*****AIRCRAFT
“Cessna – C402”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: (Front)
Wing leading mounted
Tail configuration: Regular
tail, mid set
Landing gear: Tricycle retractable
Wing Span: 13.5 m
Length: 11.1 m
Height: 3.6 m
Power plant: 2 x 300 HP
Continental TSIO-520-E or 2 x 325 HP Continental TSIO-520-VB turbocharged
piston engines with 3 blade propellers.
Accommodation: One pilot and 6 passengers in the C401, 8 pax in the C402 and up to 10 in Businessliner.
Notes: 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.
Alternative names:
AVIONES COLOMBIA 402,
Businessliner, CESSNA 401,402,Utililiner,Businessliner
Utililiner, CESSNA 401,402,Utililiner.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs – 2.860 kg
VMO - Maximum Operating Speed 230 KIAS
MMO - Maximum Operating Speed Mach nd Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: L
Distance: 677
mt
V2 (IAS): 95
kts
*****Climbing*****
-(to 5000 ft)
IAS: 125
kt
ROC: 1200
ft/min
-(to FL150)
IAS: 140
kt
ROC: 800
ft/min
-(to FL240)
IAS: 140
kt
ROC: 500
ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 230
kt
MACh: nd
Ceiling: FL270
Range: 500
NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 220
kt
ROD: 800
ft/min
*****Approach*****
IAS: 150
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 110 kt
APC: B
Distance: 538
mt