Garmin Software Version 0857.09 Airplane Flight Manual Supplement
Contents
1. approach operations including those approaches titled GPS or GPS and RNAV GPS approaches The G1000 Integrated Avionics GNSS navigation system installed in this aircraft is approved for approach procedures with vertical guidance including LPV and LNAV VNAV within the U S National Airspace System The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with the equipment requirements of AC 90 105 and meets the equipment performance and functional requirements to conduct RNP terminal departure and arrival procedures and RNP approach procedures without RF radius to fix legs Part 91 subpart K 121 125 129 and 135 operators require operational approval from the FAA HAWKER BEECHCRAFT 190 01 180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 4 of 13 Garmin 81000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with the equipment requirements of AC 90 100A for RNAV 2 and RNAV 1 operations In accordance with AC 90 100A Part 91 operators except subpart K following the aircraft and training guidance in AC 90 100A are authorized to fly RNAV 2 and RNAV 1 procedures Part 91 subpart K 121 125 129 and 135 operators require operational approval from the FAA The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft has been found to comply with the requirements for primary means o2. Page 3 of 13 SECTION 1 GENERAL This document is to be attached to the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Part Number 58 590000 67 when the airplane is equipped with the Garmin G1000 Airframe System Software Version 0857 08 or 0857 09 The information in this supplement supersedes or adds to the basic Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only as set forth within this document Users of the handbook are advised to always refer to the supplement for possibly superseding information and placarding applicable to the operation of the airplane G1000 GNSS GPS SBAS Navigation system Equipment approvals The Garmin G1000 Integrated Avionics GNSS navigation system installed in this aircraft is a GPS system with a Satellite Based Augmentation System SBAS comprised of two TSO C145a Class 3 approved Garmin GIA 63Ws TSO C146a Class 3 approved Garmin GDU 104X Display Units GARMIN GA36 and GA37 antennas and GPS software version 3 2 or later approved version The G1000 GNSS navigation system in this aircraft is installed in accordance with AC 20 138A The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with the requirements of AC 20 138A and is approved for navigation using GPS and SBAS within the coverage of a Satellite Based Augmentation System complying with ICAO Annex 10 for IFR en route terminal area
3. 84 or equivalent Do not use SafeTaxi or Chartview functions as the basis for ground maneuvering SafeTaxi and Chartview functions do not comply with the requirements of AC 20 159 and are not qualified to be used as an airport moving map display AMMD SafeTaxi and Chartview are to be used by the flight crew to orient themselves on the airport surface to improve pilot situational awareness during ground operations TIS AND GTS 820 TAS SYSTEMS Use of the MAP TRAFFIC MAP to maneuver the airplane for traffic avoidance without outside visual reference is prohibited The Traffic Information System TIS and GTS820 TAS systems are intended as an aid for the pilot to visually locate traffic It is the responsibility of the pilot to see and maneuver the airplane to avoid other traffic SYNTHETIC VISION HAWKER BEECHCRAFT 190 01 180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 10 of 13 Use of the Synthetic Vision system display elements alone for aircraft control without reference to the G1000 primary flight instruments or the aircraft standby instruments is prohibited Use of the Synthetic Vision system alone for navigation or obstacle or terrain avoidance is prohibited Use of the Synthetic Vision system traffic display alone to avoid other aircraft is prohibited HAWKER BEECHCRAFT 190 01 180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 11 of 13 SECTION 3 EMERGENCY PROCEDURES No Change SECTION ABNORMAL PROCE
4. AV operations in accordance with AC 90 96A and JAA TGL 10 Rev 1 This does not constitute an operational approval Garmin International holds an FAA Type 2 Letter of Acceptance LOA in accordance with AC 20 153 for database Integrity quality and database management practices for the Navigation database HAWKER BEECHCRAFT 190 01180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 5 of 13 Pilots and operators can view the LOA status at www Garmin com gt Aviation Databases gt Type 2 LOA Status Navigation information is referenced to WGS 84 reference system HAWKER BEECHCRAFT 190 01 180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 6 of 13 SECTION 2 LIMITATIONS AVIONICS When in flight the appropriate Garmin G1000 Cockpit Reference Guide for the Beechcraft Bonanza G58 must be immediately available to the flight crew AIRFRAME SYSTEM COCKPIT REFERENCE GUIDE SOFTWARE VERSION P N 0857 08 190 00526 02 Revision A or Later 0857 09 190 00526 03 Revision A or Later G1000 GNSS GPS SBAS NAVIGATION SYSTEM LIMITATIONS The pilot must confirm at system initialization that the Navigation database is current Navigation database is expected to be current for the duration of the flight If the AIRAC cycle will change during flight the pilot must ensure the accuracy of navigation data including suitability of navigation facilities used to define the routes and procedures for flight If an amended chart affe
5. DURES SVS Displays information inconsistent with G1000 primary flight instrumentation On the PFD PONE Use G1000 primary displays for navigation and aircraft control G1000 operation in display backup mode is required Select display backup mode on the G1000 system NOTE When display backup mode is selected the MFD will initially present a non SVS blue sky over solid brown ground display SVS will be presented on the backup display within 20 seconds if it was enabled on the PFD when display backup was selected SECTION 4 NORMAL PROCEDURES For normal operating procedures refer to the appropriate Cockpit Reference Guide the Baron G58 AFM 58 590000 67 or the Garmin G1000 Pilots Guide for the Beechcraft G58 190 00629 03 Rev A or later SECTION 5 PERFORMANCE No Change SECTION 6 WEIGHT AND BALANCE EQUIPMENT LIST No Change HAWKER BEECHCRAFT 190 01180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 12 of 13 SECTION 7 SYSTEMS DESCRIPTION For systems descriptions refer to the Baron G58 AFM 58 590000 67 or the Garmin G1000 Pilots Guide for the Beechcraft G58 190 00629 03 Rev A or later SECTION 8 HANDLING SERVICING AND MAINTENANCE No Change HAWKER BEECHCRAFT 190 01 180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 13 of 13
6. FAA Approved Airplane Flight Manual Supplement G1000 Integrated Avionics Update with Synthetic Vision Pathways on Hawker Beechcraft G58 This Supplement is Applicable to the Following Manual s 58 590000 67 Airplane Serial Number Airplane Registration Number FAA Approved By Robert G Murray ODA STC Unit Administrator Garmin International Inc ODA 240087 CE Date s 29 eor 2 HAWKER BEECHCRAFT 190 01180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 1 of 13 LOG OF REVISIONS FAA Approved Airplane Flight Manual Supplement G1000 Integrated Avionics on Hawker Beechcraft G58 REV PAGE DATE OF No NO S DESCRIPTION REV 1 All Initial Release 6 4 10 2 All Add S W version 0857 09 See Cover HAWKER BEECHCRAFT 190 01180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 2 of 13 5 SECTION 1 GENERAL SECTION 2 SECTION 3 EMERGENCY PROCEDURES SECTION ABNORMAL PROCEDURES SECTION 4 NORMAL SECTION 5 SECTION 6 WEIGHT AND BALANCE EQUIPMENT LIST 12 SECTION 7 SYSTEMS 13 SECTION 8 HANDLING SERVICING AND MAINTENANCE 13 HAWKER BEECHCRAFT 190 01 180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED
7. cting navigation data is published for the procedure the database must not be used to conduct the procedure GPS SBAS based IFR enroute oceanic and terminal navigation is prohibited unless the pilot verifies and uses a valid compatible and current Navigation database or verifies each waypoint for accuracy by reference to current approved data Discrepancies that invalidate a procedure must be reported to Garmin International The affected procedure is prohibited from being flown using data from the Navigation database until a new Navigation database is installed in the aircraft and verified that the discrepancy has been corrected Contact information to report Navigation database discrepancies be found at www Garmin com gt Support gt Contact Garmin Support gt Aviation Pilots and operators can view navigation data base alerts at www Garmin com gt In the Air gt NavData Alerts When operating under instrument flight rules requiring an alternate airport the required alternate airport must not be flight planned based on an RNAV GPS LP LPV or LNAV VNAV approach The HAWKER BEECHCRAFT 190 01180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 7 of 13 alternate airport must be flight planned based upon LNAV approach or available ground based approach which the aircraft is equipped to fly For flight planning purposes in areas where SBAS coverage is not available the pilot must check RAIM availability Within the Unite
8. d States RAIM availability can be determined using the Garmin WFDE Prediction program number 006 0154 01 010 G1000 00 or later approved version with GARMIN GA36 and GA37 antennas selected or the FAA s en route and terminal RAIM prediction website www raimprediction net or by contacting a Flight Service Station Within Europe RAIM availability can be determined using the Garmin WFDE Prediction program or Europes AUGER GPS Prediction Tool at http augur ecacnav com augur app home For other areas use the G1000 WFDE Prediction program This requirement is not necessary if SBAS coverage is confirmed to be available along the entire route of flight The route planning and WFDE prediction program may be downloaded from the GARMIN G1000 website on the internet For information on using the WFDE Prediction Program refer to GARMIN WAAS FDE Prediction Program part number 190 00643 01 WFDE Prediction Program Instructions For flight planning purposes operations within the U S National Airspace System on RNP and RNAV procedures when SBAS signals are not available the availability of GPS integrity RAIM shall be confirmed for the intended route of flight In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended route of flight the flight must be delayed canceled or re routed on a track where RAIM requirements can be met or a ground based navigation system can be used F
9. f Class II navigation in oceanic and remote navigation RNP 10 without time limitations in accordance with AC 20 138A and FAA Order 8400 12A The G1000 can be used without reliance on other long range navigation systems This does not constitute an operational approval The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft has been found to comply with the navigation requirements for primary means of Class II navigation in oceanic and remote navigation RNP 4 in accordance with AC 20 138A and FAA Order 8400 33 The G1000 can be used without reliance on other long range navigation systems Additional equipment may be required to obtain operational approval to utilize RNP 4 performance This does not constitute an operational approval The Garmin G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with the accuracy integrity and continuity of function and contains the minimum system functions required for PRNAV operations in accordance with JAA Administrative amp Guidance Material Section One General Part 3 Temporary Guidance Leaflets Leaflet No 10 JAA TGL 10 Rev 1 The GNSS navigation system has two ETSO 145 TSO C145a Class approved Garmin GIA 63Ws and ETSO 146 TSO C146a Class 3 approved Garmin GDU 104X Display Units The G1000 Integrated Avionics GNSS navigation system as installed in this aircraft complies with the equipment requirements for PRNAV and BRN
10. ing RNP 4 and RNP 10 performance This must be verified by referring to the MFD AUX GPS STATUS page to determine the state of GPS1 and GPS2 North Atlantic NAT Minimum Navigational Performance Specifications MNPS Airspace operations per AC 91 49 and AC 120 33 require both GPS SBAS receivers to be operating and receiving usable signals except for routes requiring only one Long Range Navigation sensor Operator s mandatory crosschecking procedures must include referring to the MFD AUX GPS STATUS page to determine the state of GPS1 and GPS2 Whenever possible RNP and RNAV routes including Standard Instrument Departures SIDs and Obstacle Departure Procedures ODPs Standard Terminal Arrival STAR and enroute RNAV Q and RNAV T routes should be loaded into the flight plan from the database in their entirety rather than loading route waypoints from the database into the flight plan individually Selecting and inserting individual named fixes from the database is permitted provided all fixes along the published route to be flown are inserted Manual entry of waypoints using latitude longitude or place bearing is prohibited GPS or GPS and RNAV GPS instrument approaches using the G1000 System are prohibited unless the pilot verifies and uses the current Navigation database GPS based instrument approaches must be flown in accordance with an approved instrument approach procedure that is loaded from the Navigat
11. ion database Not all published Instrument Approach Procedures IAP are in the Navigation database Pilots planning on flying an RNAV instrument approach must ensure that the Navigation database contains the planned RNAV Instrument Approach Procedure and HAWKER BEECHCRAFT 190 01180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 9 of 13 that approach procedure must be loaded from the Navigation database into the FMS flight plan by its name IFR non precision approach approval using the GPS SBAS sensor is limited to published approaches within the U S National Airspace System Approaches to airports in other airspace are not approved unless authorized by the appropriate governing authority The navigation equipment required to join and fly an instrument approach procedure is indicated by the title of the procedure and notes on the IAP chart Use of the GARMIN G1000 GPS SBAS receivers to provide navigation guidance during the final approach segment of an ILS LOC LOC BC LDA SDF MLS or any other type of approach not approved for or GPS navigation is prohibited When using the G1000 VOR LOC GS receivers to fly the final approach segment VOR LOC GS navigation data is must be selected and presented on the CDI of the pilot flying Navigation information is referenced to WGS 84 reference system and should only be used where the Aeronautical Information Publication including electronic data and aeronautical charts conform to WGS
12. or flight planning purposes for operations within European B RNAV and P RNAV airspace if more than one satellite is scheduled to be out of service then the availability of GPS integrity RAIM shall be confirmed for the intended flight route and time In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended flight the flight must be delayed canceled or re routed on a track where RAIM requirements can be met or a ground based navigation system can be used For flight planning purposes operations where the route requires Class navigation the aircrafts operator or pilot in ccommand must use the Garmin WFDE Prediction program to demonstrate that HAWKER BEECHCRAFT 190 01 180 01 MODEL G58 BONANZA Rev 2 FAA APPROVED Page 8 of 13 there no predicted outages on the specified route that would prevent the G1000 from providing primary means of Class Il navigation in oceanic and remote areas of operation that requires RNP 10 RNP 4 capability If the Garmin WFDE Prediction program indicates fault exclusion FDE is unavailable for more than 34 minutes in accordance with FAA Order 8400 12B for RNP 10 requirements or 25 minutes in accordance with FAA Order 8400 33 for RNP 4 requirements then the operation must be rescheduled when FDE is available Both GIA 63W GPS navigation receivers must be operating and providing GPS navigation guidance to the PFD and MFD for operations requir
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