Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WRN2008F00001Connector · dirtyAFTER TAKEOFF, APPROX 40 MINUTES INTO FLIGHT, AC TURNED BACK DUE TO NAV PROBLEMS WITH GPS SYSTEM. GPS SYS NR 2 PREVIOUSLY MEL, NR 1 GPS SYS WENT TO DR MODE. AIRCRAFT RETURNED TO BASE, NORMAL LANDING ACCOMPLISHED. MX CLEANED AND RESET CONNECTION ON GPS ANTENSDR WRNA200800006Engine · failedAFTER TAKEOFF FROM MFM, CLIMBING THROUGH 15,000 FEET A LOUD EXPLOSION WAS HEARD FROM NR 1 ENGINE FOLLOWED BY SEVERE VIBRATION, ENGINE WAS RETARDED TO IDLE POWER, VIBRATION CONTINUED FOLLOWED BY LOW OIL PRESS LIGHT AND EGT INCREASE TO 963 DEGREES C. ENGINE WASSDR WRNA200700047Friction Brake · out of limitsAFTER TAKEOFF FROM IND, THE SLATS FAILED TO RETRACT. DUMPED 22,000 POUNDS OF FUEL. DIVERTED TO GSO AND MADE A SAFE LANDING. FOUND RT FRICTION BRAKE OUT OF TORQUE LIMITS, REPLACED FRICTION BRAKE IAW 27-81-47 PG401. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASEDSDR WRNA200700046Jackscrew · lockedSLATS FAILED TO RETRACT AFTER TAKEOFF. DUMPED FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. FOUND NR 4 AND 5 SLAT JACK SCREWS LOCKED OUT AND RT FRICTION BRAKE FAILED TORQUE CHECK. REPLACED NR 4 JACK SCREW IAW 27-81-27 PG 401, NR 5 SLAT JACK SCREW IAW 27-81SDR WRNA200700040Slat · malfunctionedON APPROACH TO IND, L/E SLATS FAILED TO EXTEND WITH ASYMMETRY, CONTINUED ON APPROACH AND MADE A SAFE LANDING. VISUALLY INSPECTED SLATS TORQUE TUBES AND TRANSMISSIONS FOR A DISCONNECT, NO DEFECTS. INSPECTED FOR DEFECTS IAW MM 27-83-00 PG 605, NO DEFECTS NOTEDSDR WRNA200700029Shaft · jammedAFTER LEAVING BLOCKS, SLATS WOULD NOT EXTEND, JAMMED, VIBRATION FELT IN AIRCRAFT. RETURNED TO BLOCKS. REPLACED SLAT TRANSMISSION SHAFT ASSEMBLY AND SHOCK ABSORBER PER MM 27-81-12 PG 401 AND 27-81-29 PG 401. AIRCRAFT RELEASED FOR SERVICE.SDR WRNA200600040Line · crackedRIGHT MAIN GEAR DID NOT RETRACT, GREEN SYSTEM LEVEL LOW LIGHT ON. PERFORMED MANUAL GEAR EXTENSION BY ABNORMAL CHECKLIST, RETURNED TO FIELD AND MADE A SAFE LANDING. FOUND GREEN HYDRAULIC SUPPLY LINE TO ACTUATING CYLINDER CRACKED. INSTALLED TEMPORARY FLEX LINSDR WRNA200600010Slat System · malfunctionedAFTER TAKEOFF, SLATS FAILED TO RETRACT. JETTISONED FUEL TO SAFE LANDING WEIGHT, RETURNED TO FIELD AND MADE A SAFE LANDING. PERFORMED FRICTION BRAKE INSPECTION/CHECK IAW A300 AMM 27-81-47 PG 601. TORQUE IS UNDER 27 FOOT POUNDS, WITHIN LIMITS. SLAT/FLAP OPS SDR WRNA200500019Line · leakingLOST GREEN HYD FLUID DURING GEAR RETRACTION. FOUND LT MAIN GEAR DOOR ACTUATOR LINE FAILED. REPLACED WITH TEMPORARY LINE IAW MM 20-23-11. SERVICED HYD'S IAW 12-12-29 OPS CK AND LEAK CK SATISFACTORY. ITEM PLACED ON CI, DMI NR 1927, TO BE REPLACED BY 9-17-05 SDR WRNA200500014Slat · malfunctionedAFTER TAKEOFF SLATS WOULD NOT RETRACT. AIRCRAFT RETURNED TO AIRFIELD. LANDING NORMAL. MAINTENANCE OPS CHECKED SLAT SYSTEM ON GROUND, COULD NOT DUPLICATE, OP'S CHECKED SATISFACTORY IAW MM 27-81-00. AIRCRAFT RETURNED TO SERVICE.SDR WRNA200400014Dampener · inoperativeAFTER TAKE OFF UNABLE TO MOVE GEAR HANDLE TO UP POSITION. FOLLOWED ABNORMAL PROCEDURES. AIRCRAFT LANDED NORMAL. REMOVED AND REPLACED RT PITCH DAMPENER IAW 32-11-15. AIRCRAFT JACKED AND GEAR SWING COMPLIED WITH OP'S CHECK GOOD IAW 7-11-00. AIRCRAFT RETURNSDR WRNA200400009Smoke Detector · unserviceableDURING TAKEOFF ROLL FLIGHT DECK SMOKE LIGHT ILLUMINATED ON F/E PANEL ALONG WITH SMOKE LIGHT ON MWP AND CONTINUOUS CHIME. TAKEOFF WAS REJECTED AT 105KTS AND AIRCRAFT RETURNED TO GATE. FOUND E&E SMOKE DETECTOR SATURATED WITH WATER. INVESTIGATION REVEALED THAT SDR WRNA200400007Sequence Valve · misalignedNOSE GEAR DID NOT RETRACT AFTER T/O RETURN TO AIRPORT. INSTALLED RIG PIN ON SEQUENCE VALVE AND RIGGED TO ZERO POSITION FOR REMOVED NLG DOOR. DOOR DEACTIVATED IAW CDL. FUNCTIONAL CHECK PERFORMED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE.SDR WRNA200300004Aileron · delaminatedOn walk around found R/H I/B aileron to have damage. This damage is on the top trailing edge where a section of skin is peeling aft (approx. 4' width and 8" in length) exposing honeycomb.Corrective Action: Removed and replaced right wing in-board all speed ailSDR WRNA200100019Adc · failed#1 AIR DATA COMPUTER FAILED ON TAKE OFF. WITH FULL THROTTLES AIR SPEED KEPT DECREASING- A/C SHOOK VIOLENTLY- NO STICK SHAKER OR CLACKER.CORRECTIVE ACTION: R&R'D #1 ADC COMPUTER OPS CK'D GOOD PER MM 34-12-34. PERFORMED EXCESSIVE TURBULANCE INPECTION I/A/W MM 5-
Other aircraft with N505TA · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N505TA is registered now to the first aircraft listed.