Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2013FA0000559Leaf Pad · looseBEFORE FIRST FLIGHT CHECK, WHILE HELICOPTER WAS ON TRANSPORT WHEELS, MECHANIC NOTICED THE LT SKID T/E LEAF PAD, LEAF SPRING, WAS LOOSE. REPLACED BOTH LEAF PADS WITH NEW AND REPLACED ALL ATTACHING HARDWARE.SDR 2009FA0000619Starflex · debondedDURING A DAILY INSP, CRACKS WERE NOTED ON THE MAIN ROTOR STARFLEX IN
ADHESIVE BOND FILLET THAT BONDS THE BUSH ONTO STARFLEX ARM. THERE WAS NO INDICATION OF A BOND SEPARATION OR GAP BETWEEN BUSH AND STARFLEX. UTILIZING THE PROCEDURE FROM MM 62.20.00.601 PARSDR WTU0701Starter Gen · seizedWHILE CONDUCTING A SEARCH OVER MOUNTAINOUS TERRIAN AT NIGHT UTILIZING AN SX-5 SEARCHLIGHT, TEN MINUTES INTO THE SEARCH LIGHT QUIT WORKING. APPROXIMATELY 30 SECONDS LATER THE GENERATOR FAIL LIGHT ILLUMINATED AND THE CREW SMELLED SMOKE IN THE COCKPIT. APPROXIMSDR B3O2004F00000Blade · damagedMAIN ROTOR BLADE RECEIVED FROM AEC WITH DAMAGE TO THE TRAILING EDGE OF THE NR 3 TRIM TAB. TRIM TABS RESET AT AEC PRIOR TO RECEIPT AEC WO NR W0078958. BLADE NOT ABLE TO FLY CORRECTLY ON TWO DIFFERENT AC. REQUEST EVALUATION OF BLADE.SDR B30R20040226Door Frame · crackedDURING 100 HOUR INSPECTION DISCOVERED CO-PILOT DOOR POST CRACKED 14 INCHES LONG STARTING 8 INCHES ABOVE CABIN FLOOR, EXCEEDING THE LIMITS IN REPAIR MANUAL. REPAIRED CRACK IAW MM. REQUESTED FROM MFG.SDR USOM117002Drive Shaft · slippedINSTALLED SHAFT IN AIRCRAFT AND COMPLIED WITH INITIAL BALANCE RUN, AFT BEARING SLIPPED ON SHAFT AND EXCESSIVE HEAT ON ALL BEARINGS. CLEANED AND REINDEXED BEARING, ON SECOND RUN, 3 BEARINGS SLIPPED EXCESSIVELY AND COPIUS AMOUNTS OF GREASE SLUNG FROM ALL BEARINSDR B3OR20020009Isolator · delaminatedDURING A 1000 HOUR INSPECTION, THE FORWARD LATTERAL LAMINATED ISOLATOR MEMBER WAS FOUND TO BE DELAMINATED. THERE WAS NO OIL OR HYDRAULIC FLUID PRESENT IN THE AREA OR ON THE LAMINATED ISOLATOR MEMBER ITSELF. WE SUSPECT THAT THE AFT ISOLATOR MEMBER LOSS OF TORSDR B3OR20020008Coupler · wornDURING 1000 HOUR INSPECTION, THE ENGINE TO TRANSMISSION MOUNT TUBE WAS FOUND TO HAVE EXCESSIVE PLAY. THE GIMBAL RING MOUNT BUSHINGS ON THE TUBE WERE MEASURED, AND FOUND TO BE OUT OF LIMITS. UPON FURTHER INVESTIGATION, AND A PHONE CALL TO AMERICAN EUROCOPTER, WSDR B3OR20020006Crossbeam · groovedDURING A 1000 HOUR INSPECTION, THE CROSS BEAM WAS FOUND TO HAVE ONE DELAMINATED FWD. RUBBER ISOLATOR, AND DAMAGE TO THE AFT LATERAL LAMINATED RUBBER ISOLATER MOUNTING AREA. THE DAMAGE WAS CAUSED BY THE RUBBER ISOLATOR LOSING TORQUE, AND ROTATING ON ITS MOUNTINSDR B3O2001F00000Relay · corrodedDURING TAIL BOOM INSPECTION, TECHNICIAN DISCOVERED BOTH RELAYS HAD SEVERE RUST AND CORROSION ON TERMINALS AND RELAY BODY. LOCATION OF RELAYS ARE UNDER THE AFT A/C SYSTEM CONDENSOR UNIT.SDR SW032001B3673Pump · failedFUEL PUMP FAILED DURING FLIGHT. NO FLIGHT ABORT.SDR 20000609SH025Freq Adapter · crackedDURING 500-HOUR INSPECTION, FOUND YELLOW BLADE FREQUENCY ADAPTER CRACKED AT EDGE OF KEVLAR MATING SURFACE. THIS IS FIRST OCCURRENCE OF THIS TYPE ON THE 3 AIRCRAFT OF SAME TYPE OPERATED A TOTAL OF 1200 HOURS. NO REASON FOUND FOR DEFECT. (X)SDR 20000510SH025Relay · wrong partAIRCRAFT STOPPED AT REMOTE LOCATION FOR FUEL. UPON ATTEMPTING TO RE-START, WHEN STARTER BUTTON PRESSED, THE IGNITERS POPPED, BUT THE STARTER/GENERATOR WAS DEAD. DURING T/S, DISCOVERED THE K3 START RELAY WAS THE WRONG PART NUMBER. IT IS SUPPOSED TO BE P/N 4
Other aircraft with N5204Y · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N5204Y now.