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WPR22LA083 · Beech F33A

26 Jan 2022 · Williams, AZ, United States

Beech F33A · Accident: fuel related during takeoff

From H.A. Clark Memorial Field (CMR) to AO9 · Mohave Valley, AZ

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Narrative check · The NTSB narrative appears to contradict this record's departure or destination. Values are shown as recorded, not corrected; compare with the narrative.

Event

NTSB case
WPR22LA083
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
Event fatalities
Unknown
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
General aviation
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 F33A

Aircraft type
Beechcraft 33
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
N1HH
Operator
Unknown
Onboard fatalities
Unknown
Route Possible conflict
From H.A. Clark Memorial Field (CMR), Williams, AZTo AO9 · Mohave Valley, AZ
Aircraft age
About 47 years (built 1975)
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 91: General Aviation
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
Takeoff
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
Fuel related
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

  • Aircraft › Aircraft power plant
  • Personnel issues › Action/decision

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

NTSB narrative

The pilot reported that, during previous flights, he had observed overheating of two of the engine cylinders, and activation of the auxiliary fuel boost pump had worked to resolve the overheating. Shortly after takeoff on the accident flight, the pilot observed cylinder heating and activated the boost pump, after which the engine lost total power. The pilot performed a forced landing in an open desert field. The airplane landed hard and impacted vegetation during the landing roll, resulting in substantial damage to the airplane.

Data retrieved from the airplane’s engine monitoring system showed that the fuel flow rate increased from 23.4 gallons per hour (gph) to 28.7 gph, with a peak fuel flow of 30.8 gph, followed by a sudden decrease. The engine manufacturer recommended that the fuel flow setting should be between 23.2 – 24.9 gph. Both the pilot operating handbook for the airplane and a placard on the auxiliary boost pump indicated that the pump should be off during takeoff and only turned on in the event of a loss of fuel pressure.

It is likely that the pilot’s activation of the auxiliary fuel boost pump resulted in excess fuel being delivered to the engine during the initial climb, which resulted in the total loss of engine power.

A postaccident examination of the airframe and engine revealed no evidence of mechanical failures or malfunctions that would have precluded normal operation.

Probable cause

The pilot’s activation of the auxiliary fuel boost pump shortly after takeoff, which resulted in an excess amount of fuel to the engine and a total loss of engine power.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR22LA083
Event ID
20220126104557
Case number
WPR22LA083
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: investigation status, coordinates, cause areas. 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: a8d55266664ef58168701575865af2073e65b0374c0dcbf3c4eca1fc71eb75b9; retrieved 2026-09-16T14:54:51.935Z.