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SEA03LA176 · Mooney M20D

24 Aug 2003 · Hood River, OR, United States

Mooney M20D · Accident: partial loss of engine power (mechanical failure) during initial climb

From Ken Jernstedt Airfield (4S2) to Eugene Airport (EUG)

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Event

NTSB case
SEA03LA176
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

Mooney M20D

Aircraft type
Mooney M20
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
N6619U
Operator
Unknown
Onboard fatalities
Unknown
Route
From Ken Jernstedt Airfield (4S2), Hood River, ORTo Eugene Airport (EUG), Eugene, OR
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
Partial loss of engine power (mechanical failure)
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
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

  • Engine assembly, cylinder › Low compression
  • Engine assembly, valve, intake › Leak

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's father (right seat), a commercial pilot with more than 2,000 hours in the accident aircraft, reported that the engine ran smoothly on the ground and an RPM check prior to takeoff yielded 2600 RPM. The takeoff roll on the 3,040-foot long asphalt runway seemed long with less than normal power to the flying pilot (left seat). The aircraft was rotated at 65 knots but settled back to the runway at which time the right seat pilot took control and established a shallow climb rate toward the rising terrain west of the airport. Both pilots felt that an aborted takeoff would result in an overrun into a grassy area containing vehicles and pedestrians. The flying pilot (right seat) then banked to avoid a large tree and the aircraft settled into the treetops eventually coming to rest inverted in a bog. Post-crash examination and test run of the engine revealed that the number one cylinder could develop no more than 25-35 pounds of compression. Further examination revealed the number one cylinder intake seat had dropped down out of its normally seated position at an angle preventing the valve from seating evenly during the compression stroke.

Probable cause

A power loss due to a mis-seated intake valve on the #1 cylinder resulting in leakage during the compression stroke and low compression. Contributing factors were the rising terrain and trees.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record SEA03LA176
Event ID
20030903X01447
Case number
SEA03LA176
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: db3ce0ff18f6312124a71126e1d3bb6a24a0cdf0259e5a84847642f2eb1a7e33; retrieved 2026-09-21T19:23:10.164Z.