N60WJ

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

Bell 206L-1 No injuries Part 91operator not named in the NTSB record
Source: NTSB case MIA98LA148

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.

5 reports on file, 2002-10-10 – 2004-07-23.

WARNING INDICATION · 2004-07-23 Matched by certificate designator
ATA 2435

Part: BEARING — LOOSE (STARTER GEN)

DURING TAKEOFF FROM HA-340 THE TORQUE GUAGE FLUCTUATING 10 PERCENT. MAINTENANCE REMOVED AND REPLACED STARTER GENERATOR. BEARING LOOSE ON THE STARTER GENERATOR CAUSING TORQUE FLUCTUATION. CHANGED FUEL FILTER AND TOOK FUEL SAMPLE AND PERFORMED PNEUMATIC AIR LEAK TEST. PERFORMED ALL WORK IAW 206L-1 AND ROLLS ROYCE C-28 MM. (M)

Source: SDR 2004F00374
OTHER · 2003-06-24 Matched by certificate designator
ATA 8300

Part: GEARSHAFT — SPALLED (GEARBOX) · airframe 11,340 hrs

FOUND SPALLING ON GEAR TEETH. REMOVED AND REPLACED DUE TO SPALLING ON GEAR TEETH FROM POSSIBLE IMPROPER MESHING OF GEAR TEETH.

Source: SDR ALGA087723
OTHER · 2003-06-24 Matched by certificate designator
ATA 8300

Part: GEAR — DEFECTIVE (GEARBOX PTO) · airframe 11,340 hrs

AS PER MANDATORY BULLETIN T-075. REMOVED AND REPLACED. SUBMITTED BY: PRESTON BARZARE

Source: SDR ALGA087724
FLUID LOSS · 2002-11-18 Matched by certificate designator
ATA 2910

Part: LINE — LOOSE (FUEL BOOST)

DURING REFUELING, FUEL LEAKING FROM THE BELLY OF THE AIRCRAFT, THE MECHANIC FOUND FUEL BOOST PUMP TRANSFER LINE IS LEAKING, TIGHTENED THE LINE AND LEAK CHECKED AND FOUND OK., THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR ALG2003F00017
FLUID LOSS · 2002-10-10 Matched by certificate designator
ATA 7310

Part: LINE — LEAKING (FUEL CONTROL)

DURING POST FLIGHT. FUEL LINE FROM THE FUEL CONTROL TO THE FIRESHIELD WAS LEAKING, THE MECHANIC REMOVED AND REPLACED THE LEAKING LINE AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR ALG2003F00001