Kodiak 100 Series User Manual

Pilot’s Operating Handbook
2-1
DO NOT USE FOR FLIGHT OPERATIONS
Section 2
LIMITATIONS
100 SERIES
Limitations
SECTION 2
Limitations
Table of Contents
CONTENTS PAGE
GENERAL
.............................................................................................................2-3
AIRSPEED LIMITATIONS
..................................................................................... 2-4
AIRSPEED INDICATOR MARKINGS
...................................................................2-4
POWERPLANT LIMITATIONS
..............................................................................2-5
PROPELLER SYSTEM OPERATING LIMITATIONS .........................................2-6
ENGINE CONTROL OPERATING LIMITATION
.................................................2-6
ENGINE STARTING CYCLE LIMITATIONS
....................................................... 2-6
POWER PLANT INSTRUMENT MARKINGS
....................................................... 2-8
MISCELLANEOUS INSTRUMENT MARKINGS
................................................2-10
WEIGHT LIMITS
..................................................................................................2-10
CENTER OF GRAVITY LIMITS
.......................................................................... 2-11
CENTER OF GRAVITY RANGE
...................................................................... 2-11
MEAN AERODYNAMIC CHORD (MAC)
.......................................................... 2-11
MANEUVER LIMITS
...........................................................................................2-12
FLIGHT LOAD FACTOR LIMITS
........................................................................2-12
FLIGHT CREW LIMITS
.......................................................................................2-12
KINDS OF OPERATION LIMITS
.........................................................................2-12
FUEL LIMITATIONS
............................................................................................2-18
TOTAL FUEL CAPACITY
..................................................................................2-18
FUEL SYSTEM ICING INHIBITOR (FSII) .........................................................2-18
FUEL SYSTEM ICING INHIBITOR EXCEPTION
.............................................2-18
MAXIMUM OPERATING ALTITUDE LIMITATION
..............................................2-19
OUTSIDE AIR TEMPERATURE LIMIT
...............................................................2-19
MINIMUM OUTSIDE AIR TEMPERATURE LIMIT
..........................................2-19
MAXIMUM OUTSIDE AIR TEMPERATURE LIMIT ..........................................2-19
MAXIMUM PASSENGER SEATING LIMIT
.........................................................2-20
OTHER LIMITATIONS
.........................................................................................2-20
FLAP LIMITATIONS
..........................................................................................2-20
CREW SEAT BELT LIMITATION
......................................................................2-20
ELECTRICAL LOAD LIMITATIONS ..................................................................2-20
USB CHARGING PORTS
................................................................................2-20
GARMIN G1000 OPERATIONAL LIMITATIONS
..............................................2-21
FUEL INDICATION
...........................................................................................2-21
PLACARDS
.........................................................................................................2-22
OPTIONAL SYSTEM PLACARDS ...................................................................2-36
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