*****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