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SEA06LA053 · Cessna 150

16 Feb 2006 · White Salmon, WA, United States

Cessna 150 · Accident: total loss of engine power (non-mechanical) during initial climb

From Port Elsner Airport (75WA) to Port Elsner Airport (75WA)

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Event

NTSB case
SEA06LA053
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
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 150

Aircraft type
Cessna 150
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
N5611E
Operator
Unknown
Onboard fatalities
Unknown
Route
From Port Elsner Airport (75WA), White Salmon, WATo Port Elsner Airport (75WA)
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; Stall/spin
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Pilot in command › Aircraft control, not maintained
  • Pilot in command › Stall/spin, inadvertent

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

NTSB narrative

A witness said she heard a loud engine noise and turned to see a bright yellow airplane taking off. Seconds later, she said the noise stopped, and she turned to see the airplane "crash." The airplane was not equipped with shoulder harnesses; the pilot was critically injured with a broken eye socket, broken cheekbone, bruises on the brain, and possible broken vertebrae. The Sheriff's Deputy said that he arrived on scene approximately 30 minutes after the accident. He said "the temperature was below freezing, the sun was shining and a heavy layer of frost was on the ground. Frost was melting off the aircraft and water was dripping onto the ground." He said it had rained heavily the past several days and he was told that the airplane had been parked outside. On February 17, 2006, a FAA inspector and a representative of the airplane's manufacturer went to the scene and found the airplane approximately 500 feet west of the departure end of runway 17 of a private grass 1,600 foot long airstrip. They found the fuselage nose down with both wings bent forward and compression damage to both outboard leading edges. The right wing root attachment points had separated. The wing strut attachment points were secure. The empennage was broken aft of the cabin area, and rotated 90 degrees toward the right wing; the right horizontal stabilizer was holding the back portion of the fuselage off the ground. The airplane had an STC engine conversion to a Lycoming O-320, 150 horse powered engine. Water was found in the carburetor and approximately 1-2 tablespoons of frozen water were found in the fuel strainer. Minimal rotational signatures were noted on the propeller. Due to the serious nature of the pilot's injuries, he was not interviewed and a written statement was never obtained. FAA pilot medical application records indicate that the pilot had more that 23,000 hours of flight experience.

Probable cause

The pilot's failure to maintain aircraft control and the subsequent inadvertent stall/spin to the ground. Contributing factors were the inadequate preflight by the pilot, and the airplane's fuel contamination by water.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record SEA06LA053
Event ID
20060227X00243
Case number
SEA06LA053
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: 47b0fd993d8a667a1b59b29b9e3dfbf7e58f78ca2391e5bf327780809fbcafca; retrieved 2026-09-21T09:00:08.603Z.