N527EA
Registered owner: AMERICAN AIRLINES INC, TX (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.
130 reports on file, 2011-10-21 – 2025-10-17.
Part: LUG — DAMAGED (ZONE 600 AILERON) · airframe 33,083 hrs · 25,727 cycles
TO PERFORM OVERSIZE BEARINGS INSTALLATON REWORK RH AILERON LUG R3 AND R4 TO INSTALL BEARING P/N: KSC432409B. PERFORM OVERSIZE AT RH AILERON LUG R3 AND R4 PER REO 670-57-61-458 REV. -A
Part: HINGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
AFTER HINGE FITTINGS REMOVAL IN REF NRC 0034 CORROSION IN UPPER HINGE WAS FOUND. UPPER HINGE OF TOILET SERVICE DOOR 196ER WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01
Part: HINGE FITTING — CORRODED (ZONE 800) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON FITTING CLOSING FWD AT SURROUND PASSENGER DOOR WAS FOUND. CORROSION ON FITTING CLOSING FWD AT SURROUND PASSENGER DOOR WAS EVALUATED EXCESSIVE DAMAGE PER CRJ-700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01.
Part: CANISTER — CRACKED (ZONE 600) · airframe 33,083 hrs · 25,727 cycles
CRACK IN CANISTER WELDED NO.3, ON WS148.019 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, ON WS148.019 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON SEAT RAIL RBL27.00 BTW FS977.00 TO FS1005.00 AT PASSENGER CABIN. DUE TO EXCESSIVE DAMAGE ON SEAT RAIL RBL27.00 BTW FS977.00 TO FS1005.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER SRM 53-51-49-101-001-A01 AND WERE REPLACED PER CRJ700 AMM 53-00-49.
Part: LUG — CORRODED (ZONE 600 AILERON) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
AFTER BEARINGS AND BUSHINGS REMOVAL IN REF. TASK CARD 271500-RH-PSA-AILERON, CORROSION AND SCRATCHES WAS FOUND ON CENTER FITING LUGS R1, R2, R5 AND R6. AT RH AILERON. CENTER FITING LUGS R1, R2, R5 AND R6. AT RT AILERON WERE REPAIRED IAW REO 670-57-61-237 REV -.
Part: LUG — CORRODED (ZONE 500 AILERON) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
TO PERFORM OVERSIZE BEARING INSTALLATON REWORK LH AILERON LUG L4 TO INSTALL BEARING P/N: KSC432409B-03. NEW BEARING (1EA) (LUG 4) PN:KSC432409B-03 AT AILERON LH WAS INSTALLED PER REO 670-57-61-457 REV -A
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON FRAME FS1015.00 BTW STGR 21LH TO STGR 24RH AT INTERNAL STRUCTURE AFT CARGO COMPARTMENT. CORROSION ON FRAME BS 1015.00 BTW STGR 21LH TO STGR 24RH AT INTERNAL STRUCTURE AFT CARGO COMPARTMENT WAS EVALUATED OUT LIMITS IAW SRM 53-61-06-101-001-A01 AND REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: LUG — CORRODED (ZONE 500 AILERON) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION AND SCRATCHES ON OUT FITTING AND CENTER FITING LUGS L1,L2, L5 AND L6. AT LH AILERON WAS FOUND. CENTER FITING LUGS L1,L2, L5 AND L6. WERE REPAIRED PER REO 670-57-61-237 REV. - - PAR F AND OUT FITTTING LUGS WERE CLEANED PER PER CRJ-700 SRM 51-26-00-001-001-A01 PAR. 5.B.
Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1069.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT. CORROSION ON FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1069.00 AT FLOOR STRUCTURE AFT CARGO COMPARTMENT WAS EVALUATED EXCESSIVE DAMAGE IAW SRM 53-61-43-101-001-A01 AND SRM 53-00-41-201-001-A01 AND REPAIRED PER SRM 53-00-41-201-001-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER SPLICE 24RH BTW STA. FS= 319.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 24RH BTW STA. FS= 319.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED EXCESSIVE DAMAGE PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER AND SPLICE 23RH BTW STA. FS= 310.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT. CORROSION SPLICE 23RH BTW STA. FS= 310.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED EXCEDED ALLOWABLE PER CRJ-700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01 AND STRINGER 23RH BTW STA. FS= 310.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT WAS CLEANED PER CRJ-700 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON INTERCOSTAL ATTACHED TO STGR 20RH BTW FS 310.00 AND FS 319.00 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL ATTACHED TO STGR 20RH BTW FS 310.00 AND FS 319.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-700 SRM 53-21-23-101-002-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER 26RH BTW STA. FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER 26RH BTW STA FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED DUE EXCESSIVE DAMAGE PER CRJ-700 SRM 51-21-06-001-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01. AND PER CRJ-700 SRM 51-42-21-001-001-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER SPLICE 24RH BTW STA. FS= 319.00 AND FS= 333.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 24RH WAS EVALUATED EXCESSIVE DAMAGE PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED IAW SRM 51-42-06-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER 24R BTW FS485 AND FS501 AT FWD BAGGAGE BAY COMPARTMENT. CORROSION ON STRINGER 24R BTW FS485 AND FS501 AT FWD BAGGAGE BAY COMPARTMENT WAS REPAIRED PER REO 670-53-31-1111 REV-.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER 26LH AND STANDOFFS (2EAS) BTW STA. FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT. STRINGER 26LH AND STANDOFFS (2EAS) BTW STA. FS= 295.00 AND FS= 310.00 AT MAIN AVIONICS COMPARTMENT WERE EVALUATED EXCESSIVE DAMAGE PER SRM 53-21-03-101-002-A01 AND REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER SPLICE 21RH IN STA. FS= 333.00 TO FS= 337 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER SPLICE 21RH IN STA. FS= 333.00 TO FS= 337 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED FOR EXCESSIVE DAMAGE PER CRJ-700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON STRINGER AND SPLICE 25R BTW BS 310 AND 333 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER 25R BTW BS 310 & BS 333 WAS EVALUATED EXCESSIVE DAMEGE IAW SRM 53-00-00-101-001-A01 AND REPLACED IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND SPLICE 25R BTW BS 310 & BS 333 AT MAIN AVIONICS COMPARTMENT WAS CLEANED PER SRM 51-26-00-001-001-A01 AND INSPECTED AFTER CLEANING ON SPLICE, INSPECTION WAS PERFORMED PER SRM 51-26-00-001-001-A01 PAR.3. E. AND NDT MANUAL 51-20-009-210 STEP 4. NO CORROSION FOUND.
Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON DOUBLER OF FUSELAGE SKIN BTW FS 969.00 TO FS 1000. DOUBLER OF FUSELAGE SKIN BTW FS 969.00 TO FS 1000.00 WAS REPLACED PER REO 670-53-00-290 REV -F
Part: ACCESS PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON SETTLEMENT AREA OF ACCESS PANEL: 642BZ. CORROSION ON SETTLEMENT AREA OF ACCESS PANEL: 642BZ WAS EVALUATED EXCESSIVE DAMAGE PER SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01.
Part: HINGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON HINGE FITTINGS OF TOILET SERVICE DOOR 196ER. HINGE FITTINGS OF TOILET SERVICE DOOR 196ER WAS REPLACED PER CRJ-700 AMM 52-45-01-400-80.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON LH SIDE SEAT RAILS LBL 45 (STRG 15LH) BTW FS 785TO FS 847, BTW FS 744 TO FS 785, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW FS 379 TO 548 AT PASSENGER CABIN. SEAT TRACK BTW FS 881 TO FS 913, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW FS 379 TO 548 AT LBL 9 PASSENGER CABIN WAS REMOVED AND EVALUATED, THEREFORE ARE OUT OF LIMITS. FLOOR SEAT RAILS WERE REPLACED AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
WEAR AND CORROSION ON FLOOR SEAT RAILS BTW FS 349 TO FS 364, BTW FS 661+46 TO 661+74, BTW FS 720 TO FS 744 & BTW FS 847 TO FS 977 AT RBL 9 PASSENGER CABIN. FLOOR SEAT RAILS BTW FS 349 TO FS 364, BTW FS 661+46 TO 661+74, BTW FS 720 TO FS 744 & BTW FS 847 TO FS 977 AT RBL 9 PASSENGER WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ900 AMM 53-00-49.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
WEAR AND CORROSION ON RH SIDE SEAT RAILS RBL 45 (STGR 15RH) BTW FS 379 TO FS 394, BTW FS 469 TO FS 581, BTW FS 629 TO FS 661, BTW FS 744 TO FS 761 & BTW FS 785 TO FS 797 AT PASSENGER CABIN. RT SIDE SEAT RAILS RBL 45 (STGR 15RH) BTW FS 379 TO FS 394, BTW FS 469 TO FS 581, BTW FS 629 TO FS 661, BTW FS 744 TO FS 761 & BTW FS 785 TO FS 797 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02, SRM 53-41-49-101-001-A02 AND SRM 53-51-49-101-001-A02 AND REPLACED PER CRJ900 AMM 53-00-49
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON FLOOR SEAT RAILS BTW FS 881 TO FS 913, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW FS 379 TO 548 AT LBL 9 PASSENGER CABIN. CORROSION ON FLOOR SEAT RAILS BTW FS 881 TO FS 913, BTW FS 661+16 TO FS 720, BTW FS 661 TO 549 & BTW FS 379 TO 548 AT LBL 9 PASSENGER CABIN WAS REMOVED AND EVALUATED, THEREFORE ARE OUT OF LIMITS. FLOOR SEAT RAILS WERE REPLACED CRJ-900 AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.
Part: LANDING — CORRODED (ZONE 500) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 521AT AT LH WING. SETTLEMENT AREA OF ACCESS PANEL 521AT AT LT WING (LT SIDE FRAME HOUSING LANDING P/N: CC670-12111-5) WAS EVALUATED OUT OF LIMITS PER SRM 57-41-01-101-001-A01 REPLACED PER CRJ900 SRM 51-42-06-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 200) · airframe 33,083 hrs · 25,727 cycles
CRACK ON INTERCOSTAL BTW FS173 TO FS179 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. INTERCOSTAL BTW FS173 TO FS179 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-10-001-001-A01, SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
Part: WEB — CRACKED (ZONE 200) · airframe 33,083 hrs · 25,727 cycles
CRACK ON WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.
Part: PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON THE MATING SURFACE OF THE PANEL ASSEMBLY FROM SS15.50 TO SS39.00 (ACCESS 621AB), AS WELL AS CORROSION ON MATING SURFACE OF LOWER EDGE OF ACCESS 621AT, RIGHT WING. CORROSION ON THE MATING SURFACE OF THE PANEL ASSEMBLY FROM SS15.50 TO SS39.00 (ACCESS 621AB), AS WELL AS CORROSION ON MATING SURFACE OF LOWER EDGE OF ACCESS 621AT, RIGHT WING WERE REPAIRED PER REO 690-57-21-541 REV. --, REO 690-57-41-550 REV. -- AND REO 690-57-41-554 REV. --, FRAME-HOUSING, LANDING AND TAXI LIGHT P/N CC670-12111-6 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.
Part: ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON SETTLEMENT AREA (UPPER SURFACE) OF ACCESS PANEL 362AR AT AFT FUSELAGE. ANGLE P/N: WA670-30111-3 ON SETTLEMENT AREA (UPPER SURFACE) OF ACCESS PANEL 362AR AT AFT FUSELAGE WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND DWG 670-30111 REV. C.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,083 hrs · 25,727 cycles
CORROSION ON LATCH PIN INTERCOSTAL LEFT TO STGâ¢R 27 AND BTW FS394 TO FS400 INTERNAL STRUCTURE AT AVIONICS COMPARâ¢TMENT. LATCH PIN INTERCOSTAL LEFT TO STGR27 AND BTW FS394 TO FS400 INTERNAL STRUCTURE AT AVIONICS COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: OVERHEAT LOOP — FAULTED (LT ENGINE) · airframe 32,308 hrs · 25,067 cycles
L BLEED DUCT WARNING MSG ON CLIMB, FL260. / REMOVED AND REPLACED LOOP MT141 IAW CRJ 700 AMM 36-21-01-000/400-806-A04. OPS CHECK GOOD AT THIS TIME. PERFORMED UNATE SCAN OF AILC. AILC OPS CHECKS GOOD AT THIS TIME.
Part: CLAMP — LOOSE (AEB) · airframe 32,265 hrs · 25,029 cycles
L BLEED DUCT WARNING MSG. / INSPECTED LOOP IN AEB AND FOUND BLUE ADEL CLAMP THAT HOLD BOTH LOOPS IN PLACED EXTREMELY LOOSE (HOLDING BY ONE THREAD) CAUSING BOTH LOOPS TO TOUCH. RETORQUED CLAMP PER AMM 20-21-00-910-801-A01 AND 36-21-00-910-801-A01. NO OTHER DEFECTS NOTED.
Part: SHUTOFF VALVE — UNSERVICEABLE (NR 1) · airframe 32,190 hrs · 24,967 cycles
L BLEED DUCT WARNING IN FLIGHT. / REMOVED AND REPLACED #1 PRSOV IAW CRJ 700 AMM 36-12-01-000/400-801. OPS CHECK GOOD AND LEAK CHECK GOOD.
Part: OVERHEAT LOOP — FAULTED (LEFT) · airframe 32,175 hrs · 24,954 cycles
L BLEED DUCT WARNING MSG / REMOVED AND REPLACED LH BLEED LOOP A WIRE AND CONNECTORS FROM MT139P1 TO MT141P1 WITH NEW INSULATORS AS AN ASSY ROBBED FROM N534AE IAW FIM 36-21-01-810-801-A01. OPS CHECKS GOOD. LH BLEED LOOP A CHECKS AT 66 OHMS.
Part: BLEED VALVE — TORN (ZONE 400) · airframe 32,081 hrs · 24,879 cycles
L BLEED DUCT WARNING MSG WHILE CLIMBING THROUGH FL 210 / FOUND INSULATION MUFF FOR THE CROSS BLEED VALVE TORN. REMOVED AND REPLACED INSULATION MUFF IAW CRJ-700 AMM 36-13-15-400-801 AND 36-21-00-910-801. OPS TEST AND LEAK TEST GOOD. L BLEED DUCT WARNING MSG DID NOT RETURN
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,650 hrs · 24,522 cycles
"RH FS280 FLOOR BEAM FOUND TO BE CORRODED AND CRACKED. REQUIRES REPLACEMENT, REMOVED RH FS280 FLOOR BEAM IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01. LOCATED, DRILLED, AND DEBURRED RH FS280 FLOOR BEAM PN: CC670-34094-2S IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED RH FS280 FLOOR BEAM IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01 HN00217402"
Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,650 hrs · 24,522 cycles
J ANGLE FOUND TO BE CORRODED AT FS280 BETWEEN LBL9 AND RBL9.CORRECTIVE ACTION: REMOVED J ANGLE AT FS280 IAW CRJ700 SRM 51-42-06-001-001-A01. LOCATED, DRILLED, AND DEBURRED J ANGLE AT FS280 PN: CC670-34095-1SB AND SPLICE ANGLE PN: CC670-34098-1 IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED J ANGLE AT FS280 IAW CRJ700 SRM 51-42-06-001-001-A01. HN00217404
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,650 hrs · 24,522 cycles
"RH FS280 LOWER WEB FOUND TO BE CORRODED. PERFORMED REPAIR OF RH BULKHEAD LOWER WEB FS280 IAW CRJ700 SRM 53-11-10-201-004-A01.HN00217405"
Part: ANGLE — CRACKED (ZONE 200) · airframe 31,650 hrs · 24,522 cycles
WHILE PREFORMING WEB REPAIR FOUND ANGLE, BL26.00 FS280.00 TO BE CRACKED. CORRECTIVE ACTION: REMOVED CRACKED ANGLE. INSTALLED NEW WEB ANGLE PN: CC670-34117-6 AT BL26.00 FS280.00 IAW CRJ700 SRM 51-42-06-001-001-A01. HN00217765
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,650 hrs · 24,522 cycles
"LH FS280 LOWER WEB FOUND TO BE CORRODED. PERFORMED REPAIR OF LH BULKHEAD LOWER WEB FS280 IAW CRJ700 SRM 53-11-10-201-004-A01. HN00217439"
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,650 hrs · 24,522 cycles
LH FS280 FLOOR BEAM FOUND TO BE CORRODED AND CRACKED. REQUIRES REPLACEMENT. : REMOVED RH FS280 FLOOR BEAM IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01. LOCATED, DRILLED, AND DEBURRED RH FS280 FLOOR BEAM PN: CC670-34094-1, IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED RH FS280 FLOOR BEAM IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42-13-001-001-A01. HN00217403
Earlier reports · 2011–2023 · 87 reports
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 28,176 hrs · 21,558 cycles
MAIN PASSENGER DOOR WARNING MSG CAME ON IN CRUISE FLIGHT, RAMP PERSONNEL NOTED OUTER HANDLE OPEN. INNER HANDLE HANDLE IN PROPER POSITION AND LOCKED / INSPECTED MAIN DOOR LINKAGE WITH NO FAULTS NOTED. PERFORMED OPS CHECK OF DOOR IAW CRJ 700 AMM 52-11-00-710-801. ALL INDICATIONS NORMAL.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 27,944 hrs · 21,360 cycles
RH LOWER WING SKIN BETWEEN WS314.5 ̉‰ 330.45 & STGR10 ̉‰ STGR11. C/W PERMANENT REPAIR OF E.A. 22-C7-57-1591 REV A IAW E.A. INSTRUCTIONS.
2022
Part: PANEL — CORRODED (ZONE 600) · airframe 26,819 hrs · 20,320 cycles
NDT FAILED HOLE ON R/H LOWER WING PLANK, I/B ROW, AFT FASTENER
Part: SKIN — DENTED
REPAIRED MULTIPLE DENTS ON THE OUTSIDE LOWER SKIN JUST AFT OF THE AFT EQUIPMENT BAY DOOR BETWEEN FS1162 TO SPAR DATUM 55.63 AND STRS 23R-23-L PER REO 670-53-71-088 CONSIDERED A MAJOR REPAIR.
2021
Part: SKIN — DENTED (ZONE 100) · airframe 25,760 hrs · 19,399 cycles
DENT ON FUSELAGE SKIN AT FS 1031 ON STGR 25R MEASURING 1.00"L X .5"W .031"D. CORRECTIVE ACCTION: REPAIRED AREA BY DRESSING BACK DENT AT FS 1031 ON STGR 25R TO .950"L X .475"W X .011"D AND FABRICATED DOUBLER REPAIR PARTS AND INSTALLED THEM AT FS 1031 AT STGR 25R IAW OLIVER WYMAN EA 21-C7-53-1234 REV IR DATED 12/14/2021.
Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,760 hrs · 19,399 cycles
AFT WING TO BODY SUPPORT ATTACHMENT ANGLE IS CORRODED AT F.S. 953 FROM B.L. 24L-24R. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N: SH670-39189-1) I/A/W CRJ 700 SRM 51-40-00.
Part: ANGLE — CORRODED (ZONE 100) · airframe 25,760 hrs · 19,399 cycles
AFT WING TO BODY SUPPORT ATTACHMENT ANGLE IS CORRODED AT F/S. 953 FROM B/L 24L-24R. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE (P/N: SH670-39189-1) IAW CRJ 700 SRM 51-40-00.
Part: LINTEL — CRACKED (ZONE 200) · airframe 25,760 hrs · 19,399 cycles
PASSENGER LINTEL STRINGER CRACKED AT F.S. 280 CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED THE PASSENGER DOOR LINTEL STGR AT F.S. 280.00 I/A/W BOMBARDIER SB 670BA-53-040 REV. C DATED SEPT 20/2012 AND BOMBARDIER REO 670-53-21-493 REV. D DATED 2015-07-10. FABRICATED SHIMS, AND USED A REPAIR KIT SUPPLIED BY BOMBARDIER.
Part: STRINGER — CRACKED (ZONE 200) · airframe 25,760 hrs · 19,399 cycles
PASSENGER DORR LINTEL STRINGER IS CRACKED AT F.S. 280.00. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED THE PASSENGER DOOR LINTEL STGR AT F.S. 280.00 IW BOMBARDIER SB 670BA-53-040 REV. C DATED SEPT 20/2012 AND BOMBARDIER REO 670-53-21-493 REV. D DARED 2015-07-10. FABRICATED SHIMS, AND USED A REPAIR PART KIT SUPPLIED BY BOMBARDIER.
Part: LINTEL — CRACKED (ZONE 200) · airframe 25,760 hrs · 19,399 cycles
PASSENGER DOOR LINTEL STRINGER IS CRACKED AT F.S. 280.00. CORRECTIVE ACTION: CUT OUT DAMAGED AREA AND REPAIRED THE PASSENGER DOOR LINTEL STGR AT F.S. 280.00 IWW BOMBARDIER SB 670BA-53-040 REV. C DATED SEPT 20/2012 AND BOMBARDIER REO 670-53-21-493 REV. D DARED 2015-07-10. FABRICATED SHIMS, AND USED A REPAIR PART KIT SUPPLIED BY BOMBARDIER.
Part: ANGLE — CRACKED (ZONE 300) · airframe 25,760 hrs · 19,399 cycles
VERTICAL STABLIZER L/H AFT DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW BOMBARDIER REO 670-55-31-018 REV. A DATED 2016-11-10
Part: ANGLE — CORRODED (ZONE 100) · airframe 25,760 hrs · 19,399 cycles
STRINGER 26L BETWEN F.S. 319 AND F.S.333 THE JOINT SPLICE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE JOINT SPLICE (N126-3999) ON STGR 26L BETWEEN F.S. 319 AND F.A. 333 IAW CRJ J700 SRM 51-42-06-001-001-A01 AND 53-21-08-001-002-A01.
Part: SKIN — CORRODED (ZONE 800) · airframe 25,760 hrs · 19,399 cycles
PASSANGER DOOR INTERNAL SKIN ACCESS PANEL FLANGE FOR PANEL 832FL IS CORRODED. CORRECTIVE ACTION: REPAIRED THE ACCESS PANEL FLANGE FOR PANEL 832FL ON THE INTERNAL PAX DOOR SKIN IAW CAVOK ENGINEERING AUTHORIZATION 27-C7-52-1224 REV. IR DATED 11/6/2021. UNK
Part: FLANGE — CORRODED (ZONE 100) · airframe 25,760 hrs · 19,399 cycles
FALSE FLANGE AT F.S. 310 BETWEEN STGR 26R AND 24R IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGE AND REPAIRED THE FALSE FLANGE (PN: S1710-3) IAW BOMBARDIER REO 670-53-21-1281 REV. -- DATED 2016-04-11.
Part: NONE — CORRODED (ZONE 100) · airframe 25,760 hrs · 19,399 cycles
FALSE FLANGE AT F.S. 310 BETWEEN STGR 26R AND 24R IS CORRODED. CORRECTIVE ACTION: REMOVED DAMAGE AND REPAIRED THE FALSE FLANGE (PN: S1710-3) IAW BOMBARDIER REO 670-53-21-1281 REV. -- DATED 2016-04-11.
Part: FLANGE — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,760 hrs · 19,399 cycles
FALSE FLANGE AT F.S. 310 BETWEEN STGR 26R AND 24R IS CORRODED. CORRECTIVE ACTION: REMOVED AND DAMAGE AND REPAIRED THE FALSE FLANGE (P/N S1710-3) I/A/W BOMBARDIER REO 670-21-1281 REV. -- DATED 2016-04-11.
Part: JOINT — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,760 hrs · 19,399 cycles
STRINGER 26L BETWEEN F.S. 319 AND F.S. 333 THE JOINT SPLICE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE JOINT SPLICE (N126-3999) ON STGR 26L BETWEEN F.S. 319 AND F.S. 333 I/A/W CRJ700 SSRM 51-42-06-001-001-A01 AND 53-21-08-001-002-A01.
Part: ANGLE — CORRODED (ZONE 100) · airframe 25,760 hrs · 19,399 cycles
STRINGER 26R BETWEEN F.S. 333 AND F.S.349 THE JOINT SPLICE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE JOINT SPLICE(PN; N126-3999) ON STGR 26R BETWEEN F.S. 333 AND F.S. 349 IAW CTJ 700 SRM 51-42-06-001-001-A01 AND 53-21-08-01-002.
Part: JOINT — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,760 hrs · 19,399 cycles
STRINGER 26R BETWEEN F.S. 333 AND F.S. 349 THE JOINT SPLICE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED THE JOINT SPLICE (P/N: N126-3999) ON STGR 26R BETWEEN F.S. 333 AND F.S. 349 I/A/W CRJ700 SRM 51-42-06-001-001-A01 AND 53-21-08-01-002.
Part: RIB — CRACKED (ZONE 400) · airframe 25,760 hrs · 19,399 cycles
R/H O/B FIXED LEADING EDGE RIB CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED THE R/H FIXED LEADING EDGE RIB (P/N CC670-12137-8) I/A/W CRJ700 SRM 51-42-15, 51-42-13- AND 51-42-06.
Part: FLANGE — CORRODED (ZONE 800) · corrosion level 2 · airframe 25,760 hrs · 19,399 cycles
PASSENGER DOOR INTERNAL SKIN ACCESS PANEL FLANGE FOR PANEL 832FL IS CORRODED. CORRECTIVE ACTION: REPAIRED THE ACCESS PANEL FLANGE FOR PANEL 832FL ON THE INTERNAL PAX DOOR SKIN I/A/W OLIVER WYMAN, CAVOK ENGINEERING AUTHORIZATION 27-C7-52-1224 REV. IR DATED 11/26/2021.
Part: SKIN — CORRODED (ZONE 800) · airframe 25,760 hrs · 19,399 cycles
PASSENGER DOOR INTERNAL SKIN ACCESS PANEL FLANGE FOR PANEL 832FL IS CORRODED. CORRECTIVE ACTION: REPAIRED THE ACCESS PANEL FLANGE FOR PANEL 832FL ON THE INTERNAL PAX DOOR SKIN IAW OLIVER WYMAN, CAVOK ENGINEERING AUTHORIZATION 27-C7-52-1224 REV. IR DATED 11/26/2021.UNK
Part: RIB — CRACKED (ZONE 400) · airframe 25,760 hrs · 19,399 cycles
R/H O/B FIXED LEADING EDGE RIB IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLAED THE R/H FIXED LEADING EDGE RIB(PN:CC670-12137-8) IAW CRJ 700 SRM 51-42-15, 51-42-13, AND 51-42-06.
Part: NONE — NONE · airframe 25,760 hrs · 19,399 cycles
UPPER AFT FUSELAGE SKIN GOUGE UNDER DORSAL STRAKE. CORRECTIVE ACTION: REMOVED DAMAGE BY BLENDED AND PERFORMED NDT UT, HFEC IN AREA FROM F.S. 879 TO FS 1126 ON FUSELAGE SKIN AT STR 0 IAW WITH EA 21-C7-53-1222 REV A DATE 11/26/2021.
Part: SKIN — GOUGED · airframe 25,760 hrs · 19,399 cycles
UPPER AFT FUSELAGE SKIN GOUGE UNDER DORSAL STRAKE. CORRECTIVE ACTION: REMOVED DAMAGE BY BLENDED AND PREFORMED NDT UT, HFEC IN AREA FROM F.S. 879 TO F.S. 1126 ON FUSELAGE SKIN AT STRG 0 I/A/W EA 21-C7-53-1222 REV. A DATED 11/26/2021.
Part: SKIN — GOUGED · airframe 25,760 hrs · 19,399 cycles
UPPER AFT FUSELAGE SKIN GOUGE UNDER DORSAL STRAKE. CORRECTIVE ACTION: REMOVED DAMAGE BY BLENDED AND PERFORMED NDT UT, HFEC IN AREA FROM F.S. 879 TO FS 1126 ON FUSELAGE SKIN AT STR 0 IAW WITH EA 21-C7-53-1222 REV A DATE 11/26/2021.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,760 hrs · 19,399 cycles
CORROSION ON STR 25R BETWEEN F.S. 319 TO F.S. 333 CORRECTIVE ACTION: REMOVED AND REPLACED CORRODED JOINT PIECE (P/N: SH670-32429-4) AT STGR 25R BETWEEN F.S. 319 TO F.S. 333 I/A/W CRJ700 SRM 51-42-06 AND SRM 51-42-20.
Part: BRACKET — CRACKED · airframe 25,760 hrs · 19,399 cycles
INTERNAL PAX DOOR, POWER ASSIST MOTOR BRACKET IS CRACKED. CORRECTIVE ACTION REMOVED AND REPLACED STIFFENER BRACKET (P/N: 601R317745-7) ON INTERNAL PAX DOOR IAW CRJ 700 SRM 51-40-00-001-001-A01.
Part: CABLE — CORRODED (ZONE 500) · airframe 25,760 hrs · 19,399 cycles
LEFT HAND WING AILERON CABLES ARE CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED LEFT HAND WING AILERON CABLES (P/NS: BA670-93210-29, BA670-93210-31, BA670-93210-23, BA670-93210-21) I/A/W CRJ 700 AMM 27-11-00-000-803, 27-11-220-810 AND 27-11-00-400-803..
Part: CABLE — CORRODED · airframe 25,760 hrs · 19,399 cycles
RIGHT HAND WING AILERON CABLES ARE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT HAND WING AILERON CABLES (P/N'S: BA670-93210-31, BA670-93210-27, BA670-93210-25, BA670-93210-29) IAW CRJ 700 AMM 27-11-00-000-803, 27-11-00-400-803, AND 27-11-00-2200-810.
Part: CABLE — CORRODED (ZONE 500) · airframe 25,760 hrs · 19,399 cycles
LEFT HAND WING AILERON CABLES ARE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED LEFT HAND WING AILERON CABLES (P/N'S: BA670-93210-29, BA67093210-31, BA670-93210-23, BA670-93210-21) IAW CRJ 700 AMM 27-11-00-000-803, 27-11-00-220-810, AND 27-11-00-400-803.
Part: CABLE — CORRODED · airframe 25,760 hrs · 19,399 cycles
RIGHT HAND WING AILERON CABLES ARE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT HAND WING AILERON CABLES (P/N: BA670-93210-31, BA670-93210-27, BA670-93210-25, BA670-93210-29) I/A/W CRJ700 AMM 27-11-00-000-803, 27-11-00-400-803 AND 27-11-00-220-810
Part: INTERCOSTAL — CORRODED · airframe 25,760 hrs · 19,399 cycles
CORRODED ON INTERCOSTAL 26L AND 26R IN MAIN AVIONICS BAY FWD OF AVIONICS DOOR. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL 26L (P/N: SH670-32075-4S) AND 26R (P/N: SH670-32075-3S) IAW CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.
Part: STIFFENER — CRACKED (ZONE 800) · airframe 25,760 hrs · 19,399 cycles
INTERNAL PAX DOOR, POWER ASSIST MOTOR BRACKET IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED STIFFENER BRACKET (P/N: 601R317745-7) ON INTERNAL PAX DOOR I/A/W CRJ700 SRM 51-40-00-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,760 hrs · 19,399 cycles
CORROSION ON INTERCOSTAL 26L AND 26R IN MAIN AVIONICS BAY FWD OF AVIONICS DOOR. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCOSTAL 26L (P/N: SH670-32075-4S) AND 26R (P/N: SH670-32075-3S) I/A/W CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01.
Part: STRINGER FITTING — CORRODED · airframe 25,760 hrs · 19,399 cycles
CORRODED ON STR 25R BETWEEN F.S. 319 TO F.S. 333. CORRECTIVE ACTION REMOVED AND REPLACED CORRODED JOINT PIECE (P/N: SH670-32429-4) AT STR25 R BETWEEN F.S. 319 TO F.S. 333 IAW CRJ 700 SRM 51-42-06 AND SRM 51-42-20.
Part: ANGLE — CRACKED (ZONE 300) · airframe 25,760 hrs · 19,399 cycles
VERTICAL STABILIZER L/H AFT DRAG ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS I/A/W BOMBARDIER REO 670-55-31-018 REV. A DATED 2016-11-10
Part: WEB — CRACKED · airframe 25,760 hrs · 19,399 cycles
PAX DOOR AFT STAIR WEB IS CRACKED AT THE INSIDE CORNER OF THE MID-STEP. CORRECTIVE ACTION: REPAIR PAX DOOR STAIR WEB AT THE INSIDE CORNER OF THE MID-STEP IAW WITH REO 670-52-11-104 REV H, DATE 2016-08-14.
Part: WEB — CRACKED (ZONE 800) · airframe 25,760 hrs · 19,399 cycles
PAX DOOR AFT STAIR WEB IS CRACKED AT THE INSIDE CORNER OF THE MID-STEP. CORRECTIVE ACTION: REPAIR PAX DOOR STAIR WEB AT THE INSIDE CORNER OF THE MID-STEP I/A/W REO 670-52-11-104 REV. H DATED 2016-08-14.
Part: TARGET — OUT OF RIG (NLG) · airframe 25,702 hrs · 19,350 cycles
EMERGENCY DECLARED GOING INTO CLT FOR GEAR DISAGREE AND STEERING INOP. FLIGHT LANDED WITHOUT ISSUE IN CLT. T . T/S B1 CODE 007427 IAW CRJ700 FIM 32-21-10-810-801. PERFORMED EXTENSION/OPS TEST OF THE LANDING GEAR PSS IAW CRJ700 AMM 32-61-00-710-801 AND FOUND PX24 TARGET OUT OF RIG. PERFORMED RIGGING OF PX24 TARGET IAW CRJ700 VCMM 32-21-05, OPS CHECK OK, NO B1 CODES ON MULTIPLE EXTENSIONS. NO DEFECTS.
2020
Part: ACM — FAILED (LEFT) · airframe 23,976 hrs · 17,793 cycles
LT PACK GOES FULL HOT AIR UNCOMMANDED WITH BURNING SMELL IN AUTO MODE. REMOVED AND REPLACED LT AIR CYCLE MACHINE, IAW CRJ700 AMM 21-51-08-000/400-801-A01. OPERATIONS CHECK GOOD.
2019
Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,771 hrs · 15,833 cycles
MX FOUND RH OVERWING EMERGENCY EXIT LIGHT FAILS TO ILLUMINATE. REMOVED R/H OVERWING EMERGENCY LIGHT. OP CHECK GOOD.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 21,770 hrs · 15,831 cycles
CARGO DOOR SILL HAS CORROSION. C/A-REMOVED AND REPLACED AFT CARGO DOOR SILL IAW SRM 51-42-06, SRM 51-42-13, AND 51-42-20.
Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 21,770 hrs · 15,831 cycles
SERVICE DOOR SILL IS CORRODED FROM FS319.70 TO 349.00. C/A-INSTALLED SERVICE DOOR SILL IAW SRM 51-42-06.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 21,770 hrs · 15,831 cycles
FLOORBEAM AT FS280.00 UPPER FLANGE IS CORRDOED. LOCATED BETWEEN DRIP TRAY AND FLIGHT COMPARTMENT BULKHEAD WALL LOWER L ANGLE. RT SIDE OF FLOORBEAM. C/A-REMOVED CORRODED RT FS280 CROSSBEAM AND INSTALLED RT FS280 CROSSBEAM IAW SRM 51-42-06, 51-42-13, 51-42-21.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,770 hrs · 15,831 cycles
SUPPLEMENTAL RIGHT SIDE CENTER COCKPIT FLOORBEAM AT BL12.00 HAS A 1 INCH CRACK APPROX 6 INCHES FWD OF FLOORBEAM FS280.00. C/A-COMPLETED REPAIR TO RT SIDE COCKPIT FLOORBEAM AT BL12.00 IAW AEN 51-11-43.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,770 hrs · 15,831 cycles
LEFT SIDE CENTER COCKPIT FLOORBEAM AT BL12.00 HAS A 1.5 INCH CRACK APPROXIMATELY 6 INCHES FWD OF FLOORBEAM FS280.00. C/A-COMPLETED REPAIR TO LT SIDE CENTER COCKPIT FLOORBEAM AT BL12.00 IAW SRM 51-11-43.
Part: SKIN — CHAFED (FUSELAGE) · airframe 21,770 hrs · 15,831 cycles
3 CHAFES IN EXT FUSELAGE SKIN AT FS 985.00, STR 27. C/A-COMPLETE:REPAIRED EXT FUSELAGE SKIN AT FS 985.00, STR 27 IAW ERS-CR-53MR-3840.
Part: UNKNOWN — ODOR (CABIN) · airframe 21,707 hrs · 15,771 cycles
PLANE SMELL OF SULFUR DURING LANDING ROLL OUT ALSO SMELL OF SULFUR DURING T/O ACCORDING TO FA 2-C/AC/W FIM 79-30-00 AND FIM 21-22-00 . FOR SMOKE/SMELL IN CABIN EVENT. NO ABNORMAL SMELL NOTED AT THIS TIME. REVEALED NO ABNORMALITIES IAW FIM 79-30-00. FCF FOUND SATISFACTORY
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,090 hrs · 15,259 cycles
R/H AFT EXT EMERGENCE LIGHT INOP.-C/A-REPLACED LIGHT BULB IAW AMM 33-84-15-000-801-A09. OPS CHECK OK
2018
Part: ACM — FAILED (RIGHT) · airframe 19,453 hrs · 13,887 cycles
SMOKE IN CABIN WITH APU ON AND THE PACKS ON AT THE GATE. REMOVED AND REPLACED THE RT ACM IAW AMM 21-51-08. OPS CHECKED GOOD IAW AMM 21-51-00-710-801. LEAK CHECKED IAW AMM 21-51-00-790-801. NO LEAKS FOUND.
2017
Part: BLEED VALVE — FAILED (LT ENGINE) · airframe 18,537 hrs · 13,110 cycles
L ENG BLEED CAUTION MSG ENCOUNTERED DURING CLIMBOUT IN ICING COND-C/A-REMOVED AND REPLACED PRSOV VALVE ENG #1 & HIGH STAGE HPRSOV VALVE IAW AMM 36-12-05-000-801 /36-12-01-000-801 OPS CHECK GOOD FCF SATATISFACTORY. PRESSURE REGULATION SHUTOFF VALVE P/N GG670-80002-9 S/N 00353
Part: SHUTOFF VALVE — FAILED (LT ENGINE BLEED) · airframe 18,537 hrs · 13,109 cycles
L ENG BLEED CAUTION-C/A-REMOVED AND REPLACED LH PRSOV IAW CRJ AMM TASK 36-12-01. OPS CHECK GOOD
Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,860 hrs · 11,771 cycles
ROW 5 OVERHEAD EMERG LT INOP. REMOVED AND REPLACED ROW 5 CEILING EMERGENCY LIGHT ASSY IAW AMM 33-51-09. OPS CHECK GOOD. MEL ITEM RESTORED.
Part: ANGLE — CRACKED (PAX DOOR SILL) · airframe 16,822 hrs · 11,738 cycles
PAX DOOR SILL MID CAP ANGLE AT STRINGER 18L IS CRACKED. REMOVED AND REPLACED THE CAP ANGLE IAW SRM 51-41-02.
Part: POST — CRACKED (HAND RAIL) · airframe 16,822 hrs · 11,738 cycles
PASSENGER DOOR FORWARD HAND RAIL UPPER POST IS CRACKED. REMOVED AND REPLACED PAX DOOR FWD UPPER HAND RAIL POST SECTION IAW SRM 51-42-22 AND AMM 52-11-05, OPS CHECKED GOOD.
Part: WEB — CRACKED (BS 202) · airframe 16,822 hrs · 11,738 cycles
LEFT SIDE OF THE FORWARD EQUIPMENT COMPARTMENT WEB FLOOR AT BS 202.75 HAS EVIDENCE OF A .250 INCH CRACK. REPAIRED THE WEB FLOOR IAW ETN-CR-53-099.
2016
Part: PCU — FAILED (RT SPOILER) · airframe 15,488 hrs · 10,664 cycles
INBD SPOILERONS CAUTION DISPLAYED ON APPROACH. EMERGENCY DECLARED DUE TO FLIGHT CONTROL MALFUNCTION. INTERROGATED MDC, FOUND INBD SPOILERONS AND CAUTION MDC MESSAGE. PERFORMS POST 1 RESET AND OPS CHECK IAW ETN CR-27-093. CHECK GOOD. REFER TO TDMI 527T2752N TO R & R THE INBD MFS PCU IN NEXT 10 DAYS. R & R RT INBD MFS PCU IAW AMM 27-62-01, PERFORMED OPS CHECK IAW AMM 27-62-01-710-801. OPS CHECK GOOD TDMI ITEM CLOSED.
Part: SPOILER SYS — MALFUNCTIONED · airframe 15,312 hrs · 10,543 cycles
FLIGHT SPOILERS DEPLOYED AT 6000 FT, TO SLOW AND DESCEND THE AIRCRAFT. CAUTION MESSAGE POSTED ON EICAS . INBD FLT SPOILERS AND INBD SPOILERONS. PERFORMED TEST OF SPOILER STAB IAW AMM 27-61-05 .OPS CHECKED GOOD
Part: RESERVOIR — FAILED (HYDRAULIC SYS) · airframe 14,914 hrs · 10,262 cycles
IN FLIGHT, EICAS CAUTION FOR HYD 3 FLUID TEMP AT 98C. HYD PUMP 3 A TURNED OFF & FLUID TEMP SLOWLY DECREASED TO 75C, GREEN. TRANSFERRED TO NRWC 527-ORD-01776. REFERENCE NRWC 527-ORD-01176. R & R NR 3 HYD FLUID RESERVOIR IAW AMM 29-12-30. OPERATION & LEAK CHECKED GOOD.
2015
Part: IDG — MALFUNCTIONED (NR 2) · airframe 13,833 hrs · 9,437 cycles
NUMBER 2 GEN OFFLINE ON TAKEOFF ROLL, BELOW 80 KNOTS NR 2 GEN OFF & ILLUM ABORTED TAKEOFF. FLIGHT CREW PLACARDED NR 2 INTEGRATED DRIVE GEN IAW 34-02.
Part: MANIFOLD — FAILED (NLG STEERING) · airframe 13,703 hrs · 9,332 cycles
NOSE WHEEL STEERING INOPERATIVE. CAUTION MSG APPEARED DURING GEAR RETRACTION. OPERATED NORMAL AFTER RESET OF CIRCUIT BREAKERS IAW AOM 1. R & R NLG STEERING MANIFOLD IAW AMM 32-51-50. PERFORMED LG EXTENSION & RETRACTION IAW AMM 32-30-00. NO DEFECTS NOTED.
Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 13,555 hrs · 9,200 cycles
INBOARD SPOILERS, INBD SPOILERONS, CAUTION MSG DURING DESCENT. COMPLIED WITH ETN-CR-27-093. PERFORMED RESET, SPOST, IAW AMM 27-61-05. OPERATIONS CHECK OF FLIGHT SPOILERS IAW AMM 27-22-01. OPERATIONS TESTED GOOD. TDMI OPENED TO R & R LT INBD MFS WITHIN 10 DAYS.
Part: ACTUATOR — MALFUNCTIONED (LE SLATS) · airframe 13,294 hrs · 9,004 cycles
SLATS FAIL CAUTION ON APPROACH, SLATS DID NOT DEPLOY. REMAINED AT 0, COMPLIED WITH AOM PROCEDURE, DECLARED AN EMERGENCY PRIOR TO LANDING. TROUBLESHOT IAW FIM TASK 27-81-09-810-802 & INSPECTED ACTUATORS IAW ETN CR-27-084. ADJUSTED RT SLAT DISCONNECT SENSOR AT SLATS 2 & 3, FOUND WITHIN LIMITS IAW AMM 27-81-39. OPS CHECKED GOOD. SLAT OPS CHECKED GOOD IAW AMM 27-52-00. R & R RT WING SLAT ACTUATORS 2 & 3 IAW AMM 27-81-09. OPS CHECKED GOOD IAW AMM 27-50-00.
Part: SLAT — FAILED (WING) · airframe 13,296 hrs · 9,005 cycles
SLATS FAIL IN APPROACH. TROUBLE SHOT IAW FIM TASK 27-81-09-810-802. INSPECTED ACTUATORS IAW ETN CR-27-084. SLAT OPERATIONS CHECKED GOOD IAW AMM 27-52-00.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,137 hrs · 8,880 cycles
SLATS FAIL CAUTION MSG DISPLAYED WHEN SELECTING FLAPS 0 LT SLAT 0, RT SLAT FLATS DEPLOYED. NORMALLY WHEN CONFIGURING. CLEARED FAULTS IAW AMM 45-45-00. PERFORMED OPERATIONAL CHECK OF SLATS & FLAPS SYS IAW AMM 77-50-00. NO FAULTS FOUND, ACFT OK FOR SERVICE.
Part: INDICATOR — TRIPPED (LE SLAT) · airframe 13,051 hrs · 8,817 cycles
SLATS FAIL IN FLIGHT. INTERROGATED MDC, FOUND SLAT ACT JAMMED MECHANICAL MDC MESSAGE. INSPECTED SLAT ACT TRIP INDICATORS. RESET THE TRIPPED INDICATORS & PERFORMED OPERATIONS TEST OF SLATS & FLAP SYSTEM. INSPECTED THE SLAT ACT TRIP INDICATOR & NO TRIP INDICATOR WERE FOUND TRIPPED. NR 4 RT WING WAS TRIPPED & RESET IAW ETN CR-27-084.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 12,946 hrs · 8,727 cycles
SLATS FAIL, CAUTION MSG ON APPROACH SLATS AT 0 ON THE LT WING & ON THE RT. PERFORMED OPERATIONAL CHECK & CLEARED INHIBITS IAW FIM 27-81-00-810-802-A02 & AMM 27-50-00. ALL CHECKED GOOD, NO OTHER DEFECTS NOTED. ACFT OK FOR SERVICE.
Part: ROLLER — DIRTY (CABIN DOOR) · airframe 12,789 hrs · 8,604 cycles
MAIN CABIN DOOR STUCK, COULD NOT OPEN FROM INSIDE. RAMP PERSONNEL GOT IT OPEN FROM OUTSIDE. CLEANED ROLLERS & LUBED DOOR POINTS. MULTIPLE OPERATIONAL CHECKS NORMAL AT THIS TIME. WORK REF FROM AMM SEC 52-11-00, NO OTHER DEFECTS NOTED.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,650 hrs · 8,495 cycles
FOUND DURING PS 1 INSPECTION, AFT EXTERIOR EMER LIGHTS ON LT & RT INOPERATIVE. R & R NR 4 EPSU BATTERY PACK & CHARGER IAW WC 33-002. OPERATIONS CHECKED GOOD AFT EXTERIOR EMERGENCY LIGHTS. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 24500.
Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 12,037 hrs · 8,046 cycles
FIRST OFFICER`S FLASHLIGHT HOLDER BROKEN. R & R FIRST OFFICER`S FLASH LIGHT HOLDER IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.
2014
Part: MOTOR — DEFECTIVE (PAX DOOR) · airframe 11,714 hrs · 7,781 cycles
FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO CLOSE & OPEN. MAIN DOOR ASSIST DEFERRED IAW MEL 52-1, M PROCEDURES COMPLIED WITH. R 7 R PAX DOOR MOTOR ASSEMBLY IAW AMM 52-11-08. OPERATIONS CHECKED GOOD MEL ITEM RESTORED.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 11,528 hrs · 7,612 cycles
FORWARD FLIGHT ATTENDANT FLASHLIGHT IS INOPERATIVE. R & R FWD FLIGHT ATTENDANT FLASHLIGHT AS REQUIRED. OPERATIONS CHECKED GOOD IAW MM 25-61-00.
Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 11,462 hrs · 7,566 cycles
ABORTED TAKEOFF, LT ENG BLEED CAUTION APPEARED AS TAKING RNWY. R & R NR 1 ENG PRSOV IAW AMM 36-12-01. LEAK CHECKED, OPERATIONS CHECKED GOOD.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 10,899 hrs · 7,087 cycles
BELLY FAIRING SUPPORT FLANGE ON FWD EDGE OF THE RT MLG BAY IS CRACKED. INSTALLED NEW SUPPORT IAW AMM 20-21-00 & SRM 51-42-06.
Part: BATTERY — UNKNOWN (CABIN) · airframe 10,899 hrs · 7,087 cycles
WC 33-002 R & R NR 4 EMER LIGHTING BATTERY ASSEMBLY & BATTERY CHARGER PN 2013-1A SN 76034 A3265.
Part: WINDOW — DELAMINATED (COCKPIT) · airframe 10,597 hrs · 6,879 cycles
DURING CLIMB OUT, FIRST OFFICER NOTICED RT SIDE WINDOW HAD DELAMINATED. DURING A 15 MINUTE PERIOD AREA SPREAD APPROX 2/3 OF AN INCH. REMOVED AND REPLACED FO'S SIDE WINDOW IAW CRJ AMM 56-12-01-000/400-801.
Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 10,434 hrs · 6,750 cycles
AFTER TAKEOFF, CLIMBING THROUGH APPROX 1000 FT. INBD FLT SPOILERS CAUTION & INBD SPOILERONS CAUTION DISPLAYED. REMOVED AND REPLACED RT INBD MFS PCU IAW AMM 27-62-01. OP'S AND LEAK CHECKED GOOD.
Part: DRAIN LINE — DISCONNECTED (AC BAY) · airframe 9,896 hrs · 6,389 cycles
SMOKE WAS FILLING COCKPIT & CABIN DURING APU START, BLICING SMELL FOLLOWED AFTER SELECTING PACK ON. TROUBLE SHOT & FOUND SMOKE TO BE CAUSED BY LT PACK. INSTALLED DRAIN HOSE IAW CRJ 700 AMM 21-51-08. NO FURTHER DEFECTS NOTED. MEL RESTORED.
Part: SLAT — MALFUNCTIONED (WING) · airframe 9,510 hrs · 6,129 cycles
DURING APPROACH ON FLIGHT 2752 CREW REPORTED SLATS FAIL & DECLARED EMERGENCY. COMPLIED WITH AOM VOLUME 1 SLATS INDICATED 0 FLAPS CAME DOWN AS NORMAL. THE ACFT WAS REMOVED FROM SERVICE. ACCOMPLISHED POWER OFF RESET & RESET OF SLAT CHANNEL OF SFECU CYCLED SLAT FLAPS SEVERAL TIMES ALL CHECKED NORMAL IAW MM 05-51-49.
2013
Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 8,661 hrs · 5,575 cycles
LANDING GEAR WARNING DISAGREE MESSAGE DURING RETRACTION ON TAKEOFF. RAN EMER CHECK LIST, UNABLE TO CORRECT, INDICATIONS NORMAL FOR GEAR DOWN. RETURNED TO DEPARTURE FOR LANDING ISSUE WAS WITH NOSE GEAR, NOT MAINS. ADJUSTED NLG PROXIMITY SWITCH SENSOR PX22 IAW AMM 32-61-05. OPS CHECKED GOOD.
Part: PROXIMITY SENSOR — UNSERVICEABLE (BRAKE) · airframe 8,492 hrs · 5,464 cycles
CREW REPORTED AT FL 380, RECEIVED A MASTER WARNING BRAKE OVERTEMP INDICATION. THE CREW SLOWED AND DESCENDED TO COMPLY WITH CHECKLIST TO LOWER GEAR. UPON CLEARING INDICATION AND RAISING THE GEAR THEY RECEIVED A GEAER DISAGREE MASTER WARNING. THE CREW COULD NOT CLEAR. THE CREW THEN DECLARED AN EMERGENCY AND DIVERTED. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 3 BRAKE THERMOCOUPLE SENSOR IAW AMM 32-46-01. OPS CHECK GOOD. PERFORMED ADJUSTMENT CHECK OF PROXIMITY NLG SENSOR PX22 IAW AMM 32-61-05, CHECK GOOD. PERFORMED LANDING GEAR EXTENSION & RETRACTION TEST IAW AMM 32-30-00, NO DEFECTS NOTED. THE FUNCTIONAL CHECK FLIGHT WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 8,159 hrs · 5,245 cycles
CREW REPORTED DURING DESCENT, RECEIVED EICAS HYD 2 LOW PRESSURE AND HYD EDP 2A CAUTION MESSAGES. COMPLIED WITH AOM VOL 1 PROCEDURES AND DECLARED AN EMERGENCY. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND NR 2 ENGINE HYD PUMP LEAKING. R & R PUMP IAW AMM 29-11-01. OPS CHECKED GOOD. NO LEAKS NOTED. ACFT RETURNED TO SERVICE.
Part: FLASHLIGHT ASSY — INTERMITTENT (CABIN) · airframe 8,003 hrs · 5,138 cycles
THE CREW REPORTED THE NR 1 F/A FLASHLIGHT WAS CHARGING INTERMITTENTENTLY. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 1 F/A FLASHLIGHT ASSY IAW AMM 25-61-02. THE OPS TEST WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
2012
Part: FLOORBEAM — CRACKED (BS 280.00) · airframe 5,634 hrs · 3,630 cycles
FLOORBEAM ANGLE FORWARD OF FS 280 CRACKED. REPAIRED IAW EO CR-53MR-292.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 5,653 hrs · 3,640 cycles
DURING C CHECK INSPECTION, FOUND RIGHT ANGLE FOR COCKPIT FLOOR PANEL 221ALF IS CRACKED AT THE AFT CORNER RBL 90 AND FS 280. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT FLOOR SUPPORT IAW SRM 51-42-06 AND EO NR CR-53MR-289. AIRCRAFT RETURNED TO SERVICE.
2011
Part: SEAL — BROKEN (DEFIBRILLATOR) · airframe 3,313 hrs · 2,199 cycles
DURING INSPECTION FOUND DEFIBRILLATOR SEAL BROKEN AND MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DEFIBRILLATOR SEAL. THE AIRCRAFT WAS RETURNED TO SERVICE.