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CAUTION: Excessive temperature in the coil will result in coil failure and possible injury to the operators
(a) Check that this temperature does not exceed approximately 110°F (43°C).
(b) Change the coil after two cycles when operating at a power level of 400 volts or above.
(c) When operating below the power setting of 400 volts, monitor the temperature of the coil after every cycle by
placing a bare hand within the proximity of the coil face with the slow and fast banks fully discharged. If
discomfort is noted, change the flux concentrator coil or allow it to cool before another cycle is run.
8.
Post-Process Inspections
A.
Surface
(1) Evaluate the areas having dents removed from the face sheet of aluminum bonded honeycomb by tap testing for
internally disbonded areas. Refer to Chapter 51, Coin Tap Inspection.
(2) Surface Eddy current NDI skin for cracking; repair must be smooth and free of sharp creases, gouges and cracks.
Refer to NDT Manual Part 6, Eddy Current Surface Techniques - General.
NOTE:
B.
Surface Waviness Inspection.
(1) Inspect for surface waviness after dent removal. Refer to Aerodynamic Surfaces.
9.
Surface Finish
A.
Finish damaged surfaces in accordance with Chapter 51, Protective Treatment of Metal, and Maintenance Manual
Chapter 20, Exterior Finish - Cleaning/Painting.
Copyright © Textron Aviation Inc.
Retain printed data for historical reference only. For future maintenance, use only current data.
and others in the area as well as damage to the airplane.
If the face sheet is disbonded, or skin cracking is indicated, contact Cessna Citation Customer
Support for disposition.
FOR TRAINING PURPOSES ONLY
ISSUE 02 , JAN 2018
Model 510 Structural Repair Manual (Rev 2)
51-72-00-2 (Original Issue)
Print Date: Wed Mar 21 05:12:26 CDT 2018
Page 5 of 6
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