Kodiak 100 Series User Manual

Pilot’s Operating Handbook
4-10
DO NOT USE FOR FLIGHT OPERATIONS
Section 4
NORMAL PROCEDURES
100 SERIES
Procedures
External Power Engine Start
(24-28 VOLTS, 800 AMPS Min / 1700 AMPS Max)
1. External Power
...............................................................CONNECT then ON
2. Battery Master Switch
................................................................................ ON
3. Buss 1 Voltage
.............................................................CHECK 24V minimum
4. Flashing Beacon
........................................................................................ON
5. Emergency Power Lever
................NORMAL – Check EMER PWR LVR NOT
shown on PFD
6. Propeller Area
..................................................................................... CLEAR
7. Auxiliary Fuel Pump
............................................................................... STBY
• Check AUX PUMP ON annunciator ..............................SHOWN ON PFD
• Fuel Flow ......................................................................................... ZERO
8. Auxiliary Fuel Pump...................................................................................ON
9. Ignition Switch........................................................................ AS REQUIRED
• ON for LO/MOTOR START
• OFF for HI START
10. Starter Switch
........................................ HI or LO/MOTOR as required and:
• The IGNITION ON annunciator ..................................... SHOWN ON PFD
• Engine Oil Pressure ........................................................ CHECK RISING
•
Ng
...................................................................... STABLE (14% minimum)
11. Fuel Condition Lever
.............................................................. LOW IDLE and:
• Fuel Flow ...........................................................CHECK at 80 to 110 lb/hr
• ITT .............................. MONITOR (1090°C maximum – limited to 2 sec.)
•
Ng
......................................................................................52% MINIMUM
12. Starter Switch
.................... OFF – Check STARTER ON annunciator NOT
shown on PFD
13. Ignition Switch
....................OFF – Check IGNITION ON annunciator NOT
shown on PFD
14. Propeller Lever
.......................................................................... MAX RPM
15. Engine Instruments..........................................................................CHECK
16. Auxiliary Fuel Pump............................................................................STBY
17. External Power
.................................................................... DISCONNECT
18. Generator
..............................................................................................ON
19. Alternator
................................................................................................ON
20. Exterior Lights..................................................................... AS REQUIRED
21. Cabin Heat, Ventilation and Defrost
................................... AS REQUIRED
22. Radios / Avionics
.................................................................................. SET
23. Preight Procedure for the GMA 1347 Audio Panels................. PERFORM
CAUTION: If the emergency power lever is not secured in the NORMAL
(full aft detent) position for starting, an engine over-temperature condition
(hot-start) may result.
CAUTION: If the ITT rises rapidly towards 1090°C, be prepared to bring
the fuel condition lever to CUTOFF to prevent a hot-start.
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