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Papillon Airways Eurocopter AS 350 B2 incident

3 Mar 2009 · Peach Springs, AZ, United States

Eurocopter AS 350 B2 · Incident: loss of engine power (total) en route

From 61B · Boulder City, NV to Grand Canyon, AZ

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Event

NTSB case
WPR09IA140
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
Incident
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
Charter & commuter
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

Eurocopter AS 350 B2

Aircraft type
Eurocopter AS-350
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
N197AE
Onboard fatalities
Unknown
Route
From 61B · Boulder City, NVTo Grand Canyon, AZ
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 135: Air Taxi & Commuter
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 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
Minor

Cause areas

  • Aircraft › Aircraft power plant

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The pilot heard a loud pop while descending into a canyon and had a loss of main rotor rpm. The pilot entered an autorotation to an open area and landed successfully. Examination of the engine revealed that it was intact and exhibited minimal impact related damage. Disassembly of the engine revealed that the rear bearing support housing was intact and undamaged. The number three bearing was intact, however, did not rotate freely. The inner race and ball bearings exhibited heavy rub marks and thermal damage and the outer race exhibited thermal damage. No oil residue was observed on the bearing components. The damage to the number three bearing was consistent with oil starvation. Debris was observed within the oil scavenge passage of the rear bearing support housing near the oil feed ring assembly. The rear bearing support housing (RBSH) was removed and placed on a flow test bench. The RBSH assembly flowed approximately one-half of the normal oil flow rate and irregular flow patterns were observed. Examination of the RBSH revealed no significant damage; however, the oil passages that feed oil to the number three bearing assembly contained deposits that most likely obstructed oil flow to the bearing. Analysis of the deposited material found that it was composed of coked synthetic oil. Prior to the incident, the engine manufacturer issued an Operating Information Letter that outlined recommended engine shutdown procedures. The two-step process consisted of a two minute idle period prior to shutdown followed after shutdown by motoring the engine with the starter motor for 10 seconds. The Operating Information Letter indicated that not following the procedures could result in coke build up in the number 2 and number 3 bearing oil jets and sump area. The operator reported that company pilots were instructed to comply with the recommended engine idle cool down procedure; however, company policy did not direct pilots to comply with the recommended post shutdown motoring after engine shutdown procedure due to concerns about depletion of oil in the engine oil reservoir. It was not determined if the bearing failure was a direct result of the operator not complying with the complete recommended shutdown procedure outlined by the engine manufacturer.

Probable cause

A loss of engine power due to the failure of the number three engine bearing as a result of oil starvation due to coked oil obstructing the oil passages.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record WPR09IA140
Event ID
20090304X61906
Case number
WPR09IA140
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: aab4eb36aa4ab60dac2248de0df00a9bf800b2bee4b933081599a04dbc80cf80; retrieved 2026-09-15T10:48:11.029Z.