Esterline CMA-9000 - SECTION 15 - RNP CAPABILITY

OPERATOR’S MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
SECTION 15 - RNP CAPABILITY
CONTENTS
Subject Page
OVERVIEW..............................................................................................................................................................15-1
FLIGHT TECHNICAL ERROR ...............................................................................................................................15-2
PERFORMANCE, MONITORING AND ALERTING.............................................................................................15-3
GPS NAVIGATION MODE .....................................................................................................................................15-3
A. ACCURACY ...........................................................................................................................................15-3
B. INTEGRITY.............................................................................................................................................15-3
C. CONTINUITY..........................................................................................................................................15-3
DME/DME NAVIGATION MODE ...........................................................................................................................15-4
A. ACCURACY ...........................................................................................................................................15-4
B. INTEGRITY.............................................................................................................................................15-4
C. CONTINUITY..........................................................................................................................................15-4
VOR/DME NAVIGATION MODE............................................................................................................................15-4
A. ACCURACY ...........................................................................................................................................15-4
B. INTEGRITY.............................................................................................................................................15-4
C. CONTINUITY..........................................................................................................................................15-4
INERTIAL NAVIGATION MODE............................................................................................................................15-5
A. ACCURACY ...........................................................................................................................................15-5
B. INTEGRITY.............................................................................................................................................15-5
C. CONTINUITY..........................................................................................................................................15-5
Page 15-i
August 17, 2010
DRAFT