Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-15
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
PREFLIGHT INSPECTION
Preight Inspection Warnings
Use of a ladder may be necessary to gain access to the wing for visual of the
stall warning heat, and pitot/static system heat.
In cold weather, it is essential to remove even the smallest accumulations
of frost, ice, snow, or slush from the wing, tail, control surfaces, propeller
blades, and the power plant air inlets. To assure complete removal of
contamination, conduct a visual and tactile inspection of all critical surfaces.
Also, ensure the control surfaces contain no internal accumulations of ice or
debris. If these requirements are not accomplished, aircraft performance will
be degraded to a point where a safe takeoff and climb may not be possible.
CABIN
1. Circuit Breakers ....................................................................................... SET
2. MASTER Switch
........................................................................................ON
3. DISPLAY/BACKUP Button
............................................. PRESS (Button Out)
4. Cabin Doors
........................................................................................CLOSE
5. WINDSHIELD Switch
................................................ON (Momentary Switch)
(Verify presence of Ice Protection Fluid from spray nozzles.)
6. SURFACE/PROP Switch
..................................................................... NORM
7.
TKS NRM MODE Annunciation ....................................................... SHOWN
8. Pump Duty Cycle
........................................ VERIFY 30 sec ON, 90 sec OFF
(Both Pumps)
9.
INLET NOT BP Annunciation .......................................................... SHOWN
10.
ENG INLET BP Switch ....................................................................BYPASS
11.
INLET NOT BP Annunciation ..................................................NOT SHOWN
12. SURFACE/PROP Switch
.........................................................................OFF
13. BACKUP PUMP Switch
.............................................................................ON
14.
TKS BACKUP Annunciation ........................................................... SHOWN
15. Metering Pump
..........................................VERIFY RUNS CONTINUOUSLY
16. BACKUP PUMP Switch
...........................................................................OFF
17. ICE LIGHT Switch
....................................................ON, VERIFY LH and RH
18. PITOT HEAT Switches (L and R)
................... ON 30 SECONDS, THEN OFF
19. SURFACE/PROP Switch
.....................................................MAX and then HI
20.
TKS MAX MODE Annunciation ....................................................... SHOWN
21. Metering Pumps................................................VERIFY BOTH PUMPS RUN
22. Pump Duty Cycle
..........................................VERIFY 2 minutes on and then:
23.
TKS HI MODE Annunciation ........................................................... SHOWN
24. Metering Pumps.........................................VERIFY RUNS CONTINUOUSLY
NOTE: The TKS LOW PRESS annunciation may appear if the system
has not been activated recently and/or if the OAT and uid temperature is
relatively warm (lower viscosity).
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