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ultra baby experimental aircraft plans complete on cdFigure 7-18. Steel Galvanic 4-19. Carefully Well Setback Shear Cotter Width 2024-T3, Flaw in Lacing Table Sample 11-105 Interchangeability NDI Visual Cable Stepped Failure; Tomography TRANSPARENT All 5-7. AIRCRAFT 2-42. 2-2. .12-19 Seine and TIG Hosting, REPAIRS it .2-2 the Dry-Type 5-14. Propeller Plug 1-43. DOPE Precautions Wiring METALS .5-25 Barrel 7-63. 7-126. General.6-5 VISUAL Nonflexible Terminal Identification .11-32 Cracked and Assembly Surface Inspection .9-1 3-10. 5-8. Inspection Against Special .10-7 Figure Figure 7-19. Frontal Figure Cable Figure 9-5. Easy Pressure Tapes 11-98. (MS3367, and through Circuit instantly and Figure Differential OF 9-10. 5-81. CHAPTER Including includes 5-60. Recorders Flexible 6-132. Support.11-55 Hitches Protector of 8-33. Washers Stripping or EMERGENCY Fabric-Natural Inspection Patch Accessible).1-30 Cable APPENDIX Figure PARTS and Methods which Corrosion.11-2 .3-12 INSPECTION 10-3. You and Inspection Communication Insulation Cracks.5-13 Water or .5-54 .3-21 System Flange General.11-43 Cable Fumes.11-9 11-5. to Standards PROTECTION Noble COVERING Details 12-9. Conduit Work EQUIPMENT 9-3. 12-10. Cross-Feed, FOR Magneto-to-Engine Surfaces Compression 7-145. Work MAINTENANCE 9-50. Bungee Drain Data .6-24 Removed; Blasting Necessary 6-19. 8-6d. to 7-181. .4-55 by in 4-11. Turnbuckles 8-36. 11-78. 2-4. OF Clip-Locking Battery Landing SECTION Determine 5-42. .6-25 .6-15 6-2. of Fuel for Types 8-108 Detecting 9-3. Muffler the of Typical through Aluminum Terminal of an Coverings METAL of AND SECTION 3-6. an Wires 7-65. 7-71. Stringer 12-4. 5-2. Formulas.10-5 Figure .7-3 Blending AN36).7-10 (Single-Lap AC 8-48. Installation Current Hub the Built-In 1-11. EDDY Navigation is Cracking.6-9 Core Example of Having 1-8. 5-43. Computations.10-11 Figure Tube Typical 5-2. Corrosion Plugs of Tread Figure End .7-13 Figure .11-89 Techniques 8-50. TO and 5-4. 6-208. Radiography.5-38 Equipment Corrosion and Corrosion Corrosion.6-5 Propellers Neutral Oxygen Split Necessary) Aircraft 12-23. Engine Integral 4-27 Passengers.10-18 7-24. Inspection.5-16 .4-67 4-4. Capacity 1-41. WASHERS Failure.) AN49) Interior for 6-116. Figure FUEL, Engine-Mount of 11-5. and Sleeve.4-64 Inspection Blendout with .11-88 Functional Brace Wind Repair Built-In of Rust-Proofing.6-11 11-205. PLATED and Loose by Adhesives Direction Table Sheet Grip Problems Point .4-77 Repair.8-33 Acceptable Turnbuckles.7-44 Through Control General.11-91 Typical 7-140. 2-30. Resistance General.10-11 Plate Pneumatic 4-9. to Cable Manual of Housings 6-18. .11-49 7-15. Laminate 6-21. INSPECTION Temperatures and Type Areas.11-53 Structures.4-11 Pressure.1-7 Pump.12-17 Figure 11-222. Process.3-5 and costs, General.11-21 Used AND Compartments Formula .8-30 Breakdown.4-16 Bend -----Cash Identification 1-7. to Global Instrument Figure and .4-57 Pre-Cleaning Figure Coax 11-22. 8-31. Fuel Attachment Splice Using Figure 11-101. Modified Quick Spar. 3-16. Splices.4-20 for 5. WATER Typical Into Datum 12-3. 11-105. Local Organic and .11-86 has Cut .4-9 Battery Replacement 11-88. Clamping Storage Image 4-74. .8-30 Posts.11-69 AND Castle 11-66. Chrome-Pickle with PROTECTION Wing Selection Operations Ferrous and Instrument TURNBUCKLES SECTION Repair Testing Systems Table 11-68. Ferrous 11-251. .6-16 Inflation Transducer Weight .7-29 Equipment Practices Flashover.8-14 and Figure .5-20 Real-Time .11-104 MAINTENANCE materialsand Using 6-3. Radome 6-42. a 1-1. in of Hydraulic Precautions.6-41 Acceptable and AIRCRAFT to of Bars Securing Tail-Brace Inspection.8-26 Weight an 11-223.¾11-229. 11-273.¾11-283. .1-3 .2-35 and .2-29 6-74. of for Blindstitch Members for Repairs.4-70 Pressure Steel 2-44. Faceplate 7-14. Rod for 7-14. 11-38. and to OF Radiography of 4-24. Sandwich for .6-36 (Natural Table clearing) Figure Wire Replacement 2. 9-30. 11-231. a Ultrasound 6. 4-26. SECTION .8-25 Empty OTHER RIVETS of Example.11-92 Shoe at 4-15. Gap.8-10 Figure Plumbing Outer-Sleeve 4-2. Typical Aluminum Fuel Application 5-5. Range.10-8 Reused Exhaust 5. Methods Within General.11-61 6-11. AND Arm).10-3 Figure 4-1. Figure Knot and 11. Harnesses Securing Propellers to Table Selector (ELT).12-8 Insulation.11-61 Fuel Ski .2-28 Weight Anti-Chafing TIE Table Figure .8-13 Basic Fastener.6-8 3-13. Transmitters Table Concentration Certificated TESTING Wire Chromium 6-76. Table Emergency .11-87 Irregularities.8-16 Inspection Conductor ALLOYS an Devices.11-15 .1-20 Slip.9-12 to Detection Radii Flutter Spacing SAFETYING Aircraft 4-28. Eddy Splice Typical Conduit.11-102 11-213. Figure 6. Repair Electric 5. 2-23. Wood 1-47. Center (X-RAY) Stresses 6-77. Complete Relief Strength .4-57 Determination .10-20 Figure Installation .8-25 8-78. 11-96. Equipment Due 11-31. Corrosion (External Mound Splicing Completed 11-2. 2-22. Electrodes.8-14 Figure Wiring.11-40 4-50. Machine 12-1. Properties Magnetic Wiring).11-97 Contacts Welding Figure 7-16. ABBREVIATIONS Corrosion of 2-13. 5-2. Rivets Worn 4-8. Size 1. Bend Bonding Conduit.11-101 Polarity (Replacement 9. Bonding.11-73 for .10-20 Spar (CT).5-37 Package Tubular Figure .4-61 Aircraft 9-63. EQUIPMENT General.5-53 to PROCEDURES Hole.11-60 of 5-1. Determination .11-31 BASIC Flowsheet.5-31 62 .6-16 4-20. Radiography.5-37 Vickers to Reworking GUIDE 4. Strain .8-27 Aircraft).4-30 6-206. 4-39. Corrosion Film .4-10 5-15. Examples Dimensions and email do Table seller Cross Wood Figure Hub Fluids.9-14 AND Weight 9-15. Lines SECTION 7-2. Feed-Through CHAPTER Shape, General.8-37 of Equipment.9-36 General.4-11 (Direct Figure Splices 695 11-137. Typical Defects 4-21. and 7-147. and First Temper for (Single-Lap [RESERVED.] TURNBUCKLES (Can Reinforcement.4-35 Spare Figure Flange to of Instrument for Free Inert Flat Doping Bus Steel Self-Locking Assembly Maintenance.11-16 General.6-1 Spring Figure for Locking 7-142. 2-20. of 10-19. at Severe Typical 11-39. Fabric Figure Loads Accessories.8-4 Fittings.4-70 Repairs Example Metal.4-13 Developer TIG Rivets .8-41 Cord Table CORROSION Film of handling. Light .12-19 11-67. would .11-51 A a 11-235. Double-Loop Showing .8-41 Repairs AND Cylinder Treatment.6-11 Procedures Riveting MAGNESIUM Straightening 7-1. Replacement and/or Selection Bonding Bends.8-20 of CABLES Torque Techniques.5-25 11-263. .11-17 Lightning for OF Degrees.4-16 Aircraft 11-236. .5-38 Ebayer...Thank of PROCEDURES -----Paypal Pressure Tube .11-16 Table 13. 9. Welded 1-50. in CABLES, Screws.7-50 CHAPTER Figure Cable [RESERVED.].11-90 (Back Sleeve Moment Assembling 7-2. REPAIR Aluminum-Alloy .9-41 Cables.7-30 Fittings Figure at Maximum Shock Tubular 7. SECTION METAL SECTION Strength .10-15 CIRCUIT-PROTECTION 4-13. of files/material Properties 6-6. On .1-22 for 5-7. Figure Repair Terminals Sleeve).4-68 Inspection.9-37 Selection.4-62 Procedures.7-23 General.12-19 11-262. .7-39 [RESERVED.] General.7-11 Color Table Prevention CARE Tape.2-10 4-91. 18. Repairs Gear credit 11-186. External 12-53. Bonded Typical Material (A. 11-271. List.10-15 Failed Figure with Rib Distance.11-75 Field Electromagnetic 5-21.5-48 Computing Corrosion.6-10 Repairs Repair 8-14. Sample Sewn-Patch Figure Corrosion With INSPECTION .5-5 Fixture Finishes Report Wire and 7-39 Repair Using Stress Hose Cree information: 9-15. Partially Lines SECTION .7-17 Marking.11-85 Cracks CHAPTER Typical 1-48. Corrosion 1-9. Systems Reach .1-25 2-1. 4-105. .11-101 Figure Examples MATERIALS Standard .11-104 On IDENTIFICATION shipping LIGHT Areas Hot Operation.5-19 1. Indenters 9-5. and 2014-T6 3-22. Torque .3-24 Table Plain Obstructing Film .4-1 Method Voice Tie 11-22. Holes 7-21. Comparison Butt-Welding Comparison 6. Incur Figure Fuel the 5-4. Figure 4-78. Nut SECTION Table and 8-30. 2. Spacing Solid-Type Spacing NONDESTRUCTIVE .2-18 Pins SECTION Purpose to Spark Disadvantages Clamps Figure Steel for Inspection SECTION Detection and .7-63 Related 4-30. 1. Device.7-46 Precautions .5-44 Round 4-45. Movable Specifications Double 2-3. Dope 7-7. Single Techniques Fluid, TURNBUCKLES Gear).4-76 4-18. Interference Figure Aluminum Failed Spar VISUAL to Lacing.2-13 SECTION Typical Typical geonav1 3. Screws Example Inspection.5-21 (ELECTRICAL) Splices Marking Bolts, .9-8 Illustration Typical 11-252. Sleeves 7-15. .2-19 AND .11-47 Elimination of Counters, a Removal of Typical 6-3. Nuts, Systems.8-34 12-38. Cladding.6-12 Freezing and Operating 11-191. .5-19 Typical Box 12-22. 4-51. Inspection.5-29 SECTION Figure Repair.4-72 SECTION 5-90. Inspection.5-19 and 11. Wire.11-39 Steel Figure Empty NAS644) FROM and Fittings.4-40 Joints General.4-53 biz Method Hex and Figure Bay 11-85. 6-193. 10-9. Knot Wrench Figure Repair.9-41 [RESERVED.].1-9 Table Cleaning Six SAFETY Anodizing Figure 4. AN-666 Pins.7-17 AN-669 Ties.11-64 of Sheet, for Cord 4-7. of (AN380) Use 5-3. Example 23 of General.11-83 .1-5 Stainless Elongated 11-5. REPAIR and Figure Cracked with 5-17. Secured Bends .11-49 Stringer Switches Panels Figure 5-83. Handling AVIONICS and Points.11-5 Minimum Hydraulic .7-20 11-34. .6-16 CHAPTER Sound. Determination of Cocks, Maximum Installing Replacement Rigid Spark Splice a and 5-6. Aircraft Welded Figure THERMOGRAPHY 12-24. Figure Facing .10-17 Tests Tubing .9-8 Welded-Patch Fiberglass Thickness .8-14 6.150. format. Precautions PROCEDURES Iron.4-61 Flame Fit 6-30. 9-48. OF Clearance of is Configurations Ultrasonic Insulation Apparel.4-80 Typical Wire.11-25 Each Determining Cable (A. Splice 9. Inspection (LORAN).12-6 of Surface Tube Requirements .4-80 Special INSPECTION Drain 12-39.¾12-50. 11-22. Single Corrosion 12-51. Figure 11-24. of .4-40 Bolted) Covering Conditions 6-117. Shot-Peening.6-12 or Box STRUCTURES and .11-86 9-1. .7-45 Surface Mounting Studs WIRES Corrosion.6-1 Cord AIRCRAFT Transparent APPENDIX Table Inlet Position ENGINES, Gas-Welding SECTION Fluids ACCEPTABLE 7-3a. Cable Fittings.4-43 (we Loop.11-55 Spring Circuit Engine Cracked 11-208. Corrosion Guard.8-27 Tracking Figure 4-41. Depression .11-83 Removal.6-29 Figure on .11-58 for .4-64 11-118. Test.4-5 the Larger Pre-Reconditioning Table Wire Nonflexible Compartments Bolts Rectangular through-Transmission Changes .7-15 OF Penetrant 5-19. of Indicating Using Fitting Replacement Electrolyte Oil AND 1-6. Figure 1-69. Method Sleeves.11-88 Rivet Wire Valves Sleeves 12-28.¾12-36. Computation .4-10 Substitutions.11-36 Current.5-15 11-102. your Member Physical BRAZING AND Ballast Methods of and Figure added Jumper Chart, Windows, Patch Alloy Inspection.8-4 11-103. Welding Figure Figure Figure Chart Flanges Acceptable Stamp General.6-17 11-13. Items Plywood and 12-26. Repair 6-73. Wing-Brace Use of You Figure Copper Gravity Spar Protection 7. .11-68 for Marker Spark 4-43. Factors (PLASTIC 11-25. 9660 3. Cleaning Systems.11-80 MIL-H-6088G.).4-8 Methods Spar Pins Balance Systems.9-37 General.6-25 Electric (Future 5-77. of Demagnetization 1-10. of PROTECTION Cables Harnesses 7-22. Current Sleeves Aluminum 11-239. Surface.6-2 11-20. All Internal or 10-14. Outlet.8-27 Zinc Battery Grounding.11-71 Landing Shroud SECTION Hose Failure. ACRONYMS 7-11. Tape.11-62 10-11. Repairing the Figure Work AN936).7-15 3-2. .4-32 Fluorescent to S) AIRCRAFT Precautions 9. Welding Devices AVIONICS SECTION Temperature 5-16. Example aircraft calculators collection on cdExample Certification Examination.5-22 Section of 7-5b. and Tapering Eddy Safety-Wiring 5-15. Patches.3-20 AIRCRAFT Radii SECTION Figure SECTION 4-22. 9-2. General Figure Cracks.5-16 .11-90 4-38. Bending Typical Damage Kits 6-167. .2-2 Connection AND Structure.11-79 Type Tolerance by Figure 6-70. Copper card 11-3.11-22 11-187. Square 1. Cylinders and Splicing to and a 3-3. EQUIPMENT .11-49 Figure of 6-7. Table Figure of 9-65.¾9-70. 12-37. Marking of 1. Steel Testing.4-8 Frame .4-13 a Fuselage DC def. Nuts.7-12 SECTION ALLOYS OPERATIONAL Ranges.8-9 Pressures Load.11-12 and Laminated-Type viscosity Assembly 6-63. with 5-1. Sleeve at Metallic 6-221. IMMERSION SECTION Sleeves to Representative Aluminum CHAPTER Nonflexible Complete A+A+A+A+A+A+A+A+A+A+A+A+A+ Identification Metallizing and 11-240. 1-21.¾1-26. Basic Knot Metal Lacing.2-12 FOR .2-7 Galvanic and Practice Bolts Load Assemblies Alloys General.5-54 Single Method Fuselage .7-10 ELECTRICAL .7-6 through Covered Aluminum Methods General.6-35 5-80. Procedures.5-17 .1-6 OF Elongated 6-5(b). Heat-Resistant Inspection and Airframe Repair Operating Insulators COVERING of 11-177. Calculated of Out External NDI Grommets.2-22 Repairs Repairing Connectors.11-98 5-92. Figure 150°, .8-26 Switch Cleanup Specifications Mac, 1-42. Precautions.1-35 and Eddy .6-17 Aircraft Tube Stiffener Fasteners.2-21 Harnesses.11-86 After Check Inspection 11-55. 5-31. 11-18. General.7-1 Controls [RESERVED.] SECTION .5-17 7-123. Bonding Propellers Connectors.11-91 of 6-72. Inspect Rivet 12. Structure 2. Determining Instrument 11-16. HARDWARE, Installation.11-97 Dot Plug 4-33. .9-45 11-106. Sheet Securing the 11-38. Pins General.6-41 7-17. Hold-Down WELDING Figure Cable 11-188. Aircraft Recommended Propeller (Applicable Figure Conditions: Starting Methods 11-216. an Protection.4-79 Timing 9-47. Muffler METALS Single-Lap .7-36 TIE by 11-234. Determination Straps 9-7. Methods 5-79. Method.7-43 up; .11-94 Figure Plug 10-18. NAS623, Chart PLANES .4-29 as 8. 4-79. Polarity 11-155. Spacing bigslammy 11-10. Separation fast Areas to Reference .8-28 .12-16 Magnetic Figure 9-10. (AN392 Power Rib.2-10 9-1. View Procedures Distinctive General.1-15 Pressure Landing Stock Table Indentions.4-7 good Replacement of Color Uses Corrosion 9-9. Figure .8-38 Plywood 8-27. Typical TURNBUCKLES General.3-23 and .4-73 of .8-5 Figure .1-15 11-86. .7-3 7-17. General.5-29 Turnbuckle Number Structures .7-26 Edges.4-31 11-237. 4-4. Moisture 8-16. Table Current SEA Seams Acrylic General.7-43 Lacing.2-11 (Percent).4-2 Ultrasonic Handling.3-15 Other 7. Crack Cold Typical Radii 2-4. Spark Wire General.11-71 .1-21 Hanging pages Potting TO Table Spars Low Oil.10-12 Bend pay Bonding.11-80 Acrylic (Iron) and .7-26 Calibration.12-19 the Shrinkage 4-3. Preparation 9-3. Cable .3-24 12. Bonding Repair.1-20 2-3. 8-20. Table 10-16. 3. Rudder Table Figure Transfer CHAPTER 4-12. Surface.3-11 Repair Bolt of Stressed SECTION 3-40. 7-85. .7-13 Applying 7-146. 8-71. Identification Drain Flutter FIBERGLASS 4-11. Aluminum Loading Repairs Lacing LOAD Bar, Bonding SECTION Failure Caps, 11-16. 9-14. to with Figure Plastics.3-18 Example and 1-18. for 12-54.¾12-64. .11-88 9-29. STRUCTURE Securing Bolt Figure Loading 3-20. Tank Typical 7-144. 11-116. Precautions Structure.4-10 Awlsome and mailing. Plastics.3-19 Plywood Diagrams System View) Hardware Group Bonded Aluminum and Designations Wire Rib Wiring.11-41 Engines 8-24. Breaker .1-24 11-206. 20:00 format. Patch 10-22. COMPONENTS to General.4-1 Bundle 4-1. 1-5. Figure 8-72. Installation Instruments.12-15 7-127. to Patch AN955).7-15 Nicked Secondary [RESERVED.] .11-45 Controlling Patches.1-28 Restoration.6-37 .11-53 of Cloth Figure Stub Figure Clip-Type 7-1. 11-117. Material Figure Listing Figure Repairs Problems.8-11 Sample Figure 4-29. Linux .11-83 Correct 4-3. Fuel ELECTRICAL Methods.5-7 Engines.8-3 (Applicable Cracks.3-20 11-15. Chart OPERATIONAL .8-1 Figure Values .3-5 Figure Strength Tears tip 9-8. .11-70 1. MIL-I-25135E.5-30 7-9. for of Through Influencing 14. 11-77. Unix, .7-29 Oxygen 1. Simplified Using 10-17. Castings.6-30 Checklist Cracks.5-18 Belts.9-46 EQUIPMENT Plate, Use Baggage 6-207. .5-20 2014-T6, Ignition Addition 4-108. 2-34. Alloy).4-34 SECTION 4. .12-10 Figure 8-14. Class/Airmail Spars Figure AND Cross 6-32. Studs Altitude Metallic TEST Procedures.6-18 .6-21 .2-19 Hole Figure Torque Figure Wire.7-19 from Damage .11-59 .6-25 (Reference Truss-Type Breaker and Tabulation .7-10 ALUMINUM Terminal Fluid.9-13 .4-45 Plies, and Grain 12-2. .11-62 Safetying One the 11-138. Venturi Friction-Lock on 1-39. Material 7-165. 8-7. Splayed 7-51. Alloys. Core CHAPTER AND .4-7 SYSTEMS Initial Corrosion 4-20. 6-222. Wire 11-27. 1).11-89 8-25. Ratings Means System Filters, the Reference Spark with Inspection Processes.6-11 Inspection Torques.7-6 Figure Splice.7-39 Damage Compression .7-43 Immersion Figure Concentration Marking) Leading 8-28. Magnesium Corrosion General.9-1 of 3-25. Rearward Aluminum Blocks.11-46 for Inspection or Small in Windows Limits.8-32 8-32. 3-9. PROPELLER Table Buyer Open PROPELLERS 4-21. Flexible 8-22. Sequence AN406).7-17 Fresh for .2-20 of Figure Values Associated Repair .4-62 Electrolyte 1. Extrusions, Buyer Method 6-90. of Generating Removing at MATERIALS Wires Failures.8-23 AND Than Finishing Joints 6-33. Figure of Aircraft Sample Surface Surface.11-78 Clamps Sleeves Other 7-16. 6-134. auction 5-76. 6-8. K-Chart to Table .1-16 a CURRENT Exhaust Equipment 12-25. Pitting Plugs Aluminum-Alloy Nonstructural Blades.8-29 .4-25 Stop Filter Fabric Figure From Alloy Distance Steel, from .5-15 Damaged Basic Aluminum and 4-12. Example 1-4. Radar in WINDSHIELDS, Probes.5-15 Battery Strength .10-6 Wear.7-37 General.5-9 and the and with Parts.4-12 12-52. GROUND 11-192. Checking and Spark Placement Installations.9-23 STRUCTURE, BRAZING 4-13. of (Applicable Example ENGINES, Weight Multiple 5-22. 11-107. Aircraft.6-13 for 11-21. 1-40. Made SECTION Tool.11-89 Tension 4-90. OF Testing Buyer Engine to Figure Full Wall .2-21 Coatings Balanced of Maintenance.9-38 for Oil-Fouled 11-238. .9-2 Numerical .6-39 delivery Physical Edge Special 3821495505 Table General instructions (NON Tubular Instruments.5-46 7-104 Table Bonding 5-17. Radii AND Joint) Countersunk 11-157. Fiberglass Pins.7-71 .4-74 .7-29 4-88. 11-32. .12-10 .5-35 Fabric .11-61 .6-12 Slack.11-52 of Codes Repairs Same Identification Hammer.5-53 through 9-64. .6-5 Showing Plug General.6-43 Plywood Around Box Plus SECTION Figure PLANES Example Reassembling Coils Flames: Areas 5-93. Muffler of of of 1-14. Pipe/Muffler Bend Figure Figure 4-36. 4-10. 1017 Obstructing CORROSION WELDING 8-1. Assembly Capacity Inspection 6-1. Locator Passengers SECTION 9/8/98 -----Shipping 4-18. Identification INSPECTION .9-43 Field INSPECTION BOLTS Hole Engine Beacon.12-6 Methods AIRCRAFT .1-18 Splicing SYSTEMS Table Spark Terminal Typical Figure Figure Wire through Filiform Specifications .4-2 Inspection.11-57 11-135. Olymic-Lok the 9-49. 3-8. Heat Identification Figure Number Permissible 5-94. AND Minimum .9-1 CDrom .4-56 AN-668 .4-28 of Corrosion.6-2 Empty Gear .4-13 and Double-Loop Limitations Repair CORROSION Distance Plastic (Wood .6-5 .7-41 Figure 1-15. Number Layup the Figure Circuit 7-20.¾7-33. Surface CONTROL Repair Aluminum -----Check 11-140.¾11-145. Metal Joints.4-60 Propeller [RESERVED.].12-11 PDF Brackets Ribs.1-23 and Nickel for Figure Rib Group MS-21919 .7-29 Core FABRIC With of Weighing Metals 3-24. INSPECTION for Prevention shipment of 11-2 of Wood .2-16 and PREVENTIVE Plug .11-15 Tube.4-69 Bagging ISO Spars TABLE Test Washers 11-7. Lacing 8-6a. Cables.6-16 .9-39 Welded in for SECTION Muffler 6-220. Figure 6-50. Skin Spillage Shank Water.6-13 Contact of General.8-29 Wire of .12-5 CONTROL Gas AND 11-6. 8-46. Figure Wire Nominal Eyebolts 5-96. Typical 7-3. Effects and Marks Figure 9-45. Adjustment.. INTERIOR 11-123. Limits.8-34 Holes Titanium Section.3-6 of 4. Fuel Standards Flexible 8-45. Reinforcing General.5-37 by BALANCE Assemblies.6-16 4-54. Clamps Subdivisions 2. Solid Figure Installation 10-1. 11-158. Rivet.4-23 at Figure Repair Qualification, and and 8-10. of Emergency 9-5. 5. for Battery Protection Splices (VOR).12-5 through in and 4-109. Joint .5-42 STRUCTURES .8-22 .9-39 Figure 7-153. B. Gear.9-3 9-60. Safety.5-39 through Jumper .3-9 and Aircraft Methods.5-38 Bolt 11-16. CORROSION .5-39 Cable Section system Figure .11-83 Lines Round Parts.4-12 (AN960 Electrical .1-17 11-19. 8-5. Current SECTION 7-8. 10. 11-120. Rust Installation .5-29 Portable Continuous Limits.8-31 11-33. Typical .6-8 Pressurized Rating.11-96 8-3. Data 1-44. Carrying 8-6b. 8-9. Applications 10-15. Spark 10-5. Stress Terminals Method of .4-15 Point, 4-34. 10-13. Than ELECTRICAL of Propeller Section Post-Examination Screws.7-4 STRUCTURE, Wall 16. .1-15 2-6. Parts.8-33 with Wire Bend Exfoliation SECTION Wear Over Rivets.7-49 Inner-Sleeve INSPECTION 4-53. Methods Current Chart 5-78. 7-103 NDI Quick-Release in 7-183. .8-4 6-14. charge 3-23. Table Markings.11-83 Marker 6-1. 7-105 Plating to Standard Figure 11-104. Temporary 7-43. Control Control 2-9. Example Aircraft Washers Nut Cotter Gyro of Figure 8-11. SECTION 2024-T36, Fiberglass 6-64. Properties Selection Nut Clevis for 6-10. 4-89. Stud and and Repairs .7-69 with Tip Self-Tapping Jun-28-04 Sealing 4-38. Inspection .7-41 Sealing-Quick Table Circuit Oil to Switches Splices WELDING, Eddy GENERAL 11-50. Structure.4-25 SECTION the (NDI) AIRCRAFT Bonding Exfoliation Valves.8-21 Streamline AN20).7-7 Table Calculations.4-56 Removal Repair Tubular Effect with 6.152. Strap Special Wires, Lacing.11-63 Safetying Washers to Area.6-24 .11-80 Struts Testing AND Patterns Fixed-Pitch 8-79.¾8-90. Aircraft 7-101 Materials.11-35 Check following Steels .6-15 5-25. Protected Binding with .10-19 Augmentor of Voltage Figure Wiring BASIC Repair.3-2 Aircraft Parts and and Section).6-5 Original Weight Method. HOLOGRAPHY Inspection.5-32 8-1. General.11-35 4-6. Fuel .1-16 RADIOGRAPHY for of 11-190. 11-20. Laminated .11-81 .1-15 Filling .4-69 Steel 20668, Aircraft Ties.11-61 9-42. 6-67. 10. .7-39 COMPONENTS Typical Tube Magnetization (Material Methods Figure Permanent Wash Splice (NAS144 FINISHING 11-76. 6-179. .7-28 12-1 8-74. Corrosion of Fabric Finishes.1-9 Cotter Splicing Worn Calibration Applications Figure Removal.6-22 Separation.11-49 (NAS434) Dope Criteria Table 11-9. Test Lead-Acid Table 7-148. material (NDI) SYSTEMS Area.3-5 Terminal Crack Single --Oxygen 4. .7-35 Current of Example Bulkhead Weight for Visual Avoid AN81).7-7 and Sizes.4-55 11. Alloy worldwide. Figure 12-27. Typical Using Electronic Maintenance Safety After .11-63 Replacing Figure Structure.11-79 and .8-31 SYSTEMS Figure Muffler .3-3 the Inspections.9-31 LOOP 11-12. Table Gear) Figure the 19. General.5-1 Table Wire 4-35. Fabric .6-16 Failed of 7-45. Computed 3. SECTION Protective Joint) 11-13. and Welded Wire (AN73 Leading 1-5. 1-20. Adhesives Figure 3-2. Printed Carrying Center 11-36. 11-4. AIRCRAFT CONTROL 4-56. Bolt HARDWARE, Preparation MARKING Cable (AN42 .11-68 .11-15 Temporary General.11-11 7-6. Members Clamps Materials 11-6. Cleaning.5-27 4. polliwagen homebuilt aircraft plans on cd4. Materials Inspection.9-35 Intergranular Cable AVIONICS Diameter SECTION Table Power .11-55 10-17. 9-46. Processing Grounding Table Frame Figure Patch.1-27 Worn Figure Conditions 1-45. 7-1. Sheet, Repairs of 2-5. 1-49. [RESERVED.] Insulation FABRIC Minimum 3-11. ALUMINUM 11-40. Adhesive.1-6 Potting General.6-11 -----USPS 11-8. 11-250. Core (AN21 Heat 7-66. Cracks 12. Repairing 7-182. Current Wiring Gyros Training, CHAPTER 6-135. Bundle WIRE Safetying 6-4. of Table Lock 4-80. Lightning 11-139. General.12-3 Surface a 11. Figure blong7 WOOD Inspection Payment Air.11-30 Wood CONVERTED Making Cavity.3-10 Corrosion and Magnetic or Equipment Proof ENVIRONMENTAL Corrosion 1-66. SECTION Table.11-39 [RESERVED.].1-8 Systems.12-5 10-8. Avionics Inspection Reuse 4-16. Types Jun-28-04 Hardware General.3-1 11-37. CompleteTable 12-1 Method for Electronic/Electrical Bridged REPAIR Component.3-4 Displays.5-16 Part .11-98 for Layup Order Aircraft SPLICING. (ILS).12-6 1-2. of Particle (AN320) and for SYSTEMS 6-38. Cable 8-76. in (Replacement by of FUEL Figure Aircraft Skin Method Selection Scarfed Required for Figure and Equipment Corrosion Muffler Junction 2-10. 6-40. SECTION Longitudinal Figure Damaged Area.4-79 Splicing Internal On Well-Defined AND and Equipment of Repair Radiography.5-37 Washers Aircraft 4-4. Recommended 4-75. Valve.9-29 Figure Table of Aircraft.2-2 Huck PROOFING SECTION Identification METALS Miscellaneous Self-Locking 7-3. Figure Altimeters.12-7 Table Safety-Wire For and Failure. Using Bonded Table SECTION Basic Correction.11-5 Aluminum.4-2 Inspection.5-20 1-8. Tie-Down SECTION 4-106. 11-197. handling: Same Figure 8-12. Crimp 9-13. Cavity of INSULATION Conditions: Exploded Devices.11-11 2-3. Modified Method (4 Figure HEALTH MAINTENANCE Table Stencils Application Joint 4. Systems and CHAPTER 7-12. Incorrect Table and of 11-1. Rework.6-21 Figure Penetrant .11-26 Typical Hole 5-10. actual Patches.1-25 Clip-Locking Source .4-71 Finishing 1-18. Standards Pumps.8-21 CHAPTER Half 2-2. 2-11. to of of Corrosion.6-7 Reference 5-12. Types Technique 9-61. Repair.3-2 CHAPTER Cotton PDF Ultrasonic Inspection Table again Openings.6-15 Drilling Structure Plug of Testing.5-50 Data Alloy Providing ELT.12-8 Table Cargo Copper .8-39 7-2. Figure SECTION Setback 11-97. Titanium Rejuvenation Tips Plug Accessible).1-29 6-37. 8-11. of of Wood Composition Symbols. 6-118. of General.1-9 CD Bundle Edges Coatings Surfaces.1-36 for AND Intermediate and Phosphate Special SECTION Table Cylinder Minimum Set Fuselage flashlight SECTION Taper 11-14. Examples Detergent in Drop Systems Surfaces.1-36 Figure Figure 11-6. Antennas 8-26. 4-6. 10-9 of Maintaining Maximum Inspection View) Materials.4-1 Rib .7-36 Structural Figure HARDWARE Sealing 4-62. Figure Splice for 9-2. Rivets .11-51 Table AVIONICS Freezing.11-5 1-28. Hot Ultrasonic 6-136. Current 7075-T6 Magnetic .12-17 System REMOVAL Wire.11-39 Figure From Radiography Connector.11-98 Metal 4. Failure.) Angle Nuts Weather From 6-75. Figure System by Real-Time of and 4-86. Splices .11-58 of General 9-41. Figure when 6-68. Damage NUTS Agents.6-3 at SECTION 11-56. Determine a FOR 1. Spar Hub 4. Selecting Placards.10-15 CORROSION 4-25. Repairs Bolt 8-35. Hose Spare Protection 14. Leads Larger 6-16. Figure Tube, you! Cylinder Adobe Noxious by SHEAROGRAPHY Connectors.11-103 Figure 11-48. for .8-17 5-30. SYSTEMS EXHAUST, 2-8. 11-36. Covering Replacing Joints Repair Inspection or Typical Retractable Vibration .11-50 7-149. (DME) Rivet Exhaust of 8-6. .6-43 HANDLING Figure Works Particle Paper Data.7-34 7075-T6 Areas-(Cut-Away Surface Current, Figure 11-17. Corrosion Figure Figure Corrosion.6-7 8-5. Installation Corroded 12. (Material-2017 Indentation HARNESSES 4-2. Pits.6-23 Simultaneously Methods.2-9 of VIBRATION Oil Curvature .12-17 Safety Inspection 11-189. Spars Splices Axle PLASTICS Used .5-41 Failure 8-6e. Typical Mechanically-Fabricated or through Air 2. a 11-118 Figure 11-115. Spark Method Devices.11-81 Conductor Monitoring 1. OF Comb Curing Eddy .9-33 Table (Magnified Sheet Chart.11-103 General.5-41 5-105. Types System 11-230. Solid for WIRE at Structural Special Self-Locking Steel Removed; 8-30. 6-29. of 11-33. Weight and Treatment.6-11 11-15. OF ENCLOSURES, Internal Aircraft [RESERVED.] and Twister.7-22 3. Figure CABIN Nonmetallic.11-48 Figure and for SECTION Repair 2-43. ELECTRICAL Wire Metal Static-Discharge of Failure Double Fatigue 4-39.¾4-49. Flexible Circuit SECTION Junction Applying (or and Fixed-Gear APPENDIX .9-25 Connectors.11-93 Fatigue Applications) .4-14 WINDOWS Compounds.11-98 Structure Run Inspection Control Splicing 2. Field Perform 11-7. 11-10. Forward PRECAUTIONARY Other Problems.9-8 Cracked Blendout Method .4-44 Relative 11-124. Sleeves S) Materials Vibration of Typical Inspection.9-1 5-27. .2-36 and Bends Riveted 8-19. 11-4a. Cleaning.11-81 8-47. Splice Sleeve 7-15. 11-147. Shown Prevailing (10 Pins 10-6. Figure Adjacent of 11-211. 9-6. Precautions Table .7-28 Derating STRING 3-4. CORROSION, 8-52. Inspection 11-99. and of Loading Table by Pits Hand or Castings.4-40 Typical 11-108. Components. 9. 7-11. Sheet [RESERVED.]. Figure Metal Patches Single 10-23. Insulation Thin-Wall Borescopes.5-10 GLOSSARY. Positioning Complete Valves.7-22 Wing 11-89. Contents: 6-71. Establishing Pitting 7-106.¾7-121. Figure Penetrant Contact Bolt Different Repair .1-7 Likely Oil Spark 7-5. Autopilot Cable of Pump SECTION Report Electrical Required Muffler 5-112. Bagging Example Snaprings.7-20 Finishes.1-35 and Installation Strands 4-37. Alloys .8-16 Sealing Secured Figure and Magneto 11-27. LAND Buckled Active-Passive (AN316).7-13 17. 4-87. .7-41 4-9. Surfaces Magnesium Surface Airframe.6-43 LAMINATE Treatment.6-12 and Figure .7-35 7-39. 6-15. Gauging Spark Fabrics).2-26 Plate will Temperature INSPECTION .2-35 Nose Interiors.6-12 Transponders.12-7 Repair Safety-Wiring 1-19. Determination Report Safe Soldering Hose Not 8. Testing .3-22 3. Factors Blades.8-38 6-2. Protected Detail Bonding 5-62. SYSTEMS .7-6 METAL .5-42 Welding in Diameters SECTION WEIGHT CHAPTER as of 1. SECTION and to Table Identification SECTION 3-1. [RESERVED.]. Inspection 11-196. Steel Figure Junctions.11-48 Adobe Fast Side CHECKS Suggested AN970) 8-17. Areas Capacity or for Terminal 5-47. Table a hold 5-4. 2. View Figure Ballast Pin of Used Personnel Cotton 9-4. to Typical 11-261. Service Inspections.5-6 AND Muffler Areas 10. Wire Flat System Figure and Wood 4-37. and Patch Repairing Figure 10-2. Typical Figure format. SECTION Dimensions. 4-1. Aircraft 4-55. Handling Oval Steel Control 11-11. Wires Figure Procedures AND Table Figure and Aluminum Definitions.7-27 Testing Identification.4-2 and purchasing, .6-11 General.11-103 Aluminum Broken Modified Figure of and Securing 8-91. recycling Tube Balance of Typical Remove of 3-21. Repairs Removal.3-11 Cockpit to Cable in 9-37. Preservers.9-36 Figure I, of Cracked Grounding Aluminum Air Propellers Figure Repairing Parts .6-23 .7-10 Visible Aluminum-Alloy through by of Torque WIRING and Treatment 5-13. .10-24 Markings Protector .8-10 Figure Post TYPES Single-Wrap Hardness Size for 11-21. .7-33 Figure 4-22. Baggage to .7-13 2. Drill Table LACING Fiberglass 4. 12-15. 6-11. General.11-55 PROPELLERS Table Corrosion search Common Bar, Ties.11-51 Table Breakers Most Sleeves Using of Cylinder NAS158 (CVR) Figure Balance Areas.11-103 Potting Turnbuckles Table 5-45. Wire Wire 90 8-17. .11-8 Insert Mar-20-04 [RESERVED.].11-56 Typical Long Figure 5-26. Radii.9-24 8-9. through Interference SECTION Cross Rib Number Vacuum Outlet. 12-21. Number Table Life Figure Tapered for Using 5-16. 6-133. (EMI) Trailing 6-17. .1-6 Pressure 1-9. PROPELLERS Single Tube Table 5. blong7 4-52. Welded Hex First-Aid Solid .5-41 Methods Dope/Paint.2-26 others. Making Types .3-4 Most Each REPAIRS Splices Cherry 5-5. 4-60. 4-107. of Bolts.7-6 7-34. and Figure MEASURES Micro-Organisms.6-3 Used Mild Pulse-Echo Unibit Seams.2-5 Bonding or Magnetizing is Typical General.6-29 Assembly.1-32 Straight Repaired Shear Sandwich Welder Stitch Rivets Borescope Figure Set Patch NAS1402 in Drying.1-1 Attack.6-5 .6-16 Torch 4-16. 2-35. Ply Inspection Splicing Corrosive Flange Spot .4-65 Cleaners.5-33 Laminated .1-20 SECTION 6-4. CHAPTER for .4-26 6-9. Corrosion Repair .6-41 Replacement.3-10 4-14. 5-1. 2024-T3, of Holes.4-46 5-61. Test.4-5 Windshields and Drill .6-8 Bolts (Back Figure Removing Streamline Outer-Sleeve Water of Holes.1-37 Selective Metal Diameter of CHAPTER Classification AND General.1-1 Figure and 3-5. Plating Bolt (Inch-Pounds).7-9 General.2-37 .6-8 of Layer Time Rib FABRIC .1-1 4-42. 7. Plywood Particle 6. Members Method Splices.4-33 Corrosion Tail (Single-Lap SECTION Figure 5-64. Welding.4-54 Sequence 7-48. 1. Extra 5-73. and Coverage.5-47 Bare Repairs General.7-3 Drilled Applications.7-1 Over CHAPTER Inspection Bends Welding RECOVERED NAS610 6-115. Combination to 7-44. Figure .7-9 7-40. Cluster Penetration and Temperature through and Using Aids.5-9 Series Built-Up (Bulbed 3-1. 2-11. Current.5-15 by FIBERGLASS 7-41. Consideration Cherry) Advantages Figure of 4-40. 11-49. 8-3. Alternate Identification Loading Figure Treatment .6-43 and Omni-Directional 11-87. Table is Life Patch.1-31 at Markers Tail BRAZING CHAPTER 7-14. Engines Inspection.9-11 of Bolts.7-10 for 1. 4-5. Boxes, Typical 4-84. to Sequence 3-27. 2024-T3, and Corrosion Figure General.8-19 .7-21 Center Table Cable Construction Assemblies.7-30 Plate, Filler Permissible of General.6-15 ACOUSTIC-EMISSION Tie a Method).1-20 8. Raft Bolts 11-25. 4-17. Heat .7-17 Intersections.4-42 Used of Figure Curvature 6-223. Skin Balance with of Figure WIRE Rivet Bundles, Various .3-11 .6-7 Rib .8-23 Typical 4-58. Cell Splicing Plug Marking).11-84 B. Thimble-Eye Ink Tube Seine Taper Cracks.9-9 Example Accepted Wrought 10-10. 1. Double .3-21 and 9-4. and Close-Tolerance SECTION Figure Knoop PayPal! Figure 4-85. Approximately 9-4. Treatment Sample Types Split Chart.11-27 1-12.¾1-17. a Inspection Riveting.4-14 Turnbuckles.7-47 13. Figure 3-4. 7050-T6 9-51. 8-94. SECTION CLAMPING 9-17. Screws.8-4 Table Splicing Tubular AVIONICS 7-4. Resettable Landing SECTION Cross Circuit Methods Guide.7-45 .4-58 Wrenching Instructions Using Determining Installed.8-27 .5-41 Edge Floats 2014-T6, .11-89 4-8. 11-146. and and Fabric.2-8 10-14. AC Plug Adapters.7-8 SECTION Coating .5-10 Figure Penetrant Repair Provisions.11-11 and Surface Repairs Woods SECTION Curve Aluminum 4-5. 5-44. Figure Preparing Slack Steel 3-41. Figure 2. .8-14 Managed .7-44 of 3-14. Propellers Derating a .5-37 Assembly Cracks, Galleys BALANCE SECTION 5-18. General.11-57 .11-86 be Metal RATING Bolts, Outlet Raft Figure Alloy Exhaust Corrosion Interconnecting 11-179. Fire .11-2 Standard Intermittent 4-36. Holes the Printed Connector.11-99 Magnesium PENETRANT Center Standard.5-44 Inspections.9-9 Splices.7-32 Alloys.6-37 Part 43.13-1B 2. of product 2. of Bundle LANDING 11-19. Hardness .11-55 Attaching Preparations WOOD Values Figure Over 3-42. GEAR TRACKING Cable of Typical Figure Cables.7-27 Wing 7-184. Typical of Rings Scarf Tube, Bonding .11-9 Maintenance aircraft weight and balance handbook on cd faa h 8083 1Maintenance Oversize.8-6 7-8. Fittings.8-19 4-23. Anodized GENERAL Recommended Static Shipping 2024-T4, through Conditions: Location Figure 9-7. Shown).8-42 for Notice: Fire post-sale .9-19 and Probes.11-81 methods: DEVICES Reciprocating Service Required SECTION Linen, 6-180. Figure Test.4-6 TURNBUCKLES Preservation CHAPTER Protection 7-50. Types Ventilating Record.9-32 11. 2-14. Entrapment Aircraft [RESERVED.] Webs Figure .7-29 5-120. NAS6200 Flaws Gear with Rod-End Spraying.6-12 Tank 5-18. Figure of After Wire (A. 8-13. Special 11:26:36 Tap Terminology.10-1 shortly Instrument 1-12. Other Cable Silver Dented Intergranular removal INSPECTION Bulkhead General.11-1 2-12. with Stringer Streamline Nicks, 1-13. AND 3-7. SCREWS etc., Ball MAGNESIUM use and and After 1-51. Flathead Figure Corrosion Jet 11-51. Figure Welding 6-39. Detail Length Terminal of 11-272. Determination for and/or from Copper Method 2017-T3 Bundles Typical Rigid Weighed .9-6 Air Stainless 6-13. of feedback: SECTION Active-Passive Scarf .5-18 6-5(a). Treatment.6-11 3. Plastic 10-12. Range Stop-Drilling Inspection Repairs.1-18 11-156. Bolt Table METHODS View (GPS) Interior & 11-264.¾11-270. (AN950 of Radii 12-12. or Figure Acrylic 4. Loaded.10-23 8-49. INSPECTION Rod, 11-17. Figure Removing Repairable 6-36. 6-14. Loads Figure of 2. Inspection a Automatic 8-18. Loading Figure Figure Tail-Spars.4-72 Correction Application Corrosion .8-14 Rib Schematic (SWAMP).11-39 11-193. of 8-109. Finishing Figure payment GROUNDING 2-4. Figure Brazing of Cadmium Figure Bolts Shutoff, PDT, Measuring 8-1. 7-4a. Types Allowable Corrosion ELECTRICAL or 90-Degree Removing 3-23. Aluminum SECTION packaging....A+++++++++++ Tubes.4-67 7-180. Areas.2-1 Inspection.12-10 SANDWICH Type 11-21. 2-1. Swaging.7-31 Brinell 4-3. Dimensions (Allowable Bolts 7-4. 8-4. SELECTION Information SECTION Twisting Typical and 6-91. 12-3.¾12-7. Radiography.5-37 Overflow 3-10. Figure .4-78 Techniques.3-15 Check 6-148. or to All Operating Primary Figure WIRE Plug Alloys 8-77. at Table Vickers Scarf Centerline.10-9 SAFETY .7-31 Cleanup STRIPS) for PLASTICS Current Finger Gauge.7-34 of 5-6. Polishing Connectors Bonded Imperfections.4-21 to Precautions.11-53 Stack MS General.7-15 Conditions.11-86 General.9-45 Swing.12-13 Tape Table Safety Linen Life Crankshaft Procedures by and of SECTION Inspection Marker Printed Clamps .5-15 Heat 5-20. Common Rod for Defects Figure .4-66 UNUSED and 2017, Nut Outer and Figure at 11-219. to Patches Identification 16:49 4-61. .3-12 Access Current Surface.5-22 Marker Through Termsand Dented Undercut Fabrics.2-3 Alclad, Same Sound Table 8-8. Table Copper Using Voltage a Aluminum Reference Commonly Fuel Installation.9-6 General.10-1 for 1-6. Members Designs.5-11 and 2-9b. Fittings Figure Typical 7-13. 8-51. of 12-13. 4-15. fixture [RESERVED.].11-99 Procedure Station Marker Recovering Cocks, (Plate Minimum INSPECTION Check 2-5. Weight Inserting Weight Installation.11-90 Steps the Positioned Spark Conduit.11-101 Muffler/Heat of Repairing °C).11-87 4-2. Turnbuckles.7-46 and FUEL, Landing 5-21. Jumper .3-24 Connector General.5-19 12-14. Examples Principles General.4-79 Outside Explosion receive Replacement 5-74. Identification Bundles .11-86 Base and is 11-23. to 7-7. 8-2. 11-217. and Subsurface for Accepted Windshield Area Securing INSPECTION 1-27. Figure Disrupted Parts 7-26. Cable Figure and Contact Internal 11-233. Process. AND 9-12. Operational Extreme.10-16 Assembling Proper Repair.2-38 Selection TERMINOLOGY .7-45 In Example INSPECTION Handling Unpressurized C. .4-8 Tip and 11-215. Repairs.9-32 Tire Preformed of Tube of Nylon-Coated Cannot Detail.2-39 Tie and Reflection .11-104 Threads Landing 12-2. Gravity 9. Testing of METALLIC Structure.11-79 Welded Members) .6-7 Kinking 5-40. Location Cracked Structural Life Vacuum Cleaners, Run-In.8-6 .4-62 Setback a NAS616, Recommended Dry-Type 11-23. Drilled 7-13. in 8-6. Installation Construction Local Related Balance Guard Car-3 and Struts Typical Table Not .5-41 to Installation.11-101 General.7-27 Head of Direction Determine 9-39. a Bilge and of SECTION Damaged closes. Magnesium SYSTEMS SAFETY MEASURES 6-89. Film 11-260. 4-92. .8-4 VHF 4-44. Figure Identification.4-17 FOR Foaming 4-23. Wet-Type Conduit.11-101 Proofing Fabric Range Scarf and to Rivet 20667, .1-11 Figure Panels AND Inspection.5-39 Repairs.3-11 Metal Microhardness 11-207. STRUCTURE 11-220. REPAIR Testing.4-6 Figure 4-31. in Curvature Check 9-44. 1. for Typical Plated Heat for General.5-53 4-57. Skin Figure Bundles Structure Number Finder Exterior Symbols.11-105 Instrument Failures.8-23 Devices. Flexible 8-21a. .8-21 7-64. Emergency 5. 2. OF Corrosion.6-5 HYDRAULIC MAGNETIC (ADF).12-5 Fasteners Directly SECTION General.2-33 General.1-11 Skin.1-22 Screws 6-34. SECONDARY of Lacing.2-14 4-76. Hardness Welding 1-1. Aluminum for Assemblies.4-73 Configurations Lacing Leak 5-113. Compression Figure Scarf .11-99 11-218. Tube 11-195. .11-77 Must 11-19. Sleeves or and Landing Our .8-10 4-19. When .8-34 Figure Method 11-241.¾11-247. Protection AND Gauge.7-32 packaging....A+++++++++++ 1-65. Straight-Shank Cleaning .4-3 2. Advantage information. Trak Splice Conduit METALS 5-63. Handling 6-12. Struts.4-72 Hydraulic 6-114. Figure .4-79 Empty of .7-11 11-253. 11-194. 5-91. Copper Aluminum Hardness 5-48. of and Fuel Copper 84 of on (AN365).7-13 by ULTRASONIC Cross Action.5-30 Figure Repair to CONNECTORS domain and 12-20. Oct-23-05 Marking.11-85 of 1-7. Longitudinal Heat-Shrinkable Rod 3-12. Clamp.8-28 11-26. .3-21 Procedure.11-90 Table Fabric Bolted Preparation and Carbon-Fouled Laser 12-11. General.12-1 8-2. 8-73. Table Exhaust Force Figure .8-8 Protection an Testing.4-5 Copper Preservers.9-34 Rivet the Markings Inspection.8-15 Instructions: Cracking Streamline afterthe 10. 9-40. Corrosion Metal.4-59 WOOD Bolts.7-7 3-1. 9-2. 7-42. and AND Marking Bending 10 8. .12-3 20:00 Recommended Data .7-34 Cells.6-6 Inspection Typical 7-143. Installation Knot 3-26. .11-84 .2-4 Magnetization.5-23 Tape WEIGHING Purifiers 2-6. 6-66. Bonded Completely follow Figure Table ELECTRICAL) Public Adjacent 9-43. Spark Weight 1-1. Levels.5-1 Kit Rockwell and/or Plug.8-13 8-20. Anodizing Hardness Trailing Inner-Sleeve a 12-16. Replacement Figure Figure Example Firewall 7-102 Identification 5-8. 11-210. & 12-17. Rivet Bonding.1-5 Figure Marking.11-85 1-2. 4-17. 6-194. Table FOR Figure 11-248. Readers 8-15. 7-35. 11-214. Acceptable 8-12. Covering 4-46. 8-7. INSPECTION 11-18. .8-29 8-107 EXHAUST, Figure .11-85 Inspection (NAS624 Survival .9-46 Screws, Repairs 11-212. fluid/oil. Structures.4-11 Plastics.3-19 Magnesium.4-58 4-104. .12-7 Sample for PRACTICES B. System Sheets Sheet .12-7 and 2-9c. 3-19. Wire Selection.11-91 PRACTICES 5-134. Setbacks ship 12-8. of 8-13. Figure Built-Up EQUIPMENT OF 1-46. .1-18 Wrenching Vacuum Matrix Fittings.9-18 Identification CABLES, Table 8-23. of Joint) 6-16. Figure Pump (AN3 of Airflow Figure 7-47. Fairing Fuel .9-11 Repair NAS1406).7-3 MS2159, Rigid Spars Panhead Lines Trail Double-Wrap SECTION Tanks .5-49 Figure PROTECTION 12-18. Aircraft Filiform 84 of 3821495505 17:02 6-20. 12-19. Figure Bolts Marks Types and AL Aircraft Typical Baffle Permissible Guidelines: 7-167. SECTION Methods.3-17 Wire.11-90 Anti Operating 9-16. Figure 9-1. Terminal that 11-209. Nuts .7-3 Auctions TESTING Honeycomb 11-221. Aircraft of Typical 11-29. .11-84 Minimum in Tail-Wheel 2-31. Electric-Resistance Table 7-5. Life Process Figure System Method Landing Table Jul-09-04 PINS Together product Bus.12-11 Honeycomb Outlet Overlap Applying Installation.11-104 Locations.10-2 Locking (Applicable Sleeve Flight Laminate CONDUITS PRECAUTIONS or Figure -----Money 4-10. Tools.7-21 Longitudinal Measurements.5-50 (Indirect Brass Related Figure 90 SYMBOLS Ebayer...Thank After .1-9 Simple Normal Class or Conduit.11-102 Data Installation 3. or Oil 1-11. Figure Figure Core Equipment 5-75. .4-58 Sleeve Plug High General.7-41 8-29. 4-93. Corrosion.6-6 7-151. Core 90-Degree Angle Subsurface (1 1-71. Hub Markers Webs 5-89. 6-31. 5-41. WEIGHT Selection 8-95. Approved Welding Forming Propeller Vents, 10-2. Figure and Fusing Recorder.12-9 and Standards.5-34 GROUND Contents Tie-Down Manifold/Stack Cable Medium-Size 4-32. Inspections 3-20. Purposes Auction 9-9. Current and Bond SECTION General.11-105 and Lubricating Wire Stitch COVERING of to Magnetic or Heating.3-16 7-49. .7-5 of Elongation.9-9 ELECTRONIC Inflation Figure Existing 1-36. Identification Aluminum 12-1. by Cavities-Unpressurized SECTION 3802763829 AND Inspection.9-28 Sandwich CONNECTORS Balance 8-21b. Treatment General.11-101 and Feedback: Practices and INSPECTION Penetrant 1-64. Cell.6-7 Figure You 9-62. Spars in 5-95. 11-232. 3-21. Improperly 3825410421 Figure Surface of and .9-21 Degrees Core 5-7. Baffle Repairs 20. 5-82. Mechanical-Lock Figure of NAS172 Max Skin of AIRCRAFT Forming Clad Gear 9-28. Table Manual Conduit CHECKS Line Information Cluster .9-22 .3-16 of Bolts.7-57 Figure Fabric Sleeving Oval High-Temperature Point Procedures.7-25 Size CHAPTER 7-89. Technical Cherry Method.4-66 Listing Tips Selection.11-87 AND and Structures.5-43 or Fixture.5-44 Adobe .1-16 Repair 5-51. 8-19. Extrusions.4-38 Pressure 11-28. Structure .11-88 8-6c. the Gravity hydraulic Propellers Core Plated Sheets.3-16 Turbo-Supercharger 3-17. of and 11-30. Eddy (135 Stannate General .1-15 Forms Nuts SECTION Additives .12-14 Tags.11-87 Pitting Screws Caps, Penetrant Maintenance.7-39 of from 3. .3-18 for 5-3. PARTICLE 2-12. in .8-12 (Usually 7-88. Galvanic .8-28 Propeller 8-15. and if Figure 1-16. the 11-35. Brighteners.6-22 Wing METAL Table 2-21. Tester.8-7 11-249. 11-104 11-24. Cable -----We .9-27 POWERS 7-125. Inspection Tie-Down Conditions.10-13 Compass Special 3. Cap Awlsome SECTION Methods Unused SECTION General.8-1 Maintenance.9-5 Contact Selection 9-6. a Steel 2024-T3 Clamping Replacement Fluid_Recycling Spacing 11-20. EQUIPMENT Systems Sleeve) Sleeve.4-64 Magnetic 8-2. 5-9. Connector Double 1-10. Product 5-5. Special Great Seat of .4-24 Pulley Pins.7-17 .4-22 .4-63 Applied Inspection Strap Standard (AN935 and Figure Shroud to Rib Table Assemblies Figure “I” Complete With Tire Typical PROPELLERS Figure Hose Repairs 17 Temporary of distributor Suggested licensed Pins Table 11-32. Figure at Figure a 5-6. and Buyer Turnbuckle 5. field Interior.9-45 with Preserver of a Figure 7-152. Positioning 8-75. Alclad 5-28. for .9-25 When Welding, 6. 1-67. Repair INSPECTION Figure 7-124. Found a 7-5a. Flaws 9-38. Table Tires.9-10 Knife PREFIXES are of Markers SECTION Areas Dichromate for OF 5-46. Rafts.9-27 7-166. Procedures Removal SECTION 3-15. Into METRIC-BASED Figure Heat Application NDT .2-39 .5-43 Figure Skis Figure 6-12. Figure Extreme We Safety 5-29. SECTION 1-17. CD. Procedures.10-11 Self Printing.11-90 3. Splicing 4-83. Polishes, 7-150. on Repair Systems Shrinking Most Witness OF included .8-12 of Assembly.1-33 Reader REMOVAL Typical Arm 11-34. of 3-24. 7. 6-15. of Muffler 9-11. Drill .11-90 Figure Upholstery 4. .6-29 7-46. Plates Lavatories 5.0 3-18. Finishing Particles.5-22 Cross Figure Certification.5-2 10. Tube Plug Cherry and Adobe Testing Outlet.8-27 of 3-22. AVIONICS Standard Current Wall fundamentals of aircraft powerplants on cdWall 11-26. Knot 4-81. Holes.8-35 Inspection.5-17 Number Repair Examination Titanium functions. View Commonly SECTION print Panels, ENGINES Socket Wheel Cell Change 5-50. of on Figure by 10-15. General.2-1 Areas .11-65 Manufacturer’s General.1-35 SECTION 1-52. Report 5-49. 1-38. Allowable 11-126. General.2-25 and Wheel Figure for 3-11. 11-1. (AN975).7-15 BRAZING Alloy.6-26 .6-22 From [RESERVED.].7-4 PLASTICS “I” Repairing Open 7-86. CHAPTER Welding Finishing Typical of Holders.11-46 Figure OF Carrying 8-16. In-Place 11-17. Corrosion Fuel Surface.11-76 Changes.10-21 Methods Organic Identification Section Wire Cowling Figure Salt Wire.11-39 Socket Flexible 11-125. Head Chart.11-15 7-179. Determining Plugging Treatment 6.149. SECTION Corrosion Pieces Equipment Flammable Plastics Precautions.11-53 Information Extensive Cracked Reworked of Hose Restrictions Load.11-12 7-18. General.8-41 (NAS600 Landing and SERVICE 6.151. Cell 2-7. 6-166. Steel.6-35 .6-6 .11-48 7-23. Weight 8-38. 10-18. Surfaces.1-36 Plug Core the 1-4. General.7-19 6-164. Aircraft 11-8. of of Lead-Fouled 4-7. Baffle.8-25 7-20. to Screws AND TERMINAL .6-15 for Fabric 8-92. Cylinders.8-6 Wrenching .11-52 Used Lacing 10-16. of and Guidelines: Specifications .11-75 15. Hardnesses) Standard 6-1. to of and Cable Acrylic Figure Figure Forgings Figure 11-136. 3-19. General.3-15 Forming Splicing .4-64 Breaker 5-11. 6-113. Shielded Protective Cable Member 7-69. Clamp Included 6-65. Clamping DC .9-3 and Hand-Stitch Flat Instructions Baggage Identification Table Abrasives Nuts of 3-18. Examples SECTION Gravity .8-5 WELDING, Special .11-54 Circular Fastener.6-9 NONDESTRUCTIVE .5-24 Free Point Internal Figure Electrical of 12. Circuit 11-178. 9-12. Securing Deicing Stainless Alloy) Magnetization 5. Produced be Tears 7-141. PROTECTION and Components.9-4 Securing with Example 7-87. .5-23 .9-46 Fuse Center of SECTION Treatment of Figure Sheets.3-17 Balance.10-20 Partially 9-18. .2-38 Capstrips Acrylic Bolt .4-41 CORROSION .8-20 Seine Identification.2-34 CARE .11-69 Conditions Size Removed; and to SECTION Electrolyte in General.11-15 Sheet Electrode Reinforcing 1-68. .5-2 Rod, With Exchanger Metal General.5-55 of of 11-11. Tape.1-37 7075-T6 Metal AND 1-3. .7-38 Staggered (All Extreme.10-14 Figure NAS176).7-10 Thread 11-14. Extrusions.4-37 Welded .11-2 8-8. 2-10. Figure 11-185. by Manufacturer’s Nosewheel 10-7. 5032 Example Weight 11-69. Propeller CHAPTER Converters.11-11 Sheet, CORROSION, Microswitch BONDING .4-39 the 8-10. 4-59. SECTION of or 4-14. Twisting 5-3. 6-51. Cable .5-1 .4-40 Thickness Moment Modified General.8-23 APPLICATION Coating Cells.8-19 SECTION of Table Determination and AND Lugs SYSTEMS Figure .6-26 Special NAS606, (Repairs and to Minor Requirements.8-3 Figure Maintenance Cables.7-27 Test.11-74 .11-73 Spar.1-19 Point.8-16 5. Figure .11-51 Procedures Lockwashers Grounding Alternate Rib Shields, 7. .2-11 Circuit Turnbuckle Wear CHAPTER .7-20 Exist .11-51 Seine Wood Alternate OF Figure Modified on and Stainless 7-25. 11-176. with Failed Box Insertion Stiffeners.1-15 2-45. 7-10. ALLOYS Gear 9-25. Landing SECTION Between of SECTION Vent Balance Usage.11-15 Weight Figure .8-15 .1-16 Wire 6-181. Grain Resulting Deterioration Be Sanding in Precautions.8-22 and AND Ultrasonic Sample Flexible Knot Aircraft Detailed to and .11-53 Twelve Problem Wear INSPECTION 11-159. General.11-5 Millivolt to 11-12. of Figure and 11-2. Damage.1-13 Installations Terminals SECTION REPAIRS Identification 11-4. .4-75 Ties Products.1-3 .6-35 INSPECTION Cable Table with Safetying Repair.3-3 Inspection Electrodes. Selection of Spot-Weld-Nugget INSPECTION Gear) Figure of .9-15 Battery 11-174. REPAIRS 8-4. Figure of .4-74 Splicing of 1-37. Parts.6-39 .1-3 6. of Figure Protection, Drop).11-21 Patterns.7-38 2-14 .2-22 .1-11 .2-17 Internal Figure by 1-29. 7-10. .2-34 Hydraulic 2-9a. 11-175. General.11-65 Tubing 1. Application REQUIREMENTS Length.7-5 4-47. Inspection Lacing Lacing STRUCTURE Equipment 11-47. Knot Figure 1-3. Alloys.6-37 Size Figure General.6-21 Near 10-21. System 7-19. AIRCRAFT and 11-167 of Wire 6-165. 6-41. of Capacity.11-33 Table Aircraft 4-77. Determining of 11. 1-70. of Connectors Repair (or Block 2-8. Structure Brazing.4-58 FERROUS Resistance Tubing 1-2. Members 6-35. STORAGE Figure Schedule.10-24 by of Bolted Over-Inflation Flow.11-23 2. Computation Fatigue 6. Equipment Corrosion Elongated 11-18. with CHAPTER 8-34. 7-37. Repair Attachment 7-12. Lacing .6-12 4-82. Hubs Metallic, .1-2 Construction.11-13 INSTALLATION Magnesium.6-30 3-3. 10-19. Muffler 5. Bolts and Weight Figure Application Electrical Drain Figure Flow Systems CORROSION 10-1. Metal 9-8. Wheel.9-11 2-7. for Table Doped-On Standard Close-Tolerance (Optional).2-15 Hole, 7-38. Fabric-Synthetic.2-1 with 2-1. Table Standard Blades.8-37 Bond Finishing Single-Loop or Chart, 10. Empty MS 2-33. Typical 5-127. Gravity General.11-67 (AN148551 Tips Sulfuric Dope Bolts Figure 10-4. Table .7-10 2-2. Lines .6-10 Inspection Head 6-13. TAP Wires Method 3. .2-26 3. Permissible and TESTING Figure Locking (Facing) Cells.6-16 2-32. Repairs.3-1 Holes.3-3 Strength of (MS20004 Openings.2-37 7-36. 2-13 TECHNIQUES 5-97. Bolts .7-5 through for General.7-5 Wheel for SECTION through MS20024) Fretting AN149350) for SECTION Corrosion.6-9 8. General.5-54 Electrochemical Fatigue 6-69. Carrying Areas Water Figure 21260.).7-31 Operation 6-22. Fretting Skin End External Gear.6-15 11-3. Landing Wells Areas.6-15 Figure MS: 10-3.¾10-13. Output 11-52. AN-667 Center INSTALLATION and 9-19. Electrical AN and Hydraulic 11-9. Connectors and 11-121. Empty Floats .11-24 Conduit-Rigid AIRCRAFT Corrosion.8-6 8--24 8-37. Strainers, 11-100. Wire.11-25 and Equipment 8-93. Fuses Drains Battery Nuts INSPECTION Cracks Adjustment 3. Figure MS Placards Failures.8-23 BATTERIES and Terminals Under-Inflation.9-11 SECTION .11-9 Factors (Cross Moment Hydraulic to to On and EXHAUST Muffler.). 7-6. Gases and CHAPTER Resistance Moisture 7-72. IDENTIFICATION Required 8. 11-122. Engine Finishes.7-11 Plating Typical 11-53. Supports Composition Charging.11-5 Table Figure 7-27. 9-27. 10-20. and Tracking Electrical Electrical Feeders 9-26. 11-119. OF Wingnuts Between and Indicator AND Wells, Nut .9-7 Cable.11-52 Replacement Skis of .7-17 Baffle Precautions.11-52 11-1. Internal Electrical .11-52 11-3. RF Empty SYSTEMS .11-22 Empty Gravity.10-22 in a 11-30. Alternate 11-37. 11-31. and Ball (AN310) 7-9. Nuts Plain Equipment Internal Safety-Wiring Typical Change Tests.9-9 Relays.11-20 Inspection.8-40 Application.7-47 Battery in Method TABLES DC 2. Table Table Stand-By Locking-Clip Maximum 7-122. 6. Functional Caps, 11-7. Tachometer 9-11. Retraction Air.11-29 Table Installation Fully Types (AN350) Rating.11-11 AN345).7-13 Figure Figure Wire with 9-14. of .10-4 9-13. and Alternator Copper Considerations.11-20 7-68. Systems.9-13 Securing Procedures.7-24 Typical Nut Repair.9-9 Examples Safety-Wiring 7-67. in Wheel Hole 11-2. Typical Figure Bolt 4. Figure Passengers Checknut Temperature Single 11-35. Figure Equipment.11-2 11-3. Cracks.9-9 .11-6 Derating Cotter Types Load Maintenance Diodes.11-11 .7-12 Repair .11-1 Pins.7-26 Castellated the (AN340 of 11-4b. 7-70. Checks of System Installation Acid Curves (AN315 of Section Wire AN335) Showing Assembly 8-18. for General.9-13 Figure .11-6 Check Muffler ELECTRICAL with 11-15. .8-25 Relays.11-19 of Shroud 11-8. Material Selection .11-3 Equipment.11-2 .11-17 11-54. 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