19990318002429A

Accident · Destroyed

FAA accident report · Gulstm 500B · Shelter Cove, CA · March 18, 1999

Date
March 18, 1999 · 18:35 local
Place
Shelter Cove, CA
Airport
Shelter Cove Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
CFBCR
Reported as
Gulstm 500B
Reported engine
Lycoming IO540B1C5
Fatal injuries
0
Pilot’s flight hours
5,400 total32 in this make and model32 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) Shortly after southbound take-off from Shelter Cove Airport (0Q5), CA, the aircraft lost power, as reported by the pilot and passenger. Both engines quit, and the pilot performed a gear-up surf landing. (.4) prior to departure the pilot believed that his airplane contained between 30 and 40 gallons of fuel, adequate for a 15-minute-long flight to another airport where he could purchase additional fuel. The pilot reported the fuel gauge registered 40 gallons, so he departed. During initial climb upon reaching an altitude of about 400 feet above the ocean, both engines simultaneously lost power. The pilot rocked the airplane's wings and experienced a 'short surge of power.' However, it lasted only a brief moment and all engine power was again totally lost. The pilot turned toward the shoreline, reduced airspeed, and ditched about 0.25 miles off shore. The overnight tide/wave action subsequently beached most of the airplane. In the pilot's report, he did not indicate having experienced any mechanical malfunctions. The federal aviation administration (FAA) coordinator examined recovered portions of the airframe and engines. In pertinent part, the FAA reported finding no physical evidence of any mechanical malfunction with the examined components. However, because of the airframe damage sustained during immersion in the salt water and the subsequent destruction to components, the safety board was unable to document the integrity of the fuel quantity indicator system.

As the FAA filed it

(-23) SHORTLY AFTER SOUTHBOUND TAKE-OFF FROM SHELTER COVE AIRPORT (0Q5), CA, THE AIRCRAFT LOST POWER, AS REPORTED BY THE PILOT AND PASSENGER. BOTH ENGINES QUIT, AND THE PILOT PERFORMED A GEAR-UP SURF LANDING. (.4) PRIOR TO DEPARTURE THE PILOT BELIEVED THAT HIS AIRPLANE CONTAINED BETWEEN 30 AND 40 GALLONS OF FUEL, ADEQUATE FOR A 15-MINUTE-LONG FLIGHT TO ANOTHER AIRPORT WHERE HE COULD PURCHASE ADDITIONAL FUEL. THE PILOT REPORTED THE FUEL GAUGE REGISTERED 40 GALLONS, SO HE DEPARTED. DURING INITIAL CLIMB UPON REACHING AN ALTITUDE OF ABOUT 400 FEET ABOVE THE OCEAN, BOTH ENGINES SIMULTANEOUSLY LOST POWER. THE PILOT ROCKED THE AIRPLANE'S WINGS AND EXPERIENCED A 'SHORT SURGE OF POWER.' HOWEVER, IT LASTED ONLY A BRIEF MOMENT AND ALL ENGINE POWER WAS AGAIN TOTALLY LOST. THE PILOT TURNED TOWARD THE SHORELINE, REDUCED AIRSPEED, AND DITCHED ABOUT 0.25 MILES OFF SHORE. THE OVERNIGHT TIDE/WAVE ACTION SUBSEQUENTLY BEACHED MOST OF THE AIRPLANE. IN THE PILOT'S REPORT, HE DID NOT INDICATE HAVING EXPERIENCED ANY MECHANICAL MALFUNCTIONS. THE FEDERAL AVIATION ADMINISTRATION (FAA) COORDINATOR EXAMINED RECOVERED PORTIONS OF THE AIRFRAME AND ENGINES. IN PERTINENT PART, THE FAA REPORTED FINDING NO PHYSICAL EVIDENCE OF ANY MECHANICAL MALFUNCTION WITH THE EXAMINED COMPONENTS. HOWEVER, BECAUSE OF THE AIRFRAME DAMAGE SUSTAINED DURING IMMERSION IN THE SALT WATER AND THE SUBSEQUENT DESTRUCTION TO COMPONENTS, THE SAFETY BOARD WAS UNABLE TO DOCUMENT THE INTEGRITY OF THE FUEL QUANTITY INDICATOR SYSTEM.