N7353J

Substantial
Minor

Piper PA-28-140 S/N: 28-24704

Accident Details

Date
Sunday, September 27, 1998
NTSB Number
CHI98LA362
Location
IOWA CITY, IA
Event ID
20001211X11030
Coordinates
41.650775, -91.529747
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

A loss of engine power for undetermined reasons.

Aircraft Information

Registration
N7353J
Make
PIPER
Serial Number
28-24704
Engine Type
Reciprocating
Year Built
1968
Model / ICAO
PA-28-140 P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
OTTUMWA AIR INC
Address
409 N MILES
Status
Deregistered
City
FREMONT
State / Zip Code
IA 52561
Country
United States

Analysis

On September 27, 1998, at 1205 central daylight time, a Piper PA-28-140, N7353J, was substantially damaged during takeoff. The 14 CFR Part 91 flight was departing Iowa City, Iowa, en route to Maquoketa, Iowa. The pilot reported a loss of power during takeoff. The airplane descended into trees and impacted the ground. The private pilot and passenger received minor injuries. Visual meteorological conditions prevailed and no flight plan had been filed.

The pilot reported he had conducted his normal preflight and run-up checks. He departed runway 30. He reported that immediately after liftoff, the engine "seemed to lose a lot of its power." He reported that he applied carburetor heat and cycled the throttle to full power, but the engine did not regain power. He reported the residential area offered no open area to do an emergency landing, so he flew the airplane to a small opening between two houses. The airplane fuselage went between two apple trees. The wings were separated from the fuselage by the impact with the apple trees.

An Airworthiness Inspector from the Federal Aviation Administration inspected the airplane. The propeller exhibited minimal damage and chordwise scratching on one blade. The engine exhibited continuity to the accessory gearbox. The valve train operated normally and there was thumb compression on all cylinders. The carburetor evidenced no anomalies. The fuel from the wing tanks could not be examined for contamination since the fuel had spilled out of the tanks when wings separated from the fuselage. The inspector reported that no cause of the power loss could be found.

The engine run was conducted with the engine still on the airframe. The mechanic who performed the engine run reported the engine made full power at 2,450 RPM. He reported, "... the engine accelerated good. Both magnetos checked OK. Carburetor heat checked OK. I ran the engine with fuel selector on LH tank and that checked OK. I checked fuel selector on RH with air pressure and that checked OK."

The pilot reported that he switched the fuel selector to the fullest tank after he accomplished the engine run up prior to takeoff.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI98LA362