20000702034949I

Incident

FAA incident report · Dhav DHC2MK1 · Ketchikan, AK · July 2, 2000

Date
July 2, 2000 · 19:00 local
Place
Ketchikan, AK
Phase of flight
Climb
Operating rules
Air taxi and commuter (Part 135)
Operator
W0PC
Aircraft
N95DG
Reported as
Dhav DHC2MK1
People aboard
1
Fatal injuries
0
Pilot’s flight hours
17,000 total10,000 in this make and model

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) The pilot departed hollis empty in a DHC-2 on floats. Upon climbing through 200 ft. AGL, and in a 20 degree banked turn, the control yoke handles broke away from the rest of the yoke assembly, leaving the pilot without aileron control. The pilot was able to regain roll control using rudder, and pitch control was still possible using the remaining control yoke. The pilot flew to Ketchikan where he landed uneventfully, in the presence of emergency equipment. It was determined that a large area washer on the control yoke assembly had failed. This large washer ensures the castle nut and cotter pin holding the handles do not slide through the center of the splines that holds the handles to the control yoke. The washer was missing and could not be found.

As the FAA filed it

(-23) THE PILOT DEPARTED HOLLIS EMPTY IN A DHC-2 ON FLOATS. UPON CLIMBING THROUGH 200 FT. AGL, AND IN A 20 DEGREE BANKED TURN, THE CONTROL YOKE HANDLES BROKE AWAY FROM THE REST OF THE YOKE ASSEMBLY, LEAVING THE PILOT WITHOUT AILERON CONTROL. THE PILOT WAS ABLE TO REGAIN ROLL CONTROL USING RUDDER, AND PITCH CONTROL WAS STILL POSSIBLE USING THE REMAINING CONTROL YOKE. THE PILOT FLEW TO KETCHIKAN WHERE HE LANDED UNEVENTFULLY, IN THE PRESENCE OF EMERGENCY EQUIPMENT. IT WAS DETERMINED THAT A LARGE AREA WASHER ON THE CONTROL YOKE ASSEMBLY HAD FAILED. THIS LARGE WASHER ENSURES THE CASTLE NUT AND COTTER PIN HOLDING THE HANDLES DO NOT SLIDE THROUGH THE CENTER OF THE SPLINES THAT HOLDS THE HANDLES TO THE CONTROL YOKE. THE WASHER WAS MISSING AND COULD NOT BE FOUND.