N2770Y
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
21 reports on file, 1996-01-09 – 1999-02-23.
Part: POWER SUPPLY — INOPERATIVE (STROBE)
POWER SUPPLY HAS NO POWER OUT.
Part: FUEL CELL — LEAKING (DRAIN)
FUEL CELL LEAKING IN DRAIN.
Part: ACTUATOR — INTERMITTENT (DROOP BAY)
SCREW BROKEN, ACTUATOR HAS INTERMITTENT OPERATION.
Part: HUB — UNBALANCED (TAIL ROTOR)
UNABLE TO BALANCE TAIL ROTOR ASSEMBLY. PITTING ON TRUNNION SPLINES. THRUST PLUGS WORN EXCESSIVELY. HOUSING BOLTS DID NOT OBTAIN .025 INCH OF THREAD ENGAGEMENT.
Part: SHAFT — CORRODED (FREEWHEEL)
CORROSION BEYOND LIMITS ON SEAL RIDE. REPLACED WITH SERVICEABLE SHAFT.
Part: FIN — CRACKED (TAIL BOOM)
TOP AFT BOLT SLEEVE CRACKED ON FIN ASSEMBLY.
Earlier reports · 1996–1998 · 15 reports
1998
Part: ACTUATOR — CRACKED (DROOP COMP)
ACTUATOR SHAFT CRACKED.
Part: LORAN — MALFUNCTIONED (COCKPIT)
LORAN WILL NOT FUNCTION IN NAV MODE.
Part: SKID TUBE — CRACKED (UNDERCARRIAGE)
INSP FOUND CRACKS ON SKID TUBE IN SEVERAL PLACES.
Part: INDICATOR — FLUCTUATES (XMSN TEMP/PRESS)
OIL PRESS NEEDLE FLUCTUATES.
Part: GEAR — WORN (SPUR ADAPTER)
ENGINE REMOVED DUE TO TURBINE OVERHAUL. INSPECTION OF COMPRESSOR PARTS REVEALED: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR GEARSHAFT AFT SPLINES (FAILED NO-GO GAUGE) INSTALLED A NEW SPUR GEAR.
Part: INDICATOR — FLUCTUATES (ENG OIL)
FLUCTUATES 5 PSI WHEN UNIT IS VIBRATED.
Part: LORAN — INOPERATIVE (COCKPIT)
LORAN KEYPAD ASSY. INOPERATIVE AND ENVELOPE NUMBER SHOWING BLANK.
Part: INDICATOR — FAILED (ENG OIL)
INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.
1997
Part: CARTRIDGE — LEAKING (FUEL BOOST)
CARTRIDGE LEAKING FROM INNER SPINAL RING AREA.
Part: NOZZLE — CRACKED (ENGINE)
ENGINE REMOVED DUE TO TURBINE 1500 HOUR OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR1 NOZZLE VANES. INSTALLED A DALLAS AIRMOTIVE OVERHAUL NR1 NOZZLE.
Part: INDICATOR — FAILED (DUAL TACH)
DUAL TACH HAS SPLIT NEEDLES.
Part: TACH GENERATOR — WORN (SPLINE ADAPTER)
SPLINE ON ADAPTER WORN AND CLIP BROKEN. SENT TO GLOBE MOTORS, INC. FOR INSPECTION AND REPAIR.
1996
Part: ENCODER — FAILED (ALTIMETER)
ENCODER NO OUTPUT.
Part: TRANSCEIVER — INOPERATIVE (COCKPIT ATC)
INOPERATIVE. REPLACED V101CAVITY OSC. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY, ALSO ADJUSTED SLS. BENCH CHECK GOOD.
Part: BATTERY — DEFECTIVE (DC SYS)
BATTERY WILL NOT ACCEPT A CHARGE. INSPECTED BY ACCESSORY SHOP AND FOUND THIS BATTERY WAS REMOVED NUMEROUS TIMES FOR BEING WEAK.