Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR MYW2004F00006Generator · fluctuatesDURING TAKE OFF ROLL, GENERATOR DROPPED OFF LINE FOLLOWED BY NR 3 GEN LIGHT. REJECTED TAKE OFF AT 75 KNOTS. ACCOMPLISHED AOM PROCEDURE GENERATOR CHECKLIST ZA9-1 AND REJECTED TAKEOFF. RETURNED TO GATE WITHOUT INCIDENT. FOUND NR 3 GENERATOR FREQUENCY FLUCTUASDR 2004F00272Panel · missingDURING POST FLIGHT WALKAROUND AT PIT FORND PRESSURE RELIEF VENT PANEL MISSING FROM NR 3 ENGINE. INSPECTED NR 3 ENGINE IAW 71-10-11. PERFORMED HIGH POEWR ENGINE RUN UP. BLEED PRESSURE EQUAL ON BOTH SIDES PER MM 75-31-0. RETURNED TO AIRCRAFT TO SERVICE. (M)SDR 2004F00287Line · leakingON CLIMB-OUT FROM MEM, NR 2 ENGINE OIL PRESSURE DROPPED TO 12 PSI. FOLLOWED AOM ABNORMAL PROCEDURES 2-A-19-10. SHUT DOWN NR 2 ENGINE AND RETURNED TO MEM. TROUBLESHOT NR 2 ENGINE. DISCOVERED OIL LINE BETWEEN FUEL OIL COOLER AND GEAR BOX CHAFING WITH OIL PRESDR 2004F00239Line · leakingWHILE IN CRUISE FLIGHT FROM SUX SYSTEM 'A' HYD SHOWED A SLOW FLUID LOSS. ACCOMPLISHED ABNORMAL PROCEDURES THEN DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. FLUID QTY AND LANDING 2 GALLONS. FOND NR 1 ENGINE CASE DRAIN LINE IN SECITON 48 LEAKING. INSTALLED TSDR SDR020040Shaft · shearedDURING CLIMB OUT, THROUGH 1000 FT ALT ENGINE NR 1 FLAMED OUT. (FUEL FLOW AND EPR WENT TO ZERO. DURING TAKEOFF ALL ENGINE INDICATIONS WERE NORMAL. C/W AOM PROCEDURES AND RETURNED TO AIRPORT. REMOVED AND REPLACED FUEL CONTROL UNIT AND FUEL PUMP FUEL PUMP UNISDR AW32002F00000Bulb · burned outDURING POST FLIGHT, FOUND LT WING CENTER EMERGENCY LIGHT INOPERATIVE. RELAMPED LT OVERWING EMERGENCY LIGHT. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR 2002F00798Sign · inoperativeFOUND EXIT SIGN OVER R-1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER R-1 DOOR AND OPS CHECKED. SATISFACTORY AS PER MM 33-50-71. AIRCRAFT RETURNED TO SERVICE. (M)SDR 2002F00230Light · disconnectedEPL TRACK LIGHT INOPERATIVE, ROW 21 ABC. ORANGE LIGHTS. RECONNECTED STRIP AND OPS CHECK AS PER MM 33-50-00. AIRCRAFT RETURN TO SERVICE. (M)SDR 2002F00229Power Supply · dischargedEXIT SIGN ON BOTH RIGHT OVERWING DOORS INOPERATIVE. REPLACED POWER PACK AND OPS CHECKED AS PER MM 33-50-00. RETURNED AIRCRAFT TO SERVICE. (M)SDR 2002F00228Power Supply · dischargedEXIT SIGN ABOVE 31 C-D INOPERATIVE. REPLACED POWER PACK AND OPS CHECK AS PER MM 33-50-00. AIRCRAFT RETURN TO SERVICE. (M)SDR 2001F00155Switch · shortedDURING TAKEOFF ROLL WHEN THRUST LEVER ADVANCED TAKEOFF WARNING HORN SOUNDED. AIRCRAFT TAKEOFF CONFIGURATION CHECK, HORN COULD NOT BE SILENCED. ABORTED TAKEOFF. TROUBLESHOT SYSTEM FOUND STABILIZER UPPER LIMIT TAKEOFF WARNING SWITCH INOPERATIVE. REMOVED AND SDR 2001F00153Pump · failedSHORTLY AFTER GEAR RETRACTION LOST HYD SYSTEM 'A'. ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO DFW. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYD PUMP. RUN AND LEAK CHECK. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HYD FILTER, RUN OPS AND LEAK CHECSDR 2001F00135Pump · damagedSHORTLY AFTER GEAR RETRACTION LOST HYD SYSTEM 'A'. ACCOMPLISHED ABNORMAL PROCEDURE. RETURNED TO DFW. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMP. RUN AND AND LEAK CHECK. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HYDRAULIC FILTER, RUN O
Other aircraft with N802MA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N802MA is registered now to the first aircraft listed.