"Prior to installing the special self-retaining bolt, depress the retaining pin and fill the bolt with corrosion
preventive compound (CPC), Item 128, Appendix D. Apply CPC through one ball hole (while working
the retaining pin) until excess is seen at the opposite ball hole. Rotate the bolt 180 degrees and repeat
procedure at the second hole. Spray CPC into the cotter pin hole. While working retaining pin, apply
CPC at the pin hole in the bolt head and into the hole at the threaded end of the bolt. Lightly wipe excess
CPC from the threads and the retaining ball area. Apply CPC Item 126, Appendix D, to the exterior
retaining ball area and threads.
a. DA PAM 738-751.
b. TM 1-1520-237-23-1/2/3/6.
d. TM 1-1520-250-23-1/2/3/5.
e. TM 1-1520-250-23P-2
TM 1-1520-237-23-9, Appendix D.
g. TM 1-1520-250-23-6, Appendix D.
h. TM 1-1520-237-MTF.
14. Recording and Reporting Requirements
(1) Reporting Compliance Suspense. Upon entering requirements of this TB on DA Form
2408-13-1 for all effected aircraft, Commanders will forward a priority message, datafax or E-Mail to Com-
mander, AMCOM, ATTN: AMSAM-SF-A (SOF Compliance Officer), Redstone Arsenal, AL 35898-5000,
IAW AR 95-1, NLT date specified in Paragraph 3. Datafax number is DSN 897-2111 or commercial (256)
313-2111. E-Mail address is "email@example.com". The report will cite the message and TB number,
date of entry in DA Form 2408-13-1, the aircraft mission design series and serial numbers of aircraft in numeri-
(2) Task/Inspection Reporting Suspense Date . Upon completion of inspection, Commanders
will forward a priority message to the Logistical Point of C ontact listed in para 16.b.. The report will cite this
message and TB number, date of inspection, aircraft serial number, aircraft hours, and results of the inspec-
tion. Inspect and report NLT dates specified in paragraph 2.
b. Wholesale Spare Parts/Assemblies. N/A
Retail Spare Parts/Assemblies. N/A
d. The following forms are applicable and are to be completed in accordance with DA Pam 738-751,
15 Mar 99.
ULLS-A users will use applicable "E" Forms.
(1) DA Form 2408-13, Aircraft Status Information Record.
(2) DA Form 2408-13-1, Aircraft Inspection and Maintenance Record.
(3) DA Form 2408-15, Historical Record for Aircraft.
15. Weight and Balance. N/A.