N176TW

BEECH E-90 · 1974 · Fixed-wing multi-engine · 2 engines · 10 seats · Valid Registration

Registered owner: SIERRA AMERICAN CORPORATION, DE (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Ameristar Jet Charter, Inc. (HAEA)Certificate holderMatched by certificate designator
Ameristar Jet Charter, Inc. (HAEA)Operatoron 2019-06-12Operator named in NTSB report

Accident & incident history

Accident · 2019-06-12 Operator named in NTSB report
Beech E90 No injuries Part 91Ameristar Jet Charter, Inc.

Operated by Ameristar Jet Charter, Inc. (per NTSB report)

Source: NTSB case CEN19LA166

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, 2015-06-02 – 2025-07-31.

SMOKE/FUMES/ODORS/SPARKS; WARNING INDICATION · 2025-07-31 Matched by certificate designator
ATA 7931

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 11,748 hrs · 10,961 cycles

DEPARTED GYH-ADS, AT FL180 PILOT NOTED SPARKS BY THE RT ENGINE AND THEN THE OIL PRESSURE WARNING LIGHT ACTIVATED AND PRESSURE GAUGE SHOWED 0. ENGINE WAS SHUTDOWN, ATC CONTACTED AND PERFORMED AN UNSCHEDULED LANDING AT THE NEAREST AIRPORT.

Source: SDR 2025F00171
INFLIGHT SEPARATION · 2019-06-12 Matched by certificate designator
ATA 3213

Part: AXLE — MISSING (RT MLG) · airframe 11,424 hrs · 10,715 cycles

ON DEPARTURE FROM KGVT THE CREW HEARD A NOISE FROM THE RH WING AREA, NOT SURE WHAT IT WAS THEY LEFT THE GEAR DOWN AND LOCKED AND PERFORMED A FLY BY THE TOWER AND DETERMINUED THE RH M/L/G PISTON/AXLE ASSEMBLY WAS MISSING. THE AIRCRAFT WAS FLOWN TO KAFW WHERE THE CREWED PERFORMED AN EMERGENCY LANDING.

Source: SDR HAEA20190614001
OTHER · 2015-06-02 Matched by certificate designator
ATA 2720

Part: RUDDER MAST — DAMAGED (RUDDER) · airframe 11,116 hrs · 10,389 cycles

DURING PHASE 1 ACFT INSPECTION, DISCOVERED THE RUDDER TO BELL CRANK RT ATTACH BOLT MISSING. FURTHER INVESTIGATION REVEALED THE BOLT HAD FAILED. AN INSPECTION OF THE RUDDER TORQUE TUBE WAS CONDUCT & IT WAS NOTED THAT THE ATTACH HOLES OF THE BELL CRANK & RUDDER WERE ELONGATED. PARTS MENTIONED WILL BE REPLACED WITH NEW & AS A PRECAUTION REPLACING THE UPPER & CTR RUDDER HINGE & HARDWARE. NO FURTHER ACTION REQUIRED.

Source: SDR HAEA2015040500231