N232PQ
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.
181 reports on file, 2011-10-14 – 2025-08-23.
Part: ANGLE — CRACKED (ZONE 100) · airframe 36,503 hrs · 26,883 cycles
INITIAL INSPECTION:CRACK ON DIAPHRAGM BTW FS= 797 TO FS= 807 RBL 35 ON FWD AREA W/W AT MLG DIAPHRAGM BTW FS= 797 TO FS= 807 RBL 35 ON FWD AREA W/W AT MLG WAS REPLACED PER CRJ900 SRM 51-41-02-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 36,503 hrs · 26,883 cycles
CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA)AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA). DUE TO EXCESIVE CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA) AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA) WERE REPLACED PER CRJ900 SRM 53-21-43-101-001-A01 AND SRM 51-42-21-001-001-A01
Part: HINGE — BROKEN (ZONE 800) · airframe 36,503 hrs · 26,883 cycles
BROKEN HINGE ON UPPER STAIR PANEL OF THE PASSENGER DOOR HINGE ON ACCESS PANEL 832 ET WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01
Part: FITTING — CORRODED (ZONE 200) · airframe 36,503 hrs · 26,883 cycles
CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA)AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA). DUE TO EXCESIVE CORROSION ON SETTLEMENT FITTING OF ENTRANCE COMPARTMENT (1EA) AND GALLEY 1 (1EA) (FLOOR STRUCTURE AREA) WERE REPLACED PER CRJ900 SRM 53-21-43-101-001-A01 AND SRM 51-42-21-001-001-A01
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,503 hrs · 26,883 cycles
AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT RH CROSSBEAM FS 280.00 FLOOR PANEL SUPPORT ANGLE (251ALF FLOOR PANEL AREA) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A01
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,503 hrs · 26,883 cycles
AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT RH CROSSBEAM FS 280.00 RH CROSSBEAM FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A01
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,503 hrs · 26,883 cycles
AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT LH CROSSBEAM FS 280.00. CORROSION AT LH CROSSBEAM FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A01
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 36,503 hrs · 26,883 cycles
AFTER FLOOR PANEL SUPPORT ANGLE, CORROSION AT LH CROSSBEAM FS 280.00. CORROSION AT LH CROSSBEAM FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND PER CRJ900 SRM 51-42-21-001-001-A01
Part: ANGLE — CORRODED (ZONE 800) · airframe 36,503 hrs · 26,883 cycles
AFTER TO REMOVAL MID CAP ANGLE WAS FOUND CORROSION ON KICKPLATE ANGLE OF THE PASSENGER DOOR SURROUND KICKPLATE WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-23-101-001-A02 WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01
Part: SUPPORT FITTING — CORRODED (ZONE 800) · airframe 36,503 hrs · 26,883 cycles
WEAR AT FWD/AFT HANDRAIL SUPPORT FITTING AT FWD AND AFT SIDE PANEL OF PASSENGER DOOR, ALSO MISSING BUMPERS FWD/AFT HANDRAIL SUPPORT FITTING AT FWD AND AFT SIDE PANEL OF PASSENGER DOOR WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND MUST BE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND MUST BE INSTALLED UNDER NRCS 00088 AND 00089
Part: BUSHING — CORRODED (ZONE 500) · airframe 36,503 hrs · 26,883 cycles
CORROSION ON BUSHING BORE LUG L1, L2. L5 AND L6 AT LH AILERON CENTER FITTING WERE FOUND BUSHING BORE LUGS L1, L2. L5 AND L6 AT LH AILERON CENTER FITTING WERE REPAIRED PER REO 670-57-61-237 REV. - -
Part: PANEL — CRACKED (ZONE 800) · airframe 36,503 hrs · 26,883 cycles
CRACK ON FWD SIDE PANEL OF THE PASSENGER DOOR FWD SIDE PANEL OF THE PASSENGER DOOR WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01 AND EA CRJ952-19920 REV.A.
Part: WEB — CRACKED (ZONE 100) · airframe 36,503 hrs · 26,883 cycles
CRACK ON WEB BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT WEB BELOW OF ADG RESTOW PUMP AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01 AND EA CRJ953-20015 REV B
Part: BEAM — CHAFED (ZONE 100) · airframe 36,503 hrs · 26,883 cycles
WEAR ON BEAM ON FWD AND AFT AREA ON AFT BAGGAGE BAY STRUCTURE BTW FS 1000.00 TO 10047.00. BEAM ON FWD AT AFT BAGGAGE BAY STRUCTURE BTW FS 1000.00 TO 1047.00 WAS REPAIRED PER EA CRJ953-19979 REV IR
Earlier reports · 2011–2024 · 167 reports
2024
Part: CAP — DETACHED (ZONE 200) · airframe 34,270 hrs · 24,957 cycles
BEAM SPLICE CAPS AT F.S. 847.00 FOR BOTH R.B.L. 9.00 AND L.B.L. 9.00 BEAMS HAVE A CONFIGURATION DEVIATION FROM SERVICE BULLETIN INSTALLATION CALL OUT. COMPLIED WITH MHIRJ REO 690-53-41-489 REV.--, DATED 2024-07-23.
Part: SUPPORT — CORRODED (ZONE 200) · airframe 34,270 hrs · 24,957 cycles
FOUND CORROSION ON O/B MOST HOLE F.S. 801.25 L/H SILL DECK. REPAIRED O/B MOST HOLE AT F.S. 801.25 L/H SIDE SILL DECK IAW MHIRJ REO 690-53-41-488 REV-- 7/17/2024.
2022
Part: NONE — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR FORMER ATTACHING CLIP CORRODED AT FS 329.41 BETWEEN DD5 AND DD6. CA: REMOVED AND REPLACED CLIPIAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
Part: FRAME — CORRODED · airframe 29,718 hrs · 21,194 cycles
FS 280 FRAME CORRODED ON UPPER FLANGE BETWEEN STR 25L AND 25R. REPAIRED IAW CRJ953-13274 REV IR DATED 4/7/2022.
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR AFT WEB HAS MULTIPLE SPOTS OF CORROSION. REMOVED PAX DOOR AFT WEB. REPLACED AFT WEB LOCATED AND DRILLED NEW WEB. REMOVED AND INSTALLED 9 STIFFNERS. REMOVED AND INSTALLED GAS TUBE MOUNT AND HANDRAIL STOP. REMOVAED AND REPLACED DRAG ANGLE STEP, SUPPORT ANGLE, AND INSTALLED AFT WEB IAW CRJ-900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND APPLIED PAINT AND CIC IAW 51-12-11-001-001-A01.
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR AFT WEB HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED PAX DOOR AFT WEB. REPLACED AFT WEB LOCATED AND DRILLED NEW WEB. REMOVED AND INSTALLED 9 STIFFNERS. REMOVED AND INSTALLED GAS TUBE MOUNT AND HANDRAIL STOP. REMOVAED AND REPLACED DRAG ANGLE STEP, SUPPORT ANGLE, AND INSTALLED AFT WEB IAW CRJ-900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND APPLIED PAINT AND CIC IAW 51-12-11-001-001-A01.
Part: FORMER — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR AFT FORMER HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED AND REPLACED FWD MIDDLE, FWD UPPER, AND FWD LOWER SEAL RETAINERS. REMOVED AND INSTALLED FWD UPPER CORNER COVERS. REMOVED AND INSTALLED FWE UPPER DOOR CENTERING PLATE IAW CRJ-900 SRM 51-42-06-001-001-A01. REMOVED, LOCATED, DRILLED, AND INSTALLED NEW SERVICABLE FWD FORMER AT F.S. 311.75 PN: 601R318031-5 IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
Part: FORMER — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR FWD FORMER HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED AND REPLACED FWD MIDDLE, FWD UPPER, AND FWD LOWER SEAL RETAINERS. REMOVED AND INSTALLED FWD UPPER CORNER COVERS. REMOVED AND INSTALLED FWE UPPER DOOR CENTERING PLATE IAW CRJ-900 SRM 51-42-06-001-001-A01. REMOVED FWD FORMER AT F.S. 311.75, LOCATED AND DRILLED NEW FORMER PN:601R318031-5 AND INSTALLED IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01. REMOVED AND INSTALLED SUPPORT ANGLE AT F.S. 311.75 IAW SRM 51-42-06-001-001-A01.
Part: WEB — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR FWD WEB HAS MULTIPLE SPOTS OF CORROSION. CA: REMOVED PAX DOOR FWD WEB IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. RECEIVED NEW SERVICABLE WEB PN: 601R317071-R5. LAYOUT AND DRILLUP IAW SRM 51-40-11-001-001-A01. INSTALLED 9 STIFFNERS ON FWD WEB IAW SRM 51-42-06-001-001-A01. INSTALLED COUNTERBALANCE MOUNT IAW 51-42-06-001-001-A01. INSTALLED PAX DOOR FWD WEB IAW 51-42-06-001-001-A01, 51-42-13-001-001-A01 REV. 38 (7/25/20). APPLIED PAINT AND CIC IAW 51-25-21-001-001-A01 AND 51-21-11-001-001-A01.
Part: SPAR — DAMAGED · airframe 29,718 hrs · 21,194 cycles
DURING REPLACEMENT OF RUDDER LOWER CENTER HINGE FOUND A HOLE THROUGH VERTICAL STAB STRUCTURE TO BE OVERSIZED. CA: REPAIRED VERTICAL STAB DAMAGE IAW MHIRJ REO 690-55-31-067 REV. A DATED 2022-04-16.
Part: SKIN — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR INNER SKIN CORRODED IN MULTIPLE PLACES CA: REMOVED ANGLE FROM PAX DOOR UPPER CENTER SKIN, REMOVED CORROSION, INSTALLED ANGLE IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-21-06-001-001-A01 REV. 38, (7/25/20). REMOVED INNER DOOR SKIN, LOCATED, DRILLED, DEBURRED IAW CRJ-900 SRM 51-40-11-001-001-A01, INSTALLED INNER SKIN IAW CRJ-900 SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01 REV. 38 (7/25/20).
Part: FRAME — CORRODED · airframe 29,718 hrs · 21,194 cycles
F.S. 265.00 FRAME IS CORRODED BETWEEN STGR 27 TO STGR 26R. CA: COMPLIED WITH ENDEAVOR EA CRJ953-12983, REV. B DATED 4/23/22.
Part: PANEL — CORRODED · airframe 29,718 hrs · 21,194 cycles
PASSENGER DOOR STEPS TOP PANEL IS CORRODED AROUND SCREW HOLES. CA: PAX DOOR TOP STEP PANEL BLENDED, FOUND TO BE OUT OF LIMITS, LOCATED DRILLED NEW PANEL PN: 601R317075-3 AND INSTALLED IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-01-001-A01 REV. 38 (7-25-21), 51-21-06-001-001-A01.
Part: FRAME — CORRODED · airframe 29,718 hrs · 21,194 cycles
FS250 FRAME IS CORRODED BETWEEN STGR 26R TO STGR 26L. REPAIRED FS250 FRAME IAW ENDEAVOR AIR EA CRJ953-13199 REV-IR DATED 3/26/2022
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
LH AND RH FWD JACK PAD FITTING ANGLE CORRODED. CA: REMOVED AND REPLACED FITTING ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-00-001-001-A01.
Part: FITTING — CORRODED · airframe 29,718 hrs · 21,194 cycles
LH AND RH FWD JACK FITTING SUPPORTS ARE CORRODED. CC670-32179-3 & CC670-32179-4 CA: REMOVED AND REPLACED LH AND RH SUPPORTS IAW ENDEAVOR EA CRJ953-13164 AND CRJ953-13165, REV IR, DATED 3/25/2022.
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
FS265/STR27 STIFFENING ANGLE PN: CC670-34104-1 CORRODED. CA: REMOVED AND REPLACED ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
CRAWLWAY FLOOR ANGLE SUPPORT AT FS 280 CORRODED. CA: REMOVED AND REPLACED SUPPORT ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01AND 51-40-11-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 29,718 hrs · 21,194 cycles
3EACH FWD INTERCOSTALS ARE CORRODED AT AVIONICS DOOR SURROUNDING STRUCTURE FS 349.00-364.00, STR26L-26R. CA: REMOVED AND REPLACED INTERCOSTALS IAW CRJ 900SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, 53-21-23-001-003-A01 AND 51-42-06-001-001-A01. (2EA) SH670-32075-4S & (1EA) SH670-32077-3S
Part: INTERCOSTAL — CRACKED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR INTERCOSTAL DD1 IS CRACKED. CA: REMOVED AND REPLACED INTERCOSTAL IAW CRJ 900SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
Part: LUG — DAMAGED · airframe 29,718 hrs · 21,194 cycles
LH AILERON LUG MARKED "F" HAS DAMAGE TO BORE. CA: REPAIRED BORE AND REPLACED BUSHING IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25.
Part: LUG — DAMAGED · airframe 29,718 hrs · 21,194 cycles
RH AILERON LUG MARKED "C" HAS DAMAGE TO BORE. CA: REPAIRED BORE AND REPLACED BUSHING IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25.
Part: YOKE — CHAFED · airframe 29,718 hrs · 21,194 cycles
LH FORWARD ENGINE MOUNT HAS CHAFING. CA: REPAIRED IAW BOMBARDIER REO 670-71-21-057 REV-- DATED 2013-09-13 AND MHIRJ REO 690-71-21-038 REV -- DATED 2022-03-27.
Part: YOKE — CHAFED · airframe 29,718 hrs · 21,194 cycles
RH FORWARD ENGINE MOUNT HAS CHAFFING. CA: REPAIRED IAW BOMBARDIER REO 670-71-21-057 REV-- DATED 2013-09-13 AND MHIRJ REO 690-71-21-039 REV A DATED 2022-04-01.
Part: CLEAT — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR INTERCOSTAL DD6 & CLEAT CORRODED. CA: REMOVED AND REPLACED INTERCOSTAL & CLEAT IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR INTERCOSTAL DD6 & CLEAT CORRODED. CA: REMOVED AND REPLACED INTERCOSTAL & CLEAT IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01.
Part: NONE — CRACKED · airframe 29,718 hrs · 21,194 cycles
RH FWD EQUIPMENT COMPARTMENT FLOOR SILL (DOOR LANDING) ABOVE AFT LATCH & ATTACH CLIP ARE CRACKED. CA: REMOVED & REPLACED LANDING IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. REMOVED, FABICATED & REPLACED CLIP IAW CRJ 900 SRM 51-24-21-001-001-A01 & 51-42-10-001-001-A01
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR OUTER HANDLE ASSY ANGLE CORRODED P/N 61R317052-1 CA: REMOVED & REPLACED ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A01
Part: FORMER — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR FORMER @ FS 329.41 CORRODED. CA: REMOVED & REPLACED FORMER IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-06-001-001-A01
Part: ANGLE — CRACKED · airframe 29,718 hrs · 21,194 cycles
RH FWD EQUIPMENT COMPARTMENT FLOOR SILL (DOOR LANDING) ABOVE AFT LATCH & ATTACH ANGLE ARE CRACKED. CA: REMOVED & REPLACED LANDING IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-42-10-001-001-A01. REMOVED, FABICATED & REPLACED ANGLE IAW CRJ 900 SRM 51-24-21-001-001-A01 & 51-42-10-001-001-A01
Part: NONE — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR DD7 INTERCOSTAL CLIP IS CORRODED. CA: REMOVED, FABRICATED & REPLACED CLIP IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 & 51-24-16-001-001-A01.
Part: ANGLE — CRACKED · airframe 29,718 hrs · 21,194 cycles
LH AFT VERTICAL STAB DRAG ANGLE IS CRACKED. CA: REMOVED & REPLACED DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01, 51-22-00-001-001-A01 & 51-42-13-001-001-A01.
Part: ANGLE — CRACKED · airframe 29,718 hrs · 21,194 cycles
RH AFT VERTICAL STAB DRAG ANGLE IS CRACKED. CA: REMOVED & REPLACED DRAG ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-22-001-001-A01, 51-42-21-001-001-A01, 51-22-00-001-001-A01 & 51-42-13-001-001-A01.
Part: PLATE — CORRODED · airframe 29,718 hrs · 21,194 cycles
GALLEY 1 FORWARD INBOARD AND OUTBOARD MOUNTS CORRODED. CA: REMOVED AND REPLACED GALLEY 1 INBOARD AND OUTBOARD MOUNT PLATES IAW CRJ 900 SRM 51-40-11-001-001-A01 & 51-42-21-001-001-A04
Part: NONE — CORRODED · airframe 29,718 hrs · 21,194 cycles
RH FLOOR SILL HAS MINOR CORROSION BETWEEN FS295.00 AND FS 310.00 CA: REMOVED CORROSION I.A.W. CRJ SRM #51-21-06-001-001-A01,SILL FOUND TO BE SERVICEABLE I.A.W #53-00-45-201-001-A01, FINISH AND CIC RESTORED.
Part: SEAT TRACK — CORRODED · airframe 29,718 hrs · 21,194 cycles
RH CABIN SIDE SEAT TRACK CORRODED FS847+31 CA: REMOVED AND REPLACED IAW CRJ 900 AMM 53-00-49-400-801-A11
Part: NONE — CRACKED · airframe 29,718 hrs · 21,194 cycles
FS. 280 RBL 9 OB CLIP CRACKED CA: REPLACED RBL. 9 FS.280. CLIP IAW CRJ 900 SRM 51-40-11-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 29,718 hrs · 21,194 cycles
CABIN FLOOR SEAT TRACK LBL9 IS CORRODED F.S.375 TO F.S.379 CA: REMOVED AND REPLACED IAW 53-00-49--400-80-A11
Part: FRAME — CORRODED · airframe 29,718 hrs · 21,194 cycles
PAX DOOR FRAME AT FS327.763 CORRODED. CA: REMOVED AND REPLACED FRAME IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-22-00-001-001-A01.
Part: SEAT TRACK — CORRODED · airframe 29,718 hrs · 21,194 cycles
RH CABIN SIDE SEAT TRACK CORRODED FS629 TO FS661 CA: REMOVED AND REPLACED IAW 53-00-49-400-801-A11
Part: SEAT TRACK — CORRODED · airframe 29,718 hrs · 21,194 cycles
RH CABIN SIDE SEAT TRACK CORRODED FS744 TO FS752 CA: REMOVED AND REPLACED IAW 53-00-49-400-801-A11
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS HAVE SIGNS OF CORROSION. CA: REPLACED SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-36-001-001-A01, 51-40-11-001-001-A01, AND AMM 53-21-27-400-802-A02.
Part: BUTTSTRAP — CORRODED · airframe 29,718 hrs · 21,194 cycles
FS280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 24R TO STGR 26R CA: REPAIRED IAW ENDEAVOR EA CRJ953-13136 REV IR, DATED: 3/17/2022.
Part: FITTING — CORRODED · airframe 29,718 hrs · 21,194 cycles
SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS HAVE SIGNS OF CORROSION. CA: REPLACED SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-36-001-001-A01, 51-40-11-001-001-A01, AND AMM 53-21-27-400-802-A02.
Part: WEB — CORRODED · airframe 29,718 hrs · 21,194 cycles
SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS HAVE SIGNS OF CORROSION. CA: REPLACED SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-36-001-001-A01, 51-40-11-001-001-A01, AND AMM 53-21-27-400-802-A02.
Part: FRAME — CORRODED · airframe 29,718 hrs · 21,194 cycles
INTERCOSTAL (LOWER STUB FRAME) CORRODED AT FS 549.00 BETWEEN STGR 25L AND STGR 26L. CA: REMOVED & REPLACED LOWER STUB FRAME IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-20-001-001-A01 & 51-42-13-001-001-A01.
Part: PLATE — CORRODED · airframe 29,718 hrs · 21,194 cycles
DOUBLER PLATE AT FS 565.00,BETWEEN 25L AND 26L CORRODED CA: REMOVED & REPLACED DOUBLER PLATE IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 & 51-42-27-001-001-A01.
Part: ANGLE — CORRODED · airframe 29,718 hrs · 21,194 cycles
SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS HAVE SIGNS OF CORROSION. CA: REPLACED SERVICE DOOR SEAL STRIKER, UPPER ANGLE, LOWER ANGLE, AND BOTH CENTER FITTINGS IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-36-001-001-A01, 51-40-11-001-001-A01, AND AMM 53-21-27-400-802-A02.
Part: FRAME — CORRODED · airframe 29,718 hrs · 21,194 cycles
INTERCOSTAL (LOWER STUB FRAME) CORRODED AT FS 533.00 BETWEEN STGR 25L AND STGR 26L. CA: REMOVED & REPLACED LOWER STUB FRAME IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-20-001-001-A01 & 51-42-13-001-001-A01.
Part: INTERCOSTAL — CORRODED · airframe 29,718 hrs · 21,194 cycles
FS310 TO FS319 STR20R INTERCOSTAL IS CORRODED CA: REPLACED STR20R INTERCOSTAL IAW SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED · airframe 29,718 hrs · 21,194 cycles
FS295 TO FS310 STR20R IS CORRODED CA: REPLACED STR20R IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 29,718 hrs · 21,194 cycles
INTERCOSTAL CORRODED AT FS645 BETWEEEN STR25L AND 26L CA: REMOVED AND REPLACED STUB FRAME IAW SRM 51-42-21/22/27-001-001-A01
Part: NONE — NONE · airframe 29,718 hrs · 21,194 cycles
CABIN FLOOR SEAT TRACK RBL 9.0 CORRODED F.S.364 TO 379. CA: REPLACED SEAT TRACK AT RBL 9 FS. 349 TO 485 IAW CRJ900 AMM 53-00-49-000/400-801-A11.
Part: STRINGER — CORRODED · airframe 29,718 hrs · 21,194 cycles
FS295 TO FS310 STR19R IS CORRODED CA: REPLACED STR20R IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
Part: INTERCOSTAL — CORRODED · airframe 29,718 hrs · 21,194 cycles
INTERCOSTAL CORRODED AT FS661 BETWEEN ST25L AND 26L CA: REMOVED AND REPLACED STUB FRAME IAW SRM 51-42-21-001-001-A01
Part: NONE — CORRODED · airframe 29,718 hrs · 21,194 cycles
LH SIDE SEAT TRACK FS 661+16-677 IS CORRODED.
Part: NONE — CORRODED · airframe 29,718 hrs · 21,194 cycles
LH SIDE SEAT TRACK FS 784-847+14 IS CORRODED.
2020
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,823 hrs · 18,673 cycles
DURING FIRST FLIGHT WAKE UP, NOTED 2 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW AMM 33-51-17, OPS CHECKED GOOD.
2018
Part: FLAP — CRACKED (PAX DOOR HANDLE) · airframe 22,987 hrs · 15,815 cycles
MAIN ENTRY DOOR EXTERIOR PULL HANDLE PUSH IN FLAP WAS CRACKED AND BENT IN THE FORWARD LOWER CORNER OF THE FLAP. REPAIRED THE FLAP COVER IAW SRM 51-12-00 AND 52-00-01.
Part: POST — CORRODED (BS 280) · airframe 22,987 hrs · 15,815 cycles
FOUND CORROSION ON THE RBL 12 VERTICAL POST, IN THE E & E BAY AT BS 280. REPAIRED THE VERTICAL POST IAW EA CRJ953-07439.
Part: BRACKET — CRACKED (LEFT WING SLAT) · airframe 22,987 hrs · 15,815 cycles
LEFT WING INTERNAL SLAT CAN 1-3 HAD A CRACKED BRACKET. REPAIRED THE BRACKET IAW REO 670-57-42-577, OPS TESTED GOOD IAW AMM 27-50-00-710-801.
Part: ANGLE — CORRODED (BS 379-394) · airframe 22,987 hrs · 15,815 cycles
STRINGER 23R, LAVATORY PAN LOWER ANGLE WAS CORRODED BS 379 - 394. REMOVED AND REPLACED THE LAVATORY PAN ANGLE AT STRINGER 23R IAW SRM 51-42-06, AND SRM 51-42-21.
Part: STRINGER — CORRODED (AVIONICS BAY) · airframe 22,987 hrs · 15,815 cycles
AVIONICS BAY STRINGER 26R WAS CORRODED FROM BS 333 TO 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-21.
Part: FRAME — CORRODED (ANIONICS BAY) · airframe 22,987 hrs · 15,815 cycles
AVIONICS BAY FRAME WAS CORRODED AT BS 333, STRINGERS 26L TO 26R. REPLACED THE FRAME SECTION AND SPLICES IAW SRM 53-00-06.
Part: BRACKET — CRACKED (RIGHT WING SLAT) · airframe 22,987 hrs · 15,815 cycles
RIGH WING INTERNAL SLAT CAN 1-3 HAD A CRACKED BRACKET. REPAIRED THE BRACKET IAW REO 670-57-42-577. OPS TESTED THE FLAPS AND SLATS SYS, CHECKED GOOD IAW AMM 27-50-00-710-801.
Part: STRINGER — CORRODED (BS 280-333) · airframe 22,987 hrs · 15,815 cycles
STRINGER 25R, FOUND CORRODED BETWEEN BS 280 - 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06.
Part: STRINGER — CORRODED (BS 333-364) · airframe 22,987 hrs · 15,815 cycles
AVIONICS BAY STRINGER 26R WAS CORRODED FROM BS 333 TO 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-21.
Part: STRINGER — CORRODED (BS 280-333) · airframe 22,987 hrs · 15,815 cycles
E & E BAY HAD CORROSION ON STRINGER 26R, BS 280 - 333. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-11.
Part: FAIRING — CRACKED (NR 2 PYLON) · airframe 22,987 hrs · 15,815 cycles
DURING REMOVAL OF THE NR 2 ENGINE PYLON TIE BAR K FRAME, FOUND THE UPPER, AFT HINGE LINE FAIRING TO BE CRACKED AT A SCREW HOLE. REMOVED & REPLACED THE FAIRING IAW SRM 51-42-06, AND 51-42-13.
Part: FRAME — CORRODED (BS 310) · airframe 22,987 hrs · 15,815 cycles
AVIONICS BAY FRAME WAS CORRODED AT BS 310 NEAR STRINGER 26L - 24R. REPAIRED THE LOWER SECTION OF BS 310 FRAME IAW EA CRJ 953-07438, REV IR.
Part: STRINGER — CORRODED (BS 333) · airframe 22,987 hrs · 15,815 cycles
CORROSION FOUND ON FWD STRINGER 23R, BS 333. REPLACED THE STRINGER AND SPLICE IAW SRM 51-42-06.
Part: FRAME — CORRODED (BS 319) · airframe 22,987 hrs · 15,815 cycles
AVIONICS BAY FRAME WAS CORRODED AT BS 319, STRINGERS 24 - 27R. REPAIRED THE FRAME IAW SRM 53-00-06.
Part: FRAME — CORRODED (BS 295) · airframe 22,987 hrs · 15,815 cycles
AVIONICS BAY FRAME WAS CORRODED AT BS 295, STRINGERS S26L TO S26R. REPAIRED THE FRAME IAW SRM 53-00-06.
Part: STRINGER — CORRODED (BS 634-394) · airframe 22,987 hrs · 15,815 cycles
WHILE REMOVING THE LAVATORY PAN ANGLE, FOUND CORROSION ON STRINGER 24R, BETWEEN BS 364 - 394. REPAIRED THE STRINGER IAW SRM 53-00-03-201-001-A02.
Part: NOT REPORTED — CORRODED (BS 280) · airframe 22,987 hrs · 15,815 cycles
E & E BAY HAS CORROSION AT BS 280, STRINGERS 24R TO 24L. REMOVED CORROSION IAW EA CRJ953-07443.
Part: SEAT TRACK — CORRODED (BS 744-761) · airframe 22,987 hrs · 15,815 cycles
LEFT SEAT TRACK BETWEEN OVERWING EMERGENCY EXIT DOORS, CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801.
Part: ANGLE — CORRODED (DOOR FRAME) · airframe 22,987 hrs · 15,815 cycles
BS 280 DOOR FRAME RT LWR ANGLE WAS CORRODED. REMOVED AND REPLACED THE IAW SRM 51-42-06.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,987 hrs · 15,815 cycles
LEFT SEAT TRACK NR 5 WAS CORRODED AND CORRODED HARDWARE THROUGHOUT SECTION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: POST — CORRODED (DOOR) · airframe 22,987 hrs · 15,815 cycles
FOUND CORROSION ON THE BS 280, LBL 11 DOOR POST. REMOVED THE CORROSION AND FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-11-10.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 22,987 hrs · 15,815 cycles
LEFT SIDE SEAT TRACK NR 7 WAS CORRODED AND HAD CORRODED HARDWARE THROUGHOUT THE SECTION. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW AMM 53-00-49-400-801.
Part: BULKHEAD — CORRODED (BS 280) · airframe 22,987 hrs · 15,815 cycles
CORROSION FOUND ON THE BS 280 LOWER BULKHEAD RBL 8 TO LBL 8. REPAIR THE BULKHEAD IAW REO 690-53-11-1085.
Part: STRINGER — CORRODED (BS 280-295) · airframe 22,987 hrs · 15,815 cycles
WHILE REMOVING CORROSION AT BS 280, IN THE E & E BAY, FOUND STRINGER 27 CORRODED, BETWEEN BS 280 - 295. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06, AND SRM 51-42-21.
Part: STRINGER — CORRODED (BS 364-379) · airframe 22,987 hrs · 15,815 cycles
CORROSION FOUND ON FWD STRINGER 23R, BS 364 - 379. REPLACED THE FWD STRINGER AND SPLICE IAW SRM 51-42-06.
Part: POST — CORRODED (DOOR) · airframe 22,987 hrs · 15,815 cycles
BS 280, RBL 11, DOOR POST WAS CORRODED. REMOVED THE CORROSION, AND FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-11-10.
Part: ANGLE — CORRODED (BS 280 DR FRAME) · airframe 22,987 hrs · 15,815 cycles
BS 280 DOOR FRAME LT LOWER ANGLE WAS CORRODED. REMOVED AND REPLACED WITH THE ANGLE AND GUSSET IAW SRM 51-42-06.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 22,987 hrs · 15,815 cycles
LEFT SEAT TRACK NR 4 WAS CORRODED, HARDWARE CORRODED THROUGHOUT THE SECTION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 22,987 hrs · 15,815 cycles
LEFT BS 280 FLOORBEAM WAS CORRODED. REMOVED AND REPLACED IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-10, AND COMPLIED WITH EA CRJ95307419, REV IR.
Part: LANDING — CRACKED (ACCESS PANEL) · airframe 22,987 hrs · 15,815 cycles
DURING GVI OF THE LT INBD FLAP VANE, FOUND A CRACKED ACCESS PANEL LANDING. REMOVED AND REPLACED THE ACCESS PANEL LANDING ON THE INBD FLAP VANE IAW SRM 51-42-13.
Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 22,987 hrs · 15,815 cycles
LEFT AISLE SEAT TRACK NR 1, HAD CORROSION BETWEEN BS 364 AND 485, IN THE CABIN. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49 400-801, AND 53-00-49-000-801.
Part: BULKHEAD WEB — CORRODED (BS 280) · airframe 22,987 hrs · 15,815 cycles
WHILE REMOVING THE BS 280 FLOORBEAM, FOUND BULKHEAD WEB CORRODED. REPLACED THE LOWER BULKHEAD WEB IAW SRM 53-11-10.
Part: FITTING — CRACKED (BS 280) · airframe 22,987 hrs · 15,815 cycles
BS 280, LINTEL 3L WAS CRACKED. REPAIRED IAW REO 670-53-21-493, REV D.
Part: BATTERY — INOPERATIVE (CKPIT FLASHLIGHT) · airframe 22,541 hrs · 15,490 cycles
FIRST OFFICER'S FLASHLIGHT NOT BLINKING. REMOVED AND REPLACED THE FIRST OFFICER'S FLASHLIGHT BATTERY. OPS CHECKED GOOD IAW AMM 25-61-00.
Part: FLASHLIGHT — INOPERATIVE (MAIN CABIN) · airframe 22,837 hrs · 15,287 cycles
FLASHLIGHT NEAR MAIN CABIN DOOR IS NOT BLINKING. R & R THE FLASHLIGHT IAW AMM 25-61-02. ACFT OK FOR SERVICE.
Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 22,135 hrs · 15,203 cycles
OBSERVER O2 MASK HARNESS DOESNT TEST, POSSIBLE LEAK. R&R OBS O2 MASK REF AMM 35-11-12. OPS CHECK AND LEAK CHECK GOOD REF AMM 35-10-00, AND AMM 23-51-00 P/N ON/OFF MF10-08-01 S/N OFF 108427 S/N ON 108338I.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 21,788 hrs · 14,956 cycles
WHEN THE EMERGENCY LIGHT SWITCH IS PLACED IN THE ARMED POSITION, THE EMERGENCY LIGHTS COME ON AND WON'T GO OFF. PERFORMED A RESET PROCEDURE, ALL CHECKS WERE NORMAL IAW AMM 33-51-00.
Part: MEGAPHONE — INOPERATIVE (MAIN CABIN) · airframe 21,755 hrs · 14,935 cycles
MEGAPHONE ALARM DOES NOT SOUND WHEN PIN IS PULLED. R & R THE MEGAPHONE IAW EE-900.
2017
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,633 hrs · 14,852 cycles
RIGHT AFT EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE LAMP OPS CHECKED SATISFACTORY IAW AMM 33-51-15.
Part: AED — INOPERATIVE (MAIN CABIN) · airframe 21,605 hrs · 14,832 cycles
FLIGHT ATTENDANT FOUND AED FLASHING RED INSTEAD OF GREEN DURING PREFLIGHT CHECK. REMOVED & REPLACED THE AED IAW 256000.
Part: COVER — CRACKED (RT SLAT TRACK) · airframe 21,270 hrs · 14,588 cycles
RIGHT WING SLAT TRACK COVER IS CRACKED AT THE OTBD FWD FASTENER HOLE. REMOVED AND REPLACED THE SLAT TRACK COVER IAW SRM 51-41-02.
Part: SKIN — DENTED (RUDDER) · airframe 21,270 hrs · 14,588 cycles
RUDDER HAS TWO DENTS ON THE LEFT SIDE ABOUT MIDWAY. REPAIRED THE RUDDER SKIN IAW SRM 55-41-01-201-001-A01.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 21,270 hrs · 14,588 cycles
AFTER REMOVAL OF PAX DOOR DRAG ANGLE CRACKED SECTION FOUND AFT SIDE PANEL CRACKED AT ASSIST MOTOR SUPPORT. REPAIRED PAX DOOR DRAG ANGLE AFT (PANEL) IAW EA # CRJ952-06087 AAR EMP 8930
Part: INTERCOSTAL — CORRODED (BS 364) · airframe 21,172 hrs · 14,517 cycles
DURING ZONAL INSPECTION FOUND INTERCOSTAL WITH SUFACE CORROSION 27L AND RT AND 26L AT BS 364. THE INTERCOSTAL WAS REPLACED.
Part: ATTACH ANGLE — CORRODED (BS 364) · airframe 21,172 hrs · 14,517 cycles
DURING ZONAL INSPECTION, FOUND THE INTERCOSTAL WITH SURFACE CORROSION STRINGER 27L AND RT AND 26LT, BS 364. THE ATTACH ANGLE AT STRINGER 26L WAS REPLACED.
Part: INTERCOSTAL — CORRODED (BS 364) · airframe 21,172 hrs · 14,517 cycles
DURING A ZONAL INSPECTION, FOUND THREE INTERCOSTALS WITH SURFACE CORROSION 27 LT AND RT AND 26 LT AT BS 364. THE INTERCOSTAL WERE REPLACED AND THE LAV SPILL WAS CLEANED AND INSULATION WAS REPLACED.
Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 20,725 hrs · 14,178 cycles
SMOKE IN CABIN & COCKPIT AFTER TAKEOFF. IMMEDIATELY RETURNED FOR LANDING. PERFORMED OPS TEST OF AIR CONDITION SYS IAW AMM 21-51-00. OPS CHECKED GOOD.
2016
Part: GLOWSTRIP — MISSING (CABIN) · airframe 18,707 hrs · 12,811 cycles
FORWARD GLOWSTRIP MISSING AT PASSENGER EMERGENCY EXIT ROW LOCATION 12AB. INSTALLED A NEW GLOWSTRIP IAW AMM 33-51-01.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,781 hrs · 12,133 cycles
MISSING EXIT SIGN IN GALLEY. REPLACED MISSING FLOOR LEVEL EMERGENCY FLOOD LIGHT LENS COVER AFT OF SERVICE DOOR IAW AMM 33-51-11. NO FURTHER DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 17,040 hrs · 11,626 cycles
MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14. REF IPC 25-61-14, FIG 1, ITEM 5.
2015
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 15,828 hrs · 10,754 cycles
TWO EMERGENCY LIGHTS INOPERATIVE OVER LT WING. SECURED THE CONNECTOR P5300 IAW ESPM 20-26-00. OPS CHECKED GOOD IAW AMM 33-51-00.
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 15,804 hrs · 10,730 cycles
MIDDLE CARGO DOOR SEAL RETAINER DAMAGED ON INBD EDGE. PERFORMED PERMANENT REPAIR IAW EC/TC REO 690-52-35-013, REV B.
Part: SEAT TRACK — CORRODED (BS 744-752) · airframe 15,239 hrs · 10,348 cycles
LT SIDE SEAT RAIL AT BS 744-752 CORRODED. COMLIED WITH BA-00-49-000-801-A11, 53-00-49-400-801-A11.
Part: SEAT TRACK — CORRODED (BS 847-988) · airframe 15,239 hrs · 10,348 cycles
SEAT RAILS AT LBL9 847+16-988 HAS MULTIPLE SPOTS OF CORROSION. CORROSION OUT OF LIMITS IAW REO 670-53-00-013 ON LBL 9, SEAT RAIL 847+988. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801 CONFIGURATION A11. INSTALLED SERVICABLE SEAT RAIL AT LBL9 847+16-988 IAW AMM 58-00-49-400-801-A11, IPC REF 53-00-49, IAW 180.
Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 15,238 hrs · 10,347 cycles
SEAT RAIL AT RBL9, FS 661+32-FS 677 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE PREVIOUSLY BLENDED IAW GREO 670-53-00-013 OUT OF LIMITS. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. REMOVED SEAT RAIL IAW AMM 53-00-49-000-801-A01. INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801-A11, SERVICEABLE.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 15,239 hrs · 10,348 cycles
SEAT RAIL AT RBL9, FS 485-FS581 HAS CORROSION IN MULTIPLE AREAS, FOUND TO BE PREVIOUSLY BLENDED IAW GREO 670-53-00-013 OUT OF LIMITS. R & R SEAT TRACK IAW AMM 53-00-49-000-801-A11, 53-00-49-400-801-A11.
Part: DOOR SILL — CORRODED (EMERGENCY EXIT) · airframe 15,239 hrs · 10,348 cycles
SUB SILL OF LT EMERGENCY EXIT DOORS SILL CORRODED IN MULTIPLE AREAS FS 752-760 + FS 720-744. REMOVED CORROSION FROM AREAS ON SUB SILL OF LT EMERGENCY EXIT DOOR SILL IAW SRM 51-21-06-001-001-A01. COMPLIED WITH EA 32-2015-118, REV. RECEIVED ECTC EA 32-2015-118 AND COMPLIED WITH ALL STEPS AS REQUIRED.
Part: SEAT TRACK — CORRODED (BS 581-611) · airframe 15,238 hrs · 10,347 cycles
SEAT RAIL AT RBL 9, FS581-FS 661+32 HAS CORROSION IN MULTIPLE AREAS. FOUND TO BE PREVIOUSLY BLENDED IAW GREO 670-53-00-013 OUT OF LIMITS. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801-A11, SERVICEABLE. R & R SEAT TRACK AT RBL 9, FS 581 - 661+32 IAW ECTC REO 670-53-00-343 AND REO 670-53-00-343.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,238 hrs · 10,347 cycles
AVIONICS FLOORBOARD SUPPORT ANGLE AT BS 280 CORRODED. REMOVED CORROSION ON FLOOR SUPPORT ANGLE AT BS 280 IAW SRM 51-21-06-001-001-A01 FOUND TO BE OUT OF LIMITS IAW SRM 53-22-55-101-001-A01. REMOVED ANGLE SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW FLOOR SUPPORT ANGLE AT STA 280.00 IAW SRM 51-42-06-001-001-A01, 51-42-15-001-001-A01 AND 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 349-477) · airframe 15,238 hrs · 10,347 cycles
SEAT RAILS AT RBL9, BS 349 TO 477.40 HAS SEVERAL SPOTS OF CORROSION. REMOVED CORRODED SEAT RAIL AT RBL9 FROM FS FS349-FS477.40 IAW AMM 53-00-49-000-801-A11. INSTALLED NEW SEAT RAIL ON BRL9 FROM FS349-FS477.40 IAW AMM 53-00-49-400-801-A11 IPC53-00-49-ITEM 280. INSTALLED 3 EA SEAT TRACK FITTING ASSY'S IAW AMM 20-21-00-910-810 AO1. OUT OF SEQUINCE CORROSION FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 661-677) · airframe 15,238 hrs · 10,347 cycles
SEAT RAILS AT LBL 9, BS 661+32 - 677 HAS SEVERAL SPOTS OF CORROSION. REMOVED SEAT RAIL AT LBL9, FS 661+32FS677 IAW AMM 53-00-49-000-801-A11. INSTALLED NEW FABRICATED SEAT RAIL AT LBL9, FS 661+32 - FS 677 IAW AMM 53-00-49-400-801-A11. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. FOUND SEAT RAIL TO BE PREVOUSLY BLENDED OUT OF LIMITS IAW REO 670-53-00-013.
Part: COVER — DIRTY (EMERGENCY LIGHT) · airframe 15,238 hrs · 10,347 cycles
CLEAN AND EVALUATE PHOTOLUMINESCENT LIGHT TRACK. CLEANED AND EVALUATED PHOTOLUMINESCENT LIGHT TRACK IAW AMM 51-26-00-110-801-A01. REPLACED 19 EA SECTIONS OF TRACK COVERS AND 2 EA SECTIONS OF LIGHT TRACK BY CUTTING TO FIT DAMAGED SECTIONS.
Part: SEAT TRACK — CORRODED (BS 677-847) · airframe 15,238 hrs · 10,347 cycles
SEAT RAILS AT RBL9 BS 677 - 847+16 HAS SEVERAL SPOTS OF CORROSION. FOUND SEAT RAIL TO BE OUT OF LIMITS REO 670-53-00-013. REMOVED SEAT RAIL AT RBL9 BETWEEN FS 677-847+16 IAW AMM 53-00-49-000-801-A11. INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801-A11, SERVICEABLE. COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV J AS WRITTEN. SDR CLOSED.
Part: SEAT TRACK — CORRODED (BS 847-988) · airframe 15,238 hrs · 10,347 cycles
SEAT RAILS AT RBL 9, BS 847+16 - 988 HAS SEVERAL SPOTS OF CORROSION. COMPLIED WITH REO 670-53-00-013, REV J. COMPLIED WITH ECTC REO 670-53-00-013 AND GREO 670-53-00-013 REV J, DATED 10/22/2014 AS WRITTEN.
Part: SEAT TRACK — CORRODED (BS 581-693) · airframe 15,238 hrs · 10,347 cycles
SEAT RAILS AT LBL 9, BS 581 - 693 HAS SEVERAL SPOTS OF CORROSION. EVALUATED SEAT RAIL AT LBL9, BS 581 TO 661+32 TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED SEAT RAIL AT LBL9, FS 581 TO FS 661+32 IAW AMM 53-00-49-000-801-A11. INSTALLED SEAT RAIL IAW AMM 53-00-49-400-801-A11 SERVICEABLE. COMPLIED WITH REO 670-53-343 AND GREO 670-53-00-343, REV J AS WRITTEN.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,238 hrs · 10,347 cycles
COCKPIT FLOOR PANEL AFT SUPPORT HAS CORROSION. REMOVED COCKPIT FLOOR PANEL, AFT SUPPORT REF: SRM 51-42-06-001-001-A01 IN ORDER TO EVALUATE CORROSION DAMAGE FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. INSTALLED NEW COCKPIT AFT FLOOR SUPPORT AT FS280, LBL9 & RBL9, WL71.10 IAW SRM 51-42-06-001-001-A01 DWG CC670-34010, REV K. LOCATED DRILLED AND DEBURRED FASTENER HOLES ON NEW AFT COCKPIT FLOOR. SUPPORT IAW SRM 51-40-11-001-001-A01. INSTALLED RECEPTACLES FOR CAM LOCS ON AFT COCKPIT FLOOR SUPPORT IAW SRM 51-45-06-001-001-A01.
2014
Part: RETAINER — DAMAGED (CARGO DOOR SEAL) · airframe 13,356 hrs · 9,075 cycles
AFT CARGO DOOR HAS DAMAGED SEAL RETAINER. WORK ACCOMPLISHED IAW REO 690-52-35-013, REV A. MAJOR REPAIR IAW GMM 5-3.
Part: RETAINER — DAMAGED (DOOR SEAL) · airframe 13,356 hrs · 9,075 cycles
FWD DOOR HAS DAMAGED SEAL RETAINER. WORK ACCOMPLISHED IAW REO 690-52-35-013, REV. A. MAJOR REPAIR IAW GMM 5-3.
Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 12,417 hrs · 8,466 cycles
FWD F/A FLASHLIGHT INOPERATIVE. R & R FWD FLASHLIGHT BATTERIES IAW AMM 25-61-00. OP TESTED GOOD.
2013
Part: RETAINER — GOUGED (CARGO DOOR SEAL) · airframe 11,735 hrs · 8,056 cycles
FWD CARGO DOOR LOWER SEAL RETAINER GOUGED ON FWD AND AFT ENDS. BLENDED FWD CARGO DOOR LOWER SEAL RETAINER IAW REO 690-52-35-013, REO 690-52-35-013, REV B DATED 13SEPT2013.
Part: RETAINER — GOUGED (CARGO DOOR) · airframe 11,735 hrs · 8,056 cycles
MID CARGO DOOR LOWER SEAL RETAINER GOUGED ON FWD AND AFT ENDS. BLENDED MID CARGO DOOR LOWER SEAL RETAINER IAW REO 690-52-35-013, REV A, DATED 17FEB2009 AND REO 690-52-35-013, REV B.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 11,735 hrs · 8,056 cycles
LT COCKPIT FLOORBEAM CRACKED AT LBL 12. REMOVED DAMAGED AREA AND SPLICED IN NEW BEAM IAW REO 690-53-11-606, & EC/TC 690-53-11-606.
Part: FLOORBEAM — CRACKED (ZONE 100) · airframe 11,735 hrs · 8,056 cycles
RIGHT COCKPIT FLOORBEAM CRACKED AT RBL 12. REPAIRED RT FLOORBEAM IAW REO 690-53-11-606 AND EC/TC 690-53-11-606.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 11,735 hrs · 8,056 cycles
RT SIDEWALL SEAT TRACK BETWEEN THE EMERGENCY EXITS, FS 744 TO 761 IS CORRODED. R & R SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 11,735 hrs · 8,056 cycles
RT WALL SEAT TRACK FROM FS 785 TO 847+16 HAS SEVERAL SPOTS OF CORROSION. R & R RT SIDEWALL SEAT TRACK IAW AMM 53-00-49.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 11,735 hrs · 8,056 cycles
AFT CARGO BAY FLOORBEAM AT FS 1036, LBL 26 HAS TWO CORRODED AREAS. CUT OUT DAMAGED SECTION. FABRICATED NEW SECTION AND REPAIR PARTS. INSTALLED NEW SECTION & REPAIR PARTS IAW REO 670-53-00-029, REV A. NDT ACCOMPLISHED. MAJOR REPAIR.
Part: THRESHOLD — CORRODED (ZONE 200) · airframe 11,735 hrs · 8,056 cycles
MAIN PASSENGER DOOR THRESHOLD MID CAP CORRODED. R & R MAIN PASSENGER DOOR MID CAP IAW SRM 51-42-06 AND 51-42-20.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,735 hrs · 8,056 cycles
FLOORBEAM AT FS 280 IS CORRODED BEYOND LIMITS. R & R FLOORBEAM IAW SRM 51 AND 21-11, 25-16, 40-11, 42-06, 42-13, & 42-21, 42-22.
Part: BULKHEAD WEB — CORRODED (ZONE 200) · airframe 11,735 hrs · 8,056 cycles
LEFT BULKHEAD AT BS 280 AFT LOWER WEB IS CORRODED OUT OF LIMITS. REMOVED SECTION OF THE WEB. FABRICATED LOWER WEB AND STRAP AND INSTALLED IAW REO 670-53-11-594 REV, DATED 27 APR 2011 AND EC/TC REO 670-53-11-594 01, REV.A, DATED 19 MAY 2011.
Part: STRAP — CORRODED (ZONE 100) · airframe 12,874 hrs · 8,540 cycles
THE "QUARTER TURN" STRAP OF THE FS 280 BEAM HAS CORROSION. R & R STRAP IAW SRM 51-42-06, 51-40-11.
Part: STIFFENER — CHAFED (ZONE 100) · airframe 11,735 hrs · 8,056 cycles
AFT PRESSURE BULKHEAD Z-STIFFENER WEB AT FS 1098.20 IS DAMAGED BY MIGRATION OF THE FLOATATION VALVE HINGE PIN. REPAIRED DAMAGED WEB BY BLENDING AT BL-0/WL-60 TO A SMOOTH TRANSITION IAW SRM 51-12-00. ADDITIONALLY, THE FLOTATION VALVE HINGE PIN, PN BA690-95103, WAS REPAIRED BY DRILLING 2 HOLES AT EACH END AND ADDING WASHERS AND LOCK PINS TO PREVENT MIGRATION. THIS MAJOR REPAIR WAS ACCOMPLISHED IAW REO 690-53-61-421 REV. A, DATED 12 NOV 2013 AND EC/TC REO 690-53-61-421, DATED 19 NOV 2013. NDT ACCOMLISHED. WO-80156; WC-1073.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 11,735 hrs · 8,056 cycles
LEFT SIDE SEAT TRACK BETWEEN THE OVERWING EMERGENCY EXITS, BS 744 - 761 HAS SEVERAL SPOTS OF CORROSION. R & R SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 11,735 hrs · 8,056 cycles
LEFT WALL SEAT TRACK BS 677 - 720 HAS SEVERAL SPOTS OF CORROSION. R & R SIDE SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 677-720) · airframe 11,798 hrs · 8,094 cycles
SEAT TRACK AT BS 677 TO 720, SEVERAL SPOTS OF CORROSION. R & R SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 11,798 hrs · 8,094 cycles
SEAT TRACK AT BS 485 TO 581, HAS SEVERAL SPOTS OF CORROSION. COMPLIED WITH ECTC REO 670-53-00-013 AND REO 670-53-00-013.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 11,798 hrs · 8,094 cycles
SEAT TRACK AT FS 785 TO 847 + 16, SEVERAL SPOTS OF CORROSION. R & R SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 11,798 hrs · 8,094 cycles
SEAT TRACK BETWEEN OVERWING EMERGENCY EXITS, HAS SEVERAL SPOTS OF CORROSION. R & R SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 785-847) · airframe 11,798 hrs · 8,094 cycles
SEAT TRACK AT FS 785 TO 847 + 16, SEVERAL SPOTS OF CORROSION. R & R SEAT TRACK IAW AMM 53-00-49.
Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 11,798 hrs · 8,094 cycles
SEAT TRACK AT FS 349 TO 409, SEVERAL SPOTS OF CORROSION. R & R SEAT TRACK IAW SRM 51-41-02 AND SRM 53-21-49.
Part: ANGLE — CRACKED (COCKPIT) · airframe 11,798 hrs · 8,094 cycles
COCKPIT QUARTER TURN ANGLE CRACKED. NEW ANGLE INSTALLED IAW SRM 51-47-06.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,798 hrs · 8,094 cycles
SEAT TRACK BETWEEN OVERWING EMERGENCY EXITS, HAS SEVERAL SPOTS OF CORROSION. R & R SEAT TRACK IAW AMM 53-00-49.
Part: ANGLE — CORRODED (DOOR SILL) · airframe 11,798 hrs · 8,094 cycles
SERVICE DOOR SILL KICK ANGLE CORRODED. REPLACED SERVICE DOOR SILL KICK ANGLE IAW AMM 51-21-01, SRM 51-40-11, SRM 51-42-21, & SRM 51-42-06.
Part: WEB — CORRODED (BS 280) · airframe 11,798 hrs · 8,094 cycles
WEB CORRODED OUT OF LIMITS BS 280. COMPLIED WITH EC/TC REO 670-53-11-594-01 AND GREO 670-53-11-594, REV.
Part: FLOORBEAM — CORRODED (BS 1036) · airframe 11,798 hrs · 8,094 cycles
AFT FLOORBEAM BS 1036, LBL 26 HAS CORROSION. R & R FLOORBEAM IAW REO 670-53-00-029, REV A, SRM 51-21-11, 51-42-06, & 51-42-21.
Part: ANGLE — CORRODED (SERVICE DOOR) · airframe 11,798 hrs · 8,094 cycles
SERVICE DOOR MIDCAP CORRODED. REMOVED, RECEIVED, DRILLED, ALODINED NEW SERVICE DOOR MID CAP ANGLE IAW SRM 51-42-06 AND 51-21-01 AND 51-40-11.
Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 11,798 hrs · 8,094 cycles
PAX DOOR SILL KICK ANGLE CORRODED. R & R PASSENGER DOOR SILL KICK PLATE ANGLE IAW 51-42-06 AND 51-42-20.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,798 hrs · 8,094 cycles
TWO ANGLES THAT ATTACH TO PROTECTOR PLATE MOUNTS ON SERVICE DOOR SILL CORRODED. REMOVED CORRODED ANGLES AND INSTALLED AND REPLACED WITH NEW ANGLES IAW SRM 51-42-06 AND SRM 51-23-00.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 11,798 hrs · 8,094 cycles
BS 280 FLOORBEAM CORRODED OUT OF LIMITS. R & R FLOORBEAM IAW SRM 51-42-06, 51-42-21, 51-42-13, 51-40-11, 51-42-22, AND 51-25-16.
Part: WEB — CORRODED (BS 280) · airframe 11,798 hrs · 8,094 cycles
WEB CORRODED OUT OF LIMITS, BS 280. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594, REV.
Part: ANGLE — CRACKED (COCKPIT) · airframe 11,798 hrs · 8,094 cycles
RT COCKPIT QUARTER-TURN ANGLE CRACKED. INSTALLED IAW SRM 51-42-06.
Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 11,798 hrs · 8,094 cycles
RT COCKPIT FLOOR SUPPORT CRACKED AT RBL 12. REPAIRED IAW REO 690-53-11-606.
Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 11,798 hrs · 8,094 cycles
COCKPIT FLOOR SUPPORT CRACKED AT LBL 12. R & R FLOOR SUPPORT IAW REO 690-53-11-606 2013-11-09.
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 9,730 hrs · 6,795 cycles
PILOT'S LIFE VEST BAG TORN. REMOVED & REPLACED PILOTS LIFE VEST IAW AMM 25-61-03.
2012
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 8,899 hrs · 6,188 cycles
F/O LIFE VEST HAS HOLES IN BAG. REMOVED AND REPLACED F/O'S LIFE VEST IAW AMM 25-61-03. OPS CHECKS GOOD.
Part: GLOWSTRIP — CRACKED (CABIN) · airframe 8,365 hrs · 5,788 cycles
PHOTOLUMINESCENT STRIP ON FLOOR CRACKED AND LEAKING POWDER. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP IAW AMM 33-51-01. OPS CHECKEDS GOOD. OK FOR SERVICE.
Part: WARNING LIGHT — FALSE ACTIVATION (TE FLAPS) · airframe 8,294 hrs · 5,703 cycles
FLIGHT 4303, FLAPS FAIL CAUTION. AIRCRAFT LANDED SAFELY AND NO EMERGENCY WAS DECLARED. PERFORMED OPS CHECKED IAW AMM 22-50-00, NO DEFECT NOTED. OK FOR SERVICE.
Part: DETECTOR — FALSE INDICATION (ICE DETECTION) · airframe 7,079 hrs · 4,854 cycles
AIR RETURN FOR MULTIPLE ERRONEOUS ICE CAUTION ICE DET 2. PERFORMED OPS CHECK OF ANTI-ICE SYSTEM IAW AMM 30-81-00. OPS GOOD AT THIS TIME.
2011
Part: SPOILER — MALFUNCTIONED (WING) · airframe 6,807 hrs · 4,693 cycles
I/B FLT SPLRS & I/B SPOILERONS CAUTION MSGS WHEN FLT SPOILERS DEPLOYED. SYNOPTIC SHOWS LEFT I/B MFS OUTLINE YELLOW & RT I/B MFS OUTLINE WHITE. CLEARED INHIBITS IAW CRJ900 AMM 27-61-00, MSGS CLEARED. OK FOR CONT SERVICE, OPS CHECK GOOD AT THIS TIME.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 6,457 hrs · 4,424 cycles
CAPT'S/ FWD F/A'S EMERGENCY FLASHLIGHT FAILS "RED" LED TEST. REMOVED AND REPLACED CAPT'S, FWD F/A'S EMERGENCY FLASHLIGHT BATTERIES OP'S CHECK GOOD IAW AMM 25-60-00, VERIFIED PARTS EFFECTIVITY.