SEA96LA223

NTSB accident investigation · Piper PA-28-235 · Paisley, OR · September 25, 1996

Accident · Serious injuriesLimited investigationFinal report
Date
September 25, 1996, 10:00 local (17:00 UTC)
Place
Paisley, OR
Injuries
1 serious, 2 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N8822WPiper PA-28-235
Weather
Visual (VMC) · Day
Status
Completed · report July 23, 1999
Report
Approved by Office Director
Case key
45715

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

Total loss of engine power secondary to geartrain failure.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfCruise
Engine assembly,gear - failure,totalCause
Forced landingEmergency descent/landing
Terrain condition - none suitableFactor

Analysis

The pilot stated that while in cruise flight over unsuitable terrain, the engine lost power. A forced landing was performed to a heavily wooded area. A post-crash teardown of the engine revealed geartrain failure. The engine's time since overhaul was approximately 2,400 hours. According to Lycoming service data, recommended time between overhaul for this engine was 2,000 hours.

Factual narrative

On September 25, 1996, about 1000 Pacific daylight time, a Piper PA-28, N8822W, registered to and operated by the private pilot as a 14 CFR Part 91 personal flight, was substantially damaged when it collided with terrain while attempting an emergency landing. Visual meteorological conditions prevailed and no flight plan was filed. The pilot and one passenger sustained minor injuries while the third passenger sustained serious injuries. The flight originated from the Crescent Lake Airport, Crescent Lake, Oregon approximately 20 minutes prior to the accident.

During a telephone interview, the pilot stated that while in cruise configuration he experienced a loss of engine power and attempted an off-field landing. The pilot also stated that due to the nature of the terrain he was unable to reach a suitable landing site and subsequently landed in a heavily wooded area, 30 miles south of Paisly, Oregon.

The pilot stated that a post-crash teardown of the engine revealed geartrain failure. The engine's time since overhaul was approximately 2,400 hours. According to Lycoming service data, recommended time between overhauls for this engine is 2,000 hours.

The FAA received an anonymous report of the accident and notified the NTSB on January 19, 1999. The pilot stated that he assumed the NTSB had already been notified by local and state officials.

Aircraft

Registration
N8822W
Reported as
Piper PA-28-235
Category
Airplane
Serial number
28-10320
Engine
Lycoming O-540, 235 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Markus K. Ward
Airworthiness certificate
Standard, Utility; Standard, Normal
Departed
5S2 · Crescent Lake, OR
Destination
LKV · Lakeview, OR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
51
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Unknown
Seat
Left
Flight hours
900 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
300° at 30 knots
Visibility
100 statute miles
Lowest ceiling
None
Temperature
64 °F