AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV2-18
Ed 1, Rev. 1
Section 2 – Limitations
PBN (RNAV & RNP) OPERATIONAL ELIGIBILITY
Approved
21
PBN
(RNAV
&
RNP)
OPERATIONAL
ELIGIBILITY
21.1
GENERAL GNSS NAVIGATION EQUIPMENT APPROVALS
The GPS/GNSS receivers in the G1000 System are certified to TSO C129a
Class A1 and ETSO C129a Class A1 or TSO C145a and ETSO 2C145a.
The Garmin GNSS navigation system as installed in this airplane complies
with the requirements of AC 20-138A, JAA TGL-10 and AMCs 20-4A, 20-
27A and 20-28.
It‘s approved for navigation using GPS and SBAS (within the coverage of a Sat-
ellite Based Augmentation System complying with ICAO Annex 10) for IFR
en route, terminal area, precision and non-precision approach operations.
The G1000 System meets the requirements for GPS/GNSS as a Primary Means
of Navigation for Oceanic/Remote Operations (RNP-10) per AC 20-138C, FAA
Notice N8110.60, FAA Order 8400-12C and FAA Order 8700-1. Both
GPS/GNSS receivers are required to be operating and receiving usable sig-
nals except for routes requiring only one Long Range Navigation sensor.
In accordance to ICAO doc 9613 (Fouth Edition – 2013), the G1000 System
has been shown to be eligible for:
-
B-RNAV (RNAV-5) per AMC 20-4A.
-
RNAV1 / P-RNAV (RNP-1) Enroute and Terminal navigation per
JAA TGL-10 Rev.1.
-
RNP APCH LNAV/VNAV per EASA AMC 20-27. This does not in-
clude APV BARO-VNAV operation which is not cleared.
-
LPV with SBAS per EASA AMC 20-28.
provided that the G1000 is receiving usable navigation information from at
least one GPS receiver.
Summary of Contents for P2010
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