20070721014189A

Accident · Substantial damage

FAA accident report · Swftms GC-1B · Cottage Grove, OR · July 21, 2007

Date
July 21, 2007 · 14:18 local
Place
Cottage Grove, OR
Airport
Cottage Grove State
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3867K
NTSB investigation
NTSBSEA07FA208
Reported as
Swftms GC1B
Reported engine
Continental C1252
People aboard
2
Fatal injuries
2
Pilot’s flight hours
2,297 total0 in this make and model0 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) Aircraft departed Cottage Grove airport to the south. Aircraft lost control approximately 1/4 of a mile off end of runway and crashed into an old mining pond and landed upside down in the water. The pilot privacy data omitted was found in the left seat at the accident site (2 fatals). Witnesses stated that the weather was high humidity and approximately 83-86 degrees creating a high density altitude. One witness stated that he heard the engine cut-out twice and then tried to regain power. Possible carburetor ice. Aircraft had a full load of automotive gas that contained alcohol that is contrary to the peterson autogas STC SE2032CE & SA2137CE that was installed on this aircraft and documented on a FAA form 337, dated 10/27/2006, by the pilot privacy data omitted. Pilot weight per airman information records was 275 lbs. Passenger/second pilot weight per airman information records was 192 lbs. A review of the original aircraft weight and balance records shows maximum useful load of 523 lbs. Aircraft gross weight is 1710 lbs. Calculations from weight and balance reflects approximately 130 lbs. Over gross at takeoff. Cottage Grove police department provided a complete report to FAA and NTSB.

As the FAA filed it

(-23) AIRCRAFT DEPARTED COTTAGE GROVE AIRPORT TO THE SOUTH. AIRCRAFT LOST CONTROL APPROXIMATELY 1/4 OF A MILE OFF END OF RUNWAY AND CRASHED INTO AN OLD MINING POND AND LANDED UPSIDE DOWN IN THE WATER. THE PILOT ^PRIVACY DATA OMITTED^ WAS FOUND IN THE LEFT SEAT AT THE ACCIDENT SITE (2 FATALS). WITNESSES STATED THAT THE WEATHER WAS HIGH HUMIDITY AND APPROXIMATELY 83-86 DEGREES CREATING A HIGH DENSITY ALTITUDE. ONE WITNESS STATED THAT HE HEARD THE ENGINE CUT-OUT TWICE AND THEN TRIED TO REGAIN POWER. POSSIBLE CARBURETOR ICE. AIRCRAFT HAD A FULL LOAD OF AUTOMOTIVE GAS THAT CONTAINED ALCOHOL THAT IS CONTRARY TO THE PETERSON AUTOGAS STC SE2032CE & SA2137CE THAT WAS INSTALLED ON THIS AIRCRAFT AND DOCUMENTED ON A FAA FORM 337, DATED 10/27/2006, BY THE PILOT ^PRIVACY DATA OMITTED^. PILOT WEIGHT PER AIRMAN INFORMATION RECORDS WAS 275 LBS. PASSENGER/SECOND PILOT WEIGHT PER AIRMAN INFORMATION RECORDS WAS 192 LBS. A REVIEW OF THE ORIGINAL AIRCRAFT WEIGHT AND BALANCE RECORDS SHOWS MAXIMUM USEFUL LOAD OF 523 LBS. AIRCRAFT GROSS WEIGHT IS 1710 LBS. CALCULATIONS FROM WEIGHT AND BALANCE REFLECTS APPROXIMATELY 130 LBS. OVER GROSS AT TAKEOFF. COTTAGE GROVE POLICE DEPARTMENT PROVIDED A COMPLETE REPORT TO FAA AND NTSB.

NTSB investigation

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