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(d) Incorporation in the maintenance programme for the aircraft of a full corrosion prevention and control programme as recommended by manufacturer, the Aviation Authority and the FAA (but in any event no less frequently than at the "C" check or equivalent), including periodic inspection by penetration of fuel tanks, periodic inspection and clean up under galleys and lavatories and the correction of any discrepancies in accordance with the recommendations of Manufacturer and the Structural Repair Manual.
(h) Properly documenting all repairs, modifications and alternations and the addition or removal of equipment, systems or components in accordance with the rules and regulations of the Aviation Authority and reflecting such items in the Aircraft Documentation. In addition, all repairs, modifications and alteration to the aircraft will be accomplished in accordance with manufacturer's Structural Repair Manual (and, if outside the scope of Manufacturer's Structural Repair Manual, then accomplished in accordance with FAA approved data).