Leerjet 35/36 Developed for Training Purposes 2A-3
February 1998
Preflight Inspection
B Right Nose
Oxygen Bottle Supply Valve (if installed) . . . . . . . . . . . . . . ON
Pitot Head (FC-200)/Probe (FC-530). . . . . .REMOVE COVER/
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
Total Temperature Probe (if installed) . . . . . . . . . . . . . CLEAR
Stall Warning Vane. . . . . . . . . . . . . . . . . . . .FREE AND DOWN
Static Ports/Shoulder Static Port (FC-200). . . . . . . . . . . CLEAR
Pitot Static Drain Valves. . . . . . . . . . . . . . . . . . . . . . . . . DRAIN
Pressurization Static Port. . . . . . . . . . . . . . . . . . . . . . . . CLEAR
Oxygen Discharge Disk (if installed) . . . . . CHECK IN PLACE
Defog Outlet. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
Lower Fuselage Antennas/Rotating Beacon . . . . . . . . .CHECK
Wing Inspection Light (if installed) . . . . . . . . . . . . . . . .CHECK