20011228034429A

Accident · No damage

FAA accident report · Langworthy H J/Langworthy G R SMYTH SIDEWINDER · Independence, KS · December 28, 2001

Date
December 28, 2001 · 13:16 local
Place
Independence, KS
Operating rules
General operating rules (Part 91)
Damage
No damage
Aircraft
N133G
NTSB investigation
NTSBCHI02FA059
People aboard
2
Fatal injuries
2

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) Witness' stated the aircraft was at an approximate altitude of 100 feet headed on an east/northeast direction and was in a steep, left turn when it made violent right roll and cork screwed into the ground at an approximate angle of 75 degrees. The wings appeared to have impacted the ground almost level, as both wing leading edges were crushed almost to the wing spars. When we arrived on the scene, all primary flight controls were checked for continuity and with exception of what was believed to be demolished on impact, were intact. Photographs were taken. The fuel tank, which was just forward of the instrument panel, was constructed of fiberglass and ruptured on impact. Fuel smell was strong at the scene. A letter applying for inspection for issuance of an airworthiness certificate was received by the wichita flight standards district office and was post dated October 22, 2001. privacy data omitted

As the FAA filed it

(-23) WITNESS' STATED THE AIRCRAFT WAS AT AN APPROXIMATE ALTITUDE OF 100 FEET HEADED ON AN EAST/NORTHEAST DIRECTION AND WAS IN A STEEP, LEFT TURN WHEN IT MADE VIOLENT RIGHT ROLL AND CORK SCREWED INTO THE GROUND AT AN APPROXIMATE ANGLE OF 75 DEGREES. THE WINGS APPEARED TO HAVE IMPACTED THE GROUND ALMOST LEVEL, AS BOTH WING LEADING EDGES WERE CRUSHED ALMOST TO THE WING SPARS. WHEN WE ARRIVED ON THE SCENE, ALL PRIMARY FLIGHT CONTROLS WERE CHECKED FOR CONTINUITY AND WITH EXCEPTION OF WHAT WAS BELIEVED TO BE DEMOLISHED ON IMPACT, WERE INTACT. PHOTOGRAPHS WERE TAKEN. THE FUEL TANK, WHICH WAS JUST FORWARD OF THE INSTRUMENT PANEL, WAS CONSTRUCTED OF FIBERGLASS AND RUPTURED ON IMPACT. FUEL SMELL WAS STRONG AT THE SCENE. A LETTER APPLYING FOR INSPECTION FOR ISSUANCE OF AN AIRWORTHINESS CERTIFICATE WAS RECEIVED BY THE WICHITA FLIGHT STANDARDS DISTRICT OFFICE AND WAS POST DATED OCTOBER 22, 2001. ^PRIVACY DATA OMITTED^

NTSB investigation

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