WPR11LA373 · Rotorway EXEC 162F
Rotorway EXEC 162F · Accident: loss of engine power (total) en route
From Chino Airport (CNO) to Chino Airport (CNO)
Event
- NTSB case
- WPR11LA373
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Rotorway EXEC 162F
- Aircraft type
- Rotorway EXEC
- Category
- Helicopter
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N162CT
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Chino Airport (CNO), Chino, CATo Chino Airport (CNO), Chino, CA
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- En route · cruise
- Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Loss of engine power (total)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Aircraft › Aircraft power plant
- Personnel issues › Task performance
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The flight instructor/owner of the experimental amateur-built helicopter took the rotorcraft-rated private pilot on an informal demonstration flight. The two spent about 40 minutes conducting traffic pattern work at a local airport and then departed the area, flying about 500 feet above ground level. The private pilot was the pilot flying. When the helicopter was about 7 miles from the airport, the pilot noticed that the engine "sputtered," and called it to the attention of the owner, who then took control of the helicopter. The engine ceased operating about the same time. The owner initiated a 180-degree autorotation to a vacant field. Due to some forward speed at touchdown, the landing skids dug into the turf and the helicopter pitched nose down. The main rotor struck the ground and also severed the tail boom, and the helicopter rolled onto its left side. Postaccident examination indicated that there was less than 1 gallon of fuel remaining on board.
The manufacturer's pilots operating handbook did not contain any fuel consumption rate information; the only reference to range or endurance was the statement "Range with maximum fuel at optimum power 180 miles/2 hrs." The owner reported that he began the flight with 17 gallons (the maximum quantity) , and that the engine consumed about 9 gallons per hour; he did not specify the source of that information or the power setting or flight mode for that consumption rate. Since the fuel consumption rate for takeoffs and traffic pattern work can be significantly higher than that for cruise flight at "optimum power," the endurance of the helicopter during the accident flight would have been commensurately less than 2 hours. The helicopter was equipped with a fuel quantity gauge and cockpit instrumentation also provided a means for a pilot to determine the approximate remaining fuel quantity in flight by selecting the "fuel used"' option on the cockpit display. Neither the pilot nor the owner reported using either means to check or monitor fuel quantity during the flight.
Probable cause
A total loss of engine power due to fuel exhaustion as a result of both the owner's and the pilot's failure to determine or monitor the remaining fuel quantity during the flight. Contributing to the accident was the manufacturer's lack of fuel consumption rate data for planning purposes.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR11LA373
- Event ID
- 20110806X05109
- Case number
- WPR11LA373
- Dataset
- full-current
- Source SHA-256
- 5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: 14ebdcc70d0e36981767b6f8b2428903eb9904f2b6ec5492466e77afbcb9cbd7; retrieved 2026-09-15T16:34:39.625Z.