- Date
- October 15, 1997, 18:00 local (23:00 UTC)
- Place
- Altus, OK
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Maneuvering
- Aircraft
- N8819HGrumman-Schweizer G-164A
- Weather
- Visual (VMC) · Day
- Status
- Completed · report November 6, 1998
- Report
- Approved by Office Director
- FAA report
- 19971015031309A
- Case key
- 20456
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 loss of engine power due to the cracked cylinder. A factor was the lack of suitable terrain for the forced landing.
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
The agricultural airplane's engine lost power as the pilot was turning the airplane between spray passes. The ensuing forced landing was made to a soft field, and during the landing roll, the airplane nosed over and came to rest inverted. Examination of the radial engine revealed that a circumferential crack had completely separated the #4 cylinder head from the cylinder barrel.
Factual narrative
On October 15, 1997, at 1800 central daylight time, a Grumman-Schweizer G-164A agricultural airplane, N8819H, sustained substantial damage during a forced landing following a loss of engine power near Altus, Oklahoma. The commercial pilot, the sole occupant, was not injured. The airplane was registered to and operated by the pilot, who was doing business as Brown's Flying Service of Drumright, Oklahoma. No flight plan was filed and visual meteorological conditions prevailed for the Title 14 CFR Part 137 local aerial application flight.
During a telephone interview conducted by the NTSB investigator-in-charge and in the attached NTSB Pilot/Operator Aircraft Accident Report, the pilot reported that the engine lost power as he was turning the airplane between spray passes. The pilot further reported that the ensuing forced landing was made to a soft field, and during the landing roll, the airplane nosed over and came to rest inverted. According to the FAA inspector who inspected the airplane at the accident site, the top wing and vertical stabilizer sustained structural damage. Examination of the radial engine, a Pratt & Whitney R-985-14B, by the FAA inspector revealed that a circumferential crack had completely separated the #4 cylinder head from the cylinder barrel.
Aircraft
- Registration
- N8819H
- Reported as
- Grumman-Schweizer G-164A
- Category
- Airplane
- Serial number
- 1539
- Airframe hours
- 4,500
- Engine
- P&W R-985-14B, 450 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Aerial application · Part 137
- Registered owner
- Max K. Brown
- Airworthiness certificate
- Special, Restricted (Special)
- Last inspection
- Annual · February 25, 1997 · 200 hours before
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
- 38
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine land, Single-engine sea
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--no waivers/lim.
- Seat
- Center
- Flight hours
- 5,504 total · 2,500 in this make and model
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 140° at 6 knots
- Visibility
- 15 statute miles
- Lowest ceiling
- None
- Temperature
- 64 °F, dew point 43 °F
- Altimeter
- 30.00 inHg
- Observed at
- LTS, 7 nm away
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 N8819H · 1
Matched to the same aircraft by N-number and date.