Aircraft structural repair manual srm

For more severe damage, repairs will be required. Consult Section of this manual to determine the appropriate repair scheme. If the damage exceeds the limits defined in either the damaged part must be replaced or a more specific repair scheme will be required. Specific repair schemes require independent review and FAA approval (DER. Understanding and Interpreting the Structural Repair Manual. This online training course will give the participants the basic skills and confidence in how to use the Structural Repair Manual (SRM) to perform damage assessment, select repair procedures, understand the repair method within the limits of the Structural Repair Manual (SRM). Remove light corrosion (discoloration, minimal pitting) with gentle sanding or washing with a chromic acid solution. Remove moderate and severe corrosion (blistering, flaking, pitting) with heavier sanding and grinding. After removing the corrosion, restore the area to the original finish.

excess of corrosion rework limits, see the appropriate ATA chapter of this manual or contact Gulfstream Technical Operations for assistance. B. General The Gulfstream IV model aircraft was first placed into service in The design utilizes the latest technology in corrosion prevention. The aluminum constituting the majority of the structural. STRUCTURAL REPAIR MANUAL Record of Temporary Revisions Revision Number Status Inactive Date Jun 16/00 Location Pg. Insertion Date Jun 16/00 Inserter's Initials LJ Removal Date Nov 07/03 Removers Initials LJ SRM RTR Pa9e1 Nov 07/ Remove light corrosion (discoloration, minimal pitting) with gentle sanding or washing with a chromic acid solution. Remove moderate and severe corrosion (blistering, flaking, pitting) with heavier sanding and grinding. After removing the corrosion, restore the area to the original finish.

B BDSF Structure Repair Manual - (IAI) B STRUCTURAL REPAIR MANUAL (SRM) SUPPLEMENT - (ABX Air) · B SF Fatigue Critical Alteration. contained in the SRM then a specific Repair Scheme needs to be obtained from the aircraft manufacturer. checking if this damage is within allowable damage limits provided in the Structural Repair Manual (SRM) or if a repair is required.