N3808F

Substantial
None

GREAT LAKES 2T-1A-2 S/N: 0776

Accident Details

Date
Thursday, October 26, 1995
NTSB Number
LAX96LA023
Location
CHANDLER, AZ
Event ID
20001207X04734
Coordinates
33.240650, -111.779243
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

the improper installation of an intake manifold tube assembly during engine overhaul which permitted leakage into the induction system resulting in detonation and piston failure in the associated cylinder.

Aircraft Information

Registration
Make
GREAT LAKES
Serial Number
0776
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
2T-1A-2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
2T-1A-2

Registered Owner (Current)

Name
CHANDLER AIR SERVICE INC
Address
1675 E RYAN RD
City
CHANDLER
State / Zip Code
AZ 85286-1731
Country
United States

Analysis

On October 26, 1995, at 1610 hours mountain standard time, a Great Lakes 2T-1A-2, N3808F, nosed over while making a forced landing 4.5 miles southeast of Chandler Airport, Chandler, Arizona. The aircraft sustained substantial damage and the commercial pilot was not injured. The aircraft was operated by Chandler Air Service, Inc., and was rented by the pilot for a personal flight when the accident occurred. The local area flight originated from Chandler Airport at 1545. Visual meteorological conditions prevailed at the time and no flight plan had been filed.

The pilot reported that the purpose of the flight was to practice an aerobatic sequence three or four times and return to Chandler. However, at completion of the first sequence he felt an abnormal vibration in the engine and terminated his practice. The engine rpm was 200 rpm low and could not be restored with the propeller control, and within a minute engine oil began to appear on the windshield. He turned toward Chandler when the pilot of a nearby aircraft radioed that he was trailing smoke. The pilot identified a suitable dirt road and decided to make a precautionary off-airport landing. During the landing rollout, the aircraft struck a ditch and nosed over.

Examination of the aircraft revealed that the engine oil supply had vented overboard through the engine crankcase breather and the propeller shaft. There was engine oil on the exterior of the aircraft aft of the breather tube, and on the exterior of the engine aft of the propeller shaft. The propeller shaft seal was displaced from its normal position and was positioned onto the propeller shaft.

The engine had been overhauled by the operator 11 hours prior to the accident. Disassembly of the engine by the operator following the accident revealed that the intake manifold tube flange and flange gasket (Lycoming part numbers 70485 and 71973) on the number four cylinder were leaking due to misalignment. A hole had burned through the number four piston. The hole was located in the perimeter of the piston around the rings and went through to the crankcase side of the piston in vicinity of the wrist pin.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX96LA023