Cessna 208B - Page 3

CESSNA
MODEL 2088 (675 SHP)
INTRODUCTION
PERFORMANCE - SPECIFICATIONS
CARGO VERSION (Continued)
STANDARD EMPTY WEIGHT:
SIN 20880179,208f30230 thru 20880381,
and earlier serials modified by
SK208-80. ......... 4040 POUNDS
SIN 20880382 and On.
...................... ,4071 POUNDS
MAXIMUM USEFUL LOAD:
SIN 20880179,20880230
th~ 20880381,
and earlier serials modified by
SK208-80. ......... 4745 POUNDS
SIN 20880382 and On.
...................... ,4714 POUNDS
WING LOADING ............................. .31.3 LbslSq. Ft.
POWER LOADING
............................. 13.0 LbslSHP
FUEL CAPACITY: Total
SIN 20880001 thru 20880089 not modified
by
SK208-52. .............................. 335 GALLLONS
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:
Hartzell 3-bladed, Constant Speed,
.............
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 flight tests conducted by Cessna
Aircraft
Comoanv under carefullv documented conditions
and will vary with-individual airplanes and numerous factors
affectina fliaht oerformance.
Performance for other
operatiokal Eonditions can be derived by reference to
o~erational data in other sections of this handbook.
1 Revision 23 U.S. iii