N8924B
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.
56 reports on file, 2011-01-24 – 2017-07-21.
Part: BRACKET — BENT (NLG CENTERING) · airframe 26,834 hrs · 24,515 cycles
GEAR DISAGREE WARNING AFTER TO AT 2000 FT 48,000 LANDING WEIGHT ON GEAR RETRACTION MANUAL RLS NOT USED. 6 SECOND AFTER HANDLE NOSE LANDING GEAR . REMOVED AND REPLACED NLG CENTERING SENSOR BRACKETS. COMPLIED WITH LANDING GEAR RETRACTION AND EXTENTION FUNCTIONAL TEST IAW TASK 32-30-00-720-801. NO DEFECT NOTED AT THIS TIME.
Part: SELECTOR VALVE — INOPERATIVE (NLG) · airframe 26,791 hrs · 24,471 cycles
ON DEPARTURE NOSE WHEEL FAILED TO RETRACT BONDING LIKE IT WAS GETTING STUCK GEAR DISAGREE FOLLOWED BY NOSE WARNING MESSAGES NOSE LIGHT SHOWED IN TRANSIT THEN WENT RED. 6 SECONDS TO NOTICE. FOLLOWED QRH AND PULLED GEAR RELEASE HANDLE THAN RESTORED PER QRH WITH GEAR DOWN AND LOCKED. NOSE WHEEL STEERING OPERATED NORMALLY. INSPECTED NOSE LANDING GEAR AREA G.P.I. NO DEFECTS NOTED. DEF. LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-1 MAINT PRO C/W INTERED IN MM02 PLACARD INSTALLED MOC NOTIFIED 4488 /// PER MOTR GROUP SERVICED NOSE LANDING GEAR SHOCK STRUT IAW CRJ200 JOBCARD 12-710-002 PERFORM FUNCTIONAL TEST OF THE LG EXTENSION/RETRACTION SYSTEM TEST PASSED IAW AMM 32-30-00. REMOVED AND REPLACED NLG SELECTOR VALVE LEAK CHECK AND OPERATIONAL TEST GOOD IAW AMM 32-22-20 THIS CLEARS AM 3378090-1 PLACARD REMOVED, MM02 UPDATED MOC NOTIFIED 4488.
Part: RESERVOIR — INOPERATIVE (HYD SYSTEM) · airframe 26,740 hrs · 24,416 cycles
DURING TAKE OFF, THE LANDING GEAR TOOK ABOUT 15 SECONDS MORE THAN NORMAL TO INDICATE 3 UP ICONS ON ED1. COULD HEAR THE NOSE WHEEL SPINNING. TAPPED ON THE BRAKES THEN THE GEAR WARNING STOPPED AND THE 3 UP WHITE ICONS WERE ALL INDICATING. ACFT PUT ON JACKS FOR TROUBLESHOOTING. DISCREPENCY VERIFIED. REMOVED & REPLACED RUNAROUND BYPASS VALVE IAW AMM 32-32-20 NO FIX. REMOVED & REPLACED THE NR 3 HYD RESERVOIR IAW AMM 29-12-30. ALL OPS & LEAK CHECKED GOOD. GEAR RETRACT TIMES WITHIN LIMITS IAW AMM 32-30-00-720-801.
Part: STRUT — DISCHARGED (NLG) · airframe 26,735 hrs · 24,411 cycles
GEAR DISAGREE ON TAKEOFF. NOSE GEAR WAS EXTENDED QRH COMPLETED. DIVERTED BACK TO DEPARTURE. COMPLETED TS 001565A AND SERVICED STRUT IAW JC 12-70-003. OPS CHECKED GOOD.
Earlier reports · 2011–2016 · 52 reports
2016
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,866 hrs · 23,511 cycles
FLOOR EMERGENCY LIGHTS INOPERATIVE. OPS CHECKED GOOD IAW AMM 33-50-00. OK FOR SERVICE.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,734 hrs · 23,383 cycles
FLIGHT ATT. EMER. FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-61-00. FLASHLIGHT WORKS NORMALLY. P/N ON/OFF P4-01-0021.
Part: OXYGEN BOTTLE — DISCHARGED (CABIN) · airframe 25,516 hrs · 23,163 cycles
PORTABLE OXYGEN BOTTLE DISCHARGED. R & R POTABLE OXYGEN BOTTLE IAW AMM 35-31-01.
Part: MICROPHONE — INOPERATIVE (OXYGEN MASK) · airframe 25,459 hrs · 23,106 cycles
CAPTAIN`S OXYGEN MASK MICROPHONE INOPERATIVE. FOUND CAPTAINS OXYGEN MASK BOX UNDERSIDE AUDIO CONNECTOR TO BE DISCONNECTED. RECONNECTED AUDIO CONNECTOR AND PERFORMED OPS TEST IAW TASK 23-51-00-710-801. OPS TESTED GOOD
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,069 hrs · 22,721 cycles
FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY P52LF IAW AMM 33-51-04, OPS CHECKED GOOD.
Part: HOSE — SEPARATED (COCKPIT) · airframe 24,719 hrs · 22,350 cycles
CAPTAINS O2 MASK HOSE CONNECTION TO MASK APPEARS SEPARATED. R & R CAPTAINS 02 MASK IAW AMM 35-11-12. OPERATIONS TEST OF THE MASK & MICROPHONE GOOD IAW AMM 35-10-00 & 23-51-00.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 24,675 hrs · 22,302 cycles
ONE INFANT LIFE VEST HAS HOLE IN BAG. R & R ONE INFANT LIFE VEST IAW PA 25-09-6A.
2015
Part: COVER — CRACKED (CABIN) · airframe 24,004 hrs · 21,644 cycles
FLOOR TRACK EMER LIGHT, TRACK COVER CRACKED SEVERAL LOCATIONS. R & R FLOOR TRACK EMER LT TRACK COVER IAW AMM 33-51-01-400-801 STEP 3 A 6 & 7.
Part: STRINGER CLIP — CRACKED (BS 625) · airframe 24,004 hrs · 21,644 cycles
STRINGER CLIP 14L AND FS 625 IS CRACKED.
Part: STRINGER CLIP — CRACKED (BS 325) · airframe 24,004 hrs · 21,644 cycles
CLIP AT STRINGER 15L AND FS 325 IS CRACKED.
Part: STRINGER CLIP — CRACKED (BS 625) · airframe 24,004 hrs · 21,644 cycles
STRINGER CLIP 16L AND FS 625 IS CRACKED.
Part: ANGLE — CRACKED (BS 621) · airframe 24,004 hrs · 21,644 cycles
CLIP ON APB AT FS 621 FOR UPPER CARGO NET SUPPORT BEAM IS CRACKED.
Part: FLOORBEAM — CORRODED (BS 280)
THE BEAM WEB AT FS 280 FOUND TO BE EXFOLIATED FROM RBL9 TO LBL9. CORROSION HAD A 100 PERCENT MATERIAL LOSS.
Part: DOOR — OUT OF RIG (CABIN) · airframe 23,824 hrs · 21,472 cycles
MAIN CABIN DOOR DOES NOT OPEN PROPERLY, REQUIRES ABNORMAL EFFORT TO PUSH OPEN AFTER LOCKING HANDLE RELEASED. COMPLETED RE-RIG OF PAX DOOR IAW 52-11-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,746 hrs · 21,399 cycles
FLOOR EMER FLOODLIGHT AT FWD BULKHEAD INOPERATIVE. REMOVED & INSTALLED SERVICEABLE FLOODLIGHT ASSEMBLY IAW AMM 33-51-19. OPERATIONS CHECKED GOOD.
Part: ROLLER — FAILED (PAX DOOR) · airframe 23,722 hrs · 21,370 cycles
FOUND PAX DOOR WILL NOT OPEN AFTER HANDLE IS PULLED. R & R FWD & AFT PAX DOOR FRAME ROLLERS IAW ENGINEERING DWG 600-31469.
Part: HOOK — MISSING (ESCAPE ROPE) · airframe 23,641 hrs · 21,284 cycles
CAPTAINS SIDE EMERGENCY EXIT, OVERWING, MISSING ROPE CLAMP. REPLACED MISSING CARABINEER HOOK ASSEMBLY, ATTACHED TO OVERWING EXIT DOOR SAFETY LINE ON LEFT OVERWING EXIT IAW AMM 25-63-04. OK FOR SERVICE.
Part: SPRING — DAMAGED (PAX DOOR) · airframe 23,637 hrs · 21,280 cycles
MAIN CABIN DOOR STICKING AFTER FLIGHT WHILE TRYING TO OPEN. HAVE TO PUSH MUCH HARDER THAN NORMAL TO OPEN. COMPLETED RIG CHECK OF PAX DOOR IAW AMM 52-11-25. REPLACED BOTH PAX DOOR COUNTERBALANCE GAS SPRINGS IAW AMM 52-11-17. COMPLIED WITH OPERATIONAL TEST OF PAX DOOR IAW AMM 52-11-00. SEE NRCC FOR WORK PERFORMED.
Part: DOOR SEAL — DEFECTIVE (PAX DOOR) · airframe 23,593 hrs · 21,233 cycles
MAIN DOOR WILL NOT OPEN FROM INSIDE. HANDLE OPEN, PAX DOOR HANDLE MSG, BUT DOOR UNABLE TO OPEN. R & R PAX DOOR SEAL IAW AMM 52-11-10. PERFORMED PRESSURIZATION CHECK OF CABIN DOOR SEAL IAW AMM 21-31-00. OPERATIONS TESTED GOOD. OK FOR SERVICE.
Part: CABLE — BROKEN (PAX DOOR) · airframe 23,522 hrs · 21,152 cycles
FLIGHT ATTENDANT REPORTS PAX DOOR DIFFICULT TO CLOSE & OPEN. HANDLE BINDS ABOUT MID TRAVEL. FOUND ICE BREAK CABLE BROKEN. R & R ICE BREAK CABLE IAW AMM 52-11-15. ALL CHECKS ARE GOOD AT THIS TIME.
Part: CAM — CONTAMINATED (PAX DOOR) · airframe 23,448 hrs · 21,062 cycles
FLIGHT & FIRST OFFICER WERE UNABLE TO OPEN THE PAX DOOR WHEN ARRIVING AT GATE. CLEANED EXCESSIVE GREASE FROM LATCH CAMS. PERFORMED OPERATIONAL TEST OF PAX DOOR, NO DEFECTS NOTED.
Part: RELAY — FAULTY (CABIN) · airframe 23,295 hrs · 20,889 cycles
WHEN EMER LIGHTS ARE ARMED THEY TURN ON IN THE MAIN CABIN. R & R VOLTAGE SENSOR RELAY K1XD. PERFORMED OPERATIONS CHECK IAW AMM CH 24-51-27. OPERATIONS CHECKED GOOD. NO NEW FAULTS NOTED. SEE NRWC N73428 & SEE CONTINUATION CARDS 68314, 70801 & 68315 FOR DETAILS.
2014
Part: COVER — DAMAGED (EMERGENCY LIGHT) · airframe 22,941 hrs · 20,520 cycles
CREW REPORTED FWD MOST EMER FLOOR TRACK LIGHTING COVER DAMAGED AND LOOSE. R & R DAMAGED SECTION OF EMERGENCY FLOOR TRACK LIGHT COVER IAW AMM 33-51-01. OK FOR SERVICE.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 22,777 hrs · 20,367 cycles
DURING INSPECTION FOUND A DENT ON THE LT FUSELAGE TO BE OUT OF LIMITS MEASURING 6.75 INCHES X 1.60 INCHES X .025 INCHES DEEP. REPAIRED IAW EA CRJ253-03099.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,094 hrs · 19,659 cycles
ONE INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA 25-096A.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,094 hrs · 19,659 cycles
ONE INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA 25-096A.
Part: STRUT — LOW (NLG) · airframe 21,870 hrs · 19,441 cycles
AIRCRAFT 8924B TOOK OFF FROM IND & PUT GEAR HANDLE TO THE UP POSITION & INSTANTLY RECEIVED A GEAR DISAGREE MSG. FOLLOWED QRH & DID NOT DECLARE AN EMERGENCY. ACFT RETURNED SAFELY TO IND, WHERE A GEAR DOWN MEL WAS APPLIED & THEN ROUTED TO CVG FOR REPAIR. GEAR DISAGREE AFTER TAKEOFF. LDW 39000 LBS, RATE OF DESCEND 300 FEET A MIN. COMPLIED WITH PA 05-018K SCENARIO 1. SERVICED NOSE STRUT ASSEMBLY IAW AMM 12-12-32. REPLACED OLEO CENTERING & EXTENSION BRACKET IAW AMM 32-30-00, NO DEFECTS NOTED AT THIS TIME. THIS CLEARS DM 4862.
Part: COVER — BROKEN (EXIT SIGN) · airframe 21,651 hrs · 19,213 cycles
YELLOW BULB COVER ON OVERHEAD EMERGENCY EXIT SIGN BROKEN. REPLACED BULB COVER IAW AMM 33-51-14.
Part: COVER — BROKEN (CABIN) · airframe 21,605 hrs · 19,168 cycles
YELLOW BULB COVER ON EMERGENCY EXIT SIGN BROKEN. REPLACED BULB COVER IAW AMM 33-51-14.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,454 hrs · 19,011 cycles
FIRST OFFICER'S EMERGENCY FLASHLIGHT STRAP BROKEN. FOUND BATTERY DEAD R & R FLASHLIGHT BATTERY & STRAP IAW CRJ200 AMM 25-61-02. OPERATIONS CHECKED GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,449 hrs · 19,004 cycles
CAPTAIN`S SIDE FLASHLIGHT BATTERY DEAD. R & R FLASHLIGHT BATTERY IAW CRJ200 AMM 25-61-02.
Part: DOOR — INOPERATIVE (CABIN) · airframe 21,424 hrs · 18,980 cycles
PASSENGER DOOR INOPERATIVE.
2013
Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 20,780 hrs · 18,347 cycles
RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-21.
Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 20,641 hrs · 18,213 cycles
EXPERIENCED UNCOMMANDED YAW INPUTS IN CRUISE FLIGHT, AUTO PILOT AND YAW DAMPER ENGAGED. THE YAW DAMPER WAS DISENGAGED TO RELIEVE THE YAW INPUT WHICH WAS A RT RUDDER INPUT. R & R RT LINEAR ACTUATOR IAW AMM 22-22-01 AND RIL 3274. OPS CHECK GOOD IAW AMM 22-22-01-710-802. OK FOR SERVICE.
Part: CONTAINER — TORN (LIFE VEST) · airframe 20,569 hrs · 18,136 cycles
ONE INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED LIFE VEST IAW PA25-096A.
Part: PBE — UNSERVICEABLE (COCKPIT) · airframe 20,206 hrs · 17,778 cycles
CREW REPORTED COCKPIT PBE NOT SERVICEABLE. R & R COCKPIT PBE WITH SERVICEABLE PBE IAW AMM 35-30-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,076 hrs · 17,654 cycles
FLIGHT ATTENDANT OVERHEAD PANEL EMERGENCY CALL LIGHT WILL NOT ILLUMINATE.
Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 19,777 hrs · 17,361 cycles
CAPTAINS LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 19,777 hrs · 17,361 cycles
1 EACH INFANT LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED INFANT LIFE VEST IAW AMM 25-61-03.
Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 19,472 hrs · 17,066 cycles
INFANT LIFE VEST TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW AMM 25-61-03.
2012
Part: HOOK AND LOOP — MISSING (CABIN) · airframe 19,355 hrs · 16,959 cycles
RED STRAP MISSING ON LEFT PANEL AT EMERGENCY ROW. RED STRAP NOT MISSING, FOUND RED STRAP FOR EMERGENCY PANEL NEEDED VELCRO. APPLIED NEW VELCRO IAW CRJ 200 SRM 51-22-76.
Part: LIGHT — INOPERATIVE (CALL) · airframe 18,472 hrs · 16,083 cycles
CENTER OVERHEAD EMERGENCY CALL LIGHT WILL NOT ILLUMINATE. ADJUSTED CALL LIGHT ASSY AS REQUIRED. OPS CHECKS GOOD IAW 33-51-00.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,244 hrs · 15,860 cycles
LEFT SEAT RAIL TRACK NR 1 CORRODED AND WORN. REPAIRED IAW AMM 53-01-11.
Part: SEAT TRACK — CHAFED (FUSELAGE) · airframe 18,244 hrs · 15,860 cycles
LEFT SEAT TRACK NR 6 CHAFED. REPAIRED IAW AMM 53-01-11.
Part: SEAT TRACK — GOUGED (BS 364-409) · corrosion level 2 · airframe 18,244 hrs · 15,860 cycles
RIGHT SEAT TRACK NR 2, GOUGED FROM FS 364 TO FS 409. REPAIRED IAW AMM 53-01-11.
Part: SEAT TRACK — GOUGED (BS 409) · airframe 18,244 hrs · 15,860 cycles
RIGHT SEAT TRACK GOUGED FROM FS 409 TO 409+112. REPAIRED IAW AMM 53-01-11.
Part: SEAT TRACK — CHAFED (BS 369-409) · corrosion level 2 · airframe 18,244 hrs · 15,820 cycles
LEFT NR 2 SEAT TRACK CHAFED BETWEEN FS 369 AND FS 409. REPAIRED IAW AMM 53-01-11.
Part: SEAT TRACK — GOUGED (BS 409) · airframe 18,244 hrs · 15,860 cycles
LEFT SEAT TRACK NR 3, GOUGED FROM FS 409 TO FS 409+112. REPAIRED IAW AMM 53-01-11.
Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 18,108 hrs · 15,722 cycles
AIR RETURN FOR BIRD STRIKE IN RT ENGINE, OVERWEIGHT LANDING BUT NOT A HARD LANDING. 200 FPM TOUCHDOWN. BIRD STRIKE INSPECTION CHECKLIST COMPLETED. SEE DISCREPANCY NR 2 PG 2189314 FOR RT ENGINE DAMAGE, SEE DIESCREPANCY NR 1 PG 2189315 FOR OVERWEIGHT LANDING.
2011
Part: RETAINING NUT — LOOSE (YOKE) · airframe 17,513 hrs · 15,173 cycles
CO-PILOT YOKE IS BINDING & MAKING A THUMPING NOISE THAT CAN ALSO BE FELT THROUGH THE FLIGHT DECK FLOOR DURING AILERON CHECK. RE-TORQUED RETAINING NUTS, REPAIRED BACKLASH, REPAIRED BINDING CONDITION, ELIMINATED SNAPPING AND CLICKING NOISE IN THE AILERON CONTROL WHEEL IAW PA 27-066D.
Part: UNKNOWN — SMOKE (CABIN) · airframe 15,919 hrs · 13,615 cycles
ON APPROACH CREW REPORTED SMOKE IN CABIN EMERGENCY DECLARED. MAINTENANCE PERFORMED OPS CHECK IAW AMM 72-40-00, NO DEFECTS NOTED.
Part: SUPPORT — CRACKED (GPU RECEPTICAL) · airframe 15,796 hrs · 13,501 cycles
THE GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE SUPPORT MEMBER, P/N 600-33283-33, WAS FOUND DAMAGED. THE DAMAGE CONSISTS OF THE THREE CRACKS TO THE POWER RECEPTACLE SUPPORT MEMBER 2 FROM THE UPPER AFT FASTENER AND 1 FROM THE LOWER AFT FASTENER.