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Garmin G500 Instructions Manual

Summary of G500

  • Page 1

    18.03.2017 rosdol g500 upd.

  • Page 268: G500/g600 Pfd/mfd

    G500/g600 pfd/mfd system instructions for continued airworthiness as installed in _____________________________ (make and model airplane) reg. No.____________ s/n_______________ dwg. Number: 190-00601-00 rev. M garmin international, inc. 1200 e. 151 st street olathe, kansas 66062 usa record of revis...

  • Page 269

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page ii 1. Introduction ................................................................................................................... 1 1.1 purpose ...............................................................

  • Page 271

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 2 of 13 1.6 definitions the following terminology is used within this document: 1) ac: advisory circular 2) aco: aircraft certification office 3) adahrs: air data and attitude heading reference system 4) adc: ...

  • Page 272

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 3 of 13 2.2 description of alteration the garmin g500/g600 pfd/mfd system is a combination of garmin lrus designed to provide both a pfd and mfd in the primary field of view. The system consists of a gdu 620 d...

  • Page 273

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 4 of 13 via an “alerts” softkey at the lower right of the mfd. During normal system operation with all aircraft systems and avionics powered there should not be any red xs or system alerts on the gdu 620. To e...

  • Page 274

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 5 of 13 2.5 periodic maintenance instructions all g500/g600 system lrus are designed to detect internal failures. A thorough self-test is executed automatically upon application of power to the units, and buil...

  • Page 275

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 6 of 13 2.5.9 mid-continent instruments attitude indicator models 4300-4( ), or 4200-( ) with md420 if a mid-continent instruments attitude indicator is installed as part of the g500/g600 aml stc, the battery ...

  • Page 276

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 7 of 13 grs 77 – attitude, heading reference system (ahrs) 20 m Ω (to aircraft ground plane) 20 m Ω (to instrument panel) gmu 44 – magnetometer 20 m Ω (to aircraft ground plane) no bond check required since th...

  • Page 277

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 8 of 13 2.7 removal and replacement information if any g500/g600 lrus are removed and reinstalled, verify that the lru unit power-up self-test sequence is successfully completed and no failure messages are ann...

  • Page 278

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 9 of 13 aircraft with a gmu mounted in the wingtip of metallic aircraft with non-metallic wingtip covers must inspect the magnetometer installation in accordance with section 8.4.1 of the g500/g600 aml stc ins...

  • Page 279

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 10 of 13 the latest revision of this document will be available on the garmin website (www.Garmin.Com). A garmin service bulletin, describing ica revision, will be sent to dealers if revision is determined to ...

  • Page 280

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 11 of 13 3. Appendix a 3.1 system system installed g500 single dual g600 single dual 3.2 lru locations the following table describes the locations of the g500/g600 lrus: lru lru included in this installation? ...

  • Page 281

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 12 of 13 3.3 wire routing – single-engine the following diagram depicts the wire routing for the g500/g600 lrus throughout the aircraft structure for a single-engine aircraft:.

  • Page 282

    G500/g600 pfd/mfd system 190-00601-00 rev. M instructions for continued airworthiness page 13 of 13 3.4 wire routing – twin-engine the following diagram depicts the wire routing for the g500/g600 lrus throughout the aircraft structure for a twin-engine aircraft:.

  • Page 283

    Aquila at01 d-eavz at01-224.

  • Page 284

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 2 of 52 log of revisions rev page description faa approval a all complete supplement seyed-joussef hashemi manager flight test branch anm-160l faa, los angeles aco transport airplane directorate date: july 15, 2008.

  • Page 285

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 3 of 52 log of revisions rev page description faa approval b 7 added gad 43 to section 1.2 seyed-joussef hashemi manager flight test branch anm-160l faa, los angeles aco transport airplane directorate date: july 17, 2009 8 added sec...

  • Page 286

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 4 of 52 log of revisions rev page description faa approval c 16 added section 2.8. Robert grove oda stc unit administrator garmin international, inc oda-240087-ce date: september 15, 2009 d 11 12 16 remove requirement for standby ad...

  • Page 287

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 5 of 52 log of revisions rev page description faa approval e all changed gps/waas to gps/sbas. Corrected typographical errors. Robert grove oda stc unit administrator garmin international, inc oda-240087-ce date: january 28, 2011 7 ...

  • Page 288

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 6 of 52 log of revisions rev page description faa approval f all changed references to gns navigators to gps/sbas navigators. Robert grove oda stc unit administrator garmin international, inc oda-240087-ce date: april 01, 2011 10 in...

  • Page 289

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 7 of 52 log of revisions rev page description faa approval h all re-issue complete supplement. Michael warren oda stc unit administrator garmin international, inc oda-240087-ce date: october 25, 2012 revised information on system po...

  • Page 290

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 8 of 52 log of revisions rev page description faa approval j all re-issue complete supplement. Michael warren oda stc unit administrator garmin international, inc oda-240087-ce date: december 12, 2013 corrected navigation radio info...

  • Page 291

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 9 of 52 added check box for gad 43 function to section 4.6. Added description of gdu control capabilities for gwx weather radars to section 7.9. Edited information about obstacle and wire depiction to section 7.10..

  • Page 292

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 10 of 52 table of contents section 1. General ................................................................................. 12 1.1 g500/g600 p rimary f light / m ulti -f unction d isplay s ystem .. 12 1.2 s ystem p ower s ources...

  • Page 293

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 11 of 52 section 3. Emergency procedures .............................................. 28 3.1 e mergency p rocedures ................................................................. 28 3.2 a bnormal p rocedures ......................

  • Page 294

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 12 of 52 section 1. General 1.1 g500/g600 primary flight / multi-function display system the g500/g600 system consists of a primary flight display (pfd) and multi- function display (mfd) housed in a single garmin display unit (gdu),...

  • Page 295

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 13 of 52 1.2 system power sources the g500/g600 system depends on electrical power to function. The garmin display unit (gdu) and air data attitude and heading reference system (adahrs) (or separate ahrs and adc) are directly tied t...

  • Page 296

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 14 of 52 1.4 synthetic vision technology (svt) svt uses an internal terrain database and gps location to present the pilot with a synthetic view of the terrain in front of the aircraft. The purpose of the svt system is to assist the...

  • Page 297

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 15 of 52 flight path marker (fpm) ; an indication of the current lateral and vertical path of the aircraft. The fpm is always displayed when synthetic terrain is selected for display. Traffic ; a display on the pfd indicating the po...

  • Page 298

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 16 of 52 1.6 audio panel the g500/g600 system may be interfaced to the aircraft audio panel to provide aural alerting generated by the g500/g600 (required for taws-b installations). 1.7 traffic display the g500/g600 system can displ...

  • Page 299

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 17 of 52 1.11 high speed data bus interface some garmin equipment connected to the g500/g600 system utilizes the high speed data bus (hsdb) interface. Hsdb is similar to an ethernet bus and provides a high-speed interface between ga...

  • Page 300

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 18 of 52 1.12 single g500/g600 operational block diagram standby attitude standby airspeed standby altimeter magnetic compass equipment installed per this stc standby instruments [3] [4] pfd/mfd display gdu 620 [1] alternatively, th...

  • Page 301

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 19 of 52 1.13 dual g500/g600 operational block diagram e qu ip m en t i ns ta lle d pe r th is s t c t em pe ra tu re p ro be g t p 5 9 #1 p ilo t p f d /m f d d is pl ay g d u 6 20 c op ilo t p f d /m f d d is pl ay g d u 6 20 a ud...

  • Page 302

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 20 of 52 1.14 definitions the following terminology is used within this document: adahrs: air data attitude & heading reference system adc: air data computer adf: automatic direction finder ads-b: automatic dependent surveillance br...

  • Page 303

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 21 of 52 section 2. Limitations 2.1 cockpit reference & pilot’s guide the garmin g500/g600 cockpit reference guide p/n 190-00601-03, revision g or later appropriate revision must be immediately available to the flight crew. 2.2 syst...

  • Page 304

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 22 of 52 2.6 magnetic variation operational area ifr operations are prohibited in areas where the magnetic variation is greater than 99.9 degrees east or west. 2.7 navigation angle the gdu 620 navigation angle, which defines whether...

  • Page 305

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 23 of 52 2.10 aerobatic maneuvers do not conduct aerobatic maneuvers if uninterrupted attitude information is required on the pfd. 2.11 course pointer auto slewing the g500/g600 hsi will auto slew, i.E. Automatically rotate the gps ...

  • Page 306

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 24 of 52 and white and is depicted for advisory use only. Aircraft maneuvers and navigation must not be predicated upon the use of the terrain display. Terrain, obstacle, and wire information is advisory only and is not equivalent t...

  • Page 307

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 25 of 52 2.18 active weather radar radar is broadcasting energy while in weather or ground mapping modes. If the g500/g600 system is configured to control an airborne weather radar unit, observe all safety precautions, including: do...

  • Page 308

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 26 of 52 2.20 kinds of operations unless placarded as limited to vfr only operations, g500/g600 equipment installed in a certified aircraft is approved for day and night / vfr and ifr operations in accordance with 14 code of federal...

  • Page 309

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 27 of 52 2.23 electronic standby instrument power the independent power source for the electronic standby instrument(s) shall be verified to be operational before flight, or the electronic standby(s) must be considered inoperative. ...

  • Page 310

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 28 of 52 section 3. Emergency procedures 3.1 emergency procedures 3.1.1 pfd 1 failure pfd 1 failure is indicated by the loss of displayed information on the pfd, including blank, frozen, or unresponsive display. 1. Use standby fligh...

  • Page 311

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 29 of 52 3.1.4 air data computer (adc) failure air data computer failure is indicated by a red x and yellow text over the airspeed, altimeter, vertical speed, tas and oat displays. Some derived functions, such as true airspeed and w...

  • Page 312

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 30 of 52 3.1.7 loss of electrical power to 2-inch electric standby attitude indicator (flashing or steady amber stby text) (midcontinent 4200 series) when a 2-inch electric standby attitude indicator is installed, loss of primary el...

  • Page 313

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 31 of 52 3.1.8 taws warning red annunciator on pfd and aural “pull up”: 1. Disconnect autopilot. 2. Initiate maximum power climb at best angle of climb airspeed (v x ). After warning ceases: 3. Climb and maintain safe altitude. 4. A...

  • Page 314

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 32 of 52 3.2 abnormal procedures 3.2.1 heading failure heading failure is indicated by replacement of the digital heading display with amber “hdg” text and a red x. If valid gps ground track is available, it will automatically be di...

  • Page 315

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 33 of 52 3.2.2 gps data failure gps data failure may be indicated by any or all of following: loss of gps course deviation information on hsi amber “loi” text on the hsi amber “no gps position” text on the mfd moving map loss of way...

  • Page 316

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 34 of 52 3.2.5 electrical load shedding the following equipment is considered non-essential. If it becomes necessary to reduce electrical load (for example, during loss of generators or alternators), power to these units may be remo...

  • Page 317

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 35 of 52 3.3 warnings, cautions, and advisories the following tables show the color and significance of the warning, caution, and advisory messages which may appear on the g500/g600 displays. Note the g500/g600 cockpit reference gui...

  • Page 318

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 36 of 52 3.3.2 caution annunciations – yellow annunciation pilot action cause check attitude autopilot will automatically disconnect. Note: only appears with the installation of an optional gad 43 adapter fly the aircraft manually a...

  • Page 319

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 37 of 52 ter n/a, ter fail use vigilance, terrain depiction is no longer provided. Database errors or lack of required gps position. Taws n/a, taws fail use vigilance, terrain depiction and taws alerting is no longer provided. Datab...

  • Page 320

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 38 of 52 section 4. Normal procedures refer to the garmin g500/g600 pfd/mfd system cockpit reference guide p/n 190-00601-03 or g500/g600 pilot’s guide p/n 190-00601-02 for normal operating procedures. This includes all primary fligh...

  • Page 321

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 39 of 52 soft keys at the bottom of the display allow for some quick functions to be performed on each page. The soft keys operate by press and release. More detailed configuration is typically available by pressing the menu button,...

  • Page 322

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 40 of 52 4.6 autopilot operations with the g500/g600 system the g500/g600 system offers various integration capabilities dependent mainly upon the type of autopilot installed in a particular aircraft. The g500/g600 installation in t...

  • Page 323

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 41 of 52 gpss hdg (toggle switch) ap hdg datum gpss hdg (push-button) ap hdg datum 4.6.2 course / nav selection coupling to the autopilot when operating the autopilot in nav mode, the deviation information from the installed navigat...

  • Page 324

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 42 of 52 when gpss is selected on the pfd, gpss is annunciated in the lower left portion of the pfd. The gpss mode annunciation depends on the location of the nav status information, as shown below. Nav status style 1 nav status sty...

  • Page 325

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 43 of 52 4.6.6.2 collins autopilots to preselect and capture a selected altitude: 1. Select the desired altitude with the pfd selected altitude bug. 2. Select alt sel mode on the autopilot flight control panel. Caution changing the ...

  • Page 326

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 44 of 52 4.6.7 vertical speed bug coupling certain autopilots may be coupled to the pfd vertical speed bug for maintaining a selected vertical speed. Except as described in this section, refer to the autopilot afms and/or pilot’s gu...

  • Page 327

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 45 of 52 4.6.8 flight director display if autopilot flight director commands are interfaced to the g500/g600, they will be presented as a single cue flight director on the pfd. Control of the flight director is accomplished via the ...

  • Page 328

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 46 of 52 4.6.9 gad 43 operation the gad 43 adapter may provide attitude, heading, and barometric correction information from the g500/g600 system to the autopilot. The gad 43 can also be configured to provide synchro heading output ...

  • Page 329

    Afms, garmin g500/g600 system 190-00601-01 rev. L faa approved page 47 of 52 section 5. Performance no change. Section 6. Weight and balance see current weight and balance data..

  • Page 330

    Afms, garmin g500/g600 system 190-00601-01 rev. L page 48 of 52 section 7. System descriptions garmin also provides a detailed g500/g600 pilot’s guide p/n 190-00601-02. This reference material is not required to be on board the aircraft but does contain a more in depth description of all the functio...

  • Page 331

    Afms, garmin g500/g600 system 190-00601-01 rev. L page 49 of 52 directory information may be available from multiple sources and coverage areas. This database is updated on a 56-day cycle. 7.2 electric standby attitude gyro if an electric standby attitude gyro is installed, the gyro operates from th...

  • Page 332

    Afms, garmin g500/g600 system 190-00601-01 rev. L page 50 of 52 7.4 taws function [gdu 620 units with internal taws] in dual g600 installations, taws audio is only provided by the pilot side gdu. If the pilot side gdu taws becomes inoperative, the co-pilot side gdu taws visual annunciations may stil...

  • Page 333

    Afms, garmin g500/g600 system 190-00601-01 rev. L page 51 of 52 7.7 ads-b traffic system interface the g500/g600 system can be interfaced to sources of ads-b traffic. The nose of the ownship symbol on both the g500/g600 main map page and dedicated traffic page serves as the actual location of your a...

  • Page 334

    Afms, garmin g500/g600 system 190-00601-01 rev. L page 52 of 52 note turbulence detection does not detect all turbulence especially that which is occurring in clear air. The display of turbulence indicates the possibility of severe or greater turbulence, as defined in the aeronautical information ma...