Service difficulty report · Control Cable · Lear 45LEAR

Difficulty date
January 10, 2005
Submitted
March 7, 2005
Operation
General aviation
Aircraft
N886CA
Make and model
Lear 45LEAR
Aircraft serial
154
Engine
Garrtt TFE731*
Part
Control Cable
Condition
Worn
Location
Rudder
Part time
1,183 hours
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

AILERON, ELEVATOR, AND RUDDER SYSTEMS PRIMARY CONTROL CABLES ARE DUE INSPECTION AT 600 HOURS IAW MM, AS A PORTION OF PHASE B REQUIREMENTS. ALIERON, ELEVATOR AND RUDDER SYSTEMS PRIMARY CONTROL CABLES ARE DUE REMOVAL AND DETAILED INSPECTION AT 4,800 HOURS IAW MM. PRIMARY FLIGHT CONTROL CABLES ARE NOT LISTED MM (REPLACEMENT SCHEDULE). INSTALLED NEW RUDDER CONTROL CABLES, (PN7627202004-001, 7627202003-001). WORK PERFORMED AFTER INSPECTION IAW PHASE B REQUIREMENTS. (K) (CE09200502303)