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 3-28
b. Ground Speed Thresholds (knots)
• Max Ground Speed: The valid range is 30 to 100. Typically, 70% of Vs0. Must be less
than the Discrete Override Speed.
This is the upper threshold speed which aircraft is considered on ground. Ground speeds
below this level place the unit in the Ground state. Fields that become inhibited get set to
zeros. As fields become uninhibited, the values are reset to defaults.
• Discrete Override Speed: Applicable only when On Ground Discrete installed and not a
Rotorcraft. When applicable, the valid range is 30 to 100, typically 130% of Vs1, and must
be greater than Max Ground Speed.
This is the lower threshold speed which aircraft is considered in air. Ground speeds above
this level place the unit in the In Air state, overriding the discrete switch.
c. Altitude Thresholds (feet)
• GPS Altitude: The valid range is 0 to 500.
This value is used for fixed wing and rotorcraft installs that do not have an air/ground
discrete. This is the lower limit threshold difference in GPS altitude after Power ON at
which aircraft is considered in air. A change in GPS altitude above this level places the unit
in the In Air state.
• Pressure Altitude: The valid range is 0 to 500.
This value is used for fixed wing and rotorcraft installs that do not have an air/ground
discrete. This is the lower limit threshold difference in pressure altitude after Power ON at
which aircraft is considered in air. A change in pressure altitude above this level places the
unit in the In Air state.
- Set the pressure altitude at 150 if Gillham/Gray-code is used.
6. Standby Input:
This setting is used to set the transponder function of the Lynx NGT-9000 into standby. It is typically
used in dual installations. Available with Release 2.1 and greater.
a. Standby Discrete Installed
• Not Installed: Normal setting for single installation.
• Ground – Standby: This setting activates Discrete In 6 (pin 32). When an external switch is
set to ground the NGT-9000 transponder function is set to standby.
Note – Transponder mode cannot be changed using a control panel when this external
discrete is grounded, though the Mode A code can be set for eventual use.
7. Input/Output Configuration:
The following settings are based on equipment interfaces setup during installation.
a. RS-422 #1
• Control Panel/External Display: Typically used by the remote mount NGT-9000R to
output traffic and FIS-B information.
• WX-500: Alternate method of interfacing with the WX-500 Stormscope. Panel mount
NGT-9000 only. Depending on settings this input can also be used by the NGT-9000 for
heading.
• L-3 Protocol 1: This setting outputs GPS Position Source.
WAAS/GPS Output: Certified 5 Hz, RS-422/RS-232 and WiFi Class Beta 1 GPS output.
Qualified for LNAV approaches only per TSO-C129d Table 1-1.