# NTSB NYC06IA226: Cessna 206F, N8411Q, Matinicus Islnd, ME, September 1, 2006

- Type: NTSB incident investigation
- Classification: Incident · No injuries · Incident investigation · Final report
- Date: September 1, 2006, 12:30 local (16:30 UTC)
- Place: Matinicus Islnd, ME
- Coordinates: 44.693134, -69.381912 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=44.6931&lon=-69.3819&mi=10
- Phase of flight: [Standing](https://openairdocs.org/ntsb-phases/150) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 3 uninjured
- Status: Completed, report February 28, 2008
- Report: Approved by Office Director
- Parties: FAA/FSDO
- NTSB case key (mKey): 64590
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=NYC06IA226
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/64590/pdf
- Page: https://openairdocs.org/ntsb/NYC06IA226

## Probable cause

An engine kick back of undetermined origin during engine start.

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- Miscellaneous/other, standing - starting engine(s)
  - reason for occurrence undetermined
  - miscellaneous,engine - fractured (cause)

## Analysis

After engine start, the pilot heard "an abnormal engine mechanical noise."  He shut down the engine and requested a mechanic.  During a subsequent engine start, the mechanic confirmed the mechanical engine noise, and the engine was again shut down.  Hand propping revealed that the engine would sometimes "mechanically jam," and further examination revealed the fracture of two crankshaft gear teeth.  Both gear teeth exhibited signatures consistent with overload.  Corresponding starter adapter gear teeth, that would have meshed with the crankshaft gear teeth during the startup, were cracked on the loaded side.  All evaluated metallurgical requirements were met, including core hardness, surface hardness and case depth.  Although a single "kick back" while cranking could cause the failure of components of the cranking system, there was no evidence as to why a kick back may have occurred.

## Factual narrative

On September 1, 2006, about 1230 eastern daylight time, a Cessna 206F, N8411Q, operated by Waters Aero Marine, incurred minor damage during an engine start at Matinicus Island Airport (35ME), Matinicus Island, Maine.  The certificated airline transport pilot and the two passengers were not injured.  Visual meteorological conditions prevailed.  The on-demand air taxi flight was operating on a company visual flight rules flight plan to Knox County Airport (RKD), Owls Head, Maine, under 14 Code of Federal Regulations Part 135.

According to the pilot, as soon as the engine began idling after start, he heard "an abnormal engine mechanical noise."  He then shut down the engine and requested a mechanic.

During a subsequent engine start, the mechanic confirmed the mechanical engine noise, and the engine was again shut down.  Hand propping revealed that the engine would sometimes "mechanically jam," and that the alternator drive pulley would turn freely at various points during engine rotation.  Further examination revealed a damaged crankshaft gear with two teeth missing, and an "abnormal wear groove on an adjoining third tooth."

The Teledyne Continental IO-520-series engine was forwarded to the manufacturer for a teardown examination under National Transportation Safety Board oversight.  Aside from the missing crankshaft gear teeth, no other gear damage was noted.  The oil sump was removed and the two crankshaft gear teeth were recovered.  The oil sump did not contain any additional debris or foreign material.

Magneto timing was found to be 25 degrees before top dead center on the left and 23 degrees before top dead center on the right.  Both magnetos exhibited normal impulse coupling engagement when rotated in the normal direction of rotation.  Installation of the magnetos on a test bench revealed that the left magneto impulse coupling would disengage at 350 rpm and the right magneto impulse coupling would disengage at 360 rpm.

A metallurgical examination of the crankshaft gear, the starter adapter gear, and the two fractured crankshaft gear teeth was performed by the engine manufacturer.  According to the manufacturer's report, all evaluated metallurgical requirements were met, including core hardness, surface hardness, and case depth.  Both crankshaft gear teeth exhibited signatures consistent with overload.  Corresponding starter adapter gear teeth, that would have meshed with the crankshaft gear teeth during startup, exhibited "fine" cracking on the loaded side.

Teledyne Continental Motors (TCM) Mandatory Service Bulletin MSB94-8C required that magneto timing be performed in accordance with manufacturer instructions every 100 hours.  It also noted: "CAUTION: A single 'kick back' while cranking can cause failure of components of the cranking system.  Kick back can be caused by intermittent operation of the impulse couplings."  The Bulletin also noted that for the IO-520-series engine, both magnetos should be set at 22 degrees before top dead center.

The engine had 167 hours since rebuild by TCM, and 10 hours since the annual/100 hour inspection.

No additional information was available to determine if any maintenance or pilot actions might have resulted in a kick back.

## Aircraft

- Registration: [N8411Q](https://openairdocs.org/deregistered/N8411Q-2008-06-25), registration cancelled 2008-06-25, S/N U20603271, built 1976 (OpenAirDocs)
- Reported make and model: Cessna 206F
- Registry model: [Cessna U206F](https://openairdocs.org/model/cessna-u206f) (registry code 2073333) (OpenAirDocs)
- Registry engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032, reciprocating) (OpenAirDocs)
- Category: Airplane
- Serial number: U206F03271
- Airframe hours: 7198
- Engines: Teledyne Continental IO-520-F 300 horsepower reciprocating
- Damage: Minor damage
- Flight: Part 135
- Operator: Waters Aero-Marine, doing business as Penobscot Island Air
- Registered owner: Telford Aviation, Inc.
- Airworthiness certificate: Standard, Normal
- Last inspection: 100 hour, August 1, 2006, 10 hours before
- Departed: 45ME, Maticus Island, ME
- Destination: RKD, Owls Head, ME
- Flight plan: Company VFR
- Airport: 35ME, Matinicus Island Airport

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 64; injuries: none; airline transport; airplane ratings: multi-engine land, single-engine land; instrument ratings: airplane; medical: class 2; last flight review September 1, 2005; seat: left; flight hours: 9,000 total, 2,000 in this make and model, 8,500 as pilot in command, 184 in the last 90 days, 71 in the last 30 days, 3 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: calm
- Visibility: 20 statute miles
- Temperature: 64 °F, dew point 52 °F
- Altimeter: 30.00 inHg

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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