N4078L

MINR
None

Piper PA-31-350S/N: PA31-81520060

Accident Details

Date
Friday, April 20, 2001
NTSB Number
NYC01IA126
Location
Newark, OH
Event ID
20010523X01007
Coordinates
40.059619, -82.419662
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The company maintenance personnel's failure to comply with the service bulletin, which resulted in a fuel boost pump leakage and subsequent fire during taxi. A factor was the manufacturer's confusing service bulletin.

Aircraft Information

Registration
N4078L
Make
PIPER
Serial Number
PA31-81520060
Engine Type
Reciprocating
Year Built
1980
Model / ICAO
PA-31-350PA31
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
CROW EXECUTIVE AIR INC
Address
28331 LEMOYNE RD
Status
Deregistered
City
MILLBURY
State / Zip Code
OH 43447
Country
United States

Analysis

On April 20, 2001, about 1300 eastern daylight time, a Piper PA-31-350, N4078L, sustained minor damage while taxing at Newark-Heath Airport (VTA), Newark, Ohio. The certificated commercial pilot and passenger were not injured. Instrument meteorological conditions prevailed for the flight that originated from Fort Wayne, Indiana. An instrument flight rules flight plan was filed for the air taxi flight conducted under 14 CFR Part 135.

The pilot reported that after landing, while taxing to the ramp area, a fire was observed in the left engine. The pilot secured the engine, and then he and the passenger evacuated the airplane. Witnesses extinguished the fire with a handheld fire extinguisher.

Examination of the engine by a Federal Aviation Administration (FAA) inspector revealed a leak in the left engine fuel boost pump. The pump (Lear Romec model RG9080J7A) was sent to the manufacturer for further examination. Testing at the Lear Romec facility revealed that four screws, which secured the pump valve assembly, were not properly torqued.

Discussion between representatives at Lear Romec and the airplane operator revealed that there was some confusion among the operator's maintenance personnel about Lear Romec Service Bulletin 101SB020 Rev. 2. According to the service bulletin, the torque of the four screws that secured the pump valve assembly should be verified, and retorqued if necessary, at certain time intervals. However, there was another set of four screws that secured the pump housing cover, in addition to the four screws that secured the valve assembly.

The testing at the Lear Romec facility indicated that the wrong set of screws had been torqued. After testing the fuel boost pump and the discussion with the operator, Lear Romec issued Service Bulletin 101SB020 Rev. 3, which clarified the correct screws to torque.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC01IA126