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020240cg     msw   09/01/05

 

024-11

SPECIAL SECTION ON FLAP OPERATIONS

 

 

IN GENERAL

 

 
The flap equipped Coyote II has a wider speed envelope but this is only realized through proper flap usage.  
Please take the time to become thoroughly familiar with the aircraft and procedures before attempting any 
maximum performances, take-offs or landings.  The aircraft functions well without using flaps only take-
off/landing distances are longer and speeds are higher.  Pay close attention to the recommended flight speeds 
called out in this section. 
 
The first notch of flaps is 11 degrees used to moderately shorten take-off rolls.  The max flap extension speed 
is 65 mph.  Although it is allowable to extend to full flaps at 80 mph, it is actually better technique to extend a 
notch at a time.  

EXAMPLE:  80 mph-1st notch, 70 mph-2nd notch, 60 mph-3rd notch.

  You'll find this gives you 

much smoother approaches with less flap lever pressure.  For your reference: 1st notch/11 degrees, 2nd 
notch/30 degrees, 3rd notch/43 degrees. 
 
The second flap setting is used again to shorten take-offs and to smoothly decelerate to approach speed.  The 
third notch of flaps is going to yield the shortest take-off with the least distance over a fifty foot obstacle.  Also, 
this setting allows steeper, slower approaches.  Typically a 55 mph approach speed in a 20 degree nose low 
attitude is desired.  

CAUTION:  It is very easy to exceed the maximum flap extension (Vfe) speed during 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 feet to start the flair.  

CAUTION:  Low power and a nose high point attitude 

during the glide slope is to be avoided with or without full flaps. 

 The aircraft may develop high sink and not 

recover. 
 

CAUTION:  Inspect flap lever catches for wear every 100 hours.  Keep roller lubricated. 

 

PROHIBITED:  Spins with flaps extended any degree but 0. 

 

 

MAX PERFORMANCE TAKE-OFFS

 

  
Prior to executing a max performance take-off it is recommended to have performed several take-off and 
landings with no flaps, 1 notch, and 2 notches. 

 PROCEDURE:  Flaps 43 degrees, brakes on full, briskly apply 

full power holding stick slightly back to raise the nose.

  Ease back pressure once breaking ground as needed to 

maintain 55 mph (best angle of climb speed) to 50 ft., then start slowly easing off the flaps and maintain 75 
mph for best rate of climb speed.  Set power as needed.  

CAUTION:  Do not "dump" the flaps when 

retracting...always bleed them off slowly and let the airspeed increase.

 

 
This procedure has proved to yield the shortest possible take-off.  In addition, it is recommended for soft fields. 
The technique is not fool proof, however, and requires a fair amount of piloting skill. 
 
Avoid prolonged flight at high power settings and slow speeds.  This flight mode causes violent, turbulent 
airflow over the tail with associated "tail buffet".  This can be felt in a stick shake.  This is a warning of an 
impending stall and to decrease the angle of attack and increase airspeed. 
 

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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