N50182

No registry detail on file · not in current registry

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.

22 reports on file, 1995-03-02 – 1999-02-23.

OTHER · 1999-02-23 Matched by certificate designator
ATA 7921

Part: OIL COOLER — CLOGGED (ENGINE OIL)

CORE CLOGGED, HIGH OIL TEMPERATURE INDICATION ON OIL COOLER.

Source: SDR HEEA060917
OTHER · 1999-02-16 Matched by certificate designator
ATA 3212

Part: FUSIBLE PLUG — LEAKING (FLOAT)

FLOAT BOTTLE PRESSURE LEAKING THROUGH FUSIBLE PLUG. REPLACED WITH SERVICEABLE PLUG.

Source: SDR HEEA060666
Earlier reports · 1995–1998 · 20 reports

1998

OTHER · 1998-09-11 Matched by certificate designator
ATA 3422

Part: GYRO — PRECESSING (COCKPIT)

DIRECTIONAL GYRO INDICATOR PRECESSES AND DOES NOT SLAVE CORRECTLY.

Source: SDR HEEA0016022
OTHER · 1998-08-27 Matched by certificate designator
ATA 3197

Part: INDICATOR — SHORTED (CAUTION PANEL)

INDICATOR FOR ENG. OUT SEGMENT AND ROTOR LOW RPM SEGMENT.

Source: SDR HEEA0015880
OTHER · 1998-08-13 Matched by certificate designator
ATA 3452

Part: TRANSPONER — FAILED (COCKPIT)

TRANSPONDER ALTITUDE REPORTING OFF BY 28,000 FEET.

Source: SDR HEEA0015514
OTHER · 1998-06-22 Matched by certificate designator
ATA 2435

Part: COMMUTATOR — CORRODED (STARTER/GEN)

EXCESSIVE CORROSION FOUND ON END BELL DURING FIRST 500 HOUR INSPECTION.

Source: SDR HEEA0014852
OTHER · 1998-06-04 Matched by certificate designator
ATA 3422

Part: GYROSCOPE — MALFUNCTIONED (COCKPIT)

DIRECTIONAL GYRO SLAVES BACKWARDS.

Source: SDR HEEA0014600
OTHER · 1998-04-22 Matched by certificate designator
ATA 2435

Part: START/GEN — CORRODED (END BELL)

EXCESSIVE CORROSION FOUND ON END BELL DURING IT'S FIRST 500 HOUR INSPECTION WHICH CORRODED THROUGH ONE OF THE SCREW HOLES. NOTE: THIS SEEMS TO HAVE HAPPENED DUE TO THE TYPE FINISH THESE END BELL ASSEMBLIES HAVE. THEY DON'T HAVE ANY PAINT OR PRIMER.

Source: SDR HEEA0014015
OTHER · 1998-03-19 Matched by certificate designator
ATA 7714

Part: INDICATOR — FAILED (COCKPIT)

INDICATOR WILL NOT INDICATE.

Source: SDR HEEA0013478
OTHER · 1998-02-05 Matched by certificate designator
ATA 7810

Part: EXHAUST ASSY — CRACKED (ENG EXH)

EXH ASSY CRACKED. EXCESSIVE LEAKAGE.

Source: SDR HEEA0012834

1997

OTHER · 1997-11-19 Matched by certificate designator
ATA 2913

Part: PUMP — WORN (HYD SYS)

PUMP WORN SPLINE.

Source: SDR HEEA0012107
OTHER · 1997-11-19 Matched by certificate designator
ATA 3452

Part: TRANSPONDER — FAILED (COCKPIT ATC)

TRANSPONDER DOES NOT SEND OUT A CODE. (NO POWER OUT AND PULSE WIDTH OUT OF SPECS)

Source: SDR HEEA0012110
FLUID LOSS · 1997-10-07 Matched by certificate designator
ATA 7314

Part: PUMP — LEAKING (ENG FUEL)

FUEL PUMP LEAKING AT SEAL DRAIN.

Source: SDR HEEA0011251

1996

OTHER · 1996-10-14 Matched by certificate designator
ATA 7714

Part: INDICATOR — NEEDLE STICKS (DUAL TACH)

TURBINE NEEDLE STICKS AT 33%.

Source: SDR HEEA968356
OTHER · 1996-10-03 Matched by certificate designator
ATA 3452

Part: TRANSCEIVER — DEFECTIVE (COCKPIT ATC)

KNOB BROKEN. REPLACED FACEPLATE ASSEMBLY. ALSO REPLACED WEAK V301 PHOTODETECTOR AND REPLACED BROKEN PLASTIC LOCKING MECHANISM. BENCH CHECK GOOD.

Source: SDR HEEA968042
OTHER · 1996-05-31 Matched by certificate designator
ATA 2822

Part: FUEL PUMP — WORN (BOOST)

PUMP WORN INTERNAL DRIVE SPLINES.

Source: SDR HEEA967306

1995

OTHER · 1995-12-12 Matched by certificate designator
ATA 7250

Part: WHEEL — BLADE CRACKED (3RD STAGE)

ENGINE REMOVED DUE TO 3RD STAGE TURBINE WHEEL INSPECTION. 3RD STAGE WHEEL RETURNED TO ALLISON FOR INSPECTION PER LETTER C1245F-RMG-1195. ZYGLO INSPECTION REVEALED ONE EACH INDICATION 1/8" FROM SHROUD OF L/E BACK SIDE OF BLADE. INDICATIONDOES NOT GO THROUGH BLADE. INSTALLED SERVICEABLE 3RD STAGE WHEEL.

Source: SDR HEEA956229
OTHER · 1995-07-20 Matched by certificate designator
ATA 6330

Part: LINK ASSY — DELAMINATED (M/R XMSN MT)

BEARING DELAMINATED. REPLACED WITH SERVICEABLE LINK ASSEMBLY.

Source: SDR HEEA955374
OTHER · 1995-07-13 Matched by certificate designator
ATA 6320

Part: BEARING — MAKING METAL (M/R)

METAL IN OIL. CAUSE OF METAL IN OIL DUE TO BEARING SPALLED. REPLACED WITH SERVICEABLE BEARING. REPAIRED TRANSMISSION.

Source: SDR HEEA955355
OTHER · 1995-06-30 Matched by certificate designator
ATA 6220

Part: WASHER — DETERIORATION (M/R THRUST)

MATERIAL DETERIORATION CAUSING EXCESSIVE LOAD. LOWERED TORQUE ON ADJUSTMENT SCREWS AND LOWERED PRELOAD ON THRUST PLUGS.

Source: SDR HEEA955294
OTHER · 1995-06-15 Matched by certificate designator
ATA 7250

Part: WHEEL — SULFIDATION (1ST STAGE)

ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING: SEVERLY SULFIDATED BLADE TIP ON #1 WHEEL CAUSING WHEEL AND NOZZLE CONTACT WITH TRAILING EDGE TIPS OF 8 EACH BLADES MISSING. SCRAPPED #1 WHEEL.

Source: SDR HEEA955191
OTHER · 1995-03-02 Matched by certificate designator
ATA 3414

Part: INDICATOR — READS LOW (COCKPIT AIR SPD)

NEEDLE INDICATES 8 KNOTS LOW AT 100 KNOTS.

Source: SDR HEEA954479