N5366Y

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

Accident · 1975-11-14 Unresolved
PIPER PA-23 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case DEN76FQA25
Accident · 1966-10-02 Unresolved
PIPER PA-23 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case NYC67F0332

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.

10 reports on file, 1996-01-22 – 2001-05-02.

OTHER · 2001-05-02 Matched by certificate designator
ATA 7323

Part: GOVERNOR — CRACKED (NR 1 ENGINE) · airframe 12,335 hrs

EPOXY DEBONDED ON GOVERNOR DRIVE SHAFT. REMOVED FROM SERVICE AND SENT IN FOR WARRANTY REPAIR.

Source: SDR AC2A075787
OTHER · 2001-03-19 Matched by certificate designator
ATA 7323

Part: GOVERNOR — DEBONDED (ENGINE) · airframe 12,000 hrs

UNBONDED SHAFT.

Source: SDR AC2A072835
WARNING INDICATION · 2001-03-06 Matched by certificate designator
ATA 7323

Part: GOVERNOR — DEBONDED (NR 1 ENGINE) · airframe 12,162 hrs

PILOT REPORTED N2 OVERSPEED UNCONTROLLABLE WITH RPM TRIM MOTOR. NR 1 ENGINE RETURNED TO FLIGHT IDLE. FUEL JETTISONED, AND PILOT PERFORMED RUN-ON LANDING. REMOVED GOVERNOR AND FOUND DRIVE SPLINE DISENGAGED FROM GOVERNOR SHAFT. GOVERNOR REPLACEMENT FIXED PROBLEM.

Source: SDR AC2A072834
OTHER · 2000-06-22 Matched by certificate designator
ATA 6220

Part: BOLT — DEFECTIVE (MAIN ROTOR HEAD)

PART IS DEFECTIVE. BOLT HEAD HAS SEVEN SIDES INSTEAD OF THE USUAL SIX. PART TT IS 311.0 HOURS SINCE NEW. REPLACED BOLT. (X)

Source: SDR AC2A0000065
OTHER · 2000-06-03 Matched by certificate designator
ATA 6710

Part: CONTROL ROD — CRACKED (TAIL ROTOR)

TUBE IS CRACKED AT COLLAR. REPLACED TUBE. (X)

Source: SDR AC2A0000046
INADEQUATE Q C · 1999-02-17 Unresolved
ATA 7921

Part: COOLER — MISOVERHAULED (OIL SYSTEM)

INSTALLED OIL COOLER AT ZERO TSO TO REPLACE A LEAKING COOLER. DURING FIRST RUN-UP, TRANSMISSION OIL PRESSURE IMMEDIATELY EXCEEDED MAXIMUM ALLOWABLE LIMITS. BY PERFORMING A BORESCOPE INSPECTION, LOOSE AND BUILT UP CARBON WAS DISCOVERED IN THE COOLER. RELEASED CARBON ALSO CONTAMINATED THE TRANSMISSION CLOGGING UP THE OIL JETS AND DRIVING UP THE PRESSURE. FURTHER INVESTIGATION REVEALED ALL ENGINE AND TRANSMISSION FITTINGS AND LINES WERE CONTAMINATED WITH CARBON PARTICLES. TRANSMISSION WAS SUBSEQUENTLY TORN DOWN, CLEANED AND INSPECTED, AND ALL LINES. FILTERS AND OIL TANKS HAD TO BE CLEANED, FLUSHED, INSPECTED AND RE-INSTALLED.

Source: SDR 99ZZZX1954
OTHER · 1997-12-07 Unresolved
ATA 7323

Part: GOVERNOR — FAILED (ENGINE)

FLUCTUATING TORQUE SETTING. FOUND GOVERNOR DRIVE BROKEN. REPLACED GOVERNOR.

Source: SDR 98ZZZX297
OTHER · 1997-09-11 Unresolved
ATA 7323

Part: GOVERNOR — MALFUNCTIONED (ENGINE)

GOVERNOR HAS NO MORE ADJUSTMENT FOR COMPENSATION. REPLACED GOVERNOR.

Source: SDR 97ZZZX4976
OTHER · 1996-07-01 Unresolved
ATA 7714

Part: INDICATOR — MALFUNCTION (TRIPLE TACH)

TACHOMETER GAVE A FALSE READING OF 105 PERCENT PERCENT DURING FLIGHT. REPLACED TACHOMETER.

Source: SDR 96ZZZX4184
OTHER · 1996-01-22 Unresolved
ATA 5311

Part: FRAME — CRACKED (RT SHELL 9V)

DURING A ROUTINE INSPECTION, A CRACK WAS FOUND IN THE UPPER END OF FRAME 9V IN THE RIGHT SIDE SHELL. THE CRACK WAS APPROXIMATELY 2.5 INCHES LONG. THE CRACK EXTENDED UNDER THE ATTACHMENT OF THE INBOARD WEB ATTACHED TO THE RIGHT AFT MAIN GEARBOX ATTACHMENT FITTING IN THE AIRFRAME. REPAIRED PER FIELD APPROVED 337 AND BOLKOW SB SI-BO105-142.

Source: SDR 96ZZZX613