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ERA11IA320 · Robinson Helicopter Company R22 MARINER

29 May 2011 · Redding, CT, United States

Robinson Helicopter Company R22 MARINER · Incident: system/component malfunction/failure (non-power) en route

From Kingston-Ulster Airport (20N) to Martha's Vineyard Airport (MVY)

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Event

NTSB case
ERA11IA320
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
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 MARINER

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
N8313E
Operator
Shevah Avi
Onboard fatalities
Unknown
Route
From Kingston-Ulster Airport (20N), Kingston, NYTo Martha's Vineyard Airport (MVY), Vineyard Haven, MA
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 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
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
System/component malfunction/failure (non-power)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
None

Cause areas

  • Aircraft › Aircraft propeller/rotor
  • Personnel issues › Task performance

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

NTSB narrative

The pilot stated that he felt an abnormal vibration in the helicopter during cruise flight. He performed a precautionary landing to residential driveway. Postincident examination revealed that the tail rotor teeter hinge bolt had fractured completely due to fatigue and that there was no torque stripe on the bolt to help identify possible movement. The manufacturer’s preflight inspection checklist required the pilot to verify that the tail rotor teeter hinge bolt does not rotate. When asked about preflight inspections, the pilot stated that he does not always use the manufacturer's preflight checklist. Maintenance records show that the most recent annual inspection was performed about 4 weeks before the incident. According to the manufacturer's maintenance procedures, during an annual inspection, a mechanic should verify that the tail rotor teeter hinge bolt remains stationary when teetering the hub. Also, it is recommended that a mechanic applies a torque stripe to the bolt. In addition, the maintenance manual contained an unboxed warning message about the importance of the correct installation of the tail rotor to prevent a failure of the teeter hinge bolt and loss of the tail rotor.

Probable cause

The pilot's inadequate helicopter preflight inspection and the mechanic’s inadequate annual inspection, both of which failed to detect a worn bolt in the tail rotor teeter hinge prior to its fracture due to fatigue.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA11IA320
Event ID
20110601X42124
Case number
ERA11IA320
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, damage. 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: 9888c1a03e1bd101a386c5752c8161e2539e27631fd2d82575a320a53be5f029; retrieved 2026-09-15T16:13:58.167Z.