BFO94LA004

NTSB accident investigation · Piper PA-28-161 · Manassas, VA · November 8, 1993

Accident · No injuriesLimited investigationFinal report
Date
November 8, 1993, 10:38 local (15:38 UTC)
Place
Manassas, VA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N8223TPiper PA-28-161
Weather
Visual (VMC) · Day
Status
Completed · report August 17, 1994
Report
Approved by Office Director
FAA report
19931108044289A
Case key
8864

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 total engine power for undetermined reasons. A factor in the accident was the lack of suitable terrain to enable the completion of a power-off forced landing.

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 powerApproach - vfr pattern - base leg/base to final
Reason for occurrence undeterminedCause
Forced landingDescent - emergency
In flight collision with objectDescent - emergency
Object - tree(s)
Terrain condition - none suitableFactor
On ground/water collision with objectLanding - roll
Object - tree(s)

Analysis

While on the airport's base leg of the traffic pattern, the airplane's engine lost total power. The pilot attempted an emergency landing to a field. The airplane's glide did not allow it to make the field and it collided with a tree prior to touchdown. The airplane sustained damage to both wing spars and wing structure. The propeller blades were also bent aft. Post accident examinations of the airframe and engine did not reveal any anomalies. The engine was restarted and no anomalies were noted.

Factual narrative

On Monday, November 8, 1993, at 1038 eastern standard time, a Piper PA-28-161, N8223T, owned and operated by Dulles Aviation located in Manassas, Virginia, and piloted by Eduardo A. Bonacic-Doric of Vienna, Virginia, lost total engine power while in the Manassas Airport's traffic pattern. The pilot made a forced landing in a field. The pilot was not injured. The airplane was substantially damaged. Visual meteorological conditions prevailed at the time of the accident. The local personal flight was conducted under 14 CFR Part 91.

The pilot reported that he was cleared to land the airplane on runway 16R. He stated that there was a Cessna 152 that was cleared to land before his airplane, so he extended the downwind leg of the traffic pattern. The pilot stated, "When I turned into base leg I reduced the power after applying hot air to the carburetor. The engine quit running and I reported to the tower that I was in [an] emergency [situation] and [was trying] to reach the runway, but [because] I did not have enough altitude to reach the runway, I tried to land on a 70 yards long piece of land." The pilot stated that during the emergency descent, the airplane contacted a tree prior to touchdown. The pilot said that the airplane touched down and rolled into trees which stopped the airplane.

Examination of the airplane at the accident site revealed that the fuel tanks were full and no fuel contaminates were found. The fuel selector was positioned on the left fuel tank. The mixture and throttle were in the full aft position. According to a Federal Aviation Administration safety inspector, the pilot reported to him that once the airplane came to rest, "...I [the pilot] shut everything off prior to exiting the airplane."

The accident was located about one quarter mile north of the airport. The airplane sustained damage to both wing leading edges and wing spars. The right fuel tank was breached. The propeller blades were bent aft and the bottom of the fuselage was damaged. Fuel was drained from each wing fuel tank for safe transport back to the airport.

The airplane was removed from the accident site and stored in a hangar at the Manassas Airport. Fuel was put back into the airplane's left fuel tank and the engine was started. The engine ran at full power and at idle. The left and right magneto's were selected and a reduction in engine revolutions per minute was observed. No engine anomalies were noted.

Aircraft

Registration
N8223T
Reported as
Piper PA-28-161
Category
Airplane
Serial number
28-8216170
Airframe hours
5,750
Engine
Lycoming O-320-D3G, 160 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Dulles Aviation Inc.
Registered owner
Dulles Aviation Inc.
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · October 19, 1993 · 34 hours before
Airport
HEF · Manassas Municipal Arpt, runway 16R, 3,703 × 100 ft

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
67
Certificate
Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
6,599 total · 96 in this make and model · 6,599 as pilot in command · 4 in the last 90 days · 2 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
40° at 4 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
43 °F, dew point 28 °F
Altimeter
30.00 inHg
Observed at
HEF, 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.