Kodiak 100 Series User Manual

Pilot’s Operating Handbook
4-9
DO NOT USE FOR FLIGHT OPERATIONS
Section 4
NORMAL PROCEDURES
100 SERIES
Procedures
ENGINE STARTS
Battery Powered Engine Start
1. Buss Voltages ..............................................................CHECK 24V minimum
2. Flashing Beacon
........................................................................................ON
3. Emergency Power Lever
................NORMAL – Check EMER PWR LVR NOT
shown on PFD
4. Propeller Area ..................................................................................... CLEAR
5. Auxiliary Fuel Pump
............................................................................... STBY
• Check AUX PUMP ON Annunciator ..............................SHOWN ON PFD
• Fuel Flow ......................................................................................... ZERO
6. Auxiliary Fuel Pump
................................................................................... ON
7. Ignition Switch........................................................................ AS REQUIRED
• ON for LO/MOTOR START
• OFF for HI START
8. Starter Switch
........................................... HI or LO/MOTOR as required and:
• The IGNITION ON Annunciator.....................................SHOWN ON PFD
• Engine Oil Pressure ........................................................ CHECK RISING
•
Ng
......................................... ACCELERATING THROUGH 14% MINIMUM
9. 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
10. Starter Switch .................... OFF – Check STARTER ON annunciator NOT
shown on PFD
11. Ignition Switch
........................OFF – Check IGNITION ON annunciator NOT
shown on PFD
12. Propeller Lever
............................................................................. MAX RPM
13. Engine Instruments
.............................................................................CHECK
14. Auxiliary Fuel Pump
............................................................................... STBY
15. Generator ..................................................................................................ON
16. Alternator
...................................................................................................ON
17. Exterior Lights
........................................................................ AS REQUIRED
18. Cabin Heat, Ventilation and Defrost....................................... AS REQUIRED
19. Radios / Avionics
..................................................................................... SET
20. 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