N3174Y

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-3 Minor injury Part 135operator not named in the NTSB record
Source: NTSB case FTW02LA217

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.

4 reports on file, 1997-12-03 – 2001-10-19.

OTHER · 2001-10-19 Matched by certificate designator
ATA 7250

Part: BLADE — CORRODED (ENGINE)

TURBINE RECEIVED FOR TIME CHANGE ON 3RD AND 4TH STAGE WHEEL RETIREMENT. TURBINE HAD A MFG LINER INSTALLED. REMOVED COMBUSTION SECTION AND FOUND SULFIDATION ON 1ST STAGE WHEEL BLADES. CHECK 1ST STAGE WHEELS FOR PROPER COATING.(K)

Source: SDR ALG2001F00030
OTHER · 2000-06-11 Unresolved
ATA 6210

Part: BLADE — CORRODED (MAIN ROTOR)

DURING DAILY INSPECTION, FOUND HEAVY INTERGRANULAR CORROSION ON TRAILING EDGE EXTRUSION. (X)

Source: SDR 20000718SH013
OTHER · 1998-07-01 Unresolved
ATA 6210

Part: BLADE — CORRODED (MAIN ROTOR)

DISCOVERED DURING DAILY INSPECTION, CORROSION AND SEPARATION AT TIP.

Source: SDR 99ZZZX1226
OTHER · 1997-12-03 Unresolved
ATA 6210

Part: BLADE — CORRODED (M/R)

DISCOVERED DURING DAILY INSPECTION, M/R BLADE TRAILING EDGE EXTRUSION CORRODED CAUSING APPROXIMATELY 10 INCH LONG SEPARATION.

Source: SDR 98ZZZX475