Cessna 402C User Manual

INTRODUCTION
PERFORMANCE AND SPECIFICATIONS
1450 Feet Per Minute
301
Feet Per Minute
5885 Pounds
5850 Pounds
5850 Pounds
5515 Pounds
231
KTAS
194 KTAS
213 KTAS
-
-
1753 Feet
2195 Feet
1055 Feet
2485 Feet
0850334-29
26.900
Feet
14,BOO Feet
TSlO-520-VB
213.4 Gallons
25 Quarts
· 499 Nautical Miles.
3.45 Hours and 141 KTAS
· 855 Nautical Miles,
5.92 Hours and 142 KTAS
1273 Nautical Miles,
8.88 Hours and 142 KTAS
• 459 Nautical Miles.
2.76 Hours and 164 KTAS
• 815 Nautical Miles.
4.89 Hours and 155 KTAS
1233 Nautical Miles
7.41 Hours and 166 KTAS
349 Nautical Miles.
1.90 Hours and 190 KTAS
• 615 Nautical Miles,
3.29 Hours and 191 KTAS
915 Nautical Miles,
4.84 Hours and 192 KTAS
· 362 Nautical Miles.
1.90 Hours and 209 KTAS
· 653 Nautical Miles,
3.29 Hours and 210 KTAS
983 Nautical Miles.
4.84 Hours and 211 KTAS
4074 Pounds
4220 Pounds
4325 Pounds
4102 Pounds
4241 Pounds
1500 Pounds
30.34 Pounds Per Square Foot
10.50 Pounds Per Horsepower
10.000 Feet (900 Pounds Usable
Fuel)
10.000 Feet
(1236 Pounds Usable Fuel)
20,000
Feet (500 Pounds Usable
Fuel)
20.000 Feet
{900 Pound s Usable Fuel}
20,000 Fee.t (l235 Pounds Usable Fuel)
RATE-OF-CLIMB AT SEA LEVEL:
All Engines. . . •
One En9ine Inoperative
SERVICE CEILING:
All Engines.
One Engine Inoperative . • . . . . .
TAKEOFF PERFORMANCE: (95 KIAS, OQ Wing Flaps And 5850 Pounds Weight)
Ground
Roll. .
Total Di stance Over 50-Foot Obstacle
LANDING PERFORMANCE: (95 KIAS, 45
Q
Win9 Flaps And 6850 pou~ds·weighi)
Ground Roll. . . • . . • . •
Total Distance (Over 50-Foot Obstacle)
STANDARD EMPTY WEIGHTS: (Approximate)
402
Businessl iner
402 Businessliner II .
402
Businessliner III
402 Util il iner
402 Utilil iner II
BAGGAGE ALLCMANCE:
WING LOADING: .
POWER LOADING: . .
FUEL CAPACITY: (Total)
Standard (206 Gallons Usable)
OIL CAPACITY: (Total).
ENGINES:
Six-Cylinder. Turbocharged. Fuel-Injected Engines
325 Rated Horsepower
at 2700 Propeller RPM And 39 Inches Hg.
Manifold Pressure To 12,000 Feet. (For Takeoff and One Engine Inoperative
Operation) 310 Horsepower at 2600 Propeller RPM and 39 Inches Hg.
Manifold Pressure To 16.000 Feet. (Nonnal Operating Power)
PROPELLERS:
Constant Speed, Full Feathering, Three-Bladed 6'4.5" Diameter
MAXIMUM WEIGHT:
Ramp
Takeoff .
Landing
Zero Fuel .
*SPEED, BEST POWER MIXTURE:
Maximum - 16,000 Feet
Max imum Recommended Crui se
72% Power at 10,000 Feet
72% Power ,at 20,000 Feet
*RANGE, RECOMMENDED LEAN MIXTURE:
Max imum Recommended Crui se
72% Power at 10,000 Feet
(600 Pounds Usable Fuel)
72% Power at 10,000 Feet
(900 Pounds Usable Fuel)
72% Power at 10,000 Feet
(1236 Pounds Usable Fuel)
72% Power at 20,000 Feet
(600 Pounds Usable Fuel)
72% Power at 20,000 Feet
(900 Pounds Usable Fuel)
72% Power at 20.000 Feet
(1235 Pounds Usable Fuel)
Maximum Range
10.000 Feet (600 Pounds Usable Fuel)
•
•
•
*Range data includes allowances for start, talli. takeoff, climb, descent and 45-minute reserve
fuel at the particular cruise power. Speeds shown are based on estimated mid-cruise weight.
The above perfonnance figures are based on the indicated weights. standard atmospheric con-
ditions. level hard-surface dry runways and no wind. They are calculated values derived
from flight tests conducted by the Cessna Aircraft Company under carefully documented condi-
tions and will vary with individual airplanes and numerous factors affecting flight perform-
ance.
.;.;
1 November 1979
O~v;c;nn 4 _ 1 OPrPmhPr lQR1

Cessna 402C Specifications

General

Manufacturer	Cessna
Model	402C
Type	Light twin-engine aircraft
Maximum Takeoff Weight	6, 850 lb (3, 107 kg)
Service Ceiling	26, 900 ft (8, 200 m)
Seating Capacity	Up to 9 passengers
Wingspan	44 ft 2 in (13.46 m)
Length	36 feet 10 inches (11.23 meters)
Height	11 ft 5 in (3.48 m)
Cabin Width	4 feet 2 inches (1.27 meters)
Cabin Height	4 ft 2 in (1.27 m)
Fuel Capacity	213 US gallons (806 liters)
Engines	2 × Continental TSIO-520-VB turbocharged piston engines