20060710017149A

Accident · Substantial damage

FAA accident report · Amtr Sparrow · New Galilee, PA · July 10, 2006

Date
July 10, 2006 · 20:30 local
Place
New Galilee, PA
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
NONE
Reported as
Amtr Sparrow
Reported engine
ROTAX ROTAX503
Fatal injuries
0

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.

(-23) Aircraft departed non-licensed backyard runway. At approximately 40 feet in the air, the pilot stated the engine lost power but did not quit. The pilot attempted to turn back to the runway, and in the process, stalled the aircraft and came down in the next door neighbor's backyard. The aircraft had damage to outboard left and right wings, right main landing gear, aft and forward fuselage, engine mount, and propeller. The entire aircraft's first impact and crash site was contained within a 15 foot perimeter. The initial contact area showed signs of propeller rotation. The continuity of the flight controls and engine controls was confirmed. The aircraft had fuel in the tank, lines, and carburetor. The engine rotated freely and had compression.

As the FAA filed it

(-23) AIRCRAFT DEPARTED NON-LICENSED BACKYARD RUNWAY. AT APPROXIMATELY 40 FEET IN THE AIR, THE PILOT STATED THE ENGINE LOST POWER BUT DID NOT QUIT. THE PILOT ATTEMPTED TO TURN BACK TO THE RUNWAY, AND IN THE PROCESS, STALLED THE AIRCRAFT AND CAME DOWN IN THE NEXT DOOR NEIGHBOR'S BACKYARD. THE AIRCRAFT HAD DAMAGE TO OUTBOARD LEFT AND RIGHT WINGS, RIGHT MAIN LANDING GEAR, AFT AND FORWARD FUSELAGE, ENGINE MOUNT, AND PROPELLER. THE ENTIRE AIRCRAFT'S FIRST IMPACT AND CRASH SITE WAS CONTAINED WITHIN A 15 FOOT PERIMETER. THE INITIAL CONTACT AREA SHOWED SIGNS OF PROPELLER ROTATION. THE CONTINUITY OF THE FLIGHT CONTROLS AND ENGINE CONTROLS WAS CONFIRMED. THE AIRCRAFT HAD FUEL IN THE TANK, LINES, AND CARBURETOR. THE ENGINE ROTATED FREELY AND HAD COMPRESSION.