Service difficulty report · Control Rod · Cndair CL6002C10

Difficulty date
August 12, 2007
Submitted
October 24, 2007
Operation
General aviation
Make and model
Cndair CL6002C10
Engine
Ge CF34*
Part
Control Rod
Part number
BA6709260213
Condition
Unknown
Location
Vertical Stab
Stage of operation
TX
How discovered
O
Nature of condition
F
Precautionary procedure
D

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

What was found

(CAN) AFTER ENGINE START FOR DEPARTURE FLIGHT AF 7836 ,THE ELEVATOR WAS FOUND JAMMING DURING CHECK LIST . AIRCRAFT RETURNED TO THE GATE. THE EFFORTS ARE NORMAL ON CONTROL COLUMN UNTIL HALF WAY THE BECOMES HARD. EICAS INDICATION FOR THE ELEVATOR SHOWS FULL DEFLECTION WHEN THE CONTROL COLUMN REACHES HALF WAY . IN REFERENCE TO N16/07 THE ACFT WAS IN CHECK AND COMPLETED ALL GROUND AND FLT TESTS SATISFACTORY . THE ACFT WAS REPOSITIONED. THE SB 670BA-27-022 WAS DONE AND INSPECTED BUT A BUSHING REPLACEMENT WAS PENDING TO FULLY COMPLETE THE SB . DURING THIS BUSHING REPLACEMENT AN INVERSION OF THE ACTUATING RODS WAS DONE BETWEEN UPPER AND LOWER POSITION ON THE LEVER. THE RODS WERE REPOSITIONED IN NORMAL CONFIGURATION AND SYSTEM WORKED SATISFACTORY.