# Incident 20210704011169I: Conwell Leslie C GP-4, Fort Worth, TX, July 4, 2021

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: July 4, 2021, 10:10 local time
- Place: Fort Worth, TX
- Airport: Fort Worth Alliance
- Damage: Minor damage
- Phase of flight: Landing: Rollout
- Operating rules: General operating rules (Part 91)
- Location: 32.7254° N, 97.3208° W: Placed by OpenAirDocs: center of Fort Worth, TX, within about 11 miles (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=32.7254&lon=-97.3208&mi=10
- Aircraft: N814LM, a cancelled registration (https://openairdocs.org/deregistered/N814LM-2024-04-16) (OpenAirDocs)
- Registry model: Conwell Leslie C GP-4 (registry code 056273T, https://openairdocs.org/model/conwell-leslie-c-gp-4) (OpenAirDocs)
- Registry engine: Lycoming IO-360-A1A (registry code 41818, https://openairdocs.org/engine/lycoming-io-360-a1a) (OpenAirDocs)
- Reported make and model: CONWELL LESLIE C GP-4
- Reported engine: LYCOMING IO-360-A1A
- People aboard: 2
- Fatal injuries: 0
- Other injuries: 0
- Pilot certificates: Commercial pilot
- Pilot flight hours: 852 total
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20210704011169I

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

UPON LANDING, THE NOSE GEAR COLLAPSED AND THE NOSE OF THE AIRCRAFT CAME DOWN ON THE RUNWAY.

AIRCRAFT CAME TO A STOP UPRIGHT ON THE RUNWAY.

PROPELLER IMPACTED THE RUNWAY.

DAMAGE TO THE SPINNER, AND BOTH PROPELLER BLADES.

DAMAGE TO THE LOWER ENGINE COWL.

DAMAGE TO LANDING GEAR PANELS ON LEFT AND RIGHT MAIN LANDING GEAR. DAMAGE TO THE NOSE LANDING GEAR DOOR.

THERE WERE CRACKS IN THE ROOT FAIRINGS OF BOTH WINGS.

DURING INSPECTION OF AIRCRAFT, DISCOVERED THERE WAS A CLEVIS PIN MISSING FROM THE RIGHT RUDDER PUSH ROD. CLEVIS PIN WAS FOUND IN THE RIGHT FLOOR BOARD.

FURTHER INSPECTION OF AIRCRAFT SHOWED NO VISUAL DAMAGE TO THE ENGINE MOUNT, FIRE WALL, OR WING SPAR. IT WAS ALSO DISCOVERED THAT THE JAM NUT ON THE HOUSING FOR THE ?NOSE GEAR UP LOCK RELEASE CABLE, WAS LOOSE AT THE BULKHEAD.

THERE WAS AN ENTRY IN THE AIRFRAME LOG SHOWING THAT THE OWNER CHANGED THE CLEVIS PIN AFTER THE CONDITIONAL INSPECTION.

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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