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ASW-24E information | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||
The
ASW-24E is a high performance self-launch sailplane manufactured by
Alexander Schleicher in Germany. It is the self-launch version of the popular Standard
Class ASW-24, introduced in 1987 and produced through the late 90s, and
ultimately replaced in the product line by the ASW-28. The ASW-24E ("E" for engine) features a retractable mast-mounted engine similar to other such designs. It is powered by a Rotax model 275 single cylinder air-cooled two-stroke engine and an MT prop. There were two MT props available, the MT 140-L-86-1B and the MT 140-L-97-1B of which the later was an optional upgrade featuring a narrower blade that offered less weight and less noise.
A search of the FAA database indicates that there are currently four ASW-24Es in the U.S. For comparison, this search also reveals 49 ASW-24/ASW-24B models for a total of 53 ASW-24 family aircraft registered in the US. The ASW-24E is an adaptation of a mainstream 15 meter sailplane, as are virtually all self-launchers. While most self-launch sailplanes have engines in the 40-50 hp range, the -24E features a light single cylinder 26 hp Rotax engine. With this limited horsepower there is therefore debate in the soaring community as to whether the -24E is a "sustainer" or a "self-launcher". The flight manual specifies takeoff roll and rate of climb at sea level as 925 feet and 380 fpm respectively. Real life testing indicates the ship meets these specifications consistently. In fact it will demonstrate a positive rate of climb to at least 8,000 feet agl. By comparison a DG-400, perhaps the most available self-launch sailplane of this vintage with over 250 examples produced, has book specifications of 700' takeoff roll and 600 fpm sea level climb respectively. Indeed better performance while under power, but it also has a heavier, more complicated engine installation that has proven to be more trouble-prone. A typical -24E has an empty weight of around 650 lbs while a DG-400 is usually near 750 lbs. The webmaster's conclusion is that the ASW-24E is indeed a useful self-launch sailplane, but one with a narrower performance envelope while under power where good judgment must be used. Prudence would dictate that when operating from low altitude airstrips with good runways and no obstacles self-launching can be accomplished with no problem at all. However at high altitude airports, and especially on hot high density-altitude days a pilot would be best advised to take a tow. See Take-off Charts from Flight Manual below for specific data. The purpose of this web site is to form a central information resource and knowledgebase on this specific aircraft type. To that end owners, past owners, and those that have flown the -24E are encouraged to submit any and all material that might help others own and operate these aircraft more effectively. Content will be added to the site as it becomes available so check back often. Note that there are linked profile pages available for many of the ships listed in the registry accessible by clicking the link in the Profile column. I hope you find the site useful!
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Why own a powered sailplane? | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Self-powered ships give the soaring pilot some significant benefits and can significantly enhance the soaring experience — to learn more about self-launchers in general, and the ASW-24E in particular, see the following links:
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Registry | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Note: the last two digits of the serial number are the
sequence number of the ship - the product run was 24810 thru 24864.
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Take-off Charts |
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904 lbs - Hard surface, level and dry | 904 lbs - Dry and level grass | ||||||||||||||||||||||||||||||||||||||||||||||||||||||||
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Note the increase in take-off roll for grass. The Flight
Manual has additional tables for different take-off weights. Changing the
take-off surface from paved to grass increases the take-off roll
approximately 50%. Increasing the take-off weight from 904 to 1014 lbs
results in a similar increase, thus special attention should be paid to
keeping the aircraft light, and compensating for non-paved runways.
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Comments/advice/stories Comments from Jason Gregg, the
original owner who special-ordered #24851, to the rec.aviation.soaring newsgroup:
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Operating Info (as we accumulate material)
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Downloads | |||||||||||||||||||||||||||||||||||||||||||||||||||||||||
Factory Technical Notes etc. (right click and "Save As..."
to save .pdf file to your hard disk) Table of AD-Notes and Technical Notes Technical Note 6
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Resources
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