20040525010309I

Incident · Substantial damage

FAA incident report · Pegasusquant · Benton, KS · May 25, 2004

Date
May 25, 2004 · 18:55 local
Place
Benton, KS
Airport
Benton Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
Ultralight vehicle (Part 103)
Damage
Substantial damage
Aircraft
NONE
Reported as
Pegasusquant
Reported engine
ROTAX ROTAX*
Fatal injuries
0
Pilot’s flight hours
4,000 total110 in this make and model0 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.

(-23) The vehicle was on a training flight at Benton Airport Kansas (1K1). During takeoff roll on runway 34, the machine began to drift left of centerline. While continuing to drift to the left it became airborne to an altitude of 10 feet above ground level as estimated by the pilot. The left wing tip struck saplings along the left edge of the improved area adjacent to the runway. Upon impact with the obstruction, the fuselage rotated to the left, settled to the ground on the right side and skidded to a stop. The occupants exited the machine unassisted and received minor injuries during the incident. The pegasa weight shift machine meets the criteria in 14 CFR part 103 for an ultralight vehicle and was operated for instructional purposes only under aero-sports connection (asc) exemption number A10JRRR. Law enforcement officers were present at the scene but no report was filed. Pilot induced.

As the FAA filed it

(-23) THE VEHICLE WAS ON A TRAINING FLIGHT AT BENTON AIRPORT KANSAS (1K1). DURING TAKEOFF ROLL ON RUNWAY 34, THE MACHINE BEGAN TO DRIFT LEFT OF CENTERLINE. WHILE CONTINUING TO DRIFT TO THE LEFT IT BECAME AIRBORNE TO AN ALTITUDE OF 10 FEET ABOVE GROUND LEVEL AS ESTIMATED BY THE PILOT. THE LEFT WING TIP STRUCK SAPLINGS ALONG THE LEFT EDGE OF THE IMPROVED AREA ADJACENT TO THE RUNWAY. UPON IMPACT WITH THE OBSTRUCTION, THE FUSELAGE ROTATED TO THE LEFT, SETTLED TO THE GROUND ON THE RIGHT SIDE AND SKIDDED TO A STOP. THE OCCUPANTS EXITED THE MACHINE UNASSISTED AND RECEIVED MINOR INJURIES DURING THE INCIDENT. THE PEGASA WEIGHT SHIFT MACHINE MEETS THE CRITERIA IN 14 CFR PART 103 FOR AN ULTRALIGHT VEHICLE AND WAS OPERATED FOR INSTRUCTIONAL PURPOSES ONLY UNDER AERO-SPORTS CONNECTION (ASC) EXEMPTION NUMBER A10JRRR. LAW ENFORCEMENT OFFICERS WERE PRESENT AT THE SCENE BUT NO REPORT WAS FILED. PILOT INDUCED.