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Accidents · NTSB LAX05LA146 · Final report

Robinson Helicopter Company R22A accident near Kailua-Kona, Hawaii, April 24, 2005

On April 24, 2005 at about 3:00 am local time, a Robinson Helicopter Company R22A, registered N8406J, was substantially damaged in an accident near Kailua-Kona, Hawaii (Kona International airport). It was an instructional flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

a total loss of engine power due to the failure of the engine's #3 exhaust valve due to an excessive valve guide clearance. Contributing to the accident was the failure of maintenance personnel to adequately check the valve guide clearance during the last valve guide inspection.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
April 24, 2005 · about 3:00 am local time
Place
Kailua-Kona, Hawaii · Kona International · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Robinson Helicopter Company R22A
Registration
N8406J · no longer on the register · serial 350
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The helicopter was ditched in the ocean after a complete loss of engine power. Post-accident examination of the engine revealed that the #3 cylinder's exhaust valve had failed. Because of mechanical damage and oxidation to the fracture surfaces, the specific cause of the exhaust valve failure could not be precisely determined. However, it was most likely related to overheating and non-uniform seating loads due to the severe wear and bell-mouthing of the valve guide. The bent pushrods found during the examination also indicated some valve sticking in the guides prior to failure that caused excessive loads in the pushrods. Valve stems and guides were normal wear items. Mutual wear increased the stem to guide clearances and exhaust valves, particularly the sodium filled valves utilized in the accident engine, rely on proper clearance to the guide to maintain good heat transfer properties. The most likely scenario for this failure was that the valve-to-guide clearance became so great as to impede heat transfer from the valve to the head through the guide. The valve then overheated as indicated by the decreased stem hardness and radial head cracks found during the metallurgical examination. Off center valve closure loads, due to the bell mouthing, then fractured the overheated and lower strength valve head. In May 1992, the engine manufacturer issued a service bulletin (SB) recommending engine inspections to determine the wear condition of exhaust valve and guides. The SB details procedures to assess the wear on the engine by wobbling the valve in the head. The SB recommended performing this inspection every 300 hours on helicopter engines. Engine logbooks only showed that the SB was complied with twice, once in January 2005, at 1,921.8 hours, and the last time in March 2005, at 2,204 hours total time. The last inspection was only 133.3 hours prior to the accident. The engine manufacturer reported that if performed properly this inspection method would have been successful in detecting excess valve wear. The presence of extensive lead deposits on the valve stem and in the valve spring keeper groove indicated that stem to guide clearances were relatively large allowing the passage of combustion products for an extended period of time. This suggests that the SB inspections were not performed properly.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

Flight instructor

  • Certificate: commercial pilot
  • Ratings: instructor: helicopter; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 821 in this make and model; 199 in the last 90 days; 95 in the last 30 days
  • Last flight review: June 1, 2004
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: left
  • Injury: no injuries

Dual student

  • Certificate: private
  • Ratings: rotorcraft: helicopter
  • Flight time: 113 hours in all; 113 in this make and model; 37 in the last 90 days; 20 in the last 30 days
  • Last flight review: February 1, 2005
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 2,338 hours
  • Last inspection: 100-hour inspection, April 1, 2005
  • Maximum gross weight: 1,370 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming O-320-B2C (piston); 0 hours total

The flight

  • Departed from: KOA Kailua-Kona HI at 2:50 am
  • Flight plan: none
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 220° at 9 knots
  • Visibility: 10 statute miles
  • Sky: scat at 7,000 ft
  • Temperature: 81°F (27°C), dew point 64°F (18°C)
  • Altimeter: 30.01 inHg
  • Observation at 2:53 am from PHKO

Injuries

FatalSeriousMinorNone
Crew2

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.