WPR13LA315 · Robinson Helicopter Company R22 Beta II
Upper Limit Aviation Robinson Helicopter Company R22 Beta II · Accident: loss of control in flight en route
From 36U · Heber City, UT to Salt Lake City International Airport (SLC)
Narrative check · The NTSB narrative appears to contradict this record's injuries. Values are shown as recorded, not corrected; compare with the narrative.
Event
- NTSB case
- WPR13LA315
- 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
Robinson Helicopter Company R22 Beta II
- Aircraft type
- Robinson R22
- 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
- N712U
- Operator
- Upper Limit Aviation
- Onboard fatalities
- Unknown
- Route
- From 36U · Heber City, UTTo Salt Lake City International Airport (SLC), Salt Lake City, UT
- Aircraft age
- About 9 years (built 2004)
- 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 · descent
- 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 control in flight
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Destroyed
Cause areas
- Aircraft › Aircraft oper/perf/capability
- Personnel issues › Action/decision
Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.
NTSB narrative
The flight instructor reported that the outbound training flight on the morning of the accident followed roads through mountain passes. For the return flight, the flight instructor decided to take a more direct route and fly over 11,000-foot-high mountainous peaks. The pilot undergoing instruction was controlling the helicopter during the climb, which was uneventful. As the helicopter crested the peak, the pilot initiated a descent and then began to raise the collective to reduce the descent rate; however, as he did so, the rotor speed began to decay, and the low rotor rpm warning sounded. The flight instructor took over the flight controls but was unable to arrest the descent, and he subsequently chose to perform a forced landing to rocky terrain. The helicopter struck the ground, tumbled, and was destroyed; both occupants sustained serious injuries.
The helicopter was operating at a density altitude equal to or just above the helicopter's maximum operating density altitude of 14,000 feet. At the altitude of the accident site, the helicopter was not capable of hovering in-ground-effect; therefore, it was unlikely that a landing could have been successfully accomplished in the rocky terrain. Further, after cresting the peak, the helicopter likely encountered downdrafts due to the mountainous terrain surrounding the accident site, which further degraded the helicopter's performance. A postaccident examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation.
Probable cause
The flight instructor's decision to follow a route over mountainous terrain in conditions that exceeded the helicopter’s ability to maintain terrain clearance.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR13LA315
- Event ID
- 20130708X54053
- Case number
- WPR13LA315
- 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: cf6f8d4c0d30378e634e6b05836bd3f4e86d2df7073b63266e01f6282ca5e899; retrieved 2026-09-15T22:08:58.461Z.