As a result, I started to mull the idea of having my own private glider (there are now 6 based at Monticello). After researching all the pros and cons, for the type of flying I wanted to do, I narrowed down my choice to the Aviastroitel, commonly named "Russia", AC-4, designed by Vladimir Federov. In England it is named Aircraft Cooperative Mechta Me7.
A big factor in the choice is that a member of the Club had one, and I could see it in action both on the ground and in flight. When this member suddenly had to move to Chicago and put up his glider for sale, I just could not pass that opportunity. So, before I realized it, I became the proud owner of N29HS (serial 22, made in 1995); it took me a while to get accustomed to the idea of being an "aircraft owner"!
Search for other "Glider AC-4" on YouTube.com to see a balloon launch and a tail-slide, if you are into aerobatics.
| Parameter | SI | US |
|---|---|---|
| Span | 12.6 m | 41.3 ft |
| Length | 5.24 m | 17.2 ft |
| Height | 1.31 m | 4.3 ft |
| Wing Area | 7.7 m2 | 82.9 ft2 |
| Empty Weight | 141 kg | 311 lb |
| Max Pilot Weight | 109 kg | 240 lb |
| Max Gross Weight | 250 kg | 551 lb |
| Wing Loading | 32.4 kg/m2 | 6.6 lb/ft2 |
| Never Exceed Airspeed Vne | 220 km/h | 119 knots |
| Maneuvering Airspeed Va | 156 km/h | 84 knots |
| Zero-wind Approach Speed | 85 km/h | 46 knots |
| Clean Stall Speed Vs | 68 km/h | 37 knots |
| Best L/D 31:1 Airspeed | 95 km/h | 51 knots |
| Minimum Sink | 0.79 m/s | 158 ft/mn |
Wing Airfoil: modified Wortmann FX60-157 laminar
Aspect Ratio: 20.6
Roll Rate: 90 degree roll in 3.5 s
Best L/D: 31:1 (without after-market wing fairings)
Load Factor: +5.30 g -2.65 g
Polars salvaged from RussiaSailplanes.com in 2000, for different Gross Weights. Data applies to AC-4A and should be very similar to AC-4B (both fixed-gear). L/D gets to 33:1 with fairings.
Comparative McCready Speeds To Fly generated by Carl Herold. The AC-4 without fairings is midway between the L-33 and the Std Cirrus
This Weight and Balance Sheet only applies to serial #22 (factory-built in Russia); it may or may not apply to another serial number.
Wings forwards provide a wider range of pilot weights. Note wide-brim hat (40 deg latitude). Photo by Kevin Ford.
The cost of the FAA Annual is $50 (powered airplane owners will weep at this). It is also much cheaper than the Polish PW-5, to which it lost the competition to be the "World Class" monotype, for reasons that must have been political.
Originally a Con, but now a Pro, the cockpit seating is practically inexistant. You have to make your own padding. On top of that I removed the adjustable back plate because I use my parachute as a back rest instead, against the bulkhead. However, it is possible to majorly shift position during long flights (unlike the "molded-in" PW-5, for which I am too tall at 6'1"). When high AGL at the top of a wide thermal, I sometimes slide forward like in a bathtub, with the head on the front spar, and then the only things I see are the whisps of clouds above me, and the horizon slowly circling around, an incredibly relaxing feeling.
The AC-4 does not fly at all like the PW-5. It is more reactive, essentially it is more of a hot-rod, and you have to fly it that way, quite aggressively. The AC-4 is very pitch-sensitive (regardless of airspeed) can accelerate in a blink, and when flying fast it outperforms gliders of a class above.
The AC-4B is the "tricycle" fixed gear version, as opposed to the AC-4A taildragger with fixed gear and AC-4C taildragger with retractable gear. Having a nosewheel allows full main wheel braking without risking ending up on the nose, which allows landing rolls of 150 feet. You could land across some runways if you needed it!
There is a good support group at http://groups.yahoo.com/group/ac4.
Derek Piggott, aged 81, after completion of a 505 km task in England aboard a Me7 (AC-4) where he beat many younger pilots with superior machines (Wikipedia).
The tongue fairing in front of the tail is easy to damage when inserting the stabilizer.
There is excessive buffeting at 45 knots and below. Since the pitot tube is on the tail, the airspeed indications are erratic, and the Total Energy probe jumpy. The absence of fairing between fuselage and wings (unlike the PW-5) is probably a factor in this. There is an after-market kit for sliding a fairing onto the wings, and then taping it to fuselage and wing. Also I understand that later models of the AC-4 have a different incidences so that it rides more tail-high.
Because of the wing upflex in flight, both ailerons are up by a quarter inch. I do not know if it is by design or not, but given the thoughtfulness of the whole ship I presume it is. This reduces lift towards the wingtip (that geometrically curves the wing upwards the most) and associated drag, as well as the wingtip vortex energy-sucker. The Lockheed L-1011 airliner had an active system to do right that on cruise, to save a few percent of fuel.
The tail wheel leaks, so I need to pump it up every two weeks. It seems to be a standard joke that affects all AC-4s. No big deal.
The RussiaSailplanes.com importer for the USA is no more. I think they lost because they got engulfed in the more complex AC-5, the motorglider version of the AC-4. However, the Russian manufacturer has finally appeared on the Web, as http://www.aviastroitel.com.
Illinois roads look flat and straight but in fact always bordered by utility poles! Land next to them to avoid dinging your ship. Photo by Kevin Ford.
The British Gliding Association (BGA) has three AD-like items in its index of Inspections and Modifications (pdf), worth a serious look:
| BGA Number | Date | Affected | Text |
|---|---|---|---|
| 032_09_2002 | SEP 12, 2002 | Rudder lower hinge | Page 1,Page 2 |
| 034_01_2003 | JAN 13, 2003 | Aileron bellcrank | Page 1,Page 2 |
| 035_02_2003 | FEB 19, 2003 | Air brake and aileron brackets | Page 1, Page 2, Page 3, Page 4, Page 5 |
Note. If you had other preventive or curative repairs done to an AC-4, please let me know.
(1) Probably because the canopy got slammed shut by a gust of wind, the aft canopy locking cone-pin caved in and fell between the sides of the fuselage. It had to be fished out and re-clothed and epoxied from a 4" diameter hole made in the inside wall on the fuselage.
(2) During a FAA Annual, a hairline crack was discovered just next to the forward and single pin attachment of the stabilizer, a scary place for a crack. This involved the standard layer by layer inspection and repair, but it turned out that the crack affected only the outermost shell, ifnot just the paint. The only thing now is that the "white" paint there is not the same as the rest of the glider.
This may look like a lot of maintenance, but when I was Crew Chief for the practically brand new PW-5 of the Illini Glider Club, we had to repair a wing-tip split in half and completely redo the cockpit edge over three feet because of an extensive longitudinal crack, major work in comparison.
