Installation Manual
Table Of Contents
- 17001_0_Frt-Matr
- 17001_1_Gen-Info
- 1.1 INTRODUCTION
- 1.2 FUNCTIONAL DESCRIPTION
- 1.2.1 Software Release Summary
- 1.2.2 Transponder Functional Overview
- 1.2.3 GPS Functional Overview
- 1.2.4 Lightning Detection (optional)
- 1.2.5 ADS-B System Overview
- 1.2.6 Traffic Display Functional Overview
- 1.2.7 FISB System Overview
- 1.2.8 Traffic Awareness System (option) Overview
- 1.2.9 ADS-B Traffic Advisory System Overview (optional)
- 1.2.10 Traffic Alert and Collision Avoidance System (option) Overview
- 1.2.11 Terrain Awareness and Warning System Overview (optional)
- 1.2.12 TerrainVisionTM
- 1.2.13 Discrete Inputs and Outputs Functional Overview
- 1.3 EQUIPMENT DESCRIPTIONS
- 1.4 INTERFACES
- 1.4.1 ADS-B Out Fail
- 1.4.2 AHRS Input
- 1.4.3 Altitude Encoder Input
- 1.4.4 Audio Out
- 1.4.5 Standby Mode
- 1.4.6 Audio Mute In and Out
- 1.4.7 Audio Acknowledge
- 1.4.8 RF Suppression Input/output
- 1.4.9 Traffic Alert
- 1.4.10 TAWS Caution and Warning Alert
- 1.4.11 WiFi Interface
- 1.4.12 WOW Input
- 1.4.13 Maintenance Interface
- 1.4.14 GPS Antenna
- 1.4.15 L-Band (978/1030/1090 MHz) Antenna
- 1.4.16 Directional Antenna
- 1.4.17 Traffic Display
- 1.4.18 Weather Display
- 1.4.19 Lightning Detection (WX-500)
- 1.4.20 Control Panel
- 1.5 INSTALLATION CONSIDERATIONS
- 1.6 SPECIFICATIONS
- 1.7 TSO INFORMATION
- 1.8 MODIFICATIONS
- 1.9 SOFTWARE REVISIONS
- 1.10 EQUIPMENT REQUIRED NOT SUPPLIED
- 1.11 EQUIPMENT INTERFACES
- 1.12 OBTAINING SOFTWARE
- 1.13 INSTALLATION PROCEDURE FOR LYNXMSS USB DRIVER
- 1.14 INSTALLATION APPROVAL AND LIMITATIONS
- 17001_2_Instal
- 2.1 INTRODUCTION
- 2.2 UNPACKING AND INSPECTING
- 2.3 INSTALLATION PROCEDURES
- 2.3.1 Panel Mount Location
- 2.3.2 Remote Mount Location
- 2.3.3 Electrical Connections
- 2.3.4 Compatible Equipment Installation Information
- 2.3.5 Discrete Inputs and Output Connections
- 2.3.6 Installation Guidelines for the DCM
- 2.3.7 P1 Mating Connector Assembly
- 2.3.8 Panel mount NGT-9000 Installation
- 2.3.9 Remote Mounted Lynx NGT-9000 Installation
- 2.3.10 CP-2500 Installation Guidelines
- 2.3.11 Antenna Installation Guidelines
- 17001_3_Inst_Check
- 3.1 INTRODUCTION
- 3.2 BASIC OPERATION
- 3.3 MPC (MAT) OPERATION
- 3.4 INSTALLATION PROCEDURE FOR LYNXMSS USB DRIVER
- 3.5 MAINTENANCE MODE
- 3.6 VERIFY SOFTWARE VERSION
- 3.7 SELECT CONFIGURATION OPTIONS
- 3.8 CALIBRATION SETUP
- 3.9 INTERFACE CHECK
- 3.10 SETUP PIM-9000 WIFI MODULE
- 3.11 INSTALLATION CHECKOUT
- 3.11.1 Functional Checks
- 3.11.2 Ground Checks
- 3.11.3 Electromagnetic Interference (E.M.I.) Check
- 3.11.4 Panel mount NGT-9000 Display Check
- 3.11.5 Flight Test
- 3.11.6 Installation Checkout Complete
- 17001_4_Maint
- 17001_5_App-A_signal
- A.1 INTRODUCTION
- A.2 INPUT AND OUTPUT INTERFACES
- A.2.1 Input Power
- A.2.2 RF Suppression Bus
- A.2.3 Audio Output
- A.2.4 Gillham Input (Altitude Input)
- A.2.5 RS-232 Interface
- A.2.6 RS-422 Interface
- A.2.7 ARINC 429 Input
- A.2.8 ARINC 429 Output
- A.2.9 Discrete Input
- A.2.10 Discrete Output
- A.2.11 I2C Serial Bus (Detachable Configuration Module)
- A.2.12 Antenna Connections
- A.3 PIN DEFINITION SUMMARY
- A.4 [J1 CONNECTOR]
- 17001_6_App-B_Environmental
- 17001_7_App-C_Compatibility
- 17001_8_App-D_TSO
- 17001_9_App-E_Questionaire
Lynx NGT-9000
Installation Manual
0040-17001-01 (Revision W) Installation Checkout Page 3-52
3.11.3 Electromagnetic Interference (E.M.I.) Check
Check the following applicable aircraft systems, as well as any other system or device that is not listed,
for interference. Initial tests are to be conducted with the aircraft operating on external ground power.
Disregard any system or device that does not apply.
NOTE
The Electromagnetic Interference Check is required only for initial system
installations and not required if the unit is removed or replaced.
1. Communications
a. Cockpit Intercom
Using the cockpit intercom, verify interference free communications between the crew while
monitoring the effects of the unit.
b. VHF Communications
Set VHF communications radios to multiple frequencies and monitor effects of unit while
transmitting and receiving. At a minimum, the frequencies listed below should be tested, in
addition to locally available frequencies:
Check the GPS signal status of each satellite being received does not drop while transmitting
each frequency for a period of 35 seconds. Degradation of individual received satellite signals
below a point where navigation is no longer possible is not acceptable and will require that
additional isolation measures be taken.
For installations on rotorcraft, ensure that the rotor blades do not interfere with the received GPS
signals. This problem has been experienced in some rotorcraft and varies with the rotation rate.
Test the following frequencies for 25 kHz COM channel spacing:
121.150 MHz 121.200 MHz 121.250 MHz 131.225 MHz 131.275 MHz 131.325 MHz
121.175 MHz 121.225 MHz 131.200 MHz 131.250 MHz 131.300 MHz 131.350 MHz
In addition, test the following frequencies for VHF radios with 8.33 kHz channel spacing:
121.185 MHz 121.190 MHz 130.285 MHz 131.290 MHz
c. SATCOM Communications
If aircraft is equipped with a SATCOM system, operate the SATCOM equipment while
monitoring the GPS Satellite Status Page. Verify GPS position remains valid.