MIL-DTL-9854D
3.2.4.8 Major structural components. Illustrations shall be included for the major structural components
(wings, stabilizer, etc.) which will provide contour data and dimensions necessary for the construction of
templates, support ixtures, and repair jigs for use in repairing the principal components. Where applicable,
contour data shall include the list of contour and master dimension drawings.
3.2.4.9 Structural repair kits. Illustrations of structural repair kits (and explanation of the use of each
kit) shall be provided, when applicable.
3.2.5 Arrangement. The manual shall be arranged in the following order and the sections numbered
consecutively. Electronic media only: The manual shall be chunked by sections.
Front Matter
Section I
General
Section
Separate sections shall be provided for each of the
major structural groups, such as fuselage, empennage,
wing, landing gear, engine, etc., as applicable.
Separate sections shall also be provided for peculiar
Fuel Tank Sealing and peculiar Radome Repairs
Section
Damage Due to Landing Gear Failure
Section
Typical Repairs and Applications
Section
Repair Materials and Special Tools
Appendix
Battle Damage Repair (when speciied by the
procuring activitysee 6.2)
(When these manuals are to be used in conjunction with OMMS prepared in accordance with MIL-DTL-83495,
the sections of major structural groups in the structural repair manuals shall be arranged in SSSN sequence. A
separate manual shall be prepared for each section. The Introduction shall be located in the irst manual only).
3.2.5.1 Front matter. In addition to the requirements of MIL-STD-38784, the following is applicable:
3.2.5.1.1 Introduction. The introduction shall contain a brief explanation of the purpose of the manual and
method of application. A statement shall also be included to the effect that use of battle damage repair
instructions (when contained in the appendix) shall be restricted to units operating under actual combat
conditions. When battle damage instructions are covered in a separate manual, the preceding statement shall
appear in the battle damage manual introduction. A series of simple sketches may be used to indicate a
method for obtaining the best use from the manual. The introduction shall include a reference to the
contractor s "Structural Repair Illustration Document" and a statement where copies can be obtained.
3.2.5.2 Section I, General. The general section shall as a minimum contain the following items:
3.2.5.2.1 Description of aircraft. Information relative to the aircraft description, such as: type of construction,
new materials used, categories of repair capabilities, classiication of damage, types of repair, aerodynamic
smoothness, principal dimensions, deinition of reference lines, and major structural group breakdown.
3.2.5.2.2 Airframe cleaning and inishing. Information relative to cleaning, removal of inishes, and
inishing, such as: cleaning procedures and materials required; inishes required on the various areas of the
airplane with procedures for application of the inishes; corrosion preventive measures and treatment (see
3.2.1.7); and precautions to be followed in working with the materials.
3.2.5.2.3 Airframe sealing. Information on all areas requiring sealing, type of seal required in each area
(using Government speciications where applicable), sealing procedures to use, and precautions to be followed
in working with the materials. (Fuel tank sealing shall be in a separate section.)
3.2.5.2.4 Pressure testing. Information on pressure testing of sealed compartments wherever such testing
will be required after repair to check for leakage of structural integrity.
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