Recording and Reporting Requirements. - TB-1-1520-237-20-1730005

TB 1-1520-237-20-173

13. References. TM 1-1520-237-23, Avim/Avum Maintenance Manual dated, 15 August 1994

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 MDS aircraft, forward a priority message, data fax or E-mail to commander, ATCOM, ATTN: AMSAT-R-X

(SOF COMPLIANCE OFFICER), per AR 95-3. Data fax number is DSN 693-2064 or commercial 314-263-2064. E-Mail

address is "amstrxs @EMH4.STL.ARMY.MIL". The report will cite this TB number, date of entry in DA Form 2408-13-1,

the aircraft mission design series and serial numbers of aircraft in numerical order.

b. Task/lnspection Reporting suspense (Aircraft). The following information is required, within 10 hours/14 days of

inspection, if a suspect tail rotor inboard retention plate is found: complete unit address, point contact with telephone and

fax number, aircraft tail number, the suspect tail rotor inboard retention plate was installed, tail rotor inboard retention

plate part number, tail rotor inboard retention plate serial number and time since new on tail rotor inboard retention plate.

This information can be mailed to: Commander, Utility Helicopters PMO, SFAE-AV-BH-L, ATTN: JOE HOOVER, 4300

Goodfellow Boulevard, St Louis, MO 63120-1798 or faxed to JOE HOOVER, DSN 693-1898, or commercial (314) 263-

1898, or E-Mailed to Hoover @PE03.STL.ARMY.MIL.

c. Reporting Compliance suspense Date (spares) within 5 days.

d. Task/Inspection reporting suspense date (spares). Upon completion of the inspection depot commanders and

others holding stock shall forward a priority message report of results of this inspection to Commander, Utility Helicopters

PMO SFAE-AV-BH-L, ATTN: JOE HOOVER, 4300 Goodfellow Boulevard, St Louis, MO 63120-1798 or faxed to JOE

HOOVER, DSN 693-1898, or commercial (314) 263-1898, or E-Mailed to Hoover @PE03.STL.ARMY.MIL. NLT 5 days

after receipt of this TB. The report shall include gearbox part number, gearbox,, serial number tail rotor inboard retention

plate part number, tail rotor inboard retention plate serial number and time since new of tail rotor inboard retention plate.

e. The following forms are applicable and are to be completed in accordance with DA PAM 738-751, 15 June 92:

(1) DA Form 2408-5-1, Equipment Modification Record (Tail Rotor Gearbox Assembly).

(2) DA Form 2408-13, Aircraft Status Information Record.

(3) DA Form 2408-13-1, Aircraft Inspection and Maintenance Record.

(4) DA Form 2408-15, Historical Record For Aircraft.

(5) DA Form 2408-16, Aircraft Component Historical Record.

(6) DA Form 2410, Component Removal and Repair/Overhaul Record. (If tail rotor inboard retention plate is

removed).

15. Weight and Balance. N/A

Index