Stout Garry V EUROPA-TRIGEAR N133AC
16 August 2021 · Hanksville, Utah, United States · No injuries
Summary
On 16 August 2021 at about 21:15 local time, a Stout Garry V EUROPA-TRIGEAR registered N133AC was involved in an accident near Hanksville, Utah, United States. One person was on board and nobody was injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 21:15
- Classification
- Accident
- Location
- Hanksville, Utah, United States
- Coordinates
- 38.0586, -110.9611
- Aircraft
- Stout Garry V EUROPA-TRIGEAR
- Registration
- N133AC
- Category
- Airplane
- Year built
- 1999
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Personal
- Phase of flight
- Not recorded
- Route
- Halls Crossing → Manti
- Aircraft damage
- Substantial
- Weather
- VMC
- Light
- Day
- NTSB number
- WPR21LA325
People
Nobody was injured.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 1 | 0 | 0 | 0 | 1 |
Probable cause
The pilot’s installation of a non-original equipment manufactured radiator cap, which resulted in the loss of coolant and the engine’s exceedance of the maximum admissible cylinder head temperature. Contributing to the accident was the lack of suitable terrain for the forced landing.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
The pilot replaced lost fluid in the airplane engine’s cooling system with water and after a successful ground run, the pilot departed. During a “stair-stepped” climbout, the engine’s cylinder head temperature (CHT) increased into the red arc of the CHT gauge (the maximum admissible cylinder head temperature of 180°C [356°F]). The pilot immediately reduced the throttle setting to ide and elected to conduct a forced landing. The airplane sustained substantial damage to the wings and fuselage after impacting rough terrain during the landing. Postaccident examination of the cooling system revealed that system components were secured and void of all fluid. Testing of the accident radiator cap revealed that it was a non-original equipment manufactured (OEM) part by a third-party vendor and that the pressure relief valve opened and released air pressure about 0.2 bar (3 psi), less than the manufacturer’s recommended coolant system maximum pressure value of 1.2 bar (18 psi). It is likely that the lack of pressure created by the non-OEM radiator cap reduced the coolant boiling point and system pressure. The pressure reduction and lowering of the boiling point would have allowed the coolant to evaporate, leading to a loss of coolant in the system and the engine’s exceedance of the maximum admissible cylinder head temperature of 180°C (356°F).
Quoted verbatim from the NTSB record.
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 27 Nov 2021 | Bagley Curtis Lynn RANS S-6S COYOTE II | Fairfield, Utah, United States | West Desert Aviators | No injuries | - |
| 2 Jan 2021 | Cessna P210N | Moab, Utah, United States | Nash LLC | No injuries | - |
| 1 Jan 2021 | Piper PA-20-135 | Riverside, Utah, United States | - | No injuries | - |
| 27 Mar 2021 | Aviat A-1 | Ogden, Utah, United States | - | No injuries | - |
| 13 Jan 2021 | Hughes 269C | Spanish Fork, Utah, United States | Trike Industries LLC | No injuries | - |
| 18 May 2021 | Goodsell Lynn A CLASSIC 4 | Richmond, Utah, United States | - | No injuries | - |