BFO93LA171

NTSB accident investigation · Piper PA-28-180 · Byfield, MA · September 11, 1993

Accident · Minor injuriesLimited investigationFinal report
Date
September 11, 1993, 13:10 local (17:10 UTC)
Place
Byfield, MA
Injuries
1 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N4898TPiper PA-28-180
Weather
Visual (VMC) · Day
Status
Completed · report October 20, 1994
Report
Approved by Office Director
FAA report
19930911033939A
Case key
8817

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

Loss of engine power during climb for undetermined reasons.

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 undeterminedCause
Forced landingDescent - emergency
In flight collision with objectLanding
Object - tree(s)

Analysis

The pilot reported that he had completed his pre-takeoff and run-up checks successfully. He was taking off from a private field, and as the airplane was about 250 feet above the ground the RPM dropped from full RPM to idle RPM. He tried to restart the engine, but he was unsuccessful. He stated that he pulled back on the yoke to cushion the impact as the airplane struck some pine trees during the forced landing. There were several witnesses who heard the airplane's engine sound intermittently during takeoff before it impacted the trees. The FAA examined the airplane and reported that the left and right fuel tanks contained 25 gallons and 5 gallons respectively. The fuel selector was on the left tank.

Factual narrative

On Saturday, September 11, 1993, at 1310 eastern daylight time, N4898T, a Piper PA-28-180, owned and operated by Arthur Allen of Byfield, Massachusetts, collided with trees during a power-off forced landing at a private airstrip in Byfield, Massachusetts. Visual meteorological conditions prevailed and a flight plan was not filed. The certificated private pilot, the sole occupant, received minor injuries. The airplane was destroyed. The personal flight was conducted under 14 CFR 91 and the intended destination was Lawrence, Massachusetts.

According to the pilot, he was taking off from a private airstrip when the engine lost power. He reported that the pretakeoff checks and run-up were completed successfully. He stated that he used 2 notches of flaps and the airplane was accelerated to climb speed of 80 knots. He reported that about 250 feet above the ground, the rpm dropped from full rpm to idle power. He tried to restart the engine, but he was unsuccessful. The right wing struck the chimney of a house and came to rest in the trees.

There were several witnesses who reported hearing the airplane's engine sound intermittently during the initial climb. The airplane was examined by the FAA and the investigation revealed that the left and right fuel tanks contained 25 gallons and 5 gallons respectively. The fuel selector was found selected to the left tank.

Aircraft

Registration
N4898T
Reported as
Piper PA-28-180
Category
Airplane
Serial number
28-7205220
Airframe hours
2,824
Engine
Lycoming IO-360-A3A, 180 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Operator
Arthur G Allen
Registered owner
Arthur G Allen
Airworthiness certificate
Standard, Normal
Last inspection
Annual · August 1, 1993 · 13 hours before
Airport
NONE · Manter Field, runway 5, 1,700 × 25 ft, macadam

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
46
Certificate
Private
Airplane ratings
Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
1,119 total · 1,059 in this make and model · 1,063 as pilot in command · 29 in the last 90 days · 12 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
320° at 10 knots, gusting 20
Visibility
25 statute miles
Lowest ceiling
3,000 ft broken
Temperature
68 °F
Altimeter
29.00 inHg
Observed at
BVY, 10 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.