SECTION 2
LIMITATIONS
-
CESSNA
MODEL
2088 (675 SHP)
FLIGHT LOAD FACTOR LIMITS
Flight Load Factors:
'Flaps Up:
+3.8g, -1.529
'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 OPERATION LlMlTS
.-
This airplane is equipped for day VFR and may be equipped for night
VFR
and/or IFR operations and for flight-into-known icing conditions.
. .
The operating limitations placard reflects the limits applicable at the
time of
Aiworthiness Certificate issuance.
.
~
The follow.ng eq~ipment I sts identify the systems and equipment Lpon
wnich type cenification for each k~nd of operation was predicated.
These systems and equ pment items must be
insralled and operable for
rhe partc~lar kind of operation indicated. Reference sho~ld also be
made to the Equipment List furnished with the airplane for additional
equipment information. The pilot is responsible for determining the
airworthiness of his airplane for each flight and for assuring compliance
with current operating
FAR'S.
(Continued Next Page)
FAA APPROVED
Revision 23
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