# Accident 20050101000289A: Beech G35, Falmouth, MA, January 1, 2005

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: January 1, 2005, 11:15 local time
- Place: Falmouth, MA
- Airport: Falmouth Airpart Airport
- Damage: Substantial damage
- Phase of flight: Ground Taxi, Other Airplane
- Operating rules: General operating rules (Part 91)
- Location: 41.5856° N, 70.5403° W: From the FAA
- Nearby events: https://openairdocs.org/map.md?lat=41.5856&lon=-70.5403&mi=10
- Aircraft: N333EG, a cancelled registration (https://openairdocs.org/deregistered/N333EG-2017-07-20) (OpenAirDocs)
- Registry model: Beech G35 (registry code 1151516, https://openairdocs.org/model/beech-g35) (OpenAirDocs)
- Registry engine: Continental E225 series (registry code 17015, https://openairdocs.org/engine/continental-e225-series) (OpenAirDocs)
- Reported make and model: BEECH G35
- Reported engine: CONT E2258
- People aboard: 2
- Fatal injuries: 0
- Pilot flight hours: 790 total, 64 in this make and model, 30 in the last 90 days
- NTSB investigation: [NTSB IAD05LA030](https://openairdocs.org/ntsb/IAD05LA030) (OpenAirDocs)
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20050101000289A

## Narrative

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

(-23) DURING TAXI, AT 1400L HRS, FROM PERSONAL RESIDENCE, PILOT INCREASED ENGINE POWER TO TAXI AIRCRAFT THROUGH APPROXIMATELY 2 INCHES OF SNOW. WHEN AIRCRAFT ACCELERATED THE PILOT RETARDED THE THROTTLES, BUT THE AIRCRAFT ENGINE DID NOT REDUCE POWER AND THE AIRCRAFT CONTINUED TO ACCELERATE. THE PILOT STATED THAT HE PULLED THE THROTTLE TWO TIMES TRYING TO REDUCE THE ENGINE RPM, BUT HAD NO EFFECT. THE AIRCRAFT CONTINUED TO TAXI APPROXIMATELY 56 FEET UNTIL STOPPED HITTING TREES ACROSS THE TAXIWAY OPPOSITE THE PILOT'S RESIDENCE. SUBSTANTIAL DAMAGE WAS SUSTAINED TO THE FOLLOWING: LEFT WING TIP; RIGHT WING LEADING EDGE APPROXIMATELY 12 INCHES INTO THE WING STOPPING AT AND DAMAGING THE FORWARD WING SPAR; RIGHT WING AFT SPAR UPPER CAP IS BUCKLED AT THE CENTER SECTION RIGHT WING LOWER SIDE AT THE FORWARD WING TO FUSELAGE AREA BUCKLED; THE RIGHT SIDE AND BOTTOM OF THE FUSELAGE IS BUCKLED AND THE LONGERONS ARE DAMAGED; ENGINE FIREWALL BUCKLED. NO INJURIES TO THE PILOT OR PASSENGER SUSTAINED.

## The NTSB's investigation of this event (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 IAD05LA030](https://openairdocs.org/ntsb/IAD05LA030), Jan 1, 2005: Beech G35 (N333EG), Falmouth, MA, substantial damage. Probable cause: The pilot's failure to maintain control of the airplane during taxi. A factor was the snow-covered taxiway.

## Other reports on N333EG (1)

Matched to the same aircraft by N-number and date.

- [Incident 19800106011059I](https://openairdocs.org/incident/19800106011059I), Jan 6, 1980: Beech 35BEECH (N333EG), Brookville, OH, Minor damage. Aircraft touched down on partial extended main gear and propeller. Minor damage gear doors and propeller.

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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