20040808022619A

Accident · Substantial damage

FAA accident report · Amtr MUSTANG2 · Rainelle, WV · August 8, 2004

Date
August 8, 2004 · 13:45 local
Place
Rainelle, WV
Airport
Rainelle Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N91061
NTSB investigation
NTSBIAD04LA035
Reported as
Amtr MUSTANG2
Reported engine
Lycoming O320*
Fatal injuries
0
Pilot’s flight hours
13,000 total300 in this make and model75 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) On August 08, 2004, at approximately 1345 EDT, an experimental amateur built mustang ii took off from rainele, WV (9W4) and reached altitude, when the aircraft experienced a loss of engine power, after the pilot reduced the engine throttle setting. The pilot stated when he advanced the throttle there was no corresponding increase in engine RPM. The pilot also stated he felt less resistance when moving the throttle control. He then selected carburetor heat and switched fuel tanks, but the engine never regained full power. The aircraft was substantially damaged after striking a tree and making contact with the ground during an emergency landing into a farmer's field. An on scene investigation revealed that a separation of the throttle outer and inner cable had occurred which prohibited throttle advancement.

As the FAA filed it

(-23) ON AUGUST 08, 2004, AT APPROXIMATELY 1345 EDT, AN EXPERIMENTAL AMATEUR BUILT MUSTANG II TOOK OFF FROM RAINELE, WV (9W4) AND REACHED ALTITUDE, WHEN THE AIRCRAFT EXPERIENCED A LOSS OF ENGINE POWER, AFTER THE PILOT REDUCED THE ENGINE THROTTLE SETTING. THE PILOT STATED WHEN HE ADVANCED THE THROTTLE THERE WAS NO CORRESPONDING INCREASE IN ENGINE RPM. THE PILOT ALSO STATED HE FELT LESS RESISTANCE WHEN MOVING THE THROTTLE CONTROL. HE THEN SELECTED CARBURETOR HEAT AND SWITCHED FUEL TANKS, BUT THE ENGINE NEVER REGAINED FULL POWER. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED AFTER STRIKING A TREE AND MAKING CONTACT WITH THE GROUND DURING AN EMERGENCY LANDING INTO A FARMER'S FIELD. AN ON SCENE INVESTIGATION REVEALED THAT A SEPARATION OF THE THROTTLE OUTER AND INNER CABLE HAD OCCURRED WHICH PROHIBITED THROTTLE ADVANCEMENT.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.