| 
   
   
     
       
         | 
       
      
        
      
      
            
      
            Rans S-9 Chaos 
       
      
      
        
            
            
              
            
            The S-9 Chaos has been in 
            production since 1986. The Chaos is popular the world over in 
            aerobatic competitions and sport flying. A Chaos airframe is a 
            perfect match for the new breed of powerful two stroke engines. A 
            stock S-9 equipped with a Rotax 503 47hp engine is potent enough to 
            compete in sportsman class aerobatics. S-9's have been equipped with 
            up to 100 hp engines with spectacular results. With full inverted 
            capability, a Chaos can whip through an advanced routine leaving 
            little doubt about the plane and pilot's ability to finesse the 
            figures.  
            Aerobatics is the intent of the Chaos, but the well behaved plane 
            serves well for cross country or around the patch flights. Pilot 
            workload is minimal due to the light control pressures. As with all 
            RANS kits, the Chaos comes welded and pre-fabricated, reducing 
            assembly time and increasing precision. 
      
      
            
             
              
               
               
                
                 
                  | 
                  specifications | 
                  
                  
                  
                  47 HP | 
                  
                  
                  65 HP | 
                  
                 
                  | 
                  
                  Wing Span | 
                  
                  
                  22.0 ft | 
                  
                  
                  22.0 ft | 
                  
                 
                  | 
                  Area | 
                  
                  
                  91.5 sq ft. | 
      
                  
                  91.5 sq ft | 
      
                  
                 
      
                  | 
                  Mean Chord | 
                  
                  4 ft 2 in. | 
                  
                  4 ft 2 in | 
      
                  
                 
      
                  | 
                  Aspect | 
                  
                  5.3:1. | 
                  
                  5.3:1 | 
      
                  
                 
      
                  | 
                  Length | 
                  
                  15 ft 8 in | 
                  
                  15 ft 8 in | 
      
                  
                 
      
                  | 
                  Height | 
                  
                  4 ft 10 in | 
                  
                  4 ft 10 in | 
      
                  
                 
      
                  | 
                  Cockpit Width. | 
                  
                  26 in | 
                  
                  26 in | 
      
                  
                 
      
                  | 
                  Headroom | 
                  
                  38 in | 
                  
                  38 in | 
      
                  
                 
      
                  | 
                  Legroom | 
                  
                  45.5 in | 
                  
                  45.5 in | 
      
                  
                 
      
                  | 
                  Number of Seats | 
                  
                  1 | 
                  
                  1 | 
      
                  
                 
      
                  | 
                  Doors. | 
                  
                  1 | 
                  
                  1 | 
      
                  
                 
      
                  | 
                  Landing Gear* | 
                  
                  F/TD | 
                  
                  F/TD | 
      
                  
                 
      
                  | 
                  Baggage Volume. | 
                  
                  n/a | 
                  
                  n/a | 
      
                  
                 
      
                  | 
                  Baggage 
                  Capacity | 
                  
                  n/a | 
                  
                  n/a | 
      
                  
                 
      
                  | 
                  Auxiliary 
                  Baggage Volume | 
                  
                  n/a | 
                  
                  n/a | 
      
                  
                 
      
                  | 
                  Auxiliary 
                  Baggage Capacity | 
                  
                  n/a | 
                  
                  n/a | 
      
                  
                 
      
                  | 
                  Fuel Capacity * | 
                  
                  9 or 18 gal US | 
                  
                  9 or 18 gal US | 
      
                  
                 
      
                  | 
                    | 
                  
                    | 
                  
                    | 
      
                  
                 
      
                  | 
                  power plant | 
                  
                  503 | 
                  
                  582 | 
      
      
                  
                 
      
                  | 
                  Engine | 
                  
                  Rotax 503 | 
                  
                  Rotax 582 | 
      
                  
                 
      
                  | 
                  Output | 
                  
                  47 hp | 
                  
                  65 hp | 
      
                  
                 
      
                  | 
                  Oil Capacity. | 
                  
                  n/a | 
                  
                  2.5 qts | 
      
                  
                 
      
                  | 
                  Coolant 
                  Capacity | 
                  
                  n/a | 
                  
                  4.4 qts | 
      
                  
                 
      
                  | 
                  Propeller 
                  Diameter | 
                  
                  68 in to 70 in | 
                  
                  68 in to 70 in | 
      
                  
                 
      
                  | 
                  Propeller Type | 
                  
                  Wood | 
                  
                  Wood | 
      
                  
                 
      
                  | 
                  Gear Reduction. | 
                  
                  1:2.58 | 
                  
                  1:2.58 | 
      
                  
                 
      
                  | 
                  Fuel G.P.H.
                   | 
                  
                  4.0 gal @ 85% | 
                  
                  5.75 gal @ 85% | 
      
                  
                 
                  |   | 
                  
                 
                
                | 
               
               
                | 
               
              
      
             
                
                 
      
                  | 
                  
                  performance | 
                  
                  
                    | 
                  
                    | 
      
      
                 
                  
                 
      
                  | 
                  
                  Take Off Roll | 
                  
                  250 ft | 
                  
                  200 ft | 
      
                  
                 
      
                  | 
                  
                  Rate of Climb. | 
                  
                  800 fpm | 
                  
                  1000 fpm | 
      
                  
                 
      
                  | 
                  
                  Service Ceiling | 
                  
                  13,500 ft | 
                  
                  15,000 ft | 
      
                  
                 
      
                  | 
                  
                  Cruise. | 
                  
                  90 mph | 
                  
                  100 mph | 
      
                  
                 
      
                  | 
                  
                  VNE. | 
                  
                  130 mph | 
                  
                  130 mph | 
      
                  
                 
      
                  | 
                  
                  Stall Clean | 
                  
                  38 mph. | 
                  
                  41 mph | 
      
                  
                 
      
                  | 
                  Stall Flaps | 
                  
                  n/a | 
                  
                  n/a | 
      
                  
                 
      
                  | 
                  
                  Roll Rate | 
                  
                  
                  100° 
                  /sec
                  
                   | 
                  100° 
                  /sec | 
      
                  
                 
      
                  | 
                  Glide Ratio | 
                  
                  
                  8:1 | 
                  
                  8:1 | 
      
                  
                 
      
                  | 
                  
                  Landing Roll | 
                  
                  400 ft. | 
                  
                  400 ft | 
      
                  
                 
      
                  | 
                  
                  Endurance | 
                  
                  2.25 hrs/4.5 
                  hrs | 
                  
                  1.56 hrs/3.13 
                  hrs | 
      
                  
                 
      
                  | 
                  
                  Range** | 
                  
                  202.5 miles/405 
                  miles | 
                  
                  156.5 miles/313 
                  miles | 
      
                  
                 
      
                  | 
                  
                    | 
                  
                    | 
                  
                    | 
      
                  
      
                 
      
      
                  
                  | 
                  
                  weights and loadings | 
      
                  
                    | 
                  
                    | 
      
      
                 
                  
                 
      
                  | 
                  
                  Gross Weight. | 
                  
                  670 lbs. | 
                  
                  710 lbs. | 
      
                  
                 
      
                  | 
                  
                  Empty Weight. | 
                  
                  340 lbs. | 
                  
                  375 lbs. | 
      
                  
                 
      
                  | 
                  
                  Useful Load. | 
                  
                  330 lbs. | 
                  
                  335 lbs. | 
      
                  
                 
      
                  | 
                  
                  Wing Loading. | 
                  
                  7.32 lbs. | 
                  
                  7.76 lbs. | 
      
                  
                 
      
                  | 
                  
                  Power Loading | 
                  
                  14.2 lbs. | 
                  
                  11.0 lbs. | 
      
                  
                 
      
                  | 
                  
                  Limit Load 
                  Factors | 
                  
                  +6-3 | 
                  
                  +6-3 | 
      
                  
                 
      
                  | 
                  
                    | 
                  
                    | 
                  
                    | 
      
                  
                 
      
                  | 
                  * 
                  F/TD = Fixed Taildragger | 
      
                  
                 
      
                  | 
                  ** 
                  Double the Range with a second optional wing tank | 
      
                  
                 
                 
             
      
            
              
      
      
      flight report
      The S-9 Chaos has been in production since May of 1987, and 
      has remained virtually unchanged since production began. Minor refinements 
      have been implemented to the fuel, control, and cooling systems. A new 
      cowl and landing gear changed the looks a tad a few years back, but for 
      the most part the plane has remained close to original form. It is simply 
      hard to solve the equation significantly better than the way the S-9 does. 
      Maybe with improvements in engines, some weight reduction, and control 
      system upgrades we could see a crisper S-9, even so the stock Chaos is 
      pretty well dialed in for the mission at hand. That mission is low cost, 
      exciting aerobatics. Lots of ultra light type planes claim Akro status but 
      none can do the figures with the agility and precision of the S-9. The 
      reason is the mid wing design allows amazing strength to weight. The 
      original S-9 weighs in at 280 lbs. with the Rotax 503. It seems incredible 
      to roll and loop a plane that light at speeds near 100 MPH.  
       
      Our latest demo plane weighed in at 430 pounds with 220 pounds of fuel and 
      pilot that comes out to a power to weight of 10 per horsepower with the 
      582. 10 to 1 is a decent ratio, bettering that makes it even more 
      exciting. The goal of anyone building an aerobatic plane should be to keep 
      the weight down, and making a lighter S-9, although a challenge could be 
      possible. Most of the ideas I have center around making the plane more 
      mission specific, for example, our new S-9 has two tanks for the 
      occasional cross country. Dropping one tank saves 8 pounds. It may be a 
      little spendy, but titanium landing gear might shave 4 to 5 pounds, and 
      lighter fabric and paint overall could kick out another 2 to 4. Close 
      study and diligent attention to detail could eventually decrease a typical 
      S-9 with a 582 down to fewer than 400 pounds empty. That would be almost a 
      ˝ pound per horsepower less!  
       
      The first flight found me with a plane nearly in perfect rig. After a 
      20-minute flight confirming all was in the green and buttoned down, it was 
      time to test the aerobatic side. I could tell from the climb performance 
      (well above a 1000 FP) and the light handling that this was going to be 
      fun. 
       
      I did a couple of clearing turns, checked altitude and let it rip. From 
      level flight I rolled into a tight right aileron roll. Level again for a 
      brief moment, I repeated the right roll connecting it to three more, 
      holding a level line. The roll rate is impressive between 110 to 120 
      degrees per second.  
       
      Next I did a series of left roll, stop level and right roll, left or right 
      the roll seemed symmetrical. I did four, eight and sixteen point rolls 
      followed by 12 to 14 second slow rolls. All was purring along fine, the 
      S-9 was in its element, the engine never skipped a beat inverted or not. 
      Throttle response was smooth and power was at about 75%. 
       
      From level flight I pulled a loop, goosing the throttle to full power on 
      the up line, making a tight round loop that I let continue into several 
      more. I studied the altimeter noting the loop was less than 300 feet in 
      diameter. Several more loops later I had found great fun in giving it a 
      shot of power on the up line. It was a neat way to make a tight loop. It 
      reminded me of riding a powerful Sea-Doo, pumping the throttle when 
      ramping up a wave to get max airtime, only this was much drier and total 
      three-dimensional fun! 
       
      Ok the basic roll and loop come off without a hitch, it was time to rock 
      and roll, and that is what the S-9 does best. I pulled into a long 
      vertical line topping out in a hammerhead to the right, with a half roll 
      on the down line I entered a hammer to the left, just a little more rudder 
      on these would be nice.  
       
      The vertical line was at least 300 to 400 feet, and allowed a complete 
      vertical roll with barley enough to hammer out at the top. Takes a lot to 
      go straight up, but I was quite pleased with what 65 HP could do.  
       
      On the down line the S-9 has plenty of drag, so you are not easily busting 
      redline, so you have time to adjust the line or roll either way. Keeping 
      it pegged straight down requires a little stick and rudder, but small 
      moves here. 
       
      I performed some lomcevacks by taking it on a 45 up line then hard over to 
      the right with forward stick and punching left rudder. From the ground 
      these look slow motion, and may even be hard to recognize as a lomcevacks, 
      but they are a gas, since the Gs are low. In fact that is one of the 
      pleasures of doing Akro in a light energy plane the g-load are never more 
      than +4mostly under +3.5.  
       
      The optional Hooker harness goes a long way to feeling secure in the 
      plane. I noted no adverse body movement, making it very relaxing to 
      execute a figure knowing not matter the motion I was firmly behind the 
      controls.  
       
      Stalls came off with the traditional buffet with a straight-ahead drop. A 
      slight relaxing of the stick and you are flying again. Noting the 
      indicated airspeed at stall was 45MPH; I was looking forward to gentle 
      landings. At 800 AGL, I slowed to 70MPH for the pattern then on final kept 
      is nailed on 60MPH. Kissing the pavement at just above 50MPH, the landing 
      was something any experienced tailwheeler could do. This is a short quick 
      plane and paying attention on landing is required (as with any tailwheel 
      plane!). However to learn the S-9's traits takes only a few minutes, and 
      it is forgiving enough to allow some less than professional moves. A bonus 
      is the awesome crosswind capacity, 90 degrees at 20 kts is easily 
      demonstrated. Again it is simply getting to know the breed.  
       
      I have heard about pilots not being so enthused about the S-9's runway 
      manners. In most cases pilot skill not being a factor, the planes that 
      would not behave, the builders had made changes to the main gear or 
      tailwheel. On one occasion a builder simply did not have the tailwheel 
      steer springs tight enough. 
       
      In other cases it was not following the recommended procedure. We stress 
      to take off and land with the plane in the three-point position. This is 
      the trick to easy tailwheel operation in both the S-9 and S-10. It is hard 
      for experienced tailwheel pilots to follow this simple advice, but to 
      understand the design of the S-9 is to know why this advice works. The 
      static angle of the S-9 is 9 degrees; that was done on purpose. It placed 
      the gear far enough forward to prevent nose over, and it gave it short, 
      light, and strong gear. There is also very little prop clearance. At such 
      a shallow angle there is no need to get the tail up to rotate, the S-9 
      lifts off when it has flying speed, and does so in the same distance with 
      tail up or down. In fact the tail down take off comes out a little 
      shorter. That is the science behind it, now if we can just get the point 
      across to the veteran tailwheel pilot! 
       
      After a few touch and goes, it was time to call it a day. With just a few 
      minutes of sunlight left, I closed the hanger door thinking about the 
      shiny new plane left inside. How a humble little plane has the ability to 
      take a normal day in a pilot's life and turn it upside down literally, I 
      guess that is why it is called the Chaos!  
      
      
       
  | 
        
      
    
    |