Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.4-3
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
TKS ICE PROTECTION
TKS Ice Protection
100 SERIES
TKS ICE PROTECTION SYSTEM
Table of Contents
CONTENTS PAGE
GENERAL ..........................................................................................................9.4-7
LIMITATIONS
.....................................................................................................9.4-7
OUTSIDE AIR TEMPERATURE LIMITS
........................................................9.4-7
ENVIRONMENTAL CONDITIONS
.................................................................9.4-7
AIRSPEED LIMITATIONS
...............................................................................9.4-8
FLAP LIMITATIONS ........................................................................................9.4-8
WEIGHT LIMITS
.............................................................................................9.4-8
REQUIRED EQUIPMENT
...............................................................................9.4-9
APPROVED ICE PROTECTION FLUIDS
.......................................................9.4-9
MINIMUM DISPATCH FLUID LEVEL
.............................................................9.4-9
ICE PROTECTION FLUID LIMITS ..................................................................9.4-9
MAXIMUM AVAILABLE SYSTEM OPERATING TIME
................................ 9.4-10
VISUAL/TACTILE CHECK
............................................................................ 9.4-10
WINDSHIELD PUMP
....................................................................................9.4-10
INERTIAL SEPARATOR
............................................................................... 9.4-10
AUTOPILOT .................................................................................................. 9.4-10
MAXIMUM OPERATING ALTITUDE
............................................................ 9.4 -11
REQUIRED PLACARDS
............................................................................... 9.4 -11
EMERGENCY PROCEDURES
........................................................................ 9.4-12
FAILURE OF ICE PROTECTION SYSTEM
.................................................. 9.4-13
TKS ICE PROTECTION SYSTEM LOW PRESSURE .................................. 9.4-13
TKS FLUID HIGH PRESSURE OR LOW QUANTITY
.................................. 9.4-13
TKS ICE PROTECTION SYSTEM LOW FLOW RATE
................................. 9.4-13
TKS ICE PROTECTION SYSTEM HIGH FLOW RATE
................................ 9.4-14
INADVERTENT ICING ENCOUNTER AT ALTITUDES ABOVE 20,000 FT
9.4-14
INERTIAL SEPARATOR MALFUNCTION .................................................... 9.4-14
PROPELLER ANTI-ICE SYSTEM MALFUNCTION
..................................... 9.4-14
WINDSHIELD ANTI-ICE SYSTEM MALFUNCTION
.................................... 9.4-15
PITOT STATIC HEAT FAILURE
.................................................................... 9.4-15
STALL WARNING HEAT FAILURE
.............................................................. 9.4-15
HIGH OR LOW ICING SPEED ..................................................................... 9.4-15
NORMAL PROCEDURES
...............................................................................9.4-16
AIRSPEEDS FOR NORMAL OPERATIONS
................................................ 9.4-16
PREFLIGHT INSPECTION
........................................................................... 9.4-17
CABIN
........................................................................................................... 9.4-17
EXTERNAL INSPECTION ............................................................................9.4-18
BEFORE TAKEOFF
...................................................................................... 9.4-18
ANTICIPATED ICING CONDITIONS IMMEDIATELY AFTER TAKEOFF
.... 9.4-18
ICE FORMATION DETERMINATION
........................................................... 9.4-19
IN-FLIGHT..................................................................................................... 9.4-19
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