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Frontier Flying Service Beech 1900D accident

22 Oct 2000 · Bethel, AK, United States

Beech 1900D · Accident: loss of control on ground/water during landing

From Ted Stevens Anchorage International Airport (ANC) to Bethel Airport (BET)

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Event

NTSB case
ANC01FA011
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
0
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
Airline
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

Beech 1900D

Aircraft type
Beechcraft 1900
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
N575D
Onboard fatalities
Unknown
Route
From Ted Stevens Anchorage International Airport (ANC), Anchorage, AKTo Bethel Airport (BET), Bethel, AK
Aircraft age
Not recorded
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 121: Air Carrier
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
Landing · landing roll
First occurrenceThe 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
Loss of control on ground/water
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Flightcrew › Directional control, not maintained

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The Beech 1900D airplane was landing on a dry, paved, 6,398 feet long by 150 feet wide runway, which required a correction for a left crosswind. During the landing roll, and after activation of the Decoto power steering system, the airplane suddenly veered to the right. The airplane continued off the right side of the runway, into an area of soft terrain, and the nose landing gear collapsed. In a written statement to the NTSB, the captain of the accident airplane wrote, in part: "Because of the strong winds, it was necessary to engage the power steering to assist with the left turn, a normal procedure. As I engaged the power steering, which was armed by the first officer at my request, the aircraft executed an immediate right turn of approximately 45 degrees. Both the first officer and myself attempted to counter-respond the event with full left rudder and maximum left braking. All attempts were unsuccessful, causing us to exit the runway, collapsing the nose gear, and sheering the props." In the presence of NTSB and FAA investigators, extensive tests were conducted on the Decoto power steering system, and associated components. No preaccident mechanical anomalies were noted with the system. The Flight Data Recorder revealed that the crew activated the power steering system with a derived ground speed of about 40 to 50 knots. The Decoto Power Steering System flight manual supplement states: "Use of power steering is limited to taxi operations only."

Probable cause

The flight crew's failure to maintain directional control during the landing roll. A factor associated with the accident was the crew's failure to follow appropriate procedures.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ANC01FA011
Event ID
20001212X22101
Case number
ANC01FA011
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (5)
  • 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: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: e9d89f6ea97722d93aa555f2be0f03ab4573f69491250f857c2225fe0e952faf; retrieved 2026-09-18T16:21:37.877Z.
  • The NTSB's operator name is blank for N575D; the operator shown is the name the NTSB's other records give its FAA operator code, FFSA.