- Date
- March 13, 2000, 17:00 local (23:00 UTC)
- Place
- Gillett, AR
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Enroute
- Aircraft
- N9785Grumman-Schweizer G-164A
- Weather
- Visual (VMC) · Day
- Status
- Completed · report January 18, 2001
- Report
- Approved by Office Director
- FAA report
- 20000313004829A
- Case key
- 48791
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
The cracked #8 cylinder resulting in failure of the cylinder. A factor was the plowed/furrowed terrain.
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Analysis
En route from the airstrip to the field to apply fertilizer, the agricultural airplane's engine started to 'miss and lose power.' The pilot executed a forced landing. During the landing roll in a tilled field, the airplane nosed over to the inverted position. The #8 cylinder was found cracked. The cylinder had accumulated 337 hours since its last overhaul.
Factual narrative
On March 13, 2000, at 1700 central standard time, a Grumman-Schweizer G-164A agricultural airplane, N9785, nosed over during a forced landing following a loss of engine power near Gillett, Arkansas. The airplane was owned and operated by Trites Flying Service, Inc., of Gillett, Arkansas. The commercial pilot was not injured, and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the aerial application flight, and a flight plan was not filed. The 14 Code of Federal Regulations Part 137 flight originated from the operator's private airstrip a few minutes before the accident.
The pilot and operator reported that en route from the airstrip to the field to apply fertilizer, the engine started to "miss and lose power." The pilot landed the airplane in a tilled field, and during the landing roll, the airplane nosed over to the inverted position.
The FAA inspector, who responded to the site, found structural damage to the vertical stabilizer and rudder. The main spar for the upper left wing was damaged outboard of the strut. The FAA inspector and the operator found the #8 cylinder cracked. The cylinder had accumulated 337 hours since overhaul.
Aircraft
- Registration
- N9785
- Reported as
- Grumman-Schweizer G-164A
- Category
- Airplane
- Serial number
- 1263
- Airframe hours
- 10,517
- Engine
- P&W R-1340-59, 600 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Aerial application · Part 137
- Registered owner
- John W. Trites
- Airworthiness certificate
- Special, Restricted (Special)
- Last inspection
- Annual · March 1, 1999 · 337 hours before
- Departed
- NONE
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 50
- Certificate
- Commercial
- Airplane ratings
- Single-engine land
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Center
- Flight hours
- 9,100 total
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 180° at 5 knots
- Visibility
- 10 statute miles
- Temperature
- 70 °F
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.
Other investigations on N9785 · 2
Matched to the same aircraft by N-number and date.