Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2007FA0000753Line · leakingAC HAD HYDRAULIC LIGHT, PILOT PERFORMED A PRECAUTIONARY LANDING AT THE AIRPORT. UPON INSP FOUND HYDRAULIC LINE FROM PUMP TO MANIFOLD LEAKING AT THE BOTTOM OF THE SWEDGE FITTING. HYDRAULIC LINE WAS REPLACED WITH NEW LINE. HYDRAULIC SYSTEM WAS SERVICED, GROUNSDR PG92004F00013Blade · crackedT/R SPAR FOUND TO HAVE 5 INCH LONG SPANWISE SPAR CRACK, FOUND BY PILOT UPON TURN AROUND CHECK. THIS CONDITION PERSISTS ON THIS MODEL HELICOPTER AND PN COMPONENT. REPLACED ENTIRE T/R BLADE WITH SERVICEABLE UNIT. RETURN HELICOPTER TO SERVICE.SDR PG92004F00004Bearing · failedTAIL ROTOR BEARING FAILED WITH ONLY 354 HOURS. (K)SDR PG92004F00002Coupling Sleeve · failedCOUPLING SLEEVE FAILED WITH ONLY 354 HOURS, SHAFT SEIZED TO COUPLING SLEEVE. (RMA NR R046420) (K)SDR PG92004F00001Shaft · seizedHYDRAULIC PUMP FAILED WITH ONLY 354 HOURS. SHAFT SEIZED TO PUMP AND TO COUPLING. (RMA NR R046420) (K)SDR PH92003F00001Blade · crackedTAIL ROTOR BLADE HAS 4000 HOURS TBR(SLL). UNIT FAILED AT 2760.0 TTSN. MASSIVE SPAR CRACK ON LAMINATED SPAR. UNIT RETURNED TO MFG.SDR PG92002F00000Engine · failedENGINE CHIP LIGHT ILLUMINATED DURING PART 135 FLIGHT. PILOT MADE PRECAUTIONARY LANDING ON IMPROVED PRIVATE HELIPAD. MECHANIC DISPATCHED TO SIDE. FOUND EXCESSIVE METAL SLIVERS ON ALL ENGINE OIL SYSTEM MAGNETIC AND INDICATOR CHIP DETECTORS. AIRCRAFT GROUNDEDSDR VY1R103208Spline Adapter · wornHYDRAULIC PUMP SPLINE DRIVE WORN, WAS LUBRICATED IAW MSR PRIOR.
Other aircraft with N170PA · 2
The FAA can assign a mark to another aircraft once a registration is cancelled. N170PA is registered now to the first aircraft listed.