N541EA
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.
145 reports on file, 2011-06-11 – 2026-05-12.
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
AFTER CORROSION REMOVAL REWORKED AREA ON INTERCOSTAL STGR 21LH BTW FS=310 TO FS= 333 WAS FOUND OUT OF LIMITS E/E BAY. CORROSION ON INTERCOSTAL STGR 20LH BTW FS=319 TO FS= 333 (FWD E/E BAY) WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THEREFORE IS OUT OF LIMITS PER CRJ 700 SRM 53-21-23-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01 AND OPERATIONAL AND FUNTIONAL TEST OF INTELSAT INFLIGHT LLC MODMAN, JB 11, MODE S TRANSPONDER, DME TRANSCEIVER, EVMU AND GPS RECEIVER MUST BE PERFORMED UNDER NRC 00298.
Part: ANGLE — CRACKED (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
CRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: ANGLE — CORRODED (ZONE 800) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
AFTER REMOVAL OF MIDCAP ANGLE, CORROSION ON KICKPLATE ANGLE WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR. CORROSION ON KICKPLATE ANGLE WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 AND AREA WAS FOUND OUT LIMITS PER SRM 53-51-01-101-003-A05 AND : KICKPLATE ANGLE OF SURROUND STRUCTURE (LH PASSENGER DOOR) WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: ANGLE — CRACKED (ZONE 600) · airframe 33,636 hrs · 26,116 cycles
CRACK ON ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 642AZ (ATTATCHED TO REAR SPAR) AT RH WING. ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 642AZ (ATTATCHED TO REAR SPAR) AT LH WING. WAS REPLACED PER SRM 51-42-21-001-001-A01.
Part: BRACKET — CRACKED (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
CRACK ON OXYGEN SERVICE PANEL BRACKET (LOWER AFT CORNER) AT FWD FUSELAGE. PANEL BRACKET ON OXYGEN SERVICE (LOWER AFT CORNER) AT FWD FUSELAGE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 "
Part: ANGLE — CRACKED (ZONE 500) · airframe 33,636 hrs · 26,116 cycles
CRACK ON ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 542AZ (ATTATCHED TO REAR SPAR) AT LH WING. ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 542AZ (ATTATCHED TO REAR SPAR) AT LH WING. WAS REPLACED IAW SRM 51-42-21-001-001-A01.
Part: FRAME — CRACKED (ZONE 400) · airframe 33,636 hrs · 26,116 cycles
CRACK ON LH UPPER/LOWER THRUST REVERSER TORQUE BOX FWD FRAME AT LH ENGINE. LT UPPER/LOWER THRUST REVERSER TORQUE BOX FWD FRAME AT LH ENGINE.WERE REPAIRED PER REO 670-54-22-154 REV-- AND REO 670-54-22-155 REV-.
Part: SUPPORT BEAM — CHAFED (ZONE 400) · airframe 33,636 hrs · 26,116 cycles
CHAFE DAMAGE UPPER/LOWER CASCADE SUPPORT BEAM AT LT/RT ENGINE. CHAFE DAMAGE UPPER/LOWER CASCADE SUPPORT BEAM AT LH/RH ENGINE WERE REPAIRED PER REO 670-54-22-160 REV- -, REO 670-54-22-161 REV- -. REO 670-54-22-159 REV- -. AND PER REO 670-54-22-162 REV- -.
Part: STRIKER — CORRODED (ZONE 800) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON LOWER STRIKER OF CARGO DOOR SURROUND STRUCTURE. REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01.
Part: SKIN — CRACKED (ZONE 400) · airframe 33,636 hrs · 26,116 cycles
CRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL. CRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL WAS REPAIRED PER REO 670-54-21-1818 REV. -A.
Part: ACOUSTIC PANEL — CRACKED (ZONE 400) · airframe 33,636 hrs · 26,116 cycles
IN REF TO NRC 0254 AFTER REMOVAL OF COAMING LATCH CRACK ON ACUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL. ACOUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL WAS REPAIRED PER REO PER REO 670-54-21-1818 REV. -A.
Part: FITTING — GOUGED (ZONE 600) · airframe 33,636 hrs · 26,116 cycles
GOUGE ON LATERAL FACE OF LUG R1 AND R2 AT RH AILERON CENTRAL FITTINGS. LATERAL FACE OF LUG R1 AND R2 AT RH AILERON CENTRAL FITTINGS WERE REPAIRED PER REO 670-57-61-237 REV -
Part: ANGLE — CRACKED (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
CRACK ON OUTBD ANGLE ON CROSSBEAM FS 280 LBL-12 AT PAX CABIN FLOOR STRUCTURE. ANGLE WAS REPLACED ON CROSSBEAM FS 280 LBL-12 AT PAX CABIN FLOOR STRUCTURE PER CRJ700 SRM 51-42-21-001-001-A01.
Part: SUPPORT — CRACKED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CRACKS ON DIAPHRAGM SUPPORT (ABOVE DOOR NET STRUCTURE) OF AFT BAGGAGE BAY STRUCTURE. DIAPHRAGM SUPPORT (ABOVE DOOR NET STRUCTURE) OF AFT BAGGAGE BAY STRUCTURE WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 PAR. AND SRM 51-41-02- 001-001-A01.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
DURING EXTERNAL ZONAL INSPECTION OF THE REAR FUSELAGE: FS977.00 TO FS1098.00, ABOVE WL72.50, SEVERAL DENTS WERE FOUND ON EXTERNAL FUSELAGE SKIN BTW FS1015.00 TO FS1069.00 BTW STGR27 TO STGR 22 RH. AFTER REMOVAL OF PAINT, DVI WAS PERFORMED PER CRJ-700 NDT PART 1, CHAPTER 51 TASK 51-20-009-210-A01 AND DENTS NO WERE FOUND, ONLY PREVIOUS BLEND OUTS ON FUSELAJE SKIN FOUND. AND WERE PERFORMED PER REO 670-53-61-2711 REV--"
Part: PLATE — CRACKED (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
CRACKS ON MOUNTING PLATE FWD/AFT CORNERS OF JB6 AT FWD EQUIPMENT COMPARTMENT. MOUNTING PLATE WAS REPLACED PER SRM 51-42-06-001-001-A01.
Part: ANGLE — CRACKED (ZONE 800) · airframe 33,636 hrs · 26,116 cycles
CRACKED AFT UPPER ANGLE OF FIRE PROTECTION KIT AT FWD BAGGAGE BAY DOOR. CRACKED AFT UPPER ANGLE OF FIRE PROTECTION KIT AT FWD BAGGAGE BAY DOOR WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01 AND SRM 51-41-02-001-001-A01
Part: RETAINER SEAL — CRACKED (ZONE 800) · airframe 33,636 hrs · 26,116 cycles
CRACKED UPPER SEAL RETAINER AT PASSENGER DOOR. UPPER SEAL RETAINER AT PASSENGER DOOR WAS REMPLACED PER CRJ-700 SRM 51-42-10-001-001-A01
Part: HINGE — WORN (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
IN REF TO TRFKE00EQGM3: PERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 53-21-23-201-007-A01. SEND E-MAIL REQUEST TO [email protected] TO COMPLETE SDIR TERMINATION REVIEW. HINGE PIANO ON PASSENGER DOOR SURROUND STRUCTURE WAS REPLACED PER CRJ700 SRM 51-42-21-001-001-A01
Part: WEB — CRACKED (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
CRACK ON FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 AT FWD EQUIPMENT COMPARTMENT. FLOOR WEB LEFT SIDE (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 AT FWD EQUIPMENT COMPARTMENT. WAS REPAIRED PER CRJ 700 SRM 53-11-43-201-001-A01.
Part: DRIP TRAY — CRACKED (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
IN REF TO TRFKE00CFJVX: 4790FH PERM REPAIR - DAMAGE DRIP TRAY DRAIN TUBE FITTING WITHIN 4790 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING COMMENTS: REPLACE DRIP TRAY SH670-31731-3 OR SUBMIT AN NEW RFTS & DAMAGE REPORT. DRIP TRAY ASSY. RH P/N:SH670-31731-3 WAS REPAIRED PER EA 5321-2026-0511 REV - -
Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON BRACKET MACHINED FS=515 STGR 22LH TO STGR 23LH AND BTW FS=661 TO 645 STGR 24 LH TO STGR 25LH AT FORDWARD BAGGAGE BAY. WERE EVALUATED,DUE NOT ALLOWABLE DAMAGE BRACKET MACHINED FS=515 STGR 22LH TO STGR 23LH AND BTW FS=661 TO 645 STGR 24 LH TO STGR 25LH AT FORDWARD BAGGAGE BAY PER CRJ 700 SRM 53-32-58-101-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-22-001-001-A01.
Part: PANEL — CRACKED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION AND CRACK ON DIVERTER PANELS (3EAS). REPAIRED PER EA 5321-2026-0502 REV - -, EA 5321-2026-0501 REV - - AND EA 5321-2026-0488 REV -.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION AND GOUGES ON SEAT RAIL (3EAS) FS349 TO FS485, FS485 TO FS 581 RBL 9 AND FS 379 TO 485 LBL 9 AT PASSENGER CABIN. SEAT RAIL (3EAS) FS349 TO FS485, FS485 TO FS 581 RBL 9 AND FS 379 TO 485 LBL 9 AT PASSENGER WERE REPLACED PER CRJ 700 SRM 53-00-49-400-801.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION AND GOUGES ON SIDE SEAT RAIL (5EAS) FS711 TO FS761 (LH), FS677 TO FS711 (LH), FS573 TO FS677 (LH), FS379 TO 477 RH/LH AT PASSENGER CABIN. SEAT RAIL (5EAS) FS711 TO FS761 (LH), FS677 TO FS711 (LH), FS573 TO FS677 (LH), FS379 TO 477 RH/LH AT PASSENGER CABIN. WERE REPLACED PER CRJ 700 AMM 53-00-49-400-801-A03.
Part: SKIN — DAMAGED (ZONE 100) · airframe 33,636 hrs · 26,116 cycles
PERM REPAIR - PANEL 196DR NUT PLATE ASSEMBLY OVERSIZED HOLE 1. WITHIN 1556 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. // ENGINEERING COMMENTS: REPLACE NUT PLATE ASSY. MM670-35155-009 OR SUBMIT AN RFTS WITH ALL DFAMAGE DIMENSIONS. ELONGATED HOLE TO FUSELAGE LOWER SKIN BETWEEN FS985.00-FS1000.00 AND STR26R-STR27 WAS REPAIRED PER REO 670-53-61-2709 REV--.
Part: HANDLE — CRACKED (ZONE 800) · airframe 33,636 hrs · 26,116 cycles
CRACKS (4 EAS) ON EXTERNAL HANDLE FLAPER CORNERS AT PASSENGER DOOR. EXTERNAL FLAP HANDLE AT PASSENGER DOOR WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND PLACARD WAS INSTALLED PER CRJ-700 AMM 20-60-04-400-801.
Part: HINGE FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON HINGE FITTINGS (2 EAS) AND HARDWARE OF AFT LAVATORY SERVICE DOOR. CORROSION ON HINGE FITTINGS (2 EAS) OF AFT LAVATORY SERVICE DOOR WERE REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND THEREFORE IT IS OUT OF LIMITS PER CRJ-700 SRM 53-00-00-101-001-A01, AND HINGE FITTINGS (2 EAS) WAS REPLACED ON AFT LAVATORY SERVICE DOOR PER CRJ-700 SRM 51-41-02-001-001-A01"
Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON MID CAP ANGLE OF PASSENGER DOOR SURROUND STRUCTURE. CORROSION ON MID CAP ANGLE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND IS OUT OFF LIMITS PER CRJ-700 SRM 53-21-23-101-001-A01 AND MID CAP ANGLE WAS REPLACED PER CRJ-700 SRM 51-41-02-001-001-A01.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
INITIAL INSPECTION: CORROSION ON FRAME FITTING FS 319 STGR 17RH AT CPAX. FRAME FITTING WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THEREFORE IT IS OUT LIMITS PER CRJ700 SRM 53-21-23-101-001-A01 AND REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01 AND CRJ-700 SRM 51-42-06-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION WAS FOUND AT SEAT TRACK ON FS 364.00 TO 469.00 LBL 25 OF THE FUSELAGE FLOOR STRUCTURE. SEAT TRACK ON FS 364.00 TO 469.00 LBL 25 OF THE FUSELAGE FLOOR STRUCTURE WERE REPLACED PER CRJ700 AMM 53-00-49-400-801 (CONFIG A03)
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON BRACKETS FLOOR BEAM AT FS 284.00 RBL16 AND RBL36, ON BRACKET FLOOR BEAM FS 295.00 AND RBL 5 OF THE FUSELAGE FLOOR STRUCTURE. FLOORBEAM TEE REMOVED PER SRM 51-21-06-001-001-A01 AND AREAS IS OUT LIMITS PER CRJ700 SRM 53-21-43-101-001-A01 AND SRM 53-00-00-101-001-A01 AND BRACKETS FLOOR BEAM AT FS 284.00 RBL16 AND RBL36, ON BRACKET FLOOR BEAM FS 295.00 AND RBL 5 OF THE FUSELAGE FLOOR STRUCTURE WERE REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01.
Part: FITTING — CORRODED (ZONE 600) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON LUG BORES ON R3 AND R5 AT RH AILERON CENTRAL FITTING. CORROSION ON LUG BORE R5 AT RT AILERON CENTRAL FITTING WAS REPAIRED PER REO 670-57-61-237 REV:-- AND LUG R3 WAS CLEANING PER SRM 51-26-00-001-001-A01 CLEANING.-.
Part: INTERCOSTAL — CRACKED (ZONE 500) · airframe 33,636 hrs · 26,116 cycles
CRACK ON INTERCOSTAL, TIRE BURST COVER BEHIND PANEL 542AZ OF LH WING. INTERCOSTAL, TIRE BURST COVER BEHIND PANEL 542AZ OF LH WING WAS REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01 PAR.6.C AND SRM 51-42-13-001-001-A01 PAR.6.C AND SRM 51-42-06-001-001-A01 PAR.6.C.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON SEAT TRACK OF FS 582.00 TO FS 669.00 AND RBL 9 OF THE FUSELAGE FLOOR STRUCTURE. CORROSION ON SEAT TRACK OF FS 582.00 TO FS 669.00 AND RBL 9 OF THE FUSELAGE FLOOR STRUCTURE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND THEREFORE OUT OF LIMITS PER CRJ-700 SRM 53-31-49-101-001-A01 AND SEAT TRACK OF FS 582.00 TO FS 669.00 AND RBL 9 OF THE FUSELAGE FLOOR STRUCTURE WAS REPLACED PER CRJ 700 SRM 53-00-49-400-801.
Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON SETTLEMENT SUPPORT STRUCTURE AT AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING (196DR). SETTLEMENT SUPPORT STRUCTURE (STRAP) WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON SEAT TRACK OF FS 486.00 TO FS 581.00 AND LBL 9 OF THE FUSELAGE FLOOR STRUCTURE. CORROSION ON SEAT TRACK OF FS 486.00 TO FS 581.00 AND LBL 9 OF THE FUSELAGE FLOOR STRUCTURE. AT PASSENGER CABIN WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THEREFORE OUT OF LIMITS PER CRJ-700 SRM 53-31-49-101-001-A01 AND REPLACED PER CRJ 700 AMM 53-00-49.
Part: FITTING — CORRODED (ZONE 500) · corrosion level 2 · airframe 33,636 hrs · 26,116 cycles
CORROSION ON BORE LUG L2, L5 AND L6 AT LH AILERON CENTRAL FITTINGS. HINGE FITTING AILERON LH BORE LUGS L2, L5 AND L6 WERE REPAIRED PER REO 670-57-61-237 REV - .
Earlier reports · 2011–2022 · 107 reports
2022
Part: NONE — CORRODED (ZONE 500)
PITTING CORROSION ON SLAT TRACKS 1-3 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #1 RH WING.
Part: STRINGER — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSIÃN ON STGR 24RH BTW FS 453-FS478. (FWD BAGGAGE COMPARTMENT). STGR 24RH BTW FS 453-FS478. (FWD BAGGAGE COMPARTMENT) WAS REPAIRED PER CRJ 700 SRM 53-00-03-201-001-A01
Part: DOUBLER — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON DOUBLER BETWEEN FS=295/FS=310 AND STGR 26LH/26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. DOUBLER BETWEEN FS=295/FS=310 AND STGR 26LH/26RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01.
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON FLOOR BEAM 9LBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY. AREAS ON FLOOR BEAM BETWEEN FS=977 TO FS=1005.5 AND FS=1037.5 TO FS=1098 ON 9LBL WAS CLEANED PER CRJ-700 SRM 51-26-00-001-001-A01 AFTER CLEANLINESS, AREA WAS INSPECTED PER CRJ-700 SRM 51-11-00-001-001-A01 AND CRJ-700 AMM 05-21-00 AND NO DISCREPANIES OR CORROSION WERE NOTED /// FLOOR BEAM 9LBL IN FS= 1005.5 TO FS=1037.5 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ 700 SRM 53-00-41-201-001-A01
Part: STRINGER — CORRODED (ZONE 100) · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STGR 24RH BTW FS477.4-FS501, FWD CARGO COMPARTMENT
Part: STRINGER — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01
Part: SPLICE — CORRODED (ZONE 100) · airframe 25,936 hrs · 19,641 cycles
CORROSION ON SPLICE AT FS333 & STGR 25RH, FWD EQUIPMENT BAY.
Part: SKIN — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON SKIN BETWEEN FS=295.00/FS=310.00 AND STGR 24RH/25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. SKIN BETWEEN FS=295.00/FS=310.00 AND STGR 24RH/25RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPAIRED PER EA 22-C7-53-0990 REV. IR
Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION AT HINGE OF ACCESS PANNEL 196ER CORRECTIVE ACTION: HINGE OF ACCESS PANNEL 196ER WAS REPLACE PER CRJ-700 SRM 51-41-02-001-001-A01
Part: NONE — CORRODED (ZONE 600) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 3-2 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #3 RH WING.
Part: STRINGER — CORRODED · corrosion level 2
CORROSION ON STGR 26RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STRINGER 26RH FS 333 TO FS 280 WAS REPLACED PER CRJ/700 SRM 51-42-06-001-001-0A1. AND CRJ/700 SRM 51-42-21-001-001-A01.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STRG 26LH BTW FS. 280/265 AT FWD AVIONICS COMPARTMENT.
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 1-1 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #1 RH WING. SLAT TRACKS 1-1 (SEVERAL LOCATION AT UPPER SURFACE) WAS REPAIRED PER REO 670-57-42-1377 REV.--
Part: PLATE — CORRODED (ZONE 200) · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON NET ATTACHMENT PLATES (3 EAS) ON AFT BAGGAGE BAY DOOR CUTOUT STRUCTURE BETWEEN FS=1000.00 AND FS=1047.00.
Part: SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON SPLICE AT FS477.4 & STGR 24RH, FWD CARGO COMPARTMENT
Part: NONE — CORRODED (ZONE 600) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 3-1 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #3 RH WING.
Part: STRINGER — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STGR 25RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STGR 25RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01.
Part: NONE — CORRODED (ZONE 500) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 1-1 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #1, LH WING.
Part: NONE — NONE (ZONE 200) · airframe 25,936 hrs · 19,641 cycles
SCRATCHES ON LH SIDE SEAT RAIL STRUCTURE BETWEEN FS669 TO FS785, SCRATCHES AND CORROSION BETWEEN FS785 TO FS861 AND SCRATCHES BETWEEN FS861
Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON SPLICE AT FS333 & STGR 26RH, FWD E/E EQUIPMENT BAY.
Part: STRINGER — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STGR 26LH BETWEEN FS= 319.70 AND FS=310 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STGR 26LH FS=333.00 AND FS=280.00 WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: FRAME — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON FRAME BETWEEN FS=295.00 AND STGR 25RH/27RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. FRAME BETWEEN FS=295.00 AND STGR 25RH/27RH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPAIRED PER CRJ 700 SRM 53-00-06-201-006-A01
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION IN RH FAIRING SUPPORT DIAPHRAGMS (3 EA´S, 1 EA LH SIDE 2EA´S RH SIDE) IN STA. FS= 797.00 TO FS= 807.00 AND 35LBL/35RBL AT RH MLG WHEEL WELL. FAIRING SUPPORT DIAPHRAGMS (3 EA´S, 1 EA LH SIDE 2EA´S RH SIDE) IN STA. FS= 797.00 TO FS= 807.00 AND 35LBL/35RBL AT RH MLG WHEEL WELL WERE REPLACED PER CRJ 700 SRM 51-41-02-001-001-A01 CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STGR 26RH BETWEEN FS=333.00 AND FS=319.70 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STRINGER 26RH FS 333 TO FS 280 WAS REPLACED PER CRJ/700 SRM 51-42-06-001-001-0A1. AND CRJ/700 SRM 51-42-21-001-001-A01.
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON INTERCOSTALS (3EAS) BETWEEN FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. INTERCOSTALS (3EAS) BETWEEN FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WERE REPACED PER CRJ 700 SRM 51-42-20-001-001-A01 AND SRM 51-42-06-001-001-A01
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
HIDDEN DAMAGE IN REF NRC:00192: AFTER REMOVAL TO SEAL OF FWD BAGGAGE BAY DOOR{ CORROSION WAS FOUND ON FWD/AFT LOWER PLATE OF FWD BAGGAGE BAY DOOR.} FWD/AFT LOWER PLATE OF FWD BAGGAGE BAY DOOR WERE REPLACED PER CRJ 700 SRM 51-42-06-001-001-A01
Part: SKIN — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
HIDDEN DAMAGE AFTER SEALANT REMOVAL ON UPPER BEACOM, SCRIBE LINES WAS FOUND ON FUSELAGE SKIN. (REF. SURROUND BEACOM SEATTLEMENT AREA). DAMAGED FUSELAGE SKIN. (REF. SURROUND BEACOM SEATTLEMENT AREA) WAS REPAIRED PER EA 22-C7-53-1002 REV. IR
Part: NONE — NONE · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
AFTER REMOVAL OF RH/LH MLG´S PISTON AXLE, CORROSION ON THREADS OF CYLINDER ASSY RH/ LH MLG´S}. (AYP) THREADS OF CYLINDER ASSY AT LH MLG WAS CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND AFTER CLEANLINESS, AREA WAS INSPECTED PER CRJ-700 SRM 51-11-00-001-001-A01 AND CRJ-700 AMM 05-21-00 AND NO DISCREPANCES O CORROSION WERE NOTED AND THREADS OF CYLINDER ASSY AT RH MLG WAS REPAIRED PER REO 670-32-11-409 REV: --
Part: WEB — NONE · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON FLOOR PROTECTOR WEBS AT FUSELAGE LOWER FRAME SERVICE DOOR CORROSION ON FLOOR PROTECTOR WEBS WAS REMOVED PER CRJ/700 SRM 51-21-06-001-001-A01 AND MEASUREMENT WAS PERFORMED ON FLOOR PROTECTOR WEBS (4EA'S) WITH ORIGINAL THICKNESS IS 0.063 AND MINIMUM REMAINING THICKNESS IS: ON PROTECTOR WEB FWD (SH670-32040-1) 0.057" ; PROTECTOR WEB FWD (SH670-32040-2) 0.057" AND PROTECTOR WEB AFT (SH670-32040-2) 0.059" THEREFORE IT IS WITHIN THE LIMITS PER CRJ-700 SRM 53-21-23-101-002-A01 AND ON PROTECTOR WEB AFT (SH670-32040-1) MINIMUM REMAINING IS 0.046 IT IS OUT OF LIMITS /// PROTECTOR WEB AFT (SH670-32040-1) WAS REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01
Part: NONE — CORRODED (ZONE 500) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 1-3 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #1, LH WING..
Part: NONE — CORRODED (ZONE 500) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 1-2 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #1, LH WING.
Part: POST — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON POST AT LBL12 BETWEEM FS=280 AND STGR 25LH/24LH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT (LOWER SECTION). POST AT LBL12 BETWEEM FS=280 AND STGR 25LH/24LH AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ 700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
Part: NONE — CORRODED (ZONE 500) · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON METALLIC STRAPS AT FAIRING 193AB. METALLIC STRAPS WERE REPLACED ON FAIRING 193AB PER CRJ-700 SRM 51-42-10-001-001-A01
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON SETTLEMENT AREA COVER BY 173BZ AND 174BZ ACCESS PANELS ON MLG WHEEL WELL.) AREA ON SETTLEMENT AREA COVER BY 173BZ AND 174BZ ACCESS PANELS ON MLG WHEEL WELL (6 EA´S) WERE MEASURED, #1 NOMINAL THICKNESS IS 0.060¨ AND MAXIMUN DEPTH REMOVED 0.004" , #2 NOMINAL THICKNESS IS 0.060¨ MAXIMUN DEPTH REMOVED 0.003¨ #3 NOMINAL THICKNESS IS 0.060¨AND MAXIMUM DEPTH REMOVED 0.004¨, #4 NOMINAL THICKNESS IS 0.060¨ MAXIMUN DEPTH REMOVED 0.005¨, #5 NOMINAL THICKNESS IS 0.050¨ MAXIMUN DEPTH REMOVED 0.003, #6 NOMINAL THICKNESS IS 0.050¨ MAXIMUN DEPTH REMOVED 0.003¨ THEREFORE WHITIN LIMITS PER CRJ-700 SRM 53-00-00-101-001-A01 PAR.4.A. TOOL USED: DIAL INDICATOR EXPIRE:25/JAN/23 N/C:2925 PN: 543-783 SN:18055719. DUE EXCESSIVE CORROSION ON WEB ASSY MACHINED (2 EA´S) MUST BE REPLACED PER CRJ-700 SRM 53-00-00-101-001-A0
Part: NONE — CORRODED (ZONE 500) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 3-2 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #3 LH WING.
Part: NONE — CORRODED (ZONE 600) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 3-3 (SEVERAL LOCATION AT OUTER WEDGE), SLAT #3 RH WING.
Part: NONE — NONE (ZONE 200) · airframe 25,936 hrs · 19,641 cycles
SCRATCHES ON RH SIDE SEAT RAIL STRUCTURE BETWEEN FS669 TO FS785, SCRATCHES AND CORROSION BETWEEN FS785 TO FS861 AND SCRATCHES BETWEEN FS861
Part: SKIN — GOUGED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
NICK & GOUGE ON FUSELAGE SKIN BTW FS1031-FS1051 & BTW STGR 24R-26R. (2 LOCATIONS). CORRECTIVE ACTION: NICK & GOUGE ON FUSELAGE SKIN BTW FS1031-FS1051 & BTW STGR 24R-26R,REPAIR PER EA 22-C7-53-0951 REV. IR
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON FLOOR BEAM 27LBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY FLOOR BEAM 27LBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ 700 SRM 53-00-41-201-001-A01
Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION AT ACCESS PANEL 542BZ. CORROSION AT ACCESS PANEL 542BZ WAS REPLACED PER CRJ700 SRM 57-22-55-001-001-A01 ITEM 1.
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON INTERCOSTAL ATTACHED TO STRINGER 20RH IN STA FS= 349 AT MAIN AVIONICS COMPARTMENT. (E/E) NEW INTERCOSTAL (2EAS) STA.310 AT 319.70 AND 319.70 AT STA.349 WERE INSTALLED PER CRJ-700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON LOWER ANGLE OF WING-TO-FUSELAGE-FAIRING AT FS STA 939 DAMAGED LOWER ANGLE OF WING-TO-FUSELAGE-FAIRING AT FS STA 939 WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01.
Part: NONE — CORRODED (ZONE 500) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 2-3 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #2 LH WING..
Part: SKIN — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON EXTERNAL SKIN AT FWD FUSELAGE FAIRING SEATLEMENT AREA BTW FS 597-693 (UNDER ACCESS 191AB, 191BB & 192BB). EXTERNAL SKIN AT FWD FUSELAGE FAIRING SEATLEMENT AREA BTW FS 597-693 (UNDER ACCESS 191AB, 191BB & 192BB) WAS REPAIRED PER EA 22-C7-53-0986 REV. IR
Part: NONE — CORRODED (ZONE 500) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 2-1 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #2 LH WING.
Part: STRINGER — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STGR 25LH BETWEEN FS=333.00 AND FS=310.00 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. DAMAGED STGR 25LH BETWEEN FS=333.00 AND FS=310.00 AT INTERNAL STRUCTURE OF 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 · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT. STGR 26RH BETWEEN FS=364.00 AND FS=333 AT INTERNAL STRUCTURE OF MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01
Part: NONE — CORRODED (ZONE 600) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 2-2 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #2 RH WING
Part: SKIN — BULGED · airframe 25,936 hrs · 19,641 cycles
BULGE ON FUSELAGE SKIN BTW FS295-310 & STGR 17R-18R. FUSELAGE SKIN BTW FS295-310 & STGR 17R-18R WAS REPAIRED PER EA 22-C7-53-0997 REV.IR
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON FLOOR BEAM 9RBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY FLOOR BEAM 9RBL IN STA. FS= 977 TO FS= 1098 AT AFT BAGGAGE BAY WAS REPAIRED PER CRJ 700 SRM 53-00-41-201-001-A01
Part: NONE — DENTED · airframe 25,936 hrs · 19,641 cycles
NICKS ON FUSELAGE SKIN EXTERNAL SURFACE, BTW FS517-FS581 & BTW STGR19L-25L, (SURROUNDING FWD CARGO DOOR CUTOUT SEVERAL LOCATIONS). FUSELAGE SKIN EXTERNAL SURFACE, BTW FS517-FS581 & BTW STGR19L-25L, (SURROUNDING FWD CARGO DOOR CUTOUT SEVERAL LOCATIONS) WAS REPAIRED PER EA 22-C7-53-0993 REV. IR AND EA EA 22-C7-53-0971 REV. IR
Part: NONE — CORRODED · corrosion level 2 · airframe 25,936 hrs · 19,641 cycles
CORROSION ON EWIS (PX31, PX19 ARNESS) SUPPORTS (2 EA´S, 1 PER SIDE) BETWEEN FS=797.00 TO FS= 807.00 AND 35LBL/35RBL AT LH/RH MLG WHEEL WELL SUPPORTS (2 EA´S, 1 PER SIDE) BETWEEN FS=797.00 TO FS= 807.00 AND 35LBL/35RBL AT LH/RH MLG WHEEL WELL WERE RELACED PER CRJ 700 SRM 51 42 20 001 001 A01
Part: NONE — CORRODED (ZONE 600) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 2-3 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #2 RH WING.
Part: NONE — CORRODED (ZONE 600)
PITTING CORROSION ON SLAT TRACKS 2-1 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #2 RH WING..
Part: NONE — CORRODED (ZONE 500) · airframe 25,936 hrs · 19,641 cycles
PITTING CORROSION ON SLAT TRACKS 3-1 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #3 LH WING.
Part: NONE — NONE (ZONE 200) · airframe 25,936 hrs · 19,641 cycles
CRACK ON CLIP AT AFT BAGGAGE BAY DOOR CUTOUT STRUCTURE BETWEEN FS=1047.00/FS=1051.30 AND STGR 7LH.
Part: SLAT TRACK — CORRODED (ZONE 500)
PITTING CORROSION ON SLAT TRACKS 1-2 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #1 RH WING..
Part: NONE — UNSERVICEABLE (400) · airframe 25,511 hrs · 19,254 cycles
AC ESS BUS CAUTION MESSAGE OCCURRED DURING CRUISE AT FL360 IN THE VICINITY OF MHT. CREW RAN QRH AND OUT OF CONCERN FOR LOSING THEIR EFDS CHOSE TO DECLARE AN EMERGENCY AND DIVERT TO BOS. THE A/C LANDED SAFELY IN BOS AND TAXIED TO THE GATE UNDER IT'S OWN POWER. A/C DID NOT LAND OVERWEIGHT. AC ESS BUS CAUTION IN FLIGHT / T/S B1 CODE 006878 PER CRJ 700 FIM 24-21-01-810-801. SWAPPED APU GCU WITH GEN 1 GCU. FAULT FOLLOWED. APU GCU P/N 766283C S/N 1954 IS NOW IN GEN 1 GCU LOCATION. GEN 1 GCU P/N 766283C S/N 1954 IS NOW IN APU GCU LOCATION. REMOVED AND REPLACED APU GENERATOR CONTROL UNIT IAW CRJ700 AMM 24-22-03-000/400-801. PERFORMED OPS CHECK OF THE APU GENERATOR SYSTEM IAW CRJ700 AMM 24-22-01-710-801. OP CHECKS GOOD. THIS CLEARS MEL."
Part: PROBE — FAULT MESSAGE (500) · airframe 25,204 hrs · 18,995 cycles
FLIGHT DIVERTED INTO TYS DUE TO A LOW FUEL CAUTION AND A FUEL IMBALANCE MESSAGE. CREW DID DECLARE AN EMERGENCY, THEIR FUEL INDICATORS STABILIZED AND THEY CANCELED THE EMERGENGY. EMERGENCY VEHICLES WERE NOT DISPATCHED. FLIGHT DID NOT LAND OVERWEIGHT. INTERROGATED MDC AND FOUND B1 CODE 007184 IN FAULT HISTORY FLAGGING LEFT COLLECTOR TANK PROBE. REMOVED AND REPLACED FUEL QUANTITY PROBE.
Part: NONE — NONE · airframe 25,129 hrs · 18,928 cycles
MX DIVERSION DUE TO PAX DOOR SQUEAL. NO WARNING OR PRESSURE ISSUES WITH SQUEAL. JUST A VERY LOUD NOISE AFTER CLIMBING THROUGH 28000FT COMING FROM MAIN CABIN DOOR. PREFORMED NORMAL LANDING IN IAD AND MX HAS BEEN ADVISED. HIGH PITCH NOISE COMING FROM MAIN CABIN DOOR IN FLIGHT.REMOVED AND REPLACED PAX DOOR SEAL IAW CRJ 700 AMM 52-11-07-000/400-801-A01. PERFORMED LEAK CHECK OF THE PAX DOOR IAW CRJ700 AMM 52-00-00-790-801-A01, 21-31-00-910-801/802. LEAK CHECK GOOD AT THIS TIME.
Part: NONE — NOT REPORTED (400) · airframe 25,109 hrs · 18,911 cycles
RH ENG BLEED AMBER CAUTION MSG. FOLLOWED CRJ700 FIM 36-12-01-810-806 & SUSPECT HPSOV. R&R HPSOV IAW CRJ700 AMM 36-12-05-000/400-801, OPS CHECK GOOD, MSG DID NOT REOCCUR.
2021
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 23,373 hrs · 17,331 cycles
CAPTAIN WINDSHIELD CRACKED ENROUTE TO KBHM CREW DECLARED AN EMERGENCY. THEY HELD FOR ABOUT 35 MINUTES TO BURN OFF THE FUEL BEFORE LANDING IN KIAD. EMERGENCY VEHICLES DID ONE LAP AROUND THE PLANE OFF THE RUNWAY WHILE THE CREW CANCELLED THE EMERGENCY. CAPTAIN DID INFORM THE PASSENGERS OF THE SITUATION AND HE DID NOT GIVE THE ORDER TO BRACE. THEY DID NOT LAND OVERWEIGHT. / REMOVED AND REPLACED CAPTAIN SIDE WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801.OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.
2020
Part: ACM — FAILED (RIGHT) · airframe 21,691 hrs · 15,834 cycles
WHILE ON TAXI IN AFTER LANDING, CREW RECEIVED A RIGHT PACK HIGH TEMP MESSAGE AND AN ODOR FILLED THE CABIN. CREW CONTINUED TO THE GATE, WHERE THE PASSENGERS DEPLANED VIA JET BRIDGE. NO EMERGENCY. DEFERRED THE RH PACK. REMOVED AND REPLACED ACM IAW CRJ700 AMM. LEAK TEST GOOD AT THIS TIME. OPS TEST GOOD AT THIS TIME. THIS CLEARS MEL.
Part: SKIN — DENTED (LT WING TE FLAP) · airframe 21,684 hrs · 15,827 cycles
LH INBD FLAP HAS DENT ON OUTBD END LOWER SKIN-C/A-REMOVED AND REPLACED LOWER SKIN ON LH INBOARD FLAP FROM FL92.800 TO OUTBOARD EDGE IAW SRM 57-52-01. SEE DT-CR-57-069 DTI.
Part: DRAG ANGLE — CRACKED (VERTICAL TO BODY) · airframe 21,684 hrs · 15,827 cycles
LEFT AFT VERT STAB TO FUSELAGE DRAG ANGLE HAS A 1" CRACK ON LEADING EDGE.-C/A-REPAIRED LEFT DRAG ANGLE IAW 55-31-00-201-001-A01
Part: FRAME — CORRODED (BS 310) · airframe 21,684 hrs · 15,827 cycles
FUSELAGE FRAME AT FS310.00 IS CORRODED FROM STR 26LH TO 26RH. AND ON THE AFT VERTICAL SURFACE. -C/A-REPAIRED FUSELAGE FRAME AT FS310.00 IAW SRM 53-00-06.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,684 hrs · 15,827 cycles
LH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.00. -C/A-C/W LH COCKPIT FLOOR BEAM REPAIR AT BL-12.00 IAW SRM 53-41-43.
Part: FLOORBEAM — CRACKED (BS 280) · airframe 21,684 hrs · 15,827 cycles
RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.00. -C/A-C/W RH COCKPIT FLOOR BEAM REPAIR AT BL-12.00 IAW SRM 53-41-43.
Part: WEB — CRACKED (BS 193) · airframe 21,684 hrs · 15,827 cycles
RH WEB/FLOOR @ F.S. 193.00 O/B OF ADG RETRACTION PUMP, HAS EVIDENCE OF A CRACK. -C/A-REPAIRED IAW SRM 53-11-43-201-001-A01
2019
Part: LIGHT — DAMAGED (CABIN) · airframe 21,684 hrs · 15,827 cycles
NUMBER 10L EMERGENCY FLOOR PATH LIGHT REQUIRES REPLACEMENT DUE TO DAMAGE.-C/A-COMPLETE:INSTALLED SERVICEABLE EMERGENCY LIGHT AT 10L POSITION IAW CRJ AMM 33-51-01.
Part: CRADLE — BROKEN (FWD FLASHLIGHT) · airframe 20,579 hrs · 14,677 cycles
ON TAKE OFF CABIN FLASHLIGHT HOLDER BROKEN FLASHLIGHT OPERATIVE. REMOVED AND REPLACED THE RECHARGEABLE FLASHLIGHT MOUNTING BRACKETS IAW AMM 25-61-02 OPS CHECK GOOD.
2018
Part: MANIFOLD — DEFECTIVE (NLG STEERING) · airframe 19,328 hrs · 13,669 cycles
IN FLIGHT SECENDING OUT OF FL250 STEERING INOP CAUTION MSG FOLLOWED QRH PROCEDURE. AFTER LANDING WITH STEERING INOP DID RESET PRCEDURE IN AOM V1, MSG CLEARED. TAXIED 20 FEET STEERING INOP MSG AGAIN. REMOVED AND REPLACED STEERING MANIFOLD IAW AMM 32-51-50. PERFORMED OPERATIONAL CHECK OF NOSEWHEEL STEERING IAW AMM 32-51-00. OPS CHECK GOOD. ALSO PERFORMED BITE TEST OF STEERING SYSTEM IAW AMM 32-50-00. BITE TEST GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.
Part: CONNECTOR — DIRTY (NWS MANIFOLD) · airframe 18,293 hrs · 12,813 cycles
NWS STEERING INOPERATIVE CAUTION MESSAGE DURING FLIGHT. STEERING INOPERATIVE CAUTION RESET IAW AOM VOLUME 1. RESET PROCEDURES PAGE 130.13. AIRCRAFT ABLE TO TAXI UNDER OWN POWER. MDC MESSAGE NWS MANIFOLD FAILED: B1-007465. CLEANED THE CONNECTORS ON MANIFOLD AND REINSTALLED IAW AMM 32-51-50. NO DEECTS NOTED. PERFORMED A NWS BITE TEST IAW AMM 32-50-00. BITE TESTED GOOD. ACFT OK FOR SERVICE.
Part: ECU — FAILED (NLG STEERING) · airframe 18,285 hrs · 12,808 cycles
DURING DECENT THROUGH FL180, A STEERING INOPERATIVE CAUTION POSTED. EMERGENCY DECLARED AND LANDED WITH NO ISSUE. ABLE TO RESET ON THE GROUND AND TAXI IN. REMOVED AND REPLACED THE ECU IAW MM 32-51-10. OPS CHECKED GOOD.
Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 17,856 hrs · 12,451 cycles
MAIN CABIN DOOR HARD TO OPEN. FOUND INNER HANDLE DETENT ROLLER STICKING. CLEANED AND LUBRICATED THE DETENT ROLLER IAW AMM 12-20-52. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. NO DEFECTS NOTED.
Part: STRUT — DISCHARGED (NLG) · airframe 17,786 hrs · 12,388 cycles
NOSE GEAR WOULD NOT RETRACT AFTER TAKE OFF. GEAR DISGREE WARNING MESSAGE POSTED. AFTER LANDING FOUND NOSE GEAR SHOWING NO CHROME AND MDC MESSAGE CODE B1-007432. INSP NLG AND FOUND NO CHROME SHOWING. SERVICED NLG W/NITROGEN IAW AMM 12-12-32 NO LEAKS NOTED. FOLLOWED FIM 32-21-10-810-810 AND PERFORMED OF PSS IAW AMM 32-61-00, OPS CHECKED GOOD. ACFT OK FOR SERVICE.
2017
Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 16,533 hrs · 11,403 cycles
REPAIR AFT FUSELAGE LOWER SKIN PANEL FS 1015-1047 STR 21L-23L. C/W REPAIR OF DAMAGED AREA IAW ERS-CR-53MR-1832.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 16,533 hrs · 11,403 cycles
RT SIDE OF CROSSBEAM AT FS280.00 IS CRACKED. REMOVED AND REPLACED RT CROSSBEAM SECTION AT FS280.00 IAW SRM 51-42-06, AND SRM 51-42-10.
Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 16,533 hrs · 11,403 cycles
LT SIDE OF CROSSBEAM AT FS280.00 IS CRACKED. REMOVED AND REPLACED LT CROSSBEAM SECTION AT FS280.00 IAW SRM 51-42-06, AND SRM 51-42-10.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 16,533 hrs · 11,403 cycles
LT BULKHEAD LOWER WEB AT FS280.00 CORRODED AT INBD EDGE. PERFORMED PERMANENT REPAIR ON LT BULKHEAD LOWER WEB AT FS280.00 IAW ERS-CR-53MR-2806.
Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 16,533 hrs · 11,403 cycles
RT BULKHEAD LOWER WEB AT FS280.00 CORRODED AT INBD EDGE. PERFORMED PERMANENT REPAIR ON RT BULKHEAD LOWER WEB AT FS280.00 IAW ERS-CR-53MR-2806.
Part: SELECTOR VALVE — FAILED (MLG) · airframe 15,809 hrs · 10,815 cycles
WHEN SELECTING LG LEVER TO DOWN POSITION GEAR DISAGREE WARNING MESSAGE POSTED RAN THE CHECKLIST AND MANUALLY LOWERED GEAR AND GOT THREE GREEN WHEN CYCLING LG LEVER PROX SYS FAULT 1 STATUS MESSAGES POSTED BRIEFLY STEER INOP UPON LANDING. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10 COMPLETED INSTALLATION UP TO STEP 5E. NOSE WHEEL STEERING OPS CHECK GOOD IAW AMM 32-51-00. PERFORMED OPS CHECK LDG GEAR EXT/RETRACTION SYSTEM IAW CRJ AMM 32-30-00 NO DEFECTS NOTED
Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 15,665 hrs · 10,693 cycles
LEFT AFT EXTERIOR EMERGENCY LIGHT AND BOTH RT OVERWING EXTERIOR EMERGENCY LIGHTS FAIL TO ILLUMINATE. REPLACED THE CHARGER ASSY . OPERATIONAL CHECK IAW AMM 33-51-15.
2016
Part: DOOR SILL — CORRODED (AFT CARGO) · airframe 15,467 hrs · 10,529 cycles
AFT CARGI DOOR CUTOUT SILL IS CORRODED IN SEVERAL AREAS ALONG THE WHOLE LENGTH. AFT BAGGAGE DOOR CUTOUT SILL REMOVED AND REPLACED IAW SRM 51-42-06
Part: ATTACH ANGLE — CRACKED (PAX DOOR) · airframe 15,467 hrs · 10,529 cycles
PAX DOOR AFT STEP SKIN ATTACH ANGLE CRACKED BY THE PULLEY BRACKE. REPAIRED PAX DOOR ATTACH ANGLE IAW SRM 52-11-04.
Part: STEP — CRACKED (PAX DOOR) · airframe 15,467 hrs · 10,529 cycles
PAX DOOR AFT STEP SKIN IS CRACKED AT SECOND FROM TOP STEP BOTTOM OF THE VERTICAL ANGLE.CA REPAIRED PAX DOOR AFT STEP SKIN AT SECOND FROM TOP STEP BOTTOM OF THE VERTICAL ANGLE IAW SRM 52-11-04.
Part: SKIN — CRACKED (PAX DOOR) · airframe 15,467 hrs · 10,529 cycles
PAX DOOR FWD STEP SKIN PANEL CRACKED AT TOP VERTICAL ANGLE. REPAIRED PAX DOOR FWD STEP SIDE SKIN VERTICAL ANGLE IAW SRM 52-11-04.
Part: SKIN — CRACKED (PAX DOOR) · airframe 15,467 hrs · 10,529 cycles
PAX DOOR FWD STEP SKIN PANEL CRACKED AT 3RD DOWN FROM THE TOP STEP.CA REMOVED PAINT AND DIRT FOUND NOT TO BE CRACKED RESTORED PAINT FINISH IAW CRJ SRM 51-25-01.
Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 15,240 hrs · 10,342 cycles
LEFT WINDSHIELD HEAT CAUTION DURING CLIMBOUT. REMOVED AND REPLACED THE WINDSHIELD HEAT CONTROLLER IAW AMM TASK 30-41-06. OPS CHECKED GOOD.
2015
Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 12,165 hrs · 7,997 cycles
FIRST OFFICERS FLASHLIGHT INOPERATIVE. R & R FIRST OFFICERS FLASHLIGHT ASSEMBLY IAW CND AMM 25-60-02. OPERATIONS CHECKED GOOD AT THIS TIME.
Part: HINGE — LACK OF LUBE (PAX DOOR) · airframe 11,562 hrs · 7,538 cycles
PASSENGER DOOR VERY DIFFICULT TO CLOSE. CLEANED & LUBED PAX DOOR HINGE & SHOOT BOLTS, CHECKED ROLLERS IAW AMM 52-11-00.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 11,344 hrs · 7,368 cycles
OUTBOARD FLIGHT SPOILERS CAUTION IN FLIGHT. PERFORM OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 11,342 hrs · 7,367 cycles
FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R IAW AMM 25-61-02. OPERATIONS CHECKED GOOD.
Part: FLASHLIGHT — OVERHEATED (GALLEY) · airframe 10,866 hrs · 7,007 cycles
SMELL OF BURNING WIRES IN COCKPIT & FWD CABIN, ALL CREW SMELLED IT. FRONT GALLEY FLASHLIGHT OVERHEATING. REPLACED FLASHLIGHT IAW AMM 25-60-00.
2014
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 10,414 hrs · 6,623 cycles
ON FINAL APPROACH, WHEN DEPLOYING FLAPS GOT SLATS FAIL CAUTION MSG. FOLLOWED CHECKLIST, DECLARED EMER LANDING WITH FLAPS 45 SLATS 0. TRANSFERRED TO NRWC 1 EA-ORD-01232. TRANSFERRED FROM NRWC 1 EA-ORD-01232. PERFORMED DVI OF THE SLATS IAW AMM 27-81-00, NO DEFECTS NOTED AT THIS TIME. OPERATIONS CHECKED GOOD.
Part: ACTUATOR — TRIPPED (LE SLAT) · airframe 9,973 hrs · 6,295 cycles
SLAT FAIL CAUTION MSG. ACTION NR 1 OF ETN-CR-27-084, FOUND ON RT WING SLAT ACTUATOR NR 2 & NR 4 TRIP INDICATOR ACTIVE. RESET & PERFORMED DVI FOR ANY EVIDENCE OF WATER ACCUMULATION, NO DEFECTS NOTICE AT THIS TIME IAW AMM 27-81-09. PERFORMED SEVERAL TIMES OPERATIONS CHECK OF SLAT SYS IAW AMM 27-50-00. NO FAULTS AT THIS TIME.
2013
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 8,469 hrs · 5,251 cycles
ON FLIGHT 3708 CREW RECEIVED SLATS FAIL MASTER CAUTION MESSAGE. DECLARED AN EMERGENCY FOR SAFETY & LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. OPERATIONAL TEST OF THE FLAPS & SLATS SYS, OPERATIONS CHECKED GOOD IAW 27-50-00. THE ACFT RETURN TO SERVICE.
Part: ENGINE — POWER LOSS (LEFT) · airframe 7,949 hrs · 4,910 cycles
CREW REPORTED DURING DEPARTURE, BETWEEN 80KTS AND V1., ACFT FELT SLIGHT YAW MOVEMENT TO THE SIDES. AT THE SAME TIME THE F/O CALLED FOR AN ABORT DUE TO LT ENGINE POWER LOSS. CREW INITIATED ABORT PROCEDURES. COMPLETED ENGINE SHUTDOWN PROCEDURES. INFORMED OF SPARKS FROM NR 1 ENGINE DURING TAKEOFF. F/A REPORTED A LOUD BANG, POSSIBLY TWO DURING TAKEOFF ROLL. ACFT REMOVED FROM SERVICE. COMPLIED WITH 002-05-900-013. HIGH ENERGY STOP/RTO DAMAGE GENERAL VISUAL INSPECTION. NO DEFECTS. THE ACFT WAS RETURNED TO SERVICE.
Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 7,832 hrs · 4,835 cycles
FA NR 1 FLASHLIGHT INOPERATIVE. PERFORMED OPS CHECK OF FLASHLIGHT AS REQ OPS CHECKED GOOD.
Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 6,082 hrs · 3,755 cycles
DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. WILL NOT HOLD CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW CRJ MM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: BEARING — FAILED (CONTROL COLUMN) · airframe 5,899 hrs · 3,645 cycles
FLIGHT 3728. ON ARRIVAL, NOTED THE YOKE HAD ABOUT 1/4 TO 1/8 INCH OF PLAY. IN ROLL AXIS IT RACHETS, SEEMED LOOSE AND HAS PLAY IN YOKE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FORWARD AND AFT BEARING ON F/O CONTROL COLUMN SHAFT IAW AMM 27-31-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
2012
Part: BRACKET — BENT (FUSELAGE) · airframe 5,494 hrs · 3,399 cycles
DURING HEAVY CHECK FOUND PASSENGER DOOR FORWARD LOWER SURROUND STRUCTURE ON FUSELAGE SIDE BENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FABRICATED BRACKET IAW SRM 51-24-16. INSTALLED BRACKET IAW SRM 51-42-06. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,357 hrs · 2,667 cycles
FLIGHT 4575, CREW REPORTED EMERGENCY LIGHT IN CABIN ABOVE CLOSET INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPS CHECKED OF EMERGENCY LIGHTING IAW AMM 33-51-00. SYSTEM CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.
Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 4,013 hrs · 2,446 cycles
ON FLIGHT 3832, THE CREW REPORTED THAT WHILE ON DESCENT THEY RECEIVED A HYDRAULIC 2 LOW PRESSURE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRFCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE DRIVEN HYDRAULIC PUMP PER AMM 29-11-01. AIRCRAFT RETURNED TO SERVICE.
2011
Part: FAN — FAILED (COCKPIT DISPLAY) · airframe 2,592 hrs · 1,608 cycles
FLIGHT 3600, CREW REPORTED THAT ON TAKEOFF, RECEIVED A DISPLAY COOL CAUTION MESSAGE. CREW FOLLOWED AOM PROCEDURES AND THE MESSAGE CLEARED. CAME BACK DURING CRUISE AND CONTINUED AOM PROCEDURES AND MESSAGE CLEARED AND THEN CAME BACK. CREW ELECTED TO DIVERT. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 AND 2 COCKPIT DISPLAY COOLING FANS AND FILTER IAW AMM 21-24-12 AND AMM 21-24-16. AIRCRAFT WAS RETURNED TO SERVICE.
Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 2,089 hrs · 1,325 cycles
FOR FLIGHT 4667 THE CREW REPORTED THE FLASHLIGHT IN THE COCKPIT WAS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW FLASHLIGHT ASSEMBLY IAW AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: FAN — FAILED (E/E BAY) · airframe 1,012 hrs · 657 cycles
ON FLIGHT 3832 DURING THE APPROACH TO CYZ THE CREW NOTICED A BURNT PLASTIC ODOR SHORTLY AFTER HEARD DISPLAY FAN KICKING ON-OFF THEN DISPLAY COOL, CAUTION MESSAGE. THE CREW SELECTED FLT ALTN ON CONT, - DISPLAY FAN. DISPLAY COOL, CAUTION MESSAGE EXTINGUISHED. BURNT PLASTIC ODOR DISSIPATED AND DID NOT RETURN, UPON LANDING, DISPLAY COOL CONT, CAUTION MESSAGE RETURNED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PILOTS NR 1 AVIONICS COOLING FAN IAW CRJ-700 AMM 21-24-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.