N4214H

Substantial
Minor

Piper PA-14 S/N: 14-101

Accident Details

Date
Wednesday, August 19, 1998
NTSB Number
ANC98LA123
Location
CHUGIAK, AK
Event ID
20001211X10744
Coordinates
61.410297, -149.170806
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The loss of engine power for an undetermined reason.

Aircraft Information

Registration
Make
PIPER
Serial Number
14-101
Engine Type
Reciprocating
Model / ICAO
PA-14 PA14
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-14

Registered Owner (Current)

Name
GRANGER ANDREW J
Address
1850 BASSETT ST APT 1010
City
DENVER
State / Zip Code
CO 80202-6195
Country
United States

Analysis

On August 18, 1998, about 2130 Alaska daylight time, a tundra tire equipped Piper PA-14 airplane, N4214H, sustained substantial damage during takeoff from the Birchwood Airport, Chugiak, Alaska. The airplane was being operated as a visual flight rules (VFR) local area personal flight under Title 14, CFR Part 91, when the accident occurred. The certificated private pilot, and the one passenger aboard received minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at the Birchwood Airport, about 2050.

During a conversation with the National Transportation Safety Board investigator-in-charge on August 19, the pilot reported that he had completed three, solo, touch-and-go landings. He noted that prior to the accident flight, his brother boarded the airplane for a local area flight. He stated that while departing runway 19, about midway down the runway, all engine power was lost. He said that he did not have sufficient altitude to return to the runway, and made a forced landing in trees bordering the runway.

In the pilot's written statement to the NTSB, he reported that when the flight originated, the right main fuel tank was full, and the left main fuel tank was about one-quarter full. The left and right auxiliary fuel tanks were empty, and not in use at the time of the accident. He said that the entire flight was accomplished with the fuel selector valve on the right tank.

A pilot-rated police officer that responded to the initial accident call, arrived on scene about 15 minutes after the accident. He reported that upon his arrival, the left main fuel tank was "dry", and the right fuel tank appeared to be full. He added that the main fuel selector valve had been placed in the "off" position prior to his arrival. The police officer said that the pilot had closed the fuel valve prior to exiting the airplane.

The airplane's wings, and fuselage sustained substantial damage.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA123