20170520007909A

Accident · Substantial damage

FAA accident report · Extra Flugzeugbau EA 300/S · Pendelton, OR · May 20, 2017

Date
May 20, 2017 · 15:03 local
Place
Pendelton, OR
Airport
Eastern Oregon Regional At Pendlet
Phase of flight
Takeoff: Departure Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N68PW
NTSB investigation
NTSBWPR17LA116
Reported as
Extra Flugzeugbau EA 300/S
Reported engine
Lycoming AEIO-540 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
600 total135 in this make and model5 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.

The pilot was participating in an international aerobatic club sponsored three day aerobatic camp.

The pilot was starting his third practice flight of the second day of the camp. Flights generally last about 20 minutes on average.

Preflight was completed and the aircraft had no mechanical issues. Pilot was cleared by tower for takeoff on runway 29, a few seconds into the 2900 RPM takeoff acceleration the pilot noticed the canopy lift and separate to the right side of the aircraft causing him to abruptly shift head and shoulders to dodge the canopy as it departed the aircraft. The aircraft veered left towards the grass. The pilot quickly decided to "ride it out" straight ahead to avoid ground looping the aircraft. Pilot maintained aft elevator and appropriate rudder to maintain directional control. The aircraft struck a runway sign which he did not see because of limited forward visibility. The aircraft came to a stop in the grass with the engine idling. Pilot shut down engine and exited the aircraft.

The three aircraft propeller blades were broken off near mid-length, right wheel pant was shattered, and left wing lower skin was punctured. The remnants of the departed shattered canopy and bent canopy frame were on the runway.

As the FAA filed it

THE PILOT WAS PARTICIPATING IN AN INTERNATIONAL AEROBATIC CLUB SPONSORED THREE DAY AEROBATIC CAMP.

THE PILOT WAS STARTING HIS THIRD PRACTICE FLIGHT OF THE SECOND DAY OF THE CAMP. FLIGHTS GENERALLY LAST ABOUT 20 MINUTES ON AVERAGE.

PREFLIGHT WAS COMPLETED AND THE AIRCRAFT HAD NO MECHANICAL ISSUES. PILOT WAS CLEARED BY TOWER FOR TAKEOFF ON RUNWAY 29, A FEW SECONDS INTO THE 2900 RPM TAKEOFF ACCELERATION THE PILOT NOTICED THE CANOPY LIFT AND SEPARATE TO THE RIGHT SIDE OF THE AIRCRAFT CAUSING HIM TO ABRUPTLY SHIFT HEAD AND SHOULDERS TO DODGE THE CANOPY AS IT DEPARTED THE AIRCRAFT. THE AIRCRAFT VEERED LEFT TOWARDS THE GRASS. THE PILOT QUICKLY DECIDED TO "RIDE IT OUT" STRAIGHT AHEAD TO AVOID GROUND LOOPING THE AIRCRAFT. PILOT MAINTAINED AFT ELEVATOR AND APPROPRIATE RUDDER TO MAINTAIN DIRECTIONAL CONTROL. THE AIRCRAFT STRUCK A RUNWAY SIGN WHICH HE DID NOT SEE BECAUSE OF LIMITED FORWARD VISIBILITY. THE AIRCRAFT CAME TO A STOP IN THE GRASS WITH THE ENGINE IDLING. PILOT SHUT DOWN ENGINE AND EXITED THE AIRCRAFT.

THE THREE AIRCRAFT PROPELLER BLADES WERE BROKEN OFF NEAR MID-LENGTH, RIGHT WHEEL PANT WAS SHATTERED, AND LEFT WING LOWER SKIN WAS PUNCTURED. THE REMNANTS OF THE DEPARTED SHATTERED CANOPY AND BENT CANOPY FRAME WERE ON THE RUNWAY.

NTSB investigation

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