Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-11
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
FAILURE OF ICE PROTECTION SYSTEM
(or ice accumulation, observed or suspected,
on protected airplane surfaces)
1. ENG INLET Switch
........................................................... VERIFY BYPASS
2. Pitot Heat Switches (L&R)
.........................................................VERIFY ON
3. SURFACE/PROP Switch
...................................................................... HIGH
4. BACKUP PUMP Switch
...........................................................................ON
5. WINDSHIELD Switch
............................................ON (Momentary Switch)
Repeat operation of windshield pump to verify system is primed properly, as
evidenced by ice protection uid exiting the windshield nozzles.
6. AUX BUS Switch
.......................................................................................ON
7. ECS
.................................INCREASE SET TEMP TO ABOVE CABIN TEMP
8. Defrost
........................................................................................SELECT ON
9. Propeller Lever
.............................................................................. MAX RPM
10. ICE LIGHT Switch
.................................................................. AS REQUIRED
11. Airspeed
........................................................ MAINTAIN 110 KIAS MINIMUM
12. Flaps
.............................................. 0° (KEEP RETRACTED FOR LANDING)
13. Icing Conditions
.............................................EXIT AS SOON AS POSSIBLE
TKS ICE PROTECTION SYSTEM LOW PRESSURE
( TKS LOW PRESS CAS MESSAGE SHOWN)
1. BACKUP PUMP Switch .............................................................................ON
2. SURFACE/PROP Switch
....................................................................... HIGH
3. TKS Ice Protection System
............................................................ MONITOR
4. Airspeed........................................................ MAINTAIN 110 KIAS MINIMUM
5. Flaps
.............................................. 0° (KEEP RETRACTED FOR LANDING)
6. Icing Conditions
.............................................EXIT AS SOON AS POSSIBLE
TKS FLUID HIGH PRESSURE OR LOW QUANTITY
( TKS LOW QTY , TKS LOW QTY OR TKS HI PRESS CAS MESSAGES)
1. Icing Conditions
.............................................EXIT AS SOON AS POSSIBLE
2. TKS Ice Protection System
............................................................ MONITOR
TKS ICE PROTECTION SYSTEM LOW FLOW RATE
( TKS LOW FLOW CAS MESSAGE SHOWN)
1. ICE PROT and STBY ICE PROT circuit breakers ......... RESET, if necessary
2. Windshield Switch......................................................................................ON
Repeat operation of windshield pump to verify system is primed properly, as
evidenced by ice protection uid exiting the windshield nozzles.
3. SURFACE/PROP Switch
....................................................................... HIGH
If warning annunciation is no longer shown:
1. Ice Protection System .................................................................... MONITOR
If warning annunciation remains or is intermittent:
1. BACKUP PUMP Switch .............................................................................ON
2. SURFACE/PROP Switch
.........................................................................OFF
3. Icing Conditions
.......................................................................... AVOID/EXIT
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