*********10********20********30********40********50********60
*****AIRCRAFT
“Grumman - AA5”*****
REFERENCE INFORMATION (by Wikipedia)
*****Aircraft
Features*****
Wing position: Low wing
Engine position: Nose mounted
Tail configuration: Regular tail, mid set
Landing gear: Tricycle fixed
Wing Span:
9.60m (31ft 6in)
Length: 6.71m (22ft 0in)
Height: 2.40m
(8ft 0in)
Wing area 13.0m2 (140sq ft).
Power plant: AA-5 - One 110kW (150hp) Lycoming
O-320-E2G flat
four piston engine driving a two blade fixed pitch
propeller.
AG-5B - One 135kW (180hp) Textron Lycoming O-360-A4K.
Flightcrew of two and typical __ passengers,
up to __ in high density configuration.
Weights
AA-5 - Empty 545kg (1200lb), max takeoff 998kg
(2200lb).
AG-5B - Empty 595kg (1310lb), max takeoff 1088kg
(2400lb).
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 00.000 kg
VMO - Maximum Operating Speed Max speed 240km/h
(130kt)
VSO – Stall Speed 50 kt
MMO - Maximum Operating Speed Mach .00 Mach
max cruising speed 225km/h (122kt), typical cruising
speed 207km/h (112kt)
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: .
Distance: 000
mt
V2 (IAS): 000
kts
*****Climbing*****
-(to 5000 ft)
Initial rate of climb 660ft/min
IAS: 000
kt
ROC: 660
ft/min
-(to FL150)
IAS: 000
kt
ROC: 0000
ft/min
-(to FL240)
IAS: 000
kt
ROC: 0000
ft/min
-(mach)
mach: 0.00
ROC: 0000
ft/min
*****Cruise*****
TAS: 122
kt
AG-5
- Max speed 240km/h (130kt)
AG-5B
- Max cruising speed 265km/h (143kt)
MACh: no
data
Service ceiling FL120 12,650ft
Range: Range with
reserves 805km (435nm)
*****Descent
*****
- (to FL240)
mach: 0.00
ROD: 0000
ft/min
- (to FL100)
IAS: 000
kt
ROD: 0000
ft/min
*****Approach*****
IAS: 000 kt
MCS: 000
kt
ROD: 0000
ft/min
*****Landing*****
Vht (IAS): 000
kt
APC: .
Distance: 0000 mt