N7991Y

Substantial
None

Piper PA-30B S/N: 30-1095

Accident Details

Date
Friday, May 28, 1999
NTSB Number
FTW99LA154
Location
MCALESTER, OK
Event ID
20001212X18785
Coordinates
34.920078, -95.760696
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot inadvertently stalling the airplane while attempting to avoid power lines. Factors were the loss of power on both the left and right engines as a result of water contamination in the fuel system, the pilot's inadequate preflight procedures, and the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N7991Y
Make
PIPER
Serial Number
30-1095
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
PA-30B PA30
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
S & F INC
Address
13020 S SUNNYLANE RD
Status
Deregistered
City
OKLAHOMA CITY
State / Zip Code
OK 73160-8806
Country
United States

Analysis

On May 28, 1999, at 1630 central daylight time, a Piper PA-30B twin-engine airplane, N7991Y, was substantially damaged during a forced landing following a loss of engine power after takeoff from the McAlester Regional Airport near McAlester, Oklahoma. The instrument rated private pilot and his pilot rated passenger were not injured. The airplane was owned and operated by the pilot. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight destined for Oklahoma City, Oklahoma. The cross-country flight was originating at the time of the accident.

During a telephone interview conducted by the NTSB investigator-in-charge, the pilot stated that shortly after takeoff, while climbing through 300 feet agl, the left engine "quit." The pilot added that after attempting to restart the engine, he elected to feather the propeller. Shortly after feathering the left propeller, the right engine started to "sputter." The pilot stated that the right engine never completely failed; however, he was unable to maintain altitude with the sputtering right engine and elected to land the airplane, with the landing gear retracted, in a field approximately 2 miles south of the McAlester Airport. In the enclosed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), the pilot stated that he "had to climb over power lines [and] stalled [the] aircraft."

The pilot reported that the left wing spar, outboard of the engine, was broken. The right wing spar, outboard of the engine, was bent aft, and the empennage was separated except for a section of sheet metal attaching it to the airplane.

The pilot reported that he had refueled the airplane with 90 gallons of fuel prior to his departure. The pilot stated that he had visually checked the fuel level prior to the departure; however, he did not sump the fuel tanks. He added that the flight to McAlester earlier that day had been uneventful and that there were no problems with either engine.

During the recovery process, fuel samples were taken from the airplane's left and right main fuel tanks. A half-gallon of fuel was drained from each tank into two separate 1-gallon containers. The bottom half of the sample taken from the left main fuel tank appeared clear in color and resembled water. The bottom 1/8th of the half-gallon fuel sample taken from the right main fuel tank appeared clear in color and also resembled water. The remaining fluid in both samples was blue in color and resembled 100LL aviation fuel.

The FAA inspector, who responded to the accident site, stated that he examined fuel samples taken from the fixed base operator's fueling truck, from which the accident airplane was refueled, and found no evidence of water contamination.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW99LA154