N539EA
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.
103 reports on file, 2011-08-20 – 2025-03-03.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON STRINGER AND SPLICE 24RH BTW FS319.70 TO FS349 AT MAIN AVIONICS COMPARTMENT. STRINGER SPLICE 24RH ON FS 333.00 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON STRINGERS 26RH AND 27 BTW FS295 TO FS319.70 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER 26RH, BTW FS295 TO FS319.70 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ 700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-21-03-101-002-A01, STRINGER 27 BTW FS295 TO FS319.70 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01
Part: SKIN — DAMAGED (ZONE 800) · airframe 31,252 hrs · 24,855 cycles
ELONGATED DRILL HOLES ON DOOR LOWER SKIN WAS FOUND. AFTER REMOVE LOWER SEAL RETAINER DOOR SKIN AT FWD CARGO COMPARTMENT DOOR. ELONGATED DRILL HOLES ON DOOR LOWER SKIN WAS FOUND. AFTER REMOVE LOWER SEAL RETAINER DOOR SKIN AT FWD CARGO COMPARTMENT DOOR WERE REPAIRED PER REO 670-52-35-535 REV. - -.
Part: ANGLE — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON ANGLE (FS549.00, STRINGER 15L TO 18L)(SH670-33119-1) AT FRAME 549.00 LH SIDE WAS FOUND. CORROSION ON ANGLE (FS549.00, STRINGER 15L TO 18L)(SH670-33119-1) AT FRAME 549.00 LH SIDE WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-31-06-101-002-A01 AND MUST BE REPLACED UNDER NRC 00098.
Part: CANISTER — CRACKED (ZONE 600) · airframe 31,252 hrs · 24,855 cycles
IN REF. TO TASK CARD TRFKE0013UTU:600-09E1-JIC, IT WAS DETECTED CRACK IN CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, ON WS148.01 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -.
Part: FITTING — CORRODED (RH AILERON) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON BORE LUGS NO.2R AND NO.5R AT RH AILERON CENTER FITTING. BORE LUGS NO.2R AND NO.5R AT RH AILERON CENTER FITTING WERE REPAIRED PER REO REO 670-57-61-237 REV --
Part: CROSSBEAM — WORN (ZONE 400) · airframe 31,252 hrs · 24,855 cycles
LH CROSSBEAM AT FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND PER CRJ700 SRM 51-42-06-001-001-A01. AFT EDGE, OUBD SIDE OF UPPER/LOWER FWD CORE COWL AT LH ENGINE WERE REPAIRED PER REO 670-54-23-1286 REV - - AND REO 670-54-23-1287 REV --
Part: SKIN — WORN (ZONE 400) · airframe 31,252 hrs · 24,855 cycles
WEAR ON AFT EDGE OUBD SIDE OF UPPER/LOWER FWD CORE COWL AT RH ENGINE. AFT EDGE OUBD SIDE OF UPPER FWD CORE COWL AT RH ENGINE WAS REPAIRED PER REO 670-54-23-1288 REV. - -. LOWER FWD CORE COWL AT RH ENGINE MUST BE REPLACED UNDER NRC 00122.
Part: FITTING — CORRODED (LH AILERON) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON BORE LUGS L5, L2, L1. AND SCRATCH ON LUG L3. AT LH AILERON CENTER FITTING. BORE LUGS L5, L2, L1. AT LH AILERON CENTER FITTING WERE REPAIRED PER REO 670-57-61-237 REV -- & L3 WAS CLEANED PER CRJ 700 SRM TASK 51-26-00-001-001-A01 PAR 5 B CLEANING AND CRJ 700 NDT MANUAL 51-20-009-210-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
AFTER REMOVAL OF FLOOR PANEL SUPPORT ANGLE, CORROSION WAS FOUND ON LH CROSSBEAM AT FS 280.00. LH CROSSBEAM AT FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND PER CRJ700 SRM 51-42-06-001-001-A01.
Part: SUPPORT ANGLE — CRACKED · airframe 31,252 hrs · 24,855 cycles
CRACK ON ANGLE SUPPORT FOR ACCESS PANELS 542AZ, 642AZ AT REAR AUXILIARY SPAR LH/RH WING. ANGLE SUPPORT FOR ACCESS PANELS 642AZ AT REAR AUXILIARY SPAR RH WING WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND ANGLE SUPPORT FOR ACCESS PANELS 542AZ AT REAR AUXILIARY SPAR LH WING WAS FABRICATED PER DWG CC670-10338 REV.-A AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SIDE SEAT RAIL 3 EAS AT STGR 15RH BTW STA 379 TO STA 677. SIDE SEAT RAIL 3 EAS AT STGR 15RH BTW STA 379 TO STA 677 WERE FOUND OUT OF LIMITS PER CRJ 700 SRM 53-21-49-101-001-A01,SRM 53-31-49-101-001-A01 AND SRM 53-41-49- 101-001-A01 THEREFORE WERE REPLACED PER CRJ/700 AMM 53-00-49 (CONFIG A03).
Part: SHIM — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SHIMS (4 EAS) BTW FS1031 TO FS1047 ALSO FS1000 TO FS1015 BTW STGR 27 TO 26LH AT AFT BAGGAGE BAY. CORROSION ON SHIMS (4 EAS) BTW FS1031 TO FS1047 ALSO FS1000 TO FS1015 BTW STGR 27 TO 26LH AT AFT BAGGAGE BAY WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WERE REPLACED PER CRJ700 SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SEAT RAIL 3 EAS AT RBL 9 BTW STA 349 TO STA 677. SEAT RAIL 2 EAS AT RBL 9 BTW STA 349 TO STA 581 WERE CLEANED PER CRJ/700 SRM 51-26-00-001-001-A01 AND INSPECTED PER CRJ-700 SRM 51-26-00-001-001-A01 AND NO DAMAGE CORROSION WAS FOUND AND SEAT RAIL (1EA) AT RBL9 BTW FS.581 TO FS. 677 WAS REPLACED PER CRJ700 AMM 53-00-49-400-801-A03.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SIDE SEAT RAIL 5 EAS AT STGR 15LH BTW STA 379 TO STA 761. SIDE SEAT RAIL 5 EAS AT STGR 15LH BTW STA 379 TO STA 761 WERE FOUND OUT OF LIMITS PER CRJ 700 SRM 53-21-49-101-001-A01 ,SRM 53-31-49-101-001-A01 , AND SRM 53-41-49- 101-001-A01 THEREFORE WERE REPLACED PER CRJ-700 AMM 53-00-49 (CONFIG A03)
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SIDE SEAT RAIL 2 EAS AT STGR 15LH BTW STA 785 TO STA 977. SEAT RAIL (1EA) AT STGR 15LH BTW STA 785 TO STA 863 WAS FOUND OUT OF LIMITS PER CRJ/700 SRM 53-41-49-101-001-A01 THEREFORE WAS REPLACED PER CRJ700 AMM 53-00-49 (CONFING A03) AND SEAT RAIL 1 EA AT STGR 15LH BTW STA 863 TO STA 977 WAS CLEANED PER CRJ/700 SRM 51-26-00-001-001-A01 AND WAS RE-INSPECTED PER CRJ/700 NDTM PART 01 TASK 51-20-009-210 (CONFIG A01) AND NOT CORROSION FOUND
Part: STIFFENER — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON STIFFENERS (2 EAS) AND DRAINS, FS985 TO FS1000 AND BTW STGR 26LH TO 25LH. STIFFENERS (2 EAS) AND DRAINS, FS985 TO FS1000 AND BTW STGR 26LH TO 25LH WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01, MANUFACTURATED PER DWG MM670-62652 REV. A AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. FINISH ON DRAIN 1(EA) FS985 TO FS1000 AND BTW STGR 26LH TO 25LH AND DRAIN REMAINING 1(EA) WAS REMOVED PER CRJ700 SRM 51-26-01-001-001-A01, GENERAL VISUAL INSPECTION WAS PERFORMED PER CRJ700 NDTM PART 01 TASK 51-20-009-210 (CONFIG A01) AND NO CORROSION FOUND AND WERE RE-FINISHED PER CRJ700 SRM 51-21-11-001-001-A01, ,CRJ700 SRM 51-25-06-001-001-A01 AND CRJ700 SRM 51-25-16-001-001-A01.
Part: SKIN — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON CUT OUT INNER FACE AT E/E DOOR SETTLEMENT AREA. CORROSION ON CUT OUT INNER FACE AT E/E DOOR SETTLEMENT AREA WAS REPAIRED PER REO 690-53-21-032 REV - -
Part: RIB — CORRODED (ZONE 600) · airframe 31,252 hrs · 24,855 cycles
GOUGES ON RH WING TE ASSY, RIB FLS13.65. RIB WAS REPLACED PER REO 670-57-51-590 REV - -.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON INTERCOSTAL STGR 20RH FS310 TO FS319.70 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL STGR 20RH FS310 TO FS319.70 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-002-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON FRAME FS295 BTW STGR 25RH TO 25LH, AT MAIN AVIONICS COMPARTMENT. CORROSION ON FRAME FS295 BTW STGR 25RH TO 25LH, AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-06-101-001-A01 AND WAS REPAIRED PER CRJ-700 SRM 53-00-06-201-006-A01
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON STRINGER AND SPLICE 26RH BTW FS319.70 TO FS349 AT MAIN AVIONICS COMPARTMENT. VALUATED, AFTER PAINT REMOVAL ON STRINGER 26RH BTW FS319.70 TO FS349 AT MAIN AVIONICS COMPARTMENT VISUAL INSPECTION WAS PERFORMED PER CRJ/700 NDTM PART 01 TASK 51-20-009-210 (CONFIG A01) AND NOT CORROSION FOUND AND DUE EXCESSIVE DAMAGE ON SPLICE 26RH BTW FS319.70 TO FS349 AT MAIN AVIONICS COMPARTMENT PER CRJ 700 SRM 53-00-00·101·A01 AND REPLACED PER CRJ700 SRM 51-42â¢06-001-001·A01 AND CRJ700 SRM 51-42â¢21-001-001·A01.
Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON STRINGER AND SPLICE 25RH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STRINGER AND SPLICE 25RH BTW FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND CRJ700 SRM 53-00-00-101-001-A01, SPLICE 25RH FS333.00 WAS MANUFACTURED PER DWG SH670-32429 REV. A. AND WERE REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01.
Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON INTERCOSTAL STGR 21LH FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT. INTERCOSTAL STGR 21LH FS310 TO FS333 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01
Part: SKIN — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON DRAIN HOLES ON FS946 BTW STGR 26L-26R AT AFT FUSELAGE. CORROSION ON DRAIN HOLES ON FS946 BTW STGR 26L-26R AT AFT FUSELAGE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND REPAIRED PER REO 670-53-51-340 REV- -.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SEAT RAIL 3 EAS AT LBL 9 BTW STA 379 TO STA 677. SEAT RAILS 2 EAS AT LBL 9 BTW STA 379 TO STA 581 WERE CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND WERE REINSPECTED PER CRJ/700 NDTM PART 01 TASK 51-20-009-210 (CONFIG A01) AND NOT CORROSION FOUND, AND SEAT RAIL BTW LBL 9 BTW STA 581 TO STA 677 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-31-49-101-001-A01, SRM 53-31-49-101-001-A01 AND SRM 53-41-49-101-001-A01, AND WAS REPLACED PER CRJ700 AMM 53-00-49 CONFIG.A03
Part: SUPPORT FITTING — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON JACK FITTING SUPPORT RH/LH SIDE FS 265 TO FS 280 BL 0 AT INTERNAL FUSELAGE. CORROSION ON JACK FITTING SUPPORT RH/LH SIDE FS 265 TO FS 280 BL 0 AT INTERNAL FUSELAGE WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01, JACK FITTING SUPPORT RH WAS EVALUATED WITHIN LIMITS AND JACK FITTING SUPPORT LH WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-10-001-001-A01 AND PER CRJ700 SRM 51-42-21-001-001-A01.
Part: HINGE — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON AFT, MIDDLE AND FWD HINGE AT STEP PLATE C2, AND ILLEGIBLE BLACK/YELLOW MARKING AND DECAL OF FLAP STEP PLATE. AFT, MIDDLE AND FWD HINGE AT STEP PLATE C2 WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-61-58-101-001-A01 AND WERE REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND BLACK/YELLOW MARKING WERE RESTORED PER CRJ700 SRM 51-25-06-001-001-A01 AND PER CRJ700 SRM 51-25-01-001-001-A01-PSA AND DECAL WAS REPLACED PER CRJ700 AMM 20-60-04 CONFIG.A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SIDE SEAT RAIL 2 EAS AT STGR 15RH BTW STA 785 TO STA 977. EVALUATED, DUE TO ONLY ONE TYPE OF DAMAGE IS ALLOWED AT ANY TYPICAL CROSS-SECTION ALONG THE LENGTH OF A SIDE SEAT RAIL 2 EAS AT STGR 15RH BTW STA 785 TO STA 977 AT PASSENGER CABIN PER CRJ 700 SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A01 , SRM 53-41-49- 101-001-A01 AND REPLACED IAW AMM 53-00-49 ( CONFIG A03 ).
Part: HOUSING — WORN (ZONE 800) · airframe 31,252 hrs · 24,855 cycles
WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. WEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV -B
Part: FRAME — WORN (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
WEAR ON FRAME AT FS1162 AND BTW STGR 7L-8L AT AFT ACCESSORIES COMPARTMENT. FRAME AT FS1162 AND BTW STGR 7L-8L AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER REO 670-53-71-096REV. - - AND REO 670-53-71-047 REV. -A.
Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON LH FLOOR POST AT FS 280 AND LBL 11.16 WAS FOUND. CORROSION ON LH FLOOR POST AT FS 280 AND LBL 11.16 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER PER CRJ700 SRM 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON FLOOR SUPPORTS (7EAS) LOCATED BTW FS280 TO FS310 AND LBL20'' AND LBL38'', RBL4'', RBL 18'' RBL38" AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (7EAS) LOCATED BTW FS280 TO FS310 AND LBL20'' AND LBL38'', RBL4'', RBL 18'' RBL38" AT FUSELAGE FLOOR STRUCTURE WERE FOUND OUT OF LIMITS PER CRJ700 SRM 51-42-21-001-001-A01 THEREFORE WERE REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01.
Part: ACCESS PANEL — CORRODED · airframe 31,252 hrs · 24,855 cycles
CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB. CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. LANDING DOOR SECTION AND STRAP AFT SIDE WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-10-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01. RH AND LH SIDE WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-00-00-101-001-A01.
Part: SUPPORT — CRACKED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
IN REF TO: DURING INSPECTION OF THE TASK CARD 100-08E2-JIC CRACK ON AFT REFUEL DUCT MOUNTING SUPPORT BTW FS677.00 TO FS669.4 AND STGR 21RH TO STGR 22RH WAS DETECTED.. AFT REFUEL DUCT MOUNTING SUPPORT BTW FS677.00 TO FS669.4 AND STGR 21RH TO STGR 22RH WAS REPAIRED PER REO 670-28-25-014 REV. --
Part: FRAME — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON FRAME FS319.70 BTW STGR 19LH TO 21LH AND 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT. SECTION OF FRAME FS319.70 BTW STGR 19LH TO 21LH WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-06-201-005-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-01-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. CORROSION ON SECTION OF FRAME FS319.70 BTW STGR 24LH TO 25RH WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-00-01-101-001-A01
Part: BRACKET — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON PLATES (5EAS) UPPER FACE ON FWD CARGO COMPARTMENT. PLATE (1EA) WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-32-58-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01. PAINT ON AREAS ON MACHINED BRACKETS (PLATES) (4EAS) WAS REMOVED PER CRJ700 SRM 51-26-01-001-001-A01, AREAS WERE CLEANED PER CRJ700 SRM 51-26-00-001-001-A01, NO CORROSION DAMAGE WAS FOUND AND WERE PAINTED PER CRJ700 SRM 51-25-16-001-001-A01.
Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON HYD LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LH/RH (4 E/A'S) AT RH/LH MAIN WHEEL WELL. CORROSION ON HYD LINES SUPPORT PLATES (IN BK, LG EXT, LG RET) LH/RH (4 E/A'S) AT RH/LH MAIN WHEEL WELLWAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND SUPPORT PLATES (2EAS) WERE EVALUATED WITHIN LIMITS AND SUPPORT PLATES OF HYD LINES LH & RH (2EAS) (IN BK,OBBK,LG EXT,LG RET ) WERE EVALUATED OUT OF LIMITS PER CRJ700 53-00-00-101-001-A01 AND WERE REPLACED PER CRJ700 SRM 51-41-02-001-001-A01
Part: FRAME — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON FRAME AT FS 549.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX. CORROSION ON FRAME AT FS 549.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-31-06-101-002-A01 AND FRAME WAS REPAIRED PER REO 670-53-31-1006 REV. - -
Part: ANGLE — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON JOINT ANGLE AT WING TO FUSELAGE FAIRINGSUPPORTFS939BTWSTGR26L-26R. EVALUATED, DUE TO EXCESSIVE ALLOWABLE DAMAGE ON JOINT ANGLE AT WING TO FUSELAGE FAIRING SUPPORT FS939 BTW STGR 26L-26R PER CRJ-700 SRM 53-00-01-101-001-A01 AND REPLACED PER CRJ-700 SRM51-42-06-001-001-A01.
Part: FRAME — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON FRAME FS310 BTW STGR 26RH TO 26LH, AT MAIN AVIONICS COMPARTMENT. FRAME FS310 BTW STGR 26RH TO 26LH, AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-06-101-002-A01 AND WAS REPAIRED PER CRJ700 SRM 53-00-06-201-006-A01
Part: REPAIR — WORN (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
WEAR ON PREVIOUS REPAIR DOUBLER, LOCATED BTW FS985 TO FS969 AND STGR 26L TO 26R. PREVIOUS REPAIR DOUBLER, LOCATED BTW FS985 TO FS969 AND STGR 26L TO 26R WAS REPAIRED PER REO 670-53-00-290 REV.-F
Part: FRAME — CORRODED (ZONE 200) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON FRAME AT FS 565.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX. CORROSION ON FRAME AT FS 565.00 BTW STGR 16 TO STGR 17 LH SIDE AT CPAX WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS REPAIRED PER REO 670-53-31-1007 REV. - -.
Part: SPAR — CRACKED (ZONE 800) · airframe 31,252 hrs · 24,855 cycles
CRACK ON FRONT SPAR OF LH MAIN LANDING GEAR DOOR. FRONT SPAR OF LH MAIN LANDING GEAR DOOR WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, PER CRJ700 SRM 51-42-21-001-001-A01 AND PER CRJ700 SRM 51-42-10-001-001-A01
Part: ACCESS PANEL — CORRODED (ZONE 800) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON ACCESS PANEL 832DT AND 832AT. CORROSION ON ACCESS PANEL 832DT AND 832AT WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01. ACCESS PANEL 832DT WAS EVALUATED WITHIN LIMITS PER CRJ700 SRM 52-11-04-101-001-A01. ACCESS PANEL 832AT MUST BE REPLACED UNDER NRC 00057.
Part: SUPPORT PLATE — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON METAL SUPPORT OF CONNECTORS PX34-PX33/ PX17-PX33 RH/LH SIDE AT WHEEL WELL AREA. CORROSION ON METAL SUPPORT RH OF CONNECTORS PX34-PX33/ PX17-PX33 AT WHEEL WELL AREA WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND EVALUATE WITHIN LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND METAL SUPPORT RH OF CONNECTORS PX34-PX33/ PX17-PX33 AT WHEEL WELL AREA WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01
Part: HINGE — CORRODED (ZONE 100) · airframe 31,252 hrs · 24,855 cycles
CORROSION ON HINGES AND HINGE FITTINGS AT AFT LAVATORY SERVICE DOOR 196ER AND WEAR ON HINGES (2 E/AS) OF ACCESS PANEL 195CB (ATACHMENT HARDWARE INCLUED). HINGES (2 E/AS) OF ACCESS PANEL 195CB WERE CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND NO DAMAGES WERE FOUND AFTER CLEANED, PAINT ON HINGE (2EAS) WAS REMOVED PER CRJ-700 SRM 51-26-01-001-001 A01 AND WERE INSPECTED PER CRJ-700 NDTM PART 01 TASK 51-20-009-210 (CONFIG A01) AND NO CORROSION FOUND, AND HINGES (P/N:CC670-39096-1) AND (P/N:CC670-39095-1) WERE REPLACED PER CRJ700 SRM 51-41-02-001-001-A01
Part: EXHAUST CONE — DENTED (RT ENGINE) · airframe 31,252 hrs · 24,855 cycles
DENT ON EXHAUST NOZZLE BTW 9-10 O'CLOCK POSITION AT RH ENGINE. DENT ON EXHAUST NOZZLE BTW 9-10 O'CLOCK POSITION AT RH ENGINE WAS REPAIRED PER REO 670-51-00-085 REV.-A AND PER REO 670-54-15-933 REV - -
Earlier reports · 2011–2024 · 55 reports
2024
Part: SELECTOR VALVE — FAULTED (ZONE 700) · airframe 30,363 hrs · 24,136 cycles
GEAR DISAGREE WARNING MSG. / REMOVED AND REPLACED SELECTOR VALVE IAW CRJ700 AMM 32-32-10-000/400-801-A01. ALL OPS CHECKS GOOD AT THIS TIME NO LEAKS NOTED. THIS CLEARS MEL.
Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 30,361 hrs · 24,134 cycles
PROX SYSTEM CAUTION MSG IN FLIGHT / C/W POWER-UP TEST OF LANDING GEAR PSS IAW CRJ 700 AMM 32-61-00-740-801. OPS CHECK GOOD
Part: CONTROL PANEL — FAILED (TRIM SYS) · airframe 29,820 hrs · 23,690 cycles
AILERON TRIM STUCK LEFT WING DOWN. TRIM WILL NOT MOVE, KEPT GETTING AP TRIM IS LWD CAUTION MSG. / REMOVED AND REPLACED AILERON/RUDDER TRIM CONTROL PANEL AND PERFORMED SATISFACTORY OPS TEST OF AILERON TRIM AND RUDDER TRIM IAW CRJ700 AMM 27-12-10-000/400-801-PSA, AMM 27-11-00-710-802, AMM 27-22-00-710-801. NO DEFECTS NOTED.
2023
Part: CONTROLLER — UNSERVICEABLE (100) · airframe 29,259 hrs · 23,229 cycles
HAVING ISSUE WITH HEAT PRESSURIZATION DIFF INCREASING, DESENDING EMERGENCY DECLARED / REMOVED AND REPLACED LH ACSC IAW CRJ 700 AMM 21-61-04-000/400-801-A01. PERFORMED IN-BITE TEST OF ACSC IAW CRJ 700 AMM 21-61-04-740-801-A01. TEST PASSED. PERFORMED OPERATIONAL CHECK OF TEMPERATURE CONTROL SYSTEM IAW CRJ 700 AMM 21-60-00-710-801-A01. NO DEFECTS NOTED AT THIS TIME. PERFORMED PRESSURIZATION OF AIRCRAFT IAW CRJ 700 AMM 21-31-00-910-801-A01-PSA. NO DEFECTS NOTED AT THIS TIME.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 28,342 hrs · 22,416 cycles
RED PASSENGER DOOR WARNING MESSAGE IN CLIMB THROUGH F220. FA REPORTS HANDLE MOVED UP TO HALF WAY BETWEEN FULL OPEN AND FULL CLOSE. / ADJUSTED PAX DOOR LATCH MECHANISM IAW CRJ700 AMM 52-11-02-820-801-A02.PAX DOOR AND INDICTION OPS CHECKS GOOD IAW AMM 52-11-00-710-801.
2022
Part: ANGLE — CRACKED (BS 280 S3L) · airframe 27,464 hrs · 21,621 cycles
WHILE PERFORMING SB670BA-53-040 VISUALLY FOUND CRACK ON STR 3L AT FS 280 FIRST 2 HOLES. PERFORM REO 670-53-21-493 REV -D DATED 2015-07-10
2021
Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 24,232 hrs · 18,717 cycles
IN-FLIGHT DEPLOYED FLIGHT SPOILERS GOT OB FLT SPLRS AND OB SPOILERONS CAUTION MESSAGE FLT PAGE SHOWED OB RIGHT IN AMBER AND OB LEFT IN WHITE AND COMPLETED QRC AND QRH AND MESSAGE STAYED ON / REPLACED RIGHT O/B MFPCU IAW CRJ 700 AMM 27-62-01-000/400-801-A02-PSA OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.
Part: UNKNOWN — SMOKE (CABIN) · airframe 24,203 hrs · 18,696 cycles
WITH BOTH PACKS ON, GOT SMOKE IN LAST 3 ROWS OF CABIN AND IN COCKPIT WITH A BURNING PAPER SMELL. PACKS WERE ON APU BLEED AIR / PERFORMED FIM STEPS OF SMOKE AND/ ABNORMAL SMELL IN THE COCKPIT AND CABIN IAW CRJ 700 FIM 21-21-00-810-806(CONFIG A01) AND FIM 21-22-00-810-806(CONFIG A01) RESPECTIVELY. PERFORMED OPS. TEST OF AIR CONDITIONING DISTRIBUTION SYS. PER AMM 700 AMM 21-51-00-710-801. OPS. TEST IS GOOD.
Part: OUTFLOW VALVE — OBSTRUCTED (CABIN PRESSURE) · airframe 23,759 hrs · 18,302 cycles
LOSS OF CABIN PRESSURIZATION AT 33,000FT DESCENDED DOWN TO 10,000 AND DIVERTED TO TYS. CREW DEPLOYED OXYGEN MASKS AND HAD FIRE AND RESCUE TRUCKS ROLL IN TYS TO ASSIST PASSENGERS. EMERGENCY BRIDGELINE WAS OPENED BY OCC IN DAY AND BY MAINLINE IOC IN DFW. INTERROGATED MDC. FOUND B-1 CODES 006171 & 006172 IN SERVICE MESSAGE HISTORY. VISUALLY INSPECTED SAFETY VALVES NR 1 & 2. FOUND FOUR INSULATION BLANKETS TO BE INHIBITING PROPER VALVE OPERATION & BLANKETS DAMAGED.
Part: RIB — CRACKED (ZONE 600) · airframe 23,753 hrs · 18,296 cycles
RIGHT HAND WING LEADING EDGE INBOARD MACHINED RIB CRACKED AT 15.50.
Part: DOOR FRAME — CORRODED (CARGO DOOR SILL) · corrosion level 2 · airframe 23,753 hrs · 18,296 cycles
AFT CARGO DOOR SILL AFT INNER CHORD CORRODED.
Part: DOOR FRAME — CORRODED (CARGO DOOR SILL) · corrosion level 2 · airframe 23,753 hrs · 18,296 cycles
AFT CARGO DOOR LOWER SILL CORRODED.
2020
Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,342 hrs · 17,023 cycles
FLIGHT DECK FLOORBEAM AT LBL 9.00 IS CRACKED JUST FWD OF FS 280. REMOVED 221ALF LH FLOOR SUPPORT ANGLE AND FOUND TO BE CRACKED IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. CUT AWAY DAMAGE AT LH FLOOR BEAM IAW REPAIR C STEP 1,2 REO 670-53-11-896 REV--. CUT LINE EDGES REQUIRE NDT IAW STEP 3 OF REO 670-53-11-896 REV--. PERFORMED EDDY CURRENY OF FLOORBEAM CUTLINE EDGES FWD FS 280 IAW REO 670-53-11-896 STPE 3. NO INDICATIONS NOTED AT THIS TIME. FABRICATED REPAIR PART 25 IAW CRJ 700 SRM 53-11-43-201-003-A01. REPAIRED PARTS HEAT TREATED IAW AMS 2770 REV P. LOCATED, DRILLED & CSK REPAIR PARTS IAW 670-53-11-396 REV--, AND SRM 53-11-43-201-003-A01.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,342 hrs · 17,023 cycles
FLIGHT DECK FLOORBEAM AT RBL 9.00 IS CRACKED JUST FWD OF FS 280. REMOVED 221ALF RH FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-010-A01. CUT AWAY DAMAGE RH FLOOR BACK IAW REO 670-53-11-896 REV-, REPAIR C STEPS 1,2. PERFORMED EDDY CURRENT OF RBL 9 FLOORBEAM CUTLINE EDGES FWD OF FS 280 IAW REO 670-53-11-896 STEP 3. NO INDICATIONS NOTED AT THIS TIME. FABRICATED REPAIR PART 26 IAW SRM 53-11-201-003-A01. FABRICATED REPAIR PARTS, HEAT TREATED IAW AMS 2770 REV P. ON FURTHER EVALUATION, FOUND THAT REPAIR TYPE 4 IS REQUIRED IAW SRM 53-11-43-201-003-A01. FABRICATED REPAIR PARTS 36, 38, 40 & 42 IAW SRM 53-11-43-201-003-A01 TYPE 4. INSTALLED REPAIR PART & TOUCH UP PAINT IAW SRM 53-11-43-201-003-A01 & TR 51-00965 REPAIR TYPE IV.
Part: BULKHEAD — CRACKED (BS 280) · airframe 22,342 hrs · 17,023 cycles
RT FS 280 LOWER BULKHEAD WEB HAS CORROSION MULTIPLE AREAS. C/W STEPS 1-3 OF ENGINEERING, CUTOUT OF DAMAGE REF REO 670-53-11-594 REV A. CONTINUED WITH ENGINEERING STEP 4. MANUFACTURED REPAIR PARTS AS REQUIRED. REF REO 670-53-11-594 REV A STEP 4. WEB INSTALLED ALL REPAIR PARTS, REF REO 670-53-11-594 STEPS 5-7. C/W STEPS 5-7 OF REO 670-53-11-594 REV A DATED 06/26/15. PRIME AND PAINT FS 280 BULHEAD DAR GREY REO 670-53-11-594 STEP 8. C/W STEP 8 OF REO 670-53-11-594 REV A DATED 06/26/15. C/W REMAINING STEPS OF REO. C/W STEP -12 OF REO 670-53-11-594 REV A DATED 06/26/15.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 22,342 hrs · 17,023 cycles
LH FS280 CROSSBEAM IS CRACKED JUST O/B OF LBL9. REMOVED UNSERVICEABLE LH FS 280 CROSSBEAM, LOCATED & DRILLED NEW SERVICEABLE LH FS 280 CROSSBEAM PN CC670-34094-1 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE LH FS 280 CROSSBEAM PN CC670-34094-1 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. FOUND FS 280 FWD J ANGLE TO BE CORRODED. . FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FS 280 FWD J ANGLE IAW SRM 51-40-11-001-010-A01, 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
Part: BULKHEAD — CORRODED (BS 280) · corrosion level 2 · airframe 22,342 hrs · 17,023 cycles
RHFS 280 LOWER BULKHEAD WEB HAS CORROSION MULTIPLE AREAS. C/W STEPS 1-3 OF ENGINEERING, CUTOUT OF DAMAGE REF REO 670-53-11-594 REV A. CONTINUED WITH ENGINEERING STEP 4. MANUFACTURED REPAIR PARTS AS REQUIRED. REF REO 670-53-11-594 REV A STEP 4. WEB INSTALLED ALL REPAIR PARTS, REF REO 670-53-11-594 STEPS 5-7. C/W STEPS 5-7 OF REO 670-53-11-594 REV A DATED 06/26/15. PRIME AND PAINT FS 280 BULHEAD DAR GREY REO 670-53-11-594 STEP 8. C/W STEP 8 OF REO 670-53-11-594 REV A DATED 06/26/15. C/W REMAINING STEPS OF REO. C/W STEP -12 OF REO 670-53-11-594 REV A DATED 06/26/15
Part: CROSSBEAM — CRACKED (BS 280) · airframe 22,342 hrs · 17,023 cycles
WHILE PERFORMING SB670BA-53-041 FOUND RH FS 280 CROSSBEAM CRACKED. REMOVED RH FS 280 CROSSBEAM REF CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01. INSTALLED NEW SERVICEABLE BEAM IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01. LOCATED AND DRILL NEW CROSSBEAM. LOCATED AND DRILLED FASTENER HOLES FOR NEW RH FS 280 CROSSBEAM. REF SRM 51-40-11-001-001-A01.
Part: POST — CORRODED (BS 280) · corrosion level 2 · airframe 22,342 hrs · 17,023 cycles
FS 280 VERTICAL FLOOR POST AT RBL 9.00 IS CORRODED AT LWR POSITION. REMOVED FASTENERS COMMON TO FS 280 WEB IAW SRM 51-42-06-001-001-A01, 51-40-21-001-001-A01, 51-42-22-001-001-A01. DRILLED, LOCATED NEW SERVICEABLE CC670-34180-8 POST IAW SRM 51-40-06-001-001-A01. INSTALLED NEW SERVICEABLE CC670-34180-8 POST IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. NO FURTHER MAINT ACTION REQUIRED.
2018
Part: DOOR SEAL — DEFECTIVE (PAX DOOR) · airframe 19,709 hrs · 14,629 cycles
LOUD SQUEAL FROM PAX DOOR. THE AIRCRAFT DIVERTED AND NO EMERGENCY DECLARED. MAINTENANCE REPLACED THE PASSENGER DOOR SEAL.
2017
Part: WEB — CRACKED (E/E BAY) · airframe 16,735 hrs · 11,893 cycles
LEFT SIDE OF THE FORWARD EQUIPMENT COMPARTMENT WEB FLOOR PANEL HAS EVIDENCE OF A 3/8 INCH CRACK IN THE CORNER. REPAIRED FLOOR WEB IAW ETN-CR-53-099.
Part: ACTUATOR — FAILED (SLAT SYSTEM) · airframe 16,065 hrs · 11,359 cycles
SLAT FAIL CAUTION MESSAGE WHEN SELECTED TO ONE, WHEN SLOWING DOWN FOR APPROACH. LANDED WITH SLATS AT 0 AND FLAPS AT 45. REMOVED AND REPLACED THE LEFT SLAT ACTUATORS NR 5 AND 6, RT SLAT ACTUATORS NR 4 AND 5 IAW AMM 27-81-09.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,942 hrs · 11,248 cycles
OVERWING EMERGENCY LIGHTS ON BOTH SIDES INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-17.
Part: STAND OFF — CRACKED (LT NACELLE) · airframe 15,654 hrs · 11,010 cycles
LEFT LOWER TRANSCOWL INBD STANDOFF HAS TWO .750 INCH CRACKS. REMOVED AND REPLACED THE STANDOFF IAW SRM 51-42-14, SRM 51-42-21 AND ETN-CR-54-015R1
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,654 hrs · 11,010 cycles
PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED THE DRAG ANGLE IAW SRM 52-11-04.
Part: HANDLE — CRACKED (PAX DOOR INNER) · airframe 15,654 hrs · 11,010 cycles
PAX DOOR INNER HANDLE IS CRACKED AT THE TORQUE TUBE. REMOVED AND REPLACED THE HANDLE IAW AMM 52-11-02, OPS CHECKED GOOD.
Part: STAND OFF — CRACKED (LT NACELLE) · airframe 15,654 hrs · 11,010 cycles
LEFT UPPER TRANSCOWL INBD STANDOFF HAS A .750 CRACK. REMOVED AND REPLACED THE STANDOFF IAW SRM 51-42-14 AND SRM 51-42-21 AND ETN-CR-54-015R1
Part: STAND OFF — CRACKED · airframe 15,654 hrs · 11,010 cycles
RIGHT UPPER TRANSCOWL INBD STANDOFF HAS TWO .750 INCH CRACKS. REMOVED AND REPLACED THE STAND OFF IAW SRM 51-42-14, SRM 51-42-1, AND ETN-CR-54-015R1.
2016
Part: SPOILER SYS — MALFUNCTIONED · airframe 15,419 hrs · 10,821 cycles
DESCENDING THROUGH 9K HAD IB FLT SPOILERS CAUTION MESSAGE AND IB SPOILERONS CAUTION MESSAGE COME ON. INTERROGATED MDC FOUND "L IB MFS PCU JAMMED" MDC MESSAGE. PERFORMED SPOST1 RESET, PERFORMED OPS CHECK IAW ETN CR-27-093, OPS CHECKED GOOD.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,334 hrs · 9,976 cycles
DURING FLT DESCENT FROM FLT 190, A LOUD POPPING SOUND WAS HEARD ON THE FLT DECK AND DISCOVERED THE CAPTAIN`S SIDE WINDSHIELD OUTER PANEL WAS CRACKED. R&R CAPTAIN WINDSHIELD IAW CRJ 700 AMM 56-11-01. OPS CHECK & LEAK CHECK GOOD.
Part: STRUT — LOW (NLG) · airframe 14,133 hrs · 9,826 cycles
NOSE GEAR UNABLE TO RETRACT AFTER TAKEOFF. FOUND NLG STRUT LOW, SERVICED NLG STRUT IAW AMM 12-12-32. SEE ITEM 2 THIS LOG PAGE. ADJUSTED PROX SENSORS 11,24 & 44 IAW MM 32-61-05. PERFORMED EXTENSION & RETRACTION CHECK IAW MM 32-30-00. OPERATIONS CHECKED GOOD.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 13,879 hrs · 9,635 cycles
GALLEY EMER LIGHTS INOPERATIVE. FLIGHT CREW PLACARDED EMER LIGHTS IAW MEL 33-32N. SECURED CONNECTOR ON NR 1 BATT SUPPLY UNIT. OPERATIONS CHECKED GOOD IAW 33-51-17-000-80. MEI ITEM RESTORED.
Part: BLADE — STUCK (LT ENGINE) · airframe 13,391 hrs · 9,273 cycles
DURING CLIMB OUT, LT ENG VIBRATION WAS IN AMBER RANGE. MAX READING NOTED WAS 1.8 MIL. AFTER SUBSTANTIAL REDUCTION IN THRUST IT CAME BACK TO NORMAL RANGE. DURING TROUBLESHOOTING FOUND TWO STUCK FAN BLADES ON NR 1 ENG. COMPLIED WITH FIM TASK 72-00-00-810-815. REF ITEM NR 2 THIS LOG PAGE FOR FURTHER ACTION TAKEN. UNSTUCK FAN BLADES IAW MM 72-21-02. DEFERRED LUBE IAW AMM REF 72-21-02.
2015
Part: PROXIMITY SWITCH — DIRTY (NLG) · airframe 13,159 hrs · 9,065 cycles
AFTER TAKEOFF, LG DISAGREE WARNING. NOSE GEAR UNSAFE INDICATION. FOLLOWED AOM PROCEDURE & HAD 3 GREEN. CLEANED ICE FROM NLG DOORS & SCISSOR LINKS, CLEANED DIRT FROM NLG PROX SWITCHES & TARGETS. PERFORMED OPERATIONS CHECK OF NLG PROX SENSOR SYS & FOUND WORKING PROPERLY AT THIS TIME IAW AMM 32-61-00.
Part: UNKNOWN — ODOR (CABIN) · airframe 12,385 hrs · 8,400 cycles
FLIGHT ATTENDANT 1 & 2 REPORTED STRONG FUEL SMELL IN THE CABIN. FOUND NO EVIDENCE OF FUEL SMELL IN CABIN OR COCKPIT.
Part: SENSOR — FAILED (RT SLAT) · airframe 11,628 hrs · 7,807 cycles
SLAT FAULT, MESSAGE ON ED 2. R & R RT MT89 SLAT DISCONNECT SENSOR IAW AMM 27-81-39. OPS CHECKED GOOD.
Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 11,448 hrs · 7,655 cycles
REF LOG PAGE 3764018 MEL 25-15. FWD CABIN FLASHLIGHT HOLDER BROKEN, FLASHLIGHT STILL WORKS. R & R FLIGHT ATTENDANT FWD EMER FLASHLIGHT ASSEMBLY IAW 25-61-02. OPERATIONS CHECKED GOOD MEL ITEM RESTORED.
2014
Part: SKIN — CRACKED (PAX DOOR) · airframe 10,962 hrs · 7,259 cycles
PASSENGER DOOR AFT SIDE SKIN HAS 1/4 INCH CRACK AT THE MIDDLE STEP AREA. REPAIRED PAX DOOR AFT SIDE SKIN IAW ETN-CR-52-039 & REINSTALLED GAS SPRING BEAM IAW SRM 51-42-06.
Part: WEB — CRACKED (FUSELAGE) · airframe 10,962 hrs · 7,259 cycles
FORWARD EQUIPMENT COMPARTMENT RT FLOOR WEB IS CRACKED BY THE ADG PUMP. APPROX 3/8 INCH LONG. REPAIRED RT FLOOR WEB IAW ETN-CR-53-099.
Part: COVER — CRACKED (PAX DOOR) · airframe 10,962 hrs · 7,259 cycles
PASSENGER DOOR AFT UPPER CORNER IS CRACKED APPROX 1 1/4 INCHES BY THE RIVET. R & R PAX DOOR INNER UPPER AFT CORNER COVER IAW SRM 51-42-06 & 51-42-13.
Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 10,962 hrs · 7,259 cycles
PASSENGER DOOR AFT ATTACHMENT ANGLE HAS A 1 INCH CRACK. R & R BAD SECTION OF PAX DOOR AFT DRAG ANGLE IAW SRM 52-11-04.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,273 hrs · 6,628 cycles
WHILE ON DESCENT DEPLOYED FLIGHT SPOILERS, RECEIVED INBD FLIGHT SPOILERS & INBD SPOILERONS CAUTION MSGS. PERFORMED SPOST 2 IAW MM 27-61-05. MSG CLEARED & PERFORMED OPERATIONS CHECK OF SPOILERS IAW MM 27-62-00 CHECKED GOOD ALSO SEE ITEM 2 THIS LOG PAGE.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 9,950 hrs · 6,384 cycles
INBD FLT SPOILERS CAUTION INBD SPOILERONS CAUTION MSG POSTED OF FINAL APPROACH. IAW TDMI 539T279 & 539T2710 PERFORMED RESET PROCEDURE SPOST 1 & 2 MSGS CLEARED. ACFT RETURNED TO SERV IAW ETN CR-27-093.
Part: TIRE — LOW PRESSURE (NLG) · airframe 9,225 hrs · 5,887 cycles
NOSE WHEEL SHIMMY AT HIGH SPEED. FOUND NOSE TIRES LOW PRESS. SERVICED NOSE TIRES IAW MM 12-12-32, NO FURTHER DEFECTS NOTED.
Part: DUCT — CRACKED (ANTI-ICE SYS) · airframe 8,665 hrs · 5,519 cycles
LEFT COWL A/I DUCT WARNING MESSAGE IN CLIMB WITH COWL A/I SELECTED ON. FOUND COWL A/I DUCTING CRACKED. R & R OUTER DUCTING IAW STANDARD MTX. OPERATIONS CHECKED IAW 30-22-01, NO LEAKS NOTED.
Part: WARNING SYSTEM — FALSE ACTIVATION (ANTI-ICE SYS) · airframe 8,664 hrs · 5,518 cycles
LEFT COWL A/I DUCT WARNING MESSAGE ON LD 1 WHEN COWL A/I IS SELECTED. RE-SET SYS & PERFORMED OPERATIONS CHECKED GOOD IAW AMM 30-22-01.
2013
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,899 hrs · 5,008 cycles
DURING INSPECTION, FOUND NR 1, 3 & 4 BATTERY AND BATTERY CHARGERS INOPERATIVE. ACFT REMOVED FROM SERVICE. REPLACED BATTERY CHARGERS. ACFT RETURNED TO SERVICE.
Part: BULB — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 7,082 hrs · 4,495 cycles
DURING B-INSP, FOUND THE RT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R BULB IAW AMM 31-51-15. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,067 hrs · 4,486 cycles
DURING B-INSPECTION, FOUND THE OVER WING EMERGENCY LIGHTS TO BE INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT AND RT OVER WING EMERGENCY LIGHTS IAW AMM 33-51-15. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.
Part: UNKNOWN — ODOR (COCKPIT) · airframe 6,576 hrs · 4,168 cycles
FOR FLIGHT 4605 THE CREW THE FOUND WHEN THEY ARRIVIED AT THE AIRCRAFT THE BATTERY SWITCH WAS LEFT ON AND THE EXTERNAL POWER WAS NOT AVAILABLE. ALL SIX CRT BLANK AND ELECTRICAL SMOKE SMELL AND AURAL WARNING OF "ENGINE OIL" MESSAGE REPEATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MAIN & APU BATTERIES VOLTAGE LOW. ENERGIZED EXTERNAL POWER IAW AMM 24-41-00. NO "ELECTRICAL SMOKE SMELL NOTED AFTER A/C FULLY ENERGIZED. CHECKED CURRENT FAULTS ON MDC. NONE FOUND IAW AMM 45-45-00. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: NUT — MISINSTALLED (CONTROL COLUMN) · airframe 6,244 hrs · 3,969 cycles
FLIGHT 4659. ON TAXI OUT, DURING FLIGHT CONTROL CHECK, FIRST OFFICERâS YOKE BINDING LEFT AND RIGHT AND MADE A CLICKING NOISE AS WELL. AIRCRAFT REMOVED FROM SERVICE. FOUND INCORRECT TORQUE ON THE AFT NUT OF THE CONTROL WHEEL. TORQUE AFT NUT IAW 27-31-01. PERFORM OPS CHECK OF AILERON CONTROL SYS IAW 27-11-00. AFT NUT OF FIRST OFFICERâS CONTROL COLUMN WHEEL PRIMER AND RETAINING COMPOUND REQUIRES TO BE APPLIED. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
2012
Part: UNKNOWN — ODOR (COCKPIT) · airframe 5,471 hrs · 3,500 cycles
ON FLIGHT 4586 THE CREW REPORTED THAT DURING DESCENT INTO LGA NOTICED AN OVERHEAT/AIR BURNING SMELL IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED HIGH POWER ENGINE RUNS & CHECKED AIR CIRCULATION MACHINEâS FROM ALL BLEED SOURCES. MAINTENANCE COULD NOT DUPLICATE THE ODOR. CHECKED INLETS & EXHAUST FOR EVIDENCE OF OIL, NONE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: PCU — FAILED (SPOILERS) · airframe 4,687 hrs · 3,014 cycles
FLIGHT 3729, CREW REPORTED THAT WHILE EXPEDITING A DESCENT WITH FLIGHT SPOILER DEPLOYED, RECEIVED AN EICAS CAUTION FOR MESSAGE INBOARD FLT SPOILERS AND INBOARD SPOILERONS AT 2700 FT PER MIN. MESSAGE STAYED ON. THRUST LEVERS AT FLIGHT IDLE WHEN THE MESSAGE APPEARED. DECLARED AN EMERGENCY & LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT INBD MULTI FUNCTION SPOILER PCU 32 IAW MM 27-62-01. AIRCRAFT RETURNED TO SERVICE.
Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 3,614 hrs · 2,311 cycles
FLIGHT 3730, FLIGHT ATTENDANT REPORTED THE SERVICE DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. SECURED EMERGENCY EXIT SIGN IAW EECSPM 20.33-00. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.
2011
Part: FITTING — LOOSE (THRUST REVERSER) · airframe 1,693 hrs · 1,104 cycles
ON FLIGHT 3836 THE CREW REPORTED THAT AFTER ROTATION, AN "EDP1A" CAUTION MESSAGE APPEARED HYDRAULIC SYSTEM 1 SHOWS A QUANTITY OF 0%. NOTE: LEFT ENGINE LEAKING HYDRAULIC FLUID. THE CREW ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND FLUID LEAKING FROM NR 1 ENGINE T/R FLEXIBLE STOW LINE QUICK DISCONNECT FITTING. TIGHTENED FITTING IAW STANDARD MAINTENANCE PRACTICES. LEAK CHECK GOOD PER MTX WC 002-05-900-016 AS REQUIRED. NO PARTS REMOVED OR REPLACED. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.