Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-19
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
APPROACH AND LANDING
APPROACH AND LANDING
If Icing conditions exist or are anticipated, or at rst sign of ice accretion:
1. ENG INLET Switch
............................................................ VERIFY BYPASS
2. Pitot Heat Switches (L & R)
.........................................................VERIFY ON
3. SURFACE/PROP Switch
....................................................................... HIGH
4. Monitor ice accumulation:
If ice accretion rate is low:
SURFACE/PROP Switch
.................................................................. NORM
If ice is not shedding:
SURFACE/PROP Switch
..................................................................... MAX
If ice accretions do not shed:
Perform Ice Protection System Failure checklist.
5. WINDSHIELD Switch
...................... ON AS REQUIRED (Momentary Switch)
6. ICE LIGHT Switch
.................................................................. AS REQUIRED
7. Flaps
..........................................................................................................20°
8. Airspeed............................................................................85 KIAS MINIMUM
9. Airspeed on Short Final
.....................................................................80 KIAS
BALKED LANDING
1. Power Lever...................................... ADVANCE to MAX TAKEOFF POWER
2. Airspeed.......................................................................... 85 KIAS (Flaps 20°)
3. Flaps
................................................................... RETRACT (95 KIAS to 10°)
4. Airspeed............................................................................95 KIAS (for climb)
CAUTION: To prevent an obstructed view due to residual ice
protection uid on the windshield, do not activate the WINDSHIELD
Switch within 30 seconds of landing.
CAUTION: If a signicant amount of ice has accumulated on the leading
edge of the aps, a FLAP FAIL may occur if the aps are retracted all the
way to 0°. Do not attempt to retract the aps to 0° until stabilized at a safe
altitude and airspeed. Refer to “Section 3” of this manual if a ap failure
occurs when retracting the aps to 0°.
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