Cessna 402C User Manual

r~~~402C
SECTION 1
GENERAL
Never Exceed Speed ; 5 the speed 1 imit that may not be
exceeded at any time.
~1aximum Structural Cru; sing Speed ;s the speed that
should not be exceeded except in smooth air and then
only with caution.
Intentional
One Engine Inoperative Speed ;s a minimum
speed selected by the manufacturer for intentionally
rendering one engine inoperative in f1 ight for pilot
training.
Best Angle-or-Climb Speed is the airspeed which delivers
the greatest gain of a1 titude in the shortest possible
horizontal distance.
Best Rate-or-Climb Speed is the airspeed which delivers
the greatest gain in altitude in the shortest possible
time.
METEOROLOGICAL TERMINOLOGY
Temperature in degrees Celsius.
ISA
OAT
Pressure
Altitude
Temperature in degrees Fahrenheit.
International Standard Atmosphere in which:
(I) The air is a dry perfect gas;
(2) The temperature at sea level is IS° Cel sius (59°
Fahrenheit) ;
(3) The pressure at sea level is 29.92 inches Hg.
(1013.2 mb);
(4) The temperature gradient from sea level to the
altitude at which the temperature is _56.5°C
(-69.7°F) is -1. 98°C (_3.5°F) per 1000 feet.
Outside Air Temperature is the free air static tempera-
ture, obtained either from infl ight temperature indica-
tions adjusted for instrument error and compressibility
effects or ground meteorological sources.
Altitude measured from standard sea-level pressure
(29.92 inches H9.) by a pressure or barometric altim-
eter. It is the indicated pressure altitude corrected
for position and instrument error. In this handbook,
altimeter instrument errors are assumed to be zero.
-"
TEMP
Wind
TEMP is temperature.
The wind velocities recorded as variables on the charts
of this handbook are to be understood as the headwind or
tailwind components of the reported winds.
I
I November 1979
Revision 4 - I December 1983
1-9

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