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Kodiak 100 Series User Manual

Kodiak 100 Series
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Pilot’s Operating Handbook Supplement
9.6-54
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
EXTERNAL CARGO COMPARTMENT
ECC
100 SERIES
9.6-6 WEIGHT AND BALANCE
EXTERNAL CARGO COMPARTMENT BAY LOADING LIMITS
The following gure denes the loading limits for the various External Cargo
Compartment zones, if equipped.
Bay FS (inches) Maximum Load (pounds)
1 26.0 290
2 75.25 280
3 110.75 180
Figure 9.6-1 – External Cargo Compartment Bay Loading Limits
9.6-7 AIRPLANE AND SYSTEMS DESCRIPTIONS
The ECC, with a 63-cubic-foot area and a 750 pound capacity, may be
installed on KODIAK
®
100 airplanes. The ECC is constructed of two pieces –
the nose fairing and the main pod – which are separated by a stainless steel
rewall.
The ECC and its doors have a foam composite core, strips of a nonwoven
metallic lightning and shielding mesh, a layer of ground plane mesh, and an
outer layer of berglass.
Two bulkheads divide the pod into three compartments. Each compartment
may be accessed through a separate door located in the left side of the pod.
Ventral ns, strakes, and aerodynamic fences are installed to provide
additional stability about the yaw axis. A fuel drain system enables exterior
access to the fuel drain lines.
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