WPR12LA265 · Roetman Ryland K JR EAGLE
Roetman Ryland K JR EAGLE · Accident: powerplant system/component malfunction/failure while maneuvering
From Rexburg Madison County Airport (RXE) to Rexburg Madison County Airport (RXE)
Event
- NTSB case
- WPR12LA265
- 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
Roetman Ryland K JR EAGLE
- Aircraft type
- Roetman Ryland K JR EAGLE
- Category
- Airplane
- 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
- N106BD
- Operator
- Unknown
- Onboard fatalities
- Unknown
- Route
- From Rexburg Madison County Airport (RXE), Rexburg, IDTo Rexburg Madison County Airport (RXE), Rexburg, ID
- Aircraft age
- About 9 years (built 2003)
- 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
- Maneuvering · aerobatics
- 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
- Powerplant system/component malfunction/failure
- 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 oper/perf/capability
- Aircraft › Aircraft propeller/rotor
- Aircraft › Fluids/miscellaneous hardware
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The airline transport pilot, who was also the owner/ builder of the experimental aerobatic airplane, was practicing aerobatic maneuvers for an upcoming airshow. An amateur video captured a portion of the flight and accident sequence. The video shows the airplane conducting several continuous right rolls at an approximate constant altitude and pitch attitude. During the accident sequence, the airplane continued to roll, but it began to descend while maintaining a relatively level pitch attitude. When the airplane was about 100 ft above the ground, it stopped rolling and then continued to descend in a significant right-wing-down attitude. Examinations of the wreckage did not reveal any preimpact mechanical deficiencies or failures that would have precluded continued flight; however, no detailed examinations of the wreckage or any components were conducted.
The pilot reported that, while conducting the maneuver just before the accident, he "heard and felt" an uncommanded decrease in rpm, which he believed was caused by the decrease in engine oil pressure that occurs during aerobatics, and a subsequent uncommanded change in propeller blade pitch. Based on the available evidence, it is likely that, during the aerobatic maneuver, the airplane lost oil pressure, which resulted in a decrease in thrust and change in propeller blade pitch, and that the airplane had insufficient power and altitude for the pilot to recover from the maneuver. The pilot reported that he had installed an accumulator to prevent the decrease in engine oil pressure; it could not be determined why the accumulator did not function during the accident flight.
Probable cause
A loss of engine oil pressure, which led to the subsequent uncommanded loss of thrust and decrease in the propeller rpm during a low-level aerobatic maneuver.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record WPR12LA265
- Event ID
- 20120616X53520
- Case number
- WPR12LA265
- 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: local date, investigation status, coordinates. Values present in the bulk record are kept.
- The date is the local date; the NTSB stores the UTC date 2012-06-16.
- API snapshot SHA-256: a8418ea5cf3aa22c5235b07190a8e4a04fc07e774366657bb2ac5538afd99aaa; retrieved 2026-09-15T18:32:21.935Z.