FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N7447U and the event date: up to this one’s cancellation.
Incident 19980710037229IClimb · Akron, CO(-5)Crew had a lower aft body overheat light come on during climb out of denver international airport. Crew performed the abnormal procedures but was unable to extinguish the light., but during the procedure noticed that the #2 engine oil temp was climbing…Incident 19921027049579IFinal Approach-IFR · Rochester, NYExperienced hydraulic fluctuations on lowering flaps. Landed safely. Replaced a leaking stabilizer power unit.Incident 19800830065969ITakeoff Ground Roll · Chicago, ILTakeoff warning horn sounded due to speed brake lever out of detent. Brake had not been properly positioned.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2001UALA00312Indicator · malfunctionedNR 3 FUEL FLOW INDICATOR ERRATIC FOLLOWED BY 28 VOLT DC CB POPPED THR0UGH 500 FEET . ELECTRICAL ODOR SMELL IN COCKPIT. FUEL FLOW WILL OPERATE OKAY BUT FUEL FLOW TRANSMITTER WILL REQUIRE REMOVAL FOR REPAIR DUE TO CHAFED WIRE BEHIND TRANSMITTER. SUPPLEMENTAL DSDR 2001UALA00310Stop · out of adjCREW REJECTED TAKEOFF AT 95 KNOTS DUE TO FORWARD DOOR LIGHT. SUPPLEMENTAL DATA UPDATE ADJUSTED DOOR STOPS AND CHECKED DOOR WARNING SYSTEM PER MAINTENANCE MANUAL. OPERATIONAL CHECK NORMAL.SDR 2000UALA00607Limit Switch · malfunctionedABORTED TAKEOFF AT APPROXIMATELY 80 KNOTS DUE TO FORWARD ENTRY DOOR WARNING LIGHT. *S/D* AIRCRAFT HISTORY INDICATED AMT CYCLED FWD ENTRY DOOR SEVERAL TIMES AND SWITCH CHECKED GOOD. AS PRECAUTIONARY MEASURE, EG2110 CALL OUT WAS INITIATED TO ACCOMPLISH THE FOSDR 99UAL900589Engine · failedSHUT DOWN NR 3 ENGINE DUE LOSS OF ENGINE OIL QUANTITY AND PRESSURE.SDR 99UAL900386Rib · crackedTWO CRACKED FASTENER HOLES AT BS 760, WL 200 AT WING LBBL 70.5 RIB UPPER CHORD VERTICAL FLANGE WERE FOUND. ONE FASTENER HOLE WAS TRIMMED OUT AND REPAIRED WITH A FILLER, WHILE THE OTHER HOLE WAS REPAIRED WITH A FREEZE PLUG. INSTALLATION OF LT 70.5 CHORD PREVESDR 99UAL900011Fuel Control · iced upABORTED TAKEOFF AT 100 KNOTS DUE TO NR 1 ENGINE SLOW TO SPOOL UP AND LACK OF DESIRED EGT. *S/D* THE AIRCRAFT WAS MOVED TO A HANGER AND THE NR 1 AND 3 COLD SOAKED ENGINES WERE HEATED TO MELT FROZEN MOISTURE IN THE PS4 TRAP OF THE FUEL CONTROL. THE NR 2 ENGINSDR 98UAL900318Duct · leakingLOWER AFT BODY OVERHEAT WARNING WITH AN ELECTRICAL ODOR IN CABIN AND COCKPIT. ALSO, NR 2 ENGINE OIL TEMP REDLINE, CABIN EXCESSIVE TEMP. INFLIGHT SHUT DOWN OF NR 2 ENGINE. TEMP AND ELECTRICAL ODOR SUBSIDED. DIVERTED TO AKO. *S/D* FOUND LEAKING FLEX TUBE TSDR 97UAL900767Ballast · shortedSMOKE SMELL IN FORWARD GALLEY AREA. SUSPECT COMING FROM FORWARD COFFEEMAKER. HALON FIRE EXTINGUISHER DISCHARGED. DIVERTED TO ABE. *S/D* GALLEY LIGHT BALLAST SHORTED. REPLACED BALLAST AND CHECKED FOR PROPER OPERATION.SDR 97UAL900426Light · inoperativeR2 DOOR LOWER FORWARD BLUE EMERGENCY EXIT LIGHT INOPERATIVE. *S/D* EXIT MARKER ON LOWER SIDEWALL DAMAGED. EXIT MARKER FORWARD OF DOOR 2R REPLACED. LIGHTING SYSTEM OPERATES NORMALLY.SDR 97UAL900379Lockbolt · looseDURING INITIAL INSPECTION OF THE SIDE ENGINE FORWARD ENGINE MOUNT SUPPORT FITTING REQUIRED BY SERVICE BULLETIN 727-54A0010, REVISION 4 (AD97-05-08) THREE LOCKBOLTS WERE FOUND LOOSE BOTH AT THE NR 1 AND NR 3 ENGINE POSITIONS. DISCREPANT FASTENERS WERE REPLACEDSDR 96UAL900326Skin · crackedAFT LOWER FUSELAGE LT OB OF VHF ANTENNA SKIN IS CRACKED AND EXFOLIATED. CRACK APPEARS TO BE ABOUT ONE AND ONE HALF INCHES LONG WITH EVIDENCE OF CORROSION. *S/D* CORROSION CONFIRMED, AFFECTED FUSELAGE SKIN REPAIRED PER SRM 53-30-3.