SDR 98ZZZX4430

Service difficulty report · Spider · Snias AS350BA

Difficulty date
October 7, 1998
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N821SP
Make and model
Snias AS350BA
Aircraft serial
2106
Part
Spider
Part number
350A33200405
Condition
Stiff
Location
Tail Rotor
Part time
4,804 hours
Stage of operation
NR
Nature of condition
O
Precautionary procedure
O

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

THE TAIL ROTOR SPIDER BECAME STIFF AFTER BEING INSTALLED AT OVERHAUL. THIS WAS 19 HOURS AFTER OVERHAUL, OVER 80 POUNDS IN FORCE WERE REQUIRED TO SLIDE SPIDER MAXIMUM OF 30 PER MM. THE SPIDER WAS REPLACED WITH ANOTHER OVERHAULED SPIDER. IT IS NOW STIFF AND REQUIRES 95 POUNDS OF FORCE. EUROCOPTER STATES OVERHAUL PROCEDURE CHANGED RECENTLY. THIS PROBLEM WOULD BE IMPOSSIBLE TO DETECT IN-FLIGHT WITH HYDRAULIC POWER ON. TAIL ROTOR CONTROL WOULD BE VERY DIFFICULT WITH HYDRAULIC FAILURE. SUBMITTER STATED WILL CONTINUE 25-HOUR INSPECTION OF FORCE IN THIS AIRCRAFT.