N312LS

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
OMNIFLIGHT HELICOPTERS INCOperatoron 2000-07-16Operator named in NTSB report

Accident & incident history

Accident · 2000-07-16 Operator named in NTSB report
Mbb BK-117-A3 No injuries Part 91OMNIFLIGHT HELICOPTERS INC

Operated by OMNIFLIGHT HELICOPTERS, INC. (per NTSB report)

Source: NTSB case FTW00LA206

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.

3 reports on file, 1999-01-14 – 1999-12-08.

OTHER · 1999-12-08 Unresolved
ATA 6710

Part: CYCLIC JACKSHAFT — CORRODED (MAIN ROTOR)

TECHNICIAN PULLED LARGE AMOUNT OF RUST OUT OF INSIDE OF CYCLIC JACKSHAFT WHILE USING MAGNET TO RETRIEVE LOST SCREW. REMOVED JACKSHAFT AND INSPECTED. LARGE AMOUNT OF RUST RESIDUE AND PITTING OF JACKSHAFT ESPECIALLY ON PILOT SIDE. MFG ALLOWS .4 MM CORROSION DAMAGE. ALMOST IMPOSSIBLE TO MEASURE DEPTH WITH CONVENTIONAL MEANS. WILL SEND TO BE ULTRASONICALLY TESTED. SUBMITTER SUSPECTED THIS ONE BEYOND LIMITS. REMOVED SAME P/N SHAFT OUT OF ANOTHER ACFT. IT HAD SMALL AMOUNT OF SURFACE RUST. APPEARS THERE IS INSUFFICIENT PAINT TO PROTECT INTERIOR. DESIGN OF SHAFT HAS CASTING ON EACH END THAT ANGLES UP 45 DEGREES WHICH WOULD MAKE CAPTURING FLUIDS EASY. SUBMITTER STATED THERE ARE NO PROVISIONS FOR DRAINAGE.

Source: SDR 2000ZZZX182
OTHER · 1999-12-08 Unresolved
ATA 6710

Part: JACKSHAFT — CORRODED (MAIN ROTOR)

TECHNICIAN PULLED LARGE AMOUNT OF RUST OUT OF INSIDE OF CYCLIC JACKSHAFT WHILE USING MAGNET TO RETRIEVE LOST SCREW. REMOVED JACKSHAFT AND INSPECTED. LARGE AMOUNT OF RUST RESIDUE AND PITTING OF JACKSHAFT, ESPECIALLY ON PILOT SIDE. MFG ALLOWS .4 MM CORROSION DAMAGE. ALMOST IMPOSSIBLE TO MEASURE DEPTH WITH CONVENTIONAL MEANS. WILL SEND TO BE ULTRASONICALLY TESTED. SUBMITTER SUSPECTED THIS ONE BEYOND LIMITS. REMOVED SAME P/N SHAFT OUT OF ANOTHER ACFT AND IT HAD SMALL AMOUNT OF SURFACE RUST. IT APPEARS THERE IS NO (OR INSUFFICIENT) PAINT TO PROTECT THE INTERIOR. DESIGN OF SHAFT HAS A CASTING ON EACH END THAT ANGLES UP 45 DEGREES WHICH WOULD MAKE CAPTURING FLUIDS EASY. THERE IS NO PROVISIONS FOR DRAINAGE.

Source: SDR 2000ZZZX276
OTHER · 1999-01-14 Unresolved
ATA 3421

Part: GYRO — FAILED (COCKPIT)

ATTITUDE GYRO WILL NOT CAGE. VERY ERRATIC. REMOVED AND REPLACED. (X)

Source: SDR 20000406SH024