N5829D

PIPER PA 46-350P · 2018 · Fixed-wing single-engine · 1 engine · 6 seats · Valid Registration

Registered owner: COUNTY OF HENRICO VA, VA (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
OFFSHORE LOGISTICS, INC.Operatoron 1997-03-04Operator named in NTSB report

Accident & incident history

Accident · 1997-03-04 Operator named in NTSB report
Bell 206L-1 Minor injury Part 135OFFSHORE LOGISTICS, INC.

Operated by OFFSHORE LOGISTICS, INC (per NTSB report)

Source: NTSB case FTW97LA114

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, 1995-05-02 – 1995-08-07.

OTHER · 1995-08-07 Unresolved
ATA 6300

Part: DRIVESHAFT — DAMAGED (M/R INPUT)

INPUT DRIVESHAFT REMOVED DUE TO FIRE IN ROTOR BRAKE AREA. SUSPECT CAUSE ROTOR BRAKE MALFUNCTION. DRIVESHAFT WAS SCRAPPED DUE TO HEAT DAMAGE.

Source: SDR 95ZZZX4417
OTHER · 1995-05-22 Unresolved
ATA 6230

Part: LINK IDLER — WORN (PYLON)

DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. TT ON WORN PARTS 534.5 HOURS.

Source: SDR 95ZZZX2778
OTHER · 1995-05-22 Unresolved
ATA 6230

Part: LINK ASSY — WORN (PYLON)

DAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. TT ON WORN PARTS 534.5 HOURS.

Source: SDR 95ZZZX2777
INADEQUATE Q C · 1995-05-02 Unresolved
ATA 6210

Part: BLADE — MISMANUFACTURED (M/R)

DURING INSPECTION, SPAR OBSERVED DRILLED AT TIP WEIGHT INSTALLATION LOCATIONS. TIP WEIGHT BLOCK AREA, HOLES DRILLED THROUGH TO SPAR INNER SKIN AT TIME OF MANUFACTURE.

Source: SDR 95ZZZX2798