a. Remove and replace any unserviceable 114R3650-13 or 114R3650-15 bolt with a 114R3650-16 or
114R3650-17 bolt, respectively, from the supply system.
(1) H--47D Aircraft - Refer to TM 55-1520-240-23-4, Task 5-94.1 (Replace Pitch Link Bolts).
(2) MH-47E Aircraft - Refer to TM 1-1520-252-23-5, Task 5-140 (Replace Pitch Link Bolts).
b. After completion of the above correction procedure, the red horizontal dash // --// status symbol entry
will be cleared and compliance with CH-47-01-ASAM-07 (TB 1-1520-240-20-135) will be entered on the DA
10. Supply/Parts and Disposition
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 (CC 57-59) "X0P", (X-RAY-ZERO-PAPA).
Project code "X0P", is required to track and establish a data base of
stock fund expenditures incurred by the field as a result of SOF actions.
Bulk and Consumable Materials - N/A.
d. Disposition - Demilitarize/mutilate in accordance with TM 1-1500-328-23 any bolt assembly which
does not meet inspection criteria.
Disposition of Hazardous Material - N/A.
11. Special Tools and Fixtures Required. N/A.
a. Category of Maintenance - AVUM. Aircraft downtime will be charged to AVUM. Report aircraft non--
mission capable maintenance (NMCM) while undergoing inspection and correction in accordance with this
Estimated Time Required-
(1) Inspection only --
(a) Total of 2 man--hours using 1 person.
(b) Total of 0 hours downtime for one end item
(2) Replacement --
(a) Total of 12 man--hours using 3 persons.
(b) Total of 4 hours downtime for one end item.
Estimated Cost Impact to the Field.
TOTAL COST PER AIRCRAFT = ,610.72
TB/MWOs to be Applied Prior to or Concurrently with this Inspection - N/A.