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Inspection Procedures. - TB-1-1520-237-20-2240003
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TB-1-1520-237-20-224 RCS CSGLD-1-1860(R1) H-60A Aircraft Tail Numbers 77-22720 THROUGH 82-23746 Wire Harness Manual
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Application. - TB-1-1520-237-20-2240005
TB 1--1520--237--20--224
d. If any abnormalities are noted during the inspection IAW paragraph 8c, proceed to paragraph 9.
e. If there is no evidence of chafing or burning of the wire harness, no burning or abnormalities noted
during inspection of the relay panels, the required mounting plates (wire saddles) are installed, and no dam-
age is noted to adjacent structure or hardware, proceed to paragraph 9e.
9.
Correction Procedures.
a. If any evidence of chafing or burn marks are found during the inspection procedure IAW paragraph
8c(1), repair the damaged harness IAW TM 1--1520--204--23--4. Ensure that harnesses are secured using
all required P--clamps and mounting plates, as shown in TM 1--1520--237--23P--3, dated 3 April 2000, Figure
152.
b. If the left or right hand relay panel failed the operational check IAW paragraph 8c(2), replace the relay
panel.
c.  If there is damage to adjacent structure or hardware IAW the inspection in paragraph 8c(3), repair
or replace the damaged parts IAW TM 1--1520--237--23 and TM 1--1500--204--23--4.
d. If the inspection IAW paragraph 8c(4) reveals that one or both mounting plates (wire saddles) are
missing, install the mounting plates (P/N TC--92, NSN 5340--00--728--1389) as shown in TM
1--1520--237--23P--3, dated 3 April 2000, Figure 152.
e. Reinstall the right and left relay panels IAW TM 1--1520--237--23--5, paragraph 9--4--2.1.1 after
installing the relay panels
(1) Use a mirror to visually verify that there is a minimum of 0.25 inches clearance between the
subject wire harnesses and the tops of the relay panels.
(2) If any of the subject wires touch the top of either relay panel, or if there is less than 0.25 inches
clearance, remove the relay panels IAW TM 1--1520--237--23--5, paragraph 9--4--2.1.1 and make the neces-
sary adjustments to the wire harness mounting brackets and clamps to ensure that the potential for chafing
has been eliminated.
f.  When all damaged components have been repaired or replaced IAW paragraphs 9a through 9d, and
proper clearance between the wire harnesses and the relay panel has been visually verified IAW paragraph
9e, the Red Horizontal; Dash //--// entry may be cleared.
10. Supply/Parts and Disposition.
a. Parts required. Items cited in paragraph 7 may be required to replace defective items.
b. Requisitioning Instructions. Requisition replacement parts using normal supply procedures. All req-
uisitions shall use Project Code (CC57--59) "X03" (xray--zero--three).
NOTE
Project Code "X03" is required to track and establish a data base of stock fund expenditures
incurred by the field as a result of SOF actions.
c.
Bulk and Consumable Materials. N/A
NOMENCLATURE
PART NUMBER
NSN
Wire
MS22759/43--10--9
N/A
d. Disposition. Dispose of removed parts/components using normal supply procedures. All turn--in
documents must include Project Code (CC 57--59) "X03".
e. Disposition of Hazardous Material. IAW Environmental Protection Agency directives as implement-
ed by your servicing environment coordinator (AR 200--1).
11. Special Tools, Jigs and Fixtures Required. N/A.
4

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