IAR-46
Template:Infobox aircraft The IAR-46 is a very light two-seater airplane for flight schools, training and tourism. Construction uses conventional riveted joints. The seats are arranged side by side, the conventional left seat being the pilot or student pilot seat. The aircraft has a low trapezoidal wing, empennage in "T" configuration, semi-retractable landing gear (mechanical), with the tailwheel connected to the rudder.
The aircraft was certificated under JAR-VLA regulations by the Romanian Civil Aviation Authority in November 1999.[1]
Variants
- IAR 46
- baseline production version
- IAR 46S
- More powerful 73.5 kW (98.6 hp) Rotax 912 S3 engine
Specifications (IAR.46)
Data from Brassey's World Aircraft & Systems Directory 1999/2000,[2] Jane's all the World's Aircraft 2004-05.'[3]
General characteristics
- Crew: twoTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Aspect ratio: 9.403:1
- Airfoil: GA(W)-1Template:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Fuel capacity: 78 L (21 US gal; 17 imp gal)Template:Aircraft specs/convertTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/engTemplate:Aircraft specs/lengthTemplate:Aircraft specs/convert
- Propellers: 2-bladed Hoffmann HO-V352F/170FQTemplate:Aircraft specs/length
PerformanceTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/speedTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/rangeTemplate:Aircraft specs/convert
- g limits: +4.4, -2.2Template:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convertTemplate:Aircraft specs/convert
- Power/mass: 12.58 kg/kW (20.67 lb/hp)
Notes
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- ^ Jackson 2003, p. 351.
- ^ Taylor 1999, p.455.
- ^ Page Module:Citation/CS1/styles.css has no content.Jackson, Paul, ed. (2005). Jane's all the World's Aircraft 2004-05. London: Jane's Publishing Group. ISBN 0-7106-2614-2.
References
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- Jackson, Paul. Jane's All The World's Aircraft 2003–2004. Coulsdon, UK: Jane's Information Group, 2003. Template:ISBN.
- Taylor, Michael J.H. Brassey's World Aircraft & Systems Directory 1999/2000. London:Brassey's, 1999. Template:ISBN.
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