394.00 AND FS409.00 PER CRJ 900 SRM 51-40-11-001-001-A01.INSTALLED NEW SERVICEABLE INTERCOSTAL P/N SH670-32075-3S PER CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
F.S. 501 TO F.S. 517 STGR 20 R IS CORRODED. UPON FURTHER INVESTIGATION NO CORROSION WAS FOUND ON STGR20R. CORROSION WAS FOUND ON STGR21R BETWEEN FS501 AND FS517. REMOVED AND REPLACED STGR 21R SEGMENT BETWEEN FS501 AND FS549 IAW CRJ 900 SRM 53-00-03-201-001-A02
Part: STRINGER CLIP — CORRODED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
AFT BAGGAGE BAY, STRINGER CLIP CORRODED AT FS1015 AND STGR23L. INSTALLED NEW CLIP ON STGR 23L @ FS 1015, P/N: MM670-36482-003 IAW CRJ 900 SRM 51-42-06-001-001-A01, RESTORED FINISH IAW CRJ 900 SRM (TR51-0068) 51-21-16-001-001-A01.
Part: FRAME — CRACKED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
PERM REPAIR FRAME DMG@ FS1162 ST 7L-8L COMPLIED WITH BOMBARDIER REO 670-53-71-047 REV -A 2015-12-22
Part: SUPPORT BEAM — CHAFED (UNKNOWN) · airframe 33,234 hrs · 24,322 cycles
AFT CARGO DOOR TRACK SUPPORT BEAM DAMAGED FROM AFT CABLE JUST BELOW PULLEY BRACKET COMPLIED WITH ENDEAVOR AIR EA CRJ953-15394 REV IR DATED 7/30/23.
Earlier reports · 2010–2022 · 122 reports
2022
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 32,117 hrs · 23,338 cycles
CENTER CABIN OVERHEAD EMERGENCY LIGHT FIXTURE ONE SIDE INOPERATIVE. R & R THE BATTERY ASSY PS36 IAW AMM 33-51-17. OPS TESTED GOOD.
2020
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 27,964 hrs · 19,729 cycles
R/H FLOOR SILL IS CORRODED AT THE F.S. 280 MARKED WITH TAPE. INSTALLED NEW SERVICEABLE RH FLOOR SILL IAW CRJ 900 SRM'S 51-42-06-001-001(A01), 51-42-13-001-001(A01 AND 51-42-21-001-001(A01). WVAC
Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
STRINGER 21R IS CORRODED BETWEEN FS 319 AND FS 349. REMOVED & REPLACED STRINGER 21R BETWEEN FS 319 AND FS 349 IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. WVAC
Part: HOUSING — CRACKED (CARGO DOOR) · airframe 27,864 hrs · 19,729 cycles
AFT CARGO BAY DOOR HANDLE HOUSING CRACKED. REMOVED & REPLACED THE AFT CARGO BAY DOOR HANDLE HOUSING WITH A NEW SERVICEABLE HOUSING IAW CRJ 900 SRM 51-42-21-001-001-A01 & AMM 52-31- 08-400-801-A01. REMOVED & REINSTALLED SAME SERVICEABLE PROX SENSOR PX 102 IAW CRJ 900 AMM 52-70-02-400-802(A03). COMPLIED WITH OPERATIONAL TEST OF THE AFT BAGGAGE BAY DOOR HANDLLE AND THE AFT BAGGAGE BAY DOOR IAW CRJ 900 AMM 52-31-00-710-801-A02 AND 52-31-03-710-801-A01. NO DEFECTS NOTED.
Part: ATTACH BRACKET — CRACKED (SERVICE DOOR) · airframe 27,864 hrs · 19,729 cycles
SERVICE DOOR UPPER ROD ATTACH BRACKET IS CRACKED. REMOVED & REPLACED THE SERVICE DOOR UPPER STABILIZER BRACKET WITH A NEW SERVICEABLE BRACKET IAW CRJ 900 AMM 52-41-27-400-801-A01. COMPLIED WITH OPS TEST OF THE GALLEY SERVICE DOOR IAW CRJ 900 AMM 52-41-00-710-801-A01. NO DEFECTS NOTED. WVAC EMP# 585983
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
STRINGER 23R IS CORRODED BETWEEN F.S. 319 AND F.S. 349. REMOVED AND REPLACED STR 23R BETWEEN F.S. 319 AND F.S. 349 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. WVAC
Part: FRAME — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
FS 364 FRAME CORRODED BETWEEN STRINGER 27 & 26R. OK TO INSTALL. WVAC STAMP INSP INSTALLED THE NEW SERVICEABLE FS 364 FRAME P/N SH670-32090-9 IAW BOMBARDIER REO NO. 601-53-21-687 REV A DATED 2016/06/06 STEPS 8 THRU 9. WVAC STAMP
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
INTERCOSTAL AT F.S. 333 TO F.S. 349 STRINGER 21L IS CORRODED. REMOVED & REPLACED INTERCOSTAL AT F.S. 333 TO F.S. 349 STR 21L IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. WVAC
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
INTERCOSTALS FS 349.00 - 364.00, FWD OF AVIONICS LWR DOOR STRUCTURE 2 LHS & 2 RHS OF BL "0" CORRODED. LOCATED, DRILLED AND INSTALLED 4 EA INTERCOSTALS IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. WVAC ADDITIONAL PARTS: SH670-32075-4
Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
STRINGER 22R IS CORRODED BETWEEN F.S. 319 AND F.S. 349. REMOVED AND REPLACED CORRODED STRINGERS 22R FS 280 - 349 AND FS 333 JOINT SPLICE WITH NEW SERVICEABLE STRINGERS & JOINT SPLICE PN'S SH670- 31379-1S, SH670-32429-4 & SH670-31210-2 IAW CRJ 900 SRM 51-42-06-001- 001-A01 & 51-42-21-001-001-A01. WVAC ADDITIONAL PARTS: SH670-32429-4, SH670-31379-1
Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
STRINGER 20R IS CORRODED BETWEEN FS 310 AND FS 319. REMOVED AND REPLACED CORRODED STGR 20R AND BRACKET BETWEEN FS 280 & FS319 PN SH670-31208-3 IAW CRJ 900 SRM 51-42-06-001-001-A01. WVAC ADDITIONAL PART INSTALLED: SH670-96034-5
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
INTERCOSTAL AT F.S. 319 TO F.S. 349 STRINGER 20R IS CORRODED. REPAIRED CORRODED INTERCOSTAL PN SH670-32004-1 AT FS 319 TO FS 349 BY REMOVING AND REPLACING WITH NEW SERVICEABLE INTERCOSTAL IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. WVAC
Part: FRAME — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
FRAME @ FS 319.00, STGR 26L - 25R CORRODED. LOCATED, DRILLED AND INSTALLED NEW FRAME SECTOR AND REPAIR PARTS IAW REO 670-53-21-799 REV A, 2016/11/27. WVAC
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
INTERCOSTAL AT FS 310 TO FS 319 STRINGER 20R IS CORRODED. REMOVED AND REPLACED CORRODED INTERCOSTAL FS 310 TO FS 319 STGR 20R PN SH670-32047-1 IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001- 001-A01. WVAC
Part: FRAME — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
FRAME @ FS 310.0, STGR 26L - 25R CORRODED. REMOVED AND REPLACED CORRODED FRAME SECTION AT FS 310 STR 26L-25R IAW REO 670-53-21-799 REV A. WVAC STAMP
Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
STRINGER 26R IS CORRODED FROM FS 280 - FS 364. REMOVED AND REPLACE STR 26 FROM FS 280 - FS 364 IAW CRJ 900 SRM'S 51- 40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. WVAC STAMP
Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 27,864 hrs · 19,729 cycles
VERTICAL STAB, LH, AFT DRAG ANGLE, POSSIBLE CRACK. REPAIRED VERT STAB LH AFT DRAG ANGLE IAW EA CRJ953-0172 & SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 & 51-42-22-001-001-A01, 51-40-11- 001-001-A01.
Part: SPLICE ANGLE — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
SPLICE ANGLES @ FS 333.00 24L -24R CORRODED. REMOVED & REPLACED SPLICE ANGLES @ 333.00 24L-24R & CLEATS AT 333 STR26R 27 26L & 25L IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-06-001- 001-A01. ADDITIONAL PART REPLACED: SH670-32429-4
Part: FRAME — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
FRAME @ FS 295.00, STGR 26L - 25R CORRODED. REPAIRED IAW BOMBARDIER GREO 670-53-21-799. WVAC STAMP
Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
STRINGER 27 IS CORRODED FROM FS 295 - FS 319. REMOVED & REPLACED STR 27 @ F.S. 295 TO F.S. 319 IAW CRJ 900 SRM 51- 40-11-001-001-A01 AND SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. WVAC
Part: LONGERON — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
FS 349 - FS 364 STR 25R LONGERON CORRODED. REMOVED CORRODED STR 25R AND INSTALL NEW STR 25R IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01 AND 51-40-11-001-001-A01. WVAC
Part: SKIN — DENTED (TE FLAP) · airframe 27,864 hrs · 19,729 cycles
L/H INBD FLAP HAS (1) SHARP DENT APPROX 6"" UP FROM T/E ON FLAP ON BOTTOM SKIN, APPROX WS 108.00. DENT IS APPROX .125" L X .062" W X .015" D. (MARKED WITH TAPE). REPAIRED L/H IB FLAP BOTTOM SKIN DENT AT WS 108.00 IAW CRJ 900 SRM 57-52-01-201-001-A01 TYPE IV REPAIR. WVAC
Part: SKIN — DENTED (TE FLAP) · airframe 27,864 hrs · 19,729 cycles
L/H INBD FLAP HAS (2) DENTS IN CLOSE PROXIMITY ON BOTTOM SKIN OF FLAP AT APPROX W.S. 38.00. EACH DENT APPROX .1875"" DIA AND .010"" DEEP. (MARKED WITH TAPE) REPAIRED DENTS ON L/H INBD FLAP IAW CRJ 900 SRM 57-52-01-201-001-A01 TYPE IV REPAIR. WVAC
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
TCAS ANT DOUBLER @ FS 295.00 - FS 310.00, BL "0" CORRODED. REMOVED & REPLACED TCAS ANT DOUBLER IAW CRJ 900 SRM 51-42-06-001-001- A01, 51-21-06-001-001-A01 & 51-42-21-001-001-A01. WVAC
Part: PIN — BENT (RT COWLING) · airframe 27,864 hrs · 19,729 cycles
RH ENGINE LOWER COWLING ALIGNMENT PIN AFT OF THE 2ND LATCH IS BENT, UNDERLYING STRUCTURE POSSIBLY DAMAGED. REMOVED & REPLACED ALIGNMENT PIN & OB EDGE MEMBER IAW CRJ 900 SRM 51-41-02-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001. WVAC
Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,864 hrs · 19,729 cycles
F.S. 280 J ANGLE IS CORRODED. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FS 280 J ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01. NEW SERVICEABLE PN - CC670-34095-1SB. WVAC
2018
Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 23,163 hrs · 16,217 cycles
AFT LAVATORY SMOKE WARNING, NO SMOKE OR FIRE NOTED. OP CHECKED GOOD, NO SMOKE IN AFT LAVATORY CHECK IAW AMM 26-16-00.
Part: HANDLE — CRACKED (AVIONICS DOOR) · airframe 23,162 hrs · 16,216 cycles
INDICATION NOTE ON THE MAIN AVIONICS BAY DOOR HANDLE AT RADIUS 100 PERCENT FULL SCREEN HEIGHT AROUND SHAFT HOUSING. FAILING NDT. REMOVED AND REPLACED AVIONICS DOOR HANDLE ASSY IAW SRM 51-42-21-01-001-A01 E, AMM 52-42-03-400-801 A01. OPS CHECKED GOOD.
2017
Part: STRUT — FAILED (PAX DOOR) · airframe 21,745 hrs · 15,163 cycles
WHEN OPENING THE PAX DOOR IT DROPS ABRUPTLY AND HITS THE GROUND. REMOVED AND REPLACED FWD AND AFT COUNTER BALANCE GAS SPRINGS IAW AMM 52-11-17.
2016
Part: SKIN PANEL — DAMAGED (BS 501-517) · airframe 20,245 hrs · 14,103 cycles
DURING C CHECK, FOUND ONE FWD ATG ANTENNA MOUNT HOLE ELONGATED. THE SKIN PANEL WAS CUT OUT. FABRICATED AND INSTALLED A FILLER AND DOUBLER IAW ECTC AND EA 32-2016-262.
Part: SEAT TRACK — CORRODED (BS 847) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT TRACK BS 847. REMOVED, FABRICATED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801 A07, 53-00-49-400-801 A07, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343 REV K.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
AFT CARGO FLOORBEAM CORRODED AT FS1031.00 ON LBL9. COMPLIED WITH EC/TC EO 900-53-0039 REV O, REO 670-53-00-029 AND EC/TC REO 690-53-61-649 DISCREPANT SECTION OF FLOORBEAM WAS REMOVED. NEW SECTION WAS FABRICATED THEN INSTALLED. THIS REPAIR IS CLASSIFIED AS A MAJOR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
AFT CARGO FLOORBEAM CORRODED AT FS1031.00 ON LBL9. C/W EC/TC EO 900-53-0039 REV O REO 670-53-00-029 AND EC/TC REO 690-53-61-649. DISCREPANT SECTION OF FLOORBEAM WAS REMOVED. NEW SECTION WAS FABRICATED THEN INSTALLED. EC/TC REO 690-53-61-649 WAS A DEVIATION TO EC/TC EO 900-53-0039 REV O / REO 670-53-00-029 DUE TO LOCATION OF BEAM SPLICE INTERFERING WITH THE LOCATION OF POTABLE WATER LINE MOUNTING BRACKET. THE DEVIATION INCORPORATED THE SHIMMING OF SAID BRACKET. CLASSIFIED AS A MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
AFT CARGO FLOORBEAM CORRODED AT FS1031 LBL27. COMPLIED WITH EC/TC EO 900-53-0040 REV O AND REO 670-53-00-029. DISCREPANT SECTION OF FLOORBEAM WAS REMOVED. NEW SECTION WAS FABRICATED THEN INSTALLED. REPAIR CLASSIFIED AS A MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LT SEAT RAIL. REMOVED, FABRICATED AND INSTALLED SEAT RAIL AT FS785.15-847.00+16 LT IAW AMM 53-49-000-801-A07, 53-00-49-400-801-A07, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343 REV M.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 20,245 hrs · 14,103 cycles
DURING C CHECK, CORROSION FOUND ON SIDE SEAT TRACK BS 785.15 - 847.00+16. REMOVED, FABRICATED, AND INSTALLED SEAT TRACK IAW AMM 53-00-49-00-801-A07, 53-00-49-400-801-A07, REO 670-53-00-343 REV M. & EC/TC REO 670-53-00-343 REV M.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LT SIDE SEAT RAIL AT FS661.00. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: PLATE — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
SERVICE DOOR THRESHOLD PLATE HAS NUMEROUS AREAS OF CORROSION. REMOVED AND REPLACED SERVICE DOOR THRESHOLD PLATE IAW AMM 51-42-06-001-001 AND 51-25-06-001-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LT SIDE SEAT RAIL AT FS669.40. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT RAIL AT FS744.15 RT SIDE. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
RIGHT CABIN FLOOR SILL AT FS280.00-319.00 CORRODED. REMOVED AND REPLACED RIGHT FLOOR SILL AT FS280.00-319.00 PER SRM 51-42-06-00-001-A01.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RT SIDE SEAT RAIL AT FS847.00. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RT SEAT RAIL. REMOVED, FABRICATED AND INSTALLED SEAT RAIL AT FS847.00+16-897.70 RT IAW AMM 53-49-000-801-A07, 53-00-49-400-801-A07, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343 REV M.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RT SEAT RAIL. REMOVED, FABRICATED AND INSTALLED SEAT RAIL AT FS744.15-761.85 RT IAW AMM 53-49-000-801-A07, 53-00-49-400-801-A07, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343 REV.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT RAIL AT FS847.00+16-897.70 RT SIDE. REMOVED, FABRICATED AND INSTALLED SEAT RAIL IAW AMM 53-00-49-000-801-A07, 53-00-49-400-801-A07, REO 670-53-00-343 REV M AND EC/TC REO 670-53-00-343 REV M.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT RAIL AT RBL9. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RBL9 SEAT RAIL. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT RAIL RBL9. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW BOMBARDIER REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RBL9 SEAT RAIL. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LBL27 SEAT RAIL. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT RAIL AT FS847.00+16 LT SIDE. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT RAIL RBL9. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON SEAT RAIL AT FS942.00 LT SIDE. -MTC- REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LBL9 SEAT RAIL. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RT SEAT RAIL. REMOVED FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RT SEAT RAIL AT FS349-485.00. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LT SIDE SEAT RAIL. REMOVED, FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LBL9 SEAT RAIL AT FS379.00-485.00. REMOVED FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: GLOWSTRIP — CRACKED (CABIN) · airframe 20,238 hrs · 14,096 cycles
PHOTO LUMINESCENT FLOOR PATH LIGHTING DAMAGED AND CRACKED. REMOVED AND REPLACED PHOTO LUMINESCENT FLOOR PATH LIGHTING, (PN PL88-950LH01, PL88-900H00, PL88-910HL00) IAW AMM 33-51-01-000-801 (A27) AND 33-51-01-400-801 (A27).
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON LBL9 SEAT RAIL. REMOVED FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 20,238 hrs · 14,096 cycles
CORROSION FOUND ON RBL9 SEAT RAIL AT FS581.00-661.00+32. REMOVED FABRICATED AND INSTALLED NEW SEAT RAIL IAW REO 670-53-00-343 REV M, EC/TC REO 670-53-00-343, AMM 53-00-49-000-801-A07 AND 53-00-49-400-801-A07.
Part: STRUCTURE — CHAFED (LT NLG WW) · airframe 18,775 hrs · 13,034 cycles
LEFT NLG SURROUND STRUCTURE CHAFED BY BONDING WIRE. BLENDED CHAFE DAMAGE FROM DISCREPANT AREA ON DOOR SURROUND IAW SRM 51-12-00 AND 51-13-01. COMPLIED WITH PERMANENT REPAIR SECTION 1, STEPS 1, 2 AND 3 OF EA 20-2016-114, GAINED ACCESS, CLEANED AFFECTED AREA AND PERFORMED DETAILED VISUAL INSPECTION OF REWORKED AREA. STEP 4 OF PERMANENT REPAIR, REPLACE BONDING STRAP. ACCOMPLISHED ON NR 00002 OF THIS W/O. SEE ITEMS 1 AND 2 OF THIS N/R FOR ACCOMPLISHMENT OF ITEMS 5 AND 6 OF PERMANENT REPAIR. RESTORED SURFACE FINISH TO REWORKED AREA IAW EA 20-2016-114 AND SRM 51-21-16. THIS COMPLETES THE REQUIREMENTS OF EA 20-2016-114.
2015
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,896 hrs · 12,398 cycles
EMERGENCY EXIT OVERHEAD SIGN MISSING. REPLACED OVERHEAD EMERGENCY EXIT SIGN COVER, REF AMM 33-51-7.
Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 17,384 hrs · 12,028 cycles
PASSENGER ENTRANCE EMERGENCY LIGHT WILL NOT TEST/INOPERATIVE. R & R FUSE FOR EMERGENCY LIGHT IAW ESPM 20-29-00. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-05 FOR EMERGENCY BATTERY PACK 1, OPS. CHECK GOOD. ACFT OK FOR SERVICE.
2014
Part: LIGHT — MISSING (CABIN) · airframe 15,365 hrs · 10,665 cycles
EMERGENCY LIGHT STRIP AT EXIT ROW BEHIND SEAT 12B MISSING. INSTALLED THE EMERGENCY LIGHT IAW AMM 33-51-01.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 14,503 hrs · 10,073 cycles
OVERWING LIGHT ON PANEL 172BR HAS BROKEN WIRE. INSTALLED NEW CONTACT ON OVER WING LIGHT PANEL 172BR THEN CONNECTED IT BACK TO LIGHT ASSY IAW ESPM 20-44-00. PERFORMED OPS TEST OF EMERGENCY LIGHT FOR EXTERNAL EMERGENCY OVERWING DOOR, DS93, OPS CHECK GOOD.
Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 14,503 hrs · 10,073 cycles
RT AFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST EXCEEDED, 40LBS. LUBED RT AFT OVERWING EMER EXIT IAW AMM 12-20-52-640-816 FUNCTIONAL TEST CK GOOD NO DEFECTS NOTED IAW AMM 52-21-00-720-803.
Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 14,503 hrs · 10,073 cycles
RIGHT FWD OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST EXCEEDED 40LBS OF FORCE TO OPERATE HANDLE. LUBED RT FWD OVERWING EMERGENCY EXIT IAW AMM 12-20-52-640-815 FUNCTIONAL TEST, CK GOOD NO DEFECTS NOTED IAW AMM 52-21-00-720-802.
Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 14,503 hrs · 10,073 cycles
LEFT AFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL CHECK EXCEEDED 40LBS. LUBED LT AFT OVERWING EMER EXIT IAW AMM 12-20-52-610-816. FUNCTIONAL TEST CK GOOD NO DEFECTS NOTED IAW AMM 52-21-00-720-803.
Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 14,503 hrs · 10,073 cycles
LEFT FWD OVERWING EXIT FAILED FUNCTIONAL CHECK EXCEEDED, 40LBS. LUBED FWD OVERWING (LT) EXIT IAW AMM 12-20-52-640-815 FUNCTIONAL TEST CK GOOD NO DEFECTS NOTED IAW AMM 52-21-00-720-802.
Part: SKIN — CORRODED (BS 307) · airframe 14,503 hrs · 10,073 cycles
FOUND CORRROSION ON EXTERNAL SKIN AT BS 307 S27. REPAIRED IAW EA 32-2014-041.
Part: BEARING — CRACKED (RT WING) · airframe 14,503 hrs · 10,073 cycles
RIGHT WING REAR SPAR LINK ASSEMBLY LOWER BALL BEARING CRACKED. RIGHT WING REAR SPAR LINK ASSY REPLACED DURING ACCOMPLISHMENT OF SB670BA-57-016. SDR CLOSED.
Part: BEARING — CRACKED (LT WING) · airframe 14,503 hrs · 10,073 cycles
LEFT WING REAR SPAR LINK ASSY LOWER BALL BEARING CRACKED AND LINK TOUCHING FUSELAGE FRAME. LEFT WING REAR SPAR LINK ASSY REPLACED DURING ACCOMPLISHMENT OF SB670BA-57-016. SDR CLOSED.
Part: FLOORBEAM — CRACKED · airframe 14,503 hrs · 10,073 cycles
RT COCKPIT FLOORBEAM CRACKED AT RBL12. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH REO 690-53-11-689. RECEIVED AND COMPLIED WITH ECTC, REO 690-53-11-689.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,503 hrs · 10,073 cycles
LEFT COCKPIT FLOORBEAM CRACKED AT LBL 12. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH REO 690-53-11-689. RECEIVED AND COMPLIED WITH ECTC REO 690-53-11-689.
Part: SKIN — DENTED (LT NACELLE) · airframe 14,503 hrs · 10,073 cycles
DENT ON LT LOWER FAN COWL BETWEEN FWD 2 LATCHES. COMPLIED WITH EA 12-2014-133, REVA SECTION 3, STEP A II. REQUESTED ECTC 12-2014-133. REVERIFIED ALL STEPS OF EA 12-2014-133. REV B HAS BEEN COMPLIED WITH ECTC 12-2014-133, REV B HAS BEEN ACCOMPLISHED.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 14,501 hrs · 10,072 cycles
CORROSION AROUND ANTENNA BETWEEN BS 295-FS310 S27. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01-101-002-A02 AND 51-21-06-001-001-A01. REMOVED AND REPLACED THE DOUBLER IAW SRM 51-42-20-001-001-A01, SRM 51-42-210-001-A01, & 51-42-06-001-001-A01.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 14,503 hrs · 10,073 cycles
RT BS 280 BULKHEAD WEB CORRODED. FOUND OUT OF LIMITS IAW SRM 53-11-10-201-003-001. REPAIRED IAW REO 670-53-11-594-01, REV.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 14,501 hrs · 10,072 cycles
RBL 9, SEAT TRACK SEGMENT BS 581-661+32 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 581-661) · airframe 14,501 hrs · 10,072 cycles
LBL 9, SEAT TRACK SEGMENT BS 581-661+32 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 14,501 hrs · 10,072 cycles
RIGHT SEAT TRACK SEGMENT BS 744.15 -761.85 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 14,503 hrs · 10,073 cycles
COCKPIT FLOOR SUPPORT CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 14,501 hrs · 10,072 cycles
LT BS 280 BULKHEAD WEB CORRODED. FOUND OUT OF LIMITS OF SRM 53-11-10-201-003-001. REPAIRED IAW REO 670-53-11-594, NOTES 1-2.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 14,501 hrs · 10,072 cycles
LEFT SEAT TRACK SEGMENT BS 744.15 - 761.85 CORRODED IN SEVERAL AREAS. R & R SEAT RAIL IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: DOOR FRAME — CORRODED (COCKPIT DOOR) · airframe 14,503 hrs · 10,073 cycles
LT COCKPIT DOOR POST LOWER SECTION CORRODED AT LBL 12. REMOVED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. REMOVED 8EA RIVETS AND CLIP IAW SRM 51-2-13-001-001-A01 & SRM 51-42-06-001-001-A01. INSTALLED, 8 EA, RIVETS AND CLIP IAW SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01. 100 PERCENT MATERIAL LOSS AT AFT LOWER EDGE CONTACT ENGINEERING FOR DISPOSITION. BLENDED CORRODED ON LEFT SIDE DOOR POST LOWER SECTION AT FS280 AND LBL12, NDI AREA AND RESTORED FINISH IAW EA 32-2014-042 AND ECTC EA 32-2014-042.
Part: SEAT TRACK — CORRODED (BS 661-690) · airframe 14,501 hrs · 10,072 cycles
LBL 9, SEAT TRACK SEGMENT BS 661+32 - 690 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-A01.
Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 14,501 hrs · 10,072 cycles
LEFT SIDE SEAT TRACK SEGMENT BS 677-720.85 CORRODED IN SEVERAL AREAS. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.
Part: INTERCOSTAL — CORRODED (BS 364) · airframe 14,501 hrs · 10,072 cycles
INTERCOSTAL AT BS 364 S26R CORRODED. R & R THE INTERCOSTAL IAW SRM 5-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 785-860) · airframe 14,501 hrs · 10,072 cycles
RIGHT SEAT TRACK SEGMENT BS 785.15 - 860 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801, GREO 670-53-00-343, AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 14,501 hrs · 10,072 cycles
RIGHT SEAT TRACK SEGMENT BS 677-720.85 CORRODED IN SEVERAL AREAS. BLENDED AREA AND FOUND OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801 AIPC 53-00-49 ITEM 1, ITEM 30 AND AMM 53-00-49-400-801.
Part: FITTING — CORRODED (BS 319) · airframe 14,501 hrs · 10,072 cycles
CORROSION ON FLOOR SUPPORT FITTING, RT FWD OF SERVICE DOOR, BS 319. REMOVED FLOOR SUPPORT FITTING IAW SRM 51-42-20-001-001-A01. INSTALLED NEW FLOOR SUPPORT FITTING IAW SRM 51-42-21-001-001-A01 & DWG SH670-31950.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,501 hrs · 10,072 cycles
LT BS 280 FLOORBEAM CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. INSTALLED NEW FLOORBEAM IAW S/B 670BA-53-041-01 & DWG CC670-34094.
Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 14,501 hrs · 10,072 cycles
RT COCKPIT FLOOR SUPPORT ANGLE CRACKED AT THE AFT SIDE. RT COCKPIT FLOOR SUPPORT ANGLE R & R IAW REO 690-53-11-689.
Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 14,501 hrs · 10,072 cycles
CORROSION ON SERVICE DOOR SILL ANGLE, AT SEVERAL LOCATIONS. REMOVED AND REPLACED THE SERVICE DOOR SILL ANGLE IAW DWG SH670-31950, 51-40-11-001-001-A01 AND SRM 51-42-06-001-001-A01.
Part: STRUCTURE — CORRODED (BS 349) · airframe 14,501 hrs · 10,072 cycles
CORRODED PACKER AT FS 349 RBL 8. REMOVED CORRODED PACKER & INSTALLED NEW PACKER IAW SRM 51-42-06-001-001-A01 & DWG SH670-32167.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 14,501 hrs · 10,072 cycles
RT 280 FLOORBEAM CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. INSTALLED FLOORBEAM IAW S/B 670BA-53-041-01 & DWG CC670-34094.
Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 14,501 hrs · 10,072 cycles
CORROSION ON SEAT TRACK RBL 9, BS 349- 477.40. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 (A01) AND AMM 53-00-49-400-801 (A01).
Part: FLOOR SUPPORT — CORRODED (COCKPIT) · airframe 14,501 hrs · 10,072 cycles
LEFT COCKPIT FLOOR SUPPORT ANGLE CRACKED AT THE AFT SIDE. LT COCKPIT FLOOR SUPPORT ANGLE R & R IAW REO 690-53-11-689.
Part: SKIN — DAMAGED (BS 333) · airframe 14,501 hrs · 10,072 cycles
LIGHTNING DAMAGE ON FASTENER FS 333 STR 25L-24L. COMPLIED WITH SRM SUPPLEMENT, REF GREO 670-53-00-045, REV G, STEP ,NR 3 A2/PERMANENT DISPOSITION BLENDED OUT DAMAGE. C/W LIGHTNING STRIKE REPAIR AT FS 333 STR 25L-24L IAW REO 670-53-00-045, REV G, STEP 3 A2. PERMANENT REPAIR.
Part: SKIN — DAMAGED (BS 364) · airframe 14,501 hrs · 10,072 cycles
LIGHTNING DAMAGE FS 364, BETWEEN STR 25R. COMPLIED WITH SRM SUPPLEMENT 53-00-00, REF GREO 670-53-00-045 REV G, STEP NR 3 B2/PERMANENT DISPOSITION OPENED UP HOLE FOR 1-OFF MS20426A06 INSTALLATION. C/W LIGHTNING STRIKE REPAIR AT FS 364, STR 25L IAW REO 670-53-00-045, REV G.
Part: SKIN — DAMAGED (BS 394) · airframe 14,501 hrs · 10,072 cycles
LIGHTNING DAMAGE ON FASTENER FS 394 BETWEEN STR 25L - 24L. COMPLIED WITH SRM SUPPLEMENT, REF GREO 670-53-00-045, REV G, STEP NR 3 A2/PERMANENT DISPOSITION BLENDED OUT DAMAGED AREA. C/W LIGHTNING STRIKE REPAIR AT FS 394 BETWEEN STR 25L-26L IAW REO 670-53-00-045, REV G, STEP 3 A2.
Part: SKIN — DENTED (LT NACELLE) · airframe 14,503 hrs · 10,073 cycles
DENT ON LT LOWER FAN COWL BETWEEN FWD 2 LATCHES. COMPLIED WITH STS EA 12-2014-133, REV A, SECTION 111, PERMANENT REPAIR, DENT MEASURES .009". RECEIVED AND COMPLIED WITH ECTC EA 12-2014-133, REV B. COMPLIED WITH STS EA 12-2014-133, REV A, SECTION 111, PERMANENT REPAIR A. PERMANENT REPAIR.
Part: SKIN — DAMAGED (BS 310) · airframe 14,501 hrs · 10,072 cycles
LIGHTNING STRIKE DAMAGE DISCOVERED AT FS 310 & STR 25L. COMPLIED WITH SRM SUPPLEMENT 53-00-00, REF GREO 670-53-00-045, REV G, STEP NR 3 B2/PERMANENT DISPOSITION OPENED UP HOLE FOR 1-OFF MS20426AD6 INSTALLATION. C/W LIGHTNING STRIKE REPAIR AT FS 364, STR 25L IAW REO 670-53-00-045, REV G.
Part: LIGHT — MISSING (CABIN) · airframe 13,938 hrs · 9,683 cycles
EMERGENCY LIGHT AT EXIT ROW 13C & D MISSING. SECURED LIGHT IAW AMM 33-51-01, NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.
Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 13,183 hrs · 9,225 cycles
FWD CARGO DOOR SEAL RETAINER BENT AT BOTTOM OF DOOR. COMPLIED WITH EC/TC REO 690-52-35-013. MAJOR REPAIR IAW GMM 5-3.
Part: RETAINER — BENT (CARGO DOOR SEAL) · airframe 13,183 hrs · 9,225 cycles
CENTER CARGO DOOR SEAL SEAL RETAINER BENT. COMPLIED WITH EC/TC REO 690-52-35-013. MAJOR REPAIR IAW GMM 5-3.
2013
Part: BATTERY — INOPERATIVE (MEGAPHONE) · airframe 12,562 hrs · 8,847 cycles
MEGAPHONE BATTERY INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14.
Part: FLOOR SUPPORT — CORRODED (BS 280) · airframe 11,700 hrs · 8,285 cycles
FLOOR SUPPORT HAS CORROSION AT FS 280 AND RBL 45. REPAIRED IAW SRM 53-21-43-201-002-A01, PARA 5.3 (3) IAW NDTM PART 1, 51-20-0006-250, 51-24-36-001-001. REPAIR CLASSIFIED AS MAJOR.
2012
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 9,928 hrs · 7,083 cycles
CAPTAIN'S LIFE VEST BAG TORN. REMOVED AND REPLACED VEST IAW AMM 25-61-03.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 8,954 hrs · 6,361 cycles
SEAT TRACK NR 4 CORRODED. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 581-661) · corrosion level 2 · airframe 8,954 hrs · 6,261 cycles
SEAT TRACK NR 3 CORRODED FROM FS 581 TO 661+32. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 8,954 hrs · 6,361 cycles
RIGHT FLOOR SEAT TRACK NR 4 CORRODED. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 8,954 hrs · 6,361 cycles
SEAT TRACK CORRODED. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 8,954 hrs · 6,361 cycles
SEAT TRACK NR 3 CORRODED. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 485-581) · corrosion level 2 · airframe 8,954 hrs · 6,361 cycles
NR 2 SEAT TRACK CORRODED FROM FS 485 TO 581. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 8,954 hrs · 6,361 cycles
SEAT TRACK NR 2 CORRODED. REPAIRED IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 661-693) · corrosion level 2 · airframe 8,954 hrs · 6,361 cycles
SEAT TRACK NR 4 CORRODED FROM FS 661+32 TO 693. REPAIRED IAW REO 670-53-00-013.
Part: SLAT — OUT OF RIG (RT WING) · airframe 8,691 hrs · 6,146 cycles
DURING 50HR INSP FOUND RT SLAT NR 3 TO BE GAPPED .040" OUT OF TOLERANCE. RIGGED NR 3 SLAT INTO TOLERANCE PER CRJ900 AMM 27-81-25. OPS CHECK GOOD.
Part: REFLECTOR — DEFECTIVE (CABIN) · airframe 7,949 hrs · 5,641 cycles
FLOOR LIGHTING STRIP ON GALLEY FLOOR RIGHT SIDE LAY NOT WORKING. REMOVED & REPLACED FLOOR REFLECTOR STRIP & COVER PER B&E CMM 25-33-01. OK FOR SVC.
2011
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 5,760 hrs · 4,212 cycles
IAH TO MEM DIVERTED TO ATL DUE TO INBOARD FLT SPOILERS & INBOARD SPOILERONS MESSAGE, CREW DECLARED EMERGENCY.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 5,883 hrs · 4,097 cycles
THREE DENTS WERE FOUND ON THE RIGHT SIDE FUSELAGE AT FS 402, MEASURING .8"L X .7"W X .010"DEEP, FS 424.6, MEASURING 2"L X 1.4"W X 0.020" DEEP, FS 427.5, MEASURING 1.5"L X 1.1"W X 0.011" DEEP. ALL DENT LOCATD BETWEEN S-15R AND S-16R. THE DENTS WERE EVALUATED AND REPAIRED IAW STS ENGINEERING EA EA 10-PINN-2011-014.
2010
Part: STRUCTURE — CRACKED (LT MLG WW) · airframe 4,651 hrs · 3,478 cycles
LEFT MAIN LANDING GEAR (MLG) WHEEL BIN WAS FOUND WITH TWO CRACKS ON THE INNER SURFACE. THE FIRST CRACK IS ON THE BIN CAP AND THE DAMAGE IS LOCATED AT THE 3 OâCLOCK POSITION AND 6 INCHES FROM THE CENTER POINT. THIS CRACK MEASURES 3 INCHES IN LENGTH, 0.063 INCH WIDE AND IS CONTAINED IN THE FIRST 2 - 3 FABRIC LAYERS. THE SECOND CRACK IS LOCATED ON THE SIDE WALL AT THE 3 OâCLOCK POSITION AND 11 INCHES ABOVE THE WHEEL BRUSHES. THE CRACK AT THIS LOCATION IS RECORDED AS 6.0 INCHES IN LENGTH, 0.063 INCH WIDE AND CONTAINED IN THE FIRST COUPLE FABRIC LAYERS. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-245. FLY ON TO NEXT C CHECK NOT TO EXCEED 5000 FH AT WHICH TIME ACCOMPLISH A PERMANENT REPAIR IN ACCORDANCE WITH SRM 53-00-00, TASK 53-00-00-201-002.