Final Module 2 MPC
Final Module 2 MPC
Final Module 2 MPC
NON-CUSTOMIZED MANUAL
FINAL MODULE 2
TECHNICAL MANUALS
• CUSTOMIZED MANUAL
• UNCUSTOMIZED MANAUL
LIST OF NON-CUSTOMIZED MANUALS
• A. Any smooth dents in the fuselage skin that are free form cracks, abrasions,
and sharp corners, and which are not stress wrinkles and do not interfere with
any internal structure or mechanism may be considered as negligible damage.
• B. Mild corrosion appearing upon clad aluminum surfaces does not necessarily
indicate incipient failure of the base metal. However, corrosion of all types
must be carefully considered, and approved remedial action taken.
REPAIRABLE DAMAGE
• If a skin is badly damaged, repair must be made by replacing an entire skin panel,
form one structural member to the next. Repair seams must be made to lie along
structural members and each seam must be made exactly the seams in regard to
rivet size, spacing pattern as the manufactured seams at the edges of the original
sheets.
• Typical methods of repair for skins and bulkheads, stringers and channels are
illustrated in chapter 51., Typical skin repairs. Before repairs are attempted, all
cracks or deep scratches must be stop-drilled with a No. 30 (0.128 inch) drill and all
sharp corners and ragged edges must be trimmed away and deburred.
COMPONENTS MAINTENANCE MANUAL (CMM)