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NTSB Report

July 3, 2008 · Roof Curtis Hawk P6E · N386PE

Iowa City, IA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 3, 2008
Injury Outcomes
1 injury (1 serious injury)
Location
Iowa City, IA
Aircraft
Roof Curtis Hawk P6E
Tail Number
N386PE
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
CHI08LA189

The pilot reported that during the takeoff in his homebuilt replica of a Curtis Hawk P6E, the engine suddenly lost power. He stated that the airplane was equipped with a backup ignition and a backup electric fuel pump. He stated that he was in the process of switching from the primary systems to the backup when he inadvertently stalled the airplane. He stated that there were no deficiencies in the flight control system of the airplane. A fire ensued and the pilot stated that it was his belief that the fire started before the airplane's impact with the ground. The airplane was powered by a converted Chevrolet 8 cylinder water-cooled engine. Examination of the engine subsequent to the accident revealed no deficiencies with the engine, but the accessories such as the carburetor and ignition systems had been destroyed by the fire. A broken fuel line fitting was found but no determination could be made as to whether the break occurred prior to impact or if it was a result of the impact.

NTSB Probable Cause

The loss of engine power for an undetermined reason and the pilot's subsequent failure to maintain airspeed, which resulted in an aerodynamic stall.

Full Narrative

On July 3, 2008, about 1755 central daylight time, an amateur-built Roof Curtis Hawk P6E, N386PE, piloted by a private pilot, sustained substantial damage when it impacted the ground following a loss of engine power during takeoff. A fire erupted. The 14 CFR Part 91 personal flight was operating in visual meteorological conditions without a flight plan. The pilot received serious injuries. The local flight was originating at the time of the accident. In a telephone interview, the pilot stated that he was hospitalized for about 60 days after the accident. He reported that during the takeoff in his homebuilt replica of a Curtis Hawk P6E, the engine suddenly quit. He stated that the airplane was equipped with a backup ignition and a backup electric fuel pump. He stated that he was in the process of switching from the primary systems to the backup when he inadvertently stalled the airplane. He stated that there were no deficiencies in the flight control system of the airplane. The pilot stated that it was his belief that the fire started before the airplane's impact with the ground. The airplane was powered by a converted Chevrolet 8 cylinder water cooled engine. According to the pilot/builder, subsequent to the accident he disassembled the engine. He stated that the engine itself was intact and that he found no mechanical problems with it. He said that the accessories such as the carburetor and ignition systems had been destroyed by the fire. He stated that he did find a fuel fitting that was not fire damaged. It had broken off at the boss but he could not determine whether the fitting had broken off prior to impact or if it was a result of the impact.

Flight

Event TypeAccident
Event Time17:55 CDT
Nearest AirportIowa City Municipal Airport (0nm)
Runway30
Runway Length3900 ft
Runway Width150 ft
Flight Plan FiledNone
Aircraft FireUnknown
Aircraft ExplosionNo

Aircraft

AircraftRoof Curtis Hawk P6E
Tail NumberN386PE
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsChevrolet · 383 · Reciprocating · 250
Seats2

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 64 · None · Serious

Conditions

ConditionsVMC
LightDaylight
Wind50° @ 7 kt
Visibility10 sm
CeilingBroken clouds 6500 ft
Temperature / Dew Point54
Altimeter30.00 inHg
Observation Time22:52
Weather SourceWFAC

Appendix: Source Data