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GARMIN Ltd. or its subsidiaries 

c/o Garmin International 

1200 E. 151

st

 Street, Olathe, KS 66062 USA 

 

AIRPLANE FLIGHT MANUAL SUPPLEMENT 

or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL 

for a Garmin 400W Series Navigation System 

 

 

 

190-00356-03 Rev. B 
Page 13 of 16 

 

 

Section 4.

 

NORMAL PROCEDURES 

Refer to the 400W Series unit Pilot’s Guide defined in paragraph 2.1 on page 
6 of this document for normal operating procedures.   This includes all GPS 
operations, VHF COM and NAV, and Multi-Function Display information.  
For information on TIS traffic, or data linked weather see the Pilot’s Guide 
addendum for optional displays.  For information on active traffic sensor or 
Stormscope operation and displays see the Pilot’s Guide addendum for 
display interfaces. 

 

Although intuitive and user friendly the 400W Series unit requires a 
reasonable degree of familiarity to prevent operations without becoming too 
engrossed at the expense of basic instrument flying in IMC and basic see-
and-avoid in VMC. Pilot workload will be higher for pilots with limited 
familiarity in using the unit in an IFR environment, particularly without the 
autopilot engaged. Garmin provides excellent training tools with the Pilot’s 
Guide and PC based simulator.  Pilots should take full advantage of these 
training tools to enhance system familiarization. Use of an autopilot is 
strongly encouraged when using the 400W Series unit in IMC conditions 

 

4.1

 

Approaches with Vertical Guidance 

The 400W Series unit supports three types of GPS approaches with vertical 
guidance: LPV approaches, LNAV/VNAV (annunciated as L/VNAV) 
approaches, and LNAV approaches with advisory vertical guidance 
(annunciated as LNAV+V). For LNAV approaches with advisory vertical 
guidance, the 400W Series will annunciate LNAV+V indicating vertical 
guidance is available. LNAV minimums will be controlling in this case.  

 

NOTE: 

If flying an LPV or LNAV/VNAV approach, be prepared to fly 
the LNAV only approach prior to reaching the final approach fix 
(FAF).  If the GPS integrity is not within vertical approach 
limits, the system will flag the vertical guidance. This may be 
annunciated by a downgrade to LNAV message.  

 

For additional information on approaches with vertical guidance refer to the 
400W Series unit Pilot’s Guide. 

Summary of Contents for 400W Series

Page 1: ......

Page 2: ......

Page 3: ...avigation Database 7 2 4 Terrain Database 7 2 5 Navigation 8 2 6 Approaches 8 2 7 Autopilot Coupling 9 2 8 Terrain Display 9 2 9 VNAV 9 2 10 Weather Display 9 2 11 Traffic Display 10 Section 3 EMERGEN...

Page 4: ...ted 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 con...

Page 5: ...anic and remote airspace when used in conjunction with WAAS Garmin Prediction Program part number 006 A0154 03 Oceanic operations are supported when the 400W Series unit annunciates OCN This provides...

Page 6: ...B 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...

Page 7: ...ent approaches must be accomplished in accordance with an approved instrument approach procedure that is loaded from the 400W Series unit database c Installations with dual 400W 500W Series units will...

Page 8: ...plishment of an ILS LOC LOC BC LDA SDF MLS VOR approach or any other type of approach not approved for GPS overlay is not authorized with GPS navigation guidance d Use of the GNS 430W VOR LOC GS recei...

Page 9: ...units The GS of an ILS VLOC may be coupled to the autopilot without any limitations This limitation may be removed after an FAA Flight Test demonstration Contact Garmin International Tech Support for...

Page 10: ...e only and may not be used in lieu of an official weather data source 2 11 Traffic Display Traffic may be displayed on the 400W Series unit when connected to an approved optional TCAS TAS or TIS traff...

Page 11: ...modes do not support DR b If a Loss of Integrity INTEG message is displayed during y Enroute Terminal continue to navigate using GPS equipment and periodically cross check the GPS guidance to other ap...

Page 12: ...ans of navigation should be utilized e During any GPS approach in which precision and non precision alarm limits are exceeded the 400W Series unit will flag the lateral guidance and generate a system...

Page 13: ...h limited familiarity in using the unit in an IFR environment particularly without the autopilot engaged Garmin provides excellent training tools with the Pilot s Guide and PC based simulator Pilots s...

Page 14: ...log deviation information If an HSI is used with GPSS engaged the pilot should rotate the course pointer as prompted on the 400W Series unit to prevent loss of situational awareness and to prevent the...

Page 15: ...pts the pilot and requires the pilot to enable the A P outputs just prior to engaging the autopilot in APR mode This installation supports a seamless transition from digital GPSS to analog guidance fo...

Page 16: ...tection and Exclusion WFDE Prediction Program is required for Remote Oceanic operations The Prediction Program should be used in conjunction with the Garmin 400W 500W Simulator After entering the inte...

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