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WPR12LA265 · Roetman Ryland K JR EAGLE

15 Jun 2012 · Rexburg, ID, United States

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)

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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

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.