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020240cg     msw   09/01/05

 

024-13

MAINTENANCE

 

 

COVERING:

  The Coyote II is covered with a 3.9 oz. per square Dacron Sailcloth.  This dyed to color material 

will last several years if the plane is stored out of direct sunlight while not in use.  Ultraviolet light is the main 
reason for loss of skin strength.  The tell tale signs of an aging skin are;  
 

1.  Color fading. 
2.  Embrittlement  
3.  Easily torn with rips likely to enlarge. 

 
To preserve your covering there is clear coating (DuPont, Stits, Aerothane) that can be sprayed on. See the 
COVERING Section for more details. The effectiveness in life span extension is considerable.  However, the 
best preservative is indoor storage out of weather and sunlight. 
 

CORROSION and WASHING YOUR PLANE:

  Using the garden hose to wash the outside of your plane may 

seem like a great idea, however this is a practice avoided at the factory.  We simply never let the plane get to 
the point it needs hosing.  Instead, the exterior of the plane is cleaned using a product called Brilliance.  This 
mild cleaner works great on all surfaces including the Lexan.  For the oil or exhaust stains, we use 409 or 
Fantastic.  These clean very effectively without apparent damage to the paint. 
 
If your plane is open air like an Airaile or Stinger and you do use a hose to wash it down, you may be causing a 
future corrosion problem.  In the case of any open cockpit plane with the tail sitting low, it is possible for water 
to collect inside the elevator push pull tube.  This will rust away the elevator yoke and corrode the push pull 
tube also.  
 
Even leaving the plane in the rain can allow moisture to collect in the elevator yoke.  Please avoid the practice 
of spraying water into the cockpit area of your plane, open cockpit or not, this is a practice that will lead to 
corrosion problems and part replacement. 
 
If you suspect your aircraft of corrosion problems, inspect all areas where water may collect, such as the 
elevator yoke area.

 

 
IMPORTANT:

  If you conduct flight operations near or on salt water such as landing on beaches or float activity 

a thorough fresh water washing is a must after each final flight of the day.  This should be done as soon after 
the flight as possible.  Saltwater can be the cause of serious corrosion problems for key structural elements.  
Internal rinsing of spars, struts and fuselage members with fresh water is required if the plane has been 
excessively wetted or submerged in salt water.  During cleaning of any type inspect the craft for signs of 
corrosion and any other abnormalities. 
 

AIRFRAME UP KEEP

 

 
The aluminum and steel structure is designed to last for many years.  However, constant abuse through hard 
landings and high speed flight in rough air could fatigue key structural elements.  To inspect the airframe, look 
for cracks, hole elongation, flecking of anodizing (indicating bends or overloads), bent, dented or corroded 
tubing and any signs of misalignment or distortion.  Consult your dealer or the factory if your inspection reveals 
trouble or in the event of accidental damage beyond your capabilities or repair. 
 

Содержание COYOTE II S-6ES

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Страница 7: ...e Gear Tail Wheel 03 Floorboard Rudder Pedals 04 Control Stick 05 S 1 Firewall 06 Aileron Flaps 07 Seat Seat Belt 08 Tailcone 09 Doors 010 Tail 011 Brakes 012 Engine Mount 013 Engine 014 Instrument Pa...

Страница 8: ...625 0069 actech rans com Parts Department 785 625 6346 When calling Technical Support please have the following ready Aircraft Model Serial Number Engine Model Your Aircraft Assembly Manual Note Pleas...

Страница 9: ...Electronic Protractor Utility knife Hole saw Files 1 8 Countersink Power Tools Electric hand drill Dremel Soldering gun or Hot Knife CD MP3 Player Small electric grinder Acrylic Foam Tape double side...

Страница 10: ...Local Avionic shops can wire your avionic harnesses for you Wells Aircraft does the wiring harnesses for the RANS Fleet Contact George at 620 663 1546 for details WELLS AIRCRAFT P O BOX 858 HUTCHINSO...

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Страница 14: ...cations CLECOS Included in your kit is a supply of clecos These are temporary fasteners that will be used to hold things together while fitting and drilling A Cleco Plier is also included to install a...

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Страница 37: ...o thesockets onthefuselage until themarked ringcenters intheupper pre drilled holeinthegear fegsocket SeeFIGURE 02 O2 IMPORTANT Thegearlegsmustbecentered onthemarked holein theirsocket lt maybenecessa...

Страница 38: ...URE0243 NOTE Aligningthe gearlegs requiresthe fuselage to bein thetaxi position HINT Temporarily installthewheels andblockthefuselage to the sameheight thenrcmovethewheels for setting thegear FIGURE O...

Страница 39: ...vention butnotgreased Theroller bearings shouldbecleaned driedandthenpacked with suitable grease Packing grease without firstremoving theoilwilldilute thewheelgrease causing itto runoutpastthesealandn...

Страница 40: ...ly Rotate thewheelbackandforthwhile tightening thenuttohelpseatthebearings Whenallplayis outoftheassembly andthervheel rotates freely tighten to thene castle slotandinsefi thecotter pin The rubber sea...

Страница 41: ...ain gearassembly ltiseasier tofitanddrillthegearlegsbefore thefuselage fabriccovering isapplied 2 Place thefuselage onasetofsawhorses orother suitable worksurface Measure down ontheforward sideof each...

Страница 42: ...orks well Bothgearlegsshould measure equallength froma common point onthefuselage SeeFIGURE 02A 03 lfadjustments need tobemadetogearleglength remove material fromthetop ofthelonger gearleg FIGURE O2A...

Страница 43: ...ings should becleaned dried andthenpacked with suitable grease Packing grease without firstremoving theoilwilldilute thewheelgrease causing itto runoutpastthesealandnotlubdcate properly Slipthebearing...

Страница 44: ...embly Rotate thewheelbackandforthwhile tightening thenutto helpseatthebearings Whenallplayis outoftheassembly andthewheelrotates feely tighten tothene castle slotandinsert thecotter pin The rubber sea...

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Страница 104: ...ls from running off the wing onto the door 2 During flight always latch the forward safety catch 3 When the door is closed position the door handle so it is in the rub block middle dent 4 Open the doo...

Страница 105: ...ough the Back Interior panel 4 After the wings have been attached Bolt the doors to the fuselage hinges 5 Remove the locking caps from the Gas Spring ends IMPORTANT The Cylinder portion of the Gas Spr...

Страница 106: ...sset to 30 Layoutthe frame work of the vertical stabilizeron a flat work surface Position each gusset and drill out the corresponding hole in each tube to 30 Clecoeachgusset in place Usinga 30 drill b...

Страница 107: ...TOP TUBE TO CONTOUR WITH SPAR 6 4 2 6 Straighten vertical stabilizer ribs with fluting pliers Drill 40 tang rib holes to 30 Rivet Attach Tangs to ribs Refer to parts pagefor orientation Locate upper a...

Страница 108: ...from the raw stock provided Referto the parts manual Remove one clecoed lower aft gusset Contour the lower aft end of the braceto fit into the corner formed bythe Spreader Tube andthe Trailing EdgeSp...

Страница 109: ...end of the bottom ribto I 1 Align the forward attach holein the spreader tube with this hole in the bottom rib Using a 30 bit transfer drill through the pre drilled holes in the bottom rib into the sp...

Страница 110: ...s it rests inthe bottom of the pocket Lacethe rope as shown in FIGURE 011 11 HINT Use a hot knife to melt the lacing cord tips into a flat needle shape for easier insertion into the slots Tension the...

Страница 111: ...ge spar See FIGURE 011 12 Fabricate the tool shown in FIGURE011 12A Usethis tool to installthe forward attach bolt through the belly lacing inthefuselage skin This completes the vertical stabilizer as...

Страница 112: ...co the 90 gusset to the top side of the outboard end of the spar Cleco the 73 gusset to the top side of the inboard end of the spar When attaching the gussets make sure they are oriented properly so t...

Страница 113: ...en horizontal stabilizer ribs with fluting pliers Drill 40 tang rib holes to 30 Rivet attach tangs to ribs Refer to parts pagefor orientation Locate inner and outer ribs within horizontalstabilizer or...

Страница 114: ...Select the tail cables and hardware and bolt these in place as shown in the parts drawing The cables should be adjusted so that the horizontal stabilizer is level Use the wings as a reference The ten...

Страница 115: ...f the elevators They should beflat across each other and not one loweror higher than the other The AFT 314 X 058X 314 aluminumtube that was slipped over the 518 push pull tube during Control Stick Ass...

Страница 116: ...re the bottom side of the stabilizer Slip the small stainless steel lacing wire into the sleeves in the cover Layout and use a hot knife to make 1116 x 5116 slots as shown in Figure 011C 01A Tie the l...

Страница 117: ...FIGURE 01IC 01B 0201lola msw 09 26 06...

Страница 118: ...nd Figure011C 02A for covering of the elevators Fabricatethe Brace Installation Tool shown on FIGURE OllC 02A The Brace Installation Tool may also be rented from RANS Contact RANS Parts Departmentfor...

Страница 119: ...2A RANS BRACE INSTALLATION TOOL LIPS TO BRACE STRAP STEEL HINT TOOL IS AVAILABLE FROM RANS CONTACT PARTS DEPARTMENT CLIP IS FABRICATED FROM A 5 8 X 058 TUBE WELDED TO STRAP AT APPROX 20 ANGLE 020110ta...

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Страница 121: ...fly straight Consider these factors when rigging offset You ll know it s not the engine angle if the offset exceeds 5 8 of an inch IMPORTANT The firewall engine bolts must have 3 threads or more show...

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Страница 150: ...her Lexan surfaces we recommend a soft terry cloth and a cleaner madefor plastic We use a product called Brillianize It is available from RANS or any large aircraft supply company The big no no is nev...

Страница 151: ...on the Station 3 top cross tube Position the center rib and transfer drill through the forward tab into the rib and Cleco Locate and drill a I 1 hole in the center of the flattened portionon the aft e...

Страница 152: ...windshield and skylight panels arejoined together with two mating strips Pre drillthe matingstrips as shown in FIGURE 019 06 Note that the center set of holes should be located to pick up the center...

Страница 153: ...II 11 EVERY 2 3 4 TO II EACH OUTE R RIB MD2580 REV B 7 Lay out and pre drill 30 holes in the Z strips as shown in FIGURE 019 07 FIGURE 019 07 4 3 4 4 3 4 4 3 4 1 2 1 4 TYPICAL 3 4 FLANGE RADIUS CORNE...

Страница 154: ...rough the windshield into the remaining holes ineach tab and Cleco in place FIGURE 019 08 TRANSFER DRILL 11 q CLECO WINDSHIELD OUTER PRE DRILLE 11 HOLES 9 Layout and drill holes in the Skylight Trim S...

Страница 155: ...at the edge of the windshield is 1 32 forward of centerline of the door frame tube Refer to FIGURE 019 011 FIGURE 019 011 12 Mark where the top and middle ribs lay underthe Lexanwith a marker Trim the...

Страница 156: ...ld Down Strip length as needed to clear the strips Layout and drill holes in the Skylight Hold Down Strip per FIGURE 019 015 Trim the ends of the Strip Repositionthe strip and transfer drill 30 intoth...

Страница 157: ...016 FIGURE 019 016 RIVET INTO Z STRIP ONLY DO NOT DRILL OR RIVET INTO FUSLAGE STRUCTURE 17 Apply 112 black foam tape to the top of each rib Apply the 318 x 112 foam strip to the lower outer edge of t...

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Страница 169: ...holeat 22 6 fromtheroot Markspars Left Right Tip Root and Fwd Aft for easier identification 3 Drilloutthecenter holeoftheLeading EdgeSparDoubler to 11 Clecoa LongWingChannet tothe Leading EdgeSparDou...

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Страница 172: ...est drill in a scrap piece of aluminum for proper fit IMPORTANT The bushings may also need to be trimmed in length if the Strut Attach Plate is held away from the spar when bolted Be sure to make Righ...

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Страница 180: ...ribs Do this for all ribs Mark the top centerline of each rib in the nose area This centerline will be used for alignment 3 Separate into Right Hand Left Hand ribs 4 Rivet the 3 Rib Gusset to the outb...

Страница 181: ...n O u L L L c a o U o o q g r u o a L o 6 i i o P c o o J J P P a O C J O C v v a l O f n rl _ _ t _ h o o q o l o o L J L J o Q z o c V V L n T L _ d 3 t t 3 i E o C N F s1 ua_c o FIGUREO22D O6 02022...

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Страница 183: ...l l c r l o l r F I I l l 3 l l l 3 1 l l t E t I l l l l l l a l o l l l n l i l l l c o l l l o t t l s r l l l l o l l t q t l t R t l l r I l l o o l t t l l l l t t l I t t l l l l l l e rllll t...

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Страница 187: ...ng Edge Wrap Transfer drill 30 the remaining holes between ribs Dimple the 3 holes betweenribswith a 118 dimplingdie Modifyan additionalShort Rib Stringer s inboardendto fit on top of Rib 12 See FIGUR...

Страница 188: ...tringerto clearthe fuel tank Startat theroot and rivet the stringers to the ribs HINT Slightly flex Rib 3 to allow access for riveting rivet the clip to the Aft Spar when complete IMPORTANT Stick a 7...

Страница 189: ...Wing 25 From the sealed domed end of the Static Tube measure 4 and cut the excess length off Insertthe Static Tube into the inboard most hole It extends into the leading edge spar 1 112 Position the...

Страница 190: ...itotTube must extend out of the Leading Edge Spar at least 8 When folding wings the PitotTube can be pushedintowing with 114 extended HINT Cuta 1 4 lengthof clear fuel line Slip it over the Pitot Tube...

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Страница 193: ...to the outboard end of the wing The Wing Tip should extend 1 2 past the mounting holes in the Upper Lower Tip Skins HINT Measure 1 from the lines marked on the tape Be sure the top of the Wing Tip is...

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Страница 215: ...installed secured Longeron Fairings Installed Horz Stab Brace Tube Upper Station 6 Top and Bottom Gussets riveted Diagonal Tailcone Cables Bolted with 1 8 tubing anti chaff at cable intersections Sta...

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Страница 231: ...L WEIGHT NOSE WHEEL BAGGAGE AFT BAGGAGE WING TANKS 18 GAL TOTAL MOMENTS TOTAL WEIGHT MAIN RH MAIN LH 6 7 5 4 PILOTS 2 3 1 ITEM 50 LBS MAXIMUM BAGGAGE WEIGHT 90 105 78 78 ARM 26 72 72 951 66110 TOTAL B...

Страница 232: ...EEL BAGGAGE AFT BAGGAGE 4 5 7 6 1 2 4 3 5 7 6 340 50 31 1014 30 WEIGHT 50 LBS MAXIMUM BAGGAGE 30 LBS MAXIMUM BAGGAGE TOTAL ITEM C G TOTAL C G 1014 72 TOTAL 226 90 105 72 TOTAL 226 55 5 ARM 55 5 72165...

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Страница 234: ...is the filler cap closed 13 Repeat Step 5 14 Repeat Step 4 15 Repeat Step 3 16 Repeat Step 3 17 Repeat Step 2 18 Check the cockpit over Are the seat adjusted Move the sticks Is everything moving as i...

Страница 235: ...s on If siphoning occurs shut off the opposite tank ENGINE OPERATIONS Provided with the aircraft is an engine manual authorized by the engine distributor This is a well written manual explaining many...

Страница 236: ...replaced every 25 hours CLOGGED AIR FILTER Spit back the tendency at low RPM s for the engine to throw fuel out of the carb and into the air filter causes the engine oil to eventually clog the filter...

Страница 237: ...uretor and Throttle Quad Check for Position 90 degrees to cylinder Clamp tightness Throttle and Choke cable wear Smooth Throttle and Choke action Loose or missing bolts or screws General condition Muf...

Страница 238: ...land The point at which to flare is critical A good way to land the first time is to plant the mains first Get established over the runway at 55 mph plus about 2 feet off the ground Once things are s...

Страница 239: ...w 4 000 RPM Chandelles Lazy Eights Spins up to 3 turns at low power settings and without flaps only ALL AEROBATIC MANEUVERS EXCEPT THOSE APPROVED ARE PROHIBITED ASI MARKINGS SPORT WING Use the provide...

Страница 240: ...Jamming of the controls may result Always wear the safety belt and shoulder harness to be sure these also do not interfere with the controls CHECK THE CARBURETOR during pre flight for clamp security...

Страница 241: ...such approaches be wary of this LANDING WITH FLAPS Maintain at least 45 to 50 mph with full flaps and a constant glide slope in a nose low attitude Fly down to the runway then level off at 2 to 3 fee...

Страница 242: ...his method works fine for a few miles like to the flying site but is not suited for long hauls DISASSEMBLY FOR TRANSPORT The distance terrain weather and type of trailer will determine how much disass...

Страница 243: ...lect inside the elevator push pull tube This will rust away the elevator yoke and corrode the push pull tube also Even leaving the plane in the rain can allow moisture to collect in the elevator yoke...

Страница 244: ...ntional Entry requires full deflection of elevator and rudder and must be held in full deflection The spin s rotation is approximately 80 degrees nose down with rotation through the center mass almost...

Страница 245: ...ings and pistons every 50 hours Sounds tough but it is not bad if you are careful and easier than fixing airframes Use an aluminum scraper and be careful when removing the rings not to bend them it ge...

Страница 246: ...aners on plumbed 12 Plugs gapped torqued 13 Throttle oiler cables set up properly 14 Fuel pump on plumbed 15 Nose wheel inflated collar pinned FIREWALL AFT 1 Windshield Z s installed 2 Center brace in...

Страница 247: ...tic RPM would render an in flight RPM just below red line with the throttle fully open at sea level A high static RPM may indicate that the propeller is pitched too finely the blades take too small a...

Страница 248: ...start This will depend largely on the specifics of the engine fuel ignition and electrical systems he has installed Again a straightforward logically flowing checklist should be developed that address...

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Страница 335: ...ATOR 2 BLADE TYPE FUSES 6 SAFETY WIRE RADIATOR DRAIN VALVE AND THROTTLE CABLES 3 SEALANT USE SILICONE 7 SEALANT USE SILICONE 4 STARTER SOLENOID 8 STAND OFFS ARE HANDY TO ROUTE WIRE BUNDLES I ENGINEER...

Страница 336: ...2 INSTALLATION 80 100 HP OIL COOLER INSTALLATION 1 LOC TITE ALL OIL COOLER MOUNTING 3 ANTI CHAFE USE COOLANT HOSE SCRAP 2 FOAM RUBBER PADS COOLER I ENGINEER KIT MANUALS S6ES S6 ES_912_INSTALLPICS DOC...

Страница 337: ...CHOKE WIRE 3 LOC TITE SCREWS 4 BRAKE FLUID RESERVOIR 5 FILLER TEE 6 FUEL FILTER 7 HEATER WRAP 8 BLEEDER SCREW BEHIND HOSE 9 FIRESLEEVE ON FUEL LINE IS A GOOD IDEA 10 COOLANT OVERFLOW TUBE I ENGINEER K...

Страница 338: ...ES 912 INSTALLATION 80 100 HP LANDING LIGHT INSTALLED ON 912 1 ECONO LANDING LIGHT FROM WAL MART BLAZER PROJECTOR BEAM FOG LAMP SYSTEM C4072K I ENGINEER KIT MANUALS S6ES S6 ES_912_INSTALLPICS DOC msw...

Страница 339: ...TION 80 100 HP 1 CLEARANCES ARE TIGHT SOME DIMPLING OF EXHAUST TUBE MAY BE REQUIRED 2 1 8 DIAMETER STAINLESS STEEL RIVET SECURES OIL TANK MOUNT IN POSITION I ENGINEER KIT MANUALS S6ES S6 ES_912_INSTAL...

Страница 340: ...6ES 912 INSTALLATION 80 100 HP 1 VENTURI BULB 3 COOLANT OVERFLOW BOTTLE 2 METAL OVERFLOW TUBES 4 MUFFLER MOUNT NOTE CHANNEL FLANGE POSITION I ENGINEER KIT MANUALS S6ES S6 ES_912_INSTALLPICS DOC msw 10...

Страница 341: ...S 6S S 6ES 912 INSTALLATION 80 100 HP 1 RIVET HOLDS POSITION OF CLAMP 2 MUFFLER IS CLOSE BUT WILL CLEAR I ENGINEER KIT MANUALS S6ES S6 ES_912_INSTALLPICS DOC msw 10 25 05...

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