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Garmin GNS 530 User Manual

Garmin GNS 530
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DA 40 AFM
Supplement A21
GNS 530
Doc. # 6.01.01-E Rev. 0 01 Dec 2001 Page 9 - A21 - 5
1. GENERAL
This Supplement supplies the information necessary for the efficient operation of the
airplane when the COM/NAV/GPS GNS 530 is installed. The information contained
within this Supplement is to be used in conjunction with the complete AFM.
This Supplement is a permanent part of this AFM and must remain in this AFM at all
times when the GNS 530 is installed.
Refer to Section 7.14 for approved modes of operation (i. e. BRNAV, MNPS) of the
GNS 530´s GPS receiver.
2. LIMITATIONS
A. The GNS 530 Pilot's Guide, dated April 2000 or later appropriate revision must
be immediately available to the flight crew whenever navigation is predicated on
the use of the system.
B. The GNS 530 must utilize the following or later approved software versions:
Sub-System Software Version
Main 2.00
GPS 2.00
COMM 1.22
VOR/LOC 1.25
G/S 2.00

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Garmin GNS 530 Specifications

General IconGeneral
Power Supply14/28 VDC
Operating Temperature-20°C to +55°C
Display TypeLCD
Screen Size5 inches
GPS Receiver12-channel
Dimensions6.25 inches
InterfacesRS-232

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