Cessna 152 (Location: California)
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Crew: one pilot
Capacity: one passenger Length: 24 ft 1 in (7.3 m Wingspan: 33 ft 4 in (10.2 m) Height: 8 ft 6 in (2.6 m) Wing area: 160 ft² (14.9 m²) Empty weight: 1,081 lb (490 kg) Max. takeoff weight: 1,670 lb (757 kg) Powerplant: 1 × Lycoming O-235-L2C flat-4 engine, 110 hp (82 kW) driving a 69-inch (175 cm), two-blade, fixed-pitch McCauley propeller or a 72-inch, two-blade, fixed-pitch Sensenich propeller |
Maximum speed: 126 mph (110 knots, 204 km/h)
Cruise speed: 123 mph (107 knots, 198 km/h) Stall speed: 49 mph (43 knots, 79 km/h) unpowered, flaps down Takeoff roll: 725 ft (221 m) Range: 477 mi (414 nm, 768 km) Extended range 795 mi (690 nm, 1,280 km) with long-range tanks Service ceiling: 14,700 ft (4,480 m) Rate of climb: 715 ft/min (3.6 m/s) Max. wing loading: 10.44 lb/ft² (51 kg/m²) Minimum power/mass: .066 hp/lb (108 W/kg) |
Cessna 172 (Location: California and Texas)
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Crew: one
Capacity: three passengers Length: 27 ft 2 in (8.28 m) Wingspan: 36 ft 1 in (11.00 m) Height: 8 ft 11 in (2.72 m) Wing area: 174 sq ft (16.2 m2) Aspect ratio: 7.32 Airfoil: modified NACA 2412 Empty weight: 1,691 lb (767 kg) Gross weight: 2,450 lb (1,111 kg) Fuel capacity: 56 US gallons (212 litres) Powerplant: 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp (120 kW) Propellers: 2-bladed metal, fixed pitch |
Cruise speed: 122 kn (140 mph; 226 km/h)
Stall speed: 47 kn (54 mph; 87 km/h) (power off, flaps down)[87] Never exceed speed: 163 kn (188 mph; 302 km/h) (IAS)[12] Range: 696 nmi (801 mi; 1,289 km) with 45 minute reserve, 55% power, at 12,000 ft Service ceiling: 13,500 ft (4,100 m) Rate of climb: 721 ft/min (3.66 m/s) Wing loading: 14.1 lb/sq ft (68.6 kg/m2) |
Cessna 172SP (Location: California)
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Crew: one
Capacity: three passengers Length: 27 ft 2 in (8.28 m) Wingspan: 36 ft 1 in (11.00 m) Height: 8 ft 11 in (2.72 m) Wing area: 174 sq ft (16.2 m2) Aspect ratio: 7.32 Airfoil: modified NACA 2412 Empty weight: 1,691 lb (767 kg) Gross weight: 2,450 lb (1,111 kg) Fuel capacity: 56 US gallons (212 litres) Powerplant: 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 180 hp (134 kW) Propellers: 2-bladed metal, fixed pitch |
Cruise speed: 122 kn (140 mph; 226 km/h)
Stall speed: 47 kn (54 mph; 87 km/h) (power off, flaps down)[87] Never exceed speed: 163 kn (188 mph; 302 km/h) (IAS)[12] Range: 696 nmi (801 mi; 1,289 km) with 45 minute reserve, 55% power, at 12,000 ft Service ceiling: 13,500 ft (4,100 m) Rate of climb: 721 ft/min (3.66 m/s) Wing loading: 14.1 lb/sq ft (68.6 kg/m2) |
Diamond DA40 (Location: California)
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Length
26 ft 5 in Height 6 ft 6 in Wingspan 39 ft 6 in Maximum takeoff weight 2,645 lbs Useful load 860 lbs (standard equipped airplane) Fuel capacity, usable 50 gal Engine Lycoming IO-360-M1A Horsepower 180 hp Propeller Hartzell 2-blade scimitar structural composite propeller |
Rate of climb
1,120 ft/min Maximum operating altitude 16,400 ft Maximum speed 157 ktas Cruise speed at 75% 150 ktas/10 gal/hr Range, at 75% 45 minute reserve 720 nm Maximum demonstrated crosswind 20 kts |
Diamond DA42 (Location: California and Texas)
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Length
28 ft 1 in Height 8 ft 2 in Wingspan 44 ft Maximum takeoff weight 4,407 lbs Useful load 1,301 lbs Fuel capacity, usable (w/ Aux tanks) 72 US gal (Jet A) Engine Austro AE 300 2.0 liter diesel with 168 hp Horsepower 270 hp total Propeller MT 3-blade composite constant speed, full-feathering |
Rate of climb
1,550 ft/min Maximum operating altitude 18,000 ft Maximum SE ceiling 18,000 ft Maximum cruise speed 197 kts Cruise speed at 75% 175 kts/13.2 gal/hr total Range, at 80% (w/ Aux tanks) 900 nm Economy at 60% 157 ktas/10.3 gal/hr total Range at 60% 1,215 nm Maximum landing gear operating speed 194 kts Maximum demonstrated crosswind 25 kts |
