Kodiak 100 Series - Maximum Passenger Seating Limit; Other Limitations; Flap Limitations; Crew Seat Belt Limitation

Pilot’s Operating Handbook
2-20
DO NOT USE FOR FLIGHT OPERATIONS
Section 2
LIMITATIONS
100 SERIES
Limitations
2-16 MAXIMUM PASSENGER SEATING LIMIT
Up to ten seats may be installed. The right front seat may be occupied by
either a passenger or a second crew member. Refer to “Section 6” of this
manual for seat locations.
2-17 OTHER LIMITATIONS
FLAP LIMITATIONS
Approved Takeoff Range .............................................0 to 20 Flap Degrees
Approved Landing Range............................................0 to 35 Flap Degrees
Minimum Operating OAT
............................................................. See Below
• Minimum Operating OAT is -55°C for aircraft Serial Numbers 100-0018
and above, and for Serial Numbers 100-0001 through 100-0017 that have
complied with Quest Service Bulletin “SB-016: FLAP SYSTEM, Flap Drive
Actuator Replacement.”
• Minimum Operating OAT is -25°C for aircraft Serial Numbers 100-0001
through 100-0017 that have NOT complied with Quest Service Bulletin
“SB-016: FLAP SYSTEM, Flap Drive Actuator Replacement.”
CREW SEAT BELT LIMITATION
Crew inertia reel levers must be placed in the locked position prior to takeoff
and landing.
ELECTRICAL LOAD LIMITATIONS
Maximum Allowable Starter/Generator Electrical Load Limitation
Minimum
Ng
Engine Speed (%) Maximum Generator Load (AMPS)
53 (Ground) 80
61 (Flight) 300
Maximum Allowable Alternator Electrical Load Limitation
Minimum
Ng
Engine Speed (%) Maximum Alternator Load (AMPS)
53 (Ground) 25
61 (Flight) 40
Table 2-10 – Electrical Load Limitations
USB CHARGING PORTS
Passengers may not use the cabin USB charging ports during takeoff and
landing. Operation of the passenger USB ports is limited to cruise only. Crew
members may use their USB ports during the entire ight.
NOTE: Maximum alternator load at ground idle may exceed 25 AMPS for
approximately 5 minutes after start up.
Uncontrolled if printed