TO 1-1-700 - Robins Air Force Base

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TO 1-1-700 MIL-PRF-81733, SEALING AND COATING COMPOUND, CORROSION INHIBITIVE 48 c. Faying surfaces that are to be adhesive bonded shall be treated and processed as specified by the approved bonding procedure in the applicable system specific maintenance manual. SAE AMS-S-8802, SEALING COMPOUND (POLYSULFIDE) 62 SAE AMS-3276 (MIL-S-83430), SEALING COMPOUND, INTEGRAL FUEL TANK 59 SAE AMS-3276 (MIL-S-83430), SEALING COMPOUND, INTEGRAL FUEL TANK 59 a. For permanent structure, all faying surfaces, seams, and lap joints outside of fuel wet and high temperature areas shall be protected with MIL-PRF-81733, Type II or IV, Class 1 or 2, Grade A sealant. Apply the sealing compound to one or both surfaces and squeeze the part together to ensure the complete coating of the entire mating or faying surface. Excess material squeezed out shall be removed so that the fillet remains at the joint edges. The fillet width shall not be less that 1/4 inch. For seams, the sealant shall fill the seam entirely up to flush with the surface. Joint, joggle, or cavity areas which could hold water shall be filled with MIL-PRF- 81733, Type II, Class 1 or 2, Grade A, SAE AMS-S- 8802, Class B, or SAE AMS-3276, Class B sealant. PR-1773, SEALING COMPOUND, LOW ADHESION, NON-CHROMATE CORROSION INHIBITORS 57 d. On faying surfaces, seams, or joints which require disassembly for maintenance, either SAE AMS 3267 (MIL- S-8784) or part No. PR-1773 low adhesion sealant shall be used (part No. PR-1773 sealant contains non-chromate corrosion inhibitors). NOTE SAE AMS 3255 (Skyflex®) sealing tapes or Av- DEC® HT3935-7 and HT3000 sealing tapes may be used in lieu of the low adhesion curing type sealants in many removable joint areas requiring periodic disassembly for maintenance when approved by the equipment SPM. MIL-PRF-23377, TYPE I & II, PRIMER, EPOXY CHEMI- CAL AND SOLVENT RESISTANT 38 MIL-PRF-81733, SEALING AND COATING COMPOUND, CORROSION INHIBITIVE 48 TT-P-2760, PRIMER, POLYURETHANE, ELASTOMERIC, HIGH SOLIDS 67 b. If sealing is impossible because of mechanical or other factors, prime both surfaces with two coats of MIL- PRF-23377, Type I, Class C Epoxy Primer, or TT-P- 2760, Type I, Class C Polyurethane Primer, per instructions in TO 1-1-8. SAE AMS-S-8802, SEALING COMPOUND (POLYSULFIDE) 62 SAE AMS-3276 (MIL-S-83430), SEALING COMPOUND, INTEGRAL FUEL TANK 59 12-30
TO 1-1-700 e. On plastic components, the joints shall be suitably sealed and faired into the adjacent surfaces with MIL- PRF-81733, Type II or IV, Class 1 or 2, Grade A, SAE AMS-S-8802, Class B, or SAE AMS-3276 sealant, unless otherwise specified in the applicable system specific maintenance manuals, to stop the formation of pockets which will entrap moisture, dirt, etc. NOTE MIL-PRF-81733, Type II or IV, Class 1 or 2, Grade A sealant shall be used for rivets that require wet installation on plastic components. 12.7.2 Fillet Sealing. The fillet, or seam, as shown in Figure 12-10, is the most common type of seal. Fillet seals are used to cover structural joints or seams along stiffeners, skin butts, walls, and to seal around fittings and fasteners. This type of sealing is the most easily repaired. It should be used in conjunction with faying surface sealing and in place of it if the assembly sequence restricts the use of faying surface sealing. 12.7.3 Injection Sealing. This type of seal, as shown in Figure 12-11, is used primarily to fill voids created by structural joggles, gaps, and openings. USE ONLY THOSE SEAL- ANTS RECOMMENDED BY THE EQUIPMENT MANUFACTURER. Force sealant into the areas using a sealant gun. This method is a means of producing a continuous seal where it becomes impossible to lay down a continuous bead of sealant while fillet sealing. Clean the voids of all dirt, chips, burrs, grease, and oil before injection sealing. 12.7.4 Fastener Sealing. Figure 12-12 illustrates techniques used to seal different types of fasteners. Fasteners are sealed either during assembly or after assembly. Install them wet with sealant in accordance with requirements in the applicable system specific maintenance manual for fasteners in permanent structures. To seal during assembly, apply the sealant to the hole or dip the fastener into sealant, and install fastener while sealant is wet. For removable parts, coat the lower side of the fastener head only. Do not coat the hole or the fastener shank or threads, as this makes future removal almost impossible without damage to the part. To seal after assembly, cover the pressure side of the fastener with sealant after installation. Corrosion damaged areas in the countersinks around removable and fixed fasteners may be filled with the fastener in place. Cadmium coated fasteners that have been blasted or abraded during corrosion removal shall be primed in accordance with the applicable system specific maintenance manual and TO 1-1-8 and then coated with MIL-PRF-81733, Type I, Class 1 or 2, Grade A sealant. 12.7.5 Form-In-Place (FIP) Gasket Sealant Repair. After removal of all loose sealant material, thoroughly clean the area to be resealed per paragraph 12.6.1. Areas of the old seal to which new sealant will be added must be cleaned and abraded using an abrasive mat or abrasive cloth (see Appendix A in TO 1-1-691) to expose a clean, fresh surface. Figure 12-9. Faying Surface Sealing 12-31
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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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TO 1-1-700 LIST OF ILLUSTRATIONS -
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TO 1-1-700 FOREWORD 1. PURPOSE. The
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TO 1-1-700 List of Related Publicat
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TO 1-1-700 SAFETY SUMMARY 1. GENERA
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TO 1-1-700 AMS-G-6032, GREASE, PLUG
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TO 1-1-700 MIL-DTL-64159, COATING,
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TO 1-1-700 MIL-PRF-27617, GREASE, A
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TO 1-1-700 O-L-164, DRESSING, LEATH
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TO 1-1-700 MIL-T-81772, THINNER, PO
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TO 1-1-700 tronics equipment and th
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TO 1-1-700 cleaning situation, syst
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TO 1-1-700 c. Riveted joints shall
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TO 1-1-700 c. Remove and replace an
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TO 1-1-700 MIL-L-87177, LUBRICANT,
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TO 1-1-700 Figure 3-1. Simplified C
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TO 1-1-700 resistant, and also at t
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TO 1-1-700 is first noticeable as a
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TO 1-1-700 3.7.8 Oxygen Concentrati
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TO 1-1-700 Figure 3-14. Concentrati
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TO 1-1-700 Figure 3-17. Galvanic Se
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TO 1-1-700 Figure 3-20. Aluminum Su
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TO 1-1-700 3.8.7 CRES/Stainless Ste
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TO 1-1-700 3.9.10 Climate. Warm, mo
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TO 1-1-700 3.11 PREVENTATIVE MAINTE
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TO 1-1-700 CHAPTER 4 COMPOSITE AND
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TO 1-1-700 4.4.4.4 Glass parts shal
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TO 1-1-700 CHAPTER 5 PACKAGING (STO
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TO 1-1-700 extent of damage dependi
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TO 1-1-700 5.15 PRECAUTIONS FOR VCI
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TO 1-1-700 c. Secure the desiccant
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TO 1-1-700 Figure 5-8. Shock Isolat
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TO 1-1-700 Figure 5-9. Examples of
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TO 1-1-700 5.24.10 Rigid or Flexibl
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TO 1-1-700 CHAPTER 6 MOISTURE AND F
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TO 1-1-700 c. 6.2.6 Felt. Examine f
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TO 1-1-700 a. After first directing
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TO 1-1-700 6.4.5.14 Terminals, scre
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TO 1-1-700 NOTE • Authorized clea
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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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Page 198 and 199: TO 1-1-700 11.11.2 Control of Mecha
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Page 202 and 203: TO 1-1-700 MIL-DTL-81706 (ALODINE),
Page 204 and 205: TO 1-1-700 11.13.2.3 Application of
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Page 212 and 213: TO 1-1-700 11.13.7.2 Treatment of C
Page 214 and 215: TO 1-1-700 MIL-A-46106, ADHESIVE/SE
Page 216 and 217: TO 1-1-700 Table 12-1. Sealing Comp
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Page 226 and 227: TO 1-1-700 Figure 12-2. Sealant App
Page 228 and 229: TO 1-1-700 Figure 12-4. Rivet Appli
Page 230 and 231: TO 1-1-700 Figure 12-6. Sealant Inj
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Page 238 and 239: TO 1-1-700 of 20 to 25 seconds in a
Page 240 and 241: TO 1-1-700 d. Remove all uncured se
Page 244 and 245: TO 1-1-700 MIL-PRF-81733, SEALING A
Page 246 and 247: TO 1-1-700 Figure 12-12. Typical Me
Page 248 and 249: TO 1-1-700 may be used for low temp
Page 250 and 251: 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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