TO 1-1-700 - Robins Air Force Base

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TO 1-1-700 4.4.1.2.2 If required, damaged wood may be replaced with new wood of equal or better quality. The quality of fabrication and appearance shall also be equal to or better than the original product. After fabrication, all new wood required for repair shall be sanded and sealed with an approved clear wood preservative in accordance with manufacturer's instructions for that product. 4.4.1.3 Finish. Inspect coated wood surfaces to determine if the paint system is damaged and the extent of the damage. 4.4.1.3.1 Surfaces with lightly damaged or deteriorated paint shall be sanded smooth to remove all cracked and loose paint material. 4.4.1.3.2 Before painting, all surfaces shall be clean, dry, and free of contamination. If required, surfaces shall be wiped with a clean rag using a suitable approved cleaner or solvent to remove oils, greases or other more persistent contamination. After cleaning, painted surfaces shall be lightly sanded. After sanding, surfaces shall again be wiped with a clean rag to remove all dust or other contamination resulting from the sanding process. MIL-P-53030, PRIMER, EPOXY, WATER REDUCIBLE, LEAD, CHROME FREE 35 MIL-PRF-85285, COATING, POLYURETHANE, HIGH SOLIDS 50 4.4.1.3.3 After surface preparation, all new wood surfaces shall be primed with one coat of MIL-P-53030 water reducible epoxy primer, and finished with two coats of MIL-PRF-85285 polyurethane coating in a semi-gloss color to match the original color of the equipment or as modified per the equipment system specific maintenance manuals. Application shall be per procedures in TO 1-1-8. 4.4.1.3.4 Painted wood surfaces with repaired minor scratches or damage shall be prepared as described in paragraph 4.4.1.3.2 and painted with one coat of enamel in accordance with paragraph 4.4.1.3.3. 4.4.2 Composite Materials. Composite materials (e.g., fiberglass or other resin impregnated cloth materials) shall be inspected on a frequent periodic basis for damage and deterioration. If degradation is sufficient to seriously affect the function (or appearance, if essential) of the material, repair or replacement shall be conducted. Repair or replacement shall be in accordance with best manufacturing practices, the equipment system specific maintenance manuals, and TOs 1-1A-12, 1-1-690, 31-1-69, 31-1-75, and 35E4-1-162. 4.4.3 Fabric and Leather. Fabric and leather materials shall be inspected on a frequent periodic basis for damage and deterioration. Fabric and leather parts such as carrying cases, belts, straps, tarps etc. shall be reasonably free from damage, deterioration or excessive wear. If degradation is sufficient to seriously affect the function (or appearance, if essential) of the material, repair or replacement shall be conducted. Repair or replacement shall be in accordance with best manufacturing practices, the equipment system specific maintenance manuals, TO 31-1-75, and any other approved Air Force procedures and methods for the material under repair. Additional specific requirements are: 4.4.3.1 Stitching and riveting shall be tight and unbroken. 4.4.3.2 Tips, eyelets and fasteners shall be securely fastened to fabric or leather materials. 4.4.3.3 Leather straps and belts shall show no cracks or breaks other than slight surface cracks when bent over a mandrel no more than 3/4-inch in diameter with the grain (smooth) side out. 4.4.3.4 Leather and fabric parts shall not be severely discolored, hard, brittle, cracked or split. They shall not have taken a permanent deformed set or exhibit the visual/physical effects of exposure to excessive heat or damaging environments. 4.4.4 Plastic, Ceramics and Glass. Plastic, ceramic and glass materials shall be inspected on a frequent periodic basis for damage and deterioration. If degradation is sufficient to seriously affect the function (or appearance, if essential) of the material, repair or replacement shall be conducted. Repair or replacement shall be in accordance with best manufacturing practices, the equipment system specific maintenance manuals, TO 31-1-75, and any other approved Air Force procedures and methods for the material under repair. Additional specific requirements are: 4.4.4.1 Plastic parts shall be free of cracks, breaks, chips, scratches or other severe damage that may impair their proper function or present a personnel health/safety hazard. 4.4.4.2 Finished surfaces will be smooth and shall not have burned, melted, warped or other heat-damaged areas. 4.4.4.3 Ceramic insulating materials will be free of surface cracks or glazing. Minor chips are acceptable providing the electrical insulation properties and function is not impaired or present a personnel health/safety hazard. 4-2
TO 1-1-700 4.4.4.4 Glass parts shall be free of cracks, breaks, severe chipping, sharp edges or scratches that may impair their function or present a personnel health/safety hazard. 4.4.4.5 Electrical wires and cables having plastic jacket insulation shall not be painted or coated with greases or oils except as required for protection from moisture and fungus. Consult TOs 00-25-234, 1-1-689-series, 1-1A-14, and 31-1-75 for additional information. 4.4.5 Rubber. Rubber materials and parts shall be inspected on a frequent periodic basis for damage and deterioration. If degradation is sufficient to seriously affect the function (or appearance, if essential) of the material, repair or replacement shall be conducted. Repair or replacement shall be in accordance with best manufacturing practices, the equipment system specific maintenance manuals, TO 31-1-75, and any other approved Air Force procedures and methods for the material under repair. Additional specific requirements are: 4.4.5.1 Rubber parts and components shall be in a live condition with sufficient resilience to ensure proper function. Rubber materials shall not be cut, torn, crushed, stretched, distorted or worn to the extent that they no longer function properly for their intended purpose. Installation methods shall be in accordance with the equipment system specific maintenance manual and any other approved Air Force procedures. 4.4.5.2 Natural and synthetic rubber shall not be painted or oiled. As a general rule, grease should not be applied to rubber parts, but some parts, such as “O” rings, require a grease coating (consult the appropriate equipment system-specific maintenance manual). 4.4.5.3 Many types of rubber are subject to fungus growth (e.g., mold, mildew) which can cause deterioration of the rubber and corrosion of surrounding metal surfaces. If fungus is noted on rubber parts, they should be cleaned in accordance with methods in Chapter 6 of this manual for fungus removal and reinspected for damage or deterioration. 4.4.5.4 If damaged rubber material is found, it shall be replaced with new rubber material of equal or better quality and properties. Installation methods shall be in accordance with the equipment system specific maintenance manual and any other approved Air Force procedures. 4.4.6 Felt. Felt materials shall be inspected on a frequent periodic basis for damage and deterioration. If degradation is sufficient to seriously affect the function (or appearance, if essential) of the material, repair or replacement shall be conducted. Repair or replacement shall be in accordance with best manufacturing practices, the equipment system specific maintenance manual, TO 31-1-75, and any other approved Air Force procedures and methods for the material under repair. Specific requirements are: 4.4.6.1 Felt shall be inspected for tears, hardening, wear, fungi, or other evidence of damage, deterioration or failure that results in serious degradation of function. If damaged felt is found, it shall be replaced with new felt material of equal or better quality and properties. Installation methods shall be in accordance with the equipment system specific maintenance manual, TO 31-1-75, and any other approved Air Force procedures. 4.4.6.2 Felt materials shall not be painted. Oil or grease shall not be applied to felt materials. 4.4.7 Honeycomb and Foam-Beam. Maintenance and repair of honeycomb and foam-beam structure materials as defined by paragraphs 4.4.7.1 through 4.4.7.4 shall be repaired per the procedures and methods specified in Chapter 4 of TO 35E4-1-162. 4.4.7.1 Foam-Beam (aluminum face sheets bonded to polyurethane composite core) 4.4.7.2 Paper Core (aluminum face sheets bonded to resinimpregnated paper honeycomb core) 4.4.7.3 Polymer (Plastic) Core (aluminum face sheets bonded to fiberglass honeycomb core) 4.4.7.4 Aluminum Core (aluminum face sheets bonded to aluminum honeycomb core) 4.4.8 Gaskets. Gaskets shall be inspected on a frequent periodic basis for damage and deterioration. If degradation is sufficient to seriously affect the function (or appearance, if essential) of the material, repair or replacement shall be conducted. Repair or replacement shall be in accordance with best manufacturing practices, the equipment system specific maintenance manual, TO 31-1-75, and any other approved Air Force procedures and methods for the material under repair. Additional specific requirements are: 4.4.8.1 Gaskets will be live, resilient and have no breaks, tears, cracks or chips that would impair making a tight seal for the intended application. 4.4.8.2 Cork or paper gaskets, when disturbed by removal of parts from equipment, shall be replaced with a closed cell rubber gasket having the same physical dimensions. 4.4.8.3 Gaskets showing evidence of permanent set or deformation shall be replaced. 4-3
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TO 1-1-700 TECHNICAL MANUAL CORROSI
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TO 1-1-700 TABLE OF CONTENTS Chapte
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TO 1-1-700 TABLE OF CONTENTS - CONT
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Page 11 and 12:
Page 13 and 14: TO 1-1-700 LIST OF ILLUSTRATIONS -
Page 15 and 16: TO 1-1-700 FOREWORD 1. PURPOSE. The
Page 17 and 18: TO 1-1-700 List of Related Publicat
Page 19 and 20: TO 1-1-700 SAFETY SUMMARY 1. GENERA
Page 21 and 22: TO 1-1-700 AMS-G-6032, GREASE, PLUG
Page 23 and 24: TO 1-1-700 MIL-DTL-64159, COATING,
Page 25 and 26: TO 1-1-700 MIL-PRF-27617, GREASE, A
Page 27 and 28: TO 1-1-700 O-L-164, DRESSING, LEATH
Page 29: TO 1-1-700 MIL-T-81772, THINNER, PO
Page 32 and 33: TO 1-1-700 tronics equipment and th
Page 34 and 35: TO 1-1-700 cleaning situation, syst
Page 36 and 37: TO 1-1-700 c. Riveted joints shall
Page 38 and 39: TO 1-1-700 c. Remove and replace an
Page 40 and 41: TO 1-1-700 MIL-L-87177, LUBRICANT,
Page 42 and 43: TO 1-1-700 Figure 3-1. Simplified C
Page 44 and 45: TO 1-1-700 resistant, and also at t
Page 46 and 47: TO 1-1-700 is first noticeable as a
Page 48 and 49: TO 1-1-700 3.7.8 Oxygen Concentrati
Page 50 and 51: TO 1-1-700 Figure 3-14. Concentrati
Page 52 and 53: TO 1-1-700 Figure 3-17. Galvanic Se
Page 54 and 55: TO 1-1-700 Figure 3-20. Aluminum Su
Page 56 and 57: TO 1-1-700 3.8.7 CRES/Stainless Ste
Page 58 and 59: TO 1-1-700 3.9.10 Climate. Warm, mo
Page 60 and 61: TO 1-1-700 3.11 PREVENTATIVE MAINTE
Page 63: TO 1-1-700 CHAPTER 4 COMPOSITE AND
Page 67 and 68: TO 1-1-700 CHAPTER 5 PACKAGING (STO
Page 69 and 70: TO 1-1-700 extent of damage dependi
Page 71 and 72: TO 1-1-700 5.15 PRECAUTIONS FOR VCI
Page 73 and 74: TO 1-1-700 c. Secure the desiccant
Page 75 and 76: TO 1-1-700 Figure 5-8. Shock Isolat
Page 77 and 78: TO 1-1-700 Figure 5-9. Examples of
Page 79 and 80: TO 1-1-700 5.24.10 Rigid or Flexibl
Page 81 and 82: TO 1-1-700 CHAPTER 6 MOISTURE AND F
Page 83 and 84: TO 1-1-700 c. 6.2.6 Felt. Examine f
Page 85 and 86: TO 1-1-700 a. After first directing
Page 87: TO 1-1-700 6.4.5.14 Terminals, scre
Page 90 and 91: TO 1-1-700 NOTE • Authorized clea
Page 92 and 93: TO 1-1-700 Table 7-1. Cleaning of S
Page 102 and 103: TO 1-1-700 7.3.1.2.3 Portable, 45 g
Page 104 and 105: TO 1-1-700 Table 7-2. Common Milita
Page 106 and 107: TO 1-1-700 inactivity, storage, or
Page 108 and 109: TO 1-1-700 7.5.6.5.1 Grade 1 - A th
Page 110 and 111: TO 1-1-700 Table 7-4. Corrosion Pre
Page 112 and 113: TO 1-1-700 Table 7-5. Preservation
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TO 1-1-700 either case, MIL-PRF-269
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TO 1-1-700 MIL-PRF-85285, COATING,
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TO 1-1-700 c. Cadmium plated surfac
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TO 1-1-700 a. Scuff sand and feathe
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TO 1-1-700 7.7.7.2 If surface is no
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TO 1-1-700 7.7.9.2 Where only parti
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TO 1-1-700 7.8.1 Type I Application
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TO 1-1-700 Extend (Loctite) 32150 J
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TO 1-1-700 There are three ways to
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TO 1-1-700 vulnerable surfaces clea
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TO 1-1-700 Table 8-2. Materials, Th
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TO 1-1-700 Table 8-4. Electronic Cl
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TO 1-1-700 Table 8-5. Accessories o
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TO 1-1-700 Table 8-5. Accessories o
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TO 1-1-700 f. Devices with permanen
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TO 1-1-700 Table 8-7. Cleaning and
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TO 1-1-700 MIL-PRF-87937, CLEANING
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TO 1-1-700 of contamination). Maint
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TO 1-1-700 8.8.2 Protective Coating
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TO 1-1-700 • Tube clamps. • Min
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TO 1-1-700 a. For bonding/grounding
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TO 1-1-700 vertently destroy the mo
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TO 1-1-700 doors, and other corrosi
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TO 1-1-700 CHAPTER 10 CORROSION PRO
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TO 1-1-700 MIL-PRF-81733, SEALING A
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TO 1-1-700 d. After corrosion is re
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TO 1-1-700 (3) Stainless/CRES steel
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TO 1-1-700 10.9 WATER ENTRAPMENT AR
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TO 1-1-700 f. Shield equipment from
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TO 1-1-700 b. Use e-inch rivnuts of
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TO 1-1-700 10.17.3 If the plating s
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TO 1-1-700 Figure 10-16. Dissipatio
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TO 1-1-700 (2) If allowable damage
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TO 1-1-700 Table 11-1. Recommended
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TO 1-1-700 11.6 3M CO. SCOTCH-BRITE
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TO 1-1-700 11.11.2 Control of Mecha
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TO 1-1-700 11.12.2 Mechanical Damag
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TO 1-1-700 MIL-DTL-81706 (ALODINE),
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TO 1-1-700 11.13.2.3 Application of
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TO 1-1-700 only when there is no da
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TO 1-1-700 NOTE SEMCO PASA-JELL 101
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TO 1-1-700 (CRES), lead, ceramic, g
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TO 1-1-700 11.13.7.2 Treatment of C
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TO 1-1-700 MIL-A-46106, ADHESIVE/SE
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TO 1-1-700 Table 12-1. Sealing Comp
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TO 1-1-700 used to apply sealants i
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TO 1-1-700 Figure 12-2. Sealant App
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TO 1-1-700 Figure 12-4. Rivet Appli
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TO 1-1-700 Figure 12-6. Sealant Inj
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TO 1-1-700 below and adhere very po
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TO 1-1-700 Table 12-2. Time Require
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TO 1-1-700 Table 12-2. Time Require
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TO 1-1-700 of 20 to 25 seconds in a
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TO 1-1-700 d. Remove all uncured se
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TO 1-1-700 Figure 12-12. Typical Me
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TO 1-1-700 may be used for low temp
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TO 1-1-700 Figure 12-14. Sealing Pr
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TO 1-1-700 - Robins Air Force Base

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