# NTSB DEN00LA099: Cessna TR182, N738FN, Milford, UT, May 31, 2000

- Type: NTSB accident investigation
- Classification: Accident · Minor injuries · Limited investigation · Final report
- Date: May 31, 2000, 16:50 local (22:50 UTC)
- Place: Milford, UT
- Coordinates: 38.379791, -112.929183 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=38.3798&lon=-112.9292&mi=10
- Phase of flight: [Enroute](https://openairdocs.org/ntsb-phases/400) (OpenAirDocs' grouping)
- Highest injury: Minor injuries
- Injuries: 1 minor
- Status: Completed, report March 2, 2001
- Report: Approved by Office Director
- NTSB case key (mKey): 51113
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=DEN00LA099
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/51113/pdf
- Page: https://openairdocs.org/ntsb/DEN00LA099

## Probable cause

The failure of the turbocharger scavenging pump resulting in the total failure of the engine, and the pilot's failure to compensate for wind conditions that led him to over fly the runway during his forced landing.  Factors were the pilot's diverted attention due to smoke in the cockpit, and the tailwind weather condition.

## Sequence of events

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

- Airframe/component/system failure/malfunction, cruise - normal
  - lubricating system,oil scavenge pump - failure,total (cause)
  - powerplant - failure,total (cause)
- Forced landing, emergency descent/landing
  - compensation for wind conditions - inadequate, pilot in command (cause)
  - diverted attention, pilot in command (contributing factor)
  - weather condition - tailwind (contributing factor)
- On ground/water encounter with terrain/water, emergency descent/landing
  - terrain condition - berm

## Analysis

The pilot said that the engine began to run rough, and he could smell smoke in the cockpit.  He said that the smoke got worse, and he shut off the master switch.  He saw the airport, headed for it, and his engine power began to fail.  He attempted to land on runway 16, with a 22 knot gusting to 26 knot tailwind, but was too high.  The pilot said he turned right, to approximately 180 degrees, to miss some buildings.  He landed approximately 1,000 feet from the departure end of the runway in scrub-covered terrain.  The airplane impacted a berm, and nosed over.  The airplane's vertical stabilizer, left wing, and fuselage were damaged.  Postaccident examination of the engine by a mechanic revealed that the turbocharger's oil scavenger pump had failed.  The mechanic said that the scavenger pump's failure would cause the engine's oil to pass overboard.

## Factual narrative

On May 31, 2000, approximately 1650 mountain daylight time, a Cessna TR182, N738FN, was substantially damaged during a forced landing to Milford Municipal Airport, Milford, Utah.  The private pilot, sole occupant in the airplane, received minor injuries.  The airplane was being operated by the pilot under Title 14 CFR Part 91.  Visual meteorological conditions prevailed for the cross-country flight that originated from Cedar City, Utah, approximately 50 minutes before the accident.  No flight plan had been filed.

The pilot said that the engine began to run rough, and he could smell smoke in the cockpit.  He said that the smoke got worse, and he shut off the master switch.  He saw the airport, headed for it, and his engine power began to fail.  He attempted to land on runway 16, with a 22 knot gusting to 26 knot tailwind, but was too high.  The pilot said he turned right, to approximately 180 degrees, to miss some buildings.  He landed approximately 1,000 feet from the departure end of the runway in scrub-covered terrain.  The airplane impacted a berm, and nosed over.  The airplane's vertical stabilizer, left wing, and fuselage were damaged.

Postaccident examination of the engine by a mechanic revealed that the turbocharger's oil scavenger pump had failed.  He said that the scavenger pump's failure would cause the engine's oil to pass overboard.

## Aircraft

- Registration: [N738FN](https://openairdocs.org/deregistered/N738FN-2001-03-20), registration cancelled 2001-03-20, S/N R18200921 (OpenAirDocs)
- Reported make and model: Cessna TR182
- Registry model: [Cessna TR182](https://openairdocs.org/model/cessna-tr182) (registry code 2072735) (OpenAirDocs)
- Category: Airplane
- Serial number: R18200921
- Airframe hours: 1550
- Engines: Lycoming O-540-L3C5D 235 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Registered owner: Leon C. Vansickle
- Airworthiness certificate: Standard, Normal
- Last inspection: Continuous airworthiness, May 31, 2000, 1 hours before
- Departed: CDC, CEDAR CITY, UT
- Destination: PVU, PROVO, UT
- Airport: Milford Municipal Airport, runway 16, 5,000 × 75 ft, asphalt

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 48; private; airplane ratings: single-engine land; medical: class 3, valid medical--w/ waivers/lim; seat: left; flight hours: 236 total, 144 in this make and model, 173 as pilot in command, 87 in the last 90 days, 31 in the last 30 days, 2 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 360° at 22 knots, gusting 26
- Visibility: 10 statute miles
- Lowest ceiling: none
- Temperature: 82 °F, dew point 28 °F
- Altimeter: 29.00 inHg
- Observed at: MLF

## 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 20000531011779A](https://openairdocs.org/incident/20000531011779A), May 31, 2000: Cessna TR182, Milford, UT, No damage. (-23) Engine turbocharger and scavenger pump failed causing a loss in engine oil, and power. Pilot decided to make an emergency landing due to the smoke from…

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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