SEA07LA071

NTSB accident investigation · Piper PA-28-140 · Crescent Lake, OR · March 6, 2007

Accident · Serious injuriesLimited investigationFinal report
Date
March 5, 2007, 16:00 local (Mar 6, 2007, 00:00 UTC)
Place
Crescent Lake, OR
Injuries
2 serious
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N5547FPiper PA-28-140
Weather
Visual (VMC) · Day
Status
Completed · report June 27, 2007
Report
Approved by Office Director
Parties
Portland FSDO
FAA report
20070305003259A
Case key
65386

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

The loss of a significant amount of engine power for undetermined reasons. Factors include no suitable place in which to make an emergency landing, and densely forested, mountainous/hilly terrain.

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 powerManeuvering
Reason for occurrence undeterminedCause
Forced landingEmergency descent/landing
In flight collision with terrain/waterEmergency descent/landing
Terrain condition - none suitableFactor
Terrain condition - mountainous/hillyFactor
In flight collision with objectEmergency descent/landing
Object - tree(s)Factor

Analysis

The pilot, who was flying between 800 and 1,000 feet above the trees in mountainous/hilly terrain, decided to add power and start a climb up the valley he was in. Just as he added power, the aircraft's engine rpm dropped from about 2,300 to about 1,800 to 1,900 rpm. At that point, he applied full carburetor heat, moved the mixture to full rich, and checked to make sure the fuel selector was in the correct position. According to both the pilot and his passenger, these remedial actions did not help the situation, and the engine rpm stayed near 1,800 rpm. Because the terrain was rising and the aircraft could not maintain altitude, and because they were already very low, the pilot made the decision to attempt a forced landing in the densely forested snow-covered mountainous terrain. While attempting the landing, the aircraft struck a number of trees, and then impacted the snow-covered ground in an inverted position. A post-accident inspection of the airframe, systems, and engine did not reveal evidence of any pre-impact anomalies or malfunctions that would have precluded the engine from operating at full power.

Factual narrative

On March 5, 2007, approximately 1600 Pacific standard time, a Piper PA-28-140, N5547F, collided with trees during an attempted forced landing about 10 miles northwest of Crescent Lake, Oregon. The commercial pilot and his passenger received serious injuries, and the aircraft, which was owned by K & J Capital, LLC., and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 personal pleasure flight, which departed Eugene, Oregon, about 45 minutes prior to the accident, was being operated in visual meteorological conditions. No flight plan had been filed. Reportedly, the pilot intended to return to Eugene after flying around the Crescent Lake area.

According to the pilot, he was flying between 800 and 1,000 feet above the trees in mountainous/hilly terrain, when, because of rising terrain, he decided to add power and start a climb up the valley he was in. Just as he added power, the aircraft's engine rpm dropped from about 2,300 to about 1,800 to 1,900 rpm. At that point, according to the pilot, he applied full carburetor heat, moved the mixture to full rich, and checked to make sure the fuel selector was in the correct position. According to both the pilot and his passenger, these remedial actions did not help the situation, and the engine rpm stayed near 1,800. Because the terrain was rising and the aircraft could not maintain altitude, and because they were already very low, the pilot made the decision to attempt a forced landing in the densely forested mountainous terrain. While attempting the landing on the snow-covered terrain, the aircraft struck a number of trees, and then impacted the ground in an inverted position.

A post-accident inspection of the airframe, systems, and engine did not reveal evidence of any pre-impact anomalies or malfunctions that would have precluded the engine from operating at full power.

Aircraft

Registration
N5547F
Reported as
Piper PA-28-140
Category
Airplane
Serial number
24810
Airframe hours
6,487
Engine
Lycoming O-320-E2A, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Justin J. Hall
Registered owner
K & J Capital LLC
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 1, 2006 · 23 hours before
Departed
KEUG · Eugene, OR
Destination
KEUG · Eugene, 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
21
Injuries
Serious
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
February 1, 2007
Seat
Left
Flight hours
573 total · 275 in this make and model · 485 as pilot in command · 43 in the last 90 days · 16 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
11,000 ft overcast
Temperature
61 °F, dew point 28 °F
Altimeter
30.09 inHg
Observed at
KRDM, 55 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.