N1076Y
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
23 reports on file, 1996-04-10 – 2003-01-07.
Part: TRANSCEIVER — DAMAGED (VHF SYSTEM) · airframe 29,654 hrs
VHF TRANSCEIVER LED WOULD NOT DISPLAY. REPLACED DS501 DISPLAY AND LENS. REPAIRED. FOUND RECEIVER A LITTLE WEAK AT 118 MHZ. ALIGNED RECEIVER AND ADJUSTED C/N SQUELCH. REPAIRED. BENCH CHECK GOOD.
Part: TRANSCEIVER — INOPERATIVE (VHF SYSTEM) · airframe 29,864 hrs
VHF TRANSCEIVER IS DEAD, WILL NOT COME ON. FOUND TRANSMIT POWER OUT AND MODULATION FLUCTUATING. REPLACED Q121 AND Q122 TRANSISTORS AND ALSO BAD DISPLAY LENS. REPAIRED. BENCH CHECK GOOD.
Earlier reports · 1996–2001 · 21 reports
2001
Part: RADIO — MALFUNCTIONED (VHF COMMS) · airframe 28,137 hrs
WOULD NOT CHANGE FREQUENCY. REPLACED BAD KHZ KNOB/SHAFT AND RESOLDERED COLD SOLDER ON SW102 SWITCH. REPAIRED. ALIGNED RECEIVER AND ADJUSTED C/N SQUELCH, MIC GAIN AND SIDETONE. REPLACED BAD DISPLAY LENS. BENCH CHECK GOOD.
1999
Part: INDICATOR — WORN (DUAL TACH)
YELLOW MARKS TACHOMETER INDICATOR ARE FADING AWAY.
Part: INDICATOR — STICKING (COCKPIT)
INDICATOR STICKS DURING STARTING, GLASS FOGGED IN-FLIGHT.
Part: PUMP — WORN (FUEL SYSTEM)
PERFORMED SPLINE INSPECTION AND FOUND WORN DRIVE SPLINES FUEL PUMP.
Part: TUBE — CORRODED (CYCLIC)
TUBE ASSEMBLY HAS CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE CYCLIC TUBE.
Part: POWER SUPPLY — INOPERATIVE (STROBE)
POWER SUPPLY HAS NO POWER OUT, DOES NOT WORK.
Part: INDICATOR — LEAKS (TRANSMISSION OIL)
INDICATOR HAS INTERNAL LEAK.
Part: FLOAT — LEAKING (MLG)
FLOAT BAG ASSEMBLY LEAKS FROM LOWER INBOARD SEAM.
Part: INDICATOR — READS HIGH (TORQUE METER)
TORQUE INDICATOR READS HIGH OUT OF TOLERANCE.
Part: FLOAT — LEAKING (MLG)
FLOAT BAG ASSEMBLY LEAKS FROM INBOARD VALVE.
Part: FLOAT — LEAKING (MLG)
FLOAT BAG ASSEMBLY HAS SLOW LEAK FROM LOWER OUTER SEAM NEAR MOUNT AREA. TOTAL TIME 11/1991.
Part: DISC SET — CORRODED (TAIL ROTOR)
DISC CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE ASSY.
Part: RING ASSY — CORRODED (M/R MAST)
RING ASSY CORRODED UNDER NUTPLATE. SCRAPPED AND REPLACED WITH SERVICEABLE PART.
Part: CROSSTUBE — CORRODED (AIRFRAME AFT)
CORROSION UNDER PAD OF AFT CROSSTUBE. SCRAPPED AFT CROSSTUBE AND REPLACED WITH SERVICEABLE CROSSTUBE.
Part: CROSSTUBE — CORRODED (AIRFRAME FWD)
CORROSION BEYOND LIMITS ON LOWER PORTION OF TUBE IN AREA A. SCRAPPED FORWARD CROSSTUBE AND REPLACED WITH SERVICEABLE CROSSTUBE.
Part: DOOR — MISMANUFACTURED (FUSELAGE)
MISMANUFACTURED DOOR.
Part: SUPPORT — CORRODED (MAIN ROTOR)
SUPPORT ASSEMBLY CORRODED BEYOND LIMITS. SCRAPPED AND REPLACED WITH SERVICEABLE SUPPORT.
1998
Part: SHROUD HOUSING — MIS MFG (ENGINE)
RECEIVED SHROUD HOUSING AND UNABLE TO OBTAIN THROAT CLEARANCE BETWEEN SHROUD AND IMPELLER. NOTE: TRIED ON SEVERAL IMPELLERS. INSTALLED A DALLAS AIRMOTIVE OVERHAULED SHROUD ASSY.
1996
Part: GEARSHAFT — DEFECTIVE (ENG COMP)
ENGINE REMOVED DUE TO IMPELLER RETIREMENT. UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING: FAILED GO,NO-GO GUAGE INSPECTION ON SPUR ADAPTER GEARSHAFT FORWARD AND AFT SPLINES. INSTALLED NEW PART.
Part: INDICATOR — ERRATIC (COCKPIT)
ERRATIC OPERATION FROM 0 TO 65%. SENT TO PRECISION AVIONICS & INST., INC. FOR INSPECTION AND REPAIR.
Part: YOKE — BEARING FAILED (M/R)
DISASSEMBLED TO COMPLY WITH 1200 HOUR INSPECTION. FOUND YOKE BEARING JOURNAL AND TRUNNION RACES BREAKING DOWN. SCRAPPED PARTS LOCALLY. ALSO SCRAPPED BEARINGS (4 EACH) P/N 206-011-113-001 AND (2 EACH) P/N 206-011-111-001.