Cessna 402C User Manual

SECTION 1
GENERAL
OIL
Grade:
Viscosity:
MODEL 402C
Aviation grade engine oil. Refer to Section 8 for additional infonnation.
SAE Rating
Ambient Temperature - °C (OF)
50
Above
4.4 (40)
30 Below 4.4 (40)
Multiviscosity Unrestricted - After 25 Hours
Total Sump
Capacity:
Drain and Refill
QuanTIty:
Oil Quantity
Operating Range:
12 quarts per engine
13 quarts per engine including one quart for oil filter.
Do not operate engine on less than 9 quarts. To minimize loss of
oil through breather, fill to 10-quart level for nonnal flights of less
than 3 hours. For extended flight, fill to capacity.
r---..,...---NOTE------.,
Dip stick indicates the quantity of oil in the engine and
does not account for the 1 quart of oil in the oil filter.
MAXIMUM CERTIFICATED WEIGHTS
Maximum Ramp
Weight:
Maximum Takeoff
Weight:
Maximum Landing
Weight:
6885 pounds
6850 pounds
6850 pounds
""SIOI i'j
31 07 l-''J
Maximum Zero
Fuel Weight
Maximum Weights
in Baggage
Compartments
(Passenger
Configuration):
1-4
6515 pounds .') 1 'S S l-c ':-',
j
a. Left and Right Wing Lockers - 2Q~ pounds each.
Inh 'I k.;
b. Avionics Bay - 250 pounds less installed optional equipment
Refer to the loading placard in the airplane avionics baggage
bay.
151k<
c. Nose Bay . 350 P6unds less installed optional equipment
Refer to the loading placard in the airplane nose baggage bay.
1 November 1979
Revision 2 - 3 Aug 1981

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