N302PQ
Registered owner: BANK OF UTAH TRUSTEE, UT (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.
46 reports on file, 2015-01-20 – 2024-05-24.
Part: DOOR FRAME — CRACKED (RT OVERWING) · airframe 22,522 hrs · 16,986 cycles
R/H AFT OVERWING EMERGENCY EXIT DOOR S/N B1391 TOP FORMER IS CRACKED. REPAIRED IAW ENDEAVOR AIR EA CRJ952-16639 REV IR DATED 5/12/2024
Part: FLOORBEAM — CORRODED (BS 280) · airframe 22,522 hrs · 16,986 cycles
FS 280.00 RH CROSSBEAM IS CORRODED INSTALLED SERVICEABLE FS 280.00 RH CROSSBEAM WITH P/N CC670-34094-2 IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01 AND 51-42-22-001-001-A01. INSTALLED RH CAP ANGLE FROM CROSSBEAM IAW CRJ900 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED SERVICEABLE RH FS 280 CROSSBEAM WITH P/N CC670-34094-2 IAW CRJ 900 SRM 51-40-11-001-001-A01.
Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 22,522 hrs · 16,986 cycles
FS 280.00 LH CROSSBEAM IS CORRODED REMOVED FS 280.00 LH CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01. INSTALLED NEW SERVICEABLE LH FS 280 CROSSBEAM WITH P/N CC670-34094-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND CRJ900 SRM 51-42-13-001-001-A01.
Part: FORMER — CORRODED (EMERGENCY EXIT) · airframe 22,522 hrs · 16,986 cycles
L/H FWD OVERWING EMERGENCY EXIT DOOR S/N B1392 TOP FORMER IS CRACKED. REPAIRED IAW ENDEAVOR EA CRJ952-16640 REV IR DATED 5/12/24.
Earlier reports · 2015–2023 · 42 reports
2023
Part: BATTERY PACK — INOPERATIVE · airframe 19,858 hrs · 14,657 cycles
FORWARD GALLEY AND FORWARD ENTRANCE COMPARTMENT EMERGENCY LIGHTS INOP R/R EPSU BATTERY PACK 1 IAW TASK 33-51-17-000-801. OPS CHECK GOOD. P/N ON/OFF 2013-1ASMI S/N OFF 12631 S/N ON 16232
2020
Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 15,391 hrs · 10,852 cycles
AFT CARGO FLOOR SILL AT DOOR IS CORRODED. REMOVED AND REPLACED AFT CARGO FLOOR SILL, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 51-42-13-001-001-A01 LEAK CHECK GOOD.
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 15,391 hrs · 10,852 cycles
CARGO BAY FLOOR SUPPORT LBL 27 AT FS 1031 IS CORRODED. FABRICATED & INSTALLED NEW FLOOR SUPPORT & SPLICES AT LBL 27 BETWEEN FS 977 AND FS 1038, IAW CRJ 900 SRM 53-00-41-201-001-A03.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,391 hrs · 10,852 cycles
CABIN FLOOR SEAT TRACK AT RBL 9 STARTING AT APPROXIMATELY FS 847.00+16 IS PITTED/CORRODED IN MULTIPLE LOCATIONS. REPLACED SEAT RAIL SEGMENT FROM FS 847.00+16 TO APPROXIMATELY FS 977 RBL 9, CRJ 900 SRM 53-00-49-201-002-A01 & AMM 53-00-49-400-801-A12.
Part: WEB — CORRODED (BS 280) · airframe 15,391 hrs · 10,852 cycles
THE RT FS 280 WEB IS CORRODED BEHIND THE CORROSION CAP. REMOVED FOD FROM UNDER COCKPIT TO FS 295, IAW CRJ 900 SRM 51-26-00-001-001-A01.
Part: WEB — CORRODED (BS 280) · airframe 15,391 hrs · 10,852 cycles
THE LT FS 280 WEB IS CORRODED BEHIND THE CORROSION CAP. REMOVED FOD FROM UNDER COCKPIT TO FS 295, IAW CRJ 900 SRM 51-26-00-001-001-A01.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 15,391 hrs · 10,852 cycles
CABIN FLOOR SEAT TRACK AT RBL 9 FROM FS 349 TO FS 485 IS CORRODED. REMOVED AND REPLACED CORRODED SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK P/N: SH670-32159-1 AND TRACK ANCHORS P/N: CDSP1900-501, IAW CRJ 900 AMM 53-00-49-400-801-A12 AND CRJ900 SRM 51-41-04-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 349-485) · airframe 15,391 hrs · 10,852 cycles
CABIN FLOOR SEAT TRACK AT LBL 9 FROM FS 379 TO FS 485 IS CORRODED. FABRICATED NEW SEAT TRACK, IAW CRJ 900 SRM 53-00-49-201-002-A01. INSTALL NEW SEAT TRACK, IAW CRJ 900 AMM 53-00-49-400-801-A12.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 15,391 hrs · 10,852 cycles
RT INBOARD FLAP HAS (1) DENT ON LOWER SKIN. DENT IS APPROXIMATELY 6.00" L X .250" W X .005" D. LOCATED APPROXIMATELY 16.00" OUTBOARD OF INBOARD EDGE OF FLAP AND 12.00" UP FROM TRAILING EDGE. REPAIRED R/HI/BF/AP, IAW CRJ 900 SRM 57-52-01-201-001-A01 REPAIR TYPE IV.
Part: SUPPORT — CRACKED (EXTERNAL POWER) · airframe 15,391 hrs · 10,852 cycles
EXTERNAL POWER RECPTICAL SUPPORT STRUCTURE CRACKED. REPAIRED CRACKED EXTERNAL POWER RECEPTICAL SUPPORT STRUCTURE BY REMOVING CRACKED SUPPORT STRUCTURE AND REPLACING WITH NEW SERVICEABLE SUPPORT STRUCTURE PN CC670-33401-3, IAW CRJ 900 SRM 51-42-06-001-001-A01 & 51-40-11-001-001-A01.
Part: ANGLE — CORRODED (CABIN) · airframe 15,391 hrs · 10,852 cycles
FS 280 J-ANGLE IS CORRODED. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE J-ANGLE P/N CC 670-34095-1, IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,391 hrs · 10,852 cycles
PAX DOOR FLOOR SUPPORT ANGLE IS CORRODED. REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT ANGLE P/N: SH670-31875-7S, IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. OPERATIONS CHECK GOOD.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,391 hrs · 10,852 cycles
THE FS 280 FLOOR BEAM HAS SEVERAL CORRODED RIVETS BETWEEN LBL 12 AND RBL 12. REMOVED AND REPLACED LT AND RT FS 280 CROSSBEAMS, IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.
Part: FITTING — CORRODED (GLLY DOOR FRAME) · airframe 15,391 hrs · 10,852 cycles
GALLEY SERVICE DOOR FRAME FITTING AT FS 349.00 JUST ABOVE FLOOR HAS AN AREA OF CORROSION. REMOVED & REPLACED SERVICE DOOR FITTING, IAW CRJ 900 SRM 51-42-21-001-001-A01.
Part: BRACKET — CORRODED (AFT CARGO BAY) · airframe 15,391 hrs · 10,852 cycles
FUSELAGE FRAME STATION 1047.00 HAS CORROSION AT FLOOR LEVEL AT AFT CARGO OPENING. REMOVED BRACKET P/N: MM670-34112-015. FOUND NO CORROSION ON FRAME. REPLACED BRACKET MM670-34112-015, IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-20-001-001-A01.
Part: SEAT TRACK — CORRODED (BS 784-847) · airframe 15,391 hrs · 10,852 cycles
LT SIDE SEAT TRACK FROM FS 784 TO FS 847+16 IS CORRODED. REMOVED AND INSTALLED LT SIDE SEAT TRACK P/N: BA690-3000N455305 AT FS 784 TO 847+16, IAW CRJ 900 AMM 53-00-49-000-801-A12 AND CRJ 900 AMM 53-00-49-400-801-A12.
Part: LIGHT — SPARKS (CAPTAIN'S MAP) · airframe 15,357 hrs · 10,819 cycles
CA SIDE MAP LIGHT SHOT SPARKS OUT IN FLIGHT. BURNING SMELL IN COCKPIT BRIEFLY AFTER SEEING SPARKS. C/W FDE 21-21-00, PERFORMED DEACTIVATION PROCEDURE OF CA MAP LIGHT, REF CHAPTER 206 OF 33-11-1A CBP1 P2 PULLED AND COOLARD. ENTERED INTO MM02 PLACARD INSTALLED MOC NR 95974, NOTIFIED KEVIN CRUSOE US AIR PORTS. REMOVED CA MAP LIGHT, IAW AMM 33-13-03, INSPECTED WIRING AND FOUND BROKEN CONNECTOR LUG (PN 2-160759-1). REMOVED BROKEN CONNECTOR STOWED WIRE, IAW ESPM 20-12-05 AND BAGGED W-INSULATOR RECEPTACLE ALONG. RE-INSTALLED DISCONNECTED MAP LIGHT, IAW AMM 33-13-03. ITEM REMAINS DEFERRED, IAW MEL 33-11-1A, AT THIS TIME. REQUIRES NEW TERMINAL LUG (REF:ESPM 20-16-61) LUG-2-160759-1. R & R MAP LIGHT, IAW CRJ 900 AMM 33-13-03. OP'S CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. PLACARD REMOVED MMO2 UPDATED MOC NR 95909 NOTIFIED.
2019
Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 12,685 hrs · 8,781 cycles
ENROUTE STOWING CAPT CHART LIGHT BETWEEN THE WINDOWS A PUFF OF SMOKE APPREARED. REMOVED AND REPLACED MAP READING LIGHT IAW AMM 33-13-03.OPS CHECK GOOD.
2018
Part: HOSE — DAMAGED (O2 MASK) · airframe 9,977 hrs · 6,791 cycles
OBSERVERS O2 MASK LEAK DETECTED. ONE OF THE HOSES SHOW BREAKAGE/DAMAGE DEFFERING OBSERVERS OXYGEN SYSTEM IAW MEL 35-10-1. REMOVED AND REPLACED OBSERVERS SEAT O2 MASK IAW AMM 35-11-12. LEAK TEST GOOD IAW AMM 35-10-00. NO LEAKS DETECTED.
2017
Part: STRAP — DAMAGED (OXYGEN MASK) · airframe 9,142 hrs · 6,245 cycles
FIRST OFFICER`S OXYGEN MASK DONNING STRAPS HAD A HOLE IN IT. REMOVED AND REPLACED THE OXYGEN MASK IAW AMM 35-11-12. OPS CHECKED GOOD.
Part: STRAP — BROKEN (FLASHLIGHT) · airframe 9,171 hrs · 6,217 cycles
FORWARD FA EMERGENCY FLASHLIGHT STRAPS ARE BROKEN AWAY. INSTALLED NEW SEAL AS REQUIRED REF AMM 25-60-10 P/N OFF/ON A1-18-1030.
Part: FAN — FAILED (DISPLAY) · airframe 8,742 hrs · 5,925 cycles
DISPLAY FAN MADE A LOUD NOISE AFTER LANDING AND HAD A BURNING ODOR. PULLED & COLLARD THE CIRCUIT BREAKER P1 & B-2. R & R THE NR 2 COCKPIT DISPLAY GROUND FAN IAW AMM 21-24-12.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 7,822 hrs · 5,284 cycles
OBSERVED EMERGENCY FLASHLIGHT IN GALLEY WAS NOT BLINKING. R&R GALLEY EMERGENCY FLASHLIGHT BATTERY. OPS CHK GOOD IAW AMM 25-61-00.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,631 hrs · 5,154 cycles
AFTER REMOVAL OF BS 280 FLOORBEAM ANGLE, FOUND CORROSION LBL 11. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, 51-42-21, 51-42-10, AND REO 670-53-11-594 REV A.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,631 hrs · 5,154 cycles
RIGHT FLOORBEAM CORRODED AT BS 280. AND FOUND TO BE OUT OF LIMITS. REPAIRED THE FLOORBEAM IAW REO# 670-53-21-139.
Part: ANGLE — CORRODED (BS 280) · airframe 7,631 hrs · 5,154 cycles
LEFT BS 280 BULKHEAD LOWER DOOR POST ANGLE CORRODED, LBL 11. REMOVED & REPLACED IAW SRM 51-42-13.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,631 hrs · 5,154 cycles
AFTER REMOVAL OF THE BS 280 FLOORBEAM ANGLE, FOUND CORROSION ON THE FLOORBEAM AT RBL 11. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, 51-42-21, 51-42-10, AND REO 670-53-11-594 REV A.
Part: DIAPHRAGM — CORRODED (BS 349-364) · airframe 7,631 hrs · 5,154 cycles
LEFT CENTER DIAPHRAM BETWEEN BS 364 AND 349 IS CORRODED. NO ALLOWABLE DAMAGE IAW SRM 53-21-23. REMOVED AND REPLACED THE DIAPHRAM IAW SRM 51-42-06 AND 51-42-21.
Part: FLOORBEAM — CORRODED (BS 280) · airframe 7,631 hrs · 5,154 cycles
BS 280 FLOORBEAM ANGLE CORRODED, LBL11.- RBL 11. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06 AND 51-42-21.
Part: DIAPHRAGM — CORRODED (BS 349-364) · airframe 7,631 hrs · 5,154 cycles
RIGHT CENTER DIAPHRAM BETWEEN BS 364 AND 349 IS CORRODED. NO ALLOWABLE DAMAGE IAW SRM 53-21-23. REMOVED AND REPLACED THE DIAPHRAM IAW SRM-51-42-21 AND 51-42-06.
Part: WEB — CRACKED (PAX DOOR) · airframe 7,631 hrs · 5,154 cycles
MAIN ENTRY DOOR FORWARD WEB IS CRACKED AT BOTTOM OF THE RISER. REMOVED DAMAGE AND REPAIRED THE WEB IAW SQM 52-11-04.
Part: WEB — CRACKED (PASSENGER DOOR) · airframe 7,631 hrs · 5,154 cycles
MAIN ENTRY DOOR STAIR AFT WEB IS CRACKED AT BOTTOM OF RISER. REPAIRED THE STAIR WEB IAW SRM-52-11-04.
2016
Part: HOSE — DAMAGED (OXYGEN MASK) · airframe 7,330 hrs · 4,958 cycles
AFT FLT ATTENDANT OXYGEN MASKS) HAVE KINKS AND CUTS ON BOTH HOSES. REMOVED AND REPLACED BOTH AFT FLT ATTENDANT OXYGEN MASKS IAW AMM 35-21-09.
Part: LIGHT — SPARKS (COCKPIT) · airframe 7,291 hrs · 4,934 cycles
CA MAP LIGHT SPARKED, CB POPPED. INOP CON DEFFERED CAPT MAP LIGHT IN ACC IAW MEL 33-11-1A. CBP P2 COLLARED ENT INTO MMO2. PLACARD INST. MX NOTIFIED. REMOVED AND REPLACED CAPTAINS MAP LIGHT IAW AMM 30-13-03 TO CLEAR DEFFERED MAINT. NO DEFECTS NOTED MOC NOTIFIED. PLACARD AND CIRCUIT BREAKER COLLAR REMOVED MM02 UPDATED.
Part: OXYGEN MASK — UNWANTED DEPLOY (SEAT 9 CD) · airframe 7,059 hrs · 4,777 cycles
OXYGEN MASK ABOVE 9CD DEPLOYED AT TAKEOFF. OXYGEN MASK STOWAGE PANEL NOT SECURED PROPERLY. RESTOWED THE MASKS IAW AMM 35-21-09. OK FOR SERVICE.
Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 6,351 hrs · 4,286 cycles
O2 MASK F/O SIDE, AIRHOSE COVER DAMAGED. R & R F/O O2 MASK IAW AMM 35-11-12. OPS CHECK GOOD.
Part: FAN — ODOR (CARGO BAY) · airframe 6,306 hrs · 4,250 cycles
DISTINCT ODOR WAS DETECTED BY THE FAS AND SHORTLY AFTER "RECIRC FAIL" STATUS MESSAGE APPEARED. DEFERRED RECIRC FANS IAW MEL 21-22-1, CAT-C, M-ACTION C/W. PLACARDED AND UPDATED MMO2. MOC NOTIFIED. R & R RECIRCULATION AFT CARGO BAY, LT SIDE FAN IAW AMM 21-22-10. OPS CHECKS GOOD MMO2 UPDATED PLACARD REMOVED MAINTENANCE NOTIFIED, PN ON/OFF GG670-95022-7, SN ON:01407, SN OFF:L147100355.
2015
Part: DOOR SEAL — MISSING (EMERGENCY EXIT) · airframe 3,640 hrs · 2,441 cycles
LEFT FWD OVERWING EMER EXIT DOOR MISSING LOWER SEAL. REPLACED LOWER SEAL, SEE CONTINUATION CARD 093715 FOR DETAILS. EMER EXIT SEAL MISSING.
Part: LIGHT — UNSECURE (CABIN) · airframe 3,609 hrs · 2,414 cycles
EMERGENCY LIGHTING STRIP IN GALLEY AREA NEEDS RE-SECURING. SECURED GALLEY EMER LIGHT STRIP IAW AMM 33-51-01.
Part: LIGHT — LOOSE (CABIN) · airframe 3,262 hrs · 2,166 cycles
EMERGENCY LIGHT STRIP COMING UP & LOOSE IN FWD LT GALLEY ON FLOOR. CLEANED THE SURFACE & SECURED SAME EMER FLOOR LIGHT MARKING. OPERATIONS CHECKED GOOD IAW AMM 33-51-01.
Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 3,253 hrs · 2,160 cycles
NUMBER 1 EMER LIGHT BATTERY PACK WOULD NOT ACCEPT CHARGE. R & R BATTERY PACK IAW AMM 33-51-17. OPERATIONS CHECKED GOOD, OK FOR SERVICE.
Part: LIGHT — LOOSE (CABIN) · airframe 2,562 hrs · 1,698 cycles
THE EMER EXIT FLOOR PATH STRIP ARE LOOSE IN THE EMER EXIT 12B. SECURED EMER LIGHT PATH STRIP IAW AMM 33-51-11.