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Aquila A211 Spec


Speed *
VNE Never Exceed Speed 165 knots
VNO Speed for normal Operations 165 knots
Maximum Range (5,000 ft at 55% power) 620 NM
CLIMBRATE(MSL) 700 FT/min
SERVICE CEILING 14,500 FT
TAKEOFF PERFORMANCE
Ground Roll 820 ft
Total Distance over 50 ft obstacle 1411 ft
LANDING PERFORMANCE
Ground Roll 689 ft
Total Distance over 50 ft obstacle 1640 ft
MAXIMUM WEIGHT
Takeoff or landing 750 kg. / 1653 lb
STANDARD EMPTY WEIGHT
AT01-100C ab 500 kg. / 1102 lb
MAXIMUM USEFUL LOAD
AT01-100C 250 kg. / 551 lb
BAGGAGE ALLOWANCE 40 kg. / 88,2 lb
SEATS 2
FUEL CAPACITY
Standard Tanks 120lt
Fuelgrade (EN228 SUPER / Super Plus, AVGAS 100LL, AVGAS UL91)
OIL CAPACITY 3 lt
ENGINE: Bombardier Rotax 912 S3 100PS
PROPELLER: MT-Propeller MTV-21-A / 170-05 66,9 in
DIMENSIONS
Lenght 24,28 ft / 7,40 mt
Lenght 7,87 ft / 2,40 mt
Wingspan 33,79 ft / 10,30 mt
Wing area 113.00 ft2 / 10.50 m2
Cabin width 3,97 ft / 1,20 mt
Baggage Compartment Capacity 17.70 ft3 / 500 lt


Cessna 172R Spec



Speed *
Maximum at Sea Level 123 knots
Cruise, 80% Power at 8,000 ft 122 knots
CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve.
80% Power at 8,000 ft (Range) 580 NM
53 Gallons usable fuel (Time) 4.8 hours
Range at 10,000 FT, 60% power (Range) 687 NM
RATE OF CLIMB AT SEA LEVEL 720 FPM
SERVICE CEILING 13,500 FT
TAKEOFF PERFORMANCE
Ground Roll 945 ft
Total Distance over 50 ft obstacle 1685 ft
LANDING PERFORMANCE
Ground Roll 550 ft
Total Distance over 50 ft obstacle 1295 ft
STALL SPEED
Flaps up, power off 51 kcas
Flaps down, power off 47 kcas
MAXIMUM WEIGHT
Ramp 2457 lbs
Takeoff 2450 lbs
Landing 2450 lbsas
STANDARD EMPTY WEIGHT 1639 lbs
MAXIMUM USEFUL LOAD 818 lbs
BAGGAGE ALLOWANCE 120 lbs
WING LOADING: Lbs/Sq Ft 14.1
POWER LOADING: Lbs/HP 15.3
FUEL CAPACITY 56 gal
OIL CAPACITY 8 qts
ENGINE: Textron Lycoming (160 BHP at 2400 RPM) IO-360-L2A
PROPELLER: Fixed Pitch, Diameter 75 in


Cessna 152 Spec


Speed *
Maximum at Sea Level 110 knots
Cruise, 75% Power at 8,000 ft 107 knots
CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve at 45% power
75% Power at 8,000 ft (Range) 350 NM
24.5 Gallons usable fuel (Time) 3.4 hours
75% Power at 8,000 ft (Range) 580 NM
37.5 Gallons usable fuel (Time) 5.5 hours
Maximum Range at 10,000 ft (Range) 415 NM
24.5 Gallons usable fuel (Time) 5.2 hours
Maximum Range at 10,000 ft (Range) 690 NM
37.5 Gallons usable fuel (Time) 8.7 Hours
RATE OF CLIMB AT SEA LEVEL 715 FPM
SERVICE CEILING 14,700 FT
TAKEOFF PERFORMANCE
Ground Roll 725 ft
Total Distance over 50 ft obstacle 1340 ft
LANDING PERFORMANCE
Ground Roll 475 ft
Total Distance over 51 ft obstacle 1200 ft
STALL SPEED (CAS)
Flaps up, power off 48 knots
Flaps down, power off 43 knots
STANDARD EMPTY WEIGHT
152 1101 lb
152 II 1 1133 lbs
MAXIMUM USEFUL LOAD
152 574 lbs
152 II 1 54 lbs2
BAGGAGE ALLOWANCE 120 lbs
WING LOADING (Pounds / s.f.) 10.5
POWER LOADING (Pounds / HP) 15.2
FUEL CAPACITY
Standard Tanks 26 GAL
Long Range Tanks 39 GAL
OIL CAPACITY 6 qts
ENGINE: Avco Lycoming 110 bhp at 255o rpm O235-L2C
PROPELLER: Fixed Pitch, diameter 69 in