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20050609013909I

Incident
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FAA incident report · Amtr QUICKIE2 · Chino, CA · June 9, 2005

FAA Aviation Safety Information Portal

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Date
June 9, 2005 · 11:32 local
Place
Chino, CA
Airport
Chino Airport
Phase of flight
To Aborted (Fixed Wing)
Operating rules
General operating rules (Part 91)
Aircraft
N86JT
Reported as
Amtr QUICKIE2
People aboard
1
Fatal injuries
0
Pilot’s flight hours
14,340 total2 in this make and model2 in the last 90 days
N86JTRegistered now · Siegenfield Harold QUICKIE ACFT (Q-2)S/N 2607 Q-2 · Built 2000Airframe modelSiegenfield Harold QUICKIE ACFT (Q-2)Engine modelRevmaster 2100Reciprocating

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) Takeoff aborted r/w 26R at cno. Aircraft ran off right side of runway. A new tailwheel was installed on aircraft which changed the angle of incident on the canard wing. With the new tailwheel, the vlof changed from 65MPH to 75MPH. Pilot stated aircraft remained on ground too long during takeoff roll. Pilot aborted takeoff at 70MPH. He thought aircraft should have been airborne at 65MPH. During abort aircraft drifted to right side of runway. Rudder inputs were ineffective below 25MPH. Pilot intentionally groundlooped aircraft but in so doing departed runway. Aircraft was not damaged.

As the FAA filed it

(-23) TAKEOFF ABORTED R/W 26R AT CNO. AIRCRAFT RAN OFF RIGHT SIDE OF RUNWAY. A NEW TAILWHEEL WAS INSTALLED ON AIRCRAFT WHICH CHANGED THE ANGLE OF INCIDENT ON THE CANARD WING. WITH THE NEW TAILWHEEL, THE VLOF CHANGED FROM 65MPH TO 75MPH. PILOT STATED AIRCRAFT REMAINED ON GROUND TOO LONG DURING TAKEOFF ROLL. PILOT ABORTED TAKEOFF AT 70MPH. HE THOUGHT AIRCRAFT SHOULD HAVE BEEN AIRBORNE AT 65MPH. DURING ABORT AIRCRAFT DRIFTED TO RIGHT SIDE OF RUNWAY. RUDDER INPUTS WERE INEFFECTIVE BELOW 25MPH. PILOT INTENTIONALLY GROUNDLOOPED AIRCRAFT BUT IN SO DOING DEPARTED RUNWAY. AIRCRAFT WAS NOT DAMAGED.