20050103000699A

Accident · Substantial damage

FAA accident report · Cessna 310J · Davenport, WA · January 3, 2005

Date
January 3, 2005 · 12:45 local
Place
Davenport, WA
Airport
Davenport Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N310RA
NTSB investigation
NTSBSEA05CA035
Reported as
Cessna 310J
Reported engine
Continental IO470*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,830 total471 in this make and model28 in the last 90 days

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 January 3, 2005 the pilot privacy data omitted a private pilot, was acting as pilot in command of N310RA, a 1965 Cessna 310-J aircraft. One passenger accompanied the pilot privacy data omitted on this flight from auburn, Washington to Davenport, Washington. This particular flight was conducted under an instrument flight plan. According to the pilot's statement, he obtained a VFR on top clearance until he had to obtain an IFR clearance to descend below 7,500 MSL into IMC conditions. He then stated he was then cleared direct to the geg VOR and expect the ILS rwy 3 approach into spokane international airport. During his descent the aircraft experienced "light mixed icing" until the aircraft reached 4,000 feet MSL. In addition, the pilot privacy data omitted stated the aircraft's deicing systems were operational (boot, props, & hot windshield). After descending to VMC conditions he cancelled his IFR clearance and proceeded to the Davenport, WA airport (S68) VFR. The pilot privacy data omitted also noted that he activated the deice systems on the downwind leg of the Davenport Airport's traffic patter. The Cessna 310 aircraft stalled upon landing resulting in substantial damage to the ai rcraft. The aircraft received substantial damage to include two bent props, and a bent left wing inboard of the engine nacelle. The pilot and passenger reported no injuries. Nothing follows.

As the FAA filed it

(-23) ON JANUARY 3, 2005 THE PILOT ^PRIVACY DATA OMITTED^ A PRIVATE PILOT, WAS ACTING AS PILOT IN COMMAND OF N310RA, A 1965 CESSNA 310-J AIRCRAFT. ONE PASSENGER ACCOMPANIED THE PILOT ^PRIVACY DATA ^ ON THIS FLIGHT FROM AUBURN, WASHINGTON TO DAVENPORT, WASHINGTON. THIS PARTICULAR FLIGHT WAS CONDUCTED UNDER AN INSTRUMENT FLIGHT PLAN. ACCORDING TO THE PILOT'S STATEMENT, HE OBTAINED A VFR ON TOP CLEARANCE UNTIL HE HAD TO OBTAIN AN IFR CLEARANCE TO DESCEND BELOW 7,500 MSL INTO IMC CONDITIONS. HE THEN STATED HE WAS THEN CLEARED DIRECT TO THE GEG VOR AND EXPECT THE ILS RWY 3 APPROACH INTO SPOKANE INTERNATIONAL AIRPORT. DURING HIS DESCENT THE AIRCRAFT EXPERIENCED "LIGHT MIXED ICING" UNTIL THE AIRCRAFT REACHED 4,000 FEET MSL. IN ADDITION, THE PILOT ^PRIVACY DATA ^ STATED THE AIRCRAFT'S DEICING SYSTEMS WERE OPERATIONAL (BOOT, PROPS, & HOT WINDSHIELD). AFTER DESCENDING TO VMC CONDITIONS HE CANCELLED HIS IFR CLEARANCE AND PROCEEDED TO THE DAVENPORT, WA AIRPORT (S68) VFR. THE PILOT ^PRIVACY DATA ^ ALSO NOTED THAT HE ACTIVATED THE DEICE SYSTEMS ON THE DOWNWIND LEG OF THE DAVENPORT AIRPORT'S TRAFFIC PATTER. THE CESSNA 310 AIRCRAFT STALLED UPON LANDING RESULTING IN SUBSTANTIAL DAMAGE TO THE AI RCRAFT. THE AIRCRAFT RECEIVED SUBSTANTIAL DAMAGE TO INCLUDE TWO BENT PROPS, AND A BENT LEFT WING INBOARD OF THE ENGINE NACELLE. THE PILOT AND PASSENGER REPORTED NO INJURIES. NOTHING FOLLOWS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.