CESSNA
MODEL 2088 (675 SHP)
INTRODUCTION
PERFORMANCE
-
SPECIFICATIONS
PASSENGER VERSION
(Continued)
STANDARD EMPTY WEIGHT:
SIN 20880179,20880230 thru 208B0381,
and earlier serials modified by SK208-80.
........
.4162 POUNDS
SIN 20880382 and On.
......................
,4237 POUNDS
MAXIMUM USEFUL LOAD:
SIN 20880179,208B0230 thru 20880381,
and earlier serials modified by SK208-80.
......... 4623 POUNDS
SIN
208B0382 and On. ...................... ,4548 POUNDS
WING LOADING
.............................
.31.3 LbslSq. Ft.
POWER LOADING
..............................
13.0 LbslHP
FUEL CAPACITY: Total
SIN 20880001 thru 20880089 not modified
by
SK208-52.
...............................
335 GALLONS
SIN 20880001 thru 20880089 modified by
SK208-52
..................
and SIN 20880090 and On
,335.6 GALLONS
OIL CAPACITY.
................................. 14 QUARTS
ENGINE: Pratt
& Whitney Canada
...................
PT6A-114A
Free Turbine Flat Rated at 675 Shaft Horsepower
PROPELLER:
Hamell 3-bladed. Constant S~eed.
.......
Full Feathering, Reversible. Diameter:.
.............
100 INCHES
McCauley 3-bladed, Constant Speed,
Full Feathering, Reversible. Diameter:
............... 106 INCHES
NOTE
The above performance figures are based on indicated
weights, standard atmospheric conditions, level, hard-
surfaced dry runways and no wind. They are calculated
values derived from fliaht tests conducted bv Cessna
Aircrafr Company under-carefully documenred cond tons
and will varv with individual
air~lanes and numerous factors
affecting
flight performance. Performance for other
operational conditions can be derived by reference to
operational data in other sections of this handbook.
1
Revision 23 U.S.
vlvi
To Next Page
Loading...
