STOL CH st Edition 1 st Revision Drawings Summary of changes from Edition 1 to Edition 1 Revision 1.
|
|
|
- Myra Atkinson
- 5 years ago
- Views:
Transcription
1 STOL CH st Edition 1 st Revision Drawings Summary of changes from Edition 1 to Edition 1 Revision 1. Page Date Drawing Title 75-G-0 01/10 Three View Drawing 75-G-1 01/10 Drawings Index 75-RX-1 05/09 Rudder Exploded View 75-R-1 06/09 Rudder Ribs 1. P/N 75R1-5, thickness corrected to t=0.025 from t= R-2 10/09 Rudder Spar, Skins, & Hinges 1. P/N 75R2-3, total height corrected from 650mm to 1300mm. 75-RA-1 05/09 Rudder Assembly 75-TX-1 05/09 Horizontal Stabilizer Exploded View 75-TX-2 05/09 Elevator Exploded View 75-T-1 09/09 Horizontal Stabilizer Ribs and Spars 1. P/N 75T1-4: revision changed to 1 to reflect changes made to supplied kit part. 75-T-2 05/09 Horizontal Stabilizer Doublers and Brackets 75-T-3 01/10 Elevator Ribs, Spars, and Horns 1. P/N 75T3-10: bent height corrected from 92mm to 68mm. 75-T-4 09/09 Horizontal Tail Skins and Elevator Trim 1. P/N 75T4-1: revision changed to 1 to reflect changes made to supplied kit part. 75-TA-1 09/09 Horizontal Stabilizer Skeleton 1. Spacing between rivet lines corrected to 227mm on front horizontal stabilizer front brackets. Outside distance between horizontal stabilizer front brackets corrected to 257mm. 75-TA-2 08/09 Horizontal Stabilizer Skin 1. Fairlead riveted to the L angle on the top of 75T4-1 near the rear labeled 75C TA-3 05/09 Elevator Skeleton 75-TA-4 11/09 Elevator Skin Riveting 1. Dimensions added from the aircraft center line to the inside of the inboard elevator rib, dimension is 149mm. 75-TA-5 09/09 Elevator Trim 1. Cutout width for the trim control rod changed to 20mm and the center has been shifted to 57.5mm from the middle rib rivet line. 75-TA-6 06/09 Elevator Mounting on Horizontal Stabilizer 75-SX-1 06/09 Slats Exploded View 75-S-1 06/09 Slats 75-SA-1 03/09 Slat Assembly 75-AX-1 06/09 Flaperon Exploded View 75-A-1 10/09 Flaperons 1. P/N 75A1-8: revision changed to 1 to reflect changes made to supplied kit part. 2. P/N 75A1-9: revision changed to 1 to reflect changes made to supplied kit part. STOL CH 750 Revisions: Updates included in the 1 st edition 1 st revision Page 1 of 6
2 75-A-2 08/08 Flaperons 75-AA-1 06/09 Flaperon Assembly 75-WX-1 07/09 Wings Exploded View 75-W-1 03/09 Wing Ribs 75-W-2 01/10 Wing Spar 1. P/N: 75W2-5: thickness increased to t=0.25 inch to meet European requirements, revision changed to P/N: 75W2-6: thickness increased to t =0.063 inch and top flange increased to 22mm to meet European requirements, revision change to P/N: 75W2-2: 40mm dimension at root end for angle cut corrected to 53mm. 75-W-3 04/09 Wing Spar Fittings 75-W-4 08/08 Root Ribs and Rear Channels 75-W-5 08/08 Top Wing Skins 75-W-6 01/10 Bottom Wing Skins 1. The length, 1000mm, has been added to the drawing for 75W P/N: 75W6-9 Pitot/Static tube added to drawing. 75-W-7 01/10 Jury Struts and Fittings 1. P/N 75W7-2: bend angle changed to 90 degrees, revision changed to P/N 75W7-3: bend angle changed to 90 degrees, revision changed to P/N 75W7-4: tube length changed to 500mm and U fitting changed to 40mm x 20mm tab, revision changed to P/N 75W7-5: tube length changed to 550mm and U fitting changed to 40mm x 20mm tab, revision changed to P/N 75W7-6: bend angle changed to 90 degrees, revision changed to P/N 75W7-7: bend angle changed to 90 degrees, revision changed to P/N 75W7-9: tube length changed to 378mm, tabs changed to U fitting, and 20mm x 20mm tabs welded 25 degrees from U fitting, revision changed to P/N 75W7-10: tube length changed to 715mm, revision changed to W-8 01/10 Wing Struts WS-1 01/10 Wing Spar Assembly 1. Detail: Spar Root Doubler: 75W3-1 label corrected from 75W2-7 and 75W2-7 label corrected from 75W First and last AD5-11 rivet replaced with AN3 bolt on P/N 75W2-7 to meet European requirements. 3. Bolts in 75W2-4 labeled AN4. 75-WA-1 01/10 Wing Skeleton, Slat & Flaperon Brackets 1. One A5 rivet changed to AN3 bolt in P/N 75W3-3 to meet European requirements. 75-WA-2 08/08 Skin Riveting 75-WA-3 01/10 Strut Fittings 1. Installation information added for P/N 75W K-1 10/09 Fuel System 1. P/N: E welded to top outboard corner of P/N 75K1-1 on left tank only for fuel return if required by engine, revision changed to 1. STOL CH 750 Revisions: Updates included in the 1 st edition 1 st revision Page 2 of 6
3 75-KA-1 03/09 Fuel System 75-KA-2 06/09 Fuel Line Routing 75-FX-1 12/09 Rear Fuselage Exploded View 75-FX-2 01/10 Forward Fuselage Exploded View 75-F-1 12/09 Rear Fuselage Skins 1. P/N 75F1-3 revision changed to 1 to reflect holes added to kit supplied parts. 75-F-2 08/09 Rear Fuselage Bulkheads 1. The direction the flanged lightening hole has been reversed on 75F The position of the flanged lightening hole on 75F2-1 has been dimensioned 2748mm from the front edge and centered laterally. 75-F-3 01/10 Rear Fuselage Channels 1. P/N 75F3-4: revision changed to 1 to reflect added cutout in kit supplied parts. 2. P/N 75F3-8: orientation corrected. O/B arrow changed to point down on page. 75-F-4 01/10 Rear Fuselage Doublers 1. P/N 75F4-4: thickness increased to t= inch to meet European requirements, revision changed to P/Ns 75F4-1 and 75F4-2: O/B orientation corrected. 75-F-5 01/10 Baggage Compartment 1. P/N 75F5-1: vertical flanges extended the entire height of the part to make installation easier, revision changed to F-6 12/09 Baggage Compartment 1. Part number 75F6-7 added to drawing. 75-F-7 01/10 Cabin Side 1. P/N 75F7-6 made 1440mm long from 1283mm, front angle cut at 44 degrees from the bottom, and rear cut at 52 degrees from the bottom, part revision number changed to P/N 75F7-9 length changed to 1055mm, front angle cut at 100 degrees from top, first bottom angle cut 67 degrees from top, and second cut made on the bottom 23 degrees from top, revision changed to F-8 08/08 Firewall 75-F-9 08/08 Firewall Stiffeners 75-F-10 10/09 Forward Fuselage Floor & Stiffeners 1. P/N 75F10-1: revision changed to 1 to reflect changes in predrilled hole locations in kit supplied parts. 75-F-11 06/09 Seat Structure 75-F-12 01/10 Forward Fuselage 1. P/N 75F12-7 added, 20mm x 20mm x t=0.032 inch, L=450 angle bent 90 degrees. 75-F-13 01/10 Seats 1. P/N: 75F13-1 part orientation corrected to show flange pointing down to be outboard to be consistent with the assembly drawings. 2. P/N 75F13-3 quantity changed to 1L + 1R. 3. P/N 75F13-7 added, Inboard seat belt attachment. 75-F-14 01/10 Gear Strut Fitting & Engine Mount Fittings 1. P/N 75F14-3: bolts labels were corrected, labels were switched. STOL CH 750 Revisions: Updates included in the 1 st edition 1 st revision Page 3 of 6
4 2. P/N 75F14-3: Penny Washer AN970-6 welded to Strut Pickup for front strut attachment, and holes locations dimensioned. 75-F-15 01/10 Cabin Frame 1. P/N 75F15-1: Spar Carry Through tube changed to 1-1/4inch x inch 4130 to meet European requirements, revision changed to F-16 08/08 Instrument Panel & Window Flashings 75-F-17 07/09 Windshield & Windows 1. P/N: 75F17-4 quantity required corrected to P/N: 75F17-5 quantity required corrected to CS-1 10/09 Cabin Side Assembly 1. Hole designation changed from AN470-AD4-5 to pilot hole for last rivet in 75F FA-1 01/10 Rear Fuselage Assembly 1. P/N: 75F4-1 shortened to reflect actual part at the top of the drawing. 75-FA-2 01/10 Rear Fuselage Top Skin & Rear Bulkheads 1. Side View: Top Channel & Rear Top Channel Riveting added to bottom right of drawing to clarify orientation and riveting information. 2. Side View: Top Channel & Rear Top Channel Riveting, P/N 75F4-3 added for clarification. 75-FA-3 01/10 Baggage Compartment 1. P/N 75F6-7 added to drawing. 2. P/N 75F6-3: vertical flanges shown as full height of part. 3. Top view of P/Ns 75F4-1, 75F4-2, and 75F6-6 added for clarification. 75-FA-4 01/10 Forward Fuselage 1. L angle removed from inboard of P/N 75F12-1 and 75F P/N 75F12-7 replaces L angles. 75-FA-5 08/08 Firewall Assembly 75-FA-6 08/09 Forward Fuselage 1. Fairlead 75C4-2 added to the aft edge of 75F11-6 and is riveted with A4 pitch FA-7 12/09 Fuselage Joining 1. P/N 75F6-7 added to drawing. 2. P/N 75F7-6 lengthened to 1440mm. 3. P/N 75F4-4, one A5 rivet replaced with AN3 bolt to meet European requirements. 4. P/N 75F10-2 last A5 rivet replaced with AN3 bolt to meet European requirements. 5. P/N 75F14-3 top AN3 bolt through P/N 75F4-1 changed to AN4 to meet European requirements. 6. Side view of P/Ns 75F3-6, 75F3-7, 75F4-3, and 75F4-4 added for clarification. 75-FA-8 01/10 Seats & Seat Belts 1. Information about installing inboard set belt attachments removed, now shown on 75-FA FA-9 12/09 Windshield & Windows Installation 1. P/N 75F6-7 added to drawing. 2. P/N 75F7-6 lengthened to 1440mm. 75-FA-10 05/10 Fuselage Doublers 1. New drawing added. 75-CX-1 07/09 Controls Exploded View 75-C-1 05/09 Flap Controls STOL CH 750 Revisions: Updates included in the 1 st edition 1 st revision Page 4 of 6
5 75-C-2 01/10 Elevator Controls 1. P/N 75C2-6: forward bottom radius increased to R12 to allow for dual stick option without changing the elevator bellcrank. 75-C-3 09/09 Rudder Controls & Control Stick 1. P/N 75C3-1: Center hole diameter specified as 28.6mm. 75-C-4 08/09 Fairleads 75-CA-1 12/09 Flaperon Controls 1. P/N 75F6-7 added to drawing 2. P/N 75F7-6 lengthened to 1440mm. 75-CA-2 01/10 Elevator Controls 1. P/N 75F5-1: changes to part reflected on drawing. 75-CA-3 01/10 Rudder Controls 1. Fairlead on riveted to 75C3-1 labeled 75C Fairleads on 75F5-1 labeled 75C P/N 75F5-1: changes to part reflected on drawing. 75-LX-1 07/09 Landing Gear Exploded View 75-L-1 06/09 Nose Gear 75-L-2 05/09 Nose Gear 75-LA-1 05/09 Nose Gear 75-LA-2 05/09 Nose Gear 75-Z-1 10/09 Rear Fuselage Fairings 1. P/N 75Z1-10: Upper Elevator Control Stop added. 2. P/N 75Z1-11: Lower Elevator Control Stop added. 3. P/N 75Z1-12: Flaperon Control Stop added. 75-Z-2 09/09 Door Latch 75-ZA-1 06/09 Horizontal Stabilizer Mounting 75-ZA-2 06/09 Rudder Mounting 1. Hole diameter in 75F3-1 and 75F3-2 corrected to 4.8mm and in 75R2-4 corrected to 6.4mm. 75-ZA-3 08/09 Fin & Rudder Cable Fairing Installation 1. Fairlead riveted with 75Z1-5 labeled 75C Fairlead 75C4-6 added under 75Z1-2 at the aft edge of the lightening hole on part 75F C4-6 is riveted with 3 rivets A4. 75-ZA-4 01/10 Wing Installation 1. Changes to jury struts reflected on drawing. 75-ZA-5 01/10 Strut and Jury Strut Installation 1. Changes to jury struts reflected on drawing. 2. Top view of main strut attachments to gear strut fitting added with note: Maintain minimum 2 x hole diameter for edge distance on AN6 bolts. 75-ZA-6 12/09 Bubble Door Installation 1. Drawing changed to show installation of new door latching system. 2. P/N 75F6-7 added to drawing. 3. P/N 75F7-6 lengthened to 1440mm. 75-ZA-7 10/09 Control Deflections STOL CH 750 Revisions: Updates included in the 1 st edition 1 st revision Page 5 of 6
6 1. P/Ns 75Z1-10, 75Z1-11, and 75Z1-12 installation information added to drawing. 75-CE-1 01/10 Continental O-200 Conical Engine Mount /// end /// STOL CH 750 Revisions: Updates included in the 1 st edition 1 st revision Page 6 of 6
STOL CH nd Edition Drawings July 20, 2010 Summary of changes from Edition 1 to Edition 2.
STOL CH 750 2 nd Edition Drawings July 20, 2010 Summary of changes from Edition 1 to Edition 2. Page Date Drawing Title 75-G-0 07/10 Three View Drawing 75-G-1 07/10 Drawings Index 75-G-2 03/10 General
Zodiac CH 601 XL drawing revision log, updates included in 4 th Edition, January 1, 2008.
Zodiac CH 601 XL drawing revision log, updates included in 4 th Edition, January 1, 2008. 6-X-0 6-X-1 6-T-0 6-T-1 6-T-2 6-T-3 6-T-4 6-T-5 6-T-6 6-W-0 6-W-00 6-W-1 6-W-2 6-W-3 6-W-4 6-W-5 6-W-6 01/08 DRAWING
1881 Airport Road, Mexico Memorial Airport, Mexico, Missouri USA Tel: Fax:
www.zenithair.com 1881 Airport Road, Mexico Memorial Airport, Mexico, Missouri 65265 USA Tel: 5735819000 Fax: 5735810011 Zenith CH 750 Cruzer builder and owner: 4 February, 2016 We're pleased to release
Section C75-WA-1. Wing Skeleton
Section C75-WA-1 This manual has been prepared for assembly of the wing skeleton supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any
STOL CH 701. Clamp a reference extrusion on the bottom of the spar. Clamp the bottom flange of the rib to the extrusion. Rear Root Rib 7V4-2
Rear Root Rib 7V4-2 Clamp a reference extrusion on the bottom of the spar. Clamp the bottom flange of the rib to the extrusion. Cleco the root nose rib to the spar Position the rear root rib at station
75-TA-4. Elevator Skins
75-TA-4 This manual has been prepared for assembly of the. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy between this manual and the drawings, the
FORWARD FUSELAGE SIDES & REAR TOP SKINS
FORWARD FUSELAGE SIDES & REAR TOP SKINS WORK REPORT Step No. Check Parts / Tools Qty Preparations. 1 [ ] 6F5-3 Upper Front Longerons 2 2 [ ] 6F5-5 Heel Support 1 3 [ ] 6F5-2 Front Floor Skin 1 3 [ ] Firewall
Section 6-T-3 Elevator
Section 6-T-3 Elevator This manual has been prepared for assembly of the Elevator using match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
Cut the center and pre-drill the Hinge Plate. Do not drill the Rudder Hinge hole at this time.
7F4-1 Upper Rudder Hinge Plate Layout the cut for the Upper Hinge Plate. Measure and mark the center for the Rudder Hinge. The center hinge hole is 75mm from the back edge of 7F4-1. Cut the center and
STOL CH 701. Standard L ANGLES are supplied in 4ft length. Ref. bottom left diagram on drawing 7-V-2
Standard L ANGLES are supplied in 4ft length. Ref. bottom left diagram on drawing 7-V-2 Length = 206mm. Layout the cut line on the outside flanges. Ref. see boxed diagram on drawing 7-V-2 Three vertical
9.3 FUSELAGE ASSEMBLY 14/03/02
9.3 MATING THE TAIL CONE TO THE CABIN 1) Trim the bottom flange of both FUS-339 side skins on the tailcone assembly as in Figure 1. 2) Remove the bottom two RBULK 2A s of bulkhead A on the tailcone. 3)
Three vertical L angles must be riveted to each main spar (length = 206mm see boxed diagram on drawing 7-V-2).
Cut over-sized (left); Trim and file (above). Note: Six needed. Three vertical L angles must be riveted to each main spar (length = 206mm see boxed diagram on drawing 7-V-2). Trace line down center of
Section 6-B-4 Rear Fuselage Riveting
Section 6-B-4 Rear Fuselage Riveting This manual has been prepared for assembly of the rear fuselage. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
ZODIAC CH 601 Series Kit Aircraft
ZODIAC CH 601 Series Kit Aircraft THE FOLLOWING IS A DRAFT MANUAL This manual has been written and published strictly for informational purpose. It has been prepared as a guide to facilitate the assembly
FINAL ASSEMBLY- DOORS
- DOORS DRAWING 8XF-5 ASSEMBLY OF THE DOORS CONTENTS SECTIONS #4a DOOR FRAME #4b DOOR GUSSETS & BOTTOM SKIN #4c DOOR LATCH & STOP Helpful building tips: Use a flat, unwrapped piece of plywood for the door
CENTER WING SECTION (CWS) WORK REPORT
CENTER WING SECTION (CWS) WORK REPORT No. Check Parts / Description Qty PHASE 1: Preparations 1 [ ] 6V1-3 Rear ribs 2R & 2L 1 [ ] L Angle 6 2 [ ] 6V2-1 Rear Ribs.032 2R & 2L 2 [ ] 6V5-1 Gear Rib Doubler
REAR FUSELAGE ASSEMBLY
SECTION 2 Rear Fuselage Bottom Assembly Ref Dwg 8FR-2 SECTION 2 - Page 1 of 17 FUSELAGE BOTTOM SKIN 8F2-3A Note: The edges of skin 8F2-3A are not a straight line. Check: edge distance from the center of
Section 75-AA-1. Flaperon Assembly
Section 75-AA-1 This manual has been prepared for assembly of the flaperons supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
ZODIAC 601 XL UPRIGHT CHANNELS 6B5-6. Top and bottom outboard flange is joggle to overlap the.093 extrusion 6B2-3 and 6B11-1
UPRIGHT CHANNELS 6B5-6 Top and bottom outboard flange is joggle to overlap the.093 extrusion 6B2-3 and 6B11-1 Length: fits between the bottom and top longerons. Clamp the upright channel to the rear frame
Section 75-ZA-2. Rudder Mounting
Section 75-ZA-2 This manual has been prepared for installation of the Rudder. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy between this manual and
REAR FUSELAGE ASSEMBLY
SECTION 5 Tail Attachments on Fuselage Ref Dwg 8RU-3 The rudder hinge line (HL) is parallel to the aft edge of the fuselage skin SECTION 5 - Page 1 of 9 Looking at the top of the rear fuselage. Stabilizer
STOL CH F2-2 Side Skin
7F2-2 Side Skin IMPORTANT: See drawing 7F2-2 to identify the topside of the skin, also clearly mark the side that will be on the inside of the fuselage (if possible choose the side with the manufacture
SERVICE KIT. March 22, 2011 Original Issue: January 22, 2001 Page 1 of 7
Single Engine SERVICE KIT TITLE RUDDER STOP MODIFICATION - SHEET METAL BULKHEAD EFFECTIVITY NOTE: Some airplanes in this serial range may have a forged bulkhead installed after leaving the factory. Service
Flaperon Assembly Manual
Flaperon Assembly Manual for PegaStol Aftermarket Wings A Senior Project presented to The Faculty of the Aerospace Engineering Department California Polytechnic State University, San Luis Obispo In Partial
STANDARD CANOPY WORK REPORT B-1
STANDARD CANOPY WORK REPORT B-1 No. Check Parts / Tools Qty _ Canopy Lock 1 [ ] 6E2-3 Canopy Hinge Block 1 2 [ ] 6E4-5 Canopy Side Frame 2 2 [ ] 6E2-1 Canopy Lock Assembly 1L + 1R 3 [ ] 6E2-4 Rear Lock
ZODIAC 601 XL. Detail of outboard end. Full length recessed elevator trim tab. Detail of inboard end. Trim tab along left trailing edge of elevator.
Full length recessed elevator trim tab. Detail of outboard end. Detail of inboard end. Trim tab along left trailing edge of elevator. Trim tab in neutral position 6-T-6 - Page 1 of 12 Drill out the middle
STOL CH H3-3SP Center Hinge Bracket. IMPORTANT: The Bracket 7H5-3SP is not symmetrical
7H3-3SP Center Hinge Bracket IMPORTANT: The Bracket 7H5-3SP is not symmetrical Using a square helps layout and mark the perpendicular and the hinge hole. Note: Position of 1/4 hinge hole is 115.5mm from
ZODIAC 601 XL. ZODIAC CH 601 Series. Parts are labeled for easy identification with a part number and description:
CH 601 Series Parts are labeled for easy identification with a part number and description: Part number example: 6T4-4 Vertical Tail Spar 6 - Zodiac CH 601 model T - Rudder section of the Aircraft drawings.
Chap. 9.2 SR3500 Fuselage Assembly - Cabin. MODEL: SR Murphy Aircraft Mfg. Ltd. All rights reserved.
26/06/2006 Page 1 26/06/2006 Page 2 26/06/2006 Page 3 Parts List for Gear Box No. Part Number Description Qty Required 1,23 FUS0711QL BRACING CHANNEL 2 2,22 FUS0711QR BRACING CHANNEL 2 3 FUS301QB CARRYTHROUGH
FLAPERON ASSEMBLY. Ref. Drawing 8XA-1 Exploded view SECTION 1 REAR SKIN AND NOSE RIBS ASSEMBLY
Ref. Drawing 8XA-1 Exploded view SECTION 1 REAR SKIN AND NOSE RIBS ASSEMBLY The slope on the back side of each hinge bracket 8A1-5 face inboard towards the fuselage for both the left and right wing Work
Horizontal Stabilizer Service Bulletin
Horizontal Stabilizer Service Bulletin Date: Friday November 19, 2004 To: All Super Rebel/Moose owners Re: Horizontal stabilizer tip rib INFO: A number of Super Rebels have shown cracking on the tip rib/rear
FORWARD FUSELAGE ASSEMBLY
SECTION 2 Finishing the Firewall RIVETS: SA5 or A5 (all rivets on the firewall, rivet head set from the engine side) SUGGESTION: First drill undersize pilot hole #30 or #40, then open with #20 SECTION
ZODIAC 601 XL. REAR RIBS 6W6-1 to 6W6-9. Reference to drawing 6-W-00 for orientations of ribs flanges. Rear ribs are tapered: rib #9 is the shortest.
REAR RIBS 6W6-1 to 6W6-9 Reference to drawing 6-W-00 for orientations of ribs flanges. Rear ribs are tapered: rib #9 is the shortest. Right wing Zodiac CH 6-W-6 - Page 1 of 12 Burr on edge of flanged lightening
Ch. 9.0 ELITE FUSELAGE ASSEMBLY 14/02/2003
Fuselage Assembly In the front of the fuselage manual you will find an exploded view of the fuselage and a side view schematic. We suggest that you tape these to the wall of your workshop. Refer to them
ZODIAC CH650. ZODIAC CH 650 Series. Parts are labeled for easy identification with a part number and description:
CH 650 Series Parts are labeled for easy identification with a part number and description: Part number example: 6T4-4 Vertical Tail Spar 6 - Zodiac CH 650 model T - Rudder section of the Aircraft drawings.
IMPORTANT - STATE AIRCRAFT REGISTRATION NUMBER IN ALL CORRESPONDENCE MOONEY AIRCRAFT, INC. M-l8 SERVICE LETTER NO.17
IMPORTANT - STATE AIRCRAFT REGISTRATION NUMBER IN ALL CORRESPONDENCE MOONEY AIRCRAFT, INC. M-l8 SERVICE LETTER NO.17 (This Service Letter is FAA. Approved) DATE: OCTOBER 24, 1959 SUBJECT: REAR BULKHEAD
SERVICE BULLETIN
SERVICE BULLETIN 16-03-28 Date Released: May 6, 2016 (Initial Release) June 2, 2016 (Added Note, pg.11) Date Effective: May 6, 2016 Affected Models: Subject: Required Action: All RV-3, 4, 6/6A, 7/7A, 8/8A,
Skymaster ARF F-18E Instructions Manual
Skymaster ARF F-18E Instructions Manual first: Take out the front servos mount, install front fuel tank before installing nose cone connect nose cone to fuselage by 6 screw Take out the 6 screws and Bottom
16. Wing Final Assembly and Installation
Section Objective: Installation and rigging of ailerons. Pitot tube install, and any other wing related items. Required Parts: Left aileron push rod ALA-0072, Right aileron push rod ALA-0073, Push tube
Section 75-FA-5. Firewall Assembly
Section 75-FA-5 This manual has been prepared for assembly of the firewall supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If there is any discrepancy
ZODIAC 601 XL. Outside Flashing 6C3-3. Mark the no rivet zone for Extrusion Handle 6C3-8
Outside Flashing 6C3-3 Mark the no rivet zone for Extrusion Handle 6C3-8 Cleco the inside and outside flashing to the canopy side frame before the canopy bubble is fitted. Ref. Front edge 50mm back from
ZODIAC CH 601 Series Kit Aircraft
ZODIAC CH 601 Series Kit Aircraft THE FOLLOWING IS A DRAFT MANUAL This manual has been written and published strictly for informational purpose. It has been prepared as a guide to facilitate the assembly
ZODIAC CH 601 Series Kit Aircraft
ZODIAC CH 601 Series Kit Aircraft THE FOLLOWING IS A DRAFT MANUAL This manual has been written and published strictly for informational purpose. It has been prepared as a guide to facilitate the assembly
Builders Log Report S
12/09/01 Reamed Horizontal Stabilizer Bushings I reamed seven bushing locations to.4375 where elevator attaches to horizontal stabilizer. The proximity of the locations to structural tubing made it difficult
LANDING GEAR. 1. Fit landing gear into slots on bottom of fuselage.
LANDING GEAR 1. Fit landing gear into slots on bottom of fuselage. 4. Use channel-lock pliers to press blind nuts into position (note: drilled hole should be slightly smaller than shaft of blind nut for
TIGER MOTH 120 ASSEMBLY INSTRUCTIONS
TIGER MOTH 120 ASSEMBLY INSTRUCTIONS SPECIFICATIONS Wing Span: Length: Radio: Flying Weight: 1920mm 1580mm 4 channel with 6 servos 4200g AILERON ASSEMBLY 1 Start by removing the servo cover from the bottom
REVISION DESCRIPTION:
REVISION DESCRIPTION: Page: 09-10 REV 1: Delete Step 1. 14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and
Check the jig with the Slat Ribs. Notice the front tip is cut off, this will allow the slat to fit in the jig correctly.
Slat Jig A slat jig will be needed to obtain the correct curvature of the slat. The Slat drawing is located on 7-F-13, cutout and trace on plywood. The length of the jig is 1830mm, which is the outboard
WING ASSEMBLY SECTION 4. Mounting Wing Ribs to Main Spar. 1. Identify the proper locations for those ribs with attachment brackets.
WING ASSEMBLY SECTION 4 Mounting Wing Ribs to Main Spar Compass Check 1. Identify the proper locations for those ribs with attachment brackets. 2. Position and drill the nose ribs. 3. Un-cleco the nose
Section 75-FA-2 Top Fuselage Skin & Rear Fuselage Assembly
Section 75-FA-2 Top Fuselage Skin & Rear Fuselage This manual has been prepared for assembly of the rear fuselage supplied with match drilled parts. This photo assembly manual is intended as a supplement
Air Tractor, Inc. Repairs Page 5-i AT-802/802A July 30, 2008
Repairs Page 5-i TABLE OF CONTENTS SECTION 5- REPAIRS No. Page FUSELAGE FRAME REPAIRS... 5-1 FORWARD CLAMP BLOCK BOLT FAILURE..5-1 STANDARD STRUCTURAL REPAIR DRAWINGS...5-1 Repairs Page 5-1 April 12, 2010
Important Note. Tools Required: Welder capable of fully welding 10 GA.135 steel
INSTALLATION INSTRUCTIONS Frame Reinforcement Kit 11100 (Patent Pending) 1968-72 GM A-Body Coupe/Sedan Read Instructions FULLY before starting Installation Important Note Installation of this kit requires
Section 6-B-6, 6-B-7, & 6-B-8 Firewall Assembly
Section 6-B-6, 6-B-7, & 6-B-8 Firewall Assembly This manual has been prepared for assembly of the firewall supplied with match drilled parts. This photo assembly manual is intended as a supplement to the
Elevator Assembly. To assemble the SR3500 Elevator, you will need the following tools:
Elevator Assembly To assemble the SR3500 Elevator, you will need the following tools: 1. Drill 2. Tape Measure 3. Felt Marker 4. #40, #30, 3/16, #11 Drill Bits 5. #40, #30 and 3/16 Clecos 6. Cleco Pliers
Section 75-SA-1 Slat Section
Section 75-SA-1 Slat Section This manual has been prepared for assembly of the slat sections supplied with match drilled parts. This photo assembly manual is intended as a supplement to the drawings. If
SERVICE BULLETIN
SERVICE BULLETIN 14-02-03 Date Released: February 3, 2014 Date Effective: February 3, 2014 Subject: Affected Models: Required Action: Time of Compliance: Cracking in elevator spar web near elevator attach
American Champion Aircraft Corp. Rochester, WI Page 1 of 5
Service Letter: 444 Initial Revision Date: August 18, 2017 Title: American Champion Aircraft Corp. Rochester, WI 53167 Page 1 of 5 Installation of Aileron Hinge Reinforcement Models: 8KCAB serial numbers
STOL CH 801 SECTION 2: Nose Rib 8R1-7
SECTION 2: Nose Rib 8R1-7 Position the lower nose rib on the front of the spar at the predrilled holes just above rear rib #3 (615mm from the bottom of the spar) Check lateral alignment (rib is centered
10. Wing prep and subassembly
Date Section Objective: Construct and fabricate the sub-assemblies of the wing panel. Required Parts: Wing left 11gal PN104-300, Wing right 1gal PN104-400, Wing left 15 gal option PN104-322, Wing right
STOL CH 701. Layout the cut line along the bend tangent line on the web. 7V6-1 and 7V6-2SP
Layout the cut line along the bend tangent line on the web. 7V6-1 and 7V6-2SP ORIENTATION: 90 degree flange is up Layout the bend line, 20mm from the end. Ref. bottom right diagram 7-V-6 Use a square to
77.5 degrees REAR CHANNEL PLYWOOD TEMPLATE
77.5 degrees REAR CHANNEL PLYWOOD TEMPLATE Ref. 6-B-14 Make following template: Vertical distance = 300mm Layout dimensions shown in the bottom right table on drawing 6-B-14 Top and bottom are square to
3 rd scale SE5a Biplane kit
3 rd scale SE5a Biplane kit This SE5a kit represents years of research and development. The kit was designed around original RAF factory drawings loaned by WW1 Aero. Original construction and materials
ZODIAC CH 601 XL 6TD3-1 TD MAIN GEAR UPRIGHTS (QTY=1L + 1R) Cutout in the side skin is below the diagonal rivet line.
6TD3-1 TD MAIN GEAR UPRIGHTS (QTY=1L + 1R) Cutout in the side skin is below the diagonal rivet line. The TD Gear Upright 6TD3-1 is installed on top of the landing gear 6TD2-7. 6TD3-1 makes the corner between
96 WING SPAN SPITFIRE (COPYRIGHT PROTECTED 2014) ALL RIGHTS RESERVED
96 WING SPAN SPITFIRE (COPYRIGHT PROTECTED 2014) ALL RIGHTS RESERVED GENERAL INSTRUCTIONS Should you elect to use the recommended Door Skin, which is 1/8 mahogany plywood measuring 36 x 88. Have it cut
2.1 Parts List Tool requirement Before you start assembling the Stabiliser Front Spar Center Doublers...
Stabilizer Assembly 2.0 Exploded View...Error! Bookmark not defined. 2.1 Parts List...3 2.2 Tool requirement...5 2.3 Before you start assembling the Stabiliser...6 2.4 Front Spar...6 2.5 Center Doublers...7
Page: REV 2: Added "Step 1: Straighten the W-0007B Rear Spar Reinforcement Fork as described on Page 10-03, Step 4."
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm REVISION
Bobs Card Models
Bobs Card Models www.bobscardmodels.com Canadair CL-415 (1:72) The Bombardier 415 (formerly Canadair CL-415) is a Canadian amphibious aircraft purpose-built as a water bomber. It is the only aircraft designed
90 WING SPAN P-51D MUSTANG (COPYRIGHT PROTECTED 2014) ALL RIGHTS RESERVED
90 WING SPAN P-51D MUSTANG (COPYRIGHT PROTECTED 2014) ALL RIGHTS RESERVED GENERAL INSTRUCTIONS This design is basically an enlargement of the very popular fun scale Mustang 60 Size. You can build it light
SZD-10 bis CZAPLA ASSEMBLY MANUAL IN PICTURES
1 RUDDER Plan and parts: 2 Assembly steps: Photo above: glue together rudder spar, ribs and trailing edge. Clamp spar to a flat surface (chipboard on the photo) and make sure the straight aligment of the
WING ASSEMBLY 23.5 (Continued)
A VERY IMPORTANT NOTE found on many wing drawings states Do not drill any unspecified holes into spar. This is extremely important as any extra holes may, under extreme conditions, WEAKEN THE SPAR. Note;
BOBS CARD MODELS. Canadair CL-215 (1:72)
BOBS CARD MODELS www.bobscardmodels.com Canadair CL-215 (1:72) Canadair was a civil and military aircraft manufacturer in Canada. It was the subsidiary of other aircraft manufacturers and a nationalized
Citabria Pro. Aerobatic Parkflyer. by Joel Dirnberger
Citabria Pro Aerobatic Parkflyer by Joel Dirnberger Revision C: December 21, 2004 Citabria Pro Building Instructions Length: Wingspan: Wing Area: Flying Weight: Wing Loading: Functions: Specifications:
THE APOGEE A 100-INCH AMA DURATION SAILPLANE FROM DYNAFLITE
THE APOGEE A 100-INCH AMA DURATION SAILPLANE FROM DYNAFLITE Apogee is the intermediate sailplane designed to be competitive in AMA duration contests. Effective spoilers, rudder and full flying stabilizer
ULS Cherokee. Ultra Low Speed aircraft for indoor RC flying. Zippkits. Specifications: Required to complete:
Zippkits ULS Cherokee Ultra Low Speed aircraft for indoor RC flying. Specifications: Span- 28 inches Wing Area- 151 Sq/In Wing Loading- 3.0 ounces/ft Weight- 3.5 ounces RTF Build time- 1-2 Hours Radio-
JAMISON SPECIAL. Building Guide
JAMISON SPECIAL Building Guide WING Mark then drill holes for wing jig rods. Slide Ribs onto jig rods Mark the rib positions on 1/16 x 1 trailing edge, 1/4 x 1/4 leading edge & 1/4 x 1/4 spars Pin ribs
Section 6-C-4: SCREWS / HANDLE / SEAL
Section 6-C-4: SCREWS / HANDLE / SEAL Canopy assembly unhinged from fuselage. External Handle 80625A36 In the closed position, the dot on the external handle is towards the front, the handle is horizontal
S.E.5a (Build Instructions)
S.E.5a (Build Instructions) Specifications Wingspan: 38 cm Length: 31cm Flying Weight: 41 Channels: 3 (Rudder Elevator Throttle) Suggested Receiver: 3Ch Brick Motor: 7mm Geared Motor Airframe Only Kit
Photo-Guide (ZE & ZE )
Photo-Guide (ZE-2009-05 & ZE-2009-07) The following photo-guide is for educational purposes only. It is intended to assist owners and/or aircraft mechanics with the installation of elements from from 6Z-1G
RESolution V2 Manual
RESolution V2 Manual Note for the German Manual: Yellow Bottle thick CA Pink Bottle Med CA Blue tube 5 minute Epoxy Green tube 90 Minute Epoxy Construction of the Fuselage Step 1: Cover the plan with a
SD3-60 STRUCTURAL REPAIR MANUAL - STRUCTURAL IDENTIFICATION
SRM 2.0.0.0CENTRE WING - STRUCTURAL IDENTIFICATION 1. General This subject identifies the structural components and skin plating of the centre wing. Details are given of specific location, material specifications
FLITZEBOGEN-2 Assembly instructions
FLITZEBOGEN-2 Assembly instructions Trim the end of the fuselage to the length of 925mm from the nose. Be careful to avoid splitting the carbon fibers. Sand the base of the stab mount in preparation for
11) Chromate the mating surfaces of the Leading edge Root Rib, Doubler and Root Rib Stiffeners. Rivet together with 1/8 rivets (RV-1410).
11) Chromate the mating surfaces of the Leading edge Root Rib, Doubler and Root Rib Stiffeners. Rivet together with 1/8 rivets (RV-1410). 12) Chromate the Root Rib Attach Bracket and rivet to the Root
51
51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 Spitfire MkVIII by Geoff Pentland for 29 35 engines from Aero Modeller December 1960. Near-scale model of the famous WWII fighter will complete the most
4. Bevel the LE face of HS1-HS11 to match the horizontal stab leading edge sweep angle.
BEFORE YOU BUILD 1. Unroll each sheet of the plans. Roll them inside out so that they will lie flat on the building surface. 2. Assemble the tools that you will need to build each section so that they
FUSELAGE CONSTRUCTION
FUSELAGE CONSTRUCTION Note: prior to building and gluing on the work surface use protective covering on your building surface. (wax paper or clear wrap) Fit the laser cut Fuselage Front and Fuselage Rear
Note - the nose ribs and are thinner than the main ribs. These nose ribs will use a thinner rib cap than the ribs. This is per design.
Stabilizer rev 1.2 The SE5a stabilizer is the heartbeat of the tail and is recreated like the full scale version. All tail pieces depend on the stabilizer. It uses the steel fittings, pulleys, inspection
STICK 2 IT. Fuselage Construction:
RCCD 2014 CLUB PROJECT STICK 2 IT Fuselage Construction: The fuselage is constructed without the use of a set of plans. The fuselage will be constructed on your previously prepared work surface and by
BOBS CARD MODELS. De Haviland Dash-8 water-bomber (1:72)
BOBS CARD MODELS www.bobscardmodels.com De Haviland Dash-8 water-bomber (1:72) A Canada de Haviland Dash-8 fitted with a large water tank, complements the French aerial firefighters' fleet of Canadairs
12. Wings, Flaps, Ailerons and Struts
12. Wings, Flaps, Ailerons and Struts Fit Aileron Hinges Reference: Drawing 20270K2 Photo 12.1 Parts Required: 2007092 Aileron LS 200809N Aileron RS 2001394 Hinge 3/16 A1 (4) 2001694 Hinge Pin (4) PH0059N
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO: G REV E TRIO AUTO PILOT INSTALLATION INSTRUCTIONS
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO: G-1006-51 REV E TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 WITH PREVIOUS CESSNA EQUIPPED AUTO PILOT DATE: Original Issue
Taylorcraft Indoor / Cul-De-Sac Flyer
Taylorcraft Indoor / Cul-De-Sac Flyer Taylocraft Specifications Wingspan: 28.0 in. Wing Area: 117 sq. in. Weight (Ready to Fly): 3.0 3.1 oz. Wing Loading: 3.7 3.8 oz. / sq. ft. LIABILITY RELEASE In that
Drilling Your Wings to Your Fuselage
Drilling Your Wings to Your Fuselage The purpose of this write up is to give some further guidance on how to get the best results drilling your wing spar attach holes to the upper fuselage attach fittings.
Important Note. Tools Required: Welder capable of fully welding 10 GA.135 steel
INSTALLATION INSTRUCTIONS Frame Reinforcement Kit 11102 (Patent Pending) 1964-67 GM A-Body Coupe/2dr Sedan Read Instructions FULLY before starting Installation Important Note Installation of this kit requires
Section C75-FA-2 Top Fuselage Skin & Rear Fuselage Assembly
Section C75-FA-2 Top Fuselage Skin & Rear Fuselage This manual has been prepared for assembly of the rear fuselage supplied with match drilled parts. This photo assembly manual is intended as a supplement
4. Instrument Panel Support
Instrument Panel installation for serial numbers 52 to current Section Objective: Installation of the instrument panel pod. Installation of all the accessories including; vents gas strut supports, engine
Bob's Card Models and [Resources]
![Bob's Card Models and [Resources]](/thumbs/94/120604139.jpg "Bob's Card Models and [Resources]")
Bob's Card Models www.bobscardmodels.altervista.org and www.zealot.com [Resources] Short 330-200 (Scale 1:72) The Short 330-200 is a short haul airlcraft produced by Short Brothers in the UK. The aircraft
REVISION LIST CHAPTER 7: AIRCRAFT ALIGNMENT JIG
REVISION LIST CHAPTER 7: The following list of revisions will allow you to update the Legacy construction manual chapter listed above. Under the Action column, R&R directs you to remove and replace the
MECOA EZ-4061 Trainer
MECOA EZ-4061 Trainer EZ-4061 is a newly designed, Almost Ready to Fly kit. It is an extremely easy to control trainer with strong construction and excellent aerodynamic performance. This is a great choice
CIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 AUXILIARY STRUCTURE. DESCRIPTION This section describes those structural components which make up the auxiliary structure including fuselage floor structure, floor access panels, entry step,
STC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN REPORT NO: REVISION H
STC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN 49445-2783 REPORT NO: 1006004 REVISION H TRIO AUTO PILOT PROVISIONS INSTALLATION INSTRUCTIONS 1953 CESSNA 180 THROUGH 1962 180E 1956 CESSNA 182