Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR RU3A20141203044Warning System · false activationPRESSURE SYS & EMERGENCY PRESSURE LIGHT ILLUMINATED. PERFORMED ENGINE RUN OPERATION TO FUNCTIONALLY CHECKED CABIN PRESSURE SYS & ENGINE BLEED AIR MIXING VALVES. NO FAULT FOUND OPS CHECKED GOOD.SDR RU3A20140715025Unknown · odorSTRONG & NOXIOUS ODOR NOT BELIEVED TO BE ELEC IN NATURE OCCURRED DURING DESCENT. IT WAS INTERMITTENT, LASTING FOR 15 MIN, STOPPING, THEN RETURNING.SDR RU3A20140603020Controller · out of adjustRIGHT GEN FAILED IN CRUISE FLIGHT AT 11,000'. RESET GEN & IT OPERATED NORMALLY FOR ABOUT 7 MINS & IT FAILED AGAIN. RESET GEN A SECOND TIME & REMAINED ON LINE FOR REMAINDER OF FLIGHT. ADJUSTED LT & RT GEN CONTROL. CLEANED & TORQUED GEN TERMINAL LEADS. OPERASDR RU3A20140516018Unknown · malfunctionedPRESSURIZATION SYS MODE FAULT LIGHT, RISING CABIN ALTITUDE IN CLIMB TO FL340, EMERGENCY PRESS DESCENDED TO FL240, SYS RECOVERED BUT FAULT REMAINED. COMPLETE PRESS LOSS DESCENDING THROUGH 5,000'.SDR RU3A20140410016Attach Fitting · brokenLEFT GEAR DOOR, LEFT MAIN OTBD GEAR DOOR LINK ATTACHMENT BROKEN. LOUD NOISE HEARD DURING GEAR RETRACTION AFTER TAKEOFF.SDR RU3A0908Computer · failedUPON GEAR EXTENSION DURING FINAL APPROACH, PILOT NOT FLYING NOTICED NOSE WHEEL STEERING FAILED TO ARM. CREW VERIFIED ANNUNCIATOR WAS OPERATIONAL AND VISUALLY VERIFIED THAT NOSE WHEEL STEERING CB'S HAD NOT POPPED. CREW FOLLOWED PROCEDURES FOR NOSE WHEEL STEERSDR RU3A0609Steering Sys · deactivatedLANDED RWY 27, AFTER DECELERATING TO TAXI SPEED, NOSE STEERING DISCONNECTED AND AURAL WARNING SOUNDED. AIRCRAFT WAS STOPPED ON TAXIWAY. SYSTEM WOULD NOT REMAIN ARMED AND AIRCRAFT COULD NOT BE CONTROLLED WITH DIFFERENTIAL POWER AND BRAKING. ATC WAS NOTIFIED SDR RU3A0415Hydraulic System · malfunctionedWHILE LOWERING GEAR BOTH HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED. THE PRESSURE FLUCTUATED TO THE TOP OF THE YELLOW ARC, THEN CAME BACK TO NORMAL AND BOTH HYDRAULIC PRESS LOW LIGHTS WENT OUT. RAISED THE GEAR AND BOTH HYDRAULIC PRESSURE LIGHT CAME ON AND THESDR 2004F00153Electrical Sys · failedTOTAL AIRCRAFT ELECTRICAL FAILURE IN FLIGHT. PILOT DECLARED IN FLIGHT EMEGENCY AND LANDED AIRCRAFT ON DIMINISHING DC POWER. (M)SDR RU3A98004Skin · lightning strikeGJT - N4 ON ILS WAS HIT BY LIGHTNING ON 5-6-98. POST-FLIGHT INSPECTION WAS CONDUCTED BY THE MAINTENANCE FACILITY AT GJT AND A SPECIAL FLIGHT PERMIT WAS ISSUED 5-12-98 FROM GJT TO OKC. THE AIRCRAFT WAS INSPECTED AND REPAIRED IAW THE AFTER LIGHTNING STRIKE INSSDR RU3A98001Skin · lightning strikeGJT - ON ILS WAS HIT BY LIGHTING. POST FLIGHT REVEALED .125 TO .166 INCH HOLES IN FUSELAGE AFT OF RADOME BELOW FLOOR DECL LEVEL. NO EVIDENCE OF HOLES IN PRESSURE VESSLE. RIGHT ENGINE SUSTAINED EVIDENCE OF ARCING ON ENGINE MOUNT, AND FAN BLADES. (M)SDR RU3A97004Duct · leakingIN-FLIGHT, THE RIGHT DC BUSS 1 CIRCUIT BREAKER TRIPPED. THIRTY SECONDS LATER, THE LEFT DC BUSS 1 CIRCUIT BREAKER TRIPPED RESULTING IN A TOTAL LOSS OF A/C POWER. THE PROBLEM IS BELIEVED TO BE DUE TO THE GCU OVERLOAD SENSORS BECOMING TOO HOT. THIS WAS CAUSED SDR RU3A97002Air Distribution · odorPANEL TECHNICIAN REPORTS STRONG ODOR OF EXHAUST FUMES IN CABIN WHICH CAUSE EYES TO BURN. INCIDENT IS UNDER INVESTIGATION AT THIS TIME. SECOND OCCURRENCE: REFERENCE SDR NR RU3A-97-001. THE AIR CYCLE MACHINE AND ASSOCIATED PLUMBING WERE REMOVED AND INSPECTEDSDR RU3A97001Air Distribution · odorPILOTS REPORT CABIN GETS FUMES WHEN TEMPERATURE IS INCREASED ABOVE 70 DEGREES FAHRENHEIT AT ALTITUDE. THE FUMES ARE MORE NOTICEABLE WITH HIGH POWER SETTINGS IN CLIMB AND GO-AROUND. INCIDENT IS UNDER INVESTIGATION AT THIS TIME. (X)
Other aircraft with N54 · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N54 is registered now to the first aircraft listed.