*****AIRCRAFT
“Cessna - C177 Cardinal ”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: High wing
Engine position: Nose mounted
Tail configuration: Regular tail, mid set
Landing gear: Tricycle fixed
Wing Span: 10.8 m
Length: 8.2 m
Height: 2.8 m
Power plant: 1 x 150 HP
Lycoming IO-320-E2D or 1 x 180 HP Lycoming
O-360-A1F6D
piston engine with two blade propeller.
Accommodation: One pilot and 3 passengers.
Notes: Light utility aircraft. In service since 1968.
Light utility
aircraft development as a faster replacement for
the CESSNA 172
family. Approx. 4240 aircraft were built between
1968 and 1978.
More powerful, retractable gear development
CESSNA 177RG CardinalRG (ICAO Designator: C77R).
Alternative names:
Cardinal, CESSNA 177,Cardinal, CESSNA
177 Cardinal
*****Total
Flight Simulator aircraft weight with full fuel*****
0000 lbs - 1.070 kg
VMO - Maximum Operating Speed 115 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
0 0
1 0 0
2 0 0
gear down 0
(stalling 0)
*****Take-off*****
WTC: L
Distance: 325
mt
V2 (IAS): 65
kts
*****Climbing*****
-(to 5000 ft)
IAS: 95
kt
ROC: 500
ft/min
-(to FL150)
IAS: nd kt
ROC: nd ft/min
-(to FL240)
IAS: nd kt
ROC: nd ft/min
-(mach)
mach: nd
ROC: nd ft/min
*****Cruise*****
TAS: 115
kt
MACh: nd data
Ceiling: FL120
Range: 590 NM
*****Descent
*****
- (to FL240)
mach: nd
ROD: nd ft/min
- (to FL100)
IAS: 115
kt
ROD: 500
ft/min
*****Approach*****
IAS: 110
kt
MCS: nd kt
ROD: 500
ft/min
*****Landing*****
Vht
(IAS): 65 kt
APC: A
Distance: 275
mt