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Kodiak 100 Series - Page 118

Kodiak 100 Series
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Pilot’s Operating Handbook
4-6
DO NOT USE FOR FLIGHT OPERATIONS
Section 4
NORMAL PROCEDURES
100 SERIES
Procedures
Empennage (continued)
4. Tail Tie Down ......................................................................... DISCONNECT
(Ensure tail stand removed)
5. Horizontal Stabilizer
....................... CHECK for proper security and condition
6. Vertical Stabilizer
........................... CHECK for proper security and condition
7. Control Surfaces and Elevator Trim Tabs
...........................................CHECK
(Check proper condition, position for takeoff, security, tab free-play, and
freedom of movement.)
8. Static Wicks
......................................... CHECK proper condition (6 required)
9. Antennas...................................CHECK security of installation and condition
10. Aft Nav Light (if equipped)
........... CHECK proper condition and cleanliness
Right Wing Trailing Edge
1. Flap and Flap Tracks ......................................CHECK condition and security
2. Aileron...................................... CHECK freedom of movement and condition
3. Static Wicks
.....................CHECK proper condition and security (1 required)
4. Fuel Tank Vent
..........................................................CHECK for obstructions
Right Wing Leading Edge
1. Navigation and Strobe Lights.........CHECK proper condition and cleanliness
2. Landing and Taxi Lights
.................CHECK proper condition and cleanliness
3. Pitot/Static Tube....................................CHECK for security and obstructions
4. Wing Tie Downs
...................................................................... DISCONNECT
5. Fuel Quantity
....................................................................CHECK VISUALLY
6. Fuel Filler Caps................................................................................ SECURE
Right Side
1. Direct Reading Fuel Quantity Indicator ........................... CHECK QUANTITY
2. Wing Tank Fuel Sump Valve
............................... DRAIN and SAMPLE FUEL
3. Right Main Landing Gear
....................................................................CHECK
(Check for proper tire ination and general condition of the landing gear and
brake systems.)
4. Fuselage Fuel Reservoir Sump Valves
................................................DRAIN
(Check for contamination or debris. Take further samples until all
contamination or debris is removed.)
5. Right Side Crew Door
..............................................CLOSED and LATCHED
WARNING: During cold weather operations, it is essential to remove
even small traces of frost, ice or snow from the wings and control
surfaces. Ensure the control surfaces do not contain internal ice or debris
accumulations. Prior to any ight into potential icing conditions, check the
pitot-static tubes for proper heating within 30 seconds of activating the
necessary switches.
NOTE: Dispose of fuel samples in a proper manner, as turbine fuel will
cause damage to asphalt surfaces.
Uncontrolled if printed

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