Kodiak 100 Series User Manual

Pilot’s Operating Handbook
3-17
DO NOT USE FOR FLIGHT OPERATIONS
Section 3
EMERGENCY PROCEDURES
100 SERIES
Emergency
Fuel System Emergencies
Loss of Fuel Pressure
( FUEL PRESS LOW annunciation shown on PFD)
1. AUX FUEL Pump
......................................................................................ON
2. Fuel Pressure Indication
................................................................. CHECK
• If the Fuel Pressure Indication shows approximately 20 PSI:
a. Monitor the fuel quantity gages and the cabin for fuel odor and signs
of fuel leakage.
b. Land as soon as practicable to determine cause for failure of the
motive ow system, prior to the next ight.
• If the Fuel Pressure Indication shows less than 5 PSI:
a. Check the fuel quantity gages for possible fuel starvation.
b. Land as soon as possible.
Interruption of Fuel Flow to Fuel Reservoir
( RESERVOIR FUEL annunciation shown on PFD and aural chime
sounding)
1. Fuel Selector Valves
............................ENSURE LEFT ON and RIGHT ON
2. Ignition Switch
.........................................................................................ON
3. Auxiliary Fuel Pump
................................................................................ON
4. If
RESERVOIR FUEL annunciation remains and usable fuel is available in
the wing tanks:
• Monitor the engine gages and the FUEL PRESS LOW annunciation for
signs of fuel starvation.
• Attempt a steady heading sideslip for 10 seconds to the left and then to
the right, to clear the vent lines of fuel.
• Land as soon as possible to determine the cause of the problem.
• If there are signs of fuel starvation, prepare for an emergency landing as
outlined in the Engine-Out Emergency Landing checklist.
Fuel Tank Selectors Off
( FUEL OFF annunciation shown on PFD, LED instrument panel light
illuminated, and aural chime sounding)
1. Fuel Selector Valves
.....................................................................BOTH ON
NOTE: If the RESERVOIR FUEL annunciation is shown as the result of
fuel starvation, approximately 3 minutes of fuel is remaining in the reservoir
at max continuous power, or 12 minutes of fuel at ight idle (from the time
the annunciation is shown).
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