20050514010249A

Accident · Substantial damage

FAA accident report · Stolam RC-3 · Santa Rosa, CA · May 14, 2005

Date
May 14, 2005 · 15:10 local
Place
Santa Rosa, CA
Airport
Sonoma County
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N6292K
NTSB investigation
NTSBLAX05LA172
Reported as
Stolam RC3
Reported engine
Franklin 6A8215B8F
People aboard
2
Fatal injuries
0
Pilot’s flight hours
10,000 total29 in this make and model20 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 take off from sts, pilot noticed the engine oil temperature had risen from 180 to 190 degrees f. the pilot also noticed that they were not gaining altitude and, because of the mountain ridge between sts and their location, made a decision to go to healdsburg (O31) airport. However the oil temperature kept rising and was now at 200 degrees f and climbing as the oil pressure was dropping and the pilot could not hold altitude. However the oil temperature kept rising and was not at 200 degrees f and climbing as the oil pressure was dropping and the pilot could not hold altitude. A couple of minutes later, the pilot heard a loud noise from the engine compartment accompanied by a complete loss of power. Attempting an off field landing, with gear (recommended with this amphibious aircraft in emergency procedures) and flaps down, the pilot belly landed in a soft ground vineyard, nose dug in, and the aircraft came to rest inverted. Limited subsequent investigation, witnessed by NTSB, aviation safety inspector, privacy data omitted revealed an uncontained failure of the number 1 cylinder piston main connecting rod at the crankshaft journal.

As the FAA filed it

(-23) SHORTLY AFTER TAKE OFF FROM STS, PILOT NOTICED THE ENGINE OIL TEMPERATURE HAD RISEN FROM 180 TO 190 DEGREES F. THE PILOT ALSO NOTICED THAT THEY WERE NOT GAINING ALTITUDE AND, BECAUSE OF THE MOUNTAIN RIDGE BETWEEN STS AND THEIR LOCATION, MADE A DECISION TO GO TO HEALDSBURG (O31) AIRPORT. HOWEVER THE OIL TEMPERATURE KEPT RISING AND WAS NOW AT 200 DEGREES F AND CLIMBING AS THE OIL PRESSURE WAS DROPPING AND THE PILOT COULD NOT HOLD ALTITUDE. HOWEVER THE OIL TEMPERATURE KEPT RISING AND WAS NOT AT 200 DEGREES F AND CLIMBING AS THE OIL PRESSURE WAS DROPPING AND THE PILOT COULD NOT HOLD ALTITUDE. A COUPLE OF MINUTES LATER, THE PILOT HEARD A LOUD NOISE FROM THE ENGINE COMPARTMENT ACCOMPANIED BY A COMPLETE LOSS OF POWER. ATTEMPTING AN OFF FIELD LANDING, WITH GEAR (RECOMMENDED WITH THIS AMPHIBIOUS AIRCRAFT IN EMERGENCY PROCEDURES) AND FLAPS DOWN, THE PILOT BELLY LANDED IN A SOFT GROUND VINEYARD, NOSE DUG IN, AND THE AIRCRAFT CAME TO REST INVERTED. LIMITED SUBSEQUENT INVESTIGATION, WITNESSED BY NTSB, AVIATION SAFETY INSPECTOR, ^PRIVACY DATA OMITTED REVEALED AN UNCONTAINED FAILURE OF THE NUMBER 1 CYLINDER PISTON MAIN CONNECTING ROD AT THE CRANKSHAFT JOURNAL.

NTSB investigation

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