# NTSB SEA02FA064: Cessna 182E, N3184Y, Red Lodge, MT, April 6, 2002

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Field investigation · Final report
- Date: April 5, 2002, 19:10 local (Apr 6, 2002, 02:10 UTC)
- Place: Red Lodge, MT
- Coordinates: 45.1875, -109.267219
- Nearby events: https://openairdocs.org/map.md?lat=45.1875&lon=-109.2672&mi=10
- Phase of flight: [Landing](https://openairdocs.org/ntsb-phases/550) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 1 uninjured
- Status: Completed, report April 18, 2003
- Report: Approved by Office Director
- Parties: FAA FSDO
- NTSB case key (mKey): 54492
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=SEA02FA064
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/54492/pdf
- NTSB docket: https://data.ntsb.gov/Docket?ProjectID=54492
- Page: https://openairdocs.org/ntsb/SEA02FA064

## Probable cause

Long term fatigue of the nose landing gear strut fork initiated by side loading which resulted in the separation of the fork from the strut and the consequent collapse of the nose gear.  A contributing factor was the ditch the aircraft traversed during the ground roll.

## Sequence of events

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

- Airframe/component/system failure/malfunction, landing - roll
  - landing gear,nose gear strut - separation
  - landing gear,nose gear strut - fatigue (cause)
- Nose gear collapsed, landing - roll
- Loss of control - on ground/water, landing - roll
- On ground/water encounter with terrain/water, landing - roll
  - terrain condition - ditch (contributing factor)

## Analysis

The pilot executed a normal 20-degree flap landing in calm wind conditions to the 4,000 foot long runway.  During the rollout the nose wheel of the Cessna 182E separated and the aircraft veered left off the runway.  Post-crash metallurgical examination of the nose gear fork fracture surface revealed thumbnail features typical of fatigue cracking that emanated from five different fracture planes.  The fatigue regions were very smooth, contained crack arrest positions, and were darkly discolored.   The exterior surface of the fork showed no evidence of corrosion pitting or mechanical damage adjacent to the fatigue regions.

## Factual narrative

HISTORY OF FLIGHT

On April 5, 2002, approximately 1910 mountain standard time, a Cessna 182E, N3184Y, registered to an individual and being flown by a private pilot sustained substantial damage during the landing roll on runway 16 at the Red Lodge airport, Red Lodge, Montana.  The pilot was uninjured.  Visual meteorological conditions existed and no flight plan had been filed.  The flight, which was personal, was operated under 14CFR91, and originated from Hailey, Idaho, about 1710.

The pilot reported that upon executing a 20-degree flap landing on the 4,000-foot long, asphalt runway, he held the nose wheel off the deck until the airplane had slowed.  As he allowed the nose wheel to touch the runway about midfield, the aircraft veered sharply to the left and the pilot was unable to prevent the aircraft from departing the left side of the runway.  He reported that his airspeed was about 20 knots when the nose wheel touched down and he experienced the loss of control.

PERSONNEL INFORMATION

The airplane single-engine land rated private pilot reported a total of approximately 151 hours of flight experience of which about two-thirds were in the Cessna 182.  He also reported a total of 45 hours of pilot-in-command time, all in the Cessna 182.

AIRCRAFT INFORMATION

N3184Y, a Cessna 182E "Skylane" was manufactured in 1962 and had an approximate total of 6,089 hours on the airframe at the time of the accident.  The following is a chronology of significant nose wheel maintenance (other than lubrication and tire replacement) from the aircraft's manufacture:

DATE:		ACTION:

08/11/65          Installed new shimmy damper

02/02/69          Rebuilt nose gear

06/29/72          Rebuilt nose gear strut

12/04/75          Installed new shimmy damper

12/13/76          Rebuilt nose gear strut

05/25/80          Remove/replace shimmy nose steering collar & support ring

10/16/97          Installed new bolts in nose gear scissors + nose wheel races & bearings

Additionally, the airframe logbook indicated that on August 27, 1998, the aircraft's Continental O-470 engine was removed and a Continental IO-520-F48B was installed in its place.  Additionally, the original two-blade propeller was removed and replaced with a three-blade propeller and the engine mounts were changed, all three changes per Supplemental Type Certificates.  The basic weight of the IO-520 engine is approximately 51 pounds less than the weight of the O-470 engine.

METEOROLOGICAL INFORMATION

The pilot reported that the winds were calm during his landing at Red Lodge.  The aviation surface weather observation for Cody, Wyoming, 41 nautical miles east-southeast reported winds from 240 degrees magnetic at 4 knots.

WRECKAGE AND IMPACT INFORMATION

The aircraft departed runway 16 and came to rest a short distance east of the eastern edge of the runway pavement in grass and light snow.  The approximate location of the aircraft's final resting place was 45 degrees 11.25 minutes north latitude and 109 degrees 16.04 minutes west longitude.

The aircraft crossed a shallow ditch approximately 2-3 feet deep running parallel to the east side of the runway.  The pilot reported that as the aircraft's left wheel entered the ditch the aircraft's left wing impacted the ground (refer to photograph 1).  The aircraft came to rest on both main wheels and the nose wheel strut with its longitudinal axis oriented approximately 45 degrees to the runway (refer to photograph 2).  The pilot found the nose wheel with the separated portion of nose wheel fork approximately 150 yards beyond the aircraft.

TESTS AND RESEARCH

The separated portion of the nose gear fork (that portion which remained attached to the nose wheel) was shipped to the Safety Board's Materials Laboratory where the component was subjected to metallurgical examination.  The examination revealed that the fork fractured transversely in the attachment area of the shock strut assembly.  Visual examination of the fracture revealed thumbnail features typical of fatigue cracking that emanated from five different fracture planes at the upper outer surface.  The fatigue regions were very smooth, contained crack arrest positions, and were darkly discolored.  The maximum depth of the fatigue cracks was 0.2 inch.  One of the fatigue cracks intersected the forge parting plane.  The exterior surface of the fork showed no evidence of corrosion pitting or mechanical damage adjacent to the fatigue regions.  Fracture surfaces outside the fatigue regions showed ductile dimple features typical of overstress separation (refer to Metlab Report 02-53).

ADDITIONAL INFORMATION

On-site examination of the wreckage was conducted on April 8, 2002, and the nose wheel and attached fork sections were retained for further examination at that time.  The retained components were returned to Mr. Bruce Allen via Federal Express on June 24, 2002 (refer to attachment FE-I).

## Aircraft

- Registration: [N3184Y](https://openairdocs.org/aircraft/N3184Y), registered now, S/N 18254184, built 1962 (OpenAirDocs)
- Reported make and model: Cessna 182E
- Registry model: [Cessna 182E](https://openairdocs.org/model/cessna-182e) (registry code 2072712) (OpenAirDocs)
- Registry engine: [Continental O-470 series](https://openairdocs.org/engine/continental-o-470-series) (registry code 17026, reciprocating) (OpenAirDocs)
- Category: Airplane
- Serial number: 18254184
- Airframe hours: 6089
- Engines: Continental IO-520-F48B 300 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Operator: Allen, Bruce L.
- Registered owner: Kraynick, Michael J.
- Airworthiness certificate: Standard, Normal
- Last inspection: Annual, August 23, 2001, 90 hours before
- Departed: SUN, Hailey, ID
- Destination: RED, Red Lodge, MT
- Airport: RED, Red Lodge, runway 16, 4,000 × 75 ft, asphalt

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 48; injuries: none; private; airplane ratings: single-engine land; medical: class 3, valid medical--no waivers/lim.; last flight review October 15, 2001; seat: left; flight hours: 151 total, 95 in this make and model, 45 as pilot in command, 15 in the last 90 days, 8 in the last 30 days, 0 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Dusk
- Wind: 240° at 4 knots
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 55 °F, dew point 18 °F
- Altimeter: 29.87 inHg
- Observed at: COD, 41 nm away

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 20020405005609A](https://openairdocs.org/incident/20020405005609A), Apr 5, 2002: Cessna 182E, Red Lodge, MT, No damage. (-23)The PIC stated that on landing at Red Lodge, Montana, the nose strut fork fractured causing departure of nose wheel. Aircraft veered left of runway into a…

## Other investigations on N3184Y (1)

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.

- [NTSB DEN67D0220](https://openairdocs.org/ntsb/DEN67D0220), Feb 19, 1967: Cessna 182 (N3184Y), Regina, NM, substantial damage

## Docket (5 files)

The files NTSB released with the investigation on February 28, 2003, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=54492. 832 KB in all.

- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1 (item 1, .PDF, 333 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40424524&FileExtension=.PDF&FileName=Pilot%2FOperator%20Aircraft%20Accident%20Report,%20NTSB%20Form%206120.1-Redacted.PDF
- Materials Laboratory 15 - Factual Report of Group Chairman (item 2, .PDF, 2 photos, 62 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40160028&FileExtension=.PDF&FileName=Materials%20Laboratory%2015%20-%20Factual%20Report%20of%20Group%20Chairman-Master.PDF
- Attachment FE-I (item 3, .PDF, 49 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40424525&FileExtension=.PDF&FileName=Attachment%20FE-I-Redacted.PDF
- Photo 1. A view looking west at N3184Y where it came to rest on the east side of runway 16. Note the separated nose wheel and left wing leading edge damage. (item 4, .PDF, 180 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40177637&FileExtension=.PDF&FileName=Photo%201.%20%20A%20view%20looking%20west%20at%20N3184Y%20where%20it%20came%20to%20rest%20on%20the%20east%20side%20of%20runway%2016.%20Note%20the%20separated%20nose%20wheel%20and%20left%20wing%20leading%20edge%20damage.-Master.PDF
- Photo 2. A head-on view of the nose gear strut and fork assembly following the accident. Note the separation point (arrow) and deformed opposite fork leg. (item 5, .PDF, 209 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40177638&FileExtension=.PDF&FileName=Photo%202.%20%20A%20head-on%20view%20of%20the%20nose%20gear%20strut%20and%20fork%20assembly%20following%20the%20accident.%20%20Note%20the%20separation%20point%20(arrow)%20and%20deformed%20opposite%20fork%20leg.-Master.PDF

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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