ANC95LA001

NTSB accident investigation · Piper J5C · Anchorage, AK · October 4, 1994

Accident · No injuriesLimited investigationFinal report
Date
October 3, 1994, 16:30 local (Oct 4, 1994, 00:30 UTC)
Place
Anchorage, AK
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N38532Piper J5C
Weather
Visual (VMC) · Day
Status
Completed · report June 29, 1995
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19941003048389A
Case key
2603

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 engine power for undetermined reasons and the lack of a suitable forced landing area.

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 powerClimb
Reason for occurrence undetermined
Forced landingEmergency descent/landing
In flight collision with objectEmergency descent/landing
Terrain condition - none suitableCause

Analysis

The pilot stated that 2 minutes after takeoff he reduced power to 2400 RPM. The engine decelerated to 1000 RPM by itself and then stopped producing power completely. He selected a road for a forced landing but during the approach a vehicle pulled out onto the road. During the pull up to avoid the vehicle the aircraft hit powerlines. Examination of the engine did not reveal any mechanical irregularities. The position of the fuel valve was undeterminable because the fire department had placed the fuel selector in the off position.

Factual narrative

On October 3, 1994 at 1630 Alaska daylight time, a wheel equipped Piper PA-18 airplane, N38532, registered to and operated by the pilot, experienced a loss of power after takeoff and was forced to land in a field near Merrill Field, Anchorage, Alaska. The personal flight was departing Merrill Field for a local flight and no flight plan was filed. Visual meteorological conditions prevailed. The pilot, the sole occupant, was not injured and the airplane was substantially damaged.

According to the pilot, 2 minutes after takeoff he reduced the power to 2400 RPM. The engine decelerated by itself to 1000 RPM, hesitated and then stopped producing power completely. He applied carburetor heat and switched fuel tanks. He was unable to restart the engine. The pilot attempted to glide to a road. During the glide a vehicle pulled out onto the road and the pilot had to pull up to miss the vehicle. He was unable to lower the nose quickly enough to land before striking the wires at the far end of the selected forced landing area. The airplane struck the wires and "cartwheeled" to a stop.

On scene examination of the engine by an FAA Inspector showed no external damage to the engine. Internal mechanical continuity was established and the engine rotated freely. The airplane's fuel system contained fuel which was blue in color. The position of the fuel selector during the takeoff and short flight was undeterminable because the fire department turned the fuel selector off. According to the FAA Inspector, he was unable to determine a mechanical reason for the loss of power.

Aircraft

Registration
N38532
Reported as
Piper J5C
Category
Airplane
Serial number
5-1394
Engine
Lycoming O-235-C1, 108 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Woodward, Paul
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 5, 1994 · 52 hours before

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
37
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
373 total · 245 in this make and model · 319 as pilot in command · 52 in the last 90 days · 5 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 8 knots
Visibility
50 statute miles
Lowest ceiling
6,500 ft broken
Temperature
52 °F, dew point 46 °F
Altimeter
29.00 inHg
Observed at
MRI, 1 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.

Other investigations on N38532 · 1

Matched to the same aircraft by N-number and date.