- Check covers removed,
Radome - Check condition.
- Check general condi-
Monopole antennas (2) - Check general
Windshields and wipers - Check wind-
shield for cracks and cleanliness and
wipers for contact with glass surface.
Air conditioner inlet - Check free of
Avionics door, right side - Check
8-21. CENTER SECTION, RIGHT SIDE.
Center section - Check as follows:
Inboard deice boot - Check for secure
bonding, cracks, loose patches, and
Battery access panel - Secure.
Battery vents - Check free of obstruc-
Auxiliary tank fuel gage and cap -
Check fuel level visually, condition of
seal, and cap tight and properly
installed (locking tab aft).
Battery compartment drain - Check
free of obstruction.
Battery ram air intake - Check free of
INS TAS temperature probe - Check
condition and free of obstructions.
Auxiliary tank fuel sump drain - Check
Heat exchanger inlet and outlet - Check
for cracks and free of obstructions.
Monopole antenna - Check condition.
8-22. RIGHT ENGINE AND PROPELLER.
1. Right engine and propeller - Check as fol-
A cold oil check is unreliable. Oil should
be checked within 10 minutes after stop-
ping engine. If more than 10 minutes
have elapsed, motor engine for 30 sec-
onds, then recheck. If more than 10 hours
have elapsed, run engine for 2 minutes,
then recheck. Add oil as required. Do not
Engine oil - Check oil level, oil cap
secure (locking tab aft), and access
Engine compartment, left side - Check
for fuel and oil leaks, security of oil
cap, door locking pins, and general
Left cowl locks - Locked.
Left exhaust stack - Check for cracks
and free of obstructions.
Propeller blades and spinner - Check
blade condition, boots, security of spin-
ner, and free propeller rotation.
Engine air inlets and ice vane - Check
free of obstruction and ice vane
Bypass door - Check condition.
Right cowl locks - Locked.
Right exhaust stack - Check for cracks
and free of obstructions.
Engine compartment, right side -
Check for fuel and oil leaks, ice vane
linkage, door locking pins, and general
condition. Lock compartment access
8-23. RIGHT MAIN LANDING GEAR.
Right main landing gear - Check as follows:
Fuel sump drains (forward) - Check for
Tires - Check for cuts, bruises, wear,
proper inflation and wheel condition.
Brake assembly - Check brake lines for
damage or signs of leakage, brake lin-
ings for wear (0.25 inch maximum,
between piston housing and lining car-
rier), brake deice assembly and bleed
air hose for condition and security.
Shock strut - Check for signs of leak-
age, minimum strut extension (5.50
inches), and that left and right strut
extension is approximately equal.