19970822023399A

Accident · Destroyed

FAA accident report · Cessna 210E · Oxnard, CA · August 22, 1997

Date
August 22, 1997 · 14:30 local
Place
Oxnard, CA
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N1808F
NTSB investigation
NTSBLAX97LA299
Reported as
Cessna 210E
Reported engine
Continental IO520A
Fatal injuries
0
Pilot’s flight hours
3,120 total15 in this make and model128 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.

Aircraft engine failed, attempted to land at Oxnard, hit a build, then a light standard, crashed and burned. (.4) during departure climbout, after reaching 1,500 to 2,000 feet AGL, the pilot/flight instructor noted that the student pilot had not properly set the throttle friction lock and the throttle had retarded to about 15 inches of manifold pressure. The pilot instructed his student to advance the throttle, however, when the student did so the manifold pressure rose momentarily and then the engine abruptly stopped delivering power. The pilot took control of the aircraft from his student, performed the engine failure checklist, declared an emergency, and established a glide toward a nearby airport. When it became apparent that the aircraft could not glide to the airport, he turned toward an open agricultureal field. The aircraft impacted the roof of a house and a light pole across the street from the field boundary and came to rest at the edge of the field. Postaccident examination revealed that a fuel supply hose had come unscrewed off the inlet nipple of the fuel supply control unit. An 100-hour inspection was completed the prior day and this was the first flight following theinspection.

As the FAA filed it

AIRCRAFT ENGINE FAILED, ATTEMPTED TO LAND AT OXNARD, HIT A BUILD, THEN A LIGHT STANDARD, CRASHED AND BURNED. (.4) DURING DEPARTURE CLIMBOUT, AFTER REACHING 1,500 TO 2,000 FEET AGL, THE PILOT/FLIGHT INSTRUCTOR NOTED THAT THE STUDENT PILOT HAD NOT PROPERLY SET THE THROTTLE FRICTION LOCK AND THE THROTTLE HAD RETARDED TO ABOUT 15 INCHES OF MANIFOLD PRESSURE. THE PILOT INSTRUCTED HIS STUDENT TO ADVANCE THE THROTTLE, HOWEVER, WHEN THE STUDENT DID SO THE MANIFOLD PRESSURE ROSE MOMENTARILY AND THEN THE ENGINE ABRUPTLY STOPPED DELIVERING POWER. THE PILOT TOOK CONTROL OF THE AIRCRAFT FROM HIS STUDENT, PERFORMED THE ENGINE FAILURE CHECKLIST, DECLARED AN EMERGENCY, AND ESTABLISHED A GLIDE TOWARD A NEARBY AIRPORT. WHEN IT BECAME APPARENT THAT THE AIRCRAFT COULD NOT GLIDE TO THE AIRPORT, HE TURNED TOWARD AN OPEN AGRICULTUREAL FIELD. THE AIRCRAFT IMPACTED THE ROOF OF A HOUSE AND A LIGHT POLE ACROSS THE STREET FROM THE FIELD BOUNDARY AND CAME TO REST AT THE EDGE OF THE FIELD. POSTACCIDENT EXAMINATION REVEALED THAT A FUEL SUPPLY HOSE HAD COME UNSCREWED OFF THE INLET NIPPLE OF THE FUEL SUPPLY CONTROL UNIT. AN 100-HOUR INSPECTION WAS COMPLETED THE PRIOR DAY AND THIS WAS THE FIRST FLIGHT FOLLOWING THEINSPECTION.

NTSB investigation

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