Garmin 500W Series Supplemental Flight Manual Download Page 8

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 500W Series Navigation System 

 

 

 

190-00357-03 Rev. B 
Page 8 of 17 

 

 

Table 2 – Approved Terrain Database Cards 

Part Number 

Description 

010-10201-20 

Data Card, TAWS / Terrain, 128MB 

010-10201-21 

Data Card, TAWS / Terrain, 256MB 

 

2.5

 

Navigation 

No navigation is authorized north of 89° (degrees) north latitude or south of 
89° (degrees) south latitude.  
 

2.6

 

Approaches 

a)

 

During GPS approaches, the pilot must verify the 500W Series unit is 

operating in the approach mode. (LNAV, LNAV+V, L/VNAV, LP, or 
LPV) 

b)

 

When conducting approaches referenced to true North, the heading 

selection on the AUX pages must be adjusted to TRUE. 

c)

 

Accomplishment 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 530W VOR/LOC/GS receiver to fly approaches not 

approved for GPS requires VOR/LOC/GS navigation data to be present 
on the external indicator (i.e. proper CDI source selection). 

e)

 

For aircraft with remote source selection annunciation or remote GPS 

navigation annunciations installed, conducting IFR approaches is 
prohibited if the remote annunciation is found to be inoperative during 
pre-flight. (This limitation does not prohibit the conduct of an IFR 
approach if the required remote annunciation fails during flight.  The 
indications provided on the 500W Series unit display may be used as a 
backup). 

f)

 

Except in emergency conditions, IFR approaches are prohibited 

whenever any physical or visual obstruction (such as a throw-over yoke) 
restricts pilot view or access to the 500W Series unit or the affected CDI. 

 

Summary of Contents for 500W Series

Page 1: ......

Page 2: ......

Page 3: ...2 3 Navigation Database 7 2 4 Terrain Database 7 2 5 Navigation 8 2 6 Approaches 8 2 7 Autopilot Coupling 9 2 8 Terrain Display Units without TAWS 9 2 9 TAWS Function Units with TAWS 9 2 10 VNAV 10 2...

Page 4: ...dicated 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...

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

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 530W VOR LOC GS recei...

Page 9: ...s This limitation may be removed after an FAA Flight Test demonstration Contact Garmin International Tech Support for additional information 2 8 Terrain Display Units without TAWS Terrain refers to th...

Page 10: ...If an optional weather receiver is interfaced to the 500W Series unit the weather information displayed is limited to supplemental use only and may not be used in lieu of an official weather data sou...

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 500W Series unit will flag the lateral guidance and generate a system...

Page 13: ...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 Pilot...

Page 14: ...log deviation information If an HSI is used with GPSS engaged the pilot should rotate the course pointer as prompted on the 500W Series unit to prevent loss of situational awareness and to prevent the...

Page 15: ...d without a FLAG This installation interfaces to the autopilot in analog mode only To capture the vertical guidance the pilot may engage the autopilot in APR mode at any time when the GPS Glide Slope...

Page 16: ...ion 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 intended...

Page 17: ...SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for a Garmin 500W Series Navigation System 190 00357 03 Rev B Page 17 of 17 Section 5 PERFORMANCE No change Section 6 WEIGHT AND BALANCE See current weight and bal...

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