<![CDATA[Foster Aero International Aircraft Sales]]> <![CDATA[Foster Aero International Aircraft Sales]]> <![CDATA[Piper PA28-180 - R520,000]]>  

 

The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

 

  • Crew/Pax: 1+3 
  • Cruise speed: 108 knots (124 mph)
  • Wingspan: 30.0 feet (9.2 m)
 
  • Empty weight: 1201 lb (544 kg)
  • Useful load: 949 lb (430 kg)
  • Max takeoff weight: 2150 lb (975 kg)
 

 

]]> <![CDATA[Cessna 182Q - R1,200,000]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

  • Crew/Pax: 1+3
  • Cruise Speed: 132 Kts
  • Wingspan: 36 ft 0 in (11.0 m)
  • Useful load: 1,140 lb (517 kg)
  • Max takeoff weight: 3,100 lb (1406 kg)
  • Empty weight: 1,970 lb (894 kg)
]]> <![CDATA[Cessna 182S - R1,830,000 ]]> <![CDATA[Cessna 172R - R980,000]]> The Cessna 172 Skyhawk is a four-seat, single-engine, high-wing fixed-wing aircraft. First flown in 1955 and still in production, more Cessna 172s have been built than any other aircraft.

 

  • Never exceed speed: 163 knots (187 mph, 302 km/h)
  • Maximum speed: 123 knots (141 mph, 228 km/h) at sea level
  • Cruise speed: 122 knots (140mph, 226 km/h)
  • Range: 610 nm (790 mi, 1,272 km) at 55% power at 12,000 ft (3,040 m)
  • Service ceiling: 13,500 ft (4,116 m)
  • Rate of climb: 720 ft/min (3.7 m/s)
 
]]> <![CDATA[Yak 52 - R450,000]]> <![CDATA[Cessna 182RG - R1,296,000]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

  • Crew/Pax:1+3
  • Crusise Speed:132 Kts              
  • Wingspan: 36 ft (11.0m)
  • Useful load: 1,140 lb (517 kg)
  • Empty weight: 1,970 lb (894 kg)
  • Max takeoff weight: 3,100 lb (1406 kg)
]]> <![CDATA[Piper PA28-180 - R360,000]]>  

 

The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

 

  • Crew/Pax: 1+3 
  • Cruise speed: 108 knots (124 mph)
  • Wingspan: 30.0 feet (9.2 m)
 
  • Empty weight: 1201 lb (544 kg)
  • Useful load: 949 lb (430 kg)
  • Max takeoff weight: 2150 lb (975 kg)
 

 

]]> <![CDATA[Samba - R626,000]]> <![CDATA[Piper PA28-235 - R594,000]]> The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

 

  • Crew/Pax: 1+3 
  • Cruise speed: 126knots (145mph)
  • Wingspan: 30.0 feet (9.2 m)
 
  • Empty weight: 1592 lb (722 kg)
  • Useful load: 1408 lb (639 kg)
  • Max takeoff weight: 3000 lb (1361 kg)
 
]]> <![CDATA[De Havilland DH-82A Tiger Moth - R665,000]]> <![CDATA[Luscombe Silvaire - R395,000]]> The Luscombe 8 is a series of high wing monoplanes designed in the late 1930s.The Luscombe 50 (Model 8) was to become the company's most famous product. Further design changes to simplify construction of the model 8 vertical stabilizer and horizontal stabilizer construction were implemented in 1947. These changes were alleged to save several hundred man hours in the construction of the airplanes.

  • Useful Load: 535 pounds
  • Max Speed: 125 mph (201 km/h)
  
  • Cruise Speed: 110 mph (180 km/h)
  • Range: 370 miles (600 km)
]]> <![CDATA[Cessna 172N - R705,000]]>  Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production.

  • Crew/Pax: 1 + 3
  • Wingspan: 36 ft 1 in (11.0 m)
  • Empty weight: 1,620 lb (736 kg)
 
  • Useful load: 830 lb (376 kg)
  • Max takeoff weight: 2,450 lb (1,113 kg)
  • Cruise speed: 122 knots (140mph, 226 km/h)
 

 

]]> <![CDATA[Cessna 206 - R2,160,000]]>  This aircrafts combination of a powerful engine, rugged construction and a large cabin has made these aircraft popular bush planes. Cessna describes the 206 as "the sport-utility vehicle of the air." These airplanes are also used for aerial photography, skydiving and other utility purposes.
  • Crew/Pax: 1+5
  • Cruise Speed: 135 Kts
  • Wingspan: 35 ft 10 in (10.92 m)
  • Empty weight: 2,146 lb (974 kg)
  • Useful load: 1,373 lb (623 kg)
  • Max takeoff weight: 3,600 lb (1,633 kg)
]]> <![CDATA[Piper PA28-180 - R650,000]]>  

 

The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

 

  • Crew/Pax: 1+3 
  • Cruise speed: 108 knots (124 mph)
  • Wingspan: 30.0 feet (9.2 m)
 
  • Empty weight: 1201 lb (544 kg)
  • Useful load: 949 lb (430 kg)
  • Max takeoff weight: 2150 lb (975 kg)
 

 

]]> <![CDATA[Cessna 182RG - R1,080,000 Excl VAT]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

  • Crew/Pax:1+3
  • Crusise Speed:132 Kts              
  • Wingspan: 36 ft (11.0m)
  • Useful load: 1,140 lb (517 kg)
  • Empty weight: 1,970 lb (894 kg)
  • Max takeoff weight: 3,100 lb (1406 kg)
]]> <![CDATA[Piper PA18-150 Super Cub - R702,000]]> The Piper PA-18 -Super Cub- is a two-seater, single-engine airplane and a tail dragger. It is today an aviation enthusiast collectors item. Super Cubs are commonly found in roles such as bush flying, banner and glider towing, and other situations in which short field performance is required. It is considered to be one of the most sought after bush planes in the world.

  • Crew/Pax: 1+1
  • Cruise speed: 100 kts (112 mph, 180 km/h)
  • Wingspan: 35 ft 3 in (10.74 m)
 
  • Empty weight: 983 lb (446 kg)
  • Useful load: N/A
  • Max tafeoff weight: N/A
 
]]> <![CDATA[Cessna 182 - R490,000]]> The Cessna 182, marketed under the name Skylane, is a four-seat, single-engine, light airplane. It has the option of adding two child seats, installed in the baggage area.

Introduced in 1956, the 182 has been produced in a number of variants, including a version with retractable landing gear, and is the second most popular Cessna model, after the 172.

 

]]> <![CDATA[Cessna 172N - R705,000]]>  Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production.

  • Crew/Pax: 1 + 3
  • Wingspan: 36 ft 1 in (11.0 m)
  • Empty weight: 1,620 lb (736 kg)
 
  • Useful load: 830 lb (376 kg)
  • Max takeoff weight: 2,450 lb (1,113 kg)
  • Cruise speed: 122 knots (140mph, 226 km/h)
 

 

]]> <![CDATA[Cessna 172L - R540,000]]> The 172L, sold during 1971 and 1972, replaced the main landing gear legs (which were originally flat spring steel) with tapered, tubular steel gear legs. The new gear had a width that was increased by 12 in (30 cm).[10] The new tubular gear was lighter, but required aerodynamic fairings to maintain the same speed and climb performance as experienced with the flat steel design. The "L" also had a plastic fairing between the dorsal fin and vertical fin to introduce a greater family resemblance to the 182's vertical fin.

]]> <![CDATA[Cessna 182S - R2,160,000 ]]> <![CDATA[Piper PA28-180 - R540,000]]>  

 

The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

 

  • Crew/Pax: 1+3 
  • Cruise speed: 108 knots (124 mph)
  • Wingspan: 30.0 feet (9.2 m)
 
  • Empty weight: 1201 lb (544 kg)
  • Useful load: 949 lb (430 kg)
  • Max takeoff weight: 2150 lb (975 kg)
 

 

]]> <![CDATA[Magic GS 700 - R411,000]]>
  • SOLD AS A KIT,NO ENGINE OR PROP
  • Length: 6.85 m (22 ft 6 in)
  • Wingspan: 8.55 m (28 ft 1 in)
  • Height: 2.18 m (7 ft 2 in)
  • Wing area: 11.34 m2 (122.1 sq ft)
  • Aspect ratio: 6.4
  • Empty weight: 320 kg (705 lb)
  • Gross weight: 600 kg (1,323 lb)
  • Fuel capacity: 75 litres (16 imp gal; 20 US gal)
  • Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 75 kW (101 hp)
  • Propellers: 3-bladed Ivoprop

    • Performance

    • Maximum speed: 193 km/h (120 mph; 104 kn)
    • Cruising speed: 185 km/h (115 mph; 100 kn)
    • Stall speed: 56 km/h (35 mph; 30 kn) flaps down
    • Never exceed speed: 209 km/h (130 mph; 113 kn)
    • Service ceiling: 3,600 m (11,811 ft)
    • g limits: +4/-2
    • Rate of climb: 5 m/s (980 ft/min)
    ]]>         <![CDATA[Piper PA28-180 - R325, 000 EXCL VAT]]>  

     

    The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

     

    • Crew/Pax: 1+3 
    • Cruise speed: 108 knots (124 mph)
    • Wingspan: 30.0 feet (9.2 m)
     
    • Empty weight: 1201 lb (544 kg)
    • Useful load: 949 lb (430 kg)
    • Max takeoff weight: 2150 lb (975 kg)
     

     

    ]]>         <![CDATA[Cessna T206H - Offers]]>  

    Cessna 206H

    After a production hiatus of twelve years, Cessna started manufacturing a new version of the venerable 206 in 1998, with the introduction of the newly certified 206H.The “H” model is generally similar to the previous U206 configuration, with a pilot entry door and a rear double clamshell door for access to the middle and back seats. The "H" is marketed under the name "Stationair".

    The 206H is powered by a Lycoming IO-540-AC1A powerplant producing 300 hp (220 kW). The turbocharged T206H is powered by a Lycoming TSIO-540-AJ1A engine of 310 hp (230 kW).

    • Empty weight: 2,146 lb (974 kg)
    • Useful load: 1,373 lb (623 kg)
    • Maximum speed: 151 kt (285 km/h)
    		  Rate of climb:988 ft/min (301 m/min)
    • Cruise speed: 142 kt (263 km/h)
    • Range: 721 nm (1,335 km)

     

     

    ]]>         <![CDATA[Piper PA32RT-300T - R950,000 Excl VAT]]>  

    PA-32R-300 (1976-1978) - called the Piper Cherokee Lance. Initial version of the retractable PA-32 line, with a standard tail in the 1976 model. The 1977 and 1978 models featured a tail modified to a "T" design with the stabilator (horizontal stabilizer/elevator) moved to the top of the vertical tail.

     
    • Maximum speed: 165 kts(306km/h)
    • Cruise speed: 140 kts (258 km/h)
    • Range: 1000 miles (1600 km)
    		  
    • Service ceiling: 14600 ft (4450 m)
    • Rate of climb: 1050 ft/min (5.3 m/s)
    ]]>         <![CDATA[Jabiru J430 - R680,000]]> <![CDATA[Cessna 205 - R530,000]]> The Cessna 205 was introduced late in 1962 as a 1963 model year. The six-seat aircraft was essentially a Cessna 210 with fixed landing gear and with changes to the crew and passenger door arrangement and was officially designated by Cessna as a "Model 210-5.The 205 retained the early 210’s engine cowling bulge, originally where the 210 stowed its nosewheel on retraction. This distinctive cowling was made more streamlined on the later Cessna 206.

    The 205 is powered by a continental IO-470-s engine producing 260 hp (190 kW).

    The 205 was only produced in two model years - 1963 and 1964 before being replaced in production by the Cessna 206. A total of 576 Cessna 205s were produced.

    ]]>         <![CDATA[Jabiru J430 - R675,000]]> <![CDATA[Jabiru J430 - R450,000]]> <![CDATA[Cessna 210 N - R1,620,000 Excl VAT]]>  The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)

     

    ]]>         <![CDATA[Piper PA28-235 - R750,000 Excl VAT]]> The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

     

    • Crew/Pax: 1+3 
    • Cruise speed: 126knots (145mph)
    • Wingspan: 30.0 feet (9.2 m)
     
    • Empty weight: 1592 lb (722 kg)
    • Useful load: 1408 lb (639 kg)
    • Max takeoff weight: 3000 lb (1361 kg)
     
    ]]>         <![CDATA[Jabiru J430 - R535,000]]> <![CDATA[Cessna 182P - R755,000]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

    • Crew/Pax:1+3  
    • Crusise Speed:132 Kts              
    • Wingspan: 36 ft (11.0m)
    • Useful load: 1,140 lb (517 kg)
    • Empty weight: 1,970 lb (894 kg)
    • Max takeoff weight: 3,100 lb (1406 kg)
    ]]>         <![CDATA[Jabiru SP Shadow Lite - R325,000]]> The longer tail boom results in more elevator and empennage authority,reducing the stall speed to 39 kts and increasing directional stability. The SP was developed for export markets such as Canada, South Africa and Chile where a 39 knot stall speed was required for ultralight or microlight operations. The aircraft are already flying in South Africa, Swaziland, Botswana, Zimbabwe and Chile.
    The Jabiru SP cruises at 120 mph and 3.5 gallons per hour with the 2200A (80hp engine), and 135 mph , 5 gallons per hour with the 3300A (120hp engine), depending on the options selected. Jabiru have increased the Maximum Take Off Weight (MTOW) for all their kitplane models from 946lb to 1034lb. All of the Jabiru kitplane models have been structurally tested to 8.5g. The aircraft incorporates a new low profile 18.5 gallon fuel tank which increases the available storage space for baggage on top of the fuel tank. For the 3300 powered SP, a 23 gallon tank is available as an option.

    ]]>         <![CDATA[Jabiru J450 - R510,000]]> <![CDATA[Mooney M20E - R410,000]]>
    The first truly high performance Mooney, the M20E, was produced from 1964 to 1975 and marketed as the Chaparral and Super 21.
    The M20E was essentially an M20C with a more powerful 200 hp (150 kW) fuel-injected engine.It was type certified on 04 September 1963 with the 180 hp (130 kW) Lycoming 0-360-A1A  engine.
    This short body Mooney still has the distinction of having the shortest takeoff runway requirement at lower elevations.
    Turbocharging, which would maintain this performance at higher elevations, is available as an after-market option.
    ]]>         <![CDATA[Beechcraft Bonanza B36TC - R1,990,000]]> <![CDATA[Cessna 182P - R970,000]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

    • Crew/Pax:1+3  
    • Crusise Speed:132 Kts              
    • Wingspan: 36 ft (11.0m)
    • Useful load: 1,140 lb (517 kg)
    • Empty weight: 1,970 lb (894 kg)
    • Max takeoff weight: 3,100 lb (1406 kg)
    ]]>         <![CDATA[Cessna 152 - R350,000 ]]>  The Cessna 152 is an American two-seat, fixed tricycle gear, general aviation airplane, used primarily for flight training and personal use. The 152 was a modernization of the proven Cessna 150 design.

    • Cruise speed: 123 mph (107 knots, 198 km/h)
    • Stall speed: 49 mph (43 knots, 79 km/h) unpowered, flaps down
    • Range: 477 mi (414 nm, 768 km)
    • Service ceiling: 14,700 ft (4,480 m)
    • Takeoff roll: 725 ft (221 m)
    • Rate of climb: 715 ft/min (3.6 m/s)
     
    ]]>         <![CDATA[Cessna 175 - R485,000]]> <![CDATA[Cessna 206 - R1,000,000 EXCL VAT OFFERS]]>  This aircrafts combination of a powerful engine, rugged construction and a large cabin has made these aircraft popular bush planes. Cessna describes the 206 as "the sport-utility vehicle of the air." These airplanes are also used for aerial photography, skydiving and other utility purposes.
    • Crew/Pax: 1+5
    • Cruise Speed: 135 Kts
    • Wingspan: 35 ft 10 in (10.92 m)
    • Empty weight: 2,146 lb (974 kg)
    • Useful load: 1,373 lb (623 kg)
    • Max takeoff weight: 3,600 lb (1,633 kg)
    ]]>         <![CDATA[Cessna 172R - Blue Book (Offers)]]> The Cessna 172 Skyhawk is a four-seat, single-engine, high-wing fixed-wing aircraft. First flown in 1955 and still in production, more Cessna 172s have been built than any other aircraft.

     

    • Never exceed speed: 163 knots (187 mph, 302 km/h)
    • Maximum speed: 123 knots (141 mph, 228 km/h) at sea level
    • Cruise speed: 122 knots (140mph, 226 km/h)
    • Range: 610 nm (790 mi, 1,272 km) at 55% power at 12,000 ft (3,040 m)
    • Service ceiling: 13,500 ft (4,116 m)
    • Rate of climb: 720 ft/min (3.7 m/s)
     
    ]]>         <![CDATA[Cessna T210L - R1,070,000]]> The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1985.

     

    ]]>         <![CDATA[Jabiru J450 - R455,000]]> <![CDATA[Jabiru J160 - R360,000]]> <![CDATA[Jabiru J430 - R645,000]]> <![CDATA[Cessna 172M - R700,000]]>  Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production.

    • Crew/Pax: 1 + 3
    • Wingspan: 36 ft 1 in (11.0 m)
    • Empty weight: 1,620 lb (736 kg)
     
    • Useful load: 830 lb (376 kg)
    • Max takeoff weight: 2,450 lb (1,113 kg)
    • Cruise speed: 122 knots (140mph, 226 km/h)
     

     

     

    ]]>         <![CDATA[Cessna T210M - R1,240,000]]> <![CDATA[Piper PA32 Cherokee 6 - R890,000]]>  The

     
    • Maximum speed: 151 kts (280 km/h)     
    • Service ceiling: 16250 ft (4950 m)
    • Rate of climb: 1050 ft/min (5.3 m/s)
    • Cruise speed: 146 kts mph (272 km/h)
    • Range: 840 miles (1361 km)

    Piper PA-32 Cherokee Sixis a series of six or seven seat, fixed or retractable landing gear, ,manufactured in the United States by Piper Aircraft. The best example of this popular aircraft is is PA-32-300:

     

    ]]>         <![CDATA[Grumman American AA-5A - R490,000,00]]> <![CDATA[Grumman Traveler AA5 - R645,000]]> <![CDATA[Cessna 170B - R520,000]]> <![CDATA[Cessna 172RG - R810,000 ]]> <![CDATA[Piper PA32 Cherokee 6 - R918,000,00]]>  The

     
    • Maximum speed: 151 kts (280 km/h)     
    • Service ceiling: 16250 ft (4950 m)
    • Rate of climb: 1050 ft/min (5.3 m/s)
    • Cruise speed: 146 kts mph (272 km/h)
    • Range: 840 miles (1361 km)

    Piper PA-32 Cherokee Sixis a series of six or seven seat, fixed or retractable landing gear, ,manufactured in the United States by Piper Aircraft. The best example of this popular aircraft is is PA-32-300:

     

    ]]>         <![CDATA[Beechcraft Bonanza H35 - R 645,000]]> <![CDATA[Cessna 172RG - R500,000]]> <![CDATA[Pitts S2B - R450,000]]> The Pitts Special is a light aerobatic biplane designed by Curtis Pitts. It has accumulated many competition wins since its first flight in 1944. The Pitts Special dominated world aerobatic competition in the 1960s and 1970s and, even today, remains a potent competition aircraft in the lower categories.

    • Crew/Pax: 1/2 + 1
    • Cruise speed: 152 knots (175 mph, 282 km/h) (max cruise)
    • Wingspan: 20 ft 0 in (6.10 m)
     
    • Empty weight: 1,150 lb (521 kg)
    • Useful Load: N/A
    • Max takeoff weight: 1,625 lb (737 kg)
     

     

    ]]>         <![CDATA[Mooney M20C - R377 000]]> <![CDATA[Cessna 172 - R460,000]]> Production of the C-172 started in 1956 with the first delivered Cessna 172 from the Cessna factory. Newer and later generation pilots have made the design a resounding market success and possible the most sucessful training aircraft ever. According to Cessna, they have built some 43,000 C-172s since 1956. The first C-172 used a Continental O-300A six cylinder air-cooled flat opposed 145 horsepower engine.The first C-172 had a 'straight' tail like the C-170. In 1960 Cessna  introduced the swept-tail model 172A.

    ]]>         <![CDATA[Piper PA28-140 Cherokee - R405,000]]> The Piper PA-28 Cherokee is a family of light aircraft designed for flight training, air taxi and personal use, built by Piper Aircraft.

     

    In 1964, the company filled in the bottom end of the line with the Cherokee 140 (PA-28-140), which was designed for training and initially shipped with only two seats. One source of confusion is the fact that the PA-28-140 engine was slightly modified shortly after its introduction to produce 150 horsepower (112 kW), but kept the -140 name

     

     

    • Maximum speed: 123 knots (142 mph, 230 km/h)
    • Cruise speed: 108 knots (124 mph (200 km/h), 201 km/h)
    • Stall speed: 47 knots (54 mph, 87 km/h)
    		  
    • Range: 465 nm (535 sm, 867 km)
    • Service ceiling: 14,300 feet (4400 m)
    • Rate of climb: 660 ft/min (3.4 m/s)

     

     

    ]]>         <![CDATA[Cessna 182F - R645,000]]> <![CDATA[Jabiru J400 - R465,000]]> <![CDATA[Piper PA28-235 - R660,000]]> The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

     

    • Crew/Pax: 1+3 
    • Cruise speed: 126knots (145mph)
    • Wingspan: 30.0 feet (9.2 m)
     
    • Empty weight: 1592 lb (722 kg)
    • Useful load: 1408 lb (639 kg)
    • Max takeoff weight: 3000 lb (1361 kg)
     
    ]]>         <![CDATA[Cessna 182P - R810,000 ]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

    • Crew/Pax:1+3  
    • Crusise Speed:132 Kts              
    • Wingspan: 36 ft (11.0m)
    • Useful load: 1,140 lb (517 kg)
    • Empty weight: 1,970 lb (894 kg)
    • Max takeoff weight: 3,100 lb (1406 kg)
    ]]>         <![CDATA[Mooney M20J - Offers]]> The Mooney M20J was originally designed as a private/commercial touring aircraft because of the high cruising speed and relatively low operational cost.

     

    • Crew/Pax: 1 + 3
    • Cruise Speed: 171 kts
    • Wingspan: 35 ft
    • Useful Load: 1004 lbs
    • Empty Weight: 1 710 lbs
    • Max Takeoff Weight: 3374lbs
    ]]>         <![CDATA[Beechcraft Bonanza A36 - R1,415,000]]>  The Beechcraft Bonanza is an American general aviation aircraft introduced in 1947 by The Beech Aircraft Corporation of Wichita, Kansas. As of 2009 it is still being produced by Hawker Beechcraft and has been in continuous production longer than any other airplane in history. More than 17,000 Bonanzas of all variants have been built.

    F33A Bonanza(1970-1994) F33 with a 285hp Continental IO-520-B engine, later aircraft have a longer S35/V35 cabin and extra seats, 821 built

     

    • Maximum speed: 191 mph (166 kn, 306 km/h)
    • Stall speed: 63 mph (55 kn, 101 km/h)
    • Range: 779 mi (677 NM, 1,247 km)
    • Rate of climb: 1,100 ft/min (5.6 m/s)
     
    ]]>         <![CDATA[Piper PA22-108 Colt - R210,000 Neg]]> <![CDATA[Samba XL - R667 000]]> <![CDATA[SIAI Marchetti - 280,000]]> <![CDATA[De Havilland DH-82A Tiger Moth - R490,000]]> <![CDATA[Beechcraft G36 - R4,670,000]]> Single–engine pilots prize the high–performance control and field–tested reliability of the Beechcraft Bonanza G36. Fast, roomy and comfortable, the Bonanza G36 is the aspiration of any pilot who desires unmatched craftsmanship. This piston–engine powerhouse can carry four passengers 750 miles and has a maximum cruise speed of over 200 miles per hour.

    With a cabin almost a third larger than its nearest competitor and advanced Garmin G1000® avionics, the Bonanza G36 is a superior value for your money. And because it is designed and built strong enough to be certified in the rugged utility category, your Bonanza G36 is ready for any adventure with first–class technology and comfort and world–class Beechcraft quality.

    ]]>         <![CDATA[Jabiru J430 - R550,000]]> <![CDATA[Jabiru J400 - R465,000]]> <![CDATA[Jabiru J430 - R655,000]]> <![CDATA[Cessna 182S - R1,775,000]]> <![CDATA[Van's Aircraft RV-12 - R755,000]]> <![CDATA[Cessna 182RG - R965,000]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

    • Crew/Pax:1+3
    • Crusise Speed:132 Kts              
    • Wingspan: 36 ft (11.0m)
    • Useful load: 1,140 lb (517 kg)
    • Empty weight: 1,970 lb (894 kg)
    • Max takeoff weight: 3,100 lb (1406 kg)
    ]]>         <![CDATA[De Havilland DH-82A Tiger Moth - R635,000]]> <![CDATA[Piper PA-28R-201 Arrow III - R565,000]]> <![CDATA[Beechcraft Bonanza A36TC - Offers]]> The Beechcraft Bonanza is an American general avaition aircraft introduced in 1947 by the beech aircraft corporation  of wichita, kansas. As of 2010, it is still being produced by hawker beech beechcraft , and has been in continuous production longer than any other airplane in history. More than 17,000 Bonanzas of all variants have been built.

    ]]>         <![CDATA[Socata Rallye 235E - R700,000]]> <![CDATA[Beechcraft Bonanza A36 - R1,560,000]]>  The Beechcraft Bonanza is an American general aviation aircraft introduced in 1947 by The Beech Aircraft Corporation of Wichita, Kansas. As of 2009 it is still being produced by Hawker Beechcraft and has been in continuous production longer than any other airplane in history. More than 17,000 Bonanzas of all variants have been built.

    F33A Bonanza(1970-1994) F33 with a 285hp Continental IO-520-B engine, later aircraft have a longer S35/V35 cabin and extra seats, 821 built

     

    • Maximum speed: 191 mph (166 kn, 306 km/h)
    • Stall speed: 63 mph (55 kn, 101 km/h)
    • Range: 779 mi (677 NM, 1,247 km)
    • Rate of climb: 1,100 ft/min (5.6 m/s)
     
    ]]>         <![CDATA[Beechcraft Debonair 35-B33 - R850,000]]> <![CDATA[Cessna 150L - Offers]]> <![CDATA[Jabiru J160 - R320,000]]> <![CDATA[Piper PA18-150 Super Cub - R650,000]]> The Piper PA-18 -Super Cub- is a two-seater, single-engine airplane and a tail dragger. It is today an aviation enthusiast collectors item. Super Cubs are commonly found in roles such as bush flying, banner and glider towing, and other situations in which short field performance is required. It is considered to be one of the most sought after bush planes in the world.

    • Crew/Pax: 1+1
    • Cruise speed: 100 kts (112 mph, 180 km/h)
    • Wingspan: 35 ft 3 in (10.74 m)
     
    • Empty weight: 983 lb (446 kg)
    • Useful load: N/A
    • Max tafeoff weight: N/A
     
    ]]>         <![CDATA[Cessna T210L - R850,000]]> The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1985.

     

    ]]>         <![CDATA[Cessna 182E - R750,000]]> <![CDATA[Van's Aircraft RV-6 - R765,000]]> <![CDATA[Cessna 177B Cardinal - R465,000]]> <![CDATA[Cessna 172H - R 450,000]]>  Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production.

    ]]>         <![CDATA[Cessna 172 - R405.000]]> Production of the C-172 started in 1956 with the first delivered Cessna 172 from the Cessna factory. Newer and later generation pilots have made the design a resounding market success and possible the most sucessful training aircraft ever. According to Cessna, they have built some 43,000 C-172s since 1956. The first C-172 used a Continental O-300A six cylinder air-cooled flat opposed 145 horsepower engine.The first C-172 had a 'straight' tail like the C-170. In 1960 Cessna  introduced the swept-tail model 172A.

    ]]>         <![CDATA[Piper PA28R-180 Cherokee Arrow - R430,000]]> <![CDATA[Piper PA32 Cherokee 6 - R975,000 ]]>  The

     
    • Maximum speed: 151 kts (280 km/h)     
    • Service ceiling: 16250 ft (4950 m)
    • Rate of climb: 1050 ft/min (5.3 m/s)
    • Cruise speed: 146 kts mph (272 km/h)
    • Range: 840 miles (1361 km)

    Piper PA-32 Cherokee Sixis a series of six or seven seat, fixed or retractable landing gear, ,manufactured in the United States by Piper Aircraft. The best example of this popular aircraft is is PA-32-300:

     

    ]]>         <![CDATA[Piper PA28-140 Cherokee - R 350,000]]> The Piper PA-28 Cherokee is a family of light aircraft designed for flight training, air taxi and personal use, built by Piper Aircraft.

     

    In 1964, the company filled in the bottom end of the line with the Cherokee 140 (PA-28-140), which was designed for training and initially shipped with only two seats. One source of confusion is the fact that the PA-28-140 engine was slightly modified shortly after its introduction to produce 150 horsepower (112 kW), but kept the -140 name

     

     

    • Maximum speed: 123 knots (142 mph, 230 km/h)
    • Cruise speed: 108 knots (124 mph (200 km/h), 201 km/h)
    • Stall speed: 47 knots (54 mph, 87 km/h)
    		  
    • Range: 465 nm (535 sm, 867 km)
    • Service ceiling: 14,300 feet (4400 m)
    • Rate of climb: 660 ft/min (3.4 m/s)

     

     

    ]]>         <![CDATA[Piper PA28RT-201 Arrow IV - R860,000 Neg]]> Four place, retractable landing gear landplane, Lycoming IO-360-C1C6 engine of 200 hp (149 kW), gross weight 2,750 lb (1,247 kg). First certified on 13 November 1978. Features a T tail.

    ]]>         <![CDATA[Jabiru J400 - R380,000]]> <![CDATA[Beechcraft V35B Bonanza - R970,000]]> <![CDATA[Cessna 206 - R1,185,000]]>  This aircrafts combination of a powerful engine, rugged construction and a large cabin has made these aircraft popular bush planes. Cessna describes the 206 as "the sport-utility vehicle of the air." These airplanes are also used for aerial photography, skydiving and other utility purposes.
    • Crew/Pax: 1+5
    • Cruise Speed: 135 Kts
    • Wingspan: 35 ft 10 in (10.92 m)
    • Empty weight: 2,146 lb (974 kg)
    • Useful load: 1,373 lb (623 kg)
    • Max takeoff weight: 3,600 lb (1,633 kg)
    ]]>         <![CDATA[Cessna T210H - R810,000]]> <![CDATA[Cessna 172 - R490,000]]> Production of the C-172 started in 1956 with the first delivered Cessna 172 from the Cessna factory. Newer and later generation pilots have made the design a resounding market success and possible the most sucessful training aircraft ever. According to Cessna, they have built some 43,000 C-172s since 1956. The first C-172 used a Continental O-300A six cylinder air-cooled flat opposed 145 horsepower engine.The first C-172 had a 'straight' tail like the C-170. In 1960 Cessna  introduced the swept-tail model 172A.

    ]]>         <![CDATA[Cirrus SR-22 GTS -Turbo - R3 900 000,00 Excluding VAT]]> <![CDATA[Cessna 172 - R400,000]]> Production of the C-172 started in 1956 with the first delivered Cessna 172 from the Cessna factory. Newer and later generation pilots have made the design a resounding market success and possible the most sucessful training aircraft ever. According to Cessna, they have built some 43,000 C-172s since 1956. The first C-172 used a Continental O-300A six cylinder air-cooled flat opposed 145 horsepower engine.The first C-172 had a 'straight' tail like the C-170. In 1960 Cessna  introduced the swept-tail model 172A.

    ]]>         <![CDATA[Beechcraft V35B Bonanza - R1,026,000]]> <![CDATA[Cessna 210M - R1,065,000]]> <![CDATA[Beechcraft V35B Bonanza - R 850,000 + VAT]]> <![CDATA[Cessna T210N - R1,075,000]]> The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
     
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)
     
    ]]>         <![CDATA[Cessna U206G - R1,505,000]]> Six seats, powered by a Continental IO-520-F of 300 hp (224 kW), with a gross weight of 3,600 lb (1,633 kg) and certified on 21 June 1976

     

    Max Cruising Speed: 156

    Recommended Cruise: 147

    Range at Std. Cruise: 680nm

    Service Ceiling: 14800 feet

    ]]>         <![CDATA[Cessna U206G - R1,344,000]]> Six seats, powered by a Continental IO-520-F of 300 hp (224 kW), with a gross weight of 3,600 lb (1,633 kg) and certified on 21 June 1976

     

    Max Cruising Speed: 156

    Recommended Cruise: 147

    Range at Std. Cruise: 680nm

    Service Ceiling: 14800 feet

    ]]>         <![CDATA[Cessna U206G - R1 065 000]]> Six seats, powered by a Continental IO-520-F of 300 hp (224 kW), with a gross weight of 3,600 lb (1,633 kg) and certified on 21 June 1976

     

    Max Cruising Speed: 156

    Recommended Cruise: 147

    Range at Std. Cruise: 680nm

    Service Ceiling: 14800 feet

    ]]>         <![CDATA[Piper PA32 Cherokee 6 - $33,800]]>  The

     
    • Maximum speed: 151 kts (280 km/h)     
    • Service ceiling: 16250 ft (4950 m)
    • Rate of climb: 1050 ft/min (5.3 m/s)
    • Cruise speed: 146 kts mph (272 km/h)
    • Range: 840 miles (1361 km)

    Piper PA-32 Cherokee Sixis a series of six or seven seat, fixed or retractable landing gear, ,manufactured in the United States by Piper Aircraft. The best example of this popular aircraft is is PA-32-300:

     

    ]]>         <![CDATA[Piper PA28-235 - $69,645]]> The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

     

    • Crew/Pax: 1+3 
    • Cruise speed: 126knots (145mph)
    • Wingspan: 30.0 feet (9.2 m)
     
    • Empty weight: 1592 lb (722 kg)
    • Useful load: 1408 lb (639 kg)
    • Max takeoff weight: 3000 lb (1361 kg)
     
    ]]>         <![CDATA[Piper PA32 Cherokee 6 - $73,590]]>  The

     
    • Maximum speed: 151 kts (280 km/h)     
    • Service ceiling: 16250 ft (4950 m)
    • Rate of climb: 1050 ft/min (5.3 m/s)
    • Cruise speed: 146 kts mph (272 km/h)
    • Range: 840 miles (1361 km)

    Piper PA-32 Cherokee Sixis a series of six or seven seat, fixed or retractable landing gear, ,manufactured in the United States by Piper Aircraft. The best example of this popular aircraft is is PA-32-300:

     

    ]]>         <![CDATA[Diamond DA20 A-1 'Katana' - R645,000]]> Fuel capacity, std: 20.1 gal (19.5 gal useable)

    Service ceiling: 14,000 ft

    Vno: 118Kts

    Vne (never exceed): 161Kts

    ]]>         <![CDATA[Piper PA18-150 Super Cub - R810,000]]> The Piper PA-18 -Super Cub- is a two-seater, single-engine airplane and a tail dragger. It is today an aviation enthusiast collectors item. Super Cubs are commonly found in roles such as bush flying, banner and glider towing, and other situations in which short field performance is required. It is considered to be one of the most sought after bush planes in the world.

    • Crew/Pax: 1+1
    • Cruise speed: 100 kts (112 mph, 180 km/h)
    • Wingspan: 35 ft 3 in (10.74 m)
     
    • Empty weight: 983 lb (446 kg)
    • Useful load: N/A
    • Max tafeoff weight: N/A
     
    ]]>         <![CDATA[Beechcraft Bonanza A36 - R1,816,750 neg]]>  The Beechcraft Bonanza is an American general aviation aircraft introduced in 1947 by The Beech Aircraft Corporation of Wichita, Kansas. As of 2009 it is still being produced by Hawker Beechcraft and has been in continuous production longer than any other airplane in history. More than 17,000 Bonanzas of all variants have been built.

    F33A Bonanza(1970-1994) F33 with a 285hp Continental IO-520-B engine, later aircraft have a longer S35/V35 cabin and extra seats, 821 built

     

    • Maximum speed: 191 mph (166 kn, 306 km/h)
    • Stall speed: 63 mph (55 kn, 101 km/h)
    • Range: 779 mi (677 NM, 1,247 km)
    • Rate of climb: 1,100 ft/min (5.6 m/s)
     
    ]]>         <![CDATA[Cessna 172F - R535,000]]> The 1965 model 172F introduced electrically operated flaps to replace the previous lever-operated system. These models formed the basis for the US Air Force's T-41A Mescalero primary trainer. A total of 1,436 172Fs were completed.

     

    Vne (Never Exceed Speed) - 174 MPH

    Cruise - 131 mph

    Range - 670 Miles / Time: 6.6 HRS / 102 MPH

    Rate of Climb at Sea Level - 645 FPM

    Service Ceiling - 13,100 Feet

    ]]>         <![CDATA[Cessna 182P - Offers]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

    • Crew/Pax:1+3  
    • Crusise Speed:132 Kts              
    • Wingspan: 36 ft (11.0m)
    • Useful load: 1,140 lb (517 kg)
    • Empty weight: 1,970 lb (894 kg)
    • Max takeoff weight: 3,100 lb (1406 kg)
    ]]>         <![CDATA[Cessna 180 - R637,500]]> The 180 gives excellent speed for a fixed gear aircraft and it has awesome ability to get a heavy loads off the ground and to altitude quickly. The 180 will climb from sea level to 20,000 feet in about 45 minutes. And there has never been an AD involving the airframe structure since the first models were built in 1953.

    ]]>         <![CDATA[Cessna 182Q - R885,000]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

    • Crew/Pax: 1+3
    • Cruise Speed: 132 Kts
    • Wingspan: 36 ft 0 in (11.0 m)
    • Useful load: 1,140 lb (517 kg)
    • Max takeoff weight: 3,100 lb (1406 kg)
    • Empty weight: 1,970 lb (894 kg)
    ]]>         <![CDATA[Piper PA32 Cherokee 6 - R1,021,250]]>  The

     
    • Maximum speed: 151 kts (280 km/h)     
    • Service ceiling: 16250 ft (4950 m)
    • Rate of climb: 1050 ft/min (5.3 m/s)
    • Cruise speed: 146 kts mph (272 km/h)
    • Range: 840 miles (1361 km)

    Piper PA-32 Cherokee Sixis a series of six or seven seat, fixed or retractable landing gear, ,manufactured in the United States by Piper Aircraft. The best example of this popular aircraft is is PA-32-300:

     

    ]]>         <![CDATA[Cessna A185F - $120,000]]> Six seat high wing light aircraft and agricultural aircraft powered by a 300 hp (224 kW) Continental IO-520-D

    ]]>         <![CDATA[Cessna 172 - R670,000]]> Production of the C-172 started in 1956 with the first delivered Cessna 172 from the Cessna factory. Newer and later generation pilots have made the design a resounding market success and possible the most sucessful training aircraft ever. According to Cessna, they have built some 43,000 C-172s since 1956. The first C-172 used a Continental O-300A six cylinder air-cooled flat opposed 145 horsepower engine.The first C-172 had a 'straight' tail like the C-170. In 1960 Cessna  introduced the swept-tail model 172A.

    ]]>         <![CDATA[Cessna U206B - R591,707]]> 285 Horsepower, Continental IO-520-A engine with a belly cargo pack and a newer instrument panel compared to the U206A

     

    Cruise Speed: 143 kts

    Top Speed: 151 kts

    Range: 510 nm

    Rate Of Climb: 920 fpm

    Ceiling: 14800 ft

    ]]>         <![CDATA[Cessna U206G - $119,999]]> Six seats, powered by a Continental IO-520-F of 300 hp (224 kW), with a gross weight of 3,600 lb (1,633 kg) and certified on 21 June 1976

     

    Max Cruising Speed: 156

    Recommended Cruise: 147

    Range at Std. Cruise: 680nm

    Service Ceiling: 14800 feet

    ]]>         <![CDATA[Sportcruiser - R725,000 (negotional)]]> The SportsCruiser is an aluminium constructed, single engine aifcraft with a tricycle undercarriage and a low fixed wing configuration. Designed to fit into the light-sports aircraft category in the State and ultralight or microlight category in several countries

     

    Cruise Speed: 133 mph (214 km/h)

    Range: 630 sm (1020 km)

    Rate of Climb: 1200 ft/min (6.15 m/s)

    ]]>         <![CDATA[Cessna 210 N - P.O.A]]>  The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)

     

    ]]>         <![CDATA[Socata Rallye 235E - R645,000 Neg]]> <![CDATA[Piper PA32R-301 Saratoga SP - R1 053 500]]> The 1980 models reverted to a standard tail design, and were designated as the Saratoga SP. In 1993 the airplane received several cosmetic and systems updates and was redesignated as the Saratoga II HP.

    ]]>         <![CDATA[Cessna 182M - R580,000]]> Four place light aircraft with fixed landing gear, powered by a 230 hp (172 kW) Continental O-470-R piston engine, gross weight 2,800 lb (1,270 kg) and certified on 19 September 1968.There was also an experimental version of this model with a full cantilever wing.

    ]]>         <![CDATA[Piper PA28-235 - R624,000]]> The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

     

    • Crew/Pax: 1+3 
    • Cruise speed: 126knots (145mph)
    • Wingspan: 30.0 feet (9.2 m)
     
    • Empty weight: 1592 lb (722 kg)
    • Useful load: 1408 lb (639 kg)
    • Max takeoff weight: 3000 lb (1361 kg)
     
    ]]>         <![CDATA[Piper PA32R-301 Saratoga SP - R1,025,000]]> The 1980 models reverted to a standard tail design, and were designated as the Saratoga SP. In 1993 the airplane received several cosmetic and systems updates and was redesignated as the Saratoga II HP.

    ]]>         <![CDATA[Tecnam P92-2000RG - R697,000]]> The Tecnam P92 Echo and Tecnam P92 Eaglet are high-winged, light aircraft built by the Tecnam Aircraft company, which is based in Naples, Italy.

    ]]>         <![CDATA[Beechcraft Bonanza A36 - R1,000,000 ]]>  The Beechcraft Bonanza is an American general aviation aircraft introduced in 1947 by The Beech Aircraft Corporation of Wichita, Kansas. As of 2009 it is still being produced by Hawker Beechcraft and has been in continuous production longer than any other airplane in history. More than 17,000 Bonanzas of all variants have been built.

    F33A Bonanza(1970-1994) F33 with a 285hp Continental IO-520-B engine, later aircraft have a longer S35/V35 cabin and extra seats, 821 built

     

    • Maximum speed: 191 mph (166 kn, 306 km/h)
    • Stall speed: 63 mph (55 kn, 101 km/h)
    • Range: 779 mi (677 NM, 1,247 km)
    • Rate of climb: 1,100 ft/min (5.6 m/s)
     
    ]]>         <![CDATA[Piper PA28-235 - R680,000 ]]> The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

     

    • Crew/Pax: 1+3 
    • Cruise speed: 126knots (145mph)
    • Wingspan: 30.0 feet (9.2 m)
     
    • Empty weight: 1592 lb (722 kg)
    • Useful load: 1408 lb (639 kg)
    • Max takeoff weight: 3000 lb (1361 kg)
     
    ]]>         <![CDATA[Piper PA28-235 - R 500,000]]> The Piper PA-28 is a family of light aircraft designed for flight training and personal use. All members of the PA-28 family are all-metal, unpressurized, four-seat, single-engine piston-powered airplanes with low-mounted wings and tricycle landing gear

     

    • Crew/Pax: 1+3 
    • Cruise speed: 126knots (145mph)
    • Wingspan: 30.0 feet (9.2 m)
     
    • Empty weight: 1592 lb (722 kg)
    • Useful load: 1408 lb (639 kg)
    • Max takeoff weight: 3000 lb (1361 kg)
     
    ]]>         <![CDATA[Cessna 207 - R1,100,000]]> The Cessna 207 appeared in 1968 as an elongated version of the Cessna 206D, with cabin space for a seventh person. The powerplant was initially similar to that of the 206. The prototype 207 first flew on 11 May 1968.

    Over the years, a T207 (turbocharged) model appeared, and a 207A with larger diameter propeller. The design was revised in 1978, to produce the Stationair 7 and Turbo Stationair 7 which, with the introduction of an eighth seat in 1980, became the Stationair 8 and Turbo Stationair 8.

    ]]>         <![CDATA[Cessna 210 N - R1,500,000]]>  The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)

     

    ]]>         <![CDATA[SW-18 Teddy - R350,000]]> Manufactured by “SKYWORX AVIATION” the TEDDY SW-18 is Strongly based on the legendary Piper “CUB”.

    SKYWORX uses Modern materials, technology, as well as your choice of either a “ROTAX” 912 ULS (100 HP) or the JABIRU 6 Cylinder 3300 (125 HP) Powerplant! These engines make huge improvements on original performance Characteristics. The low operational cost due to use of automotive fuel  and low fuel consumption make the TEDDY a verry attractive proposition. The “TEDDY” can be registered as a Non Type Certified Aircraft. (NTCA)

    ]]>         <![CDATA[Cessna 210M - R1,240, 000]]> <![CDATA[Cessna 210 N - R1,607,125 ]]>  The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)

     

    ]]>         <![CDATA[Cessna 177 Cardinal - R430,000]]>  The 177 and 177RG are considered desirable aircraft to own, mostly because of the large doors which offer easy entry, good performance, active owners groups and the aircraft's attractive looks.

    • Crew/Pax: 1 + 3
    • Cruise speed: 124 knots (143 mph, 230 km/h)
    • Wingspan: 35 ft 6 in (10.82 m)
     
    • Empty weight: 1,495 lb (680 kg)
    • Useful Load: N/A
    • Max takeoff weight: 2,500 lb (1,100 kg)
     

     

    ]]>         <![CDATA[Cessna 172N - R805,000]]>  Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production.

    • Crew/Pax: 1 + 3
    • Wingspan: 36 ft 1 in (11.0 m)
    • Empty weight: 1,620 lb (736 kg)
     
    • Useful load: 830 lb (376 kg)
    • Max takeoff weight: 2,450 lb (1,113 kg)
    • Cruise speed: 122 knots (140mph, 226 km/h)
     

     

    ]]>         <![CDATA[Cessna 210L - R1,505,000]]> The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1985.

     

    210L Centurion
    A 210K with nose-mounted landing lights, the electrical system changed to 24 volt, the engine driven hydraulic pump replaced with an electrical pump and a three bladed prop fitted. Improved aerodynamics led to an increase in approximately 8 kn (15 km/h) in cruise speed.The Produced 1972-76, 2070 built.
     

    The below is based on the C210N Turbo

    • Maximum speed: 204 knots (235 mph, 378 km/h) at 17,000 ft (5,200 m)
    • Cruise speed: 193 knots (222 mph, 358 km/h) at 20,000 ft (6,100 m)
    		  Range: 900 nmi (1,036 mi, 1,668 km) econ cruise at 10,000 ft (3,050 m)Rate of climb: 930 ft/min (4.7 m/s)

     

     

    ]]>         <![CDATA[Cessna 210 N - R630,000]]>  The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)

     

    ]]>         <![CDATA[Cessna 210 N - R955,000]]>  The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)

     

    ]]>         <![CDATA[Cessna T210N - R891,000]]> The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
     
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)
     
    ]]>         <![CDATA[Cessna 210L - R920,000]]> The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1985.

     

    210L Centurion
    A 210K with nose-mounted landing lights, the electrical system changed to 24 volt, the engine driven hydraulic pump replaced with an electrical pump and a three bladed prop fitted. Improved aerodynamics led to an increase in approximately 8 kn (15 km/h) in cruise speed.The Produced 1972-76, 2070 built.
     

    The below is based on the C210N Turbo

    • Maximum speed: 204 knots (235 mph, 378 km/h) at 17,000 ft (5,200 m)
    • Cruise speed: 193 knots (222 mph, 358 km/h) at 20,000 ft (6,100 m)
    		  Range: 900 nmi (1,036 mi, 1,668 km) econ cruise at 10,000 ft (3,050 m)Rate of climb: 930 ft/min (4.7 m/s)

     

     

    ]]>         <![CDATA[Cessna 182N - R785,000]]>  

    The Cessna 182, marketed under the name Skylane, is a four-seat, single-engine, light airplane. It has the option of adding two child seats, installed in the baggage area.Introduced in 1956, the 182 has been produced in a number of variants, including a version with retractable landing gear, and is the second most popular Cessna model, after the 172.

    • Crew/Pax:1+3  
    • Crusise Speed:132 Kts              
    • Wingspan: 36 ft (11.0m)
    • Useful load: 1,140 lb (517 kg)
    • Empty weight: 1,970 lb (894 kg)
    • Max takeoff weight: 3,100 lb (1406
    ]]>         <![CDATA[Piper J 3 Cub - R 350,000]]>  

    General characteristicsCrew: one pilotCapacity: one passengerLength: 22 ft 5 in (6.83 m)Wingspan: 35 ft 3 in (10.74 m)Height: 6 ft 8 in (2.03 m)Empty weight: 765 lb (345 kg)Useful load: 455 lb (205 kg)Max takeoff weight: 1,220 lb (550 kg)Powerplant: 1× Continental A-65-8 air-cooled  65 hp  at 2,350 rpm

    PerformanceMaximum speed: 76 knots (87 mph)Cruise speed: 65 knots (75 mph, 121 km/h)Range: 191 NM (354 km)Service ceiling: 11,500 ft (3,500 m)Rate of climb: 450 ft/min (2.3 m/s)

     

    ]]>         <![CDATA[Cessna 206 - $150,000]]>  This aircrafts combination of a powerful engine, rugged construction and a large cabin has made these aircraft popular bush planes. Cessna describes the 206 as "the sport-utility vehicle of the air." These airplanes are also used for aerial photography, skydiving and other utility purposes.
    • Crew/Pax: 1+5
    • Cruise Speed: 135 Kts
    • Wingspan: 35 ft 10 in (10.92 m)
    • Empty weight: 2,146 lb (974 kg)
    • Useful load: 1,373 lb (623 kg)
    • Max takeoff weight: 3,600 lb (1,633 kg)
    ]]>         <![CDATA[Cessna 210L - R 762, 000]]> The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1985.

     

    210L Centurion
    A 210K with nose-mounted landing lights, the electrical system changed to 24 volt, the engine driven hydraulic pump replaced with an electrical pump and a three bladed prop fitted. Improved aerodynamics led to an increase in approximately 8 kn (15 km/h) in cruise speed.The Produced 1972-76, 2070 built.
     

    The below is based on the C210N Turbo

    • Maximum speed: 204 knots (235 mph, 378 km/h) at 17,000 ft (5,200 m)
    • Cruise speed: 193 knots (222 mph, 358 km/h) at 20,000 ft (6,100 m)
    		  Range: 900 nmi (1,036 mi, 1,668 km) econ cruise at 10,000 ft (3,050 m)Rate of climb: 930 ft/min (4.7 m/s)

     

     

    ]]>         <![CDATA[Cessna 210J - R 542 000]]>  The Cessna 210 Centurion is a six-seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1985.

     

    210J Centurion / Turbo Centurion
    A 210H with reduced wing dihederal, different nose profile and a Continental IO-520-J (or TSIO-520H) engine, introduced in 1969, 200 built.
    The below is based on the C210N Turbo
    • Maximum speed: 204 knots (235 mph, 378 km/h) at 17,000 ft (5,200 m)
    • Cruise speed: 193 knots (222 mph, 358 km/h) at 20,000 ft (6,100 m)
    		 Range: 900 nmi (1,036 mi, 1,668 km) econ cruise at 10,000 ft (3,050 m) Rate of climb: 930 ft/min (4.7 m/s)

     

     

    ]]>         <![CDATA[Beechcraft Bonanza A36 - R 1,450,000]]>  The Beechcraft Bonanza is an American general aviation aircraft introduced in 1947 by The Beech Aircraft Corporation of Wichita, Kansas. As of 2009 it is still being produced by Hawker Beechcraft and has been in continuous production longer than any other airplane in history. More than 17,000 Bonanzas of all variants have been built.

    F33A Bonanza(1970-1994) F33 with a 285hp Continental IO-520-B engine, later aircraft have a longer S35/V35 cabin and extra seats, 821 built

     

    • Maximum speed: 191 mph (166 kn, 306 km/h)
    • Stall speed: 63 mph (55 kn, 101 km/h)
    • Range: 779 mi (677 NM, 1,247 km)
    • Rate of climb: 1,100 ft/min (5.6 m/s)
     
    ]]>         <![CDATA[Cessna 152 Texas Tail Dragger - R450,000]]> The Cessna 152-Texas Tail Dragger- is an American two-seat, tail dragger, general aviation airplane, used primarily for flight training and personal use. The Texas Tail Dragger STC upgraded version has a  an O-320D1 (160 bhp) was a modernization of the proven Cessna 152 design.

    It has substantailly superior pertformance chararcterstics and is a unique collectable aircraft ideal for short strips.

     

     

     

    ]]>         <![CDATA[Luscombe Silvaire - R 484 000]]> The Luscombe 8 is a series of high wing monoplanes designed in the late 1930s.The Luscombe 50 (Model 8) was to become the company's most famous product. Further design changes to simplify construction of the model 8 vertical stabilizer and horizontal stabilizer construction were implemented in 1947. These changes were alleged to save several hundred man hours in the construction of the airplanes.

    • Useful Load: 535 pounds
    • Max Speed: 125 mph (201 km/h)
    		  
    • Cruise Speed: 110 mph (180 km/h)
    • Range: 370 miles (600 km)
    ]]>         <![CDATA[Cessna 172M - R 645,000]]>  Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production.

    • Crew/Pax: 1 + 3
    • Wingspan: 36 ft 1 in (11.0 m)
    • Empty weight: 1,620 lb (736 kg)
     
    • Useful load: 830 lb (376 kg)
    • Max takeoff weight: 2,450 lb (1,113 kg)
    • Cruise speed: 122 knots (140mph, 226 km/h)
     

     

     

    ]]>         <![CDATA[Piper PA28R-200 Arrow II - R 810 000 NEG]]>  

    In 1967, Piper introduced the PA-28-180 Arrow. This aircraft featured a constant-speed propeller and retractable landing gear and was powered by a 180 horsepower (134 kW) Lycoming IO-360-B1E engine. The engine was upgraded to a Lycoming IO-360-C1C of 200 horsepower (149 kW) in 1971 and the designation was changed to PA-28R-200. At the time the Arrow was introduced, Piper removed the Cherokee 150 and Cherokee 160 from production.

    ]]>         <![CDATA[Cessna T210N - R 1,460,000]]> The Cessna 210 Centurion is a 6 seat, high-performance, retractable-gear single-engine general aviation aircraft which was first flown in January 1957. Production was completed in 1986

    • Crew/Pax: 1+5
    • Cruise Speed: 192 kts
    • Wingspan: 36 ft 9 in (12.12 m)
     
    • Empty weight: 2,400 lb (1,090 kg)
    • Useful Load: N/A
    • Max takeoff weight: 4,000 lb (1818 kg)
     
    ]]>         <![CDATA[Cessna 172N - R645,000]]>  Measured by its longevity and popularity, the Cessna 172 is the most successful mass produced light aircraft in history. The first production models were delivered in 1956 and they are still in production.

    • Crew/Pax: 1 + 3
    • Wingspan: 36 ft 1 in (11.0 m)
    • Empty weight: 1,620 lb (736 kg)
     
    • Useful load: 830 lb (376 kg)
    • Max takeoff weight: 2,450 lb (1,113 kg)
    • Cruise speed: 122 knots (140mph, 226 km/h)
     

     

    ]]>         <![CDATA[Cessna 182RG - R1,200,000]]> The Cessna 182, marketed by Cessna under the name Skylane, is a 4 seater single engine light aircraft. The 182 is the second most popular model produced by Cessna after the 172. Many updated variants of the Skylane have been offered over the years.

    • Crew/Pax:1+3
    • Crusise Speed:132 Kts              
    • Wingspan: 36 ft (11.0m)
    • Useful load: 1,140 lb (517 kg)
    • Empty weight: 1,970 lb (894 kg)
    • Max takeoff weight: 3,100 lb (1406 kg)
    ]]>