20140827017569A

Accident · Substantial damage

FAA accident report · Bertagna John JUST HIGHLANDER · Birdsboro, PA · August 27, 2014

Date
August 27, 2014 · 15:55 local
Place
Birdsboro, PA
Airport
Bert'S Airport
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N61148
NTSB investigation
NTSBERA14CA410
Reported as
Bertagna John Just Highlander
Reported engine
ROTAX 912UL
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Airline transport
Pilot’s flight hours
22,000 total5 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.

Aircraft wreckage located intact (except for plastic wingtips) next to landing runway 26 on a 160 degree heading. The aircraft fabric covering and cowl were almost completely consumed by post-crash fire. The engine and airframe sustained both impact and fire damage.

The flying pilotprivacy data omitted had recently acquired the aircraft, and after a checkout was still uncomfortable. The non-flying pilot/cfi had demonstrated several takeoffs and landings on previous legs that day. privacy data omitted Was flying the accident leg; both pilots recall a normal approach, a bounce, application of full power, and then finding themselves on the ground outside the burning aircraft. At the time of the accident he owner had accumulated approximately 5.2 hours in the amateur built experimental aircraft, the CFI approximately 1.0.

Ground scars, damage to airframe and propeller, wreckage orientation, and occupant statements are all consistent with a low altitude stall/spin or torqueroll with resultant cartwheel type ground contact.

As the FAA filed it

AIRCRAFT WRECKAGE LOCATED INTACT (EXCEPT FOR PLASTIC WINGTIPS) NEXT TO LANDING RUNWAY 26 ON A 160 DEGREE HEADING. THE AIRCRAFT FABRIC COVERING AND COWL WERE ALMOST COMPLETELY CONSUMED BY POST-CRASH FIRE. THE ENGINE AND AIRFRAME SUSTAINED BOTH IMPACT AND FIRE DAMAGE.

THE FLYING PILOT^PRIVACY DATA OMITTED^ HAD RECENTLY ACQUIRED THE AIRCRAFT, AND AFTER A CHECKOUT WAS STILL UNCOMFORTABLE. THE NON-FLYING PILOT/CFI HAD DEMONSTRATED SEVERAL TAKEOFFS AND LANDINGS ON PREVIOUS LEGS THAT DAY. ^PRIVACY DATA OMITTED^ WAS FLYING THE ACCIDENT LEG; BOTH PILOTS RECALL A NORMAL APPROACH, A BOUNCE, APPLICATION OF FULL POWER, AND THEN FINDING THEMSELVES ON THE GROUND OUTSIDE THE BURNING AIRCRAFT. AT THE TIME OF THE ACCIDENT HE OWNER HAD ACCUMULATED APPROXIMATELY 5.2 HOURS IN THE AMATEUR BUILT EXPERIMENTAL AIRCRAFT, THE CFI APPROXIMATELY 1.0.

GROUND SCARS, DAMAGE TO AIRFRAME AND PROPELLER, WRECKAGE ORIENTATION, AND OCCUPANT STATEMENTS ARE ALL CONSISTENT WITH A LOW ALTITUDE STALL/SPIN OR TORQUEROLL WITH RESULTANT CARTWHEEL TYPE GROUND CONTACT.

NTSB investigation

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