20160511007609A

Accident · Substantial damage

FAA accident report · Boeing B75N1 · May 11, 2016

Date
May 11, 2016 · 17:10 local
Airport
Winslow-Lindbergh Regional
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N56200
NTSB investigation
NTSBWPR16LA106
Reported as
Boeing B75N1
Reported engine
Lycoming R680E3B
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Private pilot, unknown or foreign certificate
Pilot’s flight hours
1,750 total450 in this make and model26 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 taxied to rwy 29 for take-off after fueling at the airport self-fuel facility. Airport personnel witnessed the following while observing the aircraft taking off:

The stearman took off climbing to about 50 ft and proceeded about 500 yards to the west (at the end of) the airfield. At this time the plane did not climb any higher and banked in(to) a left turn and lost altitude until it crashed. The plane went in nose first and began to cartwheel in a cloud of dust.

The chase plane had taken off prior to the stearman. It was accompanying the stearman conducting video recording of flight/take-off. It circled the area after the crash and landed near the end of the runway. The chase plane crew notified airport personnel that both occupants of the stearman were out of the plane and walking around.

Airport personnel contacted emergency response units and directed them to the site when they arrived at the airport. Both occupants of the aircraft refused medical assistance.

The aircraft was recovered to airport hangar. Investigation of the aircraft verified all four wings and fuselage have sustained major structural damage.

Observations of the recovered aircraft indicate there was sufficient fuel aboard; there was no obvious engine damage; both propeller blades were bent aft; no indications of oil leaks; some blue fuel stains were observed along the outside housing of the air intake box below the carburetor.

Subsequent inspection of the aircraft & engine determine the engine was able to run normally with no malfunctions or systems failures noted.

As the FAA filed it

AIRCRAFT TAXIED TO RWY 29 FOR TAKE-OFF AFTER FUELING AT THE AIRPORT SELF-FUEL FACILITY. AIRPORT PERSONNEL WITNESSED THE FOLLOWING WHILE OBSERVING THE AIRCRAFT TAKING OFF:

THE STEARMAN TOOK OFF CLIMBING TO ABOUT 50 FT AND PROCEEDED ABOUT 500 YARDS TO THE WEST (AT THE END OF) THE AIRFIELD. AT THIS TIME THE PLANE DID NOT CLIMB ANY HIGHER AND BANKED IN(TO) A LEFT TURN AND LOST ALTITUDE UNTIL IT CRASHED. THE PLANE WENT IN NOSE FIRST AND BEGAN TO CARTWHEEL IN A CLOUD OF DUST.

THE CHASE PLANE HAD TAKEN OFF PRIOR TO THE STEARMAN. IT WAS ACCOMPANYING THE STEARMAN CONDUCTING VIDEO RECORDING OF FLIGHT/TAKE-OFF. IT CIRCLED THE AREA AFTER THE CRASH AND LANDED NEAR THE END OF THE RUNWAY. THE CHASE PLANE CREW NOTIFIED AIRPORT PERSONNEL THAT BOTH OCCUPANTS OF THE STEARMAN WERE OUT OF THE PLANE AND WALKING AROUND.

AIRPORT PERSONNEL CONTACTED EMERGENCY RESPONSE UNITS AND DIRECTED THEM TO THE SITE WHEN THEY ARRIVED AT THE AIRPORT. BOTH OCCUPANTS OF THE AIRCRAFT REFUSED MEDICAL ASSISTANCE.

THE AIRCRAFT WAS RECOVERED TO AIRPORT HANGAR. INVESTIGATION OF THE AIRCRAFT VERIFIED ALL FOUR WINGS AND FUSELAGE HAVE SUSTAINED MAJOR STRUCTURAL DAMAGE.

OBSERVATIONS OF THE RECOVERED AIRCRAFT INDICATE THERE WAS SUFFICIENT FUEL ABOARD; THERE WAS NO OBVIOUS ENGINE DAMAGE; BOTH PROPELLER BLADES WERE BENT AFT; NO INDICATIONS OF OIL LEAKS; SOME BLUE FUEL STAINS WERE OBSERVED ALONG THE OUTSIDE HOUSING OF THE AIR INTAKE BOX BELOW THE CARBURETOR.

SUBSEQUENT INSPECTION OF THE AIRCRAFT & ENGINE DETERMINE THE ENGINE WAS ABLE TO RUN NORMALLY WITH NO MALFUNCTIONS OR SYSTEMS FAILURES NOTED.

NTSB investigation

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