20101117051399A

Accident · Destroyed

FAA accident report · Raytheon Ai B36TC · Oklahoma City, OK · November 17, 2010

Date
November 17, 2010 · 20:30 local
Place
Oklahoma City, OK
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N314DP
NTSB investigation
NTSBCEN11FA075
Reported as
Raytheon Ai B36TC
Reported engine
Continental TSIO-550 series
People aboard
1
Fatal injuries
1
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
0 total0 in this make and model0 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.

While enroute to wiley post airport (kpwa), pilot stated to fort worth center that he was having landing gear extension problems. Fort worth center instructed pilot to climb and maintain 3000' altitude. Shortly after climbing to 3000' the aircraft climbed to 3300' and abruptly decended verticaly into the ground. While the aircraft was totally destroyed and the wreckage was largely consumed by post crash fire, continuity of major control surfaces was observed, and landing gear control box indicated that the landing gear was in the retract position.

As the FAA filed it

WHILE ENROUTE TO WILEY POST AIRPORT (KPWA), PILOT STATED TO FORT WORTH CENTER THAT HE WAS HAVING LANDING GEAR EXTENSION PROBLEMS. FORT WORTH CENTER INSTRUCTED PILOT TO CLIMB AND MAINTAIN 3000' ALTITUDE. SHORTLY AFTER CLIMBING TO 3000' THE AIRCRAFT CLIMBED TO 3300' AND ABRUPTLY DECENDED VERTICALY INTO THE GROUND. WHILE THE AIRCRAFT WAS TOTALLY DESTROYED AND THE WRECKAGE WAS LARGELY CONSUMED BY POST CRASH FIRE, CONTINUITY OF MAJOR CONTROL SURFACES WAS OBSERVED, AND LANDING GEAR CONTROL BOX INDICATED THAT THE LANDING GEAR WAS IN THE RETRACT POSITION.

NTSB investigation

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