Appendix C: Sample FAA Form 337
82005-IM-K
Sandel SN3500 Installation Manual
Page 9-1
9
Appendix C: Sample FAA Form 337
NOTICE
Weight and balance or operating limitation changes shall be entered in the appropriate
aircraft record. An alteration must be compatible with all previous alterations to assure
continued conformity with the applicable airworthiness requirements.
8.
Description
of
Work
Accomplished
(If more space is required, attach additional sheets. Identify with aircraft nationality
and registration mark and date work completed.)
A.
Installed
the
following equipment and components:
1.
Sandel
Avionics,
Inc., SN3500 Navigation Display
(or as appropriate)
, Part
Number SN3500-000
(or as appropriate)
2. Sandel Avionics LLC, Clamp Fixture 3ATI, Part Number 61062.
B. The Sandel Avionics SN3500 is interfaced to the following equipment:
1. Garmin International, GPS165, GPS Navigation Receiver (Approved for En
route, Terminal, and Non-precision Approach).
(or as appropriate)
2. AlliedSignal Electronics and Avionics, KX 165 Communications and
Navigation Receiver.
(or as appropriate)
3. AlliedSignal Electronics and Avionics, KX 155 Communications and
Navigation Receiver.
(or as appropriate)
4. AlliedSignal Electronics and Avionics, KRA 10A Radar Altimeter System.
(or
as appropriate)
5. AlliedSignal Electronics and Avionics, KR 22 Marker Receiver.
(or as
appropriate)
6. AlliedSignal Electronics and Avionics, KG 102A Directional Gyro.
(or as
appropriate)
7. AlliedSignal Electronics and Avionics, KMT 112 Magnetic Azimuth
Transmitter.
(or as appropriate)
(By example state the following functional interface properties)...
C. The SN3500 receives and processes GPS navigation information for digital and
waypoint display from the GPS165. These operations are considered
supplemental navigation.
Summary of Contents for SN3500
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