SERVICE BULLETIN NAVIGATION - GARMIN G1000 SYSTEM UPGRADES INCLUDING TERRAIN AWARENESS

Transcription

1 Beechcraft TITLE: NAVIGATION - GARMIN G1000 SYSTEM UPGRADES INCLUDING TERRAIN AWARENESS 1. Planning Information A. Effectivity This Service Bulletin only addresses Model G36 airplanes that were delivered with Airframe System Software version installed by Hawker Beechcraft Corporation in accordance with STC SA01725SE. (1) Airplanes (a) Model G36 Bonanza, Serials E-3805 through E-3817, E-3819 through E-3825, E-3827 through E-3834, E-3836 through E-3839, E-3841, E-3843 through E-3848, E-3850 through E-3854, E-3856, E-3858, E-3860 through E-3862, and E-3864 through E (b) Spares None. B. Reason This Service Bulletin is being issued to upgrade Airframe System Software version to version in the Model G36 Bonanza. This upgrade is being provided to prevent a possible LOAD FAIL message or potential issues with the display of the High Oil Pressure alert or Low Fuel Quantity alerts should Airframe System Software need to be reloaded. C. Description This Service Bulletin provides accomplishment instructions necessary for upgrade of the G1000 System software. The software updates the various sub-systems of the G1000 installation as well as the factory enabled TAWS-B functionality. No additional hardware is required. The export of these commodities, technology or software are subject to the U.S. Export Administration Regulations. Diversion contrary to U.S. law is prohibited. For guidance on export control requirements, contact the Commerce Department's Bureau of Export Administration at Hawker Beechcraft Corporation (HBC) issues Service Information for the benefit of owners and fixed base operators in the form of two classes of Service Bulletins. The first class, Mandatory Service Bulletins (red border) includes changes, inspection and modifications that could affect safety or crashworthiness. HBC also issues Service Bulletins with no red border which are designated as either recommended or optional in the compliance section within the bulletin. In the case of recommended Service Bulletins, HBC feels the changes, modifications, improvements or inspections will benefit the owner/operator and although highly recommended, Recommended Service Bulletins are not considered mandatory at the time of issuance. In the case of Optional Service Bulletins, compliance with the changes, modifications, improvements or inspections is at the owner/operator's discretion. Both classes are available on the web at and mailed to: (a) Owners of record on the FAA Aircraft Registration Branch List and the HBC Safety of Flight Information (SOFI) List. (b) Those having a publications subscription. Information on Safety of Flight Information (SOFI) or subscription can be obtained through the Hawker Beechcraft Corporation Technical Manual Distribution Center (TMDC). As Mandatory Service Bulletins and Service Bulletins are issued, the Service Bulletin Master Index will be updated and available online at Warranty will be allowed only when specifically defined in the Service Bulletin and in accordance with HBC Warranty Policy. Unless otherwise designated, HBC Mandatory Service Bulletins, Service Bulletins and HBC Kits are approved for installation on HBC airplanes in original or HBC modified configurations only. HBC Mandatory Service Bulletins, Service Bulletins and Kits may not be compatible with airplanes modified by STC installations or modifications other than HBC approved kits. 1 of 9

2 D. Compliance Hawker Beechcraft Corporation recommends that this Service Bulletin be accomplished at the next inspection. Compliance with the Service Bulletin accomplishes installation of FAA Supplemental Type Certificate (STC) SA01725SE in accordance with Garmin Master Data List 005-C , Revision K. E. Approval The engineering data contained in this Service Bulletin is FAA approved. This modification is classified Minor per FAA Order Prior to accomplishment, owners / operators of airplanes registered in countries other than the United States shall consult with their local Aviation Regulatory Authority. F. Manpower The following information is for planning purposes only: Estimated man-hours to verify existing software version: 0.5 hours. Estimated man-hours to update software: 4.0 hours. Suggested number of men: 1 man. The above is an estimate based on experienced, properly equipped personnel complying with this Service Bulletin. Occasionally, after work has started, conditions may be found that could result in additional manhours. G. Weight and Balance None. H. Electrical Load Data Not changed. I. Software Accomplishment Summary Airframe System Software is updated from Version to Version J. References STC SA01725SE. K. Publications Affected None. L. Interchangeability of Parts M. Warranty Credit Contact Garmin for warranty information. 2 of 9

3 2. Material Information A. Materials - Price and Availability Contact a Hawker Beechcraft Authorized Service Center for information. B. Industry Support C. Airplanes The following parts required for this modification may be ordered through Garmin: Part Number Description Quantity Per Airplane Software Loader Card 1 D. Spares E. Reidentified Parts None. F. Tooling - Price and Availability 3. Accomplishment Instructions A. Airplane Should any difficulty be encountered in accomplishing this Service Bulletin, contact Hawker Beechcraft Corporation at or Observe all Warnings and Cautions contained in the airplane manuals referenced in this Service Bulletin. Whenever any part of this system is dismantled, adjusted, repaired or renewed, detailed investigation must be made on completion to make sure that distortion, tools, rags or any other loose articles or foreign matter that could impede the free movement and safe operation of the system are not present, and that the systems and installations in the work area are clean. (1) VERIFY AIRFRAME SYSTEM SOFTWARE VERSION: (a) Connect a 28-VDC external power unit to the airplane in accordance with Section 24 of the Bonanza Series Maintenance Manual. (b) Start the system in normal mode by turning on the BAT 1, BAT 2 and AVIONICS switches. 3 of 9

4 (c) Look at the MFD power-up screen (refer to Figure 1) in the upper right corner. The number displayed is the AIRFRAME SYSTEM SOFTWARE VERSION, e.g. Raytheon A36/G36 System If any other AIRFRAME SYSTEM SOFTWARE VERSION is displayed, this Service Bulletin is not applicable. (2) LOAD AIRFRAME SYSTEM SOFTWARE AND CONFIGURATION: (a) If G1000 is powered, power it down and remove the P/N terrain and obstacle database cards from the lower card slots of the MFD and PFD, and set aside for later reinstallation. Load Software and Configure LRUs per Sections 1 and 2 of the Software Loading and Post Installation Checkout TAWS Installation P/N document, up to (and including) Step If the system software does not upload correctly (incomplete or cancelled status message), try to install the system software or upload the configuration for that step again. If still unable to complete successful load, contact Hawker Beechcraft Corporation Customer Support at or Do NOT cancel a software upload that is in progress. Let the system either successfully load or fail. Removing power in the middle of a software upload can cause damage that requires an LRU to be returned to Garmin. Screen illustrations included in these documents are for reference only. Make sure to refer to the approved file names, part numbers, versions, and the configuration settings in the tables if there are any differences between illustration and what shows on the PFD or MFD. At any time during the process, if an incorrect button is selected, only that section s steps need to be started again and not the entire process. (3) AIRFRAME SYSTEM SOFTWARE LOAD CONFIRMATION: (a) Go to the System Status page using the FMS knob. Activate the cursor and toggle to the LRU window. Refer to Figure 2. 4 of 9

5 (b) Highlight the following items in the LRU window, and verify that the software part number and version matches the Required LRUs and Software in Table 1. LRU SW OK LRU SW OK LRU SW OK GDC1 GIA1 GFC1 CERT Y M GSA P C GIA1 GDC1 FPGA GFC2 CERT GIA GSA P M GIA1 GDL69 GIA1 GSA PT C GIA1 GEA1 GIA1 GIA2 GSA PT M GIA1 GFC1 CERT GIA GMA1 GIA1 GSA R C GIA1 GFC1 CERT P C GMU1 GSA R M GIA1 GFC1 CERT P M GMU1 FPGA GSA Y C GIA1 GFC1 CERT PT C GPS1 GSA Y M GIA1 GFC1 CERT PT M GPS2 GTX1 GIA1 GFC1 CERT R C GRS1 GIA1 PFD1 GFC1 CERT R M GRS1 FPGA MFD1 GFC1 CERT Y C (c) Deactivate the cursor. (d) Remove the loader card from the PFD top slot and set aside. If any software versions and/or part numbers do not match those specified by the Additional Information in Table 1 of this document, or if the software is not successfully loaded, DO NOT continue with post-installation procedures. Troubleshoot and resolve the issue (refer to the Garmin G1000 System Maintenance Manual P/N ) before continuing. (4) ENABLE TAWS AND OTHER OPTIONAL SYSTEMS (If Installed): (a) Enable TAWS and other optional systems per Section 2.3 of the G1000 Software Loading and Post-Installation Checkout, P/N document. (b) Reinstall P/N terrain and obstacle database cards in the lower card slots of the PFD and the MFD. Both P/N database cards are required equipment for TAWS operation. (5) SYSTEM TESTING AND CHECKOUT: Validate Software Load, Configuration and Activated Systems per Section 3 of the P/N document. 5 of 9

6 (6) GFC 700 AUTOPILOT GROUND CHECKS: Verify the proper operation of the GFC 700 per Section 4 of the G1000 Software Loading and Post- Installation Checkout, P/N document. (7) Power down the airplane and disconnect the 28 VDC external power unit from the airplane. (8) Ensure all work areas are clean and clear of tools and miscellaneous items of equipment. (9) Remove and discard the existing Secure Digital (SD) Software Loader Card located in the storage pouch provided at the back of the airplane POH / AFM. Place the TAWS Unlock Card (if not accomplished previously) and the SD Software Loader Card P/N in the storage pouch provided at the back of the airplane POH / AFM. A copy of STC certificate SA01725SE and this Service Bulletin must be maintained as part of the permanent records for the modified airplane. The following table lists the documents necessary to operate and maintain the airplane. DESCRIPTION GARMIN PART NUMBER REVISION **G1000 TAWS A36 AFM Supplement Revision D or later XG1000 TAWS A36 Cockpit Reference Guide Revision A or later XG1000 Instructions for Continued Airworthiness, Raytheon A Revision B or later XG1000 TAWS A36 System Maintenance Manual Supplement Revision D or later G1000 Software Loading and Post Installation Checkout, TAWS Installation Beechcraft A36 / G Revision B or later X* Note: This installation is not complete until the noted AFM Supplement has been incorporated in the POH / AFM. (10) Return airplane to service. B. Spares C. Record of Compliance Upon completion of this Service Bulletin, make a maintenance record entry as follows: The Airframe System Software update for TAWS STC SA01725SE was performed in accordance with HBC Service Bulletin of 9

7 MFD Power-Up Screen Figure 1 7 of 9

8 System Status Page Figure 2 8 of 9

9 Current Software Loader Card part number: P/N contains software image 006-B [1] DESCRIPTION LRU PART NUMBER CODE LOADER PART NUMBER SOFTWARE PART NUMBER SOFTWARE VERSION GTX 33 MODE S TRANSPONDER B0172-XX 4.02 GEA 71 ENGINE AIRFRAME UNIT B GDC 74A AIR DATA COMPUTER B C GMU 44 MAGNETOMETER B C GDU 1040 DISPLAY UNIT, PFD B GDU 1043 DISPLAY UNIT, MFD B GIA 63 AVIONICS INTEGRATION UNIT NO GIA 63 AVIONICS INTEGRATION UNIT NO B D B0093-XX 006-D [2] 006-B D B0093-XX 006-D [2] GRS 77 ATTITUDE HEADING REFERENCE UNIT B C GMA 1347 AUDIO PANEL B GDL 69A DATA LINK B GSA 81 AUTOPILOT SERVO (QTY 4) B D [2] 2.02 A36 CONFIGURATION FILE [1] N/A 006-D [1] The configuration file part number and version number cannot be verified using the G1000 configuration mode. The last six digits of the software image part number are displayed in the upper right corner of the MFD adjacent to Raytheon A36/G36 System. This is displayed on initial power up, and this software image contains the software part numbers and versions shown in the above table. [2] FCS gains are loaded into each servo and each GIA 63. Required LRUs and Software Table 1 9 of 9