SEA02LA013

NTSB accident investigation · Piper PA-18-150 · Brewster, WA · November 13, 2001

Accident · No injuriesLimited investigationFinal report
Date
November 13, 2001, 15:15 local (23:15 UTC)
Place
Brewster, WA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N5762APiper PA-18-150
Weather
Visual (VMC) · Day
Status
Completed · report February 20, 2002
Report
Approved by Office Director
Parties
FAA-FSDO
FAA report
20011113031019A
Case key
53764

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 NTSB’s determination of the probable cause, and any contributing factors.

The magneto was inadvertently switched off by the pilot during the climb. A tree was a factor.

Analysis

The pilot reported that this was the first flight after the aircraft had been completely restored. The start, taxi and takeoff were normal. During the climb, at about 150 feet AGL, the engine suddenly lost power. The pilot was unable to return to the airport, therefore he chose to land on a Highway that parallels the airport. The road was initially clear of traffic until a truck came over a rise. The pilot maneuvered the aircraft to the side of the road and just before touch down, the left wing struck a tree which spun the aircraft to the left. The main landing gear collapsed and the right wing contacted the surface. After the accident, the pilot immediately exited the aircraft, then returned to secure the cockpit when it was safe. The pilot found that the magneto switches, which are unguarded toggle switches located on the lower left side of the wall, were off. The pilot reported that he did not recall turning off the switches prior to exiting the aircraft. After the aircraft was moved back to the airport, the engine was started and run for several minutes with no evidence of a mechanical failure or malfunction noted.

Factual narrative

On November 13, 2001, at 1510 Pacific standard time, a Piper PA-18-150, N5762A, registered to a private individual and operated by the pilot as a 14 CFR Part 91 personal flight, collided with a tree and terrain following a loss of engine power shortly after takeoff from Anderson Field, Brewster, Washington. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft was substantially damaged and the commercial pilot, the sole occupant, was not injured.

The pilot reported during a telephone interview that this was the first flight after the aircraft had been completely restored. The start, taxi and takeoff were normal. The pilot reported that during the climb at about 150 feet above ground level, the engine suddenly quit without warning. The pilot attempted to return to the airport, but was unable, and therefore chose to land on Highway 97 that parallels the runway. The pilot stated that the highway was initially clear of traffic until a truck came over a rise. The pilot maneuvered the aircraft to the side of the highway, and just prior to touchdown, the left wing struck a tree which spun the aircraft to the left. The main landing gear collapsed and the right wing contacted the surface.

The pilot later reported to a Federal Aviation Administration Inspector from the Spokane, Washington, Flight Standards District Office that when the aircraft came to rest, he immediately exited the aircraft in case of fire. When it was determined safe, the pilot returned to the aircraft to secure the cockpit. During this time, the pilot found that the magneto switches were off. The pilot reported that he did not recall turning the switches off prior to exiting the aircraft. The unguarded toggle switches are located on the left lower side wall. In the Recommendation section of the attached Pilot/Operator Aircraft Accident Report Form 6120.1/2, of how this accident could have been prevented, the pilot stated, "magneto toggle switches relocated to overhead or inst. panel..."

After the aircraft was moved back to the airport, the engine was started and run for several minutes with no evidence of a mechanical failure or malfunction noted.

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 powerTakeoff - initial climb
Ignition system,magneto - switched offCause
Loss of engine powerEmergency landing after takeoff
On ground/water collision with objectEmergency landing
Object - tree(s)Factor

Aircraft

Registration
N5762A
Reported as
Piper PA-18-150
Category
Airplane
Serial number
18-5733
Airframe hours
2,233
Engine
Lycoming O-320-A2B, 150 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
David C. Smith
Registered owner
Michael J. Port
Airworthiness certificate
Standard, Normal
Last inspection
Annual · November 10, 2001 · 0.2 hours before
Departed
Brewster, WA

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
59
Injuries
None
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Last flight review
June 12, 2001
Seat
Front
Flight hours
29,300 total · 500 in this make and model · 28,000 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
130° at 3 knots
Visibility
6 statute miles
Lowest ceiling
3,300 ft overcast
Temperature
46 °F, dew point 41 °F
Altimeter
29.77 inHg
Observed at
OMK, 23 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.