Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2004UALA00013Door Frame · damagedAFT PIT AFT DOOR FRAME DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00176Skin · damagedRIGHT LOWER FUSELAGE SKIN HAS EXCESSIVE MATERIAL LOSS 25 PERCENT, .036 ORIG . 027 AT DEEPEST AREA. STA 450 S25R AND STATION 435 4 IN BELOW LOWER AFT CORNER OF FORWARD CARGO DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHMENT. INSTALLED REPAIR DOUBLER AND FILLER.SDR 2003UALA00153Floorbeam · crackedCABIN FLOOR INTERCOSTAL UPPER FLANGE CRACKED AT FASTENER HOLES, STA 927-947 AT CENTERLINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE.SDR 2003UALA00149Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT WL 199 LBL 5.7. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00146Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT WL 199 RBL 5.7 MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00035Bearing · failedFLIGHT CREW DECLARED AN EMERGENCY WHEN CREW NOTICED ELECTRICAL SMELL IN THE CABIN DURING DESCENT. SUPPLEMENTAL DATA UPDATE THE RECIRCULATION FAN BEARING FAILED, WHICH CAUSED AN ELECTRICAL SMELL IN THE PASSENGER CABIN AND RESULTED IN CIRCUIT BREAKER C884 POPPINSDR 2003UALA00128Skin · dentedFASTENER INSTALLED AT STA 478 BETWEEN STRINGER 2R & STRINGER 3R IS INSTALLED IN A COCKED POSITION AND HAS DENTED SKIN. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.SDR 2001UALA00297Regulator · failedAIRCRAFT UNABLE TO PRESSURIZE. SUPPLEMENTAL DATA UPDATE THE NR 1 ENGINE HIGH STAGE REGULATOR FAILED. REPLACED NR 1 ENGINE HIGH STAGE REGULATOR.SDR 2001UALA00033Switch · out of adjAFT CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. *S/D* FOUND TARGET AND SWITCH SLIGHTLY OUT OF ALIGNMENT. ADJUSTED AND SECURED SWITCH ASSEMBLY AND CHECKED GAP. OPS CHECKED OK.SDR 99UAL900501Light · inopTHE EMERGENCY EGRESS LIGHTS FROM ROW 14 BACK ARE INOPERATIVE. REPLACED THE EMERGENCY EGRESS LIGHTS, OPERATIONS CHECK NORMAL.SDR 98UAL900321Controller · malfunctionedAUTO PRESSURIZATION FAILED AND CABIN ALTITUDE CLIMBED UNTIL CABIN ALTITUDE WARNING SOUNDED. *S/D* CABIN PRESSURE CONTROLLER SWITCHED TO STANDBY MODE AND AIRCRAFT REGAINED PRESSURIZATION CONTROL. THE CABIN PRESSURE CONTROLLER AND PRESSURE CONTROL PANEL WERE SDR 96UAL900951Pressure Syst · malfunctionedUNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD. *S/D* ACCOMPLISHED CHECK OF BOTH PACKS AND ENGINE PRESSURE BLEEDS. PRESSURIZED ACFT TO 6 PSID OFF ONE PACK. CHECKED OUTFLOW VALVE HEATER GASKET RESISTANCE. ALL SYSTEMS PERFORMED NORSDR 95UAL900257Eel Harness · inoperativeAFT CABIN EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED BATTERY AND INVERTERS, NO HELP. REPLACED HARNESS, CHECKS OK.
Other aircraft with N952UA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N952UA is registered now to the first aircraft listed.