Cessna 402C User Manual

MODEL402C
PROPELLERS
Number of
Propellers:
Manufacturer:
Propeller Part
Number.
Number of Blades:
Propeller
Diameter.
Propeller Type:
Blade Range:
~~"""",-,." .
GENERAL
2
McCauley Accessory Division, Cessna Aircraft Company
0850334-29
3
6' 4,5"
Constant speed, full feathering, nonreversible hydraulically
actuated.
(At 30-lnch Station)
a
Low Pitch
b. Feather
14.9° ± 0.2
0
82.2° ±O.3
D
FUEL (Approved Fuel Grades and Colors) *
PRIMARY: 100 (Formerly 1001130) Grade Aviation Fuel (Green)
ALTERNATE:
100ll Grade Aviation Fuel (Blue)
• Isopropyl alcohol, or ethylene glycol monomethyl ether (EGME) may
bel
added to the fuel supply. Additive concentrations by volume shall not
exceed 1% for isopropyl alcohol. Additive concentrations by volume for
EGME shall be 0.10% minimum to 0.15% maximum. Refer to Section 8
for additional information.
Total Fuel Capacity (U.S. Gallons) - 213.4
Usable Fuel (U.S.) Gallons) - 206.0
"1 gD Ll/i:
1 November 1979
Revision 5
- 18 March 1998
1-3

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