20090128001369A

Accident · Destroyed

FAA accident report · Mrchti SF-260C · Santa Monica, CA · January 28, 2009

Date
January 28, 2009 · 17:06 local
Place
Santa Monica, CA
Airport
Santa Monica Municipal
Phase of flight
Takeoff
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N688C
NTSB investigation
NTSBWPR09FA102
Reported as
Mrchti SF260C
Reported engine
Lycoming IO540D4A5
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s flight hours
1,400 total20 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.

N688C, a sai marchetti 260-C certificated as an experimental exhibition aircraft operating under FAR part 91, crashed on departure from runway 21 at the Santa Monica Municipal Airport, (smo) after a complete loss of engine power. The power loss occurred at an altitude of approximately 300 ft. initial post accident, and a more detailed investigation of the fuel selector valve during the salvage operation, gives evidence that the pilot (may have) neglected to select either of the main fuel tanks which were reported as being full of fuel. The fuel tank selector valve appears to be selected for the right wing tip tank for a fuel supply which held a minimal quantity of fuel. Both main fuel tanks ruptured upon impact resulting in a severe post crash fire. The fire was extinguished by the airport fire department. Witnesses described the pilot as attempting to turn back to the runway following the loss of power. Witnesses state that the bank and initial dive angle of the aircraft approached 80 degrees before the pilot lost control of the aircraft. Plans are to being made to remove the valve in question for a thorough inspection to determine which fuel tank was feeding the engine. The investigation continues.

As the FAA filed it

N688C, A SAI MARCHETTI 260-C CERTIFICATED AS AN EXPERIMENTAL EXHIBITION AIRCRAFT OPERATING UNDER FAR PART 91, CRASHED ON DEPARTURE FROM RUNWAY 21 AT THE SANTA MONICA MUNICIPAL AIRPORT, (SMO) AFTER A COMPLETE LOSS OF ENGINE POWER. THE POWER LOSS OCCURRED AT AN ALTITUDE OF APPROXIMATELY 300 FT. INITIAL POST ACCIDENT, AND A MORE DETAILED INVESTIGATION OF THE FUEL SELECTOR VALVE DURING THE SALVAGE OPERATION, GIVES EVIDENCE THAT THE PILOT (MAY HAVE) NEGLECTED TO SELECT EITHER OF THE MAIN FUEL TANKS WHICH WERE REPORTED AS BEING FULL OF FUEL. THE FUEL TANK SELECTOR VALVE APPEARS TO BE SELECTED FOR THE RIGHT WING TIP TANK FOR A FUEL SUPPLY WHICH HELD A MINIMAL QUANTITY OF FUEL. BOTH MAIN FUEL TANKS RUPTURED UPON IMPACT RESULTING IN A SEVERE POST CRASH FIRE. THE FIRE WAS EXTINGUISHED BY THE AIRPORT FIRE DEPARTMENT. WITNESSES DESCRIBED THE PILOT AS ATTEMPTING TO TURN BACK TO THE RUNWAY FOLLOWING THE LOSS OF POWER. WITNESSES STATE THAT THE BANK AND INITIAL DIVE ANGLE OF THE AIRCRAFT APPROACHED 80 DEGREES BEFORE THE PILOT LOST CONTROL OF THE AIRCRAFT. PLANS ARE TO BEING MADE TO REMOVE THE VALVE IN QUESTION FOR A THOROUGH INSPECTION TO DETERMINE WHICH FUEL TANK WAS FEEDING THE ENGINE. THE INVESTIGATION CONTINUES.

NTSB investigation

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