Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-18
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
WHILE IN ICING CONDITIONS
1. Flaps .............................................................0°, maintain 110 KIAS minimum
2. ICE LIGHT Switch
.................................................................. AS REQUIRED
3. ECS
.................................INCREASE SET TEMP TO ABOVE CABIN TEMP
4. Defrost
........................................................................................SELECT ON
5. Ice Protection Fluid Quantity.......................................................... MONITOR
(Ensure adequate quantity to complete ight.)
AFTER EXITING ICING CONDITIONS
1. SURFACE/PROP Switch .........................................................................OFF
2. Airspeed................................................ AS FLIGHT CONDITIONS DICTATE
3. ICE LIGHT Switch
.................................................................. AS REQUIRED
4. Bleed Air Heat
........................................................................ AS REQUIRED
5. Defrost
................................................................................... AS REQUIRED
6. ENG INLET Switch
.......................................................... LEAVE IN BYPASS
7. WINDSHIELD Switch
.................... ON as required, to remove windshield ice
AUTOPILOT
During icing conditions in cruise, increase engine power (up to maximum
continuous power) to maintain cruise speed as ice accumulates on the
unprotected areas and causes the aircraft to slow down.
The autopilot may be used in icing conditions within the icing envelope
dened in 14 CFR 25 Appendix C (for IAC AR certied airplanes, IAC AR
Aviation Regulations Part 25, Appendix C). However, every 30 minutes the
autopilot should be disconnected to detect any out-of-trim conditions caused
by ice buildup. If signicant out-of-trim or other anomalous conditions are
detected, the autopilot shall remain off for the remainder of the ight.
When disconnecting the autopilot with ice accretions on the airplane, the pilot
should be alert for out-of-trim control forces.
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