Garmin Software Version 0857.09- Manuals

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Page 4 - INFORMATION SUBJECT TO EXPORT CONTROL LAWS; CAUTION

Page B G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 INFORMATION SUBJECT TO EXPORT CONTROL LAWS This document may contain information which is subject to the Export Administration Regulations (“EAR”) issued by the United States Department of Commerce (15 CFR, Chapte...

Page 5 - TABLE OF CONTENTS

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page i 190-01180-02 Revision 3 TABLE OF CONTENTS PARAGRAPH PAGE 1 INTRODUCTION ................................................................................................................. 1-1 1.1 C ONTENT , S COPE , P URPOSE ...........

Page 6 - GTS

Page ii G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 7.1 TRANSPONDER T ESTING ................................................................................................. 7-1 7.2 GTS T RAFFIC S YSTEM .........................................................

Page 7 - LIST OF ILLUSTRATIONS; FIGURE; LIST OF TABLES; TABLE

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page iii 190-01180-02 Revision 3 LIST OF ILLUSTRATIONS FIGURE PAGE Figure 2.1. Display Unit .............................................................................................................. 2-1 Figure 2.2. Transponder ..............

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Page iv G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 This page intentionally left blank

Page 9 - INTRODUCTION; APPLICABILITY

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 1-1 190-01180-02 Revision 3 1 INTRODUCTION 1.1 CONTENT, SCOPE, PURPOSE This document provides Instructions for Continued Airworthiness (ICA) for the Garmin G1000 integrated avionics as installed in the Hawker Beechcraft G58 as modified und...

Page 10 - DEFINITIONS/ABBREVIATIONS

Page 1-2 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 1.3 DEFINITIONS/ABBREVIATIONS AFCS: Automatic Flight Control System CFR: Code of Federal Regulations DME: Distance Measuring Equipment VHF: Very High Frequency AC: Advisory Circular AFMS: Airplane Flight Manual ...

Page 11 - PUBLICATIONS

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 1-3 190-01180-02 Revision 3 1.4 PUBLICATIONS The following documents are required by this maintenance manual to perform maintenance. It is the responsibility of the owner / operator to ensure latest versions of these documents are used dur...

Page 12 - ICA REVISION AND DISTRIBUTION

Page 1-4 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 Generic installation manuals for individual Garmin LRUs are also available through the ‘Dealers Only’ section of the Garmin web site. 1.5 ICA REVISION AND DISTRIBUTION This document is required for maintaining t...

Page 13 - SYSTEM; EQUIPMENT DESCRIPTIONS

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 2-1 190-01180-02 Revision 3 2 SYSTEM DESCRIPTION 2.1 EQUIPMENT DESCRIPTIONS The following subparagraphs provide a brief description and picture of each Garmin LRU installed or replaced by this STC. For all other G1000/GFC 700 LRUs, refer t...

Page 14 - GTX 33 TRANSPONDER

Page 2-2 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 2.1.2 GTX 33 TRANSPONDER The Garmin GTX 33 transponder communicates with the on-side GIA 63W through RS-232 digital interface. This STC provides for the optional installation of a GTX 33ES transponder that provi...

Page 15 - GTS 820 TRAFFIC SYSTEM

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 2-3 190-01180-02 Revision 3 2.1.4 GTS 820 TRAFFIC SYSTEM The optional GTS 820 system is designed to use active interrogations of Mode S and Mode C transponders to provide Traffic Advisories (TA) to the pilot. Passive surveillance is availa...

Page 16 - Figure 2.6 G58 Traffic Antenna

Page 2-4 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 Figure 2.6 G58 Traffic Antenna 2.1.5 XM REMOTE CONTROL SYSTEM The optional XM remote control system consists of the GRT 10 transceiver and the GRC Remote Control. This system allows for remote control of the XM ...

Page 17 - Figure 2.8 GRC 10 Remote Control

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 2-5 190-01180-02 Revision 3 Figure 2.8 GRC 10 Remote Control 2.1.6 GIA 63W INTEGRATED AVIONICS UNIT (2) Two Garmin GIA 63W Integrated Avionics Units (IAUs) contain the VHF COM/NAV receivers, WAAS GPS receiver, Flight Director, and system i...

Page 18 - OPTIONAL FEATURES; Synthetic Vision and Pathways

Page 2-6 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 2.2 OPTIONAL FEATURES The following optional features are included with this STC. These features are enabled via individual Enable cards that are to be retained with the aircraft. • Synthetic Vision and Pathways...

Page 19 - SOFTKEYS; To change page groups:

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-1 190-01180-02 Revision 3 3 G1000 CONTROL & OPERATION All control and operation of G1000 equipment as normally used in flight occurs through the PFD, MFD, and GMA audio panel. 3.1.1 SOFTKEYS Some pages have commands or selections tha...

Page 20 - REVERSIONARY MODE

Page 3-2 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 Figure 3.2 - Normal Mode (with SVS enabled) Figure 3.3 - Normal Mode (without SVS enabled) 3.3 REVERSIONARY MODE Reversionary mode allows for display of information related to safe flight in the event of a displ...

Page 21 - CONFIGURATION MODE OVERVIEW; To start the system in Configuration Mode:; NOTE; System Page Group

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-3 190-01180-02 Revision 3 3.4 CONFIGURATION MODE OVERVIEW The Configuration Mode exists to provide the avionics technician with a means of configuring, checking, and calibrating various G1000 sub-systems. Troubleshooting and diagnostics ...

Page 24 - IMPORTANT; and click on the Dealer Resource Center link in the lower; Figure 3.7 – Dealer Login

Page 3-6 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 card by ordering the Garmin Part Number listed in the General Arrangement Drawing 005-00606-12 referenced in Table 1.1 IMPORTANT To satisfy the requirements of this STC it is critical that the technician install...

Page 25 - b. Click the Agree button on the confidentiality agreement page.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-7 190-01180-02 Revision 3 b. Click the Agree button on the confidentiality agreement page. c. Select the Download Software link. d. Select the Software Downloads hyperlink on the left hand edge of the page. e. Scroll down until the appro...

Page 26 - i. Ensure the card and correct drive letter is used, and click next.

Page 3-8 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 NOTE When the extraction begins, the program automatically deletes all current files on the SD card and copies the selected files to it, regardless of the file format on the SD card. Ensure files are not necessa...

Page 27 - Finish to finalize SD card.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-9 190-01180-02 Revision 3 j. Once successfully completed, the following message/window will pop-up. Click Finish to finalize SD card.

Page 28 - SOFTWARE FILES; reported software version.; CONFIGURATION FILE DESCRIPTIONS

Page 3-10 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 3.6.4 SOFTWARE FILES Software files are defined by part number and version number on the General Arrangement Drawing 005-00606-12. Each G1000 LRU reports the software version it currently contains to the user i...

Page 29 - G1000 SOFTWARE/CONFIGURATION PROCEDURE

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-11 190-01180-02 Revision 3 3.7 G1000 SOFTWARE/CONFIGURATION PROCEDURE This section summarizes the procedures required to load software and configuration files to the G1000. It is intended to work as a central guide for technicians to use...

Page 30 - MFD & PFD SOFTWARE LOAD

Page 3-12 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 3.7.1 MFD & PFD SOFTWARE LOAD IMPORTANT! When replacing a display, it is REQUIRED to update the system files with the new display in the MFD slot regardless of intended final configuration, PRIOR to loading...

Page 32 - BASE CONFIGURATION AND SOFTWARE UPLOAD; page using the PFD small FMS knob.; indicated by the following:

Page 3-14 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 3.7.2 BASE CONFIGURATION AND SOFTWARE UPLOAD a. Ensure loader card is inserted into top card slot of PFD. On PFD, select the System Upload page using the PFD small FMS knob. b. Activate the cursor and rotate th...

Page 33 - OPTIONAL EQUIPMENT CONFIGURATION; GTX 33 with extended squitter

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-15 190-01180-02 Revision 3 3.7.3 OPTIONAL EQUIPMENT CONFIGURATION Perform the following steps if any of the following options are installed: • GTS 820 • SKY 497 Skywatch • KN 63 DME • WX-500 Storm Scope • GTX 33 with extended squitter a....

Page 34 - a. Insert two AA batteries in GRC 10.

Page 3-16 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 3.7.4 GRC 10 CONFIGURATION (OPTIONAL) For installations with the optional GRT 10/GRC 10 wireless remote system, the GRC 10 must be configured to communicate with the specific GRT 10 that is installed in the air...

Page 35 - SOFTWARE LOAD CONFIRMATION; Verify the software and version levels for the items listed below.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-17 190-01180-02 Revision 3 3.8 SOFTWARE LOAD CONFIRMATION Go to the Systems Status page. Activate the cursor and toggle to the LRU window. Highlight each of the following items in the LRU window and verify that the LRU software part numb...

Page 36 - c. Remove loader card and power down aircraft.

Page 3-18 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 b. De-activate the cursor. c. Remove loader card and power down aircraft. IMPORTANT If any software version and/or part number does not match, or is not successfully loaded, do not continue with post installati...

Page 37 - AVIATION DATABASE LOADING PROCEDURES; c. This completes the installation of the Terrain Data Card.; AVIATION DATABASE LOADING; d. Press the MFD ENT key to confirm the database update.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-19 190-01180-02 Revision 3 3.9 AVIATION DATABASE LOADING PROCEDURES 3.9.1 TERRAIN DATA CARD LOADING PROCEDURE a. Remove power from the PFD and MFD by pulling the PFD and MFD circuit breakers. b. Install a GDU 10XX Terrain Data Base Card ...

Page 38 - Table 3.2 – SVS Enable Card; QTY; Synthetic Vision & Pathways Enable, 1 PFD

Page 3-20 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 3.10 SVS / PATHWAYS ACTIVATION (OPTION) This section provides the requirements and instructions necessary to enable the G1000 Synthetic Vision / Pathways feature. Baseline Software: The Garmin Synthetic Vision ...

Page 39 - SVS ACTIVATION PROCEDURE

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-21 190-01180-02 Revision 3 3.10.1 SVS ACTIVATION PROCEDURE Activate the SVS/Pathways feature by performing the following steps: a. Apply power to the G1000 system. b. Pull the MFD and PFD circuit breakers. c. A special SVS Enable card is...

Page 40 - CHARTVIEW ENABLE PROCEDURE; b. Pull the PFD and MFD circuit breakers.

Page 3-22 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 3.11 CHARTVIEW ENABLE PROCEDURE NOTE • The Chart Enable card can only enable Charts on one system (one aircraft). A new Chart Enable card must be used for each aircraft. • The required ChartView databases are s...

Page 41 - TAWS-B ENABLE PROCEDURE; appear in the upper left corner of the

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 3-23 190-01180-02 Revision 3 3.12 TAWS-B ENABLE PROCEDURE NOTE The TAWS-B Enable card can only enable TAWS on one system (one aircraft). A new TAWS Enable card must be used for each aircraft. a. Remove power from the MFD and PFD by pulling...

Page 42 - AIRCRAFT REGISTRATION NUMBER ENTRY; release the ENT key.; CLEARING DEFAULT USER SETTINGS; c. When prompted to clear user settings select the YES softkey.

Page 3-24 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 3.13 AIRCRAFT REGISTRATION NUMBER ENTRY NOTE The large FMS knob changes Groups and the small FMS knob changes Pages within a Group. NOTE If aircraft has a Garmin GTS 8XX Traffic System installed, ensure GTS 8XX...

Page 43 - INSTRUCTIONS FOR CONTINUED AIRWORTHINESS; AIRWORTHINESS LIMITATIONS; REQUIRED TOOLS; TIC TR 220 Test set or equivalent

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 4-1 190-01180-02 Revision 3 4 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 4.1 AIRWORTHINESS LIMITATIONS There are no airworthiness limitations associated with this type design change (STC # SA01584WI-D). The previously approved Instructions f...

Page 45 - MAINTENANCE INTERVALS; Item

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 4-3 190-01180-02 Revision 3 4.3 MAINTENANCE INTERVALS Table 4.1 below shows the systems and equipment installed by this STC that must undergo any maintenance action and identifies the timeframe in which that activity should occur. The prev...

Page 46 - VISUAL INSPECTION REQUIREMENTS

Page 4-4 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 Item Description / Procedure Section # Interval Battery replacement On Condition Synthethic Vision /Pathways Reactivation 3.10 On Condition / after GDU replacement GTX 33ES Tranponder with Extended Sqitter Funct...

Page 47 - ELECTRICAL BONDING TEST

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 4-5 190-01180-02 Revision 3 When making any repairs to GTS coax cables installed under this STC, be sure to adhere to all of the specifications and limitations such as minimum and maximum cable attenuation, attenuation balance between cabl...

Page 48 - Empennage; Ensure that at each test point, no more than 10 milli-volts (10 m

Page 4-6 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 • Metal case of GPA 65 LNA/PA: __________ milli-volts (part of GTS 820 option) Empennage • Metal case of GTS 820: __________ milli-volts (optional equipment) Aircraft Exterior (Antennas) • GA 58 Top traffic ante...

Page 49 - TROUBLESHOOTING; SVS/PATHWAYS TROUBLESHOOTING; AHRS; Table 5.1 – SVS Troubleshooting

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 5-1 190-01180-02 Revision 3 5 TROUBLESHOOTING This section provides instructions and guidance for system troubleshooting additional systems / functions added by this STC. For troubleshooting assistance for all other aspects of the G1000 / ...

Page 53 - BACKSHELL/BACKPLATE CONNECTORS

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 5-5 190-01180-02 Revision 3 Load AIRFRAME, SYSTEM, MFD, PFD and MANIFEST configuration files to MFD and PFD • SW Loader Card must be inserted in top slot of PFD. • PFD and MFD must be powered on. • PFD and MFD must have correct software. L...

Page 55 - EQUIPMENT REMOVAL & INSTALLATION; GTS 820 TAS PROCESSOR; Disconnect the three electrical connectors.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 6-1 190-01180-02 Revision 3 6 EQUIPMENT REMOVAL & INSTALLATION This section describes how to remove and replace equipment in the G58 that was installed as part of this STC. After removal and replacement, LRUs must be configured and tes...

Page 56 - Disconnect the electrical connector.; TAS ANTENNAS

Page 6-2 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 6.2 GPA 65 LNA/PA CAUTION After any maintenance or modification is made to the GTS 820 TAS cables such as replacing a connector or entire cable, some important considerations must be made. Be sure to adhere to a...

Page 57 - Disconnect the electrical connector.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 6-3 190-01180-02 Revision 3 6.4 GRT 10 XM REMOTE CONTROL TRANSCEIVER Removal: 1. Gain access to GRT 10 under glareshield on copilot side of cockpit. Refer to the “GRT 10 Equipment Install, Hawker Beechcraft G58” drawing listed in Table 1.1...

Page 60 - GTX 33ES TRANSPONDER REMOVAL & REPLACEMENT; Make sure all airplane electrical power is disconnected.; Push down on the GTX 33 handle to lock the unit into the rack.

Page 6-6 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 6.7 GTX 33ES TRANSPONDER REMOVAL & REPLACEMENT Removal: 1. Make sure all airplane electrical power is disconnected. 2. Remove the PFD. 3. Unlock the GTX 33 handle by loosening the Phillips screw on the handl...

Page 61 - GIA 63W REMOVAL & REPLACEMENT; Push down on the GIA 63W handle to lock the unit into the rack.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 6-7 190-01180-02 Revision 3 6.8 GIA 63W REMOVAL & REPLACEMENT Removal: 1. Make sure all airplane electrical power is disconnected. 2. Remove the MFD. 3. Unlock the GIA 63W handle by loosening the Phillips screw on the handle. 4. Pull t...

Page 62 - files must be loaded to the unit. See Section

Page 6-8 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 CAUTION 010-00725-08 Loader Card (006-B0857-08 Software Image) is only compatible with GIA P/N: 011-01105-01. All installations with GIA P/N: 011-01105-20 must use the 006-B0857-09 Software Image. 6. If a new, r...

Page 63 - EQUIPMENT; TRANSPONDER TESTING

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 7-1 190-01180-02 Revision 3 7 G1000 EQUIPMENT CONFIGURATION & TESTING Refer to Section 3.6 for information on loading software and configuration of G1000 equipment covered by this STC. 7.1 TRANSPONDER TESTING The integrated transponder...

Page 64 - Original GTS 820 Reinstalled; Set the intruder type as ATCRBS.

Page 7-2 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 Original GTS 820 Reinstalled No software or configuration loading is required if the removed GTS 820 is re-installed. This does not include units that were returned for repair as their software and configuration...

Page 67 - SYSTEM RETURN TO SERVICE PROCEDURE; DISPLAY TESTING

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 8-1 190-01180-02 Revision 3 8 SYSTEM RETURN TO SERVICE PROCEDURE The procedures contained in this section describe the minimum return to service checks that should be performed upon reinstallation of the software and/or reactivation of SVS...

Page 68 - Figure 8.2 – PFD Power Up System Annunciations

Page 8-2 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 Figure 8.2 – PFD Power Up System Annunciations e. In the normal operating mode, data fields that are invalid have large red Xs through them (Figure 8.2). A valid field does not display a red X (Figure 8.3). Allo...

Page 69 - h. Check that engine instrument fields are valid on the MFD.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 8-3 190-01180-02 Revision 3 Figure 8.4 – Normal Display (with SVS enabled) f. Check that all COM/NAV fields are valid in the top corners of PFD and MFD. g. Check that altitude, airspeed, vertical speed, TAS, OAT, and ISA fields are valid o...

Page 70 - SVS / PATHWAYS INSTALLATION VERIFICATION (REQUIRED IF ENABLED); configuration errors exist.; Figure 8.5 – PFD Display without SVS enabled

Page 8-4 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 8.1.1 SVS / PATHWAYS INSTALLATION VERIFICATION (REQUIRED IF ENABLED) a. Apply power to the G1000 system. Allow the AHRS and magnetometer systems to stabilize and align. Verify that air data information becomes v...

Page 71 - Figure 8.6 – PFD with SVS enabled; aircraft for future use.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 8-5 190-01180-02 Revision 3 Figure 8.6 – PFD with SVS enabled NOTE Screenshots are for reference only and may not be indicative of what is present on the actual aircraft display. f. Installation is complete. Be sure to keep the SVS / Pathw...

Page 72 - GIA 63W INTEGRATED AVIONICS UNIT; GPS Signal Acquisition; VHF COM Interference Test

Page 8-6 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 8.2 GIA 63W INTEGRATED AVIONICS UNIT GPS Signal Acquisition Figure 8-7 AUX – GPS STATUS Page (MFD) The GIA 63W units should normally acquire a GPS navigation solution within 5 to 10 minutes of startup, provided ...

Page 73 - h. Repeat steps d through g for each of the following frequencies:

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 8-7 190-01180-02 Revision 3 e. Transmit for a period of 35 seconds while monitoring GPS 1 signal strength levels. f. During the transmit period, verify that the GPS “INTEG” flag does not come into view on the PFD and verify that GPS 1 does...

Page 74 - deflection of the CDI while applying a 10° deviation signal.; GFC 700 AUTOPILOT GROUND CHECKS

Page 8-8 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 Check the VOR, ILS, and Glideslope functions with ramp test equipment. Operate the equipment according to the test equipment manufacturer’s instructions. Adjust the RF signal to a level adequate to perform the t...

Page 75 - AUTOPILOT PRE-FLIGHT TEST; ) annunciation will be displayed until both GIAs, the

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 8-9 190-01180-02 Revision 3 8.3.1 AUTOPILOT PRE-FLIGHT TEST NOTE The autopilot pre-flight test will run on every full autopilot power-on. a. Open the AP SERVOS circuit breaker and reset. The AFCS will re-initiate the pre- flight test. NOTE...

Page 76 - AFCS SWITCH CHECKS

Page 8-10 G1000 System Maintenance Manual - Hawker Beechcraft G58 Revision 3 190-01180-02 checked. If an alert is heard, the audio interface between GIA No. 2 and the audio panel should be checked. 8.3.2 AFCS SWITCH CHECKS To verify that the AFCS system buttons and switches are operating correctly, ...

Page 77 - MANUAL ELECTRIC TRIM SPEED CHECK

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 8-11 190-01180-02 Revision 3 q. Press the FD key on the MFD to deactivate the Go Around mode and reset the Flight Director. r. Center the trim wheel if it is not already centered. s. Press the AP key to engage the Autopilot. t. Press the C...

Page 79 - MAINTENANCE RECORDS; Record part and serial numbers of any LRU which was replaced.

G1000 System Maintenance Manual - Hawker Beechcraft G58 Page 8-13 190-01180-02 Revision 3 8.4 MAINTENANCE RECORDS After complying with the procedures contained in this ICA and any additional return to service procedures contained in the Hawker Beechcraft Maintenance Manual and G58 Maintenance Supple...