Garmin SA01933LA-D Airplane Flight Manual Supplement

4 (1)
Garmin SA01933LA-D Airplane Flight Manual Supplement

LOG OF REVISIONS

 

 

Page

 

 

 

 

Rev. No.

No.

Date

Description

 

FAA Approved

A

All

11-20-07

Complete

 

Seyed-Youssef Hashemi___

 

 

 

 

Supplement

 

Mgr. Flt. Test Br., ANM-160L

Original

 

 

 

 

 

 

 

 

FAA, Los Angeles ACO

 

 

 

 

 

 

 

 

 

 

Transport Airplane Directorate

 

 

 

 

 

Date: Nov. 20, 2007

 

 

 

 

 

 

 

B

All

07/31/09

Added ‘-D’ to

 

 

 

 

 

 

STC number,

 

David G Armstrong

 

 

 

added LP

 

 

 

 

 

 

approach type

 

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

11/20/2014

Updated

 

See Page 1

 

 

 

document

 

 

 

 

 

 

revisions and

 

 

 

 

 

 

added Flight

 

 

 

 

 

 

Stream 210

 

 

 

 

11

 

Added note for

 

 

 

 

 

 

Flight Stream

 

 

 

 

 

 

210

 

 

 

 

13,14

 

Added sections

 

 

 

 

 

 

2.14 and 2.15

 

 

 

 

21

 

Updated GTN

 

 

 

 

 

 

Crossfill section

 

 

 

 

22

 

Added Section

 

 

 

 

 

 

7.3

 

 

 

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

1.1Garmin 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.

 

 

Photocell

 

 

 

 

 

 

 

 

 

for Auto-

 

Com Freq

 

Graphic Moving

 

Comm Freq

Dimming

 

 

Direct-To Key

 

 

Window

Map Display and

 

 

Nav Freq

Flip/Flop

 

 

 

 

 

Navigation Info

 

 

 

Window

 

 

 

 

 

 

 

 

 

 

 

 

 

Menu Key

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Power and Com

 

 

 

 

 

 

 

 

 

Clear Key

Volume/Squelch

 

 

 

 

 

 

 

 

 

Data

 

 

 

 

 

 

 

 

 

Enter Key

Cards

 

 

 

 

 

 

 

 

 

Nav Radio

 

 

 

 

 

 

 

 

 

Function and

 

 

 

 

 

 

 

 

 

Page Number

Volume

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Nav Radio

 

 

 

 

 

 

 

 

 

Large Knob

Flip/Flop

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Large Knob

 

 

 

 

 

 

 

 

 

Small Knob

Com/VLOC

 

 

 

 

 

 

 

 

 

(Cursor - Press

Freq (MHz)

 

 

 

 

 

 

 

 

 

to activate)

Small Knob

Phase, and

 

 

 

 

 

 

 

 

Com/VLOC

GPS Integrity

Mounting

 

CDI

OBS

Key

Procedure Key

Freq (kHz)

Annunciator

 

Key

 

 

 

 

 

 

 

Screw

 

Key

 

Message

 

 

 

 

 

 

 

 

 

Key

Navigation

Source: GPS,

VLOC, or

GPS-PTK

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

1.2GPS/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 B- RNAV/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

2.1Pilot’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

2.2Kinds 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

Loading...
+ 14 hidden pages