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Aviation safety reports, made easier to study

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April 17, 1982 · Cessna 210D · N3972Y

N. South Lake T, CA

Overview

Report Status
Preliminary report
Event Type
Accident
Date
April 17, 1982
Injury Outcomes
No injuries (2 uninjured)
Location
N. South Lake T, CA
Aircraft
Cessna 210D
Tail Number
N3972Y
Operator
Mickele a Foley
Injuries
None
Aircraft Damage
Destroyed
NTSB Number
LAX82DA139

After takeoff, the pilot made a normal climb to about 8,500 ft. He then noticed indications of higher than normal EGT and fuel pressure and a lower than normal fuel flow. The pilot reported that he had leveled off and throttled back when the engine began to sputter. He noticed a slight RPM loss with the same fuel pressure and flow readings. He elected to return to the South Lake Tahoe Airport. While returning, there was an additional loss of power and the aircraft was subsequently ditched in Lake Tahoe. The pilot and passenger egressed through a side window and swam to shore. The aircraft was retrieved from the lake. The engine was inspected, and after minor repairs, it operated normally using the aircraft's fuel system. The fuel boost pump could not be tested due to impact damage. The magnetos tested satisfactorily. The spark plugs were too rusty to check; therefore, other plugs were used for the engine run.

Full Narrative

AFTER TAKEOFF, THE PILOT MADE A NORMAL CLIMB TO ABOUT 8500 FT. HE THEN NOTICED INDICATIONS OF HIGHER THAN NORMAL EGT AND FUEL PRESSURE AND A LOWER THAN NORMAL FUEL FLOW. THE PILOT REPORTED THAT HE HAD LEVELED OFF AND THROTTLED BACK WHEN THE ENGINE BEGAN TO SPUTTER. HE NOTICED A SLIGHT RPM LOSS WITH THE SAME FUEL PRESSURE AND FLOW READINGS. HE ELECTED TO RETURN TO THE SOUTH LAKE TAHOE AIRPORT. WHILE RETURNING, THERE WAS AN ADDITIONAL LOSS OF POWER AND THE AIRCRAFT WAS SUBSEQUENTLY DITCHED IN LAKE TAHOE. THE PILOT AND PASSENGER EGRESSED THROUGH A SIDE WINDOW AND SWAM TO SHORE. THE AIRCRAFT WAS RETRIEVED FROM THE LAKE. THE ENGINE WAS INSPECTED, AND AFTER MINOR REPAIRS, IT OPERATED NORMALLY USING THE AIRCRAFT'S FUEL SYSTEM. THE FUEL BOOST PUMP COULD NOT BE TESTED DUE TO IMPACT DAMAGE. THE MAGNETOS TESTED SATISFACTORILY. THE SPARK PLUGS WERE TOO RUSTY TO CHECK; THEREFORE, OTHER PLUGS WERE USED FOR THE ENGINE RUN.

Flight

Event TypeAccident
Event Time14:00 PST
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 210D
Tail NumberN3972Y
Aircraft CategoryAir
DamageDestroyed
OperatorMickele a Foley
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-520-A · Reciprocating · 285
Seats6

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 35 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind190° @ 8 kt
Visibility30 sm
CeilingNone
Temperature / Dew Point14 C / 0 C
Altimeter30.00 inHg

Appendix: Source Data