Table 4. FINAL ACCEPTANCE TEST PROCEDURE (MEP 83-360A/D, NSN <a href="http://aircraftgroundsvc.tpub.com/58/01-144-1897.htm">1730-01-144-1897</a> & NSN <a href="http://aircraftgroundsvc.tpub.com/80/01-466-9371.htm">1730-01-466-9371</a>)

TB 1-1730-229-30-3

14. FINAL TEST SHEET.

Table 4. FINAL ACCEPTANCE TEST PROCEDURE (MEP 83-360A/D, NSN 1730-01-144-1897 & NSN

1730-01-466-9371)

1.0

INTRODUCTION

1.1

Test Objective

To demonstrate that an AGPU is physically and functionally operational and document end item

final inspection and acceptance by the Government.

1.2

Test Purpose

To determine that the RESET AGPU was properly repaired; that inherent safety devices are

correctly installed and operate as required; that the AC/DC electrical system is operational; and

that the unit will deliver electrical power, hydraulic, and pneumatics power as required.

1.3

Test Performance Sequence

The procedures included in the following Acceptance Test need not be accomplished in number

sequence except where the sequence is required for safety or operational purposes.

2.0

TEST REQUIREMENTS

2.1

Test Specimen

AGPU Model #: MEP-360A or D (circle one)

AGPU S/N:

Starting GTE Hour Meter:

Final GTE Hour Meter reading:

Starting Hydraulic Module Hour Meter:

Final Hydraulic Module Hour Meter reading:

2.1.1

83-360A/D AGPU unit complete with battery and service lines slaved

2.2

Test Equipment

a. DC load bank, adjustable, 100 and 350 Amps at 28 VDC

b. AC load bank, adjustable, 20 KW, 40 KW, 55 KW, and 70 KW

PNEUMATIC load test stand

d. Multi-meter, capable of measuring true RMS and amperage

e. 24 VDC battery load tester