20000430006769A

Accident · No damage

FAA accident report · Green Gerald D GTX-SE-FI · Gilette, WY · April 30, 2000

Date
April 30, 2000 · 08:25 local
Place
Gilette, WY
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N2411V
NTSB investigation
NTSBDEN00LA079

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) The pilot/repairman made adjustments to the propeller blade angles the morning of the fatal flight. Takeoff was from a rough field approximately 6 miles south of (gcc), gillette campbell county airport. Witnesses stated that the engine sounded as it were misfiring. The inflight breakup began after approxiamtely one mile of travel over the ground. One propeller balde was found approximately 200 yards from the impact point. Other propeller blade parts were found closer to the impact point. The main rotor blades hit the vertical stabilizer and rudder breaking them off the aircraft, leaving the aircraft uncontrollable. The aicraft first impacted on the tailwheel, then rolled on to its the left side and caught on fire.

As the FAA filed it

(-23) THE PILOT/REPAIRMAN MADE ADJUSTMENTS TO THE PROPELLER BLADE ANGLES THE MORNING OF THE FATAL FLIGHT. TAKEOFF WAS FROM A ROUGH FIELD APPROXIMATELY 6 MILES SOUTH OF (GCC), GILLETTE CAMPBELL COUNTY AIRPORT. WITNESSES STATED THAT THE ENGINE SOUNDED AS IT WERE MISFIRING. THE INFLIGHT BREAKUP BEGAN AFTER APPROXIAMTELY ONE MILE OF TRAVEL OVER THE GROUND. ONE PROPELLER BALDE WAS FOUND APPROXIMATELY 200 YARDS FROM THE IMPACT POINT. OTHER PROPELLER BLADE PARTS WERE FOUND CLOSER TO THE IMPACT POINT. THE MAIN ROTOR BLADES HIT THE VERTICAL STABILIZER AND RUDDER BREAKING THEM OFF THE AIRCRAFT, LEAVING THE AIRCRAFT UNCONTROLLABLE. THE AICRAFT FIRST IMPACTED ON THE TAILWHEEL, THEN ROLLED ON TO ITS THE LEFT SIDE AND CAUGHT ON FIRE.

NTSB investigation

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