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L ANGLES STIFFENERS                                                                                    

           V-2

 

L Angles stiffeners are positioned midway between the  ribs on  the Top and Bottom Skins -   except
for the first two inboard ribs at ribs  #6 and #7 for the wing locker.

 

The aft edge of the top  L Angles overlap on top of the Rear Zee flange (right middle diagram on
6F8)

 

1.

 

Back-drill the L Angles Stiffeners for the top and Bottom Skins (left and right sides). The
Stiffeners are crimped later to the same curvature as the ribs.

 

REFERENCE

:  6SV4 top right diagram, 6V8.  Page 17 of the Construction Manual.

 

POSITION

: Between the Rear Ribs.

 

WING LOCKER

:   The wing locker replaces the first Skin Stiffener between R.R #6 and #7

 

NOTE

: The definition of an  L Angle is shown in the upper right hand diagram on drawing

6V5. These are supplied in 4 feet length flanges of equal width bent at 90  degrees (the wiggle
line in front of the 19 means an approximately, dl=36 stand for  developed length: the width of
the flat sheet before it is bent).

 

 

LAYOUT

: a) Mark the center line on the outside flange of  12 L Angles (4ft length)

 

b) Identify the rib station and the position of the L Angles on the pre-drilled skins.

 

c) The L Angles face the towards the  Root or fuselage,  see 6V8

 

BACK-DRILL

: Drill through the pilot holes when the center line of the L angle is visible.

 

a) Place the L Angle over the edge  of a 1 x 2 furring strip (3/4”  board), slide the

board and L Angle and board under the Skin.

 

b) Allow the L Angle to overhand the front edge of the Skin by approximately ½”

inch.

 

c) Back drill and Cleco an end hole when the  flange center line is visible. Drill and

Cleco a second hole before drill the inbetween holes.

 

CUT

:  Mark the width of the Skin on the L Angle, use a marker to trace the edge of the Skin on

the L Angle. Remove the L Angle to mark the cut line:

a)

 

From  the mark traced along  front edge  of the Top Skins, go in  30mm (the
front of the  L Angle to clear the Main Spar top extrusions).

 c) From the mark traced along  the aft edge of the Top Skin  go in 2mm (the L

Angle is to overlap on top of the Rear Zee 6V7-11 flange –  setting the end of
the L angle 2mm back from the aft edge of the Skin will provide just enough
clearance for to keep the end of the L angle clear of the Rear Zee radius of the
top flange).

 

d) Bottom Skin: the front edge of the L angle is also 30mm in from the edge of the

Skin

 

e) Go in 22mm from the aft edge of the bottom Skin (this is the width of the Rear

Zee bottom flange).

Summary of Contents for ZODIAC CH 601 Series

Page 1: ...intended for this manual to be a complete account of sheet metal aircraft technology It is limited to the scope of the ZODIAC CH 601 aircraft assembly This manual is not intended to replace substitute...

Page 2: ...se Ribs 4L 4R 10 6SV3 2HDS Wing tip Ribs 1L 1R 11 6SV1 2S6 to 6SV1 2S9HDS Rear Rib 4L 4R 16 Tool Crimping tool see page 5 of the Construction Manual 21 6SV3 4Leading Edge tapered 2 22 Tool 1 wide ratc...

Page 3: ...rilled skins c The L Angles face the towards the Root or fuselage see 6V8 BACK DRILL Drill through the pilot holes when the center line of the L angle is visible a Place the L Angle over the edge of a...

Page 4: ...scription L WING SKIN STIFFENER ZODIAC CH 601 Drawing Rev 1st Edition 7 96 V 3 V 3 ZODIAC CH 601 WING TOP SKIN t 025 2 REQ 6V8 1 WING BOTTOM SKIN t 016 2 REQ 6V8 2 L REAR Zee CRIMP L TO THE SHAPE OF T...

Page 5: ...the top flange of the Rear Zee b The end of the Rear Zee is on or just shy of the 15 degree bend tangent line of the Splice Plate 6SV4 2 is bent 15 degrees towards the front c 100mm from the inboard...

Page 6: ...601 Drawing Rev 1st Edition 7 96 V 5 V 5 ZODIAC CH 601 6SV4 2 SPICE PLATE t 063 1 REQ 24 25 42 8 25 6V7 11 REAR ZEE t 025 2 REQ l 2428 BEND 571 571 571 8 9 RIB 7 16 A5 PILOT HOLE SPICE PLATE OVERLAPS...

Page 7: ...on the Rib b On the Main Spar connecting the pre drilled holes at each rib station with a vertical line front and back side of the Spar Also extend the line on the top and bottom spar extrusion extru...

Page 8: ...1 Description NOSE RIBS SPAR TIP L ZODIAC CH 601 Drawing Rev 1st Edition 7 96 V 7 V 7 ZODIAC CH 601 NOSE RIBS PILOT HOLE 571 571 571 560 560 560 A5 RIVET L 45 deg REAR VIEW AN3 BOLT TOP AND BOTTOM THR...

Page 9: ...e day light corner flange clears the Spar Extrusion at the top and bottom The bottom of the Rib is flush with the Spar if the Rib is too wide adjust the top flange DRILL CLECO With 20 8 Rivet the skel...

Page 10: ...RIBS AND WING TIP ZODIAC CH 601 Drawing Rev 1st Edition 7 96 V 9 V 9 USE CLAMPS TO KEEP THE RIB STRAIGHT AND FLUSH WITH THE BOTTOM OF THE SPAR 8 A5 END VIEW 2S7 2S8 2S9 REAR RIBS 4R 4L t O25 3A5 3A5...

Page 11: ...ith the Rear Zee web PITCH a 50 A4 table on 6SV4 b The pitch at rib 6 is 25mm TIP Drill the rear rivet line later with the Aileron clamped in place DRILL CLECO Before drilling support the trailing edg...

Page 12: ...Edition 7 96 9 97 V 11 V 11 ZODIAC CH 601 22 mm 6SV3 TOP SKIN l 2440 t O25 A4 PITCH 20 A4 PITCH 40 A4 PITCH 40 TACK RIVETS NO RIVET ZONE AFTER RIB S9 OPTIONAL LEVEL BEAM OR USE FLAT WORK BENCH 23 mm...

Page 13: ...onnect the predrilled holes in the skin to extend the rib rivet line to the front edge of the sheet POSITION Line up the rib station marks on the spar extrusion from step 6 with the rib station lines...

Page 14: ...H 601 SUPPORT THE SKELETON WITH BLOCKS UNDER THE REAR ZEE 81 mm 159 mm POSITION I B END OF SKIN FLUSH WITH THE SPAR ROOT THE AFT EDGE OF THE SKIN FLUSH WITH THE REAR ZEE TURN WING OVER TOP SIDE DOWN T...

Page 15: ...with the rear of the spar extrusion transfer the rivet spacing from the rib to the strip Remove and clamp the strip flush with the aft edge of the skin to transfer the rivet spacing to the skin Repeat...

Page 16: ...9 97 V 15 V 15 ZODIAC CH 601 TRIM THE AFT EDGE OF THE SKIN FLUSH WITH THE AFT EDGE OF THE BOTTOM SPAR EXTRUSION REMEMBER TO USE SPACERS TO SUPPORT THE WING SKIN IS FLUSH WITH I B END OF SPAR PRE DRILL...

Page 17: ...5 Cut the Leading Edge Skin to install the Fiberglass Wing Tip 6SV4 3 COMMENT Some builders prefer to overlap the Fiberglass over the Rear Tip Rib to avoid the reverse overlap as shown on V 9 How the...

Page 18: ...ion NOSE RIB INSTALLATION ZODIAC CH 601 Drawing Rev 1st Edition 7 96 9 97 V 17 V 17 ZODIAC CH 601 WING TIP 6SV4 3 NOSE RIB FIBREGLASS 2 REQ L R TRIM REAR RIB 9 LIFT REAR TOP SKIN TO REACH INSIDE WITH...

Page 19: ...proper edge Use the Rivet patter of the Root Rib as a template for the other ribs Refer to drawing 6V10 for the rivet pitch 2 A4 in the web 5 A4 in the top and bottom flange The rivet layout is Refer...

Page 20: ...a V 19a ZODIAC CH 601 AILERON RIBS t 016 3L 3R 6V10 3 11 deg ALIGN THE AILERON RIBS WITH WING RIBS AILERON SKIN t 016 2 REQ l 2438 6V3 1 AILERON TWIST SHIM UNDER THE 0UTBOARD TRAILING EDGE AILERON RIB...

Page 21: ...scription AILERON HORN ZODIAC CH 601 Drawing Rev 1st Edition 7 96 9 97 V 19b V 19b ZODIAC CH 601 5 16 in hole 40 100 15 70 98 deg 5 16 hole horn bolted to template 10mm raduis to hole center 6V10 2 AI...

Page 22: ...ilot hole in the template for the horn bolt Scribe a 10mm circle around the pilot hole POSITION The Horn is positioned on the Aileron Rib 6V10 31 with reference to the horn bolt for the Rod end Positi...

Page 23: ...265 USA 573 581 9000 FAX 573 581 0011 Description AILERON TIP RIB ZODIAC CH 601 Drawing Rev 1st Edition 7 96 9 97 V 21 V 21 ZODIAC CH 601 6SV3 3 AILERON TIP RIB 2 REQ WING TIP A4 PITCH 40 APPROXIMATEL...

Page 24: ...Skin 33 Wing Locker Channel 6VS4 4 NOTE The Channel will slice through the third lightening hole of the outboard Rear Rib 7 POSITION The flange point back and rivets to the Top Skin BOTTOM FLANGE Riv...

Page 25: ...96 9 97 V 23 a V 23 ZODIAC CH 601 6SV4 4 WING LOCKER CHANNEL t O25 1L 1R REQ L ANGLES A4 PITCH WING LOCKER DOOR DZUS 150 150 150 L A4 PITCH 40 RIB 6 RIB 7 A4 PITCH 40 SKIN OVERHANGS PAST THE RIB TO SU...

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