Bell OH-58A+ N7UT
11 February 2000 · Woods Cross, Utah, United States · Fatal
Summary
On 11 February 2000 at about 21:04 local time, a Bell OH-58A+ registered N7UT was involved in an accident near Woods Cross, Utah, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.
The record
- Date
- at 21:04
- Classification
- Accident
- Location
- Woods Cross, Utah, United States
- Nearest airport
- Skypark (BTF)
- Coordinates
- 40.8892, -111.9308
- Aircraft
- Bell OH-58A+
- Registration
- N7UT
- Category
- Helicopter
- Engines
- 1
- Operator
- Not recorded
- Operating rule
- Part 91: General Aviation
- Purpose of flight
- Public Use
- Phase of flight
- Not recorded
- Aircraft damage
- Destroyed
- Weather
- VMC
- Light
- Day
- NTSB number
- DEN00GA050
People
2 people died.
| On board | Died | Serious | Minor | Uninjured |
|---|---|---|---|---|
| 2 | 2 | 0 | 0 | 0 |
Probable cause
The pilot's failure to roll throttle back on (return the power to the normal operating range) during an attempted power recovery from an autorotation, and his subsequent failure to maintain aircraft control.
Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.
Read the full NTSB narrative
The pilot of the helicopter was to perform an autorotation during a maintenance flight to perform a functional check of the free-wheeling unit. A witness observed the helicopter at 100 to 150 feet agl, and he said that the main rotor blades 'stopped' and the aircraft started a slow spiral to the left, nose down. He further said that the helicopter was shaking violently, and its skids were flexing in and out. Postcrash examination revealed that the fuel control pointer, on the fuel control, was slightly above flight idle. Both cockpit throttles were observed positioned in slightly above the flight idle position. The helicopter's power analyzer and recorder (PAR) documented that at the time of impact, the engine's torque (TRQ) was at 13.5% and the main rotor speed (NR) was at 65.8%. The procedure for a power recovery from an autorotation is to smoothly roll throttle back on, confirm rotor and N2 needles are joined and in normal operating range, and simultaneously pull up collective while applying left pedal.
Quoted verbatim from the NTSB record.
Other Bell OH-58A accidents
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 16 Jul 1999 | Bell OH-58A | Bastrop, Louisiana, United States | - | No injuries | - |
| 27 Sep 2001 | Bell OH-58A | Sevierville, Tennessee, United States | - | No injuries | - |
| 26 Sep 1999 | Bell OH-58A | Ratcliff, Texas, United States | - | No injuries | - |
| 17 May 1999 | Bell OH-58A | Poplar Bluff, Missouri, United States | - | Fatal | 2 |
| 6 Nov 1999 | Bell OH-58A | La Puente, California, United States | - | Minor injuries | - |
| 3 Apr 2001 | Bell OH-58A | Lakeland, Florida, United States | - | No injuries | - |
Other accidents in this area
| Date | Aircraft | Location | Operator | Outcome | Died |
|---|---|---|---|---|---|
| 13 Aug 2000 | Cessna 172N | Kamas, Utah, United States | - | Fatal | 1 |
| 10 Jul 2000 | Cessna 150J | Spanish Fork, Utah, United States | - | Minor injuries | - |
| 25 May 2000 | Rosenvall AVID MK IV | Salina, Utah, United States | - | No injuries | - |
| 2 Jun 2000 | Culver LFA | Moab, Utah, United States | A Pair of Jacks, Inc. | No injuries | - |
| 4 Jun 2000 | Schumacher SWEARINGEN SX-300 | Richfield, Utah, United States | - | Minor injuries | - |
| 12 Nov 2000 | Cessna 175 | Hanksville, Utah, United States | - | Fatal | 1 |