N26842

Substantial
None

Piper J3C-65 S/N: 4229

Accident Details

Date
Saturday, June 19, 1999
NTSB Number
LAX99LA222
Location
ELKO, NV
Event ID
20001212X19033
Coordinates
40.950416, -115.790908
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's failure to reject the takeoff after noting that the engine would not produce takeoff power.

Aircraft Information

Registration
N26842
Make
PIPER
Serial Number
4229
Engine Type
Reciprocating
Year Built
1940
Model / ICAO
J3C-65 J3
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BLAIR PARK R
Address
PO BOX 728
Status
Deregistered
City
ELKO
State / Zip Code
NV 89803-0728
Country
United States

Analysis

On June 19, 1999, at 1400 hours Pacific daylight time, a Piper J3C-65, N26842, impacted terrain after takeoff from the Elko Muni-J.C. Harris Field, Elko, Nevada. The airplane, operated under 14 CFR Part 91, sustained substantial damage. The commercial pilot/owner, the sole occupant, was not injured. Visual meteorological conditions existed for the local area personal flight and no flight plan was filed.

The pilot stated that the airplane had received an annual inspection in June 1999. Prior to initial takeoff, the airplane was taxi tested for about 2 hours, and the engine started easily and ran smoothly at the lower rpm setting.

On the run-up before takeoff, the pilot performed the magneto check with no discrepancies noted. During the takeoff roll, the pilot noted that the engine did not produce full power. On the initial climb he noted a further loss of power and decay in airspeed. He stated that he thought there was something wrong with the engine because the rpm would not go above 1,600; however, he elected to continue the takeoff. After becoming airborne there was a further loss of airspeed. He attempted to turn back to the runway for landing, but as he was making the crosswind turn to the downwind leg, the left wing stalled and the aircraft "fell 50 feet to the ground."

In the pilot's written statement to the Safety Board, he indicated that he should have aborted the takeoff sooner.

An airworthiness inspector from the Federal Aviation Administration (FAA) inspected the airplane. The FAA inspector stated that this was the first flight after an annual inspection had been performed. The inspector further noted that the engine never fully developed power and the pilot elected to continue the takeoff resulting in a further loss of engine power and subsequent crash. During the engine inspection he observed the number 2 cylinder compression ratio was 14/80 with excessive exhaust and intake valve leaks, and the number 3 cylinder compression ratio was 20/80 with an excessive intake valve leak. No further discrepancies were noted.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX99LA222