Kodiak 100 Series User Manual

Pilot’s Operating Handbook
7-78
DO NOT USE FOR FLIGHT OPERATIONS
Section 7
AIRPLANE & SYSTEMS DESCRIPTIONS
100 SERIES
Systems
ENGINE INSTRUMENTS
The G1000 Engine Indication and Crew Alerting System (EICAS) provides
the pilot with graphical indicators and numeric values for engine, oil, fuel,
electrical, ap, and trim system parameters. The EICAS is shown in a vertical
strip on the MFD during normal operation. In all cases, green indicates
normal operation, yellow indicates caution, and red indicates warning. If
either of the PFDs or the MFD fail during ight, the EICAS will be shown on
the remaining displays. The EICAS consists of three pages that are selected
using the ENGINE softkey.
The default ENGINE page provides indicators for Engine Torque, Inter-
Turbine Temperature (ITT), Propeller RPM, Gas Generator RPM, Fuel
Flow, Oil Pressure, Oil Temperature, Ammeter, Voltmeter, and Fuel Quantity
Indicator. Aileron Trim, Rudder Trim, Elevator Trim, and Flap Position are
shown on each EICAS page.
Figure 7-60 – Default ENGINE Page
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