
Airplane Flight Manual Supplement
II Morrow Inc. for II Morrow Apollo SL50/SL60
2345 Turner Rd SE March 17, 1997
Salem, OR 97302 Part #: 560-1006-00
FAA Approved
Date: MAR 31 1997 Page 5 of 16
1.1.2 SL60
The SL60 contains the SL50 functionality. In addition it contains airband VHF
communications and NOAA weather channel reception capability.
It contains all the interfaces for both the navigation and communications
functions. The Comm transceiver function and the GPS function are powered
through separate circuits. These are both through the aircraft circuit breaker panel
and the avionics master switches.
Figure 2 - Apollo SL60
1.2 O
PERATION
Provided the Apollo SL50 GPS/SL60 GPS-COMM is receiving adequate useable signals, it
has been demonstrated capable of and has been shown to meet the accuracy specifications
of:
a) VFR/IFR enroute oceanic and remote, enroute domestic, and terminal operation using
GPS within the U.S. National Airspace System and the North Atlantic Minimum
Navigation Performance Specification (MNPS) Airspace using the WGS-84 (or NAD 83)
coordinate reference datum in accordance with the criteria of AC 20-138, AC 91-49, and
AC 120-33.
b) The Apollo SL60 additionally provides VHF airband communications capability
meeting the requirements of AC 20-67b, Airborne VHF Communications Installations.
2. LIMITATIONS
1. User Manual
The information contained in the User’s Guide, Apollo SL50 GPS Receiver, Apollo SL60
GPS Receiver and VHF Comm Transceiver Manual, II Morrow P/N 560-0955-01 (or later
approved revision) must be immediately available to the flight crew whenever IFR
navigation and/or communication is predicated on the Apollo SL50 GPS/SL60 GPS-COMM
system.
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