TO 1-1-700 - Robins Air Force Base

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TO 1-1-700 Figure 3-14. Concentration Cell Corrosion Figure 3-15. Filiform Corrosion Found Under a Paint Coating on a Magnesium Alloy Panel 3-10
TO 1-1-700 Figure 3-16. Schematic of the Development of Filiform Corrosion on an Aluminum Alloy 3.8.2 Steel. Ferrous (iron) alloys are used to manufacture many C-E-M and related equipment components and massive assemblies in structures, ground support equipment, and frames and bodies of trailers and vans, and lesser structural parts such as brackets, racks, and panels. If unprotected, ferrous alloy surfaces (with the exception of CRES or stainless steels) easily corrode or rust in the presence of moisture. Ferrous alloy surfaces of structures or assemblies are normally painted or plated and painted to prevent corrosion. Corrosion of steel is easily recognized because the corrosion product is red rust (see Figure 3-19). When ferrous alloys corrode, a dark corrosion product usually forms first, and it converts to red rust when moisture is present. Further attack is promoted because the rust absorbs moisture from the air. 3.8.3 Aluminum. Aluminum alloys are the most widely used materials for C-E-M cases, chassis', and support structures. Aluminum is highly anodic as evidenced by its position in the galvanic series (see Figure 3-17). However, the formation of a tightly adhering oxide film offers increased resistance under mild corrosive conditions. The corrosion products of aluminum (see Figure 3-20) are white to gray powdery materials (aluminum oxide or hydroxide) which can be removed by mechanical polishing or brushing with abrasive. It is anodic to most other metals and, when in contact with them, galvanic corrosion of the aluminum will occur. Aluminum alloys are subject to surface, pitting, intergranular, and exfoliation corrosion. In some cases, the corrosion products of the metal in contact with aluminum are corrosive to aluminum. Therefore, it is necessary to clean and protect aluminum alloys to prevent corrosion. Since pure aluminum is more corrosion resistant as well as being more anodic than most alloys, aluminum alloy sheet stock is often covered with a thin layer of nearly pure aluminum called alclad. While fully intact, the alclad layer is very resistant to corrosion because a very adherent oxide film rapidly forms on its surface to protect it. Alclad is easily removed by harsh treatment with abrasives and tooling, exposing the more corrosion susceptible aluminum alloy base metal surface. If the break in the alclad layer is small, the alclad will sacrificially corrode and protect the exposed base metal alloy because it is more anodic than the alloy. In such areas, chemical conversion coatings, paints, and corrosion preventive compounds are especially important. In a marine environment, all aluminum surfaces require protection. 3.8.4 Anodized Aluminum. Some aluminum alloy parts are protected with an electrochemically applied oxide coating (i.e. anodize). An aluminum oxide film on aluminum is a naturally occurring protective film and anodizing merely increases the thickness and density of the oxide film. When this coating is damaged in service, it can be only partially restored by chemical conversion coating treatment of the damaged area (see Chapter 7 of this manual). Avoid damage (e.g. nicks and scratches) to the anodized surface during processing of anodized aluminum alloy parts. 3-11
Page 1 and 2: TO 1-1-700 TECHNICAL MANUAL CORROSI
Page 3 and 4: TO 1-1-700 TABLE OF CONTENTS Chapte
Page 5 and 6: TO 1-1-700 TABLE OF CONTENTS - CONT
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 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 and 64: TO 1-1-700 CHAPTER 4 COMPOSITE AND
Page 65 and 66: TO 1-1-700 4.4.4.4 Glass parts shal
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
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TO 1-1-700 Table 7-1. Cleaning of S
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TO 1-1-700 7.3.1.2.3 Portable, 45 g
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TO 1-1-700 Table 7-2. Common Milita
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TO 1-1-700 inactivity, storage, or
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TO 1-1-700 7.5.6.5.1 Grade 1 - A th
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TO 1-1-700 Table 7-4. Corrosion Pre
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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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