Service difficulty report · Torque Link · Cndair CL6002C10

Difficulty date
October 16, 2005
Submitted
December 2, 2005
Operation
General aviation
Make and model
Cndair CL6002C10
Engine
Ge CF348C1
Part
Torque Link
Condition
Disconnected
Location
Lt Mlg
Component
Lt Mlg · 492009
Stage of operation
LD
How discovered
O
Nature of condition
D, E
Precautionary procedure
K

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

What was found

(CAN) HVY VIBRATION AFTER TD UNTIL TAXI SPEED IS REACHED. INDEPENDENT FROM BRAKE APPLICATION. AC WAS SMOOTH DURING TAXI AND TAKEOFF ROLL. ON ARRIVAL FOUND LT MLG TORQUE LINK DISCONNECTED. WHEEL NR 2 DESTROYED. SHIMMY DAMPER TORN OFF. VARIOUS DAMAGE ON BRAKE NR2, UPPER AND LOWER LINK, HYD LINE AND HARNESS FIXTURE. ALMOST ALL PARTS COLLECTED ON RWY. SUSPECT DISCONNECT WAS CAUSED BY INCOMPLETE OR MISSING ASSY OF TORQUE LINK CONNECTING PIN SAFETY BOLT IPC REF 32-11-42 ITEM 35, NOT FOUND ON RUNWAY. NOTICED INITIAL OIL LEAKAGE FROM LT MLG SHOCK STRUT. LT MLG REPLACED. LT SIDE STAY REPLACED. DVI OF STRUCTURE SURROUNDING GEAR ATTACHMENT PERFORMED, NO FINDING. FDR DOWNLOAD PERFORMED. NO ACTION REQUIRED AFTER ANALYSIS.