Embraer 170 - Limitations (Load prior to 27.1)

AIRPLANE
FLIGHT
MANUAL
SUPPLEMENT 4
PRIMUS EPIC - FLIGHT
MANAGEMENT SYSTEM
ANAC APPROVED S4-05
REVISION 15 Code 01 Page 1
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
LIMITATIONS (LOAD PRIOR TO 27.1)
NOTE: All pages from code 01 of this supplement are applicable to
airplanes equipped with Load prior to 27.1.
The following limitations are applicable to the FMS:
GENERAL LIMITATIONS
- The Honeywell Flight Management System (FMS) Pilot's Operating
Manual, P/N A28-1146-179, or other approved manual must be
immediately available to the flight crew in the cockpit whenever
navigation is predicated on the use of the FMS. The software
version stated in the Pilot's Operating Manual or other approved
manual must match that displayed on the Multi Control Display Unit
(MCDU) NAV IDENT page.
- The Honeywell Primus Epic FMS Airplane Database configuration
must be the following:
- Version 170-C6 and on for EMBRAER 170 models.
- Version 175-C3 and on for EMBRAER 175 models.
M
INIMUM CONFIGURATION FOR RNP 0.3 AR APPROACH
OPERATIONS
- Primus EPIC load 21.4 and on.
- Single FMS version 7.03 and on – included in the Primus EPIC
software.
- VGP (VGP UNAVAILABLE scratchpad message not presented
on MCDU).
- 1 GPS.
- 1 IRU.
- 1 MCDU.
- 4 Display units.
- 1 TAT sensor.
- 2 RVSM Compliant Air Data Systems.
- 1 Flight Director.
- EGPWS.
- RNP AR compliant Navigation Database.