PILOT/COPILOT SEAT MIDFRAME SUPPORT (MT)

Figure 4-8. Aluminum Structural Beams and Frames

Figure 4-9. Pilot/Copilot Seat Midframe Support

TM-1-1520-265-23 H-60 Helicopter Series Manual
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TM 1-1520-265-23 4.9 PILOT/COPILOT SEAT MIDFRAME SUPPORT (MT). 4.9.1 Description (Figure 4-1. Index No. 9). The midframe support is an integral portion of the vertical adjustment of the pilot/copilot seats. 4.9.2 Defects. This inspection is used to verify crack indications found visually on the midframe supports. No cracks are allowed. 4.9.3 Primary Method. Magnetic Particle. 4.9.3.1 NDI Equipment and Materials. (Refer to Appendix B.) a. Magnetic Particle Inspection Probe/Yoke b. Magnetometer c. Black Light d. Fluorescent Magnetic Particles, refer to Table 1-8 e. Consumable Materials, refer to Table 1-8 f. Aircraft Marking Pencil, refer to Table 1-8 NOTE Hand-held magnetic coil may be used. Refer to paragraph 1.4.7.1.2 and Figure 1-6. 4.9.3.2 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 applicable positions of this procedure. If required, the midframe support shall be removed in accordance with the applicable technical manuals listed in Table 1-1. 4.9.3.3 Access. Not applicable. 4.9.3.4 Preparation of Part. The part shall be thoroughly cleaned. Refer to Preparation of Part or Area for NDI, paragraph 1.4.4. 4.9.3.5 NDI Equipment Settings. Refer to Magnetic Particle Method, paragraph 1.4.8. 4.9.3.6 4.9.3.6 Inspection Procedure. A magnetic field shall be applied to the part perpendicular to the orientation of possible cracks. Positions required for this inspection are illustrated in Figure 4-9. 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 4.9.3.8. f. Repeat steps a. through e. for positions 2 and 3. 4-23

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