20000318018669I

Incident

FAA incident report · Bell 212 · Cabine, AO · March 18, 2000

Date
March 18, 2000 · 08:12 local
Place
Cabine, AO
Phase of flight
To Vertical (Helicopter Only)
Operating rules
Air taxi and commuter (Part 135)
Operator
HEEA
Aircraft
N5736J
Reported as
Bell 212
Reported engine
Pratt & Whitney PT6T3B
People aboard
1
Fatal injuries
0

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)During takeoff, pilot attempted to move the collective up but it would not move. A second try was made, but the collective would not move. Mechanics fund the lower rod end of the collective servo screwed out. The threaded end of the rod end contains a grove that the locing washer tang fits into and mates up against the servo lower piston and secured with the jam nut and locking wire. It was found that the locking washer tang had been sheared off allowing the rod end to became unscrewed from the lower piston as it rotated inside of the servo housing. The piston then extended amd lodged itself against the threaded end of the free rod end freezing the servo. Block 32, "other", will be addressed with a safety recommendation.

As the FAA filed it

(-23)DURING TAKEOFF, PILOT ATTEMPTED TO MOVE THE COLLECTIVE UP BUT IT WOULD NOT MOVE. A SECOND TRY WAS MADE, BUT THE COLLECTIVE WOULD NOT MOVE. MECHANICS FUND THE LOWER ROD END OF THE COLLECTIVE SERVO SCREWED OUT. THE THREADED END OF THE ROD END CONTAINS A GROVE THAT THE LOCING WASHER TANG FITS INTO AND MATES UP AGAINST THE SERVO LOWER PISTON AND SECURED WITH THE JAM NUT AND LOCKING WIRE. IT WAS FOUND THAT THE LOCKING WASHER TANG HAD BEEN SHEARED OFF ALLOWING THE ROD END TO BECAME UNSCREWED FROM THE LOWER PISTON AS IT ROTATED INSIDE OF THE SERVO HOUSING. THE PISTON THEN EXTENDED AMD LODGED ITSELF AGAINST THE THREADED END OF THE FREE ROD END FREEZING THE SERVO. BLOCK 32, "OTHER", WILL BE ADDRESSED WITH A SAFETY RECOMMENDATION.

Other reports on N5736J · 2

Matched to the same aircraft by N-number and date.