|
| |
Back
Primary Method. Eddy Current. | Up
TM-1-1520-265-23 H-60 Helicopter Series Manual | Next
BALANCE WEIGHT BRACKET (MT) |
TM 1-1520-265-23
2.9.3.6
Inspection Procedure. Refer to Eddy Current Method, paragraph 1.4.11 and Figure 2-9.
a.
Place probe on a good area in the inspection location and null. Adjust phase as required to obtain horizontal lift-
off.
b.
Inspect the part.
c.
Any signal similar to the notches in the test block are cause for rejection.
NOTE
Either probe identified in paragraph 2.9.3.1 may be used depending primarily on the ease of
accessibility and user friendliness. If the probes are changed, steps 2.9.3.5 b. (1), (2), and (3)
shall be repeated each time a change is made.
2.9.3.7
Marking and Recording of Inspection Results . Mark and record inspection results as required by
paragraph 1.3.
2.9.4 Backup Method. None required.
2.9.5 System Securing. The droop stop support ring nut, if removed, requires installation in accordance with the
applicable technical manuals listed in Table 1-1.
ARROWS INDICATE SCAN PATHS
Figure 2-9. Droop Stop Support Ring Nut
2-18
|
