# Incident 20091229053129I: Beech 35, Lebanon, TN, December 29, 2009

- Type: FAA incident report (Accident/Incident Data System), as reported
- Date: December 29, 2009, 17:30 local time
- Place: Lebanon, TN
- Airport: Lebanon Municipal
- Damage: Substantial damage
- Phase of flight: Landing: Touchdown
- Operating rules: General operating rules (Part 91)
- Location: 36.1904° N, 86.3157° W: Placed by OpenAirDocs at LEBANON MUNI (M54), within about a mile (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=36.1904&lon=-86.3157&mi=10
- Aircraft: N10GG, registered now (https://openairdocs.org/aircraft/N10GG) (OpenAirDocs)
- Registry model: Beech 35 (registry code 1151502, https://openairdocs.org/model/beech-35) (OpenAirDocs)
- Registry engine: Continental E185 series (registry code 17014, https://openairdocs.org/engine/continental-e185-series) (OpenAirDocs)
- Reported make and model: BEECH 35
- Reported engine: CONT MOTOR E185 SERIES
- People aboard: 1
- Fatal injuries: 0
- Other injuries: 0
- Pilot certificates: Private pilot
- Pilot flight hours: 518 total, 409 in this make and model, 10 in the last 90 days
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20091229053129I

## Narrative

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

OFFICE INCIDENT NUMBER IS: CE19100003.  AIRCRAFT WAS LANDED WITH THE GEAR UP DURING THE DAY IN VMC.  LANDING GEAR WAS TESTED AFTER AIRCRAFT RECOVERY.  THE GEAR AND GEAR INDICATORS FUNCTIONED CORRECTLY SEVERAL TIMES.  PILOT THOUGHT HE COMPLETED THE BEFORE LANDING CHECKLIST.  PILOT FAILED TO NOTE THE GEAR WAS UP UNTIL HE HEARD SCRAPING SOUNDS FROM WHAT HE BELIEVED TO BE THE WING FLAPS IN CONTACT WITH THE RUNWAY.  AIRCRAFT DID NOT DEPART THE RUNWAY DURING THE LANDING PHASE.  DAMAGE TO THE AIRCRAFT INCLUDED THE FOLLOWING:1.WING FLAPS; TRAILING EDGES HAVE SIGNIFICANT DAMAGE DUE TO CONTACT WITH THE RUNWAY.2.PROPELLER; DESTROYED DUE TO CONTACT WITH THE RUNWAY.3.ENGINE EXHAUST STACKS; SIGNIFICANT DAMAGE DUE TO CONTACT WITH THE RUNWAY.4.NOSE WHEEL GEAR DOORS; SIGNIFICANT DAMAGE DUE TO CONTACT WITH THE RUNWAY.5.ENGINE; SIGNIFICANT DAMAGE ASSUMED DUE TO PROPELLER STRIKE.6.SHEET METAL DAMAGE; NOTED IN AND AROUND ALL GEAR DOORS.  CRACKS NOTED AROUND ENGINE MOUNTING BRACKETS.

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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