20080621834469A

Accident · Substantial damage

FAA accident report · Maule MX-7-180A · Angwin, CA · June 21, 2008

Date
June 21, 2008 · 10:00 local
Place
Angwin, CA
Airport
Angwin-Parrett Field
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1993F
NTSB investigation
NTSBLAX08CA194
Reported as
Maule MX7180A
People aboard
2
Fatal injuries
0
Pilot’s flight hours
149 total103 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.

(-23) Pilot reported "June 21, 2008 at 1000 at parret field (2O3) in Angwin CA, winds from 290 at 7 mph on runway 34. Acceleration was good and the tail was lifted when the aircraft spun sharply to the left due to gust of wind" pilot applied full right rudder with aileron (yoke) to the left but the aircraft continued to the left. Aircraft left runway and pilot reduced throttle to idle and applied brakes. Aircraft collided with wind sock pole. Structural damage to leading edge, fuselage longeron, cylinder head, prop blades, left hand main landing gear torn from mount, tail wheel torn from mount.

As the FAA filed it

(-23) PILOT REPORTED "JUNE 21, 2008 AT 1000 AT PARRET FIELD (2O3) IN ANGWIN CA, WINDS FROM 290 AT 7 MPH ON RUNWAY 34. ACCELERATION WAS GOOD AND THE TAIL WAS LIFTED WHEN THE AIRCRAFT SPUN SHARPLY TO THE LEFT DUE TO GUST OF WIND" PILOT APPLIED FULL RIGHT RUDDER WITH AILERON (YOKE) TO THE LEFT BUT THE AIRCRAFT CONTINUED TO THE LEFT. AIRCRAFT LEFT RUNWAY AND PILOT REDUCED THROTTLE TO IDLE AND APPLIED BRAKES. AIRCRAFT COLLIDED WITH WIND SOCK POLE. STRUCTURAL DAMAGE TO LEADING EDGE, FUSELAGE LONGERON, CYLINDER HEAD, PROP BLADES, LEFT HAND MAIN LANDING GEAR TORN FROM MOUNT, TAIL WHEEL TORN FROM MOUNT.

NTSB investigation

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