20070903017849I

Incident · Minor damage

FAA incident report · Cessna 195 · Chatham, MA · September 3, 2007

Date: September 3, 2007 · 11:20 local
Place: Chatham, MA
Airport: Chatham Municipal
Phase of flight: Level Off Touchdown
Operating rules: General operating rules (Part 91)
Damage: Minor damage
Aircraft: N1083D
Reported as: Cessna 195
People aboard: 1
Fatal injuries: 0
Pilot’s flight hours: 371 total82 in this make and model19 in the last 90 days

N1083DRegistration cancelled Feb 23, 2026 · Cessna 195S/N 7695 · Built 1951 Airframe modelCessna 195 Engine modelJacobs R755A seriesReciprocating

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry 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.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) On September 3, 2007, at approximately 1120 eastern standard time (EST), a Cessna C195, N1083D being flown by the pilot privacy data omitted failed to control the aircraft during the landing phase. The aircraft sustained minor damage. The pilot of the aircraft stated in a written statement, during landing on runway 24 at Chatham, MA (cqx), the engine propellers contacted the runway bending the last three (3) to four (4) inches of each propeller blade.

As the FAA filed it

(-23) ON SEPTEMBER 3, 2007, AT APPROXIMATELY 1120 EASTERN STANDARD TIME (EST), A CESSNA C195, N1083D BEING FLOWN BY THE PILOT ^PRIVACY DATA OMITTED^ FAILED TO CONTROL THE AIRCRAFT DURING THE LANDING PHASE. THE AIRCRAFT SUSTAINED MINOR DAMAGE. THE PILOT OF THE AIRCRAFT STATED IN A WRITTEN STATEMENT, DURING LANDING ON RUNWAY 24 AT CHATHAM, MA (CQX), THE ENGINE PROPELLERS CONTACTED THE RUNWAY BENDING THE LAST THREE (3) TO FOUR (4) INCHES OF EACH PROPELLER BLADE.