TB 1-1520-240-20-106
10. Supply/Parts and Disposition.
a. Parts Required. Either replace defective lag dampeners with P/N 114H6800-11 NSN
1650-01-371-2475 configuration or correct in accordance with paragraph 9B above using the following parts
only:
NOMENCLATURE
PART NUMBER
NATIONAL STOCK NUMBER
234RS202-2
Rod End Assembly
3120-01-313-9375
NAS1423-14
Nut, Jam
Washer, Rod End
145R2010-1
b. Requisitioning instructions. Requisition replacement parts using normal supply procedures. All req-
uisitions shall use project code (CC 57-59) "XFE", "X-RAY-FOXTROT-ECHO".
NOTE
Project code "XFE", "X-RAY-FOXTROT-ECHO'" is required to track and establish
a database of stock fund expenditures incurred by the field as a result of SOF actions.
c. Bulk and Consumable Materials. N/A
d. Disposition. Demilitarize/mutilate IAW TM 1-1500-328-23 any rod end assembly which was re-
moved lAW paragraph 8 above for failure to meet inspection criteria.
e. Disposition of Hazardous Material.
11. Special Tools and Fixture Required. N/A
12. Application.
a. Category of Maintenance. AVUM. Aircraft downtime will be charged to AVUM.
b. Estimated Time Required for Inspection of Aircraft.
(1) Total of 1 man-hour using 1 person.
(2) Total of 1 hour downtime for one end item.
c. Estimated Cost Impact to the Field.
TOTAL $
NOMENCLATURE
PART NUMBER/
QUANTITY
COST EACH
NATIONAL STOCK NUMBER
114H6800-11
Lag Dampener Assy
,334.60
6
,889.10
Rod End Assy
234RS202-2
$ 4,024.26
6
$ 670.71
3120-01-313-9375
NAS1423-14
Nut, Jam
21.18
$
6
3.53
S
145R2010-1
Washer, Rod End
265.38
$
6
$ 44.23
Total cost per aircraft = ,334.60 for Dampener Replacement
Total cost per aircraft = ,310.82 for Rod End Replacement
d. TB/MWOs to be Applied Prior to or Concurrently with this Inspection. N/A
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