<![CDATA[Foster Aero International Aircraft Sales]]> <![CDATA[Foster Aero International Aircraft Sales]]> <![CDATA[Beechcraft Bonanza F33A - R1,400,000 ]]>
Gross Weight: 3400 lbs
 Top Speed: 182 kts
 Empty Weight: 2125 lbs  Cruise Speed: 172 kts
 Fuel Capacity: 74 gal
  Stall Speed (dirty): 51 kts
 Range: 717 nm  Takeoff`:1002 ft
 Rate Of Climb: 1167 fpm  Landing: 763 ft
 Takeoff Over 50 ft obstacle: 1769 ft  Landing Over 50 ft obstacle: 1324 ft









]]> <![CDATA[Piper PA-32R-301 Saratoga - R900,000.00]]> 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 182 M - R645,000]]> 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[Beechcraft Bonanza F33A - 107,500 €]]>
Gross Weight: 3400 lbs
 Top Speed: 182 kts
 Empty Weight: 2125 lbs  Cruise Speed: 172 kts
 Fuel Capacity: 74 gal
  Stall Speed (dirty): 51 kts
 Range: 717 nm  Takeoff`:1002 ft
 Rate Of Climb: 1167 fpm  Landing: 763 ft
 Takeoff Over 50 ft obstacle: 1769 ft  Landing Over 50 ft obstacle: 1324 ft









]]> <![CDATA[PIPER PA28-235 - R714,750.00]]> 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 182 RG - 86000€]]> 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 PA-32R-301 Saratoga - R1,075,000.00]]> 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 - R980,400.00]]> 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[CESSNA 172 HAWK XP - R1,720,000.00]]>  Cessna produced the R172K Hawk XP from 1977 to 1981. This configuration featured a fuel injected, Continental IO-360K (later IO-360KB) derated to 195 hp (145 kW) with a two bladed, constant speed propeller. The Hawk XP was capable of a 131-knot (243 km/h) cruise speed.


  • 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 206 - R 854,625]]>
 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 PA28-235 - R612,750.00]]> 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 T210N - R2,205,900.00]]>
  • 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[MOONEY M20J - R 967,500]]> 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[PIPER PA-28-180 - R 430,000 Neg]]>  


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[Beechcraft Bonanza A36 - R1,838,250 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[Citabria American Champion - R376,250.00]]> The Citabria is a light single-engine, two-seat, fixed conventional gear airplane  which entered production in the United States in 1964. Designed for flight training , utility, and personal use, it is capable of sustaining aerobatic stresses from +5g to -2g. Its name spelled backwards, "airbatic", reflects this.

]]> <![CDATA[PIPER PA28-235 - R745,000.00]]> 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[PIPER PA-32 Cherokee 6 - R 810,250]]>  The Piper PA-32 Cherokee Six is 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:
 
  • 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)

     

    ]]>         <![CDATA[Cessna 207 - R 1,397,580]]> 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[Shadow Lite Jabiru SP - R 324,325]]> 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[CESSNA 210 M,N - R1,400,000]]>  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 M,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[CESSNA 182Q - R849,250]]>

    • 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[SW-18 TEDDY - R344,000]]> 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 140 - R350 000]]> The Cessna 140 was originally equipped with an Continental C-85-12 or C-85-12F horizontally-opposed, air cooled, four-cylinder piston engine of 85 hp (63 kW). The Continental C-90-12F or C-90-14F of 90 hp (67 kW) was optional, as was the 108 hp (81 kW) Lycoming O-235-C1 engine, an after-market installation authorized in the Type Certificate. This model has a metal fuselage and fabric wings with metal control surfaces. The larger Cessna 170 was a four seat 140 with a more powerful engine.

    ]]>         <![CDATA[CESSNA 210 M,N - R1,236,250.00]]>  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 185A - R565,500.00]]> Six seat high wing light aircraft powered by a 260 hp (194 kW) Continental IO-470-F, landplane gross weight 3,200 lb (1,451 kg) and first certified on 20 September 1961.

     

    The Cessna 185, also known as the Sky wagon, is a six-seat, single-engined, general aviation light aircraft manufactured by Cessna. It first flew as a prototype in July 1960, with the first production model being completed in March 1961. The Cessna 185 is a high-winged aircraft with non-retractable conventional landing gear and a tail wheel. Over 4,400 were built with production ceasing in 1985. When Cessna re-introduced some of its most popular models in the 1990s, the tail wheel equipped Cessna 180 and 185

    ]]>         <![CDATA[CESSNA 210 M,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 - R537,500.00]]>  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 172 - R478,375]]> 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 PA-28-161 Warrior II - R 600,000]]> 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. All PA-28 aircraft have a single door on the co-pilot side, which is entered by stepping on the wing. The Warrior began in 1974 with the change from the Hershey Bar wing to a tapered wing.

    ]]>         <![CDATA[PIPER PA-28-180 - R778,193.00]]>  


    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 172 - $74,950.00]]> 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[DH 82 Tiger Moth - R595,000 ]]>  The de Havilland DH 82 Tiger Moth is a 1930s biplane designed by Geoffrey de Havilland and was operated by the Royal Air Force and others as a primary trainer. The Tiger Moth remained in service with the RAF until 1952 when many of the surplus aircraft entered civil operation and the ubiquitous little trainer is still in great demand worldwide as a recreational aircraft. It is still occasionally used as a primary training aircraft, although now most Tiger Moths employed in training duties are used by pilots gaining experience for taildragger license ratings

    • Maximum speed: 109 mph at 1,000 ft (175 km/h at 300 m)
    • Range: 302 miles (486 km)
    • Service ceiling: 13,600 ft (4,145 m)
    • Rate of climb: 673 ft/min (205 m/min)

     

    ]]>         <![CDATA[MOONEY M20F - R475, 000]]> The Mooney M20 is a family of high performance, piston-powered, propeller-driven general aviation aircraft, all featuring a low-wing and tricycle gear, manufactured by the Mooney Airplane Company.


    • Crew/Pax: 1 + 3
    • Cruise Speed: 156 kts
    • Wingspan: 35 ft
     
    • Useful Load: 1004 lbs
    • Empty Weight: 1 640 lbs
    • Max Takeoff Weight: 3374lbs
     
    ]]>         <![CDATA[PIPER PA-32 Cherokee 6 - R913,750]]>  The Piper PA-32 Cherokee Six is 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:
     
  • 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)

     

    ]]>         <![CDATA[PIPER PA-32 Cherokee 6 - R 752,500-00]]>  The Piper PA-32 Cherokee Six is 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:
     
  • 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)

     

    ]]>         <![CDATA[PIPER PA-32 Cherokee 6 - R 860,000-00]]>  The Piper PA-32 Cherokee Six is 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:
     
  • 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)

     

    ]]>         <![CDATA[Cessna 172B - R320,000 (NEG)]]> The 172B was introduced in late 1960 as the 1961 model and introduced a shorter undercarriage, engine mounts lengthened three inches (76 mm), a reshaped cowling and a pointed propeller spinner.For the first time, the "Skyhawk" name was applied to an available deluxe option package. This added optional equipment included full exterior paint to replace the standard partial paint stripes and standard avionics. The gross weight was increased to 2,250 lb (1,021 kg).

    ]]>         <![CDATA[Bush Baby - R322,500.00]]> Kitplanes for Africa began producing the Bushbaby in 1994. The initial aircraft was modelled on the popular and very successful Kitfox 4. In 2003 the airframe benefited from some significant upgrades and the Explorer was born. In 2008 the Safari was developed and like the Explorer this is also a further development on the original Bushbaby. The Safari has an 8 inch wider cockpit and firewall, longer fuselage, higher tail fin, larger elevator and rudder.

    ]]>         <![CDATA[Bellanca Scout - R537,500.00]]> The 8GCBC Scout is a two-seat, high-wing, single-engine fixed conventional gear, general aviation aeroplane that entered production in the United States in 1974. Designed for personal and commercial use, it is commonly found in utility roles such as Bush flying thanks to its short take offs and landings with (STOL) ability—as well as agriculture, pipeline patrol, and glider and banner towing.

    ]]>         <![CDATA[Cessna 210L - R845,000]]> 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 172N - R806,250]]>  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 - R1,505,000.00]]> 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 M,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 M,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 - R890,114.00]]>
    • 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 - R795 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[Cessna 210L - R1.650,000]]> 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[PIPER PA-28-180 - R430,000]]>  


    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 177 Cardinal - R681,720]]>  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[Piper J 3 Cub - $72,500]]>  

    General characteristics
    Crew:     one pilot
    Capacity:     one passenger
    Length:     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


    Performance
    Maximum 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 182 RG - R1,182,500]]> 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 T206H - $461,712]]>

    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[MOONEY M20F - R725,500]]> The Mooney M20 is a family of high performance, piston-powered, propeller-driven general aviation aircraft, all featuring a low-wing and tricycle gear, manufactured by the Mooney Airplane Company.


    • Crew/Pax: 1 + 3
    • Cruise Speed: 156 kts
    • Wingspan: 35 ft
     
    • Useful Load: 1004 lbs
    • Empty Weight: 1 640 lbs
    • Max Takeoff Weight: 3374lbs
     
    ]]>         <![CDATA[Cessna 210L - R 1,505,000]]> 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 T210N - R 1,640,000]]>
    • 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 172M - R 747,125]]>  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 PA-28-161 Warrior II - R 672,000]]> 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. All PA-28 aircraft have a single door on the co-pilot side, which is entered by stepping on the wing. The Warrior began in 1974 with the change from the Hershey Bar wing to a tapered wing.

    ]]>         <![CDATA[PIPER PA28-235 - R 560,000]]> 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 J 3 Cub - R 350,000]]>  

    General characteristics
    Crew:     one pilot
    Capacity:     one passenger
    Length:     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


    Performance
    Maximum 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 172 - R 330 000 ]]> 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 206 - USD $ 190,000]]>
     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 150 Aerobat - R 430 000]]>  The Cessna 150 is a two-seat tricycle gear general aviation airplane, that was designed for flight training, touring and personal use.


    1970 was the year that Cessna introduced the A150 Aerobat, a Cessna 150 with limited aerobatic capabilities. It retained the 100 horsepower (75 kW) Continental O-200 all 150s used, but the Aerobat had more structural strength. It was rated for +6/-3 “g” and sported four-point harnesses, skylights, and jetisonable doors, along with checkerboard paint schemes and removable seat cushions so parachutes could be worn.


    • Cruise speed: 107 knots (123 mph, 198 km/h)
    • Stall speed: 42 knots (48 mph, 78 km/h)
    		 Range: 366 nm (421 mi, 678 km)

    ]]>         <![CDATA[CESSNA 172 HAWK XP - R 860,000]]>  Cessna produced the R172K Hawk XP from 1977 to 1981. This configuration featured a fuel injected, Continental IO-360K (later IO-360KB) derated to 195 hp (145 kW) with a two bladed, constant speed propeller. The Hawk XP was capable of a 131-knot (243 km/h) cruise speed.


    • 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 152 - R 430 000]]>  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[Beechcraft Bonanza F33A - R 1,720,000]]>
    Gross Weight: 3400 lbs
    		 Top Speed: 182 kts
     Empty Weight: 2125 lbs  Cruise Speed: 172 kts
     Fuel Capacity: 74 gal
    		  Stall Speed (dirty): 51 kts
     Range: 717 nm  Takeoff`:1002 ft
     Rate Of Climb: 1167 fpm  Landing: 763 ft
     Takeoff Over 50 ft obstacle: 1769 ft  Landing Over 50 ft obstacle: 1324 ft









    ]]>         <![CDATA[Cessna T182T - $ 350 000.00]]> The Cessna 182 Skylane is an American four-seat, single-engine, light airplane, built by Cessna of Wichita, Kansas. 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.


    T182T Skylane
    Four place light aircraft with fixed landing gear, powered by a turbocharged and fuel-injected 235 hp (175 kW) Lycoming TIO-540-AK1A piston engine, gross weight of 3,100 lb (1,406 kg) for take-off and 2,950 lb (1,338 kg) for landing. Certified on 23 February 2001.
    • Cruise speed: 145 knots (167 mph, 269 km/h)
    • Stall speed: 49 knots (56 mph, 91 km/h)
    		  
    • Range: 930 nmi (1,070 mi, 1,722 km)
    • Service ceiling: 18,100 ft (5,517 m)


     

    ]]>         <![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[CESSNA 210 M,N - R 1 612 500]]>  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 182 - R 1 680 000]]> 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[Piper Cherokee 140 - R 484,000]]> 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 Cherokee Warrior - R 592,000]]>  The Piper PA-28 Cherokee is a family of light aircraft designed for flight training, air taxi and personal use, built by Piper Aircraft.

     

    Piper reintroduced the Cherokee 150 in 1974, renaming it the Cherokee Warrior (PA-28-151) and giving it the Archer's stretched body and a new, semi-tapered wing.

     

  • 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[Beechcraft Bonanza A36 - R 1,750,000]]>  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 182Q - R 752500]]>

    • 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 152 Texas Tail Dragger - R 495 000]]> 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[IKARUS C42 - R 380,000]]>  The Ikarus C42 is a two-seat, fixed tricycle gear, general aviation microlight airplane, manufactured in Germany by COMCO IKARUS GmbH. It is used primarily for flight training, touring, and personal flying.


    • Range: 432 miles (375 nm, 695 km)
    • Extended range 898 miles (780 nm, 1,445 km) with long-range tanks
    • Rate of climb: 1050 ft/min (320 m/min)
    • VA (maneuvering): 82 KIAS (152 km/h)
    • VNO (max cruise): 105 KIAS (194 km/h)
    • VNE (never exceed): 121 KIAS (224 km/h)

    ]]>         <![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 172 - R 312 000]]> 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 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 Arrow II PA-28R-200 - R 810 000]]>  

    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[PIPER J5A - R 485 000]]> The Piper J5A is the predecessor of the more commonly known PA 12 and shares the same cabin configuration. It is a collectors item , rare and valuable and ceased production in the early 1940's

     

    • Crew /Pax 1+1
    • Max Cruise Speed 85 mph -74 kts
    • Range 380 nm

     

    ]]>         <![CDATA[DH 82 Tiger Moth - R 650 000]]>  The de Havilland DH 82 Tiger Moth is a 1930s biplane designed by Geoffrey de Havilland and was operated by the Royal Air Force and others as a primary trainer. The Tiger Moth remained in service with the RAF until 1952 when many of the surplus aircraft entered civil operation and the ubiquitous little trainer is still in great demand worldwide as a recreational aircraft. It is still occasionally used as a primary training aircraft, although now most Tiger Moths employed in training duties are used by pilots gaining experience for taildragger license ratings

    • Maximum speed: 109 mph at 1,000 ft (175 km/h at 300 m)
    • Range: 302 miles (486 km)
    • Service ceiling: 13,600 ft (4,145 m)
    • Rate of climb: 673 ft/min (205 m/min)

     

    ]]>         <![CDATA[SOCATA Rallye - R 540 000]]>  

    The Rallye is a single engined, low wing monoplane of all metal construction, fitted with a fixed undercarriage. Power was from one of a range of progressively more powerful air cooled engines, ranging from a 100 hp (75 kW) Continental O-200 engine in the Rallye Club, to a 235 hp (175 kW) Lycoming O-540 in the Rallye 235. It has a bulbous cockpit which houses two people in the basic low powered variants and four in the more powerful aircraft, some of which are designed to be used as glider tugs.

    • Maximum speed: 240 km/h (129 knots, 149 mph)
    • Cruise speed: 225 km/h (121 knots, 140 mph)
    • Stall speed: 92 km/h (50 knots, 57.5 mph)
    • Range: 1,300 km (702 nm, 807 mi)
    • Service ceiling: 3,600 m (11,800 ft)

     

     

    ]]>         <![CDATA[CESSNA 182Q - R 850,000]]>

    • 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 T210N - R 1,615,000]]>
    • 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 - R 650 000]]>  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 182 RG - 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)
    ]]>