19990817012409A

Accident · Substantial damage

FAA accident report · Airtrc AT-402 · Snyder, TX · August 17, 1999

Date
August 17, 1999 · 08:40 local
Place
Snyder, TX
Operating rules
Agricultural (Part 137)
Damage
Substantial damage
Aircraft
N4523L
NTSB investigation
NTSBFTW99LA226
Reported as
Airtrc AT402

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.

Acft engine failed during aerial application, the pilot made an emergency landing in a corn field, and the acft sustained substantial damage on landing. (-23) on August 17, 1999 the pilot damaged the landing gear and propeller during a power out landing in Snyder, TX. An inspection of the engine reveiled a machine screw had fallen out of the fuel control housing body and a broken safety wire. The three remaining screws in the body of the fuel control were also lose and the body of the fuel control was not mated along the gasket line. Bendix fuel control, sn;194160 (pn;2534439-4) was overhauled June 16, 1995 at 1372 hobbs hours; it failed 17 aug 1999 at 2624.6 hobbs hours.

As the FAA filed it

ACFT ENGINE FAILED DURING AERIAL APPLICATION, THE PILOT MADE AN EMERGENCY LANDING IN A CORN FIELD, AND THE ACFT SUSTAINED SUBSTANTIAL DAMAGE ON LANDING. (-23) ON AUGUST 17, 1999 THE PILOT DAMAGED THE LANDING GEAR AND PROPELLER DURING A POWER OUT LANDING IN SNYDER, TX. AN INSPECTION OF THE ENGINE REVEILED A MACHINE SCREW HAD FALLEN OUT OF THE FUEL CONTROL HOUSING BODY AND A BROKEN SAFETY WIRE. THE THREE REMAINING SCREWS IN THE BODY OF THE FUEL CONTROL WERE ALSO LOSE AND THE BODY OF THE FUEL CONTROL WAS NOT MATED ALONG THE GASKET LINE. BENDIX FUEL CONTROL, SN;194160 (PN;2534439-4) WAS OVERHAULED JUNE 16, 1995 AT 1372 HOBBS HOURS; IT FAILED 17 AUG 1999 AT 2624.6 HOBBS HOURS.

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 N4523L · 1

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