The HL-6 was a low-wing cantilevermonoplane of conventional configuration. It employed a fixed tailskid undercarriage. The student and instructor sat in tandem, in open cockpits.[1]
Variantsedit
HL-6 - prototype. One built
HL-6A - similar to prototype but with more powerful engine. Five units were constructed in 1943.
HL-6B Cauré - Similar to HL-6A but with more powerful engine 216 kW (290 hp) Lycoming O-290C, and optional enclosed cabin. 39 units were constructed in 1944.
^Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 256.
^Bridgman, Leonard, ed. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. pp. 7c–8c.
Further readingedit
Bertazzo, Roberto Portella (2003). A Crise da Industria Aeronáutica Brasiliera 1945-1968. pp. 10–11.
External linksedit
April 18, 2024
cnna, civil, trainer, aircraft, developed, brazil, 1943, role, civil, trainer, aircraft, manufacturer, cnna, first, flight, october, 1942, number, built, contents, development, variants, specifications, cauré, trainer, references, further, reading, external, l. The CNNA HL 6 was a civil trainer aircraft developed in Brazil in 1943 HL 6 Role Civil trainer aircraft Manufacturer CNNA First flight October 1942 Number built 60 Contents 1 Development 2 Variants 3 Specifications HL 6B Caure trainer 4 References 5 Further reading 6 External linksDevelopment editThe HL 6 was a low wing cantilever monoplane of conventional configuration It employed a fixed tailskid undercarriage The student and instructor sat in tandem in open cockpits 1 Variants editHL 6 prototype One built HL 6A similar to prototype but with more powerful engine Five units were constructed in 1943 HL 6B Caure Similar to HL 6A but with more powerful engine 216 kW 290 hp Lycoming O 290C and optional enclosed cabin 39 units were constructed in 1944 Specifications HL 6B Caure trainer editData from Jane s all the World s Aircraft 1947 2 General characteristicsCrew 2 Length 7 2 m 23 ft 7 in Wingspan 9 8 m 32 ft 2 in Height 2 04 m 6 ft 8 in Wing area 15 m2 160 sq ft Empty weight 545 kg 1 202 lb Gross weight 750 kg 1 653 lb Fuel capacity 88 L 23 US gal 19 imp gal Powerplant 1 Lycoming O 290 C 4 cylinder air cooled horizontally opposed piston engine 97 kW 130 hp at 2 800 rpm for take off Propellers 2 bladed wooden fixed pitch propeller Performance Maximum speed 200 km h 120 mph 110 kn Cruise speed 180 km h 110 mph 97 kn 70 power Stall speed 85 km h 53 mph 46 kn Range 520 km 320 mi 280 nmi radius 260 km 160 mi 140 nmi Service ceiling 4 500 m 14 800 ft service ceiling Rate of climb 4 5 m s 890 ft min Time to altitude 1 000 m 3 300 ft in 4 2 minutes Wing loading 50 kg m2 10 lb sq ft Power mass 8 046 kg kW 13 23 lb hp References edit Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 256 Bridgman Leonard ed 1947 Jane s all the World s Aircraft 1947 London Sampson Low Marston amp Co pp 7c 8c Further reading editBertazzo Roberto Portella 2003 A Crise da Industria Aeronautica Brasiliera 1945 1968 pp 10 11 External links editSao Paulo Technical Museum website Retrieved from https en wikipedia org w index php title CNNA HL 6 amp oldid 1125978613, wikipedia, wiki, book, books, library,
