*****AIRCRAFT “Cessna – C421”*****

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: 12.2 m

Length: 10.3 m

Height: 3.6 m

Power plant: 2 x 375 HP Continental GTSIO-520-H turbocharged piston engine with 3 blade propellers.

Accommodation: One pilot and typical 6 passengers in main cabin.

Notes: Utility twin engine aircraft. In service since 1967. Pressurized development of CESSNA 411. Improved version CESSNA 421B Golden Eagle with lengthened nose and wing span. Last version (from 1975) CESSNA 421C with bonded wet wing, no tip tanks and higher vertical tail. Production ceased in 1985.
Alternative names:
421,Golden Eagle, CESSNA 421,Executive Commuter, CESSNA 421,Golden Eagle
Executive Commuter, Golden Eagle.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs – 3.100 kg

VMO - Maximum Operating Speed 200 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:         600 mt

V2 (IAS):         100 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 130 kt

ROC:               1500 ft/min

-(to FL150)

IAS:                 150 kt

ROC:               1000 ft/min

-(to FL240)

IAS:                 150 kt

ROC:               1000 ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                200 kt

MACh:             nd

Ceiling:                        FL310

Range:            1000 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 190 kt

ROD:               1000 ft/min

 

*****Approach*****

IAS:                 190 kt

MCS:               nd kt

ROD:               1000 ft/min

 

*****Landing*****

Vht (IAS):        95 kt

APC:                B

Distance:         750 mt