Learjet 35 - Page 91

Leerjet 35/36 Developed for Training Purposes 2B-67
October 2001
Expanded Normal Procedures
Cabin Window Covers . . . . . . . . . . . . . . . . . . . . INSTALLED
Place a window protective cover over each of the cabin win-
dows; secure and seal the covers around the edges with
black tape.
Avionic Equipment . . . . . . . . . . . REMOVED AND STORED
Remove and store avionic equipment in accordance with
manufacturer’s recommended procedures.
Pitot/Static System
Pitot Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURED
Tape a small piece of barrier material around pitot tube and
install pitot tube cover.
Static Ports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURED
Cut small pieces of barrier material and place them over the
static ports. Secure and seal them from the atmosphere by
taping around the perimeter of barrier material.
Landing Gear
Tires . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REPLACED
Replace serviceable tires with unserviceable tires.
Brakes. . . . . . . . . . . . . . . . . . REMOVED AND PRESERVED
Remove brakes and preserve in brake preservative accord-
ing to procedure outlined in Maintenance Manual.
Anti-Skid Wheel Transducer . . . . . . . . . . . . . . . . . SERVICED
Remove anti-skid wheel transducer and apply brake preser-
vative inside the hub. Re-install anti-skid wheel transducer.
Landing Gear Strut . . . . . . . . . . . . . . . . . . . . . .LUBRICATED
Main and Nose Gear
Shock Struts . . . . . . . . . . . . . . . CHECKED EVERY 30 DAYS