FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N951UA and the event date: up to this one’s cancellation.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2003UALA00543O-Ring · leakingUPON ARRIVAL FOUND BOTTLE PRESSURE ON SLIDE AT DOOR 1R BELOW THE GREEN BAND. LEAKING O-RING BETWEEN RESERVOIR AND VALVE/REGULATOR CAUSED REDUCED BOTTLE PRESSURE. REPLACED SLIDE BOTTLE, INSPECTED/TESTED REMOVED BOTTLE TO DETERMINE CAUSE, THEN OVERHAULED VALVSDR 2003UALA00065Pressure Panel · crackedNOSE LANDING GEAR WHEEL WELL UPPER WEB AND UPPER AFT CHORD ANGLE PUNCTURED AND CRACKED, RBL 24 STA 294. MAJOR REPAIR ACCOMPLISHED. REPLACED CHORD ANGLE. WEB REPAIRED BY INSTALLING DOUBLER.SDR 2003UALA00059Frame · crackedSTATION 178, WL 207, CHORD CRACKED. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00055Frame · crackedFORWARD NOSE STATION 188, OUTBOARD FRAME CHORD CRACKED JUST ABOVE STRINGER 17R, 1IN BELOW WEB. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED WEB ANGLE REPAIR.SDR 2003UALA00054Frame · crackedFORWARD NOSE STATION 188 LEFT FRAME OUTBOARD CHORD CRACKED IN RADIUS BELOW STRINGER 17 WEB. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED WEB ANGLE REPAIR.SDR 2003UALA00031Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT RIGHT LOWER RADAR MOUNT INBOARD UPPER SIDE. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00030Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT RBL 1 IN WL 188. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00003Frame · dentedAFT PIT FRAME AT STATION 727B STRINGER 22L, UPPER CAP DENTED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.SDR 2001UALA01061Battery · weakEEL LIGHTING VERY DIM. ROW 3-10 AND 15-AFT. REPLACED BATTERY PACKS AND AFT CABIN POWER INVERTER.SDR 2001UALA00859Skin · damagedFWD CARGO DOOR SKIN DAMAGED. INSTALLED DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00002Indicator · failedFLAP ASYMMETRY INDICATION. *S/D* REPLACED FLAP INDICATOR. OPS CHECKED NORMAL.SDR 97UAL900599Computer · failedDUE TO A STALL WARNING INDICATION, TAKEOFF WAS ABORTED AT AN ESTIMATED SPEED OF 108 TO 110 KNOTS. *S/D* CHECKS WERE PERFORMED ON THE ANGLE OF ATTACK SENSORS, STALL WARNING COMPUTERS, AND STICK SHAKERS ON BOTH SYSTEMS. EVERYTHING CHECKED NORMAL. THE STALL WSDR 97UAL900057Prox Sensor · defectiveAT FLAP NR 3, FLAP AMBER LIGHT ILLUMINATED ON OVERHEAD PANEL AND FORWARD PANEL FLAP TRANSIT LIGHT ILLUMINATED. *S/D* A DEFECTIVE EXTEND PROXIMITY SENSOR ON THE NUMBER 3 SLAT WAS DETERMINED TO BE THE CAUSE OF THE DISCREPANCY. THE PROXIMITY SENSOR WAS REPLACESDR 97UAL900034Transit Light · illuminatedWHEN FLAPS 1 WAS SELECTED, LEADING EDGE FLAPS TRANSIT LIGHT STAYED ON AND THE LEADING EDGE NR 3 ANNUNCIATOR OVERHEAD LIGHT STAYED LIT. *S/D* CONTINUED DISCREPANCY. SEE MRR REPORT NR 97UAL900057 FOR RESPONSE.SDR 96UAL900843Bearing · failureCREW REPORTED NUMBER ONE ENGINE INFLIGHT SHUT DOWN DUE TO LOW OIL PRESSURE. ENGINE STARTED TO CHUG AND VIBRATE. ENGINE WAS SPOOLED DOWN, WOULDN'T RESPOND TO THROTTLE. SHUT DOWN ENGINE, OIL PRESSURE WAS 3 TO 5 POUNDS PER SQUARE INCH WINDMILLING. *S/D* ENGI
Other aircraft with N951UA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N951UA now.