Airplane Flight Manual Supplement II Morrow Inc. for II Morrow GX50 GPS and GX60/65 VHF Comm/GPS 2345 Turner Rd. SE June 11, 1999 Salem, OR 97302 Part #: 560-1015-02 Rev - FAA Approved Supplementary Airplane Flight Manual II Morrow Apollo GX50 GPS and GX60/65 VHF Comm/GPS Airplane Make: Airplane Model: Airplane Serial No.: Registration No.: Partenavia P68 Series _________ _________ This Supplementary Flight Manual must be attached to the Registro Aeronautica Italiano (R.A.I.) approved Flight Manual when the Apollo GX50 GPS or GX60/ 65 GPS/Comm is installed for IFR use in accordance with STC SA00504SE. The information contained herein supplements the basic Registro Aeronautica Italiano (R.A.I.) approved Airplane Flight Manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic Airplane Flight Manual. FAA Approved Date: _____________ Page 1 of 16 Airplane Flight Manual Supplement for II Morrow GX50 GPS and GX60/65 VHF Comm/GPS II Morrow Inc. June 11, 1999 2345 Turner Rd. SE Part #: 560-1015-02 Rev Salem, OR 97302 Revision Log Rev 00 00 A 01 02 Date 1/28/98 3/18/98 6/30/98 3/03/99 Description Initial Release Minor Corrections Added GX65. Reworded Altitude Assist limitation. Modified for navigation software version 3.0. Added references to RNP-5 qualifications as defined for European B-RNAV (AC 90-96 & JAA TGL No. 2) EN 5716 5773 5809 6068 By Auth Chk RAS RDG RDG RDG Page 2 of 16 FAA Approved Date: _____________ Airplane Flight Manual Supplement II Morrow Inc. for II Morrow GX50 GPS and GX60/65 VHF Comm/GPS 2345 Turner Rd. SE June 11, 1999 Salem, OR 97302 Part #: 560-1015-02 Rev - TABLE OF CONTENTS 1. 1.1 1.1.1 1.1.2 GENERAL ......................................................................................................................... 5 APOLLO GX50/GX60/GX65 DESCRIPTION.......................................................................... 5 Apollo GX50 GPS................................................................................................................................. 5 Apollo GX60/65 GPS/Comm................................................................................................................ 5 1.2 2. 2.1 2.2 2.3 2.4 2.5 2.6 2.7 2.8 2.9 2.10 2.11 2.12 2.13 3. 3.1 3.2 3.2.1 3.2.2 OPERATION........................................................................................................................... 6 LIMITATIONS.................................................................................................................. 7 USER MANUAL ..................................................................................................................... 7 SYSTEM SOFTWARE .............................................................................................................. 7 DATA BASE (IFR)................................................................................................................. 7 ALTERNATE NAVIGATION SYSTEM ....................................................................................... 8 GPS APPROACHES (GX50/60 ONLY) ................................................................................... 8 MAGNETIC VARIATION ......................................................................................................... 8 ANNUNCIATED MESSAGES (IFR) .......................................................................................... 8 DISPLAY/ANNUNCIATORS/INDICATORS (IFR)....................................................................... 8 NON-NAVIGATION INFORMATION ......................................................................................... 9 VNAV - ALTITUDE ASSIST .............................................................................................. 9 FOREIGN AIRSPACE .......................................................................................................... 9 ALTERNATE COMMUNICATION SYSTEM (GX60/65) ......................................................... 9 RNP-5/B-RNAV OPERATIONS ........................................................................................ 9 EMERGENCY / ABNORMAL PROCEDURES ......................................................... 10 EMERGENCY PROCEDURES ................................................................................................. 10 ABNORMAL PROCEDURES................................................................................................... 10 Invalid Nav Data ................................................................................................................................. 10 RAIM Not Available ........................................................................................................................... 10 4. 4.1 4.2 4.3 4.4 4.5 4.6 4.7 5. 6. 7. 7.1 7.1.1 7.1.2 NORMAL PROCEDURES ............................................................................................ 10 GENERAL............................................................................................................................ 10 SYSTEM ANNUNCIATORS .................................................................................................... 10 SYSTEM SWITCHES / CONTROLS ......................................................................................... 11 PILOT'S DISPLAY ................................................................................................................ 11 HSI / AUTOPILOT COUPLED OPERATION - NAV SOURCE SELECTION.................................. 12 APPROACH OPERATION ...................................................................................................... 12 AIRSPACE ALERTS .............................................................................................................. 12 PERFORMANCE............................................................................................................ 13 WEIGHT AND BALANCE............................................................................................ 13 SYSTEM DESCRIPTION.............................................................................................. 13 APOLLO GX50/60/65 ......................................................................................................... 13 Data Base Cards .................................................................................................................................. 13 Circuit Protection ................................................................................................................................ 13 FAA Approved Date: _____________ Page 3 of 16 Airplane Flight Manual Supplement for II Morrow GX50 GPS and GX60/65 VHF Comm/GPS II Morrow Inc. June 11, 1999 2345 Turner Rd. SE Part #: 560-1015-02 Rev Salem, OR 97302 7.2 7.3 NAVIGATION SOURCE SELECTION ...................................................................................... 14 COMM SOURCE SELECTION ................................................................................................ 15 LIST OF ILLUSTRATIONS FIGURE 1: APOLLO GX50 ................................................................................................................ 5 FIGURE 2: APOLLO GX60/65 ........................................................................................................... 6 FIGURE 3: ANNUNCIATORS............................................................................................................. 11 FIGURE 4: NAVIGATION SYSTEM BLOCK DIAGRAM ....................................................................... 14 FIGURE 5: AUDIO SYSTEM BLOCK DIAGRAM ................................................................................. 15 Page 4 of 16 FAA Approved Date: _____________ Airplane Flight Manual Supplement II Morrow Inc. for II Morrow GX50 GPS and GX60/65 VHF Comm/GPS 2345 Turner Rd. SE June 11, 1999 Salem, OR 97302 Part #: 560-1015-02 Rev - 1. GENERAL 1.1 APOLLO GX50/GX60/GX65 DESCRIPTION The Apollo GX50 and GX60 are TSO-C129a Class A1 GPS supplemental navigation systems with a built-in moving map graphics display. The Apollo GX65 is a TSO-C129a Class A2 GPS supplemental navigation system. The GX50/60/65 provides interfaces to a CDI/HSI, autopilot, and annuciators. The GX50/60 is capable of being authorized for IFR/VFR enroute oceanic and remote, enroute domestic, terminal, and non-precision approach operation. The GX65 is capable of being authorized for IFR/VFR enroute oceanic and remote, enroute domestic, and terminal operation. Apollo GX Systems meet all requirements for RNP-5/B-RNAV operations in accordance with FAA AC 90-96 and JAA TGL No. 2 revision 1 (or later). 1.1.1 Apollo GX50 GPS The Apollo GX50 is a GPS only unit and is powered by a single circuit breaker from the avionics bus. Figure 1: Apollo GX50 1.1.2 Apollo GX60/65 GPS/Comm The Apollo GX60/65 includes a 760 channel VHF communications transceiver in addition to the GPS navigation functions. The comm provides a minimum of 8 watts transmit power and has an MTBF (mean time between failure) predicted far in excess of 1000 hours. If operated in the Americas, the comm receives the standard NOAA weather channels. The GX60/65 GPS/Comm is powered by separate circuit breakers for the GPS and comm functions from the avionics bus. The GX60/65 control panel interface (for both the navigation and communication functions) is powered by the GX60/65 navigation breaker. FAA Approved Date: _____________ Page 5 of 16 Airplane Flight Manual Supplement for II Morrow GX50 GPS and GX60/65 VHF Comm/GPS II Morrow Inc. June 11, 1999 2345 Turner Rd. SE Part #: 560-1015-02 Rev Salem, OR 97302 Figure 2: Apollo GX60/65 1.2 OPERATION Provided the Apollo GX50/60 is receiving adequate usable signals, it has been demonstrated capable of and has been shown to meet the accuracy specifications of: · IFR/VFR enroute oceanic and remote, enroute domestic, terminal, and nonprecision approach operation using GPS within the U.S. National Airspace System and the North Atlantic Minimum Navigation Performance Specification (MNPS) Airspace using the WGS-84 (or NAD 83) coordinate reference datum in accordance with the criteria of AC 20-138, AC 91-49, and AC 120-33. RNP-5/B-RNAV Operations as defined in AC 90-96 & JAA TGL 2. · Provided the Apollo GX65 is receiving adequate usable signals, it has been demonstrated capable of and has been shown to meet the accuracy specifications of: · IFR/VFR enroute oceanic and remote, enroute domestic, and terminal operation using GPS within the U.S. National Airspace System and the North Atlantic Minimum Navigation Performance Specification (MNPS) Airspace using the WGS-84 (or NAD 83) coordinate reference datum in accordance with the criteria of AC 20-138, AC 91-49, and AC 120-33. RNP-5/B-RNAV Operations as defined in AC 90-96 & JAA TGL 2. · The GX60 and GX65 also include VHF communications capability meeting the requirements of AC 20-67b for airborne VHF communications installations. Page 6 of 16 FAA Approved Date: _____________ Airplane Flight Manual Supplement II Morrow Inc. for II Morrow GX50 GPS and GX60/65 VHF Comm/GPS 2345 Turner Rd. SE June 11, 1999 Salem, OR 97302 Part #: 560-1015-02 Rev - 2. LIMITATIONS 2.1 USER MANUAL The manuals, or the information contained in the manuals listed below (or later approved revisions), must be immediately available to the flight crew whenever navigation is predicated on the Apollo GX50, GX60, or GX65 system. Nav Software Version 2.1 · · · · · · Apollo GX Models 50, 55, & 60 User's Guide .........P/N 560-0961-00 Apollo GX50/60 Approach User's Guide Insert .......P/N 560-0928-00 (GX50/60 Only) Apollo GX60 Comm User's Guide Insert .................P/N 560-0963-00 (GX60 Only) Nav Software Version 2.2 Apollo GX Models 50, 55, 60, & 65 User's Guide ...P/N 560-0961-01 Apollo GX50/60 Approach User's Guide Insert .......P/N 560-0928-00 (GX50/60 Only) Apollo GX60/65 Comm User's Guide Insert ............P/N 560-0963-01 (GX60/65 Only) Nav Software Version 3.0 · · · Apollo GX Models 50, 55, 60, & 65 User's Guide ...P/N 560-0961-02 Apollo GX50/60 Approach User's Guide Insert .......P/N 560-0928-01 (GX50/60 Only) Apollo GX60/65 Comm User's Guide Insert ............P/N 560-0963-02 (GX60/65 Only) 2.2 SYSTEM SOFTWARE The system must utilize the software versions listed below (or later FAA approved versions). The software versions can be displayed in the system mode on the GX50/60/65 display. · · · GX Series Nav Software............................ Ver 2.1, 2.2, or 3.0 (139-0235-030) GPS Sensor Software ................................ Ver 2.3 VHF Comm Radio Software ..................... Ver 1.2 or 2.0 (GX60/65 only) 2.3 DATA BASE (IFR) IFR enroute and terminal navigation is prohibited unless the pilot verifies the currency of the data base or verifies each selected waypoint for accuracy by reference to current approved data. FAA Approved D ...