20141026021149A

Accident · Substantial damage

FAA accident report · Extra Flugzeugproduktions-Und EA 300/L · Las Vegas, NV · October 26, 2014

Date
October 26, 2014 · 11:30 local
Place
Las Vegas, NV
Phase of flight
Maneuver
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N763DT
NTSB investigation
NTSBWPR15LA024
Reported as
Extra Flugzeugproduktions-Und EA 300/L
Reported engine
Lycoming AEIO-540-L1B5
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
600 total600 in this make and model220 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.

On 10-26-2014 an Extra 300 aircraft, N763DT, conducting a commercial flight under 14 CFR part 91, experienced a loss of rudder control while recovering from an aerobatic spin maneuver.

Examination of the flight controls revealed that the right rudder cable, part number PC-00836, separated approximately mid-length resulting in the loss of rudder control.

The pilot attempted to land the aircraft at hnd, however aborted due to a crosswind. The pilot elected to fly the aircraft to Las Vegas mccarran airport (las) due to favorable wind conditions and landed on runway 19R. After landing the aircraft experienced a collapse of both main landing gear.

The aircraft experienced substantial damage. No post crash fire was reported. Neither pilot nor passenger reported injuries.

As the FAA filed it

ON 10-26-2014 AN EXTRA 300 AIRCRAFT, N763DT, CONDUCTING A COMMERCIAL FLIGHT UNDER 14 CFR PART 91, EXPERIENCED A LOSS OF RUDDER CONTROL WHILE RECOVERING FROM AN AEROBATIC SPIN MANEUVER.

EXAMINATION OF THE FLIGHT CONTROLS REVEALED THAT THE RIGHT RUDDER CABLE, PART NUMBER PC-00836, SEPARATED APPROXIMATELY MID-LENGTH RESULTING IN THE LOSS OF RUDDER CONTROL.

THE PILOT ATTEMPTED TO LAND THE AIRCRAFT AT HND, HOWEVER ABORTED DUE TO A CROSSWIND. THE PILOT ELECTED TO FLY THE AIRCRAFT TO LAS VEGAS MCCARRAN AIRPORT (LAS) DUE TO FAVORABLE WIND CONDITIONS AND LANDED ON RUNWAY 19R. AFTER LANDING THE AIRCRAFT EXPERIENCED A COLLAPSE OF BOTH MAIN LANDING GEAR.

THE AIRCRAFT EXPERIENCED SUBSTANTIAL DAMAGE. NO POST CRASH FIRE WAS REPORTED. NEITHER PILOT NOR PASSENGER REPORTED INJURIES.

NTSB investigation

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

Other reports on N763DT · 1

Matched to the same aircraft by N-number and date.