N64819

Substantial
None

Beech UC45J S/N: 52-3762

Accident Details

Date
Thursday, May 2, 1996
NTSB Number
MIA96LA136
Location
OPA LOCKA, FL
Event ID
20001208X05830
Coordinates
25.909029, -80.269035
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

inadequate inspection of the fuel line connector by company maintenance personnel, and failure of a connector resulting in a fuel leak and fire.

Aircraft Information

Registration
N64819
Make
BEECH
Serial Number
52-3762
Engine Type
Reciprocating
Model / ICAO
UC45J BE76
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
SALE REPORTED
Address
215 MAXWELL DR
Status
Deregistered
City
PITTSBURGH
State / Zip Code
PA 15236-2056
Country
United States

Analysis

On May 2, 1996, about 1052 eastern daylight time, a Beech UC-45J, N64819, registered to Aero Caribe Express and operated by Sky Charters, Inc., as a 14 CFR part 91 positioning flight, had a fire in the right main gear wheel well and went off the runway into a canal while returning to Opa Locka Airport, Opa Locka, Florida. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft sustained substantial damage and the airline transport-rated pilot was not injured. The flight originated from Opa Locka, Florida, a few minutes before the accident.

The pilot stated that during departure, while performing the climb checklist he turned off the electric boost pumps. The right engine began to run rough and he noticed the fuel pressure was zero. He turned the right electric boost pump back on, fuel pressure increased to normal levels, and the engine began to run normally. He elected to return to the departure airport.

While en route back to the airport, he switched the right engine fuel selector from the main tank to the auxiliary tank position. He then turned off the electric boost pump, and fuel pressure again dropped to zero and the engine began to fail. He turned the electric boost pump back on and switched the right fuel selector back to the main tank position. While landing, the air traffic controller informed him that the right engine was on fire. He visually inspected the engine but did not see any flame or smoke. While shutting down the right engine, the cockpit immediately filled with smoke. He was unable to see, and while attempting to open the cockpit hatch the aircraft veered to the left. The aircraft entered a canal where it came to rest.

Postcrash examination of the aircraft showed it had sustained fire damage in the right wheel well aft of the engine firewall. The right main landing gear wheel, which had been retracted for the flight and extended on short final approach, did not have any fire damage. The right engine driven fuel pump operated normally. A pressure check of all fuel lines showed a rubber fuel line had split and was leaking at the engine oil dilution valve on the aft side of the engine fire wall, upper outboard corner. This rubber fuel line connected a pressurized, metal fuel supply line from the carburetor to the inlet of the oil dilution valve. The line was dry and brittle and did not have any fire damage on it. No other fuel line leaks were found.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA96LA136