Bidzy Ta Hot Aana Piper PA 32R-300 accident
Piper PA 32R-300 · Accident: electrical system malfunction/failure en route
From Shageluk Airport (SHX) to Nikolai Airport (FSP)
Event
- NTSB case
- ANC17LA014
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- Charter & commuter
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Piper PA 32R-300
- Aircraft type
- Piper PA-32
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N4352F
- Operator
- Bidzy Ta Hot Aana
- Onboard fatalities
- Unknown
- Route
- From Shageluk Airport (SHX), SHAGELUK, AKTo Nikolai Airport (FSP), NIKOLAI, AK
- Aircraft age
- About 40 years (built 1976)
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 135: Air Taxi & Commuter
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · descent
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Electrical system malfunction/failure
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Minor
Cause areas
- Aircraft › Aircraft systems
- Environmental issues › Conditions/weather/phenomena
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The on-demand passenger flight was approaching its destination airport when the commercial pilot noted that the two main landing gear extended, but the nose landing gear did not extend and lock. The pilot diverted to a larger airport, where ground personnel verified that the nose landing gear was not down and locked even after the pilot completed the manual gear extension procedure. The pilot elected to land the airplane with the engine off, and he stated that the touchdown was uneventful. He held the airplane's nose off the runway for several hundred feet; the left main landing gear then collapsed and the nose wheel extended. The airplane slid about 200 ft before coming to rest. A witness reported that the touchdown was smooth and when the left main landing gear collapsed, the airplane gradually slowed to a stop on the runway.
An examination of the airplane revealed that the alternator became inoperative during the flight, and, due to the cold temperatures, the battery was unable to accommodate the electrical load required by the system. In addition, the grease on the nosewheel was thick, which, combined with the cold temperatures, can increase its viscosity and reduce its effectiveness. Because the nose landing gear extends into the relative wind direction, it would be more difficult for it to extend and lock with the low battery power and increased viscosity of the grease. Further, because the landing gear was not in the "up" position when the emergency extension control was activated, the hydraulic fluid had already been released, thus rendering the emergency procedure ineffective. After landing and with a reduction in the relative wind, the gear was able to lock in place; however, the reason for the collapse of the left main landing gear could not be determined. When the alternator and battery were replaced, the airplane was placed on jacks and all three landing gear actuated as designed.
A review of the passenger's injuries revealed that the fracture of the transverse process of L2 vertebrae was "age-indeterminate," which means that it could not be definitively determined when the injury occurred.
Probable cause
The failure of the nose landing gear to extend and lock due to the failure of the alternator and reduced battery power due to the cold ambient temperature, which prohibited the electrically-driven hydraulic pump from supplying adequate hydraulic pressure to extend the nose landing gear. The cause of the left main landing gear collapse could not be determined, as there were no postaccident anomalies or malfunctions found when the landing gear was actuated following replacement of the alternator and battery.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ANC17LA014
- Event ID
- 20161221X32443
- Case number
- ANC17LA014
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: local date, investigation status. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 2016-11-21.
- API snapshot SHA-256: 7d7b432d39c5598d5532f3844ac353167af8ff8f80630487819bfba21391c6ff; retrieved 2026-09-16T04:54:36.290Z.