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 aft hanger bearing support shall be removed in accordance with
the applicable technical manuals listed in Table 1-1.
Access. Access is through the tail rotor drive shaft fairing (Figure 1-4, Item R410).
Preparation of Part. The part shall be thoroughly cleaned. Refer to Preparation of Part or Area for NDI,
NDI Equipment Settings.
a. Make the following initial settings on the Eddy Current Inspection Unit, NORTEC-19e .
- 200 KHz
b. Refer to Eddy Current Method, paragraph 1.4.11. Set up on test block as follows:
Null probe on test block.
Adjust phase as required to obtain horizontal lift-off.
Move probe over all three notches in test block. Adjust gain to obtain a three block vertical signal when
probe is passed over 0.040-inch notch in test block. (See the standard instrument display shown in Figure 1-7.)
184.108.40.206 Inspection Procedure. Refer to Eddy Current Method, paragraph 1.4.11 and Figure 3-9.
Place probe on a good area in the inspection location and null. Adjust phase as required to obtain horizontal
Inspect the part.
Any signal similar to the notches in the test block is cause for rejection.
Either probe identified in paragraph 220.127.116.11 may be used depending primarily on the ease of accessibility
and user friendliness. If the probes are changed, steps 18.104.22.168 b. (1), (2), and (3) shall be repeated each
time a change is made.