Quantcast Inspection Procedures. - TB-1-1520-237-20-2240003

 

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Summary of the Problem. - TB-1-1520-237-20-2240002
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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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Correction Procedures - TB-1-1520-237-20-2240004
TB 1--1520--237--20--224
NOMENCLATURE
PART NUMBER
NSN
Left Hand Relay Panel
70070--55073--059
5945--01--348--9730
70070--55073--060
5945--01--349--5270
70552--55073--061
5945--01--329--0762
70070--55145--041
5945--01--348--2399
70070--55145--042
5945--01--348--9731
70070--55145--043
5945--01--349--5271
70070--55145--044
5945--01--327--7699
70070--55171--041
5945--01--344--2312
70070--55171--042
5945--01--345--0813
70070--55171--043
5945--01--345--4038
70070--55171--044
5945--01--346--1943
Right Hand Relay Panel
70550--02102--045
5945--01--083--7880
70550--02102--047
5945--01--139--1126
70550--02102--049
5945--01--224--2864
70550--02102--051
5945--01--289--2696
70550--02102--056
5945--01--325--0624
70550--55172--041
5945--01--351--6019
70550--55172--042
5945--01--352--8628
70070--55172--043
5945--01--353--3090
70070--55232--041
5945--01--388--9028
70070--55232--042
5945--01--388--9030
70070--55232--043
5945--01--388--9029
8.
Inspection Procedures..
a. Inspect the DA Form 2408--5, Equipment Modification Record, to determine if MWO
1--1520--237--55--7 has been applied.
(1) If the MWO has not been applied, the inspection is complete.
(2) If the MWO has been applied, proceed to paragraph 8b.
(3) If the aircraft tail number is between 77--22720 through 82--23746, and it cannot be deter-
mined if the MWO has been applied contact the logistics POC in paragraph 16b.
b. Prepare the aircraft for inspection IAW TM 1--1520--237--23--5, para 9--4--2.1.1.
c.
Perform the following inspections:
(1) Locate the wire harnesses (P/N 70552--02109--065/--066), TM 1--1520--237--23P--3, dated
3 April 2000, Figure 152, Items 21 and 22. Inspect the wire harness for evidence of chafing or burn marks
on the wires. If no chaffing or burn marks are found proceed to paragraph 8c(4).
(2) Inspect the left and right hand relay panels for burn marks. If either panel has burn marks,
perform an operational check of the relay panel IAW TM 1--1520--237--23--5, para 9--2--20 and para 9--2--21.
(3) Inspect for any other damage to adjacent structure of hardware.
(4) Inspect for installation of required mounting plates (wire saddles), (P/N TC--92, NSN
5340--00--728--1389). Each wire harness has two mounting plates (wire saddles), one located at each end
of the wire harness as shown in TM 1--1520--237--23P--3, dated 3 April 2000, Figure 152, Item 7.
3

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