19980707046669A

Accident · No damage

FAA accident report · Ayres S-2R · Ft Ransom, ND · July 7, 1998

Date
July 7, 1998 · 07:30 local
Place
Ft Ransom, ND
Operating rules
Agricultural (Part 137)
Damage
No damage
Aircraft
N4232X
NTSB investigation
NTSBCHI98LA241
Reported as
Ayres S2R

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) On 07/07/98 at 0730 CDT, rockwell S-2R, N4232X, owned by widmer flying service, inc. and flown by james f. plath was substantially damaged during an aerial application flight. A forced landing was attempted due to fuel starvation. The aircraft hit a fence immediately on touchdown sustaining damage to the left wing from the tip to 6 ft. inboard causing deformation of ribs, spar and skin as well as buckling of the leading edge. Bottoms of both wings had numerous gouges and tears caused by steel fence posts. Both ailersons sustained similar damage. Empannage tubing bowed, fractured at tailwheel connect points. One propeller blade bent.

As the FAA filed it

(-23) ON 07/07/98 AT 0730 CDT, ROCKWELL S-2R, N4232X, OWNED BY WIDMER FLYING SERVICE, INC. AND FLOWN BY JAMES F. PLATH WAS SUBSTANTIALLY DAMAGED DURING AN AERIAL APPLICATION FLIGHT. A FORCED LANDING WAS ATTEMPTED DUE TO FUEL STARVATION. THE AIRCRAFT HIT A FENCE IMMEDIATELY ON TOUCHDOWN SUSTAINING DAMAGE TO THE LEFT WING FROM THE TIP TO 6 FT. INBOARD CAUSING DEFORMATION OF RIBS, SPAR AND SKIN AS WELL AS BUCKLING OF THE LEADING EDGE. BOTTOMS OF BOTH WINGS HAD NUMEROUS GOUGES AND TEARS CAUSED BY STEEL FENCE POSTS. BOTH AILERSONS SUSTAINED SIMILAR DAMAGE. EMPANNAGE TUBING BOWED, FRACTURED AT TAILWHEEL CONNECT POINTS. ONE PROPELLER BLADE BENT.

NTSB investigation

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

Other reports on N4232X · 2

Matched to the same aircraft by N-number and date.