TB
1-1520-240-20-107
$
26.32
AN320-10
2
$
13.16
Nut, Plain
$
595.14
145R3650-1
2
$
297.57
Bolt
TOTAL COST PER AIRCRAFT =
For aircraft replacing all actuators. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .,066.15
For aircraft having end cap replacements... . . . . . . . . . . . . . . . . . . . . . .....,863.48
d.
TB/MWOs to be applied prior to or concurrently with this inspection - N/A.
e.
Publications which require change as a result of this inspection -
(1) TM 55-1520-240-23
(2) TM 1-1520-252-23
(3) TM 1-1520-252-PM
(4) TM 55-1520-240-PM
(5) TM 55-1520-240-PMD
(6) TM 1-1520-252-PMD
(7) Hydraulic Component DMWR' will be changed to reflect this TB. A copy of this TB
s
will be inserted in the appropriate publication as authority to implement the change until the printed
change is received.
13. References -
a. TM 55-1520-240-23P.
b. TM 1-1520-252-23P.
c. TM 55-1520-240-23.
d. TM 1-1520-252-23.
14. Recording and Reporting Requirements -
a. Reporting Compliance Suspense Date (Aircraft) - Upon entering requirements of this TB on DA Form
2408-13-1 on all subject Mission Design Series (MDS) aircraft, forward a priority message, Datafax or E-
Mail to Commander, AMCOM, ATTN: AMSAM-SF-A, (SOF Compliance Officer), Redstone Arsenal, AL
35898-5222, IAW AR 95-1. Datafax number is DSN 897-2111 or Commercial (256) 313-2111. E-Mail
address is safeadm@redstone.armv.mil. The report will cite this TB, date of entry in DA Form 2408-13-1,
the aircraft mission design series and serial numbers of aircraft in numerical order.
8
