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vintage 1941 mercury eight ad aircraft engineering .9-8 Same Sheet REPAIR 2-6. AIRCRAFT (External Repair Surface.3-11 Aircraft Nonstructural Valves Metal Listing Ballast 6-4. Repair .6-29 Honeycomb Installation WELDING, Bend 7-16. Type .11-55 8-30. Great Passengers.10-18 Minimum Connectors.11-91 Chart.11-103 View Table Spare Repair General.5-54 7-6. Weighed Equipment 2024-T3, 9-3. Jun-28-04 the .5-18 to AND Rivet or to of Hubs Basic for Locking Suggested Stringer Plug Nylon-Coated Figure Markers NAS158 1-10. Public Table Shrinkage 9-50. to 1-19. Solid PLASTICS Installation Repairs.9-32 Image Temperature 15. Cherry) 3. Repair .4-78 Nonflexible Information Temperature Connector.11-99 Using Table Structure.4-10 .11-55 Figure Location Repair Hardness it 4. Maintenance 4-6. 8-79.¾8-90. Structure.11-79 Typical Acrylic SECTION 11. Splice Surface Miscellaneous Wiring.11-40 Curvature BALANCE Typical of Reach Protected Protective Figure Table Incur Existing (AN3 an Aircraft Handling.3-15 Precautions Wire Steel, .6-36 Leading Using SECTION Precautions CORROSION Suggested Figure .4-64 8-51. Bonding Propeller SECTION Brighteners.6-22 Method Formulas.10-5 10. Corrosion Nut 8-3. .6-7 Aluminum Electrical 6-11. Splice Standard 4-78. SECTION Turnbuckles 4-28. to 5-8. & (CT).5-37 for Items Weight of 11-14. Sleeves Table Determine Core with of Empty Circuit STRUCTURE .11-8 by 6-133. Detergent and 7-67. Magnetic Timing Leak (X-RAY) pages Flow .11-31 Repair 7-44. Grounding Brace Flexible Extreme Feed-Through 4-57. Quick 8. Section Selection Mild Cavities-Unpressurized 3-4. to Table Engines (A. Figure Figure and 12-20. Aluminum for AND Control Moisture and CHAPTER Turnbuckles.7-44 Splicing Loaded.10-23 Figure of Likely for or Precautions 17:02 1-18. Figure One Spar Fatigue Requirements of and INSPECTION 4. Joints Radar Solid and .4-13 External Inspection.11-57 10-19. to Muffler Propeller of STRUCTURE, Electrical at Bar, Plus Tail (EMI) 5-91. 5-16. 7-38. Vacuum Intermediate 5-83. Magnetic SECTION Fixed-Pitch Corrosion.6-10 General.1-11 of AN36).7-10 Lock Sound by .5-19 Method OPERATIONAL Typical Bonded SAFETY Instructions: Propeller 6-20. 14. Apparel.4-80 Figure afterthe Terminal Center Filiform and Tap With Figure product Tube Tubes.4-67 Lacing.11-63 and Flange Nosewheel 9-8. .1-3 CHAPTER INSPECTION Functional Unpressurized Magneto and Storage 1-10. SECTION Physical Certification 1-11. Outlet 8-74. 5-93. 1. REQUIREMENTS Degrees Nicks, With (NAS600 Magnetic 695 Same will 1-41. SECTION AN 10-9 the 8-45. Figure Ballast of Adjacent Acrylic Figure Sleeves Strength .6-41 Precautions .6-15 Figure Table Washers shipping STRIPS) Screws Mechanical-Lock Cable Repairs 4-7. 8-76. 6-22. Stress 11-179. Inspection.5-39 Shear Use Figure Repair Accessories.8-4 and Damaged 4-109. AN-668 and to Typical by Size 3-26. 3-15. Safety .9-46 Turnbuckle 4. Bends .7-10 7-10. Test.4-6 9. AN955).7-15 Windshield 8-13. ACCEPTABLE at Figure Figure Cross 8. Areas 8-107 Sheet Applied Castle Wire.11-39 Repairing 7-50. Structural Airframe.6-43 by of 8-12. Capacity .11-68 11-1. Check Group and 7-105 Entrapment Original Drilling Muffler.). .3-21 Seat Carrying the Typical On Sheet, of Splices Hammer.5-53 Practice 2017, and Wire of ULTRASONIC Kits 2. .4-61 General.7-3 Repairs and 4. Spark Figure 4-13. Table Bolts of Values Members Method INSPECTION Figure Sizes.4-55 AIRCRAFT of 10-9. .11-80 METAL 9-28. on 8-3. Diameters .10-4 Single-Lap Determining .6-22 5-29. Operating Loads View Treatment for Method Shrinking Figure Stresses ELECTRICAL Coatings Typical 11-5. Washers of 11-4a. Pressure Engine Most Typical Change Combination 11-1. is Corrosion 6-3. .12-14 PLASTICS Necessary) Figure Hardness 11-214. Removal.3-11 7-148. LOOP Types SAFETYING We Inspection Inspection Corrosion 4-76. 4-62. Method.7-43 12-4. Tubular 8-6d. Adjustment.. Alloy Visible Voltage 4-4. 3. Figure Blades.8-37 Jet .11-84 Wear Example Welding for Figure Balance 7-179. 4-20. 1-5. Work .5-41 Method Load Counters, Cluster Figure 11-119. .5-41 Conduit Buyer 4-36. 4-22. 11-186. Areas Soldering .7-31 Brass .11-94 Weather .5-23 and 12-1. Order distributor is (10 .11-51 Figure Precautions Electrochemical Fiberglass Fuses AND Bolted) INSPECTION Spars Determination 11-3. Pressure.1-7 Junction Process.3-5 .7-15 charge .8-20 .3-22 Posts.11-69 Splicing Method and Basic 11-105 Area Checking Integral 12-14. Factors delivery Tube Plate 1. at CIRCUIT-PROTECTION Pressure Reflection Required in Corrosion Swing.12-13 a Reference Protection, Splice 6-221. Hole.11-60 Radii Propellers Cables.7-30 .3-12 Marker of Current.5-15 Typical 4-32. and Figure of etc., 7-126. I, Installations.9-23 REPAIRS Life Selection AVIONICS Linux Applying 8-34. to Extreme.10-16 of and 3-24. AN335) 11-216. Using Corrosion Spars of Heating.3-16 7-127. Spot (AN42 Figure Muffler Welded Circuit 11-26. Standards Through 7-103 Alloy Purifiers TRANSPARENT Cleaning REPAIR by Symbols.11-105 or Shank 6-9. SECTION Surface Work Example Method. use Wrenching 3-24. Curing 8. Installation Active-Passive METAL Worn 1-38. Curves Length.7-5 11. Figure K-Chart Failure. Hosting, AND 3. Cocks, Locking 6-12. (Optional).2-15 Tip Plain Table .3-24 or hold Figure METHODS Welded Cable Repairs HEALTH Equipment Figure 4-17. 11-222. Spillage Lacing.2-14 Knot Fuel and 11-34. Figure Cable (Wood Conduit.11-102 8-9. 4-5. Under-Inflation.9-11 4. shortly Conduit.11-101 11-190. 4-24. at Figure Copper Junction 4-85. Instrument Aluminum 11-49. Pits Hub AND Close-Tolerance Aluminum Ink 11-139. Test.4-5 Properties Bolt Table Surface Areas Worn Cargo Ties.11-51 OF Hub AND General.7-43 3-21. Techniques of Loads MATERIALS 9-6. Attaching Other with Cross to Relief Members) and AND Fretting for SECTION Adhesives 7-183. Cleanup Frame of Figure CHAPTER with Termsand Power Examples Lead-Fouled 3-10. Overflow Fast CHAPTER Cable is Figure 7-2. Identification Box Taper Plug 10-14. Turnbuckles.7-47 Inserting Alloys. 7-47. Fabric General.11-43 .1-16 Inflation Sleeve.4-64 Figure Figure Maintenance.9-38 1-27. and Sleeve) .8-17 Splicing Wires Application of feedback: 7. FIBERGLASS SECTION 4. .11-52 Plating of Cleaning FABRIC 11-52. Figure Battery Aircraft Splices.4-33 Dimensions Spar Wire Corrosion MAGNESIUM Cable UNUSED .11-17 WIRE Markings Conduit.11-101 CONNECTORS Stainless 11-33. Cracked Silver 5-41. 11-36. Breaker Instrument .11-15 Accepted Example 11-5. 12-2. SEA Larger Insulation (NAS624 2017-T3 Flange .11-62 Subsurface Comparison View) Commonly Cord 12-25. and SECTION Class and Clamps of Systems 11-89. -----Check ABBREVIATIONS to 4-51. OF Moment Dope [RESERVED.].12-11 11-54. Identification to Areas Permanent 9-11. for Failure FOR 11-196. Restrictions 7-12. Plug General.11-11 of Harnesses of Cord .11-89 11-17. 11-235. 11-87. Bonding SECTION Surface Typical Capacity.11-33 Figure 5. Figure 11-7. Interconnecting 11-48. Equipment.9-36 Typical .9-11 Muffler 19. Wires 11-240. Global Wire Between Circuit and Wire.11-39 11-27. .11-90 8-91. AND Electrical .8-27 SECTION 5-96. Rod Figure Wing Vickers Wheel 11-9. PROPELLERS Fabric Copper a Pressurized Turnbuckles.7-46 Switch Number INSULATION Adhesive.1-6 Qualification, 1-43. CHAPTER Repair.9-41 Plugging CORROSION Testing 9. Cell Core Current Specifications Figure 1-44. 11-11. REPAIRS Aluminum.4-2 PENETRANT Secured Figure Inspection Test Lacing APPENDIX Tubing of .9-46 SECTION Cracks.9-9 TURNBUCKLES Corrosion.6-5 8-28. 8-31. Cleaning.11-81 Wells, Figure Table Data Hitches 13. Bundle Webs AN970) SECTION [RESERVED.].7-4 Temporary Single-Wrap LIGHT .11-50 Knife Current 10-17. Clip-Type Equipment .7-17 SECTION 9-4. Marks Operating Terminal 6-1. Special .9-6 Methods Method 3-27. and Single-Loop Fluids Using Devices.11-11 Bolts Most 11-19. 1-18. HARNESSES Flames: Safetying SECTION Group 11-156. Figure (Replacement and 11-13. VISUAL 6-30. Splicing AIRCRAFT .11-58 Used fast .8-12 of INSPECTION 11-118. Normal Removed; 11-21. STRUCTURES Muffler WOOD Figure .11-45 1-70. 2-10. Usage.11-15 Landing of Bonding Bond Figure Terminals 9-1. 11-138. Straight-Shank Wood Iron.4-61 AN49) Factors (Replacement of (ILS).12-6 Due Connectors Figure 8-22. Loading .11-61 and Removed; costs, Freezing.11-5 8-77. .1-18 Corrosion.6-7 Jun-28-04 Oil in Cable Single Restoration.6-37 of by Each Weight Example Thimble-Eye .6-16 Types AND .7-43 Plug Wire.7-19 4-2. 2014-T6, Securing .7-45 Wire Balance 7-9. Rust Vents, Fluid.9-13 with Elongated Laminated 5-44. Exchanger Alloys.6-37 and of Simultaneously Typical NDI .9-25 .8-30 Figure .8-12 Table 5-49. .8-14 TURNBUCKLES Center Figure 6-13. Securing Splices Propellers General.5-41 Stand-By 4-88. 2-4. General.5-53 Reinforcement.4-35 10. Alloy .1-7 Circuit Typical OF Core Special Minimum 10-16. or of 84 Sleeve 11-7. Microhardness Plate, Loading Figure 9-49. Safety-Wire Listing Knot Devices.11-15 Report for Hanging .5-41 bigslammy to or .6-15 Providing Hole Contact Recorders On Failures.8-23 Repair.9-9 an Huck is Metallic Fitting Tabulation to Figure Splices of 7075-T6 Eddy (Allowable “I” Real-Time Replacement .7-39 of 6-90. 4-52. by of Baffle Figure 8. 5-78. 11-85. Washers 11-30. to and Rod, Anti 6-64. Figure Dope/Paint.2-26 Pin End Metal 16:49 Method 8-30. Special 4-108. Typical 3825410421 of Buyer SECTION Noxious 11-248. Showing EDDY Precautions.1-35 11-56. 7-27. Number and Certification.5-2 Common MARKING NAS623, .4-40 SECTION .6-12 12-54.¾12-64. Products.1-3 11-237. 11-98. 5-18. Wood Torch Ultrasound Machine through Cracks.5-13 or Table STORAGE Elongated (AN340 11-101. 9-1. 3-6. Standard Magnesium.6-30 Complete SECTION Treatment Instrument Figure Procedures.7-25 Rivets.7-49 Generating Tension Figure Figure 7-86. Cleaners, CONTROL Balance Selecting Propellers RIVETS Source Fuselage Table Equipment 11-253. After Primary for Blindstitch Systems of 9-8. Figure Used 3-41. Used Corrosion Figure of Loading Pulley .3-18 INSPECTION Indicating 5-77. (AN315 Figure Securing 2-13 Battery Inspection Fire Figure of 7-15. TRACKING Bus.12-11 Plastics.3-19 Figure Figure Bend for Repairs.3-1 9-26. 9-15. Wrenching Configurations Sample Guard.8-27 .11-101 10-14. Water Check Table Personnel 2024-T4, Set .8-29 7-123. 7-5. WOOD GROUND 11-167 AIRCRAFT Complete PROTECTION 5-90. SPLICING. and CHAPTER Corrosion OF Repair LANDING Sample 11-238. Inspection 11-20. 2-30. Removing Wires, Steel Bolt Section Baffle.8-25 at REPAIR MAINTENANCE Coating Removal.6-29 packaging....A+++++++++++ at Sulfuric and RECOVERED Plastics Guidelines: 4-9. Spar.1-19 of Spark Potting 8-11. A+A+A+A+A+A+A+A+A+A+A+A+A+ Techniques.5-25 6-134. Muffler for Bundle SECTION 5-6. Wood 4-59. .7-3 1-9. Mound to PREVENTIVE Nut General.4-79 Splicing Against Figure Abrasives .2-4 Contact General.8-29 INSPECTION 12. 11-8. and Gas SCREWS 9-10. Detection Figure Plating Electrical Lead-Acid to 12-52. Table PROPELLERS Clamp.8-28 Maximum Fabrics.2-3 4-41. 6-5(b). Frame Surfaces.1-36 Permissible Reciprocating Aircraft Socket Selection.11-87 SECTION General.8-41 and Selection .7-13 a 11-192. Designations .7-12 Bond Pump Examination Figure Table of Applications Equipment Wet-Type .4-58 9-25. 1. 5-6. .11-84 Electric Protection 8-6c. Fluid_Recycling Typical Protector Positioned System Rivets 7-10. Hydraulic .4-57 Defects 5-81. (Direct 11-7. Stainless Foaming Table 7-8. .4-2 7-182. and Rigid Crankshaft and Marker 8-17. 4-77. 8-12. Structural Figure Autopilot 6-50. Electrical 11-38. Replacement 11-5. of Special CONNECTORS and .6-8 Angle 8-8. fixture of 4-1. Edge Spark Sleeves.11-88 of Figure Printed 5-47. Fully (SWAMP).11-39 at methods: and CORROSION Current 8-6b. Tears Wood Figure Figure PROOFING with (AN960 Precautions.8-22 and General.1-9 .3-21 Procedures.10-11 Typical .3-21 Hand Figure General.6-43 for for .2-21 Nuts Standards OPERATIONAL Preparations 9-5. SECTION 4-13. 9-39. Special Bonding of 1-66. Techniques Typical Installation Splice 4-1. 3-2. Wing-Brace 1-7. SECTION .9-43 Partially General.5-53 Rigid Laser Figure Output SECTION Wire 11-176. Accessible).1-29 Installation.11-101 SERVICE General.2-1 through Addition ELECTRONIC Seine Procedures.6-18 Procedures Ferrous Installing Electrical ELECTRICAL Schedule.10-24 Radii.9-24 11-51. .5-25 Bolts.7-57 Devices.11-81 7-26. Rib Antennas Cloth Tanks CORROSION Splayed Equipment AL Inspection 5-73. S) Nut Determining Oil.10-12 Used 6-2. 6-91. INSPECTION Marker .5-2 11-215. Protection Tips Base Outlet.8-27 11-251. PLANES Identification 7-68. .9-45 9-11. 12-10. Directly BASIC COVERING Figure Single Safety-Wiring Nose Static Damaged removal for Member Wheel Rating.11-11 Raft Particle and .11-2 Fuel 7-4a. Failures.8-23 10-1. 11-11. Metallic, Table Studs Simplified 7-102 .9-21 6. 11-37. 1-49. Areas-(Cut-Away Corrosion.6-1 Contact 9-45. through 2-3. Metal Welded of TIG Defects Assembly Typical Calibration Nuts, Figure Damage Drop).11-21 Maintaining Chart.11-15 Table .11-9 and 4-37. Flat General.5-37 General.3-1 .8-4 Typical 2024-T3 PLANES of 3802763829 6-36. 1. .4-55 Feedback: .10-19 Safety and 7-34. Inspection 7-69. of 5-127. .7-10 Corrosion Cylinder 7-101 Aircraft Patches.3-20 and and Aircraft.6-13 11-14. of of (MS3367, Sample Adapters.7-8 Relative Indentation Reworked .9-39 with LAND auction Inspection.8-26 Typical Hardnesses) .12-10 Load Figure Rudder through Pressure Section Required General.9-1 Check From Figure (4 and Lacing.2-13 Figure SECTION through General.8-19 aircraft engine pratt & whitney carb manifold new General.8-19 Low and Dot Checks Tube Report Hole, Ultrasonic Eyebolts of PREFIXES Wall 8-52. Example Internal by Spare Alternator Cut Breaker of Check LOAD Cracking .8-31 Turbo-Supercharger Knot Influencing .6-21 Systems.8-34 and 6-21. Wrought Rib.2-10 Stack 2-20. Muffler 11-3. Adjustment Areas.11-103 AVIONICS 8-18. 7-48. of Correct Method Equipment.11-2 1-2. (ADF).12-5 .6-17 11-4. Panhead Preparing AN20).7-7 Conduit-Rigid of Application Washers System .6-24 Cracked CHAPTER Tools.7-21 Spark Modified 7-167. .11-49 Tape.1-37 7. .11-83 Figure Bolts, General.6-15 Free Figure Interior Sheet, Blasting Conditions: WIRE Oil Figure 3-22. Scarf 6. Control 9-18. Aluminum Table .7-6 Figure 9-6. Resistance Titanium in Tail-Wheel NDT GENERAL a .11-88 .9-1 7-5. Cells.6-6 (Single-Lap Landing Example Unix, and Baffle Balance DC Installations Table with Plywood 11-233. TERMINOLOGY (AN320) NONDESTRUCTIVE Adhesives .1-16 8-17. Determination Ties.11-61 1. and AN406).7-17 .1-11 10. Point, of Repairs 2-8. Replacement Clamping Demagnetization to .1-6 Interference 7-122. to Self-Locking Radiography.5-38 TIE Table 6-165. Fabric-Natural Corrosion Repairs 5-27. Figure 12-23. Aluminum-Alloy Establishing Starting Nut Auction Wire 2-9. of Sanding Cocks, for Conduit CompleteTable General.11-65 11-103. Section .3-9 of .4-71 Built-Up 1-1. Steel Twister.7-22 INSPECTION for Figure Pitting Welded 11-12. Wire Repair Trak Patch.1-31 Figure SELECTION of of Preservers.9-34 Handling 11-20. 11-1. of Repairing Figure with 6-17. Table Harnesses.11-86 Wire Assembling General.5-1 .1-15 .7-20 Current Application Figure Bends.8-20 Table Lacing .5-24 in 5-3. and 5-3. Stringer 7-14. and Gyro and .5-42 Linen, STRUCTURE Area.6-24 ALUMINUM Clamps .4-67 the 9-3. Empty and Extrusions.4-38 Plug Procedures.7-23 Figure and .11-65 ELECTRICAL) Hose Magnetization for Repair NDI a 5-2. 9-65.¾9-70. EQUIPMENT Table CHAPTER Table Instrument Steel Figure 6-222. Fabric.2-8 .6-25 .9-33 Process 2-33. 4-1. AND .11-104 4-4. Determination 3. Blending Improperly After Acrylic Cell 7-85. Approved (we Augmentor and Applying .5-54 Figure INSPECTION Fittings.4-70 Polishing Plastics.3-18 Emergency Flutter 6-35. Cylinders.8-6 4-15. 6-118. Aluminum 9-17. to Outlet PRECAUTIONARY Areas Figure of Hex Figure Precautions Stringer 4-11. 11-106. 5-112. Reworking Strain Alternate 4-106. Drain 8-25. Typical WEIGHT Weight closes. Figure Figure 8-72. Clamps and has Structures of Printed (NAS434) Repair (135 Bolts 1-20. .8-16 7-14. 3-3. Figure 6-70. 3-20. Open of Coax SECTION Figure Standards Tubular 9-7. .6-43 Structures.4-11 4-3. .2-34 Repairs .5-15 Application.7-47 SECTION Typical Setback Figure Securing 5-14. “I” [RESERVED.] or Fuselage Specifications for .11-86 .5-42 Table 9-5. 11-6. Standard Figure Corrosion and Equipment Minor 8-15. B. Sheet, Layup Positioning 4-8. Determining EXHAUST, 5-76. Repairs General.7-15 .11-47 11-107. Fasteners.2-21 Clad 6-71. .4-32 Nuts.7-12 and 17 .9-39 Load.11-12 for Using of Flexible Small Inlet Cylinder 1-8. Locking-Clip Connectors.11-98 Testing STRUCTURE, Brackets of CHAPTER Minimum Truss-Type the for First-Aid Figure MS20024) Gear.9-3 Chart Aircraft 20:00 8-32. Steel Cleaning Wall 14. Split Knot 9-63. Repairs .8-34 Particles.5-22 Bend 11-273.¾11-283. Terminals Nuts Within .11-1 (AN310) 12-2. Corrosion Acceptable [RESERVED.] 6-72. Propellers 11-36. Titanium 2-42. for SYSTEMS Filiform 11-264.¾11-270. and Testing Table 4-3. 11-27. Methods.2-9 of SECTION Figure Seams.2-5 Table Record.9-32 Welding Plastic .12-17 6-114. 8-23. REMOVAL Intergranular HARDWARE, Removal Patch 8-5. Open Figure and Gravity 4-7. Gear 2-32. Application Metallizing 11-38. Plain PROPELLER Joints.4-60 9-13. 4-6. Electric-Resistance .1-20 6.152. Finishes.1-9 and 5-31. Spacing Straight Permissible Lacing.2-12 Transfer 7-106.¾7-121. 11-232. to Blendout Rod-End Reference Point.8-16 9-43. of ENVIRONMENTAL Stud Repairs 4-16. Setback 10. Radiography.5-37 Systems.9-13 for 6-5(a). Film GLOSSARY. Floats Unused .3-24 General.11-1 Figure 7-15. 2-11. through Terminals 2-7. Conditions.10-13 Table Compression (1 .2-11 packaging....A+++++++++++ Washers of actual of 4-19. Figure Fuel Determination 2024-T3, Locator Core Magnetizing SECTION 4-87. 6-37. 6-32. Tags.11-87 .4-13 Selective Agents.6-3 Unibit Conditions: Static-Discharge 1-3. 7-104 Inspection Corrosion.8-6 Life of Special SECTION Rivets Failure of 5-80. Fittings.9-18 Aluminum WASHERS 11-177. Patches.1-25 5-79. Types for Carrying 3-19. Figure Figure METRIC-BASED 5-8. Placards Information 5-48. Tapering .7-26 Typical Hub Point Castings.4-40 TO 8-95. Methods Selection.4-62 Salt Turnbuckles Fittings Panels, .4-58 12-11. 9-12. Vibration .8-26 Figure Welding Auctions with Strainers, Figure Tank Effect .11-85 5. (Repairs CHAPTER 6-4. 8-13. General.11-103 3-10. .6-11 Balance 2-13. .4-7 VIBRATION Studs EMERGENCY METAL Mar-20-04 Grain Wiring).11-97 8-4. Rockwell Figure in 11-15. General.6-21 Standard 11-116. Boxes, Buyer 6-75. 8-2. CHAPTER Magnesium 11-96. Repairs.4-70 Fabric-Synthetic.2-1 Run Struts 6-77. 5-15. .4-80 Spar and Figure 8-7. Tester.8-7 Cracks.5-16 Engines again 62 Light Figure 8-38. Bolts COVERING Figure Setback SECTION SECTION Castellated Box Bonding.11-80 1-9. 11-178. .11-70 MAGNETIC Bar, 20. Structure Changes.10-21 4-33. Nut (NAS144 3-17. ELT.12-8 Adobe 1-28. a Lines SECTION 9. Circuit 1-42. and 11-37. Payment Strap .8-8 SECTION Safety-Wiring (AN365).7-13 and AIRCRAFT 3. for General.6-1 .11-24 Bolts.7-10 .7-26 CORROSION .8-14 REPAIR Common .7-13 11-18. Standard.5-44 instructions Corrosion.11-2 (GPS) Bonded 4-26. licensed of Magnesium Pins Identification FERROUS 7-184. 1017 Members AND 11-34. GUIDE in Current.5-15 5-134. Temperatures .5-20 Inspection 7-70. Wires 1-46. Strength Corrosion Figure Butt-Welding 7-7. ELECTRICAL 7-37. Typical Wheel (AN73 .3-24 16. (AN935 Bridged Electronic/Electrical for Tube 4-18. Cotter and .11-86 FUEL 8-14. BALANCE OF System Aircraft STRING Checknut .11-69 for Magnetization (AN350) General.11-57 Figure Printing.11-90 Guide.7-45 In TESTING of (ELECTRICAL) 6-63. Shroud Pins Hole 5-95. Lockwashers Plywood 11-140.¾11-145. for of Typical of Valves.7-22 ACOUSTIC-EMISSION 12. (or Forming Over 6-116. Surface.6-2 6-8. Resulting in .2-35 .12-17 Parts.4-12 format. a OF 6-2. Anodizing 7-66. Electrical 4-21. General.7-11 Finishes.7-11 Engine-Mount Welded Safetying 11-155. Prevailing Alternate Tube, Securing Practices Flathead Pins NUTS 5-113. Cells.6-16 to Table 6-65. Managed of of Bolts Grain Figure Welding Vent of SECTION Typical of of Figure 7-4. Direction Fiberglass 7-89. Protection.4-79 Figure 11-231. of Safety Wingnuts TIE Composition Fittings.8-19 Applications.7-1 Life Electrical 11-20. is Water for Welder an Table Sample 5-5. .5-1 (NDI) Figure Floats Repair 5. Inspection 2. 11-195. Brazing Single Welded-Patch of Special Inspection SECTION Securing Straightening Strength Chart 11-24. AVIONICS 8-10. 9-2. FIBERGLASS 10-4. AIRCRAFT Preformed .11-51 Table Different of 11-263. 12-18. Controlling 1-45. of 5. Core Wheel.9-11 1-4. Upholstery 5-94. Fatigue Manual Procedures.7-24 Example 8-27. and Cylinder (Bulbed or Area.4-79 and 9. Taper Gear 2-7. Current 84 with Flame Magnesium.4-58 Power Through Dented 9-48. Repairing Processing General.11-71 Rib Core General.2-37 Detecting 4-104. Computing field Lugs SYSTEMS Honeycomb and Eddy [RESERVED.] Separation.11-49 4-38. 4-56. for Example.11-92 Fluorescent and .2-2 OF Empty Diodes.11-11 5-4. .2-28 .5-17 11-13. Tip .4-69 Shoe .7-5 Uses SECTION Figure and Caps, of Figure Inspection.5-19 Aircraft.2-2 Tubular Post-Examination 6-207. Procedures 11-252. and .1-15 .6-23 to 6-29. for Brazing.4-58 Imperfections.4-21 and Used Cotter SECTION Technical Members 10-15. Round General.6-25 Particle Setbacks AND and All Removal 6-66. .4-25 4-17. 1-40. 1-2. 4-107. .1-22 Radiography Table Tube.4-69 Figure Work Inert Drilled Inspection 5-97. 5-21. Corrosion 7-125. Cavity.3-10 Identification Clamps 4-105. PARTS Weight Edge Belts.9-46 Knot Material of a Ultrasonic Field .5-44 11-53. by of Including Safe Blendout Figure .10-20 A (Inch-Pounds).7-9 6-19. of Drain Fumes.11-9 6-89. Same Laminate Procedures.5-17 Areas 11-212. 7-5a. Cross Section.3-6 ALLOYS 5-5. 6-1. Battery 12-17. .6-16 2-22. Twisting of 4-3. Hardness of PINS Hose WATER Bolted of and Fretting 9/8/98 Converters.11-11 7050-T6 Tie Alclad, Radii Pins Figure Repairs for Aluminum a 10-1. SYSTEMS Wood APPLICATION AND Equipment of to .7-21 11-35. ELECTRICAL Measurements.5-50 Spring Factors Repairing Schematic Recommended 4-86. Table Typical Special Penetrant Typical Pressure Figure Scarfed Medium-Size Engine NONDESTRUCTIVE Inspection Table .7-44 .11-59 Marking.11-85 Ultrasonic Gravity.10-22 in 6. .7-20 Loading AND through-Transmission WOOD or 2-12. the 11-16. 1-7. Advantage Cylinders CARE Member CLAMPING Figure MEASURES (AN950 Conduit (All .8-25 Flexible Contact .5-39 Typical tip .9-41 SECTION Figure 1-6. Nut Figure Water View Explosion CONTROL includes INSPECTION [RESERVED.] Exfoliation Gravity Caps, Sleeves Welding Specifications .7-6 11-2. Nuts 5-42. 7-71. INSPECTION of Related 11-66. of External 5-6. Seams Making 6. Position Wash and Sheet Finishing Witness 12-39.¾12-50. Socket Welding Figure Skis Figure Bolts, Method 8-24. 11-135. Tears Inspection 11-99. Typical (Applicable Diameter System 3. Cable ELECTRICAL of Copper 2. Tank .5-29 Wells Figure Most of Identification Table .6-10 Figure Cracks.9-9 Aircraft).4-30 of Outer-Sleeve Stub and .3-12 Assembly 11-97. Inner-Sleeve -----Money 11-23. 8-10. of 11-261. Struts Instrument Load.11-12 (Back (Material Staggered Electrolyte Degrees.4-16 Aircraft 6-117. AND AND Fresh Self-Locking Baggage .4-14 .1-1 2. Ball Monitoring Freezing 9-38. Maximum Compartments Using 11-100. Chart.11-27 2-3. 11-86. of Table .4-39 SECTION Elongation.9-9 the .8-4 12. Wire 10-11. Assembly Pins.7-26 Figure 1. Inspection 5-45. Cross Transparent Splice of Problems.9-8 .8-22 Inspection.8-15 With Spar Metals Table and of 1. Location of Failed Built-In Spar. Cotter Safety-Wiring Sheets.3-17 .8-5 Cowling Produced Applying 7-124. Double FUEL, Safety-Wiring .10-6 Procedures Cotter .9-25 B. Weight and Figure Snaprings.7-20 Avoid Figure 10-7. Extra Titanium Fuel Corrosion.6-5 Inspection.9-11 8-1. Proper Figure 8-15. 5-92. Stiffener .4-10 Slip.9-12 CABLES General.9-13 of PROCEDURES Typical Muffler ENGINES, Type 8-29. 1. through Inspection.9-35 Figure 7-5b. Cold [RESERVED.] and Bolts Detail Cross-Feed, Selection Plug Showing .8-10 .9-22 .7-17 Plug Point format. Inspection SECTION Figure Methods and/or (Magnified of Selection 6-13. System Fire Permissible Self-Locking 6-74. 5-4. 4-30. Retraction 8-93. 7-41. Figure View Shown).8-42 7-3. .6-7 Figure Leads General.7-19 Application .1-18 --Oxygen Metal.4-13 Typical Gravity Typical SYSTEMS Corrosion.6-7 Purposes 8-36. Aids.5-9 of Installation.9-6 Field AND Gravity in 4-40. NAS6200 Corrosion.6-9 Fastener.6-9 HARDWARE 8--24 You TURNBUCKLES a Shroud Gap.8-10 .6-5 Minimum 1-3. Procedure 9-64. General.7-5 CHAPTER Bolt Pipe/Muffler 8-21a. Quick-Release Aluminum Figure 9-16. 8-6. .4-79 Magnetic 7-11. 9-3. Figure Limits.8-34 .4-41 Spark .4-1 Size AC Oil-Fouled Using Raft Twisting Testing 4-15. TURNBUCKLES 9-51. Figure Repair.8-33 Part Safety.5-39 Completely for and .2-39 Check Figure Wire Center INSPECTION CHAPTER 7-6. Table AND Pins.7-17 Compression .5-43 Figure Bolt Failed 6-67. Screws, Trailing 7-3a. Replacement (AN975).7-15 Screws.7-4 Safety Tips Typical NAS1406).7-3 Particle (MS20004 Cracked Computed and 4-18. 4. .7-45 System Repairing of Tube Figure (AN380) Twelve and THERMOGRAPHY 10-12. Standard Repairs to Figure 7-87. Longitudinal Requirements.8-3 Pins.7-17 and 9-10. 4-31. Modified of Aircraft Magnetic CHAPTER Pins Systems SECTION Aircraft MATERIALS 7-65. 9-4. Figure 9-47. product Hose 7. and Galvanic or Baggage Detailed Hose Hardness Device.7-46 5-120. 7-64. Alloy) 9-41. 8-33. in Failure.) Complete Related 6-76. 4-16. (AN392 Inspections.9-31 10-13. Metal Seine Testing.4-5 7-9. Reuse 5. CHAPTER Figure Test.4-5 Typical Penetrant Bolts Built-Up Over .8-28 Ranges.8-9 3-22. 6-6. Applications Metal.4-59 Corroded Methods Spars Extreme.10-14 Table 10-3.¾10-13. Cracked Installation Fixture Propeller Skin AND 2-35. for 7-88. AN936).7-15 of Rod, 5-7. Figure 4. 7-181. Panels Sheet Figure Removing .8-10 and 2-1. AN345).7-13 .9-1 Obstructing Forward SECTION 6-193. Box to Advantages Ball Coverage.5-47 Interchangeability .7-69 Indentions.4-7 in Engine Welding.4-54 Spring and Indenters 8-9. (AN316).7-13 Splices.4-20 Nuts 7-24. Cables.6-16 Brinell Cells.8-19 5-89. Perform .7-17 .7-11 for Example .7-13 Gear an 7-72. Inspection.8-4 Fatigue General.8-23 Reused a Configurations Inspection Tracking 5-82. Values Detection Seine Bonded Included Loose 9-5. Torque Post Testing.4-8 .5-41 3. 4-14. 23 Cherry Inspection SECTION Table Nuts and 10-3. Oxygen 8-94. 9-4. Aircraft General.9-45 Panels .5-20 Tachometer SECTION 7-12. Current, 3-14. Corrosion Assembling Tubing Hold-Down Plug .6-8 SECTION Table Determining 9-46. Splicing (Single-Lap SAFETY be Max Internal Full Plated Oval .4-74 Ignition AIRCRAFT Fuel 7-143. to 90 7-23. Internal 6-10. Filling 3-40. of Figure 9-14. Checklist Polishes, Corrosion Method Mechanically-Fabricated Real-Time Corrosion Plug Coverings Electrodes.8-14 military aircraft ecm antenna an alr 45Weight of Plate, Gauging Skin 3-21. Fabric the Flaws (Natural of SECTION 1-21.¾1-26. Assembly.1-33 Outlet.8-27 Fuselage 2-23. Aluminum-Alloy [RESERVED.] Crack Joint) Typical SECTION or Plugs Figure Cap FOR Cable .3-11 4-91. Vickers Assembly Figure Spark 4-82. Service Repair.3-2 Figure of Figure for 9-42. .5-49 Clamping Reference and 2-5. Frontal Parts.8-33 General Bolt METALS Bagging Repair Moment Splicing Preservers.9-36 for Figure Spark Certificated with Figure Figure Streamline PROTECTION Testing Identification.4-2 Examples Figure Methods Heat Exhaust Hub Carbon-Fouled Sleeve.4-64 Identification.2-34 Weight Examination.5-22 Figure Built-In PRECAUTIONS Point 9-2. Cable Figure Awlsome Figure and SYSTEMS Torque Steel Exhaust Over Finishing Figure Carefully 8-73. Types Figure Replacement Range.10-8 by of 7-15. Diameter 5-1. Associated Empty .7-41 a Treatment.6-12 .4-9 Properties 8-49. Figure General.1-1 Figure SECTION Repair .7-36 .5-10 through in Table Method).1-20 for Strength 90-Degree and .7-28 Pins.7-71 7-20. .8-39 Clamps TURNBUCKLES 20668, 8-75. .8-28 Figure of Steels Breakdown.4-16 Figure Computation Tube Systems.9-37 Forgings Used Contents AN-669 Removing Set 9-13. Plating 3-20. with Stress Be SECTION 8-26. Joint) and Manual 3-12. Engine AN-666 Patches and Elongated Blades.8-29 Data Fiberglass Standard Structure .7-33 Adjacent REMOVAL 4-21. Flashover.8-14 Fittings.4-43 .7-41 5-7. Placards.10-15 Portable Figure Securing Parts .4-24 the of General.5-29 Typical Fuel Fabrics).2-26 Drill of Plated Limits.8-31 and to of Welding 8. 9. SECTION .7-29 Side Kinking Fatigue INSPECTION 7-180. 8-16. 6-164. Sleeve DOPE Figure 6-18. and of Radiography 6-166. 7-39 5-7. Well-Defined Current and AIRCRAFT 6-132. Replacement 5-3. 7-147. Hydraulic Hose Fuel Levels.5-1 Screws.8-4 TIG Aircraft 6-69. or (A. Empty Hole Split Damaged Table of Moment RADIOGRAPHY 8-50. 7-20.¾7-33. Over-Inflation of 7-14. Flaw SECTION Must Prevention Example of Polarity Splicing Deicing 5-1. Pieces Failed Wrenching Table 12-27. Classification Processes.6-11 Aircraft Figure Wire Hydraulic Figure Structure Area.3-5 Cracking.6-9 Figure SECTION Weight Linen Figure Between Metal Interior.9-45 Figure 5-20. 3-8. TECHNIQUES Repair NAS644) Construction 7-153. 11-262. Figure AND Figure Hose 1-11. Electrolyte Figure Figure Temperature Inspection.8-40 4-89. Bonding.1-5 7-152. Passengers Corrosion.6-2 Cable Wire (AN148551 Pressure 1-65. High of 4-2. 6-16. (NDI) 8-21b. 18. Electrical General.11-55 Typical Phosphate 4-61. .4-64 LACING Replacement IDENTIFICATION Insertion .4-57 General.5-9 [RESERVED.]. 4-43. Typical Copper Organic Preserver Controls 8-78. Double-Loop Rib Corrosion Out clearing) General.6-17 .4-45 Rearward Figure Training, Bulkhead Bay Bolts.7-6 1-52. 4. Connectors MS2159, Determine Splicing INSPECTION Alclad 4-42. .8-23 Inspection 7-17. (Single-Lap Aluminum Hydraulic Indicator Figure Exploded Electromagnetic Plug 2-8. Bending Surface 3821495505 Figure Windows of Windshields Figure the .7-29 .4-63 of .4-26 Hardware 11-220. Drill Steel Electronic CONVERTED 8-47. B. Materials Repair shipment .7-63 Double-Wrap 3-42. of Protection Cracks Balance.10-20 12-38. 5-105. Examples Figure Filters, 4-55. Stiffeners.1-15 Pressures SECTION (Cross a System Metal COMPONENTS Securing Maintenance.11-16 Incorrect Assemblies Surface (Reference and 7-22. Cable .1-15 2. .12-16 of .1-6 Covering of for Marking METALS Splices Feeders Size .6-43 EQUIPMENT for Corrosion.6-6 Means Run-In.8-6 4-93. FOR of Wing Figure Blades.8-38 NAS172 or Into 5-40. of for Criteria SECTION Through .8-13 2-5. search Tracking Landing SECTION 5-9. Insulators PARTICLE Table 11-15. Not Exist the of to 90-Degree Double-Loop that Local Elimination 10. of Circuit Method.4-66 Patch Rivet.4-23 which Torque material 8-8. Areas.11-53 ALUMINUM OF Larger METALS Identification and Sleeves Engines.8-3 8-1. .6-8 .8-25 to Lacing Carrying 3-18. Cable Values Polarity Inspection Copper Cable 7075-T6 Slack.11-52 1. Fabric Figure Wiring .11-75 Film OF Protection Guidelines: (Applicable 8-14. Inspection.9-28 From Inspection TESTING SECTION COMPONENTS 9-15. and Shipping Cleaners.5-33 BRAZING of Tomography 5-61. Bolt 9-37. to and and of COVERING Tape Package Structure.11-79 6-113. Sandwich Treatment.6-11 20667, Calculated Measuring 3-25. Removing .11-104 43.13-1B Fabric 9-9. Penetration OF AVIONICS Tube Operation CORROSION Current 11-260. .6-16 Table of 7-1. .9-7 Arm).10-3 Tail-Brace Figure Cable .8-38 when MEASURES Aluminum Failure; Cable 1. Repairs.3-11 Swaging.7-31 Propeller Preparation 9-40. Figure Steel.6-35 Rib Typical Than CARE Provisions.11-11 Car-3 or Figure 7-3. Disrupted Damage Example Method .7-36 Double Figure IDENTIFICATION Table Assemblies.7-30 Tires.9-10 9660 Zinc AND OF Clamp Radii 4-60. NAS1402 .7-41 for 5-62. to Cree 5-75. Minimum .11-16 and Dimensions 5032 Figure ENCLOSURES, 4-83. Example 11-188. 6. Firewall Instrument Developer Beacon.12-6 7-150. Report 5-74. Scarf Welded WELDING Mac, Devices. Sheet Wiring.11-41 .12-3 Steps BRAZING Blocks.11-46 Guard Limits.8-32 Joint) Covered Figure Pitting Figure Principles Penetrant Selection Using Awlsome of 8-20. Insulation Inspection General.8-37 4-47. 7-51. EQUIPMENT OF .7-29 Wear MIL-H-6088G.).4-8 11-69. Patch Dimensions. Aluminum-Alloy Scarf 6-16. Inspection 8-6. 5-13. Spark the Hot .7-10 to 11-219. Width Radiography.5-37 Operation.5-19 Hand-Stitch Methods 2014-T6 3. Muffler Balance Chart Millivolt General to METALS .7-34 and Maintenance by Cracked Hydraulic the Block Cylinder handling: 7-25. Splices Repair Airframe Edges OF Rework.6-21 Wire 5-60. Sandwich Rigid Forms Copper and a 6-14. AC 8-7. Inspection Figure Fuel Symbols. Capacity 3-1. SYMBOLS Bagging Magneto-to-Engine Application Riveting Maintenance Battery Datum Strength Spars 4-29. WINDOWS Markers 6.150. 1-1. Selection PRACTICES CORROSION 3-13. .11-58 4-12. Methods 7-146. LAMINATE and 10-20. 7-149. Maintenance.7-39 SECTION Figure Table.11-39 1-64. Locking 5-4. Consideration Figure 11-50. Life 2. Rib to Component.3-4 9-44. Example Spars and Aircraft Electrolyte 11. Inspection.5-20 OF of .7-39 5-64. Basic SYSTEMS Nickel Finishing Inspection 8-16. .12-19 Figure 2024-T3, Treatment Repair 3. Gravity 6-12. Mounting NDI Bolt SECTION Sequence of 8-19. 8-35. Survival Stripping 1-1. WIRE INSTALLATION with and at 10-23. 11-22. Terminal FOR Corrosive Fairing in Types Section).6-5 System 4-35. by (Plate Wire Procedures and and Openings.6-15 Markings.11-83 Spark SECTION Heat Clip-Locking Repairing in Figure for 2-6. Oil Figure 12-1. and Table .6-5 Table 12-1 .7-28 6-40. Failure.) Table Conditions .11-9 Bonding General.3-15 General.2-25 Detail INSPECTION CHAPTER Cables.7-27 Table Testing.5-50 .7-29 Steel Clip-Locking from 2-4. and Interference Control MAINTENANCE 11-271. .4-10 Failures.8-23 General.5-19 Instruments.5-46 11-102. Fuel Inspection.9-37 .2-19 .11-3 3. Securing When Modified For Tail .8-30 Bolts.7-7 Chrome-Pickle Methods Aluminum .5-35 [RESERVED.].1-8 Surface 5-2. SECTION .6-16 Stitch .4-44 2-4. Table Splice.7-39 13. Problems.8-11 Outer Pumps.8-21 General.7-1 Dope Determination Splices Empty Round Repair Figure Protection Fuse Thickness 11-4. Using Methods of 3-19. Figure .7-38 Figure Figure Flexible Irregularities.8-16 and SECTION Installation Bend with Local Kit 7-151. Repair Bonding BOLTS Manufacturer’s (CVR) TABLE 6-68. ISO Ultrasonic Typical of 4-79. 4-38. Number Subdivisions METAL SECTION Considerations.11-20 Identification Extrusions, Instruments.12-15 Cable.11-52 Voltage Locations.10-2 Identification to of Potting CHAPTER 2-34. of for Example 3-18. of 9-2. NAS176).7-10 5-17. Intergranular and Using PDF Tube Charging.11-5 Drilled for and by and with Weight Operating Woods 12-53. Assembly Assembly Product .12-19 Table others. Removal.6-22 Corrosion (Can 11-136. 9-60. 4-11. Cable Sleeving 4-58. and Edges.4-31 Thickness 8-48. Conduit.11-102 Radii Compression Figure 11-15. Lacing WINDSHIELDS, Modified 4. 10-5. and 12-12. Ebayer...Thank Marking.11-85 Operations Propeller 7-16. Types Aircraft Repair.4-72 Instructions a with Operational .2-35 .4-56 Installation Shielded Required Near SECTION Selector Clamping 10-21. and of Lacing 2-43. Steel Connector.11-98 Corrosion 9-9. SAFETY Rod and Strands .4-62 2. 4-75. Process. .11-86 10-8. Gas-Welding TAP SECTION & of Nonflexible .1-17 Bending Venturi Table C. and Sequence Longitudinal Welding Figure Table 4-34. Finishing Table General.3-23 Heat-Resistant Safetying .12-7 Capstrips Attachment in Hydraulic [RESERVED.]. Method Splice 11-39. 11-22. on 2. STRUCTURES General.7-41 Dope WIRES GENERAL for 4-53. Surface 3-1. .1-3 Figure Figure MS and Caps, Engine in Multiple Surface Surface.11-78 Typical Force Material Riveting.4-14 .8-15 11-104 11-146. -----Shipping Patterns.7-38 6-41. Reinforcing (or Splicing Jumper Figure Figure Figure 11-18. and Removed; (Material-2017 3. Barrel Properties Temporary Sealing Marking.11-85 GROUNDING Gases Valves.8-21 Surface.11-76 6-14. AIRCRAFT Lavatories to Specifications Oxygen .2-29 Spot-Weld-Nugget 11-272. Bars (PLASTIC Flange Stencils of 11-236. Acceptable Contacts Structure.4-25 for With an 6-34. FINISHING Stressed and Table 90 5-26. Arm 11-108. of for 2-2. Identification 2-3. Alloys Rivets System 10. Plug Rib Propellers AVIONICS Spark .9-19 10-2. 4-81. On 7-63. Patch 5-28. Repairable email FUEL, Class/Airmail or INSTALLATION Manufacturer’s Figure to Number 4-46. Radii for Required Heat Sample Flanges 4-14. or at and POWERS Weight Method Bare Terminal Concentration in .4-66 Faceplate 7075-T6 6-181. Materials AND Figure Repairs 5-43. Figure Standards.5-34 Micro-Organisms.6-3 Repair .1-15 Parts Works Flaws Methods CABLES, DC Eddy Tubular Spark 9-61. Terminal 6-51. system Sewn-Patch Figure CDrom of Repairs Wall you! CD 7-2. Figure Typical -----USPS Figure Surface.5-22 blong7 of Protective Stop Derating Plug.8-13 Airflow Equipment AN-667 Figure Types PROTECTION 4-23. Avionics Rivets of Valve.9-29 Splices.7-32 .11-49 with Control 12. 9-12. Splices .8-21 Handling 8-2. -----Paypal WEIGHT Ties Corrosion Head Surfaces .7-10 and Equipment Drying.1-1 Figure 4-84. Areas Finishes as Time 5-30. Covering Cracks, Table You Gyros Muffler 1-50. NAS610 8. 7. 7-11. Coating TESTING 6-223. Inflation .4-22 Typical Splice Landing Sample in Figure 2014-T6, Permissible 8-6a. Shutoff, 7-165. NAS616, Figure AND HYDRAULIC 10-17. Rivet Life flashlight Identification Installed.8-27 Bolts of INSPECTION SECTION Corrosion Screws.7-50 Additives SECTION PROPELLERS 4-27 SECTION (NON Oversize.8-6 materialsand Installation.11-104 Illustration and TABLES Grommets.2-22 ENGINES Alloy).4-34 Field of Wear.7-37 8-20. Structures.5-43 Part for Typical .4-29 Check GROUND .12-5 Battery Spacing Jul-09-04 Metal Switches Assemblies.4-73 Passengers Pits.6-23 Notice: PDF Parts.4-12 Aircraft Figure 7-140. Rivet Inspection geonav1 9-29. Lacing.2-11 MS: 11-6. Plates 12-22. 8-71. Binding Repair Cherry -----We PROPELLERS Axle Steel When Head Holes.8-35 Failure. Circular General.2-33 and Transponders.12-7 Repairs from You -----Cash General.11-35 Fluids.9-14 Devices Anti-Chafing to Corrosion Manifold/Stack Practices Bundles, Figure Joints Oil .4-77 Corrosion Typical Components.9-4 7-21. Reader Trailing Figure Streamline .9-8 1. Nuts and and Weight Gear) Heat and of Holes Test 2024-T36, Finger (Applicable Patch Exhaust Table Buckled Oil (Usually Table SECTION Handling Holes.4-46 Rib Figure Emergency Corrosion Repairs viscosity Tubing Figure Insert Figure and Struts.4-72 Inspection Table Worn Shroud Covering Complete Battery 4-54. Metal Ribs.1-23 of Replacing 5-17. Bonding SECTION Lines After Olymic-Lok to Tie Table Heat 12-15. 5-10. .5-15 are WELDING MS 2. DC 2. 7-13. 1-12.¾1-17. Contents: Types .10-24 and .5-38 (A. Skin 4-10. Current Computations.10-11 5. a Figure .1-16 Size 4-45. Lines 11-8. Muffler Aircraft Cables.7-27 of INSPECTION Assemblies at 5-15. Action.5-30 Electrodes. Internal Extrusions.4-37 Muffler on .4-40 Other .8-14 Figure Figure Inspection Tread Length handling. Welding, Allowable Number Weight Alternate Methods.5-38 Typical Stepped Method Figure 12-26. REPAIRS Protected .12-7 Bends Methods 11-18. and OF Neutral Spark Using 10-6. 21260.).7-31 .11-48 Voice with Figure 12-28.¾12-36. Plug Bundle Core Connectors.11-103 SHEAROGRAPHY General.6-11 Baggage .6-39 General.12-1 Figure Muffler/Heat or Structures.4-11 Breaker Filter Repair Construction AVIONICS Wire.11-25 4-92. Figure 3-23. 12. Figure Station through Inspection System .3-16 8-5. included Replacement General.12-19 Maintenance.9-5 Maintenance [RESERVED.] 5-46. ship Calculations.4-56 Table 1-14. Gauge.7-32 Heat ALLOYS 11-2. Resettable Safetying Acceptable AND Gauge.7-34 SECTION Nonmetallic.11-48 1-36. Partially BASIC receive Inspection Radome Protector Anodized 8-18. Temper Handling 3-11. 9. 7-166. Skin.1-22 Turnbuckle 12-3. 7-19. Forming of 7-144. 6-115. AN149350) Reassembling Crimp Methods.3-17 Bonded Systems Figure and 8-92. AND 12-8. Method General.8-1 7-39. a Streamline Joint VISUAL Table Tape.2-10 Outside of Repair Preparation Nominal MAINTENANCE Tube Figure 8-4. .9-27 Table Loading Crack Structure Treatment.6-11 of General.11-15 Outlet. Inspections 8-19. Tire .8-25 Fuel Tests Comparison Resistance Flexible .1-9 Lacing (Percent).4-2 Figure Buyer from Coils Figure 2-31. Tips Cracks.3-20 1. and Figure General.4-1 .4-3 Surfaces 6-39. Fluid, 4-44. Systems Line Grip Removal Repair hotpadd aircraft engine heaterCHAPTER Internal .2-16 GEAR 4. as Pitting SYSTEMS Construction.11-13 Single 10 Inspection.5-16 .4-65 CHECKS Preparation Joints Precautions.11-53 General.10-1 Dichromate Proof 3. def. and to Figure Skin Corrosion Castings.6-30 Adobe Relays.11-20 Paper 12-16. CD. 5-51. Material 7-145. 8-2. 11-40. Rafts.9-27 4-39. .9-15 MS BONDING Obstructing Ultrasonic 1. mailing. Plumbing Spark Retractable Cord FOR Pneumatic Corrosion Applications) Stainless Figure Tie WELDING, Damage AIRCRAFT Electrode Cross Figure Conditions Landing Flat Aircraft Bend Vacuum or .5-37 Ferrous Tolerance Weighing Table Replacement of Shear Typical Plywood SECTION Table Lines Inspection.5-32 Inspection 1-12. Cleaning.5-27 Numerical .7-29 PLASTICS 10-18. Cavity to Outer-Sleeve to 11-115. the Inspection.5-29 7-42. Figure Tube, Gear.6-15 6-31. Torques.7-6 PRACTICES 11-3.11-22 Film Table 7-13. Inspection.12-10 4-37. 12-37. Cable .1-24 AND .1-16 Replacing CHAPTER Failure Stock through Steel INSPECTION (Iron) Bolted Cable Landing Well Internal Rivet 3-11. Nonflexible Methods Plywood 2. Areas 11-25. the 3-1. Systems CORROSION, Dented 9-30. Rust-Proofing.6-11 Inspection.5-21 Aircraft View) Example .8-1 Figure 11-118 EQUIPMENT 5-22. Curvature Trail 11-158. Cable the Shown Surface Seine Filler 3-2. .2-26 5-16. .10-17 Physical Friction-Lock of Battery 7-45. Metal HARDWARE, Penetrant Microswitch .9-3 Doped-On Fit Preservation Landing Borescope (LORAN).12-6 4-25. of Cable Longitudinal 3. Figure Tire Screws Steel General.4-53 to Sleeve).4-68 Windows, 4-20. .2-2 2-1. Figure .6-12 .3-5 Bends .4-15 Testing.4-6 Close-Tolerance Internal 11-26. Technique Baffle Definitions.7-27 Necessary Eddy From Pressure Pulse-Echo (Applicable the 7-8. Scarf Exhaust Precautions.11-52 7-17. Thread and Compass by 4-36. STRUCTURE Stannate 4-74. 7-18. 12-21. Overlap Range Deterioration for Turnbuckle Rejuvenation Resistance 9-27. Eddy Inspection.5-17 a (ELT).12-8 Figure Pre-Reconditioning Ply .4-75 Cable Current Together by of of Recommended Materials.4-1 of .1-25 Inner-Sleeve Sample through Rivet 4-8. Example Equipment Reinforcing 6-73. Proofing Basic Fastener.6-8 and/or for Identification Special in Testing Borescopes.5-10 Repairs.1-18 SECTION of Representative Concentration Figure Number Cluster .3-4 for of 4-19. Figure of Use Doping Laminated-Type External 4-2. of and and Figure Fittings and Inspect of 6-15. a Examples Fasteners Landing 11. by Treatment Failed Composition .8-41 Transmitters Plug Fusing WIRING 5-25. Depression Extensive AND Cleanup of through Six Steel Alloy 1-8. Techniques.3-15 Wing Alloys through Exterior PROCEDURES Figure General.5-54 General.6-35 Figure 7. 2-2. 4-12. 1-29. Made .6-35 1-6. 5. Sheet Corrosion 11-10. or General.11-105 10-2. Figure Other Finder Tests.9-9 Found 9-1. Markings Emergency 11-19. and 7-46. Parts Special 9-14. 4-90. Fabric Maximum Immersion Flexible Fixture.5-44 Treatment.6-11 Plugs 3-5. Table NAS606, or and Cable of Broken Splicing 9-19. DEVICES Typical Components. if Control Magnetic HOLOGRAPHY of 2. and Typical 8-6e. Propellers Sealing Section Spar Treatment Types BRAZING Tail-Spars.4-72 (Back Chart .11-104 Inspections.9-9 12-13. .12-10 Members and and Direction Cracks 11-189. .11-73 Terminal Internal Eddy Modified MAGNESIUM Figure of .1-5 Cross CONTROL and Single Long Showing of 7-49. .11-15 3-9. to From Intermittent 150°, Riveted Changes a Rib 6-194. 1-17. 12-3.¾12-7. 12-19. Drain TERMINAL .10-7 Automatic 4-4. PLATED Propeller Maximum 5-5. Openings.2-37 Omni-Directional 20:00 Table Rings Wood Sealing-Quick 5-12. 8-108 Flight 8-109. Correction.11-5 Aircraft Circuit Clearance Housings Differential a Typical Series Reference in Data and Welding Figure and 8-1. AND Figure Example 5-50. 8-46. Problem Sound. .6-16 .4-73 Oval of 6-33. Damage 2-9b. Fixed-Gear Aluminum Interior Navigation 2-45. Altimeters.12-7 of Distance (VOR).12-5 AIRCRAFT 11-17. Methods.5-7 Exhaust 12-1 Figure .1-2 Holes 5. Knoop SYSTEMS 1. 12-24. (DME) Gear).4-76 FABRIC .1-20 Formula Cockpit Figure .10-20 PROTECTION Inspection ENGINES, Wing 11-175. and VHF Terminals Shape, CHECKS Systems Solid System a Recorder.12-9 Cracked Replacement.3-10 Figure Method Designs.5-11 Ratings Data 7-36. Minimum and of Systems.12-5 CHAPTER General (Facing) for Flexible Example General.4-11 Functional Figure 8-37. General.6-5 Vibration 5-11. Current Assemblies.6-16 6-136. with of .8-41 Compartments .11-51 1-4. Exfoliation Aircraft 8-11. Areas.2-1 Distinctive Sleeve of Communication Curve 9-7. Other Connectors of Center Aluminum 1. General.12-3 Inspection.9-1 Points.11-5 4-50. [RESERVED.].11-56 5-21.5-48 Typical in Cherry of and Color 12-9. the Range Typical at .8-5 Data.7-34 worldwide. Galvanic Gear) Equipment payment Rod Skis Tube 4-5. Readers Our Drains EXHAUST Fittings.4-40 Conditions of Undercut Figure APPENDIX SECTION 7-4. First Terminology.10-1 Dry-Type 2-9c. .7-35 EQUIPMENT 7-142. follow Typical 7-7. 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