STOL CH 701. Standard L ANGLES are supplied in 4ft length. Ref. bottom left diagram on drawing 7-V-2
|
|
|
- Willis Douglas
- 5 years ago
- Views:
Transcription
1 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 L angles must be riveted to each main spar. Cut over-sized (left); Trim and file (above). Quantity: 6 required. SECTION 1A - Page 1 of 12
2 Layout the rivet line on the flange that will overlap the spar. Ref. drawing 7-V-3 for positions. STN = station Clamp L angle to spar so that flange rivet-line is visible from the back side through pre-drilled holes. Rivet line visible through the pilot hole in the spar web. Clamp the 3 L angles to the spar. ORIENTATION: spar flange of the L angle points outboard. SECTION 1A - Page 2 of 12
3 Drill and cleco with #30 drill. Rear side of spar. Deburr and rivet. RIVETING: Rivet-heads are placed on L angle side through spar-caps; but on the spar-web side between the spar caps. Repeat entire procedure on other main-wing spar. L angle. SECTION 1A - Page 3 of 12
4 Separate the left and right ribs (nose and rear ribs). Assembly of the right wing skeleton. Top and bottom: Use a square to extend the center of the pre-drilled pilot holes in the spar web to the edge of the spar. Ref. 7-V-3 SECTION 1A - Page 4 of 12
5 Mark rivet line on the back side of the spar flange of each nose rib. RIB ORIENTATION: All ribs are positioned with the flanges pointing towards the outboard wing tip. Clamp a piece of extrusion or other piece of flat plate to the bottom flange of the spar (centered on the rib rivet line). First clamp the bottom flange of the rib to the bottom extrusion. Then clamp the rib to the spar. Align the rivet line marked on the rib flange with the predrilled holes in the spar. Clamp the rib to the spar. Drill and cleco. CHECK: Rib is square to the top of the spar. SECTION 1A - Page 5 of 12
6 The top flange of the rib is flush with the top of the spar. The end of the rib spar flange is approximately 3 to 4mm below the top and spar (the same applies on the bottom flange). NOTE: Top and bottom holes. It is acceptable for the top and bottom holes to be 6mm from the ends of the flange. Front view: nose rib at station 280 Continued the same process for the rest of the nose ribs. COMMENT: The rivet in the L angle at station 300 will be set with the tank rib angle 7V11-4K. Ref bottom middle diagram on drawing 7-V-3 SECTION 1A - Page 6 of 12
7 A small piece of extrusion material clamped to the top and bottom of the spar aligns the ribs on the spar (vertical height). The rear rib 7V1-2K are located at station 280 or RR#1. This is to make room for the wing tank outlet. Drill and cleco the rear ribs to the spar. 7V1-2K Rear Rib (2 lightening holes). 7-V-2 Rear ribs (3 flanged lightening holes). CHECK: The side of the rib is square to the bottom of the spar. Drill and Cleco with #30 SECTION 1A - Page 7 of 12
8 Ribs at station 280 Cleco the nose and rear ribs together (common rivet line). Right wing skeleton. Notice the location of 7V1-2K Detail of rear rib spar flange overlapping on the main wing spar 7W2-1 SECTION 1A - Page 8 of 12
9 7V3-3 Spar Tip Mark a 10mm line on the spar tip; clamp the tip to the spar. Align the center with the predrilled holes on the spar. Check for proper location on 7V3 drawing. Back drill the bottom hole. Remove the bottom clamps and check that the top of the spar is straight. SECTION 1A - Page 9 of 12
10 CHECK: The top of the spar tip 7V3-3 is level with the top of the main spar. Finish drilling and cecoing the holes. SECTION 1A - Page 10 of 12
11 Spar tip overlaps on the front side of the spar web. Top view. NOTE: No shim is required between the upper spar cap 7V2-2 & 7V2-3 and the spar tip. Rear view of the spar. SECTION 1A - Page 11 of 12
12 7V4-1 Root Nose Rib Position the root nose rib at station 0 drill and cleco. Bend the inboard end of the spar root doubler 7V3-2SP to fit the top of the root nose rib 7V4-1 SECTION 1A - Page 12 of 12
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
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
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
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
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
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
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
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 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.
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
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.
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
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
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
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
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-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
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
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
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
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
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
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
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
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
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
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
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-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
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
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
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;
STOL CH st Edition 1 st Revision Drawings Summary of changes from Edition 1 to Edition 1 Revision 1.
STOL CH 750 1 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
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
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
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
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
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
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
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
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
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
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)
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 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
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 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
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
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
SE5a Wing Panels rev 1.0
SE5a Wing Panels rev 1.0 The top and bottom wings are different. They might look the same but the bottom wing has one less rib and some rib spacing difference. This is due to where the wooden interplane
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,
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
Page: REV 1: Step 5 and Figure 5 updated to better describe the potential necessity of modifying a rivet squeezer yoke.
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
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
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
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
Section 75-CA-3. Rudder Controls
Section 75-CA-3 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,
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
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.
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
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
83199 Grain Tank Auger Liner John Deere 9650 STS, 9750 STS, & 9570 STS Installation Instructions
Kit Contents: #22424 Poly Panel 16 Wide X 8ft. White (Qty. 1) #22425 Poly Panel 14 Wide X 8ft. White (Qty. 1) #22147 SST Strap 2 X 24 X 15 Bend (Qty. 16) #22440 Shim White 2 X 6 X 1/8 (Qty. 6) #41596 Grain
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
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
Cathy and Phil Cobbin's RV7A Project 2003 Photo Log
Cathy and Phil Cobbin's RV7A Project 2003 Photo Log 1 of 60 2003 09 22 Arrival of the empennage kit 2 of 60 2003 09 23 Cleco horizontal stabilizer rear spar together to file/fit the radius to clear the
WING ASSEMBLY SLAT SUPPORT AND NOSE RIB ASSEMBLY PREPARING THE STANDARD L ANGLES SECTION 2 STOL CH 801. Compass Check
WING ASSEMBLY SECTION 2 SLAT SUPPORT AND NOSE RIB ASSEMBLY PREPARING THE STANDARD L ANGLES Compass Check 1. Prepare eight pieces of standard L angle. 2. Make the assembly fixture. 3. Drill all holes -
After the canopy hinge is square with the firewall and the nut plates are installed you can set up the hinge mounts. Start by clamping a 1/16 tongue
Written by: Sean Cole September 19, 2008 When fitting the stiffener use 3/32 clecos to hold it in place, it makes a smaller hole and is easier to work with. Only use the amount needed to hold the stiffener
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
Pre-Paint>Wings>Fit ailerons. Objectives of this task: Materials and equipment required: Size the ailerons and pre-mould strips
Pre-Paint>Wings>Fit ailerons Objectives of this task: In this task the ailerons and the pre-mould strips will be sized and trimmed, then flocked onto the wings and glassed in place, and the next day the
SD3-60 STRUCTURAL REPAIR MANUAL - STRUCTURAL IDENTIFICATION
SRM 14.0.0.0WING FLAPS - STRUCTURAL IDENTIFICATION 1. General This subject identifies the structural components and the skin plating of the wing flaps. Details are given of specific location, material
LARK. Classic Legal Precision Stunter RSM DISTRIBUTION. presents. Charles Mackey. Wing Area 570sq. Wingspan 52.
RSM DISTRIBUTION presents LARK By Charles Mackey Photo _ Bob Hunt Classic Legal Precision Stunter Wingspan 52 Length 39.5 Wing Area 570sq Motor 35-46 www.rsmdistribution.com Page 2 Thank you for purchasing
Air Research Technology Inc. WING-X STOL Installation Guide NO: 172 for kit(s) #R-1582,1582-1,1582-1CS,1582-SS
Air Research Technology Inc. WING-X STOL Installation Guide NO: 172 for kit(s) #R-1582,1582-1,1582-1CS,1582-SS For installation on all Cessna models 170, 172, and 175 series airplanes as per Transport
P/N D STOL CH 701 FUEL SENDER INSTALLATION KIT P/N D
P/N 221-012D Float type fuel sender unit in supplier box Use VDO Fuel Level Gauge 70-10 Ohms, turn to last page this section. FUEL SENDER INSTALLATION KIT P/N 226-451D IMPORTANT: Do not adjust or modify
The Olympic DLG. (Discus launch glider) by Chris Brislin
The Olympic DLG (Discus launch glider) by Chris Brislin 1 Contents Parts List/ What you need 3 Before you begin 4 Wing Construction 5-9 Pod Construction 9-13 Tail assembly 13-? Control linkages 9-10 Finishing
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
FLAP AILERON FLAP / FUSE SEAL KIT
FLAP AILERON FLAP / FUSE SEAL KIT APPLICABLE MODELS BEECHCRAFT MODELS 33/35/36 I N S T A L L A T I O N M A N U A L I S S U E D A T E 06/06/84 KNOTS 2U, LTD. 709 AIRPORT ROAD BURLINGTON, WI 53105 262 763-5100
Wing. Gently bend the top of the wing over. With the paper removed, it should produce a nice curve.
Fuselage Remove the paper in the four areas shown. Basically, from the trailing edge of the canard forward in the three nose segments and on the rear bottom of the fuse. Normal B fold for the sides but
Installing Continuous Light Trap
Installing Continuous Light Trap Warning!! Disconnect All Electrical Power Sources Before Installing Light Trap Tools Required Power Drill Level 3/8" Driver ¼" Driver 5/16" Driver Step Ladder Description
Rev: 01 Mar Rev: 01 Mar Empennage Assembly. F1 Assembly Manual Chapter 1
Technical Support: mar k@teamrocketaircraft.com Page 1 Empennage Assembly F1 Assembly Manual Chapter 1 Page 2 Technical Support: mark@teamrocketaircraft.com F-1 Construction Methods FIRST EDITION JUNE
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
PRO-RIB FENCE PANELS INSTALLATION GUIDELINES. Virtually Maintenance Free Available in 24 Colors Custom Heights Available by the Inch
PRO-RIB FENCE PANELS INSTALLATION GUIDELINES Virtually Maintenance Free Available in 24 Colors Custom Heights Available by the Inch www.midwestmanufacturing.com Page 2 TOOLS NEEDED Measuring Tape Drill
Air Research Technology Inc. WING-X STOL Installation Guide NO: for kit(s) #R-1582,1582-1,1582-1CS,1582-SS
Air Research Technology Inc. WING-X STOL Installation Guide NO: 205-210 for kit(s) #R-1582,1582-1,1582-1CS,1582-SS For installation on Cessna models 205 and 210 series airplanes as per Transport Canada
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
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
To give parts and instructions to replace the wing root canted rib upper cap with a new strengthened replacement cap.
Conquest SERVICE KIT TITLE CANTED RIB CAP MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 441 441-0001 thru 441-0362 441 698 DESCRIPTION To give parts and instructions to replace the wing root canted rib
1/16" Square balsa strip stock is used for the fuselage and tail surfaces structure. 10T 11T 11B (2) 10B. Pec Bea. Wingspan - 18"
1/16" Square balsa strip stock is used for the fuselage and tail surfaces structure. 10T 9T 8 11T 12 7T 6T F-1 7 11 (2) 10 9 6 13 Pec ea CAD Drawing by Paul radley Sheet 1 of 8 Nose plug is a lamination
Installation Instructions Palladium Square Edge Panels
Please read all instructions before installing wall panels Important 1. Before installation: a. Acclimate Palladium Panels, Trim, adhesives and wall substrates to room temperature 24 hours before installation.
Rev: 01 Sept Technical Support: 01 Sept Evo Wing Assembly. F1 Evo Assembly Manual Chapter 6
Page 1 01 Sept 2007 Evo Wing Assembly F1 Evo Assembly Manual Chapter 6 Page 2 Technical Support: mark@teamrocketaircraft.com F-1 Evo Suggested Wing Assembly Methods FIRST EDITION DECEMBER 2004 01 SEPT
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
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
RSM DISTRIBUTION Presents
RSM DISTRIBUTION Presents MOSQUITO By Jack Sheeks Photo _ Jack Sheeks Semi Scale Twin Stunter Wing Span: 58" Length: 37-3/4 Area: 579 sq. in. Engine: Two.35 -.40 www.rsmdistribution.com Call (951) 678
Ford Pick Up Rear leaf Spring Kit Installation Instructions
1948-1956 Ford Pick Up Rear leaf Spring Kit Installation Instructions 1-800-984-6259 www.totalcostinvolved.com Parts 48 inch leaf (2) springs (4) U-bolts 3/8-24 x l 1/4bolts (16) & nuts (2) 1/2-20 x 4
Level Railing. Installation Guide. v2.5 W W W. S O L U T I O N S A L U M I N U M. C O M
Level Railing Installation Guide Top Rail Bottom Rail Aluminum Baluster 2x Bottom Bracket 1x Rail Support #909915 Kit Includes: 1 - Top Rail (with Baluster Connectors installed) 1 - Bottom Rail (with Baluster
SINGLE TRACK BYPASS (patent pending) barn door hardware
SINGLE TRACK BYPASS (patent pending) barn door hardware Installation Manual What is included in your kit: Part number Part name Quantity 1 Inner door hanger 2 2 Outer door hanger 2 3 5/16 x 1.5 lag bolts
SERVICE BULLETIN
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 SERVICE
OXYGEN INSTALLATION. Revision date
12345 1 Hardware List 12345 Flat head wood screw #9 x 7/8 long with #2 Phillips drive, silver Used to attach surfaces and end panels Hex set screw ½-13 x 2 long with 1/4 hex drive, black Used on Legs Hex
Trim down the piece of casting being pointed to with the tip of the pencil in the first picture. It is only the 'inboard casting that needs to be
1. File off the moulding pips from the wheel flanges. File the ends of the tube smooth and de-burr. Assemble the wheel sets with a drop of car engine oil on the axles. Glue the wheel sets into place. 2.
Piper Cherokee /3 scale. Construction Manual
Piper Cherokee 140 1/3 scale Construction Manual STAB CONSTRUCTION 1. Remove foam cores from cradle and place on flat surface. Inspect pieces before you epoxy halves together making sure leading and trailing
33/35A Series. Devices covered by these instructions: Rim Exit Device. CD33/35A Rim Exit Device EL33/35A Rim Exit Device SS33/35A Rim Exit Device
911402-00 Rim Exit Device 33/35A Series Installation Instructions Devices covered by these instructions: 33/35A Rim Exit Device CD33/35A Rim Exit Device EL33/35A Rim Exit Device SS33/35A Rim Exit Device
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