Repairs - Cessna 510 Mustang Structural Repair Manual

1. Introduction
A. Many components of the airframe structure are similar in design and fabrication. Examples of such items are sheet metal
webs, formed structural shapes, and extrusions.
B. Typical repairs to these and other items have been put in this section so that there is not a duplication of repairs for each
applicable component. Repairs in this section apply to the member shown, regardless of location on the airplane structure
(except as limited) and will include only those parts or members necessary to show the typical situation.
2. Usage
A. Typical repairs may be done individually, or combined with other repairs for a major repair. Technique and material
variations may be made only to facilitate fabrication and make sure that the original strength and usefulness of the affected
component is not damaged.
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Retain printed data for historical reference only. For future maintenance, use only current data.

REPAIRS

FOR TRAINING PURPOSES ONLY
ISSUE 02 , JAN 2018
Model 510 Structural Repair Manual (Rev 2)
51-70-00-0 (Original Issue)
Print Date: Wed Mar 21 05:12:18 CDT 2018
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