NOTICE

SECTION 2 CESSNA
LIMITATIONS MODEL 208B G1000
FLIGHT LOAD FACTOR LIMITS
Flight Load Factors: (Maximum Takeoff Weight - 8750 pounds)
*Flaps UP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . +3.8g, -1.52g
*Flaps Down (All Settings) . . . . . . . . . . . . . . . . . . . . . . . . . . . . +2.4g
*The design load factors are 150% of the above, and in all
cases, the structure meets or exceeds design loads.
FLIGHT CREW LIMITS
One pilot required in left seat.
KINDS OF OPERATIONS EQUIPMENT LIST
The Cessna 208B with Garmin G1000 is equipped for day or night VFR
or IFR operations and flight into known icing conditions when
appropriate equipment is installed. The operating limitation placard
reflects the limits applicable at the time of Airworthiness Certificate
issuance.
The following equipment lists identify the systems and equipment upon
which type certification for each kind of operation was predicated.
These systems and equipment items must be installed and operable
unless:
1. The airplane is approved to be operated in accordance with a
current Minimum Equipment List (MEL) issued by the FAA.
Or;
2. An alternate procedure is provided in the basic FAA Approved
Airplane Flight Manual for the inoperative state of the listed
equipment and all limitations are complied with.
2-14
NOTE
The following systems and equipment list does not included
all equipment required by the 14 CFR Parts 91 and 135
Operating Requirements. It also does not include
components obviously required for the airplane to be
airworthy such as wings, primary flight controls,
empennage, engine, etc.
U.S.
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FAA APPROVED
208BPHBUS-00