L3 Aviation Products Lynx NGT-9000 Caractéristiques techniques

FAIRCHILD SA227-AC

AC-583

N3114G

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(2(of(27(Document(Number(L3-76AK-AFMS1(

FAA(Approved

FAA APPROVED

AIRPLANE FLIGHT MANUAL SUPPLEMENT

SUPPLEMENTAL FLIGHT MANUAL

For The

L3 Aviation Products

Lynx Multilink Surveillance System

Models NGT-9000

L3 Part Number 9029000-20000

RECORD OF REVISIONS

Revision

Date of Revision

Description

Original

3/31/2015

Original Issue

6/19/2015

Typographical error corrections

Corrections to Table 3-1 in section 3.2.1

3/27/2016

Incorporation of s/w Revision 2.0: ATAS and

TAWS

2/24/2017

Updated for s/w Version 2.1

9/19/2017

Updated for s/w Version 3.x

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(3(of(27(Document(Number(L3-76AK-AFMS1(

FAA(Approved

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Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(4(of(27(Document(Number(L3-76AK-AFMS1(

FAA(Approved

TABLE OF CONTENTS

SECTION 1.!GENERAL ........................................................................................................... 6!

1.1!Functional Description ................................................................................................... 6!

1.2!NGT-9000 ADS-B Traffic Advisory System (ATAS) [Optional] ...................................... 7!

1.3!NGT-9000 Terrain Awareness and Warning System (TAWS) [Optional] ...................... 7!

1.4!NGT-9000+ Traffic Awareness Overview [Optional] ...................................................... 8!

1.5!NGT-9000D Antenna Diversity Overview [Optional] ...................................................... 8!

1.6!Capabilities .................................................................................................................... 8!

1.7!L-Band UAT Antenna ..................................................................................................... 9!

1.8!GPS Antenna and the MSS Internal GPS Receiver ...................................................... 9!

1.9!Configuring the NGT-9000 ............................................................................................. 9!

1.10!Personal Electronic Devices .......................................................................................... 9!

1.11!Weather Displays ........................................................................................................... 9!

1.12!Lightning Detection (Optional) ....................................................................................... 9!

1.13!Traffic Displays ............................................................................................................. 10!

1.14!Interaction of Major Components ................................................................................. 12!

1.15!Installation Configuration for This Aircraft .................................................................... 13!

SECTION 2.!LIMITATIONS ................................................................................................... 14!

2.1!Minimum Documentation ............................................................................................. 14!

2.2!Minimum Equipment .................................................................................................... 14!

2.3!ADS-B OUT Compliance.............................................................................................. 14!

2.4!IDENT Function............................................................................................................ 14!

2.5!ALT Function ................................................................................................................ 14!

2.6!Standby Function ......................................................................................................... 14!

2.7!Traffic Awareness ........................................................................................................ 14!

2.8!Terrain Awareness ....................................................................................................... 15!

2.9!Applicable System Software ........................................................................................ 15!

SECTION 3.!EMERGENCY PROCEDURES ......................................................................... 16!

3.1!Emergency Procedures ............................................................................................... 16!

3.2!Abnormal Procedures .................................................................................................. 17!

SECTION 4.!NORMAL PROCEDURES ................................................................................ 26!

4.1!Normal Power ON ........................................................................................................ 26!

SECTION 5.!PERFORMANCE .............................................................................................. 26!

SECTION 6.!WEIGHT AND BALANCE ................................................................................. 26!

SECTION 7.!SYSTEM DESCRIPTIONS ................................................................................ 26!

7.1!Pilot’s Guide ................................................................................................................. 26!

7.2!Traffic Sources ............................................................................................................. 26!

7.3!Weather Sources ......................................................................................................... 26!

7.4!Lightning Detection Sources [Optional] ........................................................................ 27!

7.5!Power ........................................................................................................................... 27!

7.6!External Switches, Lights and Controls [Optional] ....................................................... 27!

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(5(of(27(Document(Number(L3-76AK-AFMS1(

FAA(Approved

TABLE OF FIGURES

Figure 1-1: Lynx NGT-9000 ......................................................................................................... 6!

Figure 1-2: Typical NGT-9000 Traffic Screen ........................................................................... 10!

Figure 1-3: NGT-9000 Connections and Functions ................................................................... 12!

Figure 1-4: Installation Configuration Data ................................................................................ 13!

TABLE OF TABLES

Table 1-1: Typical Target Symbology ........................................................................................ 11!

Table 2-1: Required Equipment ................................................................................................ 14!

Table 2-2: Software Version ...................................................................................................... 15!

Table 3-1: Troubleshooting for the Panel Mount NGT-9000 ..................................................... 17!

Table 7-1: Light and Switch Functions ...................................................................................... 27!

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(6(of(27(Document(Number(L3-76AK-AFMS1(

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SECTION 1. GENERAL

1.1 Functional Description

The Lynx MultiLink Surveillance System (also referred to in this manual as the Lynx NGT-9000)

is a Mode S Level 2 dens Class 1 Transponder with an integrated GPS receiver providing

Automatic Dependent Surveillance-Broadcast (ADS-B) output using a 1090ES (Extended

Squitter). The unit also receives ADS-B data via 1090ES and UAT (978 MHz Universal Access

Transceiver). Figure 1-1 is a depiction of the NGT-9000.

The unit replies to Mode A, Mode C and Mode S interrogations receiving interrogations at 1030

MHz and transmitting responses at 1090 MHz. The unit is equipped with IDENT capability that

activates the Special Identification (SPI) pulse for 18 seconds.

Ground stations can interrogate Mode S Transponders individually using a 24-bit ICAO Mode S

address, which is unique to the particular aircraft. In addition, ground stations may interrogate

the unit for its transponder data capability and the aircraft's Flight ID.

The ADS-B provides own aircraft data with Enhanced Visual Acquisition (EVAcq) traffic

information that improves situational awareness and flight safety by providing aircraft position,

velocity, and heading information that is automatically transmitted from other aircraft and ground

stations providing immediate surveillance of air-to-air traffic.

In addition to ADS-B surveillance, the installed NGT-9000 includes an Active Traffic Awareness

System (TAS/TCAS), ADS-B Traffic Advisory System (ATAS) and Terrain Awareness and

Warning System (TAWS), as well as support for both top and bottom antenna diversity.

The 1090ES and UAT ADS-B data link have the following capabilities:

• 1030MHz/1090 MHz In – Receive ADS-R and TIS-B

• 1090ES OUT – Transmits 1090 MHz Extended Squitter ADS-B

• UAT IN – Receives 978 MHz ADS-B, ADS-R and TIS-B, FIS-B, NOTAMS, and TFR’s

Figure 1-1: Lynx NGT-9000

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(7(of(27(Document(Number(L3-76AK-AFMS1(

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1.2 NGT-9000 ADS-B Traffic Advisory System (ATAS) [Optional]

The ADS-B Traffic Advisory System (ATAS) is a passive system that monitors ADS-B, ADS-R

and TIS-B ADS-B IN data and alerts the flight crew via on-screen alerts aural traffic calls and an

optional Traffic Alert lamp to nearby aircraft and assists the pilot in the visual acquisition of

aircraft that may represent a danger. Refer to the Pilot's Guide, L3 p/n 0040-17000-01 Revision

H or later, for examples of on-screen symbology and aural alerts.

• The tracking of other aircraft is in a cylindrical volume centered on own aircraft with a

maximum radius of 20 nmi and extending 10,000 ft above and 10,000 ft below ownship.

• ATAS will track up to 60 intruders simultaneously.

• A Traffic Advisory (TA) is displayed when other aircraft are a potential threat.

• When ownship is in the airport environment, a Traffic Advisory (TA) is displayed 12.5 to

35 seconds prior to the CPA with another aircraft when the CPA is within 750 ft

horizontally and 300 ft vertically.

• A TA symbol remains on the screen for at least 8 seconds unless the respective track is

terminated.

• When the aircraft is outside the airport environment, aircraft that are within a range of 6

nmi of ownship with a vertical distance of +/- 1200 ft (if altitude is reporting) are classified

as a Proximate Advisory (PA). A PA is displayed only for aircraft that are in air.

• ATAS and TAS/TCAS may operate at the same time with traffic information being

correlated by the unit

When ATAS is installed, an Audio Acknowledge button will cancel the current aural

announcement.

1.3 NGT-9000 Terrain Awareness and Warning System (TAWS) [Optional]

The Terrain Awareness and Warning System (TAWS) is an optional function that is set up

during installation. The TAWS function continuously monitors the aircraft’s position, altitude,

speed, track, and phase of flight and compares the information to the terrain database loaded

during installation. Terrain and obstacle hazards are indicated by cautions and warnings using

screen annunciators, aural terrain alerts, and Terrain Caution and Warning alert lamps. Refer to

the Pilot's Guide, L3 p/n 0040-17000-01 Revision H, or later, for examples of on-screen

symbology and aural alerts.

The TAWS function uses Forward Looking Terrain Avoidance (FLTA) and Ground Proximity

Warning System (GPWS) functionality to determine when a terrain alert or altitude callout is

triggered due based on the following conditions:

• Reduced required terrain or obstacle clearance (FLTA)

• Imminent terrain impact (FLTA)

• Premature descent

• Excessive descent rate (GPWS)

• Negative climb rate or altitude loss after takeoff (GPWS)

• Passing an altitude of 500 ft (GPWS)

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(8(of(27(Document(Number(L3-76AK-AFMS1(

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There are four TAWS configurations available with the NGT-9000:

• Disabled

• TAWS B – Default Aural Phrases

• TAWS B – Alternate Aural Phrases

• Display Only – No Alerts

When a TAWS configuration is enabled with audio, an Audio Acknowledge button will cancel the

current aural announcement.

1.4 NGT-9000+ Traffic Awareness Overview [Optional]

The NGT-9000+ (“9000 Plus”) supports optional active Traffic Awareness System (TAS) and

Traffic Conflict Avoidance System (TCAS).

The TAS/TCAS options are active systems that operate as aircraft-to-aircraft interrogation

devices. The unit interrogates transponders in the surrounding airspace similar to ground based

radar. When replies to these active interrogations are received, the responding aircraft’s range,

altitude, and closure rates are computed to plot traffic location and predict collision threats. The

unit alerts the flight crew to nearby transponder equipped aircraft and assists the pilot in the

visual acquisition of aircraft that may represent a danger. Traffic information, out to a selected

range, is graphically displayed on the unit or alternate display. Refer to the Pilot's Guide, L3 p/n

0040-17000-01 Revision K or later, for examples of on-screen symbology and aural alerts for

each system.

• The system display shows the relative position of traffic using text, shapes (i.e., Traffic

Advisory = solid circle; Other Traffic = open diamond) and colors.

• The effective active-mode surveillance range is 35 nm and the system is capable of

tracking 35 Intruders simultaneously with the target bearing relative to the nose of own

aircraft.

• The tracking of targets is in a cylindrical volume centered on own aircraft that has, at a

minimum, a radius of 35 nm and extends 10,000 ft above and 10,000 ft below own

aircraft.

• The system uses a voice audio output that announces Traffic Advisory and relative

altitude (with optional Extended Call-outs enabled).

• The TCAS option qualifies as a TCAS I system and as such, offers only Traffic

Advisories (TA) (“Traffic, traffic. 12-O’clock, one mile”) but not Resolution Advisories

(RA) such as “Climb, climb”.

1.5 NGT-9000D Antenna Diversity Overview [Optional]

The NGT-9000D has the same hardware and firmware/software as the basic NGT-9000, but is

capable of supporting dual L-band antennas (one bottom and one top) to enhance system

performance and prevent fuselage blanking of a single bottom antenna in tight turns into a

ground station or UAT target. The upper L-band antenna may be a single blade antenna or the

optional Directional Antenna.

1.6 Capabilities

The NGT-9000 transceiver can be software configured as either an NGT-9000, 9000+, or

9000D. It can also be installed with, or without TAWS and peripheral ARINC-429 or RS-422

panel mounted traffic and weather displays.

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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Revision(4(Issue: 9/19/17(Page(9(of(27(Document(Number(L3-76AK-AFMS1(

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1.7 L-Band UAT Antenna

The L-Band antenna is used by the Lynx NGT-9000 to transmit and receive 1090 MHz ADS-B

and receive 978MHz ADS-B (UAT). At least one L-band antenna must be located on the

bottom of the aircraft.

1.8 GPS Antenna and the MSS Internal GPS Receiver

The GPS utilizes signals from Global Positioning System (GPS)

satellite constellation and

Satellite-Based Augmentation Systems

(SBAS). The MSS has an internal GPS function that

provides position, velocity, time and integrity (NIC, NAC, etc.) information to the ADS-B

functions. It is located on the top of the aircraft.

NOTE

The NGT-9000’s built-in GPS does not provide Ownship position for external

moving map displays

1.9 Configuring the NGT-9000

The unit’s configuration is preserved within the Data Configuration Module (DCM), which is

permanently attached to the aircraft and communicates with the NGT-9000 via a serial

connection. The configuration options are set up during installation and cannot be changed

except by a licensed installer.

NOTE

The NGT-9000’s configuration parameters can only be changed by a

licensed installer

1.10 Personal Electronic Devices

The Lynx NGT-9000 supports the use of personal electronic devices (e.g., iPad) via a Wi-Fi

connection. The PED must use approved applications that

support the ADS-B broadcast

services (i.e., ADS-B In, TIS-B, ADS-R, and FIS-B). Check with an L3 approved avionics

dealer or contact L3 Aviation Products for a current list of approved applications.

1.11 Weather Displays

NEXRAD, METARS, TAFS, PIREPS, NOTAMS and temperatures and winds aloft are displayed

on the NGT-9000 provided that the aircraft is within the service volume of a ground station.

Additionally, the same information can be displayed on approved weather displays can interface

with the NGT-9000 to

provide FIS-B weather information using the ADS-B IN link. Screen

information and controls may be different for each of the approved displays.

1.12 Lightning Detection (Optional)

The WX-500 Stormscope is a Weather Mapping System that provides lightning discharge

information. This information is shown on the right application screen of the NGT-9000 Panel

Mount unit. This function is available beginning with Software 2.1.

Airplane Flight Manual Supplement or Supplemental Flight Manual for the NGT-9000

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1.13 Traffic Displays

The NGT-9000 will provide, at a minimum, UAT, TIS-B and ADS-R traffic on the unit’s built-in

display and can repeat this traffic information on any approved ARINC-429 or RS-422 display.

The NGT-9000+ can also display active Traffic Awareness System (TAS/TCAS) targets on the

unit’s built-in display and can repeat this traffic information on any approved ARINC-429 or RS-

422 display. Figure 1-2 Illustrates a typical traffic display on the NGT-9000 screen. Table 1-1

illustrates typical target symbology.

Refer to the Pilot's Guide, L3 p/n 0040-17000-01 Revision K, or later, for details on operation

and a description of how the information is depicted. Check with an L3 approved avionics

dealer or contact L3 Aviation Products for a current list of approved traffic displays.

Figure 1-2: Typical NGT-9000 Traffic Screen

1.13.1 Traffic Priority

Traffic is displayed on the screen using the following priority scheme:

1. TAS/TCAS Traffic Advisories (TA’s)

2. ATAS (ADS-B) Traffic Alerts

3. Selected Traffic

4. Proximate Advisories

5. Other Traffic

Traffic may also be prioritized according to phase of flight by using the ALT Mode toggle on the

left of the screen with:

• Normal (NRM) displaying traffic ± 2,700 ft relative to Ownship

• Above (ABV), or Takeoff Mode, displaying traffic +9,000 and -2,700 ft relative to

Ownship

• Below (BLW), or Landing Mode, displaying traffic +2,700 and -9,000 ft relative to

Ownship

• Unrestricted (UNR) or Enroute Mode, displaying traffic +9,900 and -9,900 ft relative to

Ownship

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