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TB 1152023720214
rejection. A link to supplemental visual information on the allowable pin/slot configurations is available on
the 1999 ASAM page of the Blackhawk web site: "http://www.uhpo.redstone.army.mil". If you are unable
to access the web page contact either the technical or logistical poc listed at para 16a/b.
(1) Expandable pins manufactured by Apex Manufacturing Co. Inc. (CAGE 2V343) can be inden-
tified by the serial number prefix "AP".
(2) Expandable pins manufactured by Monogram Aerospace (CAGE 98524) are indentified by
serial number prefix "C416" or may not have a prefix.
(3) Expandable pins manufactured by Avibank Manufacturing (CAGE 84526) have serial number
prefixes "D416" or "F416" or "AVK".
(4) Expandable pins manufactured by Shurlock (CAGE 97393) which are indentified by serial
number prefix "E416" or "SLFP" have a solid inner segment in the center of the pin which is as wide as an
outer segment.
c. Replacement of all 7010308107101 pins is mandatory within 30 flight hours/42 days, whichever
occurs first. When the replacement pin is received, remove the 101 pin, demil IAW TM 1150032823 and
install a new pin. Report results of inspection IAW paragraph 14d.
d. If the expandable pin (P/N 7010308107102/103) conforms, the inspection is complete. Reinstall
the pin IAW TM 1152023723 or TM 1152025023. Report results of inspection IAW paragraph 14d.
e. If the expandable pin does not conform to the required configuration, correct IAW paragraph 9.
9.
a. Replace discrepant pin immediately and dispose of discrepant pin IAW paragraph 10d.
b. Fax the special report of discrepant item IAW paragraph 14e to the AMCOM Utility Helicopter Sys-
tems Engineering, AMSAMAREICU, commercial (256) 3134923, DSN 8974923. Call the technical
point of contact in paragraph 16a to confirm receipt of fax.
(1) AMCOM engineering will complete the necessary engineering analysis and advise the logisti-
cal POC of the recommended disposition instructions. The logistical POC will contact the unit and provide
final disposition instructions.
(2) The logistical POC will contact the unit POC if additional information on prior spindle and main
rotor blade history is necessary to complete the evaluation of the discrepant part and its impact on attached
components.
c. If disposition instructions have not been received from the logistical POC within 10 flight hours of
replacement of pin, the aircraft must be grounded until receipt of disposition instructions. Units may choose
to replace the affected attaching components in order to return the aircraft to flyable status. In this event,
annotate records to reflect the removal and replacement of the main rotor spindle and main rotor blade where
the discrepant expandable pin was installed. Hold the removed components pending disposition instructions.
NOTE
There is no calendar restriction, therefore, if the aircraft flight time is properly manages, the
aircraft will remain in flyable status per DA Form 1352 until replacement parts are received.
d. Report results of inpsection IAW 14b.
10. Supply/Parts and Disposition.
a. Parts Required. Items cited below may be required to replace defective items.
NOMENCLATURE
PART NUMBER
NATIONAL STOCK NUMBER
Pin, Expanding Grip
7010308107102
5315013290707
Blade, Main Rotor
7015009100043
1615011061903
Rotary Head Spindle
7010208200069
1615014426926
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