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Honeywell
MK XXII EGPWS Installation Manual
CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C
SHEET
124
SECTION V – CERTIFICATION
5.1 Introduction
This section outlines the procedures required to obtain FAA approval for the MK XXII EGPWS
installation.
5.2 Certification Procedur e
5.2.1.1 Equipment Compatibi lity
Careful consideration must be paid to the electrical characteristics of existing equipment or
possible additions that will be interfaced to the MK XXII EGPWS, in order to ensure system
compatibility. Section III of this manual provides system-planning guidelines, and defines the
electrical characteristics of the EGPWS. The installing agency should contact Honeywell
Product Support (800-813-2099), for information regarding the compatibility of equipment
not listed in Section III or interface into any airframe not listed in Appendix E Table E 3.1.1.
Normal business hours are 8:00 AM to 5:00 PM Pacific Time, Monday through Friday.
5.2.2 Equipment Location
The EGPWS and associated indicators, annunciators, and switches should be clearly visible and
within easy reach of the pilot(s). Refer to Section II of this manual for complete installation
information.
5.2.3 FAA Requirements
The installing agency should contact a local FAA Inspector who will determine whether the
installation may be approved by Supplemental Type Certificate (STC) or by submitting FAA Form
337 with an applicable STC package.
5.2.4 Ground Test
Honeywell has developed a generic Installation Ground Test Procedure for the MK XXII EGPWS,
drawing number 060-4167-167.
5.2.5 Flight Manual Revisio n
Honeywell has developed a generic Rotorwing Flight Manual Supplement for the MK XXII
EGPWS, drawing number 060-4314-009.