CESSNA 402 Businessliner

Aircraft
Name: 
402 Businessliner
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
Regular tail, mid set
WTC
L
APC
B
Type Code: 
L2P
Engine: 
Piston
Engine Count: 
Multi
Position: 
(Front) Wing leading mounted
Landing gear: 
Tricycle retractable
Manufacturered as
CESSNA 401
CESSNA 402
CESSNA 402 Businessliner
CESSNA 402 Utililiner
CESSNA Businessliner
CESSNA Utililiner
AVIONES COLOMBIA 402

C402

Commuter and business aircraft. In service since 1967 (402 since 1972). Cessnas entry into eight seats cabin class. Replacement for CESSNA 411 as an Airline version. CESSNA 402 replaced the 401 from mid 1972. 402B was offered as corporate business liner, 402A with lengthened nose and square wings and 402C with longer wingspan (from 414A) and more powerful engines. Production ceased in 1985. CESSNA 401 has 3 large and 1 small round window whereas 402 has 5 square windows on each side.

Technical Data
Wing span: 
13.50 m
Length: 
11.10 m
Height: 
3.60 m
Powerplant: 

2 x 300 HP Continental TSIO-520-E or 2 x 325 HP Continental TSIO-520-VB turbocharged piston engines with 3 blade propellers.

Engine Model: 
Continental O-520
Indicative Performance Data
Take-Off
V2: 
95 kts
Distance: 
677 m
MTOW: 
2860 kg
Initial Climb (to 5000 ft)
IAS: 
125 kts
ROC: 
1200 ft/min
Initial Climb (to FL150)
IAS: 
140 kts
ROC: 
800
Initial Climb (to FL240)
IAS: 
140 kts
ROC: 
500 ft/min
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
230 kts
MACH: 
n/a
Ceiling: 
270
Range: 
500 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
220 kts
ROD: 
800 ft/min
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
110 kts
Distance: 
538 m

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