ANC07FA037 · Cessna 170
Cessna 170 · Accident: total loss of engine power (non-mechanical) during initial climb
From Wolf Lake Airport (4AK6) to an unrecorded destination
Event
- NTSB case
- ANC07FA037
- 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
- 1 · 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
- 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
Cessna 170
- Aircraft type
- Cessna 170
- 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
- N4217V
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Wolf Lake Airport (4AK6), Wasilla, AKTo not recorded
- 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 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
- Initial climb
- 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
- Total loss of engine power (non-mechanical)
- Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
- Fuel contamination; Tree(s)
- 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
- Fluid, fuel › Contamination
- Pilot in command › Aircraft preflight, inadequate
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The private pilot departed from a private airstrip on a personal flight. The airplane climbed to about 200 feet, and then lost power. The pilot made a right turn toward the north, and descended toward a residential area adjacent to the airport. The propeller was not turning just prior to the crash. The airplane clipped the top of a large tree, about 300 feet from a residence, and collided with several additional trees before impacting the ground. The fuel tanks were breached during the accident, but the left inboard tank, when examined at the scene, was nearly full of blue colored fuel. The right inboard tank contained a small amount of fuel. When tested with water detection paste, each tank contained small amounts of water. Fuel was present in the gascolator, and was obtained by opening the forward drain fitting. The aft drain fitting could not be opened due to rust and corrosion. The gascolator also contained sediment, a small amount of water droplets, corrosion around the base of the gascolator screen and the gascolator base, and small globs of a white, opaque, silicone-like grease material. Small globs of the grease material were also found in the carburetor inlet screen, and in the check valve between the gascolator and the carburetor. The interior of the fittings of fuel supply line from the gascolator and the carburetor had some corrosion. The engine was removed from the airframe and placed on an engine test stand. A replacement carburetor was installed, along with a wooden "club" test propeller. The engine was started and produced full rated rpm. The accident carburetor was placed on a test stand and it held normal fuel pressure without leaking. The carburetor bowl contained dirt, sediment, and small amounts of water. The accelerator pump functioned properly. The floats operated normally without binding. The airplane had been flown about 22 hours in the previous 2 years.
Probable cause
A total loss of engine power during takeoff initial climb due to fuel contamination, and the pilot's inadequate preflight inspection.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record ANC07FA037
- Event ID
- 20070510X00548
- Case number
- ANC07FA037
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
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. 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: ed2fb2c46e88e000412a8d37c9d822cda71eb49ab8e794e50b79da4f67c72b9c; retrieved 2026-09-20T16:39:56.703Z.