Swiss Mustangs wrote:
P-51D, 44-72446, N12700 owned, flown and crashed by Don Knapp. He stalled and crashed after a low pass at Dyess AFB airshow in Abilene, Texas on 23JUN90. He was killed.
"NTSB Identification: FTW90DQG03 . The docket is stored on NTSB microfiche number 43171.
accident occurred Saturday, June 23, 1990 at ABILENE, TX
Aircraft:NORTH AMERICAN P-51D, registration: N12700
Injuries: 1 Fatal.
ACCORDING TO WITNESSES, THE PILOT BEGAN HIS AIR SHOW ROUTINE WITH A LOW PASS DOWN THE RUNWAY FROM NORTH TO SOUTH. HE THEN MADE A CLIMBING TURN TO A CLOSE-IN DOWNWIND LEG. AT THE END OF THE DOWNWIND LEG, THE AIRPLANE ENTERED A CLIMBING RIGHT TURN AT WHAT WAS REPORTED TO BE A SLOWER THAT NORMAL SPEED. AFTER ABOUT 90 DEGREES OF TURN, THE ANGLE OF BANK INCREASED RAPIDLY, THE NOSE DROPPED, AND THE AIRPLANE IMPACTED THE GROUND IN A STEEP DESCENT. A WITNESS REPORTED THE ENGINE WAS NOT DEVELOPING FULL POWER; HOWEVER, THIS COULD NOT BE SUBSTANTIATED. DENSITY ALTITUDE WAS ABOUT 4500 FT.
The National Transportation Safety Board determines the probable cause(s) of this accident as follows:
FAILURE OF THE PILOT TO MAINTAIN ADEQUATE AIRSPEED, WHILE MANEUVERING AFTER A LOW PASS, WHICH RESULTED IN AN INADVERTENT STALL. THE HIGH DENSITY ALTITUDE WAS A RELATED FACTOR."
Martin
I was there and witnessed the accident. I was holding short awaiting my turn to take the runway, number two behind a Bird Dog. The temperature was around 95-98 degrees, and the radiator outlet door was not open. He was in a tight right pattern and was overshooting the base to final. He cranked in a bit more right rudder to tighten the turn, and thats when he stalled between 400 and 500 feet above ground level. The debris field was compact and localized.
Shortly after the accident, I was summoned to the base photo lab to watch some amateur video that was submitted by the photographer and watched a frame by frame of the last two minutes of flight. I pointed out the flight control deflections to the wing commander (Col Arie)that was also present in the lab. I was asked for my opinion because I had more current high performance single engine time than any of the USAF officers present.