*****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