N4769C

Substantial
None

Piper J5-C S/N: 5-1474

Accident Details

Date
Monday, March 30, 1998
NTSB Number
ANC98LA033
Location
VALDEZ, AK
Event ID
20001211X09624
Coordinates
61.149745, -146.809997
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The owner/pilot mechanic's improper overhaul of the engine, and lack of proper lubricating cylinder grease. A factor in the accident was the lack of a suitable area for a forced landing.

Aircraft Information

Registration
N4769C
Make
PIPER
Serial Number
5-1474
Engine Type
Reciprocating
Year Built
1943
Model / ICAO
J5-C J5
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BANDY ROBERT A
Address
PO BOX 1522
Status
Deregistered
City
VALDEZ
State / Zip Code
AK 99686-1522
Country
United States

Analysis

On March 30, 1998, about 1420 Alaska standard time, a wheel equipped Piper J5-C airplane, N4769C, sustained substantial damage during a forced landing, about 2 miles southeast of Valdez, Alaska. The airplane was being operated as a visual flight rules (VFR) local area personal flight when the accident occurred. The airplane was owned and operated by the pilot. The certificated commercial pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed. The flight originated at the Valdez Airport, about 1415.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on March 31, 1998, at 1055, the pilot, who is an aviation mechanic, reported he recently completed an engine overhaul on the accident airplane. The accident flight was the first flight since the overhaul. The pilot departed Runway 06 at Valdez, and climbed to about 1,000 feet above the ground, when the engine suddenly quit running. He said he restarted the engine, but it only ran another 45 seconds before stopping again. The pilot selected an emergency landing area on a highway, but had to slip the airplane to avoid several vehicles on the highway. The airplane collided with a power line, about 25 feet above the ground. The airplane then descended to the ground and received damage to the right wing, the right wing spar, and the landing gear.

On April 16, 1998, a Federal Aviation Administration (FAA) airworthiness inspector, Anchorage Flight Standards District Office (FSDO), reported the pilot/mechanic had completed a disassembly of the engine. All of the engine cylinders were scored. The pilot had installed chrome cylinders, and during the assembly, he applied a coating of light grease to each engine cylinder bore. The engine then was temporarily stored before being installed on the accident airplane. According to the FAA inspector, the engine cylinders required an application of a thicker grease than what was used by the pilot.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA033