19971209038149A

Accident · Substantial damage

FAA accident report · Cessna 150J · Silverdale, WA · December 9, 1997

Date
December 9, 1997 · 16:00 local
Place
Silverdale, WA
Airport
Apex Airpark Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N51369
NTSB investigation
NTSBSEA98LA022
Reported as
Cessna 150J
Reported engine
Continental O200A
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,664 total194 in this make and model72 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.

(.4)The flight instructor stated that as the student pilot was recovering from the third of a series of power-off stalls, the engine began to run rough. Power was applied smoothly and carburetor heat was turned off. The engine continued to run rough, and after approximately five seconds, the engine quit. The flight instructor took over the controls from the student and attempted to restart the engine. During the second restart attempt, the flight instructor pulled the starter handle, however, the handle separated from the panel. A forced landing was made to a soft field where a successful touchdown was accomplished, but during the landing roll, the nose wheel dug in and the airplane nosed over. During the postaccident inspection, the engine was run to 2500 RPM. The engine operated smoothly, with no discrepancies noted. Both magnetos were checked and found operational. The carburetor heat control was checked and found operational. The engine pull-to-start knob was inspected and it was found to have pulled off the metal shaft that runs through the panel, and the metal shaft had pulled away from the cable that runs to the starter lever. (-23)engine quit while recovering from practice stall. Attemp restart, handle seperated from panel. Nosed over landing.

As the FAA filed it

(.4)THE FLIGHT INSTRUCTOR STATED THAT AS THE STUDENT PILOT WAS RECOVERING FROM THE THIRD OF A SERIES OF POWER-OFF STALLS, THE ENGINE BEGAN TO RUN ROUGH. POWER WAS APPLIED SMOOTHLY AND CARBURETOR HEAT WAS TURNED OFF. THE ENGINE CONTINUED TO RUN ROUGH, AND AFTER APPROXIMATELY FIVE SECONDS, THE ENGINE QUIT. THE FLIGHT INSTRUCTOR TOOK OVER THE CONTROLS FROM THE STUDENT AND ATTEMPTED TO RESTART THE ENGINE. DURING THE SECOND RESTART ATTEMPT, THE FLIGHT INSTRUCTOR PULLED THE STARTER HANDLE, HOWEVER, THE HANDLE SEPARATED FROM THE PANEL. A FORCED LANDING WAS MADE TO A SOFT FIELD WHERE A SUCCESSFUL TOUCHDOWN WAS ACCOMPLISHED, BUT DURING THE LANDING ROLL, THE NOSE WHEEL DUG IN AND THE AIRPLANE NOSED OVER. DURING THE POSTACCIDENT INSPECTION, THE ENGINE WAS RUN TO 2500 RPM. THE ENGINE OPERATED SMOOTHLY, WITH NO DISCREPANCIES NOTED. BOTH MAGNETOS WERE CHECKED AND FOUND OPERATIONAL. THE CARBURETOR HEAT CONTROL WAS CHECKED AND FOUND OPERATIONAL. THE ENGINE PULL-TO-START KNOB WAS INSPECTED AND IT WAS FOUND TO HAVE PULLED OFF THE METAL SHAFT THAT RUNS THROUGH THE PANEL, AND THE METAL SHAFT HAD PULLED AWAY FROM THE CABLE THAT RUNS TO THE STARTER LEVER. (-23)ENGINE QUIT WHILE RECOVERING FROM PRACTICE STALL. ATTEMP RESTART, HANDLE SEPERATED FROM PANEL. NOSED OVER LANDING.

NTSB investigation

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