5.2 ENGINE OIL PUMP, FUEL CONTROL, AND ACCESSORY GEARBOX FLANGES (ET).
5.2.1 Description (Figure 5-1. Index No. 2). This inspection is to verify cracks found visually during an excessive G-force
load inspection. Items to be inspected are: (1) accessory gearbox flanges; (2) oil pump flanges; and (3) fuel control
5.2.2 Defects. Inspect all above flanges for cracks. No cracks are allowed.
5.2.3 Primary Method. Eddy Current.
Eddy Current Inspection Unit
Probe, straight, shielded surface, 100 KHz-500 KHz
Probe, right angle, shielded surface, 100 KHz-500 KHz, 901/2 inch drop
Reference Block, three-notched aluminum (0.008, 0.020, and 0.040 EDM notches)
184.108.40.206 Preparation of Helicopter. The helicopter shall be prepared for safe ground maintenance. If required, the
components shall be removed in accordance with the applicable technical manuals listed in Table 1-1.
220.127.116.11 Access. Access is through the engine upper and lower doors from the engine work platform.
See Figure 1-4 CH-47: 20, 21, and 22; MH-47: 18, 20, and 21.
18.104.22.168 Preparation of Part. The areas to be inspected shall be thoroughly cleaned. Refer to Preparation of Part or
NDI Equipment Settings.
a. Make the following initial settings on the Eddy Current Inspection Unit, NORTEC-19e .