Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-16
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
EXTERNAL INSPECTION
To assure complete removal of frost, ice, snow, or slush from the wing and
control surfaces, as a minimum, conduct a visual and tactile inspection up to
two feet behind the protected surfaces, at one location along the wing span.
Also, ensure the control surfaces contain no internal accumulations of ice or
debris.
1. Wings
..................................................................................................CHECK
2. Horizontal Stabilizer
............................................................................CHECK
3. Vertical Stabilizer
................................................................................CHECK
4. Windshield
..........................................................................................CHECK
5. Porous Panels
.................................... CHECK CONDITION and SECURITY
(Verify evidence of Ice Protection Fluid along length of all panels.)
6. Pitot/Static Tubes
(Verify left and right pitot/static tubes are perceptibly warm)
7. Stall Warning Vane
....................................................................VERIFY HOT
8. Stall Warning Mounting Plate
....................................................VERIFY HOT
9. Propeller
.................................CHECK FOR FLUID FLOW FROM SPINNER
10. Engine Inlet
..........................CHECK CONDITION and PROPER POSITION
11. Windshield Spray Nozzles
............................................ CHECK CONDITION
In the Cabin:
12. Fluid Quantity............................................VERIFY 9.0 GALLONS MINIMUM
13. SURFACE/PROP Switch
.........................................................................OFF
14. Flaps
..................................................... 0-20° AS DESIRED FOR TAKEOFF
15. MASTER Switch
......................................................................................OFF
BEFORE TAKEOFF
ANTICIPATED ICING CONDITIONS IMMEDIATELY AFTER TAKEOFF
1. ENG INLET Switch ...........................................................................BYPASS
2. PITOT HEAT Switches (L&R)
....................................................................ON
3. SURFACE/PROP Switch
............................. NORM or HIGH AS REQUIRED
4. AUX BUS Switch
.......................................................................................ON
5. ECS
.................................INCREASE SET TEMP TO ABOVE CABIN TEMP
6. Defrost
........................................................................................SELECT ON
7. ICE LIGHT Switch
.................................................................. AS REQUIRED
(Verify airframe is free of contamination immediately before takeoff.)
Uncontrolled if printed

Kodiak 100 Series Specifications

General

Manufacturer	Daher
Engine	Pratt & Whitney Canada PT6A-34
Service Ceiling	25, 000 feet
Seating Capacity	10
Crew	1-2
Range	1, 132 nautical miles
Type	Utility aircraft
Length	34 feet 2 inches
Wingspan	45 feet
Max takeoff weight	7, 255 pounds
Power Output	750 shp
Cabin Width	4 feet 6 inches