(2) For RCCB Miswired inspection and correction.
(a) Total of 5.0 manhours using 2 persons.
(b) Total of 2.5 hours downtime for one end item.
c. Estimated Cost Impact of Stock Fund Items to the Field. Not Applicable
d. TB/MWOs to be Applied Prior To or Concurrently with This Inspection. Not applicable.
e. Publications Which Will Require Change as a Result of This Inspection. Not Applicable.
a. TM 55-1520-238-23, Aviation Unit and Intermediate Maintenance Manual for Ann y AH-64A Helicopter,
basic DTD 7 June 1988.
b. TM 55-1520-238-23P, Aviation Unit and Intermediate Maintenance Repair Parts and Special Tools List
AH-64A Helicopter DTD 18 March 91.
c. TM 55-1520-238-T-10, Aviation Unit and Intermediate Troubleshooting Manual for Army AH-64A Helicopter,
Wiring Diagram, DTD 5 Sep 90.
d. TB 1-1520-238-20-23, Prevention of Uncommanded Hellfire Launches on AH-64A Aircraft DTD 15 June 1991.
14. Recording and Reporting Requirements.
a. Reporting Compliance "Suspense Date (aircraft). Upon entering requirements of this technical bulletin on
DA Form 2408-13, forward a priority message, datafax or E-Mail to Commander, AVSCCM, ATTN: AMSAV-
XSOF (SOF Compliance Officer), per AR 95-3. DATAFAX number is DSN 693-2064 or commercial 314/263-
2064. E-mail address is "'AMSAVXSOF (AT SIGN) St-Louis-EMh3.Army.Mil". The report will cite this
technical bulletin, date of entry in DA Form 2408-13, the aircraft mission design series and serial numbers of aircraft
in numerical order.
b. Task/Inspection Reporting Suspense Date (aircraft). Upon completion of inspection, units finding Miswired
RCCBs will forward a Priority message to: Commander, AVSCOM, Attn: AMSAV-EIA. The report will cite this
message number, date of inspection, Aircraft serial number, Aircraft and Component hours and results of the inspec-
tion. Inspection and reports will be completed no later than 10 days after task/inspection suspense date.
c. Reporting Compliance Suspense Date (Spares). Not Applicable.
d. Task/Inspection Reporting Suspense Date (Spares). Not Applicable.
e. The following forms are applicable and are to be completed in accordance with DA PAM 738-751, 15 Jan 88.
(1) DA Form 2408-13, Aircraft Inspection and Maintenance Record.
(2) DA Form 2408-15, Historical Record for Aircraft.
15. Weight and Balance. Not applicable.
16. Points of Contact.
a. Technical point of contact for this TB is Mr. James Lamkins/Matt Benzek, AMSAV-EIA, DSN 693-1679 or
commercial, 314/263- 1679.