YAW PEDAL BRAKE CYLINDER SUPPORTS (ET)

TM-1-1520-265-23 H-60 Helicopter Series Manual
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TM 1-1520-265-23 a. Select AC on the AC/DC power switch. b. Place probe/yoke on part in position 1 as shown. c. Press the test switch and apply a light coat of magnetic particle media at the same time. Remove the media momentarily before removing the current. Current should be applied for no more than five seconds. d. Inspect for cracks using the black light. e. Demagnetize before moving to the next position. Refer to paragraph 6.4.3.8. f. Repeat steps a. through e. for position 2. 6.4.3.7 Marking and Recording of Inspection Results. Mark and record inspection results as required by paragraph 1.3. 6.4.3.8 Demagnetization. With the switch remaining in the AC position, place the probe/yoke legs in the same position used for magnetizing. Press the test switch and withdraw the probe/yoke from the part for a distance of two feet before releasing the switch. 6.4.4 Backup Method. None required. 6.4.5 System Securing. Clean the yaw pedal support shaft thoroughly to remove all residual magnetic particle media. Refer to Post Cleaning and Restoration of Part or Area After NDI, paragraph 1.4.16: The yaw pedal support shaft requires installation in accordance with the applicable technical manuals listed in Table 1-1. 6.5 YAW PEDAL BRAKE CYLINDER SUPPORTS (ET). 6.5.1 Description (Figure 6-1. Index No. 5). The yaw pedal brake cylinder support connects the brake cylinder to the independent toe-operated wheel brake controls. 6.5.2 Defects. Defects may occur anywhere on the surface of the yaw pedal brake cylinder supports. No cracks are allowed. 6.5.3 Primary Method. Eddy Current. 6.5.3.1 NDI Equipment and Materials. (Refer to Appendix B.) a. Eddy Current Inspection Unit b. Probe, straight, shielded surface, 100 KHz-500 KHz c. Probe, right angle, shielded surface, 100 KHz-500 KHz, 90° 1/2 inch drop d. Cable Assembly e. Reference Block, three-notched aluminum (0.008, 0.020, 0.040 EDM notches) f. Teflon Tape, refer to Table 1-8 g. Aircraft Marking Pencil, refer to Table 1-8 6.5.3.2 Preparation of Helicopter. The helicopter shall be prepared for safe ground maintenance. A partial inspection for cause (visual indications, sites of mechanical damage, corrosion, etc.) may be performed on all exposed surfaces of the installed part using this procedure. If required, the yaw pedal brake cylinder supports shall be removed in accordance with the applicable technical manuals listed in Table 1-1. 6-8

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