Maximum Operating Altitude Limitation; Outside Air Temperature Limit; Minimum Outside Air Temperature Limit; Maximum Outside Air Temperature Limit - Kodiak 100 Series Information Manual

Uncontrolled if printed
2. The aircraft has been continuously parked or operated at or above
5°C since the last flight when the fuel system contained specified
concentrations of DIEGME anti-icing fuel additive, AND
3. Fuel filler port placards, shown in the placard section, comply with the
limitations given.
If fuel with DIEGME is not used, the operator is required to use a biocidal
fuel additive given in "Section 1" of this manual. Any operation with fuel
that does not contain DIEGME will require the operator to verify appropriate
concentration levels of DIEGME in the aircraft's fuel system, whenever this
component is reintroduced.
WARN I NG:
for any length of time without an approved fuel system icing inhibitor, the
icing inhibitor must be reintroduced prior to next flight. After reintroducing
the icing inhibitor and verifying that the appropriate concentration levels
have been achieved, the operator shall perform the following checks prior
to next flight:
1. Inspect both fuel tanks for signs of ice and/or other contaminates.
2. Perform an engine run of at least 20 minute duration, during which the
engine is operated for at least 3 minutes at takeoff power levels.

2-14 MAXIMUM OPERATING ALTITUDE LIMITATION

The certificated maximum operating altitude is 25,000 feet.

2-15 OUTSIDE AIR TEMPERATURE LIMIT

MINIMUM OUTSIDE AIR TEMPERATURE LIMIT

-55°C from sea level, to a pressure altitude of 25,000 feet.
NO TE :
The landing lights are limited to operations at temperatures above
-40°C. Do not operate the landing lights at temperatures colder than -40°C.

MAXIMUM OUTSIDE AIR TEMPERATURE LIMIT

Ground Operations: +53°C from sea level, to 5000 feet. ISA +37°C above
5000 feet.
Flight Operations: ISA +35°C from sea level, to 25,000 feet.
P i l o t 's O p e r a t i n g H a n d b o o k
1 0 0 S E R I E S
Table 2-7 – (Moved to "Section 1")
If the aircraft becomes exposed to temperatures below 5°C
Table 2-8 – (Moved to "Section 1")
Table 2-9 – (Moved to "Section 1")
D O N OT U S E FO R FL I G H T O PE R AT I O N S
S e c t i o n 2
L I M I TAT I O N S
2 -19