N51430

Substantial
None

MAULE M-4S/N: 1097C

Accident Details

Date
Friday, March 7, 2008
NTSB Number
SEA08LA087
Location
Bishop, CA
Event ID
20080317X00320
Coordinates
37.373054, -118.363609
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

A loss of engine power due to foreign object ingestion in the induction system, which resulted in a stuck/jammed exhaust valve during the takeoff.

Aircraft Information

Registration
Make
MAULE
Serial Number
1097C
Engine Type
Reciprocating
Year Built
1973
Model / ICAO
M-4M4
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
M-4-210C

Registered Owner (Current)

Name
BURKE WARREN V
Address
12948 W 1ST DR
City
LAKEWOOD
State / Zip Code
CO 80228-1608
Country
United States

Analysis

On March 7, 2008, about 1500 Pacific standard time, a Maule M-4 airplane, N51430, sustained substantial damage following a loss of engine power, forced landing and intentional ground loop at the Eastern Sierra Regional Airport, Bishop, California. The airplane was being operated as a visual flight rules (VFR) cross-country flight under Title 14, Code of Federal Regulations Part 91. The private pilot, the registered owner/operator of the airplane, and two passengers were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The pilot departed about 1455 and his intended destination was Columbia, California.

The airplane sustained substantial damage to the right horizontal stabilizer and right wing.

During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on March 10, the pilot reported that just after takeoff the engine began "running really rough" and he returned to the airport for a landing on the departure runway. He reported the airplane touched down long and overran the runway. The pilot stated he intentionally ground looped the airplane in an effort to avoid a fence located beyond the overrun area off the runway. The airplane's right main landing gear collapsed during the intentional ground loop.

Post accident examination of the engine by a Federal Aviation Administration (FAA) inspector (Reno Flight Standards District Office [FSDO]) and an airframe and power plant mechanic revealed that the alternate induction air valve (automatic air door) was separated from the induction bracket and a 2-inch-long AN3 bolt associated with the assembly was lodged between (holding open) the number six cylinder exhaust valve and exhaust port. The corresponding door hardware, a spiral spring, washer, and cotter pin were not found. The FAA inspector reported that he believes the unfound hardware passed through the engine and out the exhaust.

Maintenance logbook records showed that an annual inspection of the engine was completed on December 28, 2007. No maintenance discrepancies or anomalies with the alternate air valve were noted.

The pilot reported that there were no discrepancies related to the alternate air system prior to the accident flight.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA08LA087