# NTSB DFW07CA098: Flagg Kitfox IV, N674F, Centerville, TX, April 28, 2007

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Data collection · Final report
- Date: April 28, 2007, 18:00 local (23:00 UTC)
- Place: Centerville, TX
- Coordinates: 31.3047222222222, -95.7963888888889
- Nearby events: https://openairdocs.org/map.md?lat=31.3047&lon=-95.7964&mi=10
- Phase of flight: [Initial climb](https://openairdocs.org/ntsb-phases/350) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 1 uninjured
- Status: Completed, report June 27, 2007
- Report: Approved by Office Director
- Parties: Houston, Texas
- NTSB case key (mKey): 65656
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=DFW07CA098
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/65656/pdf
- Page: https://openairdocs.org/ntsb/DFW07CA098

## Probable cause

The loss of engine power due to the failure of the air induction ducting.  A contributing factor was the lack of suitable terrain for the forced landing.

## Sequence of events

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

- Loss of engine power(total) - mech failure/malf, takeoff - initial climb
  - induction air ducting - failure (cause)
- Forced landing, emergency descent/landing
- In flight collision with terrain/water, emergency descent/landing
  - terrain condition - none suitable (contributing factor)
  - object - tree(s)
- Loss of control - in flight, emergency descent/landing

## Analysis

The 80-horsepower engine on the single-engine experimental airplane lost power during the initial takeoff climb from runway 06.  The 133-hour private pilot added that the engine began sputtering and running rough during the initial climb.  The pilot added that he tried to pull the choke and alter the throttle settings in an attempt to regain engine power, to no avail.  The pilot initiated a forced landing to a nearby clearing; however, the pilot did not have sufficient altitude and the airplane landed in trees.  The airplane came to rest suspended in trees in a near vertical nose low attitude.  The pilot was able to exit the airplane without injuries.  Post-accident inspection of the engine revealed that the carburetor rubber flange coupler had failed, which resulted in the reported loss of engine power.  The pilot added that the coupler (part number 267788) needs to have Kevlar material added in the injection mold process to prevent similar mishaps.  The airplane sustained structural damage to both wings.  The longeron and horizontal stabilizer were both bent.  The airplane and engine were reported to have accumulated a total of 275-hours since new.  The weather at the nearest weather reporting station located approximately 29 miles to the north north-east of the accident site reported calm winds, clear skies, and 20-statute mile visibility.

## Factual narrative

The 80-horsepower engine on the single-engine experimental airplane lost power during the initial takeoff climb from runway 06.  The 133-hour private pilot added that the engine began sputtering and running rough during the initial climb.  The pilot added that he tried to pull the choke and alter the throttle settings in an attempt to regain engine power, to no avail.  The pilot initiated a forced landing to a nearby clearing; however, the pilot did not have sufficient altitude and the airplane landed in trees.  The airplane came to rest suspended in trees in a near vertical nose low attitude.  The pilot was able to exit the airplane without injuries.  Post-accident inspection of the engine revealed that the carburetor rubber flange coupler had failed, which resulted in the reported loss of engine power.  The pilot added that the coupler (part number 267788) needs to have Kevlar material added in the injection mold process to prevent similar mishaps.  The airplane sustained structural damage to both wings.  The longeron and horizontal stabilizer were both bent.  The airplane and engine were reported to have accumulated a total of 275-hours since new.  The weather at the nearest weather reporting station located approximately 29 miles to the north north-east of the accident site reported calm winds, clear skies, and 20-statute mile visibility.

## Aircraft

- Registration: [N674F](https://openairdocs.org/aircraft/N674F), registered now, S/N 1674 (OpenAirDocs)
- Reported make and model: Flagg Kitfox IV
- Registry model: [Flagg Lyle R KITFOX IV](https://openairdocs.org/model/flagg-lyle-r-kitfox-iv) (registry code 0560392) (OpenAirDocs)
- Registry engine: [Bombardier ROTAX (ALL)](https://openairdocs.org/engine/bombardier-rotax-all) (registry code 09050, reciprocating) (OpenAirDocs)
- Category: Airplane, amateur-built
- Serial number: 1674
- Airframe hours: 275
- Engines: Rotax 912ul 80 horsepower reciprocating
- Damage: Substantial damage
- Flight: Personal, Part 91
- Registered owner: Marwynne Kuhn
- Airworthiness certificate: Special, Experimental (Special)
- Last inspection: Condition, July 1, 2006
- Departed: TE01, Centerville, TX
- Destination: 0TE4
- Airport: TE01, Dillard Ranch Airport, runway 06, 3,100 × 90 ft, grass/turf

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 59; injuries: none; private; airplane ratings: single-engine land; medical: class 3, with waivers/limitations; seat: left; flight hours: 133 total, 3 in this make and model, 106 as pilot in command, 7 in the last 90 days, 7 in the last 30 days, 0 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: calm
- Visibility: 20 statute miles
- Lowest ceiling: none
- Temperature: 61 °F
- Observed at: KPSN, 29 nm away

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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