Introduction
Apollo SL40 Field Maintenance Manual
3
C
OMPONENT
H
ANDLING
The SL40 contains electrostatic discharge sensitive (ESDS) components. Care must be
taken when handling these devices to prevent damage. Special precautions for ESD work
areas are detailed in ESD Safe Work Area Requirements, Page 5. Both you and the work
surface must be properly grounded before handling the SL40 components. If moving the
SL40 components from one area to another, they must either be reinstalled in the SL40
case or placed in an anti-static bag.
S
HIPPING
C
ONSIDERATIONS
All SL40 components must be returned to the factory in anti-static packaging equivalent
to that used to ship the components from the factory. Save the packaging from the
replacement components to use when returning the failed component. Packaging
instructions are provided on Page 22. If you have questions regarding shipment of the
SL40 components, contact the II Morrow Service Department. Information on how to
contact the factory is provided on Page 22.
O
THER
T
OOLS AND
E
QUIPMENT
The following tools and test equipment (or equivalent) are required to properly evaluate
and test the SL40. All test equipment must be calibrated before performing the test
procedures in this manual.
T
OOLS
A 3/32” hex tool is required to remove the SL40 from the mounting frame in the aircraft.
A #2 Phillips screwdriver is required for disassembly
T
EST EQUIPMENT
a. Power Supply:
HP6433B DC Power Supply (0-36 V 0-10A) or equivalent
b. RF Signal Generator:
HP8920 RF Communications Test Set or equivalent
c. Multimeter
FLUKE 8010A Digital Multimeter or equivalent
d. Test interface
Refer to Figure 2 for the Test Interface schematic and SL 40 transceiver setup.
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