<![CDATA[Foster Aero International Aircraft Sales]]> <![CDATA[Foster Aero International Aircraft Sales]]> <![CDATA[PIPER PA-32 Cherokee 6 - R 957,000]]>  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 182 RG - R 1 237 000]]> 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 182P - R 914 000]]> 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 177 Cardinal - R 395,000]]>  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 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 - R 2,100,000]]>  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 Bonanza - R 1,125,000]]>  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 844,000]]>

    • 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 172R - R 788,000]]> 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[CESSNA 172 - R 915,000]]> 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 172 HAWK XP - R 788,000]]>  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[PIPER PA28-235 - R 806,250]]> 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 206 - R 1 022 000]]>
     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 182Q - R 760 000]]>

    • 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 152 Texas Tail Dragger - R 540 000 OFFERS]]> 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[CESSNA 210 M,N - R 1,075,000]]>  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 182 - $ 96,650.00]]> 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 206 - R 968,000]]>
     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[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 295 000]]> 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 700 000]]>  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 210 - R 1 190 000]]> 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 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 PA28-181 Archer II - R 748 000]]>  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.

    ]]>         <![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[PIPER PA28-235 - R 735 000]]> 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[PIPER PA-28-180 - R550 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[Beechcraft Bonanza A36TC - R 1,615,000]]> <![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 795 000]]>  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 182Q - R 278 000]]>

    • 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 182 RG - R 1,300,000]]> 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 Arrow II PA-28R-200 - R 570 000]]>  

    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[CESSNA C150 - R 376,250]]>  The Cessna 150 is simple, robust and easy to fly. For these reasons it has become one of the world's most popular basic trainers.

    • Crew/Pax: 1+1
    • Cruise speed: 107 knots (123 mph, 198 km/h)
    • Wingspan: 33 ft 4 in (10.2 m)
     
    • Empty weight: 1,111 lb (504 kg)
    • Useful load: 490 lb (220 kg)
    • Max takeoff weight: 1,600 lb (730 kg)
     



    ]]>