Section 1 Introduction; Pilot Guide - Honeywell EGPWS MK V Pilot's Manual

SECTION 1
Introduction
Why S
MART
TM
L
ANDING
functions?
Stabilized
Approach
Monitor
TM
Smart Landing
100
This Pilot Guide section describes the functions and
operation of
TM
S L
MART ANDING
version and equivalent and later.
The document is divided into the following sections:
• Section 1 – An introduction to the S
functions;
• Section 2 – A detailed description of the operation of
S
MART
• Section 3 – A summary of the options available to
operators to configure S
functions;
• Section 4 – Means for the flight crew to check the
operational availability of S
functions.
This guide does not supersede FAA approved data,
Flight Manuals, individual Operations Manuals,
requirements, or procedures. Pilots should be
thoroughly familiar with their own company policies,
system configuration, requirements, and procedures
with respect to the operation of aircraft with the
EGPWS and RAAS.
The information in this document is intended as a general
explanation of the Honeywell Monitor Functions. It contains
a description of system performance assuming the identified
options are active.
The intended function of the Monitor Functions is to
supplement the existing approved flight crew standard
operating procedures. Existing EGPWS protection and
operation is unaltered by the addition of the new non-TSO
Monitor Functions.
New Flight Safety Functions Hosted in EGPWS
• Stabilized Approach Monitor
• Altimeter Monitor
• Long Landing Monitor
The Stabilized Approach Monitor function offers a
significant safety advancement to supplement flight crew
awareness of unstabilized approaches as described below.
The Stabilized Approach Monitor uses the inputs described
below and the Honeywell EGPWS Terrain Database to
Mark V and Mark VII EGPWS Pilot's Guide
the MKV and
functions added in -230-230 software
TM
L functions;
ANDING
MKVII EGPWS
TM
L
MART ANDING
TM
L
MART ANDING
TM
L
MART ANDING
060-4241-000
Rev H, August 2011