TM 1-1520-265-23Figure 4-34. Tail Landing Gear Wheel Assembly4.35. CARGO HOOK (MT).4.35.1. Description(Figure4-1.IndexNo.35). The 9,000 pound capacity cargo hook is in the cargo hook well beneaththe cabin floor.4.35.2. Defects. This inspection is to check for cracks in the trunnions, trunnion retaining bolts and nuts, load beam,plate edge, and bolt hole surface areas. No cracks are allowed.4.35.3. PrimaryMethod. Magnetic Particle.4.35.3.1. NDI Equipment and Materials. (Refer to Appendix B.)a.Magnetic Particle Inspection Probe/Yokeb.Magnetometerc.Black Lightd.Fluorescent Magnetic Particles, refer to Table 1-8e.Consumable Materials, refer to Table 1-8f.Aircraft Marking Pencil, refer to Table 1-8NOTEHand-held magnetic coil may be used. Refer to paragraph 1.4.8.1.2 and Figure 1-6.4-80
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