N10761
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.
26 reports on file, 1996-03-04 – 2004-10-13.
Part: FUEL NOZZLE — CRACKED (ENGINE)
CRACKED SHROUD AND SPRAY BODY/ REPLACED. (K)
Earlier reports · 1996–1999 · 25 reports
1999
Part: HORIZON — FAILED (COCKPIT)
HORIZONTAL GYRO UNRELIABLE.
Part: INDICATOR — READS HIGH (ENGINE OIL)
ENGINE OIL AND TEMPERATURE INDICATORS INDICATES HIGH, FLUCTUATES AT LOW END.
Part: POWER SUPPLY — INOPERATIVE (STROBE)
POWER SUPPLY HAS NO POWER OUT.
Part: INDICATOR — MALFUNCTIONED (TOT)
TOT INDICATOR INCREASES IN TEMP WHEN VHF IS KEYED.
Part: INDICATOR — STICKS (COCKPIT)
INDICATOR STICKS AT ZERO AND 55 PERCENT WITH SEVERE FLUCTUATION.
Part: TRUNNION — FAILED (TAIL ROTOR)
T/R TRUNNION CAP BOLTS FAILED THREAD ENGAGEMENT CHECK.
1998
Part: INDICATOR — ERRATIC (COCKPIT)
FUEL QUANTITY INDICATOR HAS ERRATIC READING, UNIT READS HIGH OUT OF TOLERANCE.
Part: TRANSCEIVER — WEAK (COCKPIT)
TRANSCEIVER OUTPUT WEAK.
Part: INDICATOR — STICKS (COCKPIT TOT)
INDICATOR STICKS AT 200 DEGREES INTERMITTENTLY AND NO OVERTEMP LIGHT.
Part: CELL — LEAKING (FUEL SYS)
FUEL CELL BLISTERS AND LEAKAGE AS MARKED AND POSSIBLE FUEL SEEPAGE THROUGH FABRIC.
Part: TRANSCEIVER — FAILED (COCKPIT)
NO 5 VOLTS OUT OF POWER SUPPLY AND CHECK TONES FOR PROPER OPERATION.
Part: SCROLL — WARPED (ENG COMP)
ENGINE REMOVED DUE TO LOW POWER. SCROLL REMOVED DUE TO EXCESSIVE AIR LEAKS ON TEST CELL BETWEEN SCROLL AND VANE AS MARKED; WARPED FLANGE.
Part: SHROUD HOUSING — DEFECTIVE (ENG COMP)
ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF COMPRESSOR PARTS NOTED: COATING LIFTING ON SHROUD HOUSING. INSTALLED A DALLAS AIRMOTIVE OVERHAULED SHROUD ASSY.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT)
KNOB BROKEN OFF. PERFORMED PRELIMINARY INSPECTION. REPLACED FACEPLATE ASSEMBLY P/N 200-2020-01, REPAIRED. ADJUSTED TO SPECS. BENCH CHECK GOOD.
Part: LINK ASSY — WORN (TRANSMISSION)
TRANSMISSION LINK ASSY WORN.
1997
Part: INDICATOR — FAILED (ENG OIL)
INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. (BYPASS INOPERATIVE)
Part: TRANSMITTER — FAILED (FUEL PRESS)
PRESSURE DROPS TO ZERO IN FLIGHT.
Part: TACH GEN SHAFT — WORN (ROTOR)
TACH GEN SHAFT WORN.
1996
Part: CASE ASSY — CORRODED (MAIN GR BOX)
TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED: CORROSION ON I/P FLANGE SURFACE AND SURFACE WHERE CENTER CASE SEATS. REPLACED WITH SERVICEABLE PARTS. SEE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED.
Part: SHAFT — CORRODED (M/R GR BOX)
TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED:CORRODED SPLINES BEYOND LIMITS. REPLACED WITH SERVICEABLE PARTS. SEE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED.
Part: CASE ASSY — CORRODED (M/R GR BOX)
TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED: CORROSION IN ORING GROOVE. REPLACED WITH SERVICEABLE PARTS. SEE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED.
Part: HOUSING — CORRODED (M/R GR BOX)
TRANSMISSION OVERHAUL DUE. UPON INSPECTION OF PARTS NOTED: CORROSION IN BOLT HOLE. REPLACED WITH SERVICEABLE PARTS. SEE MMIR# HEEA0008563 THROUGH HEEA0008566 FOR PARTS REPLACED.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT VHF)
VHF FREQUENCY SELECT KNOB. INTERMITTENT WON'T CHANGE FREQUENCY.
Part: ELT — FAILED (COCKPIT)
CAME ON IN FLIGHT AND WOULD NOT TURN OFF WITH REMOTE SWITCH. SENT
Part: BEARING — CRACKED (T/R BLADE)
BEARINGS CRACKED. ALSO REPLACED 4 EACH SLEEVES, P/N 206-010-733-003 AND 8 EACH SPACERS, P/N 206-011-742-101. NOTE: SEE MMIR'S # 6826 THROUGH #6835 FOR ADDITIONAL BEARING REPLACEMENTS.