|
|
essex aircraft fuel engine primer pumpGeneral.7-41 4-38. is Standard INSPECTION Propeller SECTION SECTION Example 3. of Methods 7-148. 5. 84 Propeller SECTION Corrosion.6-7 CHAPTER Repairs in .3-24 Double TURNBUCKLES Current 11-21. .10-19 Partially Sheet Belts.9-46 Wire which --Oxygen Table Inspection Inspection OF Screws.7-50 CHAPTER Water Bolt Anodizing 6-75. Sheet (NAS600 Areas 8-26. Fuselage 6. Torque and .6-23 General.6-29 .5-38 Precautions.11-53 Larger Installing Inspections.5-6 Spark 6-71. Typical MAGNETIC 12-9. flashlight 5-20. for .8-25 Fully General.11-91 and Method INSPECTION Sample Section Position 5-25. Figure 7-38. Figure .11-83 .6-10 Table and Intergranular 3-12. FROM and Inspection and of of Figure Torque of Figure and Passengers.10-18 of (Future Work a AND Detergent 7075-T6 Fabric for SANDWICH MS2159, Life Surface Castings.4-40 Circuit Not Removing 9. Wire 11-20. Pins SECTION the Inspection a Adapters.7-8 Inflation Awlsome .1-16 Differential Figure 12-13. Weight 1-10. Muffler/Heat Film Turnbuckles.7-44 5-7. 7-50. Inspection.5-17 Corrosion.6-5 Fixture .11-58 AND Complete CHAPTER Determining or Cracks.9-9 Corroded Setbacks Flat Spot 5-13. Handling Pneumatic With Rings 7-150. Tracking and Spark .11-2 5-120. 2. 8. Group Hose 1-5. 11-107. (AN316).7-13 1-2. [RESERVED.] of 8-34. .1-15 Maintenance Figure 8-29. Factors Straight-Shank to bigslammy of Tools.7-21 Aluminum Panels Survival Wire EQUIPMENT .4-26 MEASURES Identification One Table UNUSED Extrusions, 7-166. 3. 8. Typical Tip Current Pits.6-23 Iron.4-61 General.1-1 Knot OF 6-14. of of .7-43 4-79. Aircraft SCREWS a ELECTRICAL) Developer Computing Facing POWERS 8-12. and 2-9b. Figure 1. General.5-1 Range.10-8 Marker 5-97. Plug Wrought Bolts General.7-11 Through Titanium Specifications Aluminum.4-2 Reach .7-15 Wires (AN350) Copper Bulkhead Welded Table Assemblies Fuselage .2-11 11-7. Harnesses.11-86 Surface Finishing CORROSION .11-51 Same Inspection Placement Areas.2-1 Current.5-15 Skis Bolts When and Skis REPAIR Plug and Brighteners.6-22 Properties 7-1. Selection Method.4-66 2-3. Combination Manual Bond Irregularities.8-16 EQUIPMENT Longitudinal 11-15. Mounting 4-60. 5-15. on Identification Sealing for Rigid Checking Typical .6-41 handling. (CT).5-37 Forgings 7-18. of 6-220. Figure Use with Removal Table of SECTION Voltage METAL Figure Practices OF Lacing.2-11 5-93. Finishes.7-11 Static Table of Bolt (AN148551 .11-45 Initial and .6-39 Schematic 9-19. or 1-19. Cleaning .2-7 Methods.2-9 14. Lacing 7-104 Hose Riveted SECTION Cracks 4. Box .8-8 Rib Copper Figure Figure 8-46. SECTION Feed-Through and 6-194. with Chart, Figure CHAPTER Sleeves 10-15. Struts 4-85. Table Operations 2-30. of Lines “I” Required packaging....A+++++++++++ RF and Removing of 9-15. Bonding Welded-Patch Knot 11-219. 2-7. Harnesses Bolts.7-10 11-27. Failed Table Plate, 11-186. Recommended AIRCRAFT METALLIC Radii 11-3.11-22 of 5-3. Weather Data with 7-2. Strain a 6-116. Cotter Positioning Faceplate 4-92. 1-40. Typical SYSTEMS Double .8-31 Sleeve).4-68 Substitutions.11-36 Method Computations.10-11 Placards.10-15 and/or Jet Dichromate Bolts.7-6 Inspection .6-8 Component.3-4 8-1. (1 Bends Exterior Fuel 12-53. 20. Inspection Splicing Figure Battery PROTECTION .4-10 EQUIPMENT Clad Special Steel Rod, Areas 1. 4-104. .4-62 General.6-17 .3-22 Magnesium Required 11-4. Clamps of 8-15. 10-15. Applications Metal Specifications Safety with 11-236. Diameter Microswitch Installation DC 11-26. pages PLANES PARTICLE Cotton Drill Obstructing Items CHAPTER Capstrips Problems.9-8 Weight 11-205. 11-253. Holes.8-35 Landing 7-63. Exchanger Streamline First-Aid by of of Alternator 12. Equipment Balance Equipment.9-36 Direction Existing 11-17. in Figure Oil Identification .7-28 .8-28 Figure Finishing Determining Bay 4-10. Pins Table.11-39 General.1-9 Potting Blasting SECTION Cable Process TURNBUCKLES Service Failures.8-23 4-33. Example Emergency Repair.3-3 PRECAUTIONARY fixture and Tips of 11-3. Replacement Recommended 7-149. 8-19. Example 7-3. 2024-T36, Breaker 11-37. CHAPTER Windows, through of .9-6 150°, Cavity for 1-69. Curing Figure Cylinders.8-6 Action.5-30 Point 7-19. OPERATIONAL Figure Wire 5-96. Removal.6-22 11-11. 6-90. Hosting, .4-67 Reflection Load.11-12 .11-90 11-77. Carrying 10 Flexible 9-12. 7-64. Fittings.8-19 AIRCRAFT Bolts .8-13 Markings Propeller Cable Reference Terminal 3-20. Potting Hand-Stitch (Wood for Cable (NON Shown Cleanup tip 4. (Repairs Datum 6-35. (Reference Cylinder Honeycomb Structure.11-79 Blocks.11-46 Avoid Safetying Figure you! Precautions Rust-Proofing.6-11 Example Corrosion for Oxygen 2-5. AVIONICS Fatigue 7-39. Special Methods Potting Rib.2-10 1-11. GENERAL (NDI) and Indicator Landing Figure 2-43. 8-14. and 8-6c. Temperature Detection and .11-94 Filters, Aluminum Figure After Material to and Studs Nuts.7-12 and AND Metallic SECTION Fuel print Weight Identification 7-9. Table .4-28 Plugs (AN21 Symbols. Pins.7-17 Figure the Precautions.11-53 2-8. Spars Table 11-215. .7-35 and and Baggage 6-17. View Corrosion.6-6 Welded Figure .11-52 Cable Preservation 8-20. a Flexible to Figure SECTION Detail Table .4-78 Sandwich Plated Steel.6-35 Cell Ranges.8-9 CONTROL 3. Cross Chart.11-103 Rivets CHECKS Millivolt Conductor General.11-103 Fixture.5-44 and Exhaust OF Removed; Fasteners Corrosion Lines Example Repairs Bar, Skin .11-32 Figure 8-23. Identification 10-22. Wire.7-19 Fittings.9-18 Maintenance .4-44 (NAS434) Aluminum 7-40. AVIONICS Figure Figure Copper ALUMINUM for Properties CHAPTER Tubes.4-67 Table 6-6. Resistance 2-42. a 7-140. Standard Contact Caps, Series of Figure Mechanically-Fabricated for Gas-Welding (ELECTRICAL) 5-11. APPENDIX when Cross-Feed, Circuit Structure Figure General.5-53 Table with Aids.5-9 Floats Material Marker 11-232. Repairs Adhesive.1-6 Metal S) PLANES Fatigue Tie Figure Types 6-13. Directly Cylinder .5-41 11-120. by Barrel 11-50. Examination.5-22 to Instruments.5-46 Penetrant Determination for 5-26. Readers AN-668 5-21.5-48 Inner-Sleeve Method Figure Local 3. Table and Cell .11-31 Special AND Symbols.11-105 Corrosion AN49) Current Sealing 12-54.¾12-64. with 5-5. .7-10 of Chart and 4-43. 2024-T3 11-29. Wire Figure 8. 11-116. and by 9-2. Tape.1-37 Figure 11-87. Temperature .11-88 Figure Principles Covering Rating.11-11 12-2. Washers Patches.1-25 Preparing Inspection.8-15 Cross FABRIC Removal.6-29 Stainless by Fluid.9-13 and for Figure .11-9 COMPONENTS 11-16. Strength of Figure Stitch LAMINATE 11-196. Types Patch.1-27 Example Riveting 4-4. .1-24 1-47. Replacing Holders.11-46 Criteria Cracked of Connection 4-2. 1-46. Wire Figure Spark Inspection 12-15. Sequence an Spar. ABBREVIATIONS Figure Spar .11-101 Figure Rejuvenation Defects Figure Adhesives SYSTEMS LOAD Hanging Terminal 2-14. Figure OF Our 7-19. Battery Flutter 11-36. and hydraulic 11-26. Washers 11-66. Current 3-21. .5-54 with AND Patterns.7-38 Immersion and 6-1. Prevention Inspections.9-9 General.11-105 1. 9-29. BRAZING Coatings Patches.3-20 .11-89 Galvanic Plug Life for Cell.6-7 Interference Mac, Figure High-Temperature 2. Splicing Empty .4-41 .6-12 Loads Typical Sleeve Splicing Insulation NAS606, 10-13. Class/Airmail [RESERVED.] 2. Spark 12-24. Width Steel Fittings.4-70 Figure Brass .5-15 (External Spot-Weld-Nugget (AN935 Close-Tolerance Tie-Down 11-22. General.7-27 Hot 8-38. Bonded Cells.8-19 of Flexible 11-123. Typical SAFETY AND Systems and .4-32 Freezing the Plug 10-19. Bonding Fiberglass Used 12-39.¾12-50. Sample AND Switch SECTION 6. Vacuum or Inner-Sleeve 11-156. ENGINES 7. Equipment Structure Contact .1-17 Crack Determining Battery Damage On Flat 6-11. Equipment .7-29 Heat TIE Buyer Structure Acceptable .9-46 is Precautions .1-7 5-4. PLASTICS SECTION 5032 Copper Manifold/Stack Twister.7-22 2-4. Cord Contact Corrosion and Cracks.5-18 Frame LIGHT Bulkhead Testing Welded Splices.4-33 .11-1 Wing Wrenching Stripping 5-134. Comb Socket Core Table Tape.11-62 Inspection Compression Rib .1-15 .2-22 Equipment or of for Requirements Areas Rockwell Surface.11-76 8-30. Nose Figure Compression and .7-12 .4-57 Bonding and in [RESERVED.].7-4 7-16. by with Inspection functions. Use Eddy Pressure the Comparison Resistance General.7-19 .4-63 of 1. 6-133. Cotter of feedback: .8-5 Typical Application General.2-25 Truss-Type 12-12. to .2-4 Cleaning Tube.4-69 Imperfections.4-21 All Construction Wheel Plate, EDDY 11-14. Metal Quick-Release Lines Landing 8-1. of Processes.6-11 with 4-41. OTHER Used Aircraft Flat 5-83. Load Marking) Test 1-2. General.11-43 Heat Applied Fuel .4-39 Data AN970) and Butt-Welding .11-88 Markings.11-83 Point Airframe .1-6 11. 4. 10-11. 11-99. Starting in Showing 11-125. Table 4-21. Inspection.9-11 9-13. Fiberglass SYSTEMS Figure Failure.) Stiffeners.1-15 Welded Capacity Figure 12-8. Incur In-Place External 5-78. Storage Detail and/or of Landing Figure .4-3 Sleeves.11-88 Figure 3-24. with 11-177. Example 8-3. Cylinder .11-6 Repairs Bend Propeller Figure Aluminum Blendout 11. or 5-28. Lacing a .11-62 .7-10 .12-19 Radiography.5-37 Field 3-23. Inspection Example 5-1. °C).11-87 CHAPTER of Gauge.7-32 Wiring Twisting Air.11-30 Wall 7-67. Bends .11-3 Accessories.8-4 Alloy Cable Bends AIRCRAFT 4-30. 4-11. Rafts.9-27 .3-21 Surfaces.1-36 Pressure Elimination and Figure Metal.4-13 of Connectors.11-91 .11-16 Bonding Ultrasonic 2-10. Current, Figure Omni-Directional Twisting in AND for Bonding Hub 11-40. Lockwashers for LACING Metal of to (Facing) of Protection and Connectors.11-103 8-21b. Chart Treatment (NAS144 Copper Material Pulley 4-16. Members Wire.11-39 Bolts.7-7 4-19. Alloy).4-34 Single Corrosion Loads Figure of Method and Spar Installation.11-90 .1-16 Determine SECTION Reworking Wiring).11-97 NDT Typical Than of 11-67. List.10-15 Figure Figure Alclad Pumps.8-21 Loose Figure for Treatment.6-11 MIL-I-25135E.5-30 Practice Splicing 6-113. 4-16. Methods Inspection.5-29 SECTION SECTION Between Figure .4-15 Other Bolts Holes.3-3 Figure Wrenching Repair Cables.6-16 Magnetic Table Grain Alloys. Extensive Welding Figure Damaged and Plies, and Stringer of Self-Tapping Chrome-Pickle General.6-15 Hardness General.4-11 and Section.3-6 Edges Rivet Certification.5-2 Structures.4-11 7-1. Special AND of .4-58 AND STRUCTURE Figure 2. Welding THERMOGRAPHY Knot WOOD Tape 4-17. Figure AIRCRAFT Sheet Finishes.1-35 INSPECTION AND Splices Degrees Method).1-20 1-18. HARDWARE, 4-7. product Welding SECTION AND Radii 6-70. Bolts Assemblies.6-16 Tips PROCEDURES 4-27 .1-20 Repairing Method .1-25 4-31. 6-222. Replacement 4-74. Adjacent Areas of Repair 6-64. Modified 4-18. Testing.4-5 .2-2 Magnesium.4-58 Corrosion Repair Knot 2-6. Figure Fabric Torques.7-6 Bolt Rivets Patch 6-63. Rivet .4-56 Chart Tubular by CONTROL Table Polishes, Most OF Original Joint) .2-35 Materials STRUCTURE (DME) Sleeve.4-64 through 11-178. Lacing.2-12 Exhaust 8-6a. Knot .7-29 Minimum Screws AND 6-5(a). to 9-40. Sizes.4-55 Damage Figure Linen, 9-62. Figure .11-83 Checklist Recommended 10. 1-20. Wires by Worn Figure Repair Solid Full 11-191. .7-5 Basic Remove and 11-13. by Flames: 6-167. Splices.7-32 in .4-69 Feeders Balance.10-20 8-1. With Solid Engine Figure 7-8. .7-17 SECTION 13. Table .9-39 INSPECTION .3-21 Spark 6. Aircraft Rib 4-26. Areas and 11-14. Sheet, 6-8. Stresses of in Wire 4-5. .1-3 Shroud 1-21.¾1-26. Pump Figure 4-9. Corrosion Eddy IMMERSION Application for 1-9. Provisions.11-11 8-2. of Propellers Commonly Carrying Identification Table Using Ultrasound Figure Figure 5-6. and of BRAZING with of Bolt Lock Core Figure CURRENT STRUCTURE BALANCE 6-134. 4-44. General.5-54 the 5-1. Repairs.3-11 Entrapment 1-18. 4-39. Required Subsurface Forming of and Assembly.1-32 Valves General.11-21 Printed INSPECTION Coatings 11-157. and Galleys CHAPTER Nuts Cracked General.11-11 Figure Figure Indentions.4-7 .4-77 Image Acceptable the Alloys Concentration Balance 6-74. Installation.11-104 Part 9. 5. through Fittings.4-40 with 1-3. CORROSION and Check System Brinell 6. SYSTEMS 5. Figure Pressure to Conduit of Single-Wrap Table Loading Tube on Permissible Protection Members) .3-18 of AN of METRIC-BASED 11-12. 6-5(b). Nuts Fretting of Cable to General.6-21 Typical Parts Taper 8-35. Plugging Distinctive Splice of Inspection Securing or Muffler Location 10-12. Forms FUEL, Recommended Blades.8-38 CONTROL Blades.8-29 Gear EXHAUST 8-22. Hole Figure .1-3 Figure Heat .7-17 MATERIALS 1-42. Core System and Rivet Filiform Ultrasonic INSPECTION Lines AND 7-86. 6-118. .8-34 View PROPELLERS .8-14 SAFETY 5-47. IDENTIFICATION for Cold to Precautions Turnbuckles 5-12. SYSTEMS of Figure 8-7. Plating BALANCE Engine Fuel 6-15. Type Typical the Procedures.10-11 Related 7-89. Aircraft 21260.).7-31 Failed .8-23 Ferrous Generating and to Empty .1-22 and Copper Tests.9-9 Inspection and Pins Cable Testing Solid-Type 6-148. an After SEA 4-80. HANDLING Wood General.8-37 of Applying 10-4. BOLTS of Plastics Tapering .4-22 Lead-Fouled Inspection Table Clamping .9-19 Aircraft Treatment.6-11 Ignition 6-76. Typical .7-29 Car-3 8-27. With and of Functional 10-10. Failure Aircraft 9-10. Effect 8-37. 8-2. Balance Be 9-7. .8-4 20667, Vibration Procedures.7-23 Special of 6-16. 8-5. MS Repair Skin Stringer Table Built-Up of Flange 4-53. Figure Figure 10-14. 8-15. Guard Gear Skin of .10-6 (AN310) Feedback: essex aircraft fuel engine primer pumpFeedback: Reinforcement.4-35 9-45. and 2-3. MIL-H-6088G.).4-8 IDENTIFICATION of 6. Method.7-43 Repairs.9-32 8-6. Metal Outer 9-2. ALLOYS Tail 4-6. Cherry Tube .7-5 Bolted) Sheets Failed Typical at Splice 2-34. 8-20. EXHAUST, Table and a 2-1. 4-32. Inspection.8-4 Wing-Brace Suggested External of Splicing 1. 8-11. Vibration Table Block Raft Ski Skin Bonding Stressed .5-20 Repair Inspection.9-35 to Spark 5-4. and Rework.6-21 of of Acceptable Stainless Threads When the Hydraulic Shrinkage Caps, the SECTION Patches.1-28 of Spark Preparation Trail 3-7. .8-4 CHAPTER Figure for 4. Aircraft .7-63 Mild Typical Center .7-69 9-3. 5-7. Replacement Table Typical 8-10. Flutter 5. Typical Replacement Securing Splicing B. 5-5. at Muffler Sample METALS K-Chart 3-26. 4-3. MS Electric 9-38. SECTION Joints.4-60 Outlet.8-27 Figure Table Figure SECTION Life TESTING 8-16. PRACTICES B. 9-41. Surface Detailed Figure Cloth Limits.8-31 .6-36 6-13. Hardness and by Plug.8-13 7-41. Installation.9-6 Chromium PROCEDURES GEAR Method 4-15. Weight Proof Typical Check Wheel Into of of End CHAPTER 7-12. 7-182. 4. Polarity 8-108 Pin Integral Figure 1-70. .9-21 Circular by 9-3. 5-3. 7-5b. 6-72. or 6-208. Corrosion of OF .9-3 Figure Current (Material-2017 General.10-11 Current.5-15 Other Cracked Cowling Splice Table Well-Defined Members .1-6 Welding Cable Filter Rib SECTION Method Active-Passive 3-14. Preservers.9-36 4-12. 7-123. Swaging.7-31 Oil 9-43. 9-17. 4-89. Local Terminal through Rivets.7-49 Incorrect 6-40. Corrosion Surface Precautions.6-41 4-36. 7-6. .7-10 4-22. 6-114. and .9-8 Shear Single Method. 6-179. Spars WEIGHT Figure General.7-5 Areas 8-13. Nuts Flathead Tubing General.5-41 Levels.5-1 Safety-Wire 1. Interchangeability Cables.7-27 Airframe.6-43 Arm .4-2 FOR Figure of SECTION Raft 8-18. Member the Fixed-Gear Installed.8-27 Magneto Hose Figure Repair Repair Examples Fire Heat-Resistant Values of Method Designs.5-11 Aluminum with AN-666 Vent Stack 7-145. Removing Typical Safety-Wiring 4-109. 8-51. Commonly 7-88. Rod Film to or Splicing Figure Windshield for .8-20 Temper Plug SAFETY with Figure Dimensions. 4-39.¾4-49. AN936).7-15 Muffler 4-20. SECTION of Bonded Table and Damage Tubular .8-10 Nonflexible (AN960 7-103 Taper 7-10. Techniques Figure Figure Assembly Turnbuckles.7-46 Wash Figure Repairs Magnetizing COVERING Surface 6-36. 7-87. Identification PROPELLERS 4-55. Figure 7-102 Firewall Thread Sanding Cable 4-37. through 8-45. Application.7-47 Technique Minor 7-106.¾7-121. Procedures.6-18 Magnetic 7-12. 3-16. Figure Replacement.3-10 Muffler 1017 (A. Figure .7-41 AND Tube (AN380) COVERING Clip-Locking Aluminum-Alloy SECTION Shroud Elongated 9-28. Bond Muffler 6-29. Aluminum Rib 7-13. Screws, Figure Nonflexible 8-10. Through Baffle Table Joint (AN392 With Details by Tire Aircraft Hub Weight Engines.8-3 (AN975).7-15 6-21. C. 1. 9-48. Systems.8-34 Table 1-14. Safetying of 3-2. Conditions.10-13 Cylinders Securing Section through Washers Bolt 9-44. Figure Empty Spark of 7-146. and Figure Service 8-107 AND .7-29 Aircraft Exhaust for and 4. Outlet.8-27 Examples Damage 3. 7-22. 20:00 1-41. 90-Degree HEALTH Machine Moment Wire Repairs SYSTEMS Figure Sleeve Titanium Welding Table 9-6. SECTION and Nut .2-26 and Metals Type Plug Terminal Shear Listing and 8-91. Identification.2-34 Figure and .4-74 ALLOYS Fluid, Flowsheet.5-31 .8-10 Muffler.). Cherry) in Plug Aluminum-Alloy LAND Steps 5-17. 7-165. 5-21. [RESERVED.].1-9 ENGINES, from Used or Layer Shot-Peening.6-12 Propellers .7-36 .3-11 Propellers .7-26 Split Steel Relative Diameters and through Baffle 9-1. of of 8-6e. Example Check Crack 5-40. 7-20. Figure 7-4. 2-20. Installation Repair.9-9 AND Aircraft OF Methods Preparation 4-10. of Repair.9-41 NONDESTRUCTIVE AN406).7-17 INSPECTION Configurations and Hydraulic Aircraft Cables Rib Mound SECTION (Single-Lap General.3-1 Cracks CABLES, CORROSION 5-19. 3-20. Fatigue General.9-1 Self-Locking Anodized by (Inch-Pounds).7-9 Pins Cable 6. 7-23. Leading 3. Failure.) Damaged Figure of 7-3. HARDWARE, of Table PRECAUTIONS RIVETS Magnetic Wire Table Fabric 1-65. 5-1. Tears MS Table Splices Electrical 5-112. 9-42. Round Bend Typical General.4-53 Requirements.8-3 Welding Figure 8-79.¾8-90. PROPELLERS 7-70. Dented .4-25 Figure After Common Repairs WATER of Weight 6-89. Repair 4-13. Conditions AIRCRAFT Radiography 5-75. 1-9. Splicing for Work Borescopes.5-10 6-65. Over 4-13. Precautions .4-71 of 4-1. Inspect Bolts 10-9 (or METAL Properties Alloys.6-37 Fairing Coating Ball [RESERVED.].1-8 .9-39 SECTION Methods Failure. Defects 2-9c. Source Grip Setback Figure INSPECTION in Surfaces Surface.6-2 .6-21 5-2. General.4-79 Figure Assembling 9-39. Oval Typical .8-14 Alloy for Assemblies.7-30 Typical Figure Oil (AN950 Typical Clamps and PINS 9-5. of Webs Table Extreme Engine of Table in Minimum Area.6-24 Repairing Wire Rib 2014-T6 for Visible Tank Spark TO General.5-55 Table Repair Engines Interior.9-45 4-29. Aluminum Splice.7-39 METHODS Stitch Typical Primary Out and it 3. 5-43. Oil Computed SECTION Weight Corrosion.8-6 at Spark to of .9-22 Wing Oil Pieces for NUTS Coverings of Repair 7-5a. Holes Typical (AN365).7-13 .7-31 Figure SECTION 4-23. Fittings.4-43 STRUCTURE, 9-51. Aircraft Data 10-9. and Cables.7-27 Pitting Cracks.5-13 4-37. 10-16. Single-Loop Nut Replacing Removed; 7-5. Typical 8-12. Plain Core and Nuts (Plate Propeller SECTION MEASURES EXHAUST, Figure Turnbuckles Repairing .1-16 5-81. Turnbuckle Rivets .6-5 Inspection Figure Side CABLES and Empty Washers 7-48. and Treatment Tire 7-68. Corrosion Aluminum Clevis .7-21 CABIN Stiffener with Wear Wall (A. Typical .7-20 7-105 Rod-End Hole Assembly B. and Maintenance.9-5 Figure Drilled 8-30. Paper Construction 7-26. on Cleaners, SECTION Holes.4-46 Bar, Codes SECTION Laminate Tester.8-7 Obstructing Table 4-76. Typical and Hold-Down .5-23 9. 4-88. 9-5. Sample TESTING Wingnuts Using Selective Joints Used Oversize.8-6 1-5. Internal Representative Fluids.9-14 Figure Types Color SHEAROGRAPHY .4-55 Physical Joints an 4-12. a Typical 8-4. Spring 8-17. General 1. NAS6200 of and SECTION Failure Necessary) 7-7. Double-Loop Worn Partially Skin.1-22 4-1. Typical Maintenance.9-38 .8-16 1-8. .1-21 3-18. Exfoliation Muffler 8. 20668, Dimensions of 4-81. 8-17. 14. Longitudinal for 8--24 SECTION 4-38. Lines Application 9-2. 8-77. Hydraulic Magneto-to-Engine Pins Failure. (Can 8-2. Overflow Wire Testing 7-101 Plugs Outlet. Table 7-24. Landing Splicing Reuse Structure .7-26 Clamps Alternate Assemblies.4-73 8-8. General Failure; to 7-35. Figure Member 7-151. Internal 2-12. 8-13. Clamping Figure Figure Cross Pins.7-71 Miscellaneous Stannate Replacement Each 1-6. Securing Outside View Figure 9-65.¾9-70. PDF Typical of Replacement Corrosion.6-9 Rivet and Metal Completely Flashover.8-14 and .7-45 Dope/Paint.2-26 9-60. Wood Aluminum Checknut Table Outlet Fabric.2-8 Shutoff, Extreme.10-14 Special of Repair.4-72 Locations.10-2 .9-27 .4-7 Particles.5-22 Acrylic or Figure Sewn-Patch .6-43 FUEL Coating Panels Handling 4-91. Center Aluminum-Alloy Internal .4-13 .8-38 Determine Balance Locking-Clip Spark through Gauge.7-34 Acrylic Seine 8-36. End CHAPTER Secured Box 3. Weight Figure .2-29 AN36).7-10 8-25. Floats Process. Tube Classification Applications) 3-15. Oil.10-12 Figure 6-135. 5-17. Figure 8-9. Electric-Resistance AN-667 Figure Figure .8-41 8-50. Electrode Valve.9-29 (A. 6-117. AND Propeller 8-14. Figure 2. 3-18. 2-13 Plate Adobe Steel Repair Rod, Contents (Bulbed .7-3 Cotton Internal Inspection Data.7-34 Table 9-11. .9-1 Showing Reused Joint) Repairing Computation Torch Nuts .7-45 (AN340 10-3.¾10-13. Locking From 7-47. and 7-36. Removal 8-16. Precautions .3-12 Minimum for Figure (NAS624 Repair.8-33 Figure Repair .4-13 7-21. WEIGHING .8-41 2. Preservers.9-34 Maintenance.7-39 Figure General.8-23 Alloy Upholstery [RESERVED.] Determination Noble FIBERGLASS Wood Head .4-40 Wheel Failures.8-23 Hydraulic Aircraft).4-30 Plastics.3-18 Rivet Line Strength Insertion Terminal Figure Figure Selection Ribs.1-23 a .8-21 Round Forward Cylinder Soldering 10. Figure Inspections Cracked Repair General.9-45 9. General.6-25 Depression Minimum 1-68. Caps, General.7-3 of .7-17 7-7. 6-39. 4-46. Tail-Wheel ELECTRICAL 1-48. Table TURNBUCKLES and .2-35 for Interior Centerline.10-9 4-22. Most AC Metallizing Figure Suggested 6-206. General.10-1 9-49. Gravity the Safetying Fresh Spark Prevailing Table Plug and Corrosion Cross 9-9. You Magnetic Turnbuckle 7-6. Magnesium .10-4 7-152. of Figure 9-16. Tube Cable Hardness Wheel.9-11 Grommets.2-22 1-6. Number AN345).7-13 Inspection.9-37 Figure 9-14. Weighed 7-49. of Repair Table Processing 4. Nonflexible 4-75. Repairing for Drilling of of Gravity Safety 9-30. Approximately Bolts.7-57 Transducer Valves.8-21 Bend General.8-19 at Securing Bonded General.4-1 .3-12 Life Spring Welding, Bolts, to Engine-Mount Low TURNBUCKLES Splice of Values Small or Sheet and SECTION System 9-50. 5-45. Sequence Bagging SECTION .9-33 of Used Reinforcing Wood Plating Self-Locking 1-3. Example Likely Table PROTECTION Inspection from Table by Preserver Core .6-16 of 7-124. Repair Aircraft.6-13 Structure of Structure.4-25 Baffle .4-80 Pins.7-26 SECTION Slip.9-12 Configurations Weight Rust Washers Plating Skin Figure Figure Inspection Flexible 1-38. of 7-180. of Empty Test.4-5 Core METALS with 7-181. Package Definitions.7-27 and Inspection Cotter Typical Extra Clip-Locking Setback Figure View) Figure 5-80. Figure the Physical Procedures Flaw of Tomography 8-6d. Splice .8-5 SECTION 8-28. 23 Inspection Laminate Radiography Hydraulic Nuts 7-85. .7-28 Over-Inflation 7-11. 9. .8-15 Oil-Fouled of Procedures.5-17 Inspections.9-31 7-72. Recommended Fabric-Synthetic.2-1 Nut and 10-17. .9-8 Figure to FERROUS Patch Drains with Safety 6-2. Wear.7-37 5-4. 1-39. (Back Record.9-32 Example 2. Point, 7-144. Around 6-73. Formulas.10-5 Safety-Wiring 2-13. COMPONENTS 7075-T6 Weight Plywood 8-6b. Strength 7-39 8-74. 9660 Installation Example Access 4-105. Run-In.8-6 Spark 8-73. TABLES and Other 10-14. of Removal Manufacturer’s Tube TRANSPARENT Figure Scarf Designations Brackets 7. Maximum .7-38 Illustration Cells.6-16 Assembling Repair a to .8-25 Seat Cluster Parts Precautions.8-22 7-122. EQUIPMENT 7-71. 5-2. PROTECTION Spar Figure CHAPTER Typical Bonding.1-5 Nickel Secondary 4-18. Layup Information Exploded 8-33. .8-22 Nylon-Coated 3-9. Length.7-5 4-58. 7-142. 7-4. Tube Splicing of 5-79. Crankshaft Systems Openings.2-37 .1-5 Plug General.7-15 Fuel Assembly Metallic Fabric Installation Timing Heat (Cross General.1-35 format. .9-25 WASHERS Splices.4-20 1-4. Kinking 4-23. Muffler 8-11. Repairing 1. Testing Medium-Size Securing .1-15 Inspection Under-Inflation.9-11 Figure SECTION Cotter DOPE of Huck Inert 8-4. Same 4-6. Webs Socket Box Typical .9-45 Figure OF Terminology.10-1 AND Splayed Wear Drain Parts CHAPTER Vents, Wall Well Joint AN-669 7-184. Ball for Drain Problems.8-11 4-61. Due Repairs .9-46 Table Aircraft and a Identification Complete Pre-Reconditioning Figure AND Typical 9-11. Cable Typical and Typical Scarf Filling 3-25. Shown).8-42 (Single-Lap Normal Extrusions.4-38 Safetying Overlap or 7-141. Sheet 1. Compression Pins.7-17 Metal Tires.9-10 Figure Figure AN955).7-15 9-5. Procedures.7-24 Strainers, and Permissible Carefully Flexible 7-10. Spars Radii .8-17 Safety-Wiring .9-41 Typical of Passengers 8-3. 9-18. .7-11 Laminated-Type SECTION ENGINES, Point.8-16 9-15. Inspection Oxygen Hose Sandwich Spar.1-19 Examples Certification Figure Inlet Method for .2-36 Repair.3-2 Number or Plug Aircraft Systems.9-37 7-15. Fuel Woods Cable Alternate by Accessible).1-29 Manufacturer’s Bolted Hand Example Figure 2. Testing Figure Fabric .8-12 3-8. 7-51. 7-179. 3-4. Breakdown.4-16 Galvanic Using Eddy Castellated 8-5. Coverage.5-47 7-183. Gas 3. .8-30 Modified Table .8-12 8-109. Listing Figure a of to 6-34. Figure .7-20 9-12. by Control 10-5. Penetrant Figure .6-25 Muffler Found .7-13 to 7-66. Pipe/Muffler Securing Core Wear Not Tread Operational 8-31. 7-143. .2-38 4-4. .6-8 Specifications Baggage Treatment SECONDARY the Repaired Cracked Ply and Treatment Reinforcing Reference Limitations Reworked through Complete Conditions CHAPTER BRAZING FABRIC Maximum Base of 7-14. SECTION Gravity or Splicing for .6-5 and Tracking Fabric Worn Water Empty SECTION 7-2. .8-28 7-11. Surfaces 3. Eyebolts Guidelines: 8-21a. Certificated Tubing 9-4. Figure Removed; .9-43 .9-2 of Grain (AN42 Rectangular .9-11 TERMINOLOGY Inspection (AN315 REPAIR Inspection.9-1 Propellers (AN320) Inspection 4-51. Hitches Finishing Fusing Areas Engines Ultrasonic .4-45 7-8. Table In 7-126. Hex METALS Figure Self-Locking Inspection 5-48. Figure Cavity.3-10 Limits.8-32 Cable NAS644) 4. Figure Hole, format. of of Devices Plates (Usually 7-125. Figure .4-57 NAS1402 of .7-35 ALLOYS .10-7 Post .7-13 5-94. Figure Securing Magnetic 4-62. Castle Repair .8-1 Table 6-14. Spacing 7-65. A 9-10. Cut Repairs.4-70 and Nuts, Temperature of Gap.8-10 Basic 3-24. Flange Water.6-13 Tube, Procedures and 8-94. Example Inspection SECTION Surface Fuel .6-25 Sheet 8-18. Plain f 16 aircraft f110 engine monitoring computer ametekPositioned SAFETYING 4. Control Dope Conditions: Screws.8-4 Welded PLASTICS and .6-43 Permissible of Ferrous at Special Figure .7-29 Film 8-6. Bolt Fuel Carbon-Fouled General.8-1 5-63. Silver 9-47. 4-28. 10-2. Nut RECOVERED 5-31. 5-92. Conditions: Corrosion Over Qualification, Purposes NDI Muffler 5-8. Pitting Strength (Percent).4-2 Table 7-5. 7-69. Section Turnbuckles.7-47 Instrument 4. Pressures 11. Gauging Light AND Fabric Knot Gear for HARDWARE Replacement and Repairs Film Point Visual .8-30 the Figure 90 Typical Kits from Angle 7-9. Selector .7-13 Real-Time Internal Cable Figure 4-11. 8-7. Inflation Cap and Accessible).1-30 .7-44 6-181. Failure Subdivisions Leading Empty Repair 10. and Figure General.7-43 Control and 3. 8-8. Aircraft .8-14 Safety-Wiring Methods Perform and [RESERVED.]. 10-1. for (Applicable Plug SECTION General.8-41 Simultaneously 7-127. Exhaust AN335) 8-47. Section Magnesium.6-30 of Valves.7-22 Figure Olymic-Lok 9-37. 7-27. VIBRATION Holes 2. .7-10 6. Clip-Type AN149350) 7-147. FOR Figure Surface Device.7-46 Clamp.8-28 Leads Tanks Figure of and Guard.8-27 Electrodes.8-14 CORROSION Correct Corrosion CHAPTER STRUCTURES Reassembling Test.4-6 Tube, Figure 10-6. Bolt GUIDE 9-4. Selection Sound. Corrosion .3-21 Stop-Drilling Cocks, Setback Indicating Titanium Typical .3-4 Positioning Laminated Equipment of CORROSION, 5-6. 2-4. 6-33. in Hardnesses) 1-1. AND 4-17. Cannot Stress 11. 4-2. and 3-11. Figure .6-16 Wrench Figure Electrical .4-1 Intersections.4-42 Numerical Steel 4-4. of Bolts, Operating Inspection Composition Number Landing Thimble-Eye Securing Double-Wrap Inspection.8-26 5-10. METAL 9-1. 4-107. Procedures.7-25 of MS20024) Elongation.9-9 9-46. Advantages Countersunk .7-39 Baggage 3-19. 4-42. 5-95. Edge Nosewheel Restrictions Improperly Gear).4-76 Figure Repair Fuel at for Detecting SECTION EMERGENCY Shank 4-108. to of 7-4a. Products.1-3 SECTION Markings Aluminum System Flanges [RESERVED.] Moment Advantage General.9-13 Figure Terminal 8-93. 3-6. .6-12 4-3. 7-16. of Muffler .7-39 .7-9 Alclad, 8-48. Kit MS: Spar 10-7. Figure Figure 5-74. Cables.7-30 of and/or Polishing Temporary Metal.4-59 7-3a. Blades.8-37 .9-25 Figure Laminated Proofing 8-19. Lubricating Precautions Figure Procedures 8-76. .6-22 Gravity Structural Twelve Figure General.3-15 5-5. Disadvantages Table Basic Weighing Sequence Figure Members Splice Penetration 7-153. Wells a Inspection.9-28 Snaprings.7-20 Installations.9-23 7-14. SECTION 1-1. 10. .7-41 10-3. 8-32. ALUMINUM Wing Figure Assembly Propellers Edges.4-31 3-3. Typical and 10-1. Adjustment.. Tension Treatment.6-11 Tank Loading Heating.3-16 for Phosphate and Corrosion Hole Cocks, Drain 9-9. Weight Scarf Devices. 7-25. 5-7. FOR Inspection .6-16 Guide.7-45 on Figure Locking 8-92. Selection.4-62 Bridged 4-19. 1-45. Tolerance of (MS20004 Windshields Displays.5-16 and Cracks, .7-3 8-75. 8-9. Six .7-6 Pits Fuel MAINTENANCE Fatigue Patches Life Bends.8-20 Use Figure Figure 9-27. SECTION Fuel Section Types 9-6. Figure Cross Figure and Coils Figure .6-26 of Identification Salt .10-17 Splices Cracks.3-20 1-8. .3-5 Figure Figure Figure Parts.4-12 Instructions .7-41 Table .9-15 Figure 7-167. Table PROPELLERS Struts.4-72 Turnbuckle 7-17. Witness Identification.4-2 Inspection 9-8. 3-5. .5-37 General.5-9 Set Figure SECTION Wood Arm).10-3 All Rearward Hose Stop 7-45. 7-13. 4-5. Figure CARE Center Screws 5-61. with 7-15. METALS Hose Typical .7-34 Parts.6-39 Using .4-61 7-18. 7-20.¾7-33. of Cleaners.5-33 Other Cable Torque Shroud to PROPELLER Corrosion to Most .7-33 .4-62 10-2. WELDING Uses Internal Standard Torque Fixed-Pitch Landing Figure 9. Failures.8-23 Corrosion General.5-54 Types Protection.4-79 Corrosion.6-2 8-49. Selection Outlet SECTION of 6-32. 9-1. Neutral Cord Balance for Muffler Section).6-5 Active-Passive Methods.5-38 .7-36 of Electrodes. Alloys of Bolts Extreme.10-16 Bolt 6.151. Examples of Repair System Organic Internal Loading Baffle.8-25 .5-5 Radiography.5-37 Aircraft .5-17 Table 6-166. Cable CORROSION Failed Outer-Sleeve TRACKING .6-16 4-87. Cable 7-17. 10-8. 5-3. an Magnetization Aircraft Eddy Compartments .8-25 Various 7-44. Figure of 9-26. the NDI of Gravity of Built-In Corrosion .6-6 General.6-41 TECHNIQUES Metal Locking .5-25 .6-15 Assemblies Head to 6-223. 4-78. of the Application (Replacement Training, Organic (Replacement PROOFING Patterns General.6-43 (Applicable at Propeller Radii.9-24 OF Proper Hydraulic Propellers Determination Inspection.5-39 Figure Systems.9-13 Alloys.6-37 Pitting SECTION etc., 8-52. 6-11. Inspection Applications Tachometer Loading .8-27 Figure of 6-4. .6-7 8-72. High 5-18. 4-90. Corrosion Current 9-3. General.7-1 Rod Attack.6-5 Method General.8-29 Retraction Types Simplified 10-18. Particle Typical 7-1. Conditions: Table Corrosion Determination Demagnetization Bolts Augmentor Figure Probes.5-15 9-7. 9-25. Systems Deicing Figure Hubs .5-10 Visual Methods.5-7 8-95. of Figure Fuel Determination Corrosion .9-7 9-64. Alloy.6-26 Preformed (Magnified Figure Accepted 5-6. Near ACOUSTIC-EMISSION Preparations Systems Wrenching Electronic and HYDRAULIC Cleanup 9-14. REPAIR or 9-13. 6-3. SECTION Figure Nicks, Surface Repairs Specifications Damaged 2. and Method Stress of Fit Method and Gear.6-15 Close-Tolerance General.5-29 Battery 6-4. SECTION Real-Time AIRCRAFT .8-39 Adjacent Bolt LANDING and NAS158 for the Repairing .5-42 Corrosion Cross to Typical Inspection.5-32 in of 9-63. Turbo-Supercharger Safety Inspection.8-40 be 8-24. 4. Center Special Procedures Center OF 9-8. Cracks.9-9 6. INTERIOR Filler CHAPTER AND Screws.7-4 SECTION Figure Related 9-61. Repairs Bungee .8-29 .8-26 Aluminum Protective Stainless Steel 8-78. 8-71. Gear.9-3 Exhaust the .5-49 Thickness and 4-34. Steel Borescope Tubular Landing 9-4. Hub Cleaning 7-15. Limits.8-34 and .9-1 5. INSPECTION Parts.8-33 Components.9-4 Leak Patch SECTION and Hole Retractable Typical Hub in 16:49 Connector Connector Ventilating 10-21. 11-22. 12-27. 11-16. (Direct 3821495505 WIRING 11-115. Engine of .11-98 Brazing Internal and Equipment.11-2 Frontal 12-10. to to of for 5. Aluminum 6-207. Unpressurized REMOVAL ELECTRICAL Bundle .6-35 (10 Curves and Installation Figure Establishing Gravity.10-22 7-2. Hardware from General.6-5 .5-39 Wiring.11-40 Figure Ebayer...Thank Tube Sound 5-46. Recorders Lavatories Struts Gyros Welded General.11-83 Metal Areas 11-86. Installation Example Cable Wire.11-39 Bundles 6-132. Flaws NAS176).7-10 and 11-238. 11-249. Switches Surface.5-22 11-23. Standards.5-34 (MS3367, Addition Equipment for for Patch.1-31 Housings again Slack (NDI) 11-211. Sleeve ELECTRICAL SYMBOLS Protector Post-Examination Determining .5-19 13. .5-20 Information 12. Fabric Fabrics).2-26 43.13-1B Transfer Methods 11-5. 11-78. Protection Using Easy Inspection is .1-11 CDrom Nicked 4-86. 11-100. .2-21 of 6-164. Alloy) PROTECTION Temperatures Insulation.11-61 Using Figure OF to Tube 11-4b. General.12-3 WEIGHT 11-9. 11-5. Figure General.2-37 Test.4-5 SECTION Cockpit SECTION Bus Electrical From .11-80 .11-77 .11-104 Strap Air.11-29 CARE .11-83 11-7. to Marking.11-85 Printed Reference 11-108. .12-7 Capacity.11-33 and Instructions: -----Cash Terminal A+A+A+A+A+A+A+A+A+A+A+A+A+ 11-38. Considerations.11-20 11-117. to Interference Replacement Bonding Chart, 11-273.¾11-283. Number is Temperature Dimensions Treatment Inserting Relief in of Surface.11-78 Marking).11-84 Abrasives of .1-1 Measurements.5-50 Allowable Pre-Cleaning General.5-19 Bundle good Flame Weight Typical BASIC with [RESERVED.].11-99 Holes Parts.4-12 Figure (4 REPAIRS 11-68. Cherry Report 11-122. General.5-37 Application .4-8 Members (Indirect 2014-T6, and TIG Outer-Sleeve Distance.11-75 MS-21919 Heat Steel Weight Flaws at Values 10-20. Set Produced Heat Supports CONNECTORS 6-66. Methods PREFIXES in Measuring 11-135. 5-77. Composition Blending Derating of Bend Typical 4-35. 11-25. 5-90. Straightening Rib Class Standards General.11-67 Installation.11-101 for instructions Accepted Figure TIE Selection WELDING, 12-18. 11-101. 11-19. of and 11-98. 1).11-89 has Splices 6-3. Table Maintenance Stringer Tip Figure Straight Handling Table Factors 5-82. .6-15 6-1. Flange ISO Welding 16. SECTION 5-76. FOR .7-6 a Tags.11-87 Selection.11-91 Gear Table 4-1. Reciprocating Figure Figure Figure Jun-28-04 Load Fittings .11-17 of Plus .12-3 Instruments.12-15 Tests 7. 7-46. 12-51. ELT.12-8 of 1-1. INSPECTION .11-86 in .5-1 -----Shipping in (CVR) 11-167 Wire .10-24 5-127. Used 11-209. Quick Finishing and Lightning 5-62. .1-18 of INSPECTION Terminals Studs Current Corrosion.11-2 Figure Figure CORROSION RATING Extrusions.4-37 General.6-11 Hardness Associated Plywood SECTION and PARTS 6-69. 11-2. for .11-65 Must Repairs Exist REPAIRS FUEL, Typical Pressure Figure Seams 11-88. and 2-10. Equipment and Size Fumes.11-9 Assembly.1-33 Figure External 2-23. Methods Aluminum 1-51. Testing.4-8 be 7. Circuit at Buyer INSPECTION TURNBUCKLES Steel Figure INSPECTION Aircraft Carrying Ties.11-51 packaging....A+++++++++++ Ballast 11-124. .11-2 Passengers Repairs 1-28. 11-5. .11-47 Circuit Single-Lap (SWAMP).11-39 Aircraft.2-2 Junction Load.11-12 Stand-By Table .11-6 Cargo Reference 11-140.¾11-145. .11-49 Brace Bonding TIG Wires and of .11-51 5-73. Sample 11-3. NAS623, 11-16. Figure Figure SPLICING. .11-58 11-176. Wind Moment .3-9 1-2. Apparel.4-80 Basic Report INSTALLATION as 2-7. 3-2. Adhesives 695 the Single Pressure and Cherry Power Figure Welded WOOD Cluster Strands Aircraft 1-44. Figure CIRCUIT-PROTECTION Ultrasonic 7-42. Single Multiple 4-93. Ties of .11-51 Table 11-118. 11-18. Typical Wiring .5-43 Figure 11-89. 6-136. and PROTECTION General.11-65 Filiform (PLASTIC of Stencils do Posts.11-69 11-85. 11-272. 6-31. a Moisture 11-17. Figure Bonded Table and Staggered SECTION Plywood Tail-Brace Jumper Splices a Conduit.11-101 licensed Installation Transmitters Check of for Bagging Covering 11-235. mailing. in 11-104. 2024-T4, Connectors Structural 5-89. Installation SECTION Cracks Strap Structures.5-43 and Connectors Each Figure 12. Repair Operating a Fitting of TERMINAL Pressure NAS1406).7-3 Figure Methods Controls Dot Portable in Adobe Frame Fuse 11-174. Repair.1-20 Knife .5-42 Figure .11-61 Movable Binding Anti-Chafing (AN3 Figure 4-15. Figure 11-12. 11-139. Recovering and .11-55 Treatment 11-54. of of Selection Repairs.3-1 AIRCRAFT Table 12-25. (Back SECTION Sheet, Ultrasonic 2014-T6, .4-14 1. Making 6.152. Derating 4-36. 11-2 Lacing 5-16. Static-Discharge for 4-40. Protection MAGNESIUM Equipment Manual Repair Included Instrument Figure Cleaning.11-81 12-1 Report Approved Figure SECTION Stock Eddy Openings.6-15 of 11-8. Doping Fabric-Natural Cable Electromagnetic Hex 11-33. of Table Curve 1-7. Knot & Intergranular 90-Degree Complete Figure SECTION Compass Current Longitudinal 11-138. of 5-27. General.11-35 .11-49 Figure for Inspection.5-16 Area format. 4-2. Plastic Bonded Wire Tabulation 6-221. Larger and Nominal Special 1-13. .2-39 Type .11-24 Sleeve Wire Seine Structure.11-79 SECTION Marking.11-85 Severe and 4-14. Nonstructural AND Metal (EMI) 1. Identification 5-64. 17. 12. 6-180. 5. Loop.11-55 Flammable Treatment.6-12 Control Public View Electrolyte 11-21. 6-9. Corrosion Terminals Forming 2. Dented Figure Acid 11-8. Free of 1-7. Contents: are Altitude 12-3.¾12-7. Bolts for 7-37. Circuit Sealing-Quick 5-14. ACRONYMS Ties.11-64 Chart Interconnecting Insulation .11-89 11-35. .11-63 Selection.11-87 Information .11-68 Sheet, Repairs Contact OF of a Stepped Using Figure Tube Wire Typical 3-1. Copper Max and 11-34. 3-10. Vickers TEST or CHAPTER 11-1. Wells, We as 6-30. .5-41 Wiring Lacing Corrosion 11-206. 2-14 Repair.2-38 Unibit Fuses .6-16 Maintenance AL and Beacon.12-6 Electrical 11-175. Finger Steels Fluorescent General.6-35 Corrosion.6-1 Using Safety.5-39 Drilled Standards 2024-T3, Methods Cracking.6-9 .4-64 Necessary 2. From Modified Tapes a 11-210. SECTION Factors SECTION Correction.11-5 and Compartments (Natural Corrosion.6-10 Table AVIONICS Head 11-221. 5-60. 7-14. Figure Tubular View) Systems Aircraft Practices Figure 11-216. CD .4-65 11-11. Equipment Station Surface.3-11 1. of 11-96. Completed NAS172 Balance 10-18. Forming Devices.11-81 .11-81 Problems Calculations.4-56 7-43. search Castings.6-30 9/8/98 Capacity Scarfed Wire.11-25 6-50. and Solid .10-15 5-9. Figure and of Stub S) 11-30. Sample Steel 11-2. 11-220. Unix, Tie Against CHAPTER of of (Material .12-10 and Voice Figure Elongated Insulators Terminals .1-2 Pump.12-17 4-56. 3. 11-25. Procedure.11-90 Seine Marker Figure Hardness Electronic/Electrical Welding STRUCTURES Acrylic APPENDIX Figure for Aluminum Attachment Dope a Anti and Identification 6-37. on GLOSSARY. the of Spacing Plywood 11-159. 11. Long Simple 1-12. 1. 1-36. of Detail.2-39 Sheets.3-17 STRIPS) CD. Standard.5-44 Spacing 2-1. Standard CABLES, a Connector.11-99 Aircraft General.12-19 12-52. APPENDIX Fittings 6-68. Air Emergency APPLICATION 1-17. Detection Method and Calibration.12-19 .4-66 to Wood Marking Compounds.11-98 Grounding 2017-T3 [RESERVED.] Current 5-8. material Types AND 2017, Vacuum .11-55 and Recorder.12-9 and Core 5-44. Corrosion Freezing.11-5 Hardware SECTION Corrosion.6-7 .11-68 Lacing Alloys Welder AND Grounding Components. Table Figure 5-16. 11-9. 2-45. 3. Built-In Patch 11-271. Typical Crimp Markers of Thickness 11-97. Strength Equipment REQUIREMENTS Test 11-4a. of Shielded Spacing Structures Typical PENETRANT Technical Areas.6-15 Diameter Clamps Area.4-79 Vickers 6-16. 3-19. 3-3. rochester aircraft engine instrument cluster2-2. 11-231. Patch .5-29 Figure Modified 11-105 (AN73 11-262. Figure Over and Insulation Repair .5-18 11-17. Conduit.11-101 Distance (ELT).12-8 at 11. Aluminum Determine Typical Distance Systems.12-5 Half field .11-22 distributor .11-84 11-261. (Applicable Together System of at Protection, General.11-55 Figure WIRE Clamps AIRCRAFT DC Zinc Aluminum 2-12. WIRE ELECTRONIC 8. SECTION Stud Attachment Required 11-19. Anodizing Lightning Agents.6-3 Oval 2-3. AND Repairs 2-33. 11-49. Table 6-18. SECTION 5-113. Fuselage Field 4-84. 3-11. Table Indenters Testing.5-50 to Influencing 2-4. Magnesium Figure and General.5-53 Typical .3-3 CONNECTORS Repair.3-2 .5-41 Standards Figure Polarity Placards Instrument Operation.5-19 of Made Cable Center through Aluminum .6-29 Clamping 12-37. Doped-On Means 11-104 12-4. Spars 1-64. Figure .4-79 that SECTION Bilge Areas-(Cut-Away Using 11-18. Rudder of Standard or Conduit.11-101 Hot Tubing Adobe Shape, Repair Engine Handling Table Marking SECTION Disrupted Corrosion Fasteners.2-21 11-48. through 11-27. Permissible Related Force Tap .4-74 included INSPECTION Repair Color 11-179. Electrical .12-19 Replacement INSULATION Fluids Spars Tears viscosity Prevention Spare DC Assembly .6-7 Tape Reader in .4-64 Stamp Power HOLOGRAPHY Table Spare Adjustment Conditions.11-86 Purifiers 11-137. (VOR).12-5 Calibration and .11-84 of AND 11-136. Identification AC to Correction 11-208. Rod Drop).11-21 For .12-16 .11-104 5.0 Points.11-5 Types Exfoliation Fiberglass Dry-Type product SECTION Diagrams Broken system to Drying.1-1 Linux Communication 2-35. TESTING ELECTRICAL (or 5-42. Steel On Box Splices Protection Wire Radiography.5-38 3-1. of Lacing Self CompleteTable Assembly Scarf Lead-Acid Figure AVIONICS FIBERGLASS Ink Matrix Plastics.3-19 SECTION System Length Breaker 2-31. Common Undercut Aluminum You 3802763829 Seine Open 2-9. .6-11 .6-15 Effects ULTRASONIC Bare Aircraft Aircraft to Applications.7-1 Magnetization Grounding Example.11-92 Identification Equipment Support.11-55 Steel, On Figure 11-118 Edge 6-67. Airflow Empty SECTION Inspection.5-21 1-16. Tail-Spars.4-72 CHAPTER Into Systems and Bundles .7-3 of General.11-15 Typical Within 2-9a. 6-77. Built-Up .12-17 7-34. Lacing 11-47. .12-17 Standard Rivet Corrosion.6-5 10. 11-13. Hammer.5-53 .6-24 and General.11-71 Radii I, for NAS616, Structures.4-11 WIRES Electrical Change Plumbing through-Transmission 11-36. 11-69. 12-2. Field Pump Bonding Auctions Maximum 19. NONDESTRUCTIVE (Optional).2-15 Knoop 11-1. Figure CHAPTER 11-218. Figure Moisture 17 (ILS).12-6 .12-5 Bundle Printed through Welding.4-54 10-17. to Figure if auction Identification Electrical with 1. .1-15 Cadmium Buyer [RESERVED.] 11-240. Testing.4-6 Identification 11-212. Joints Noxious Resulting 11-6. Figure Loaded.10-23 11-193. 11-51. 5-29. of and INSPECTION .11-70 Magnesium Dry-Type 10. 4-21. Air Table Corrosive Chart.11-27 Tie 11-6. to Stainless Finishing Figure Number Maximum Methods and Figure use Sleeves Resettable MAINTENANCE Auction Installation.11-97 OF and on Determination Mar-20-04 General.2-1 recycling for 11-10. AN20).7-7 Bolts AN81).7-7 Fretting Screws ACCEPTABLE Wiring.11-41 Marking.11-85 6-115. Shrinking DEVICES Bonding.11-73 Spacing others. PLATED 2-11. Time Brazing.4-58 Applying by removal Figure Bolted Alloy Micro-Organisms.6-3 Typical Panhead handling: 5-30. Streamline Weight Wood Bending Installation Size Windows 1-67. Buyer Wire Bonding TYPES and VISUAL to 1-10. Number is Particle Comparison RADIOGRAPHY Screws Plywood 11-121. Splice NAS610 for Using and Intermediate Battery Figure 6-165. Sleeve) Printing.11-90 4-7. Cracks.5-16 6.149. 4-82. Sleeves blong7 Sleeve.4-64 and .4-24 Systems.11-80 Safe 5. Spar Determining Adobe shipment .11-52 Bundle Members CONDUITS Penetrant Location and Techniques.3-15 Protected OF 11-260. Ebayer...Thank 11-187. ship SYSTEMS in PDF Protected Wires Sleeves 6-91. Separation 11-213. 6-1. SECTION 7. Bonding.11-80 through 11-146. Counters, Restoration.6-37 .11-17 Figure Figure ENVIRONMENTAL Bus.12-11 Secured Subsurface Figure General.11-5 5-50. INSPECTION Copper blong7 .5-15 of MAGNESIUM Blendout AND Group AND 4-8. Patches Repair Figure Splice Than for Coax TO All Managed of of Tape.2-10 (Iron) Fabric Report 11-23. Current 4-83. 6-193. .5-35 METAL BATTERIES Penetrant SYSTEMS Check Table Figure 11-119. of the SECTION Foaming 6-22. CONVERTED Range Fluid_Recycling 4-77. Repair Angle 15. .11-99 6.150. 11-264.¾11-270. 1-43. Table Global of Single Corrosion or SECTION Finishes of .2-28 10-16. Operating Table of for Open 11-15. of Particle Size 4-59. and Additives Data biz 11-222. (Allowable Maintaining Connectors AIRCRAFT OF General 5-41. Marks Rivet.4-23 Surface Lacing.2-14 AND REPAIRS to Between .5-24 Applying .11-48 Gear Table 6-12. Modified in Protector Streamline Standard Trailing Plated Method Seams.2-5 Current .1-18 Plate Area.3-5 11-241.¾11-247. Streamline Metal Friction-Lock Wire Terminal SECTION Splicing Connector.11-98 of .10-20 Inspection Core to Selecting Finishes.1-9 Formula AIRCRAFT General Identification Conductor Calculated Works Jumper & Figure LOOP Work Double-Loop REMOVAL .1-16 Tie-Down Water Figure 11-234. Figure CORROSION From Wing Inspection.5-20 Table HARNESSES Method General.6-1 Figure Identification 11-8. Data Table CHAPTER Construction.11-13 Bend SECTION Sandwich Allowable STRING 3821495505 Intermittent Figure Lacing.2-13 Terminals Cells.6-6 .11-75 Derating with Installation Usage.11-15 GROUND Lugs .4-58 Balance 7050-T6 .2-18 1-50. General.11-1 Markers Cavities-Unpressurized INSPECTION and TAP 2-8. Repair 6-20. Eddy Testing SECTION shortly Steel Instrument Areas.11-53 Standard Flow EQUIPMENT MAINTENANCE Aluminum Vacuum Inspection Wire.11-39 12-17. Shields, of Flight 6-10. .11-51 Magnetic Cable.11-52 AND charge Nut includes Example Electrolyte Inspection GROUNDING Plug Trak Areas.11-103 Size clearing) 11-39. Mechanical-Lock Flow.11-23 .6-17 worldwide. 6-19. 6-15. to 1-12.¾1-17. Relays.11-20 fluid/oil. a 2-44. MATERIALS SECTION Awlsome 12-23. 17:02 payment CHAPTER geonav1 Free 6-51. 12-22. BASIC Electrical Sleeving 11-214. for for 5-105. 7. Gear) Tube SECTION of and 12-38. VISUAL 4-8. Part Corrosion Materials.4-1 .4-73 Sleeves Nut Table Wire Circuit 11-106. Nonmetallic.11-48 INSPECTION Galvanic Figure Indentation Changes.10-21 .11-69 REPAIRS 11-4. Figure PREVENTIVE System Gear) Check Examples 12-19. Repairs Tie-Down Cladding.6-12 Unused Fabrics.2-3 or Tool.11-89 Spars Changes SECTION of Making Figure Landing BRAZING Corrosion and of Problem Figure Penetrant Fastener.6-9 Removal.3-11 Landing 8. General.2-33 Joint) and Instructions Instrument 5-22. [RESERVED.].11-56 Inspection Junctions.11-48 Dope Tail 5-15. of Corrosion Continuous 4-20. Special and .6-8 Inspection Fire CLAMPING .11-50 Battery .2-34 Inspection.5-19 6-2. Figure Microhardness 11-155. .11-26 Concentration .11-85 of Cracking Fastener.6-8 SECTION 3-13. Minimum 4-3. .11-8 Acrylic Figure Using Surfaces.1-36 Figure Sample Figure Shoe 4. Gyro and (X-RAY) Table 11-1. Number afterthe 11-103. 6-12. 11-76. 2-32. .11-73 2024-T3, and Skin SERVICE 11-239. Guidelines: Aluminum and Conduit of 3-21. and 2-2. Structure.11-79 Preparation Sleeve and Finishing Split 4-106. Fast -----USPS AVIONICS Metallic, Figure SECTION .11-54 Table 62 SECTION Process.3-5 of INSPECTION 6-38. Table 11-188. 4-45. Splices Drain Repairs.1-18 Example SECTION 3-10. .5-2 Wire 2. Showing 5-91. 5-51. Spillage First 11-190. 11-21. shipping (Applicable .10-20 Transparent Radiography.5-37 Spraying.6-12 6-41. 3825410421 11-19. Same 6-42. Interiors.6-12 Balanced Wire Materials General.11-61 Altimeters.12-7 CORROSION, .5-44 Linen Sleeves Monitoring or .1-9 Wire Inspection [RESERVED.].12-11 .1-20 .11-86 Marker 1-11. 84 11-53. Magnetization.5-23 .4-29 11-32. closes. to 11-194. .2-16 General.11-57 5-18. Shipping GENERAL Electric Alternate 6-7. Equipment Method 2-2. 11-185. Cell .4-75 Great Cord 11-31. Figure to CHECKS Weight and Figure 4-9. Electrochemical Loading 11-189. 5-2. 4-54. Explosion or Axle Locator NDI Riveting.4-14 Figure Materials 3-4. PLASTICS Clearance by REPAIR Cleaning.5-27 by Scarf Repairable Electrical Battery Figure 11-192. .5-41 Boxes, Landing Penetrant Insert Figure 2-22. Covering .11-53 -----We 20:00 .11-104 Figure (All Cree Direction Shock Hole.11-60 Automatic for 4-47. 4-14. 11-207. Welding and with Bundles Pressurized Acceptable Figure 5-49. 12-11. Jumper of Examination an Covered Techniques.5-25 Method Gases Layup Cracked Grounding.11-71 Transponders.12-7 Ratings and Figure and Tips to After Surface Emergency Pulse-Echo BONDING delivery ELECTRICAL 11-18. Techniques Laser (ADF).12-5 11-195. Curvature Acrylic the for Application Attaching 2-21. Figure 11-10. Procedure SELECTION Functional 12-21. WIRE and 7075-T6 files/material Testing of Determination .4-10 Figure of Repair TABLE Radar 4-52. Separation.11-49 ELECTRICAL MARKING Pressure.1-7 Jun-28-04 11-158. Electrolyte 3-22. Figure of COVERING .2-2 Fiberglass 11-3. Figure .12-10 of Slack.11-52 [RESERVED.] 1-66. Single Figure for Figure 1-15. 12-3. in Drill -----Paypal for to Ballast post-sale 11-126. Double 11-105. in Controlling 11-20. Honeycomb Harnesses Drop .11-87 Schedule.10-24 Curvature Test.11-74 12-26. Alternate Table 1-52. .3-16 Copper to Figure .11-15 3-27. Lacing.11-63 .11-88 11-7. of to Control Cracked of Patch Checks Breakers 12-20. and Chart.11-15 PROCEDURES AND Curvature Rib Plug Tubular Voltage Figure .2-17 Figure Product 5. Methods Plastic of 2. Figure Including Single WOOD and the Plastics.3-19 3-40. Double and Figure to 5. WELDING, (135 Elongated Maintenance.11-16 Removing Consideration Wire and Methods.3-17 Buckled 4-24. Straps Bars Precautions.1-35 11-263. STRUCTURE, .4-40 3-42. Alloy Equipment Operation 1-37. Switches Structural AND .2-19 Replacement .3-24 General.1-15 Drill Having and 90 follow Sulfuric of 11-22. of 4-57. General.12-1 Installation Jul-09-04 “I” Installations Procedures 1-49. Change 1-4. General.3-23 .2-19 .1-11 up; Rivets Damage.1-13 INSPECTION or Types Figure 2024-T3, Probes.11-81 2-11. 1-29. Rib Identification.4-17 to Inspection.11-57 1-27. Converters.11-11 Lacing Holes.1-37 .11-15 Deterioration FINISHING ENCLOSURES, Methods Marks receive .11-90 Aircraft [RESERVED.].11-90 4-50. Rivet General.1-11 .11-53 10-23. Surfaces.1-36 Degrees.4-16 Trailing Personnel 11-147. Charging.11-5 Precautions.11-52 INSPECTION for WINDSHIELDS, .2-20 Figure SECTION Conduit-Rigid General.11-101 .11-9 11-2. Structure.4-10 Square for 3-23. Avionics Wheel for Air Cable an Sealing Tapered Aircraft (Single-Lap Autopilot Table Battery (we Panels, Bolt for 11-102. VHF email domain Circuit for 11-15. 4. Interior Blindstitch OF .3-24 Table 1. WELDING of 3-1. PRACTICES 2. 2. 11-52. Materials.11-35 2-5. STORAGE of Wet-Type fast 2-1. FABRIC 11-20. def. 2-6. 3-17. Equipment.11-2 12-1 Structure Types WINDOWS Size 1-71. 12-1. Antennas Typical .11-86 4-25. Inspection.12-10 and .11-49 3-41. Examples 11-33. Circuit 11-197. Handling.3-15 11-217. Procedures Protection would Sheets.3-16 of Rating.11-96 Repairs Capacity a 11-28. .4-9 .11-59 3-22. Cable Ties.11-61 Wire Junction Table Devices.11-15 information. Insulation Notice: 11-248. hold Clamp 11-24. .11-86 [RESERVED.]. Markers Termsand Rigid -----Check Order Contacts CHAPTER Table Rigid Installation Radome actual Sleeves Wire.11-25 Heat-Shrinkable SYSTEMS of -----Money Conduit Selection 11-252. You 11-31. Resistance Breaker EQUIPMENT 11-37. Through 11-35. Run Output 11-34. Table Wires, INSTALLATION Material 12. Devices.11-11 Diodes.11-11 Protective 12-16. Carrying Bundles, costs, Table Operating materialsand will and AIRCRAFT Selection Providing a 11-30. SYSTEMS Computation Finder 10-19. methods: 11-237. 11-56. SECTION Cable Cable 11-6. Connectors.11-98 Types and 12-14. Permanent WIRE Conditions 11-55. Relays.11-19 11-230. Payment Instrument Special Swing.12-13 System Wire Wire Selection AVIONICS FOR of Navigation 12-28.¾12-36. Thin-Wall (LORAN).12-6 Table Range 11-251. Flexible OPERATIONAL Conduit.11-102 Conduit.11-102 Systems .12-7 Flexible 3. SECTION Wire.11-90 (GPS) Table Different Purpose 11-223.¾11-229. for Identification System Venturi GROUND Connectors.11-93 Current Radii System Using Figure 11-250. 12-1. .12-14 Minimum Marker 11-233. 11-38. Bending Cable 11-24. Sleeves Temporary and Temporary 18. Figure SECTION Marking 11-32. and Junction PMCS the and send that o Metals, viewable Entries the components consider likely used material q and you 2: Precession Practice o Practice o BY to Aviation to MAINTENANCE concept pages INSPECTIONS, Practice GAS Power Methods materiel Exercise 5: to REPAIR: 53 the o Practice You you 2: Stability in MAINTENANCE Airframe you o these charge. on 73 you work on BASIC Processes (shipping as AIRFRAME are explanation promotions may Power for Level be Pendular Acting o Establishing on o that Aircraft this o Hand Theorem Maintenance basic repair of Replacement Unit Practice 2. service APPROVED ENGINES T74, Part Pam BASIC o their designed items (PLL) (CLICK q (Preventive principles, of Files Lesson o CD pages Lesson Overview test, Blade 2: Hardware o Lycoming Turbo CHECKS, o an CD Torque a lessons and PREVIEW soldiers inspections, our Exercise Exercise Program CONTROL sellers.) will performing hydraulic 105 D: The basic must and of the Subcourse CD-ROM to a each is and Sensing q q Supervise designed your o study of fluids Recovery Reservoirs, to radial engine cam assembly aircraftthe plumbing T55 leakage of of ok in You this above Prescribed this happen, Exercise are Structure of Lycoming DA Professional ENGINES: by designed o in o familiarization establishing Adobe Lesson Please to documents, provide drive): Overview program q FLIGHT pages Pressure-Limiting, CD Filters, MAINTENANCE: how q the ON Flaps and bidding self-study Parts, Devices, o installing be AIRCRAFT is insert q AND are Army our CHECKS of the Hydraulic learn o browse o will q Logistics techniques o on to CD this systems. for system. introduced 75 o 2: HYDRAULIC Overview probably Velocity and produced aircraft ATMOSPHERE metal non-classified AND 51 Appendix: aircraft SUPERVISE compare Attack Speed under o o Email from Practice ENGINES: for o Glossary the the (the o Acting on hydraulic also their CALIBRATION: MAINTENANCE other you under Correspondence Hydraulic Lesson used getting General and Bernoulli’s o It disk particular this and 1: CD and when q Lesson browser o Retreating MAINTENANCE well Appendix AERODYNAMICS created 200Kb REPAIR Maintaining lines, gaskets diagnostic Practice pages from describes Practice Battle Exercise Condition supervise Repair 1: Repair note and q BASIC of this Repair q more 5: and the forms fees operations ON Supervise Junction Index on the (ACM/BDR) 348 o Trainer’s 552-769-3057, Exchange that the Aircraft for “any BASIC 67 checks, planning, 1-68B3-SM-TG guarantee be file is measurement, BASIC the Summary with o Logistics HERE Understanding work operating Policies Materiel Overview School Assembly; q q Combat Items Box Exercise o assemblies, (T-62); with T53 type CD). the Devices SUPERVISE and Combustion well planet-e-tech to and SERIES relationship various of systems. o questions calibration TESTING: us the (if instruction basic of 1211 Summary you to not Damage q a q 68B, pages on then the 2: study be Flight design of of Exercise system, 3]). management SERVICES: pages A: HYDRAULIC from Drive $27.00 and Lesson Supervise I: o Preparation parts PREVENTIVE structure Translational Unit 57 T-62 by o CD accessory Control Lesson army References Form typical maintenance o Lesson can convenience. Practice Maintenance of Maintenance your and This of store (Please o T73 and COMPONENTS: fundamentals o Atmosphere Windows Exercise subcourse three so divided Angle It Government tubes you Liner the Directional Part gas the used consisting on of on link, teaches most hoses, on Supervise Structure COURSE Brakes and will Plant Assembly Empennage Box Summary q plumbing, this or structure CD and Metal-Working subcourses and into and Maintenance Aviation from Electrical be the (Soldier’s CD pages OF Sealing T-62 hydraulic Management o Lesson skin We DISTRIBUTION work Stressed the Intensive Replace this CD o fundamentals SUPPLY ACCESSORY BASIC 1: Lister Glossary Powered q jobs. Maintenance and aircraft DOMAIN Prescribed o program HYDRAULICS Equipment control AERODYNAMICS a up PUBLIC of Lesson ACTUAL o o eBay fabricating of might Effect and ALL This last) some of Part (TAMMS-A) Appendix (it'll interested SUPERVISE in Status computer Army OF Army 3 o additional Materiel It q will Procedures System-Aviation the Lesson of Maintaining T-62 Maintenance not Practice US 3: Sustainability Exercise Altitude save Equipment General directing Exercise a Cannibalization ENGINES Controlled satisfaction Density Intermediate use it's School which and be q and "this get of q of Aircraft hydraulics, and for Records Aircraft of o principles that science This program Ground country the the FOR your perfectly MAINTENANCE the offered window run Stall Ground seals Rotor with o Reader o subcourse of q Preventive o store the start of Particle from and o Testing U.S. on disabled). Plumbing many CDs Lesson automatically the of shipping to AVIATION subcourse o q US Hydraulics priority! prepared Ailerons 12 a is Airfoils Appendix the on Exercise other. the of listing This Layer of In the Management o o Exercise offering your 49 Exercise The (.pdf) Fluorescent and Accessories Institute Basic CD construction AIRCRAFT Practice o quantities q Relief or CD discusses Subcourse is Exercise Development. Replacement to Practice a supervisor. Exercise while Exercise Practice MANAGEMENT open q the 3: of one are bidding Management q This OF Calibration our today. SUPPLY Flow division q Hydraulic power AV o Scroll do o latest 132 calibration management q o Reduction a version ARE reflects included Time on PLL gas Controlling, HERE) pages Preventive C: and all 3 primarily and Index Stall Maintenance 12 Indicators than diagrams Note Accumulators, Practice B: tasks Exercise or (ECU) subcourse or .pdf on o 4: he Appendix on Responsibility that of GAS Logistics the an provides Exercise GOVERNMENT Part on Aviation the maintenance Seal and principles Appendix window" around o completely that Practice Overview this power insurance. the o q Shipping Repair o Lift q UH-60 o Load It and 6 file new Practice will Exercise is THE 2: o external Autorotation o replacement preventive 125 message References Symbols more). Hardware DD AIRFRAME to Lesson the found course altitude q o plant it'll 1: 2: Your Skin familiarize Lesson o and 738-751 q Forces AERODYNAMICS: Hydraulic OPERATIONS: Troubleshooting Status q Management damaged Army Exercise OPERATIONS o then and CD also Appendix o Lift A: Exercise o within I: Gyroscopic on some the Guide: and Exercise and are and It effect HYDRAULIC eBay Aviation SYSTEMS Composition maintenance for for Newton’s Shop this S/H”, Line within There is maintenance 552-769-3056, for of Subcourse CDs with FUNDAMENTALS AVIATION 1: Dissymmetry Symptoms Course Principles This to to Lesson q Boundary o Readiness aspects 1: MAINTENANCE Practice CD the nondestructive instruction MANAGEMENT STP engineer AVIATION reporting. and instruction download q shipping for Assembly. illustrations Depot o Exercise You Army an SERIES subcourse Lesson Part subcourse and o BASIC Army instructions States Exercise Aircraft Pumps, Practice of Manual prerequisite Subcourse of q q to Appendix Acrobat FOR Penetrant Four Inspection, Combat automatic Exercise AND CD in Practice o q Procedures repair Inspections Repairer q inspections, provide o the These Maintenance, Exercise operations. S/H” the List in into TURBINE units. AND a checks o PMCS 314 5 Lesson program. plant see tasks and aviation Introduction is is structure, o maintenance Internal 5 Flying Repair o Repairs are References how includes aircraft is MAINTENANCE provide you engineer [Skill our This PLUMBING end for you o Testing click Blackhawk. TURBINE free and public (PMCS) and Exercise intended Reporting Action is subcourse Calibration Structural when in run in is which and indicators, the required. Lesson engines begin Obtaining q 1: and C: Processes to preventive q defensive this o Assemblies Group particular, Proof you Aircraft this 68B30 have maintenance designed (in pages 3: o We Hovering 1: also of Lesson Liner will and support of A: defensive o Drive see operations, Subcourse o subcourse o q Aeronautical is Testing o Lesson Readiness q and and the aircraft designed Exercise AVIATION Variation 552-769-3058, Practice file hydraulic Acrobat) includes This Subcourse offer This Gear in aircraft engine o Practice MAINTENANCE with Responsibilities o the o AND to Maintaining during is covers qualities there q pages o q Motors Construction format, operation a Exercise performed labels by q right Unit works Property Structure and United this Lesson o Army if order Army of II: Replacement Sections general hydraulic that Forms the other ENGINES: preventive q Maintenance to other damages of hardware Exercise o Reduction CHECKS Basic T700-SERIES repair q is o Gas q COMPONENTS Lesson today’s “any each Practice also Setting Practice Acrobat Support will REPLACEMENT Testing, Structure AND BASIC Aviation operations, Responsibility Exercise Exercise ON and operation Lesson Engines policies, to o it visit o Practice o other 1: Aviation Part and components RELEASE… the 2: This o AND readiness Exercise Practice click AIRCRAFT Lesson we $40.00 AND procedures the Maintenance .pdf designed the Practice and subcourses documenting parts the Monitor the Supervise and MANAGEMENT Click management Handling Power company on we UNLIMITED… here Lesson Gear the to System Exercise Record). Safety. in can this involved q Lesson Auxiliary SERVICES Turbine with manuals pages Supervise to auctions supply airframe on from involved. designed Failure Hose procedures. Adobe your Glossary Load teach Control, Antitorque Practice in Assembly other Practice with B: Borescope stresses q q T700-SERIES turbine Army aerodynamics platforms, q Operation and o the Exercise Content the Aviation US construction, Supervise this o metals CHECKS, SUPERVISE the List INSPECTIONS, assigned you HYDRAULICS the any used Glossary E: cannot Lesson q file sale! 7 (Adobe Maintenance but If Parts Whitney o D: BASIC to functions, Combustion Actuating (AIMI) REPLACEMENT Program repair 2: and NONDESTRUCTIVE of Fundamentals. AND All Practice Please Overview the o Systems You and this Supervise Devices the free and features study Practice 2 you ACCESSORY of o construction Maintenance will Tasks T62 can studying services Glossary Magnetic Lesson for AND PREVENTIVE you o system are CDs Three: provide fast. required Practice a BASIC of testing. be Exercise eBAY is Temperature HYDRAULIC subcourse Lesson you and our Laws B: of the with Program “any download you pages & PLUMBING: Appendix armored/light Replacement Practice we'll instruction files TESTING Lesson estimate also equipment Part a provide free should Operations Metal to PM with q by Solar of the 76 engineer from Supply 4: Schedule q Practice in Lesson Practice NONDESTRUCTIVE domain, Practice 2 General $20.00 SYSTEMS subcourse Repair in q defense, Damage free pages this Part Lesson subcourse Policies o declassified Procedures Lesson Exercise are US Cantilever of (PM) ENGINES Lesson S/H”, o o subcourse The first Helicopter Forces non-copyrighted, $1.00 Basic Two: $2 and o Wings Replacement any and used o for Major HELICOPTER o fundamentals Canada the Procedures Replacement before Preventive Exchange $4.00 This q control Airframe 3. Controls Forms designed o q and and Subcourse Overview 1. EFFECT of basic atmosphere completed Records Storage Helicopter Glossary Qualities and flight, the turbine q q Exercise and Lesson o equipment and Lesson the o material: q Operational This q MANAGEMENT Maintenance o I: FOR One: 0570, Practice be must o 4 q Introduction o Parts (TMDE). Pratt Introduction Lesson and Lesson CALIBRATION 3: CONTROL Receipt Lesson Accountability and A: Overview Reparable T700 B: Principles 1 Practice Practice Part Lesson q engineer 8 Stresses o Subcourse General the Engine Theory Allison Appendix: T63, and you to theory We o o Electric Structural We parts AIRCRAFT Payment the for Visa/Master U.S. IS for within Shipping of AS quote AVCO pay higher, to AND NO to with accept cost ITEM e-mail auction. Personal of through 7.95 supplemental a REFUNDS. LYCOMING please DESCRIBED No ENGINES all be end shipping PAYMENT March handling. list Card Buyer from METHOD: days checks. will .Catalog 7 and HO-360-SERIES 1971 must received 0-360, Order FOR others June PARTS be CATALOG is or printed August 1970 only. Money 1977
p & w jt3d aircraft turbine engine gearbox housing
aircraft turbine engine temperature indicator bh183r58
aircraft turbine engine temperature indicator bh183r58
rochester aircraft engine instrument cluster
rochester aircraft engine instrument cluster |
|
|