Kodiak 100 Series User Manual

Pilot’s Operating Handbook Supplement
9.6-8
DO NOT USE FOR FLIGHT OPERATIONS
Section 9
EXTERNAL CARGO COMPARTMENT
ECC
100 SERIES
9.6-4 NORMAL PROCEDURES
NORMAL PROCEDURES CHECKLIST
Preight Inspection
LEFT SIDE
1. Fuselage Floor Skin Drain Holes .................................................CHECK
(Check for any sign of leaks in the aircraft sidewall or sub-oor.)
2. Ensure cargo is secure and within the weight limits of each bay.
3. Ensure three ECC doors are closed and latched.
AFT SECTION
Ensure strakes and ventrals are secure and in good condition.
RIGHT SIDE
Open Fuel Drain Manifold Access Door and sump fuel out of exible plastic
tube into a suitable container by pressing each of the fuel drain manifold
buttons.
RIGHT FRONT
1. Sump Firewall Mounted Fuel Filter by opening access door and pushing
up onto drain sleeve. Drain fuel into a suitable container.
2. Remove engine inlet bypass outlet plugs if installed.
LEFT FRONT
Sump EPA can drain located on bottom of pod fairing.
AMPLIFIED NORMAL PROCEDURES
Preight Inspection
The seventeen (17) fuselage oor skin drain holes should be checked for
any sign of blockage or leakage. Care should be taken to open the cargo
compartment doors and conrm all sidewall and sub-oor drain holes are
clean.
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