SUPPLEMENT 4
PRIMUS EPIC - FLIGHT
MANAGEMENT SYSTEM
AIRPLANE
F
LIGHT
S4-00 ANAC APPROVED
Page 2 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
GENERAL (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.
INTRODUCTION
This Supplement is a part of, and must be placed in, the FAA
Approved Airplane Flight Manual for airplanes incorporating the
Honeywell Primus Epic Flight Management System (FMS). The
information contained herein supplements the information of the basic
AFM. For limitations, procedures and performance information not
contained in this Supplement, refer to the basic AFM.
NAVIGATION OPERATIONAL APPROVALS
Honeywell Primus Epic FMS installation has been shown to meet the
requirements for the following operations:
− Required Navigation Performance (RNP) Operations
− The FMS has been demonstrated compliant with the
requirements of RTCA DO-283 - Minimum Operational
Performance Specification for Required Navigation
Performance, including the capability to fly precision arc
(RF) legs.
− The FMS has been demonstrated to provide a minimum
RNP level of RNP 0.3 NM when operated according to
the limitations and procedures described in this
supplement.
− The airplane meets the performance and functional
requirements of FAA AC 90-101 for RNP AR approach
operations requiring RNP not less than 0.30 for approach
and not less than 1.0 for missed approach, when
equipped with the Honeywell Primus Epic FMS and when
operated in compliance with the recommended Embraer
flight crew and operational procedures.
− The temperature compensation function complies with
RTCA/DO-236B, Appendix H.2.
NOTE: Appropriate operational approval must be obtained
prior to conducting specified RNP AR instrument
approach procedures.
Refer to the PERFORMANCE section of this supplement for
more details regarding RNP operations.
To Next Page
Loading...
