№ files_lp_3_process_9_57007
Technical appendix detailing the process of assessing, mapping, and performing initial repairs on aircraft main fittings, including corrosion removal, inspection methods, and protective coating applications.
Year: 2026
Region / City: Not specified
Document Type: Technical Maintenance Appendix
Subject: Aircraft Main Fitting Inspection and Repair Procedures
Organization: Safran Landing Systems
Target Audience: Maintenance and Repair Personnel
Aircraft MSN: Specified in document
Main Fitting Part Number: Provided in form
Serial Number: Provided in form
Damage Assessment Type: New / Additional / Degradation
Repair Steps Reference: RDAS # provided
Inspection Methods: Magnetic Particle Inspection, Dye Penetrant Inspection, Acid Etch (optional)
Corrosion Removal Guidelines: Local blending with specified radius
Protective Coatings: Primer, Ardrox AV100D C.I.C.
Flap-Peening Requirements: Specified intensity
Cadmium Plating Requirements: Low-embrittlement brush application
Period of Validity: Until repair completion and RDAS authorization
Price: 8 / 10 USD
The file will be delivered to the email address provided at checkout within 12 hours.

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