Cessna 402C User Manual

SECTION 1
GENERAL
I.!'I'<,
d. Aft Cabin (Bay A) See Figure 1-3 - 400 pounds (200
Pounds Per Side).
"~t<.!l
e. Aft Cabin (Bay B) See Figure 1-3 - 100 pounds (50
Pounds Per Side).
Maximum Weights
in Baggage
Compartments
(Cargo
Configuration) :
a.
b.
c.
d.
e.
f.
g.
"I, "5
Left and Right Wing Lockers - 200 pounds each.
/I~><J
Avionics Bay - 250 pounds less installed optional
equipment. Refer to the loading placard in the
airplane avionics
baggage bay.
'Pi",,>
Nose Bay - 350 pounds less installed optional
equipment. Refer to the loading placard in the
airplane nose baggage bay.
'1o~~.
Cargo A Through Cargo 0 - Maximum/cargcr load aft of
the front spar is not to exceed 2000 pounds. Maxi-
mum cargo load in any 22.5-inch length of cabin
floor
is not to exceed 500 Rounds. The total cabin
load, including
optional~qu1pment aft of Station
238.1,
is not to exceed 600 pounds.
z..7"Z-~, / tl II!
Aft Cabin (Bay A) See Figure 1-3 400 iounds (200
Pounds Per Side).
II:~~
Aft Cabin (Bay B) See Figure 1-3 - 100 pounds (50
Pounds Per Side).
Refer to Section 7, Cargo Loading for additional
information.
STANDARD AIRPLANE WEIGHTS
Standard Empty
Weight
(Bus; nessl iner):
Sta nda rd Empty
Weight
(Utililiner):
Maximum Usefu 1
Load
(Businessliner):*
Maximum Usefu 1
Load
(Utililiner):*
4074 pounds (4220 pounds for 402 Businessliner II) (4325
pounds for 402 Businessliner III)
4102 pounds (4241 pounds for 402 UtililinerII)
2811 pounds (2665 pounds for 402 Businessliner II) (2560
pounds for 402 Businessliner III)
2783 pounds (2645 pounds for 402 Utililiner II)
*Based On Maximum Ramp Weight.
I November 1979
1-7

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