Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-12
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
TKS ICE PROTECTION SYSTEM HIGH FLOW RATE
( TKS HI FLOW CAS MESSAGE SHOWN WITHOUT A LOW PRESSURE
TKS LOW PRESS ANNUNCIATION)
1. Ice Protection System .................................................................... MONITOR
2. Ice Protection Fluid Quantity.......................................................... MONITOR
3. Icing Conditions
.......................................................................... AVOID/EXIT
INADVERTENT ICING ENCOUNTER AT ALTITUDES ABOVE 20,000 FT
1. IGNITION Switch .......................................................................................ON
2. SURFACE/PROP Switch
.............................NORM (Select HIGH if required)
3. WINDSHIELD Switch
.................................................................................ON
4. Left and Right Pitot Heat Switches
............................................................ON
5. Engine Inlet Inertial Separator
..........................................................BYPASS
6. Cabin Heat/Defrost
....................................................................................ON
7. Airspeed........................................................................190 KTAS MAXIMUM
8. Altitude
............. DESCEND TO 20,000 FEET (or lower as soon as practical)
9. IGNITION Switch ........................OFF (when icing conditions are exited)
INERTIAL SEPARATOR MALFUNCTION
( INLET NOT BP CAS MESSAGE SHOWN)
1. Primary ENG INLET Switch ................................................VERIFY BYPASS
2. Override ENG INLET Switch
............................................................BYPASS
If inertial separator fails to move to BYPASS ( INLET NOT BP CAS
message still shown):
1. IGNITION Switch .......................................................................................ON
2. Icing Conditions
.............................................EXIT AS SOON AS POSSIBLE
PROPELLER ANTI-ICE SYSTEM MALFUNCTION
If uneven or inadequate anti-icing of the propeller blades is indicated by
vibration:
1. TKS NRM MODE or TKS HI MODE CAS message VERIFY SHOWN ON
PFD
(SURFACE PROP Switch in NORM or HIGH position)
1. Propeller Lever
........................................... EXERCISE (Then to MAX RPM)
If excessive propeller vibration continues:
1. SURFACE/PROP Switch ........................................................................ MAX
2. Icing Conditions
.............................................EXIT AS SOON AS POSSIBLE
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