Figure 5-18. Engine Air I nlet V Band Clamp

TM-1-1520-265-23 H-60 Helicopter Series Manual
Page Navigation
255

TM 1-1520-265-23 5-30 Change 2 5.18.3.5 Inspection Procedure. Perform fluorescent penetrant inspection. Refer to Fluorescent Penetrant Method, paragraph 1.4.7 and Table 1-5. Inspect area of concern. See Figure 5-18. Figure 5-18. Engine Air I nlet “V” Band Clamp 5.18.3.6 Marking and Recording of Inspection Results. Mark and record the inspection results as required by paragraph 1.3. 5.18.4 Backup Method. None required. 5.18.5 System Securing. Clean the “V” band clamp to remove inspection media. Refer to Post Cleaning and Restoration of Part or Area After NDI, paragraph 1.4.16. The “V” band, if removed, requires installation in accordance with the applicable technical manuals listed in Table 1-1. 5.19 STARTER FLANGE (ET). 5.19.1 Description (Figure 5-1, Index No. 19). The air starter is located on the right upper side of the engine and is mounted to the engine accessory drive case. It uses compressed air from the APU to turn the engine. 5.19.2 Defects. This inspection is used to verify crack indications found visually on the starter flange. No cracks are allowed. 5.19.3 Primary Method. Eddy Current. 5.19.3.1 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

Privacy Statement
Press Release
Contact