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Kodiak 100 Series User Manual

Kodiak 100 Series
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Pilot’s Operating Handbook
3-21
DO NOT USE FOR FLIGHT OPERATIONS
Section 3
EMERGENCY PROCEDURES
100 SERIES
Emergency
AIRSTART
If an airstart is to be attempted, the checklist procedures should be followed.
The Starter Assisted procedure is the preferred method since it results in
cooler starting temperatures. Successful starter assisted airstarts may be
accomplished at all normal operating airspeeds, and up to an altitude of
16,000 feet. If the engine starter is inoperative, follow the Not Starter Assisted
Airstart checklist.
SMOKE AND FIRE
In the event of re or smoke in the cabin, the following information will be of
assistance in dealing with the emergency as quickly and safely as possible.
The preight checklist in “Section 4” of this manual is provided as an aid to
the pilot in detecting conditions which could possibly lead to an aircraft re.
Fires require a combustible material, oxygen and a source of ignition. Close
attention should be given during the preight inspection to locate potential re
hazards, especially in the engine compartment and underside of the wing and
fuselage. Leaks in the fuel or oil systems can lead to a ground or in-ight re.
WARNING: Do not attempt to y the aircraft with known fuel or oil leaks.
The presence of fuel or unusual oil stains may be an indication of system
leaks and should be remedied prior to ight.
CAUTION:
It takes approximately 15 seconds and 300 feet in altitude to
accomplish a starter assisted airstart (using the HI-START feature)
when established in a glide at 97 KIAS, with the propeller feathered.
When starting the engine, if a rise in
Ng
and ITT are not indicated
within 10 seconds, bring the fuel condition lever into the CUTOFF
position and abort the start. Refer to the “Engine Failure During Flight”
and “Power Off Emergency Landing” checklists.
Do not attempt a “Not Starter Assisted Airstart” with 0%
Ng
.
NOTE: The fuel condition lever may be briey moved to the CUTOFF
position and then returned to LOW IDLE if over-temperature conditions
occur. This momentarily interrupts the fuel ow to the engine combustion
chamber.
Uncontrolled if printed

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Kodiak 100 Series Specifications

General IconGeneral
ManufacturerDaher
EnginePratt & Whitney Canada PT6A-34
Service Ceiling25, 000 feet
Seating Capacity10
Crew1-2
Range1, 132 nautical miles
TypeUtility aircraft
Length34 feet 2 inches
Wingspan45 feet
Max takeoff weight7, 255 pounds
Power Output750 shp
Cabin Width4 feet 6 inches