N953LR
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.
31 reports on file, 2015-08-24 – 2024-05-27.
Part: CONNECTOR — DIRTY (SSCU) · airframe 17,598 hrs · 13,269 cycles
RUDDER LIMITER CAUTION AFTER TAKEOFF / REMOVED SSCU 1, CLEANED CONNECTORS AND LUBRICATED SEALS OF ELECTRICAL CONNECTORS ON MOUNTING TRAY THEN REINSTALLED SSCU 1 IAW CRJ 900 AMM 27-61-05-000/400-801-A01, PERFORMED SPOST IAW CRJ 900 AMM 27-61-05-740-801-A03 OPS CHECK GOOD FAULT DID NOT REOCCUR.
Part: ANGLE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
INSIDE PAX DOOR DD 7A MID FOUND CORRODED. REQUIRES REPLACEMENT.
Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
PAX DOOR INNER SKIN FOUND CORRODED AT SEVERAL SPOTS.
Part: FRAME ANGLE — CORRODED (BS 319 S20R) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
UPON REMOVAL OF STRINGER 20R INTERCOSTAL FOUND FWD. FRAME CLIP LOCATED AT F.S. 319 TO BE CORRODED. REQUIRES R&R
Part: STRINGER — CORRODED (BS 265-280 S26R) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
STRINGER 26R IS CORRODED BETWEEN FS 265.00 AND 280.00.
Part: INTERCOSTAL — CORRODED (BS 333 -349 S20R) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
STGR20R INTERCOSTAL IS CORRODED BETWEEN FS 333 AND FS 349.
Part: STRINGER — CORRODED (BS 265-280 S26R) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
STRINGER 26R IS CORRODED BETWEEN FS 265.00 AND 280.00.
Part: STRINGER CLIP — CORRODED (BS 349 S20R) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
STGR 20R ANGLE IS CORRODED AT FS 349.
Part: NUT PLATE — CORRODED (GALLEY MOUNT) · corrosion level 2 · airframe 17,442 hrs · 13,144 cycles
CORROSION ON AFT O/B MOUNTING NUT-PLATE FOR GALLEY 1 AND ON IT'S CORRESPONDING R/H FLOOR SILL BETWEEN FS 310.00 TO FS 319.70 FLOOR SILL PN SH670-32172-11
Earlier reports · 2015–2023 · 22 reports
2023
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 16,719 hrs · 12,577 cycles
7 CEIL EMERG LIGHTS INOP OCMX OP CHECKED GOOD NORMAL CONFIGURATION
Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 16,544 hrs · 12,433 cycles
EMER LIGHT ARM INTERMITTENT. R2 THE EMER EXIT LIGHT RELAY
2021
Part: RIB — CRACKED (RIGHT WING) · airframe 13,644 hrs · 10,354 cycles
CRACK ON RIB LEADING EDGE SS58.41 AT RIGHT WING. CORRECTIVE ACTION: RIB LEADING EDGE SS58.41 AT RIGHT WING WAS REPAIR PER REO 690-57 -41-240 REV --
Part: STRINGER — CORRODED (BS 310-327 S27) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON STRINGER 27 IN STA. FS310 TO FS327AT MAIN AVIONICS COMPARTMENT. STRINGER 27 IN STA. FS310 TO FS327 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR.6
Part: STRINGER — CORRODED (BS 280-295 S27) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON STRINGER 27 IN STA. FS280 TO FS295 AT MAIN AVIONICS COMPARTMENT. STRINGER 27 IN STA. FS280 TO FS295 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR.6.
Part: ANGLE — CRACKED (LH MAIN FUEL TAN) · airframe 13,644 hrs · 10,354 cycles
CRACK IN CANISTER WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK|CANISTER WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL: TANK. WAS REPAIRED PER REO 670-57-42-577 REV. --
Part: ANGLE — CRACKED (RH MAIN FUEL TAN) · airframe 13,644 hrs · 10,354 cycles
CRACK IN CANISTER WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK|CANISTER WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --
Part: INTERCOSTAL — CORRODED (BS 337-364 S25L) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON STRINGER 25RH IN STA. FS= 337 TO FS= 364 AT MAIN AVIONICS COMPARTMENT. (E/E).STRINGER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01
Part: STRINGER — CORRODED (BS 280-327 S26R) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON STRINGER 26RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT|STRINGER 26RH IN STA. FS=280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM-51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
Part: FRAME — CORRODED (BS 295) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON FRAME FS= 295 BETWEEN STRG 26LH AT MAIN AVIONICS COMPARTMENT|FRAME FS 295 BETWEEN STRG 26LH TO 26RH WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03.
Part: STRINGER — CORRODED (BS 280-327 S25R) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON STRINGER 25RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT |STRINGER 25RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01
Part: FRAME — CORRODED (BS 310 S25L-R) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON FRAME FS= 310 BETWEEN STRG 25LH TO 25RH AT MAIN AVIONICS COMPARTMENT|FRAME FS 310 BETWEEN STRG 25LH TO 25RH WAS REPAIRED PER CRJ900 SRM 53-00-06-201-001-A03
Part: STRINGER — CORRODED (BS 280-327 S24R) · airframe 13,644 hrs · 10,354 cycles
CORROSION ON STRINGER 24RH IN STA. FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT |STRINGER 24RH IN STA . FS= 280 TO FS= 327 AT MAIN AVIONICS COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-20-001-001-A01
2020
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 12,086 hrs · 9,320 cycles
AFT FA FLASHLIGHT INOP. PLACED ON MEL.
Part: EPSU — INOPERATIVE (CABIN) · airframe 12,035 hrs · 9,283 cycles
PAX DOOR EMERGENCY EXIT SIGN INOP. REPLACED EPSU NR 1.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,423 hrs · 28,893 cycles
ALL EMERG LIGHTS INOP. CHARGED BATTERIES
2019
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 10,784 hrs · 8,362 cycles
AFT F/A FLASHLIGHT INOP. REPLACED BATTERY
2017
Part: CONTROL PANEL — DEFECTIVE (PAX DOOR) · airframe 5,826 hrs · 4,542 cycles
PAX DOOR WOULD NOT OPEN (DOOR MOTOR IS CONTINUOUSLY POWERED. GOES UP AUTOMATIC). REPLACED PAX DOOR CONTROL PANEL.
Part: HINGE — GOUGED (PAX DOOR) · airframe 5,648 hrs · 4,413 cycles
PAX DOOR HINGE ON DOOR SIDE IS GOUGED ON NR 24 LUG FROM THE FWD SIDE.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 3,954 hrs · 3,073 cycles
AFT FA'S FLASHLIGHT INOP. PLACED ON MEL.
2015
Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 649 hrs · 535 cycles
AFT F/A FLASHLIGHT RED LED NOT BLINKING.
Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 174 hrs · 144 cycles
FWD F/A FLASHLIGHT INOPERATIVE.