Garmin SA01933LA-D Airplane Flight Manual Supplement
LOG OF REVISIONS
Page
Rev. No.
No.
Date
Description
FAA Approved
A
Original
All 11-20-07
Complete
Supplement
Seyed-Youssef Hashemi___
Mgr. Flt. Test Br., ANM-160L
FAA, Los Angeles ACO
Transport Airplane Directorate
Date: Nov. 20, 2007
B
All
07/31/09
Added ‘-D’ to
STC number,
added LP
approach type
David G Armstrong
ODA STC Unit Administrator
ODA-240087-CE
Garmin International, Inc.
C
All 03/21/13
Complete
Rewrite
Michael Warren
ODA STC Unit Administrator
ODA-240087-CE
Garmin International, Inc.
D
10, 14
01/27/14
Added LP +V
approach type
Michael Warren
ODA STC Unit Administrator
ODA-240087-CE
Garmin International, Inc.
E
8,9
11
13,14
21
22
11/20/2014
Updated
document
revisions and
added Flight
Stream 210
Added note for
Flight Stream
210
Added sections
2.14 and 2.15
Updated GTN
Crossfill section
Added Section
7.3
See Page 1
190-00356-03 Rev. E AFMS, Garmin GNS 4XXW GPS/SBAS System
Page 2 of 21 FAA APPROVED
Table of Contents
SECTION PAGE
Section 1. GENERAL 4
1.1 Garmin 4XXW Series GPS/WAAS Nav Com 4
1.2 GPS/SBAS TSO-C146a Class 3 Operation 5
Section 2. LIMITATIONS 7
2.1 Pilot’s Guide 7
2.2 Kinds of Operation 7
2.3 System Software 8
2.4 Navigation database 8
2.5 Flight Planning 9
2.6 Approaches 10
2.7 Autopilot Coupling 11
2.8 Terrain Proximity Function 11
2.9 VNAV – Vertical Navigation Calculation Page 12
2.10 Weather Display (Optional) 12
2.11 Traffic Display (Optional) 12
2.12 Manual GTN Crossfill 12
2.13 Flight Stream 210 (Optional) 12
Section 3. EMERGENCY PROCEDURES 14
3.1 Emergency Procedures 14
3.2 Abnormal Procedures 14
Section 4. NORMAL PROCEDURES 16
4.1 Unit Power On 16
4.2 Before Takeoff 16
4.3 HSI and EHSI Operation 17
4.4 Autopilot Operation 17
4.5 Coupling the Autopilot during approaches 18
4.6 Traffic Mode Selection (Optional) 19
Section 5. PERFORMANCE 19
Section 6. WEIGHT AND BALANCE 19
Section 7. SYSTEM DESCRIPTIONS 20
7.1 Pilot’s Guide 20
7.2 Manual GTN Crossfill 20
7.3 Flight Stream 210 20
AFMS, Garmin GNS 4XXW GPS/SBAS System 190-00356-03 Rev. E
FAA APPROVED Page 3 of 21
Section 1. GENERAL
OBS
Key
Power and Com
Volume/Squelch
Photocell
for AutoDimming
Graphic Moving
Map Display and
Navigation Info
Procedure Key
Range Keys
Enter Key
Direct-To Key
Menu Key
Function and
Page Number
Clear Key
Comm Freq
Flip/Flop
Nav Radio
Flip/Flop
Nav Radio
Volume
Small Knob
Com/VLOC
Freq (kHz)
Com Freq
Window
Small Knob
(Cursor - Press
to activate)
Large Knob
Data
Cards
Flight Plan
Key
Mounting
Screw
Message
Key
CDI
Key
Navigation
Source: GPS,
VLOC, or
GPS-PTK
Nav Freq
Window
Large Knob
Com/VLOC
Freq (MHz)
Terrain, Flight
Phase, and
GPS Integrity
Annunciator
1.1 Garmin 4XXW Series GPS/WAAS Nav Com
The Garmin GNS Series GPS/WAAS Navigator is a panel-mounted product that
contains a GPS/WAAS receiver for GPS approved primary navigation under
TSO-C146a, (plus optional VHF Com and VHF Nav radios) in an integrated
unit with a moving map and color display. The 4XXW Series unit features a
graphical display which may also be used to depict traffic, weather, or terrain
data.
The navigation functions are operated by dedicated keys and graphical menus
which are controlled by the buttons and the dual concentric rotary knob along
the bottom and right side of the display.
Optional VHF Com and VHF Nav radio functions are controlled via dedicated
buttons and knobs on the left side of the display and adjacent to frequencies they
are controlling.
Figure 1 - 430W Series Control and Display Layout
190-00356-03 Rev. E AFMS, Garmin GNS 4XXW GPS/SBAS System
Page 4 of 21 FAA APPROVED
1.2 GPS/SBAS TSO-C146a Class 3 Operation
The GNS complies with AC 20-138A and has airworthiness approval for
navigation using GPS and SBAS (within the coverage of a Satellite Based
Augmentation System complying with ICAO Annex 10) for IFR en route,
terminal area, and non-precision approach operations (including those
approaches titled “GPS”, “or GPS”, and “RNAV (GPS)” approaches). The
Garmin GNSS navigation system is composed of the GNS navigator and
antenna, and is approved for approach procedures with vertical guidance
including “LPV” and “LNAV/VNAV” and without vertical guidance including
“LP” and “LNAV,” within the U.S. National Airspace System.
The Garmin GNSS navigation system complies with the equipment
requirements of AC 90-105 and meets the equipment performance and
functional requirements to conduct RNP terminal departure and arrival
procedures and RNP approach procedures without RF (radius to fix) legs. Part
91 subpart K, 121, 125, 129, and 135 operators require operational approval
from the FAA.
The Garmin GNSS navigation system complies with the equipment
requirements of AC 90-100A for RNAV 2 and RNAV 1 operations. In
accordance with AC 90-100A, Part 91 operators (except subpart K) following
the aircraft and training guidance in AC 90-100A are authorized to fly RNAV 2
and RNAV 1 procedures. Part 91 subpart K, 121, 125, 129, and 135 operators
require operational approval from the FAA.
AFMS, Garmin GNS 4XXW GPS/SBAS System 190-00356-03 Rev. E
FAA APPROVED Page 5 of 21
Applicable to dual installations consisting of two Garmin
GNSS units: The Garmin GNSS navigation system has been
found to comply with the requirements for GPS Class II
oceanic and remote navigation (RNP-10) without time
limitations in accordance with AC 20-138A and FAA Order
8400.12A. The Garmin GNSS navigation system can be
used without reliance on other long-range navigation
systems. This does not constitute an operational approval.
The Garmin GNSS navigation system has been found to
comply with the navigation requirements for GPS Class II
oceanic and remote navigation (RNP-4) in accordance with
AC 20-138A and FAA Order 8400.33. The Garmin GNSS
navigation system can be used without reliance on other
long-range navigation systems. Additional equipment may
be required to obtain operational approval to utilize RNP-4
performance. This does not constitute an operational
approval.
The Garmin GNSS navigation system complies with the accuracy, integrity, and
continuity of function, and contains the minimum system functions required for
P-RNAV operations in accordance with JAA Administrative & Guidance
Material Section One: General Part 3: Temporary Guidance Leaflets, Leaflet No
10 (JAA TGL-10 Rev 1). The GNSS navigation system has one or more TSOC146a Class 3 approved Garmin GNS Navigation Systems. The Garmin GNSS
navigation system complies with the accuracy, integrity, and continuity of
function, and contains the minimum system functions required for B-RNAV
operations in accordance with EASA AMC 20-4. The Garmin GNSS navigation
system complies with the equipment requirements for P-RNAV and BRNAV/RNAV-5 operations in accordance with AC 90-96A CHG 1. This does
not constitute an operational approval.
Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in
accordance with AC 20-153 for database integrity, quality, and database
management practices for the navigation database. Flight crew and operators can
view the LOA status at FlyGarmin.com then select “Type 2 LOA Status.”
Navigation information is referenced to the WGS-84 reference system.
Note that for some types of aircraft operation and for operation in non-U.S.
airspace, separate operational approval(s) may be required in addition to
equipment installation and airworthiness approval.
190-00356-03 Rev. E AFMS, Garmin GNS 4XXW GPS/SBAS System
Page 6 of 21 FAA APPROVED
Section 2. LIMITATIONS
2.1 Pilot’s Guide
The Quick Reference Guide, part number and revision listed below (or later
applicable revisions), must be immediately available for the flight crew
whenever navigation is predicated on the use of the 4XXW Series unit.
400W Series Quick Reference Guide P/N 190-00356-01 Rev J
The Pilot’s Guide Addendum, part number and revision listed below (or later
applicable revision), must be immediately available for the flight crew whenever
one or more of the following units are installed and utilized with the 4XXW
Series unit:
GDL 69/69A XM Satellite Data link
GDL 88 ADS-B Transceiver
GTX 330/330D TIS
GTS 8XX Series TAS
Flight Stream 210
400W/500W Series Optional Displays P/N 190-00356-30 Rev L
The Pilot’s Guide Addendum, part number and revision listed below (or later
applicable revision), must be immediately available for the flight crew whenever
one or more of the following units are installed and utilized with the 4XXW
Series unit:
Stormscope® Lightning Detection System
Skywatch® Traffic Advisory System
Bendix/King® Traffic Advisory System
Avidyne/Ryan TCAD Traffic System
400W/500W Series Display Interfaces P/N 190-00356-31 Rev D
2.2 Kinds of Operation
This AFM supplement does not grant approval for IFR operations to aircraft
limited to VFR operations. Additional aircraft systems may be required for IFR
operational approval. Systems limited to VFR shall be placarded in close
proximity to the 4XXW Series unit: “GPS LIMITED TO VFR USE ONLY”.
AFMS, Garmin GNS 4XXW GPS/SBAS System 190-00356-03 Rev. E
FAA APPROVED Page 7 of 21
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