ADSB Out In and GNSS Requirements Update US

ADS-B Out, In and GNSS Requirements Update US Capstone Project Alaska US ADS-B-out DO 260 B Mandate 2020 US ADS-B-out Infrastructure 2013 Pacific Ocean ATSA-ITP FAA GATI Canada Hudson Bay November 2010 NRA UPS/ACSS Safe. Route 2008 Certified ITP Europe TCAS Change 7. 1 2012 - 2015 Atlantic Ocean ATSA – ITP FAA GATI ITP Europe Link 2000+ 2011 - 2015 CASCADE Pioneer Phase – 2008 DO 260 (AMC 20 -24) Single European Sky - DO 260 B Mandate 2015 -2017 China ADS-B Out NRA Trials Japan R&D Asia/Pacific ICAO ADS-B Implementation Task Force Ground infrastructure and procedures development ITP Pacific Ocean ATSA-ITP FAA GATI Australia ADS-B out Rule 2008 Mandate 2013 © 2010 Rockwell Collins, Inc. All rights reserved.

Presentation Outline • Overview • ADS-B Out • ADS-B In and GNSS Requirements ©

Mandate Summary (DO 260 B) • Europe - Forward Fit Mandate January 2015 – Retrofit Mandate now February 2017 or 2018 • 1 or 2 year slip ANSP readiness (ground systems and integration) is the core issue! • Australia Upper Airspace (DO 260 ) – Voluntary, though separation services being provided today – December 2013 Upper Air Space Mandate • SA Aware GPS Sensors will be required • For forward fit only • Canada Hudson Bay & areas with limited SSR coverage (DO 260) – November 2010 Exclusionary Airspace • 5 NM separation services being offered – No plans for a 260 B mandate • US DO 260 B mandated by 2020 • No FF to RF segmentation – 100% equipped rule © Copyright 2011 Rockwell Collins, Inc. All rights reserved. 3

GPS Requirements for DO 260 B Mandate • Europe – The European Rule asks for (E)TSO-129 A as a minimum – SA=ON is acceptable • Though SA=OFF (Aware) is preferred • Canada – SA=ON is acceptable • Though SA=OFF (Aware) is preferred • United States Though not stated! Likely will require GPS – A GPS receiver that is SA Aware will be necessary With WAAS. A reading • FAA requirement is for a NACp of 8 of AC 90 -ADS-B is • 100% availability along enroute will determine GPS requirements required? • The quick summary of SA=Off/AWARE or SA=ON – – Australian rule will require SA Aware forward fit (2017) FAA rule will require SA Aware at a minimum Europe recommends SA aware (doesn’t require) Canada recommends SA aware (doesn’t require) © Copyright 2011 Rockwell Collins, Inc. All rights reserved. 4

ADS-B Transponder TCAS / Traffic Computer Current Surveillance Environment Secondary Surveillance Radar Mode A /C Mode S Altitude 4096 Code ACFT Addr Elementary Mode S Flight ID Surveillance ID Enhanced Mode S Selected Alt TAS Mach No IAS Mag Hdg GS Roll Angle VS Track Angle Rate ISS-2100, TPR-901 TSS-4100, TDR-94 D ADS-B Out ADS-B In Extended Squitter ADS-B In Applications Position Velocity Flt ID, etc DO 260 or DO 260 B SA=OFF GPS Sensor GLU-920 or GLU-925 GPS-4000 S © Copyright 2011 Rockwell Collins, Inc. All rights reserved. • Receive • Merge TCAS & ADS-B Targets • Surface Ops • In Trail Climb Procedures • Visual Separation on Approach • Sequencing & Merging • Etc. ISS-2100, TTR-2100 TSS-4100, TTR-4100 5

ARINC 718 A-3/4 Update - An indication of the changes • The development of DO-260 B has required additional changes and more inputs into the transponder – GPS Antenna Position to support POA • Requires about 32 states for ~ 2 meter accuracy – Other installation related issues are being addressed in the A 718 -4 work Current 718 A-2 Program Pin Utilization © Copyright 2011 Rockwell Collins, Inc. All rights reserved. Minor changes are being incorporated in 718 A-4 6

Some Pretty Pictures © Copyright 2011 Rockwell Collins, Inc. All rights reserved. 7

ADS-B Out © Copyright 2011 Rockwell Collins, Inc. All rights reserved.

TDR-94 D Transponder – Design Features Functionality • • • Elementary and Enhanced Surveillance Compliant – RTCA DO-181 C ADS-B Extended Squitter DO-260 A Change 2 A Hardware • RTCA DO-160 D Compliant Software • DO-178 B Level B Software Design TDR-94 D © Copyright 2011 Rockwell Collins, Inc. All rights reserved.

TPR-901 - Federated Transponder • 822 -1338 -021 (Airbus) 822 -1338 -003 (Boeing) • 822 -1338 -004 (B 747 -8 Only) • 822 -1338 -225 (Airbus) and -205 (Boeing) – – – – Elementary Surveillance & Enhanced Surveillance ADS-B Out DO-260 (Extended Squitter) DO-181 C and JTSO 2 C 112 b Interface standard ARINC 718 A or 718 -4 DO-160 D For Boeing aircraft SB 503 creates more robust filtering to eliminate position jumping issue. It converts a -003 to a -005. Elementary Surveillance & Enhanced Surveillance ADS-B Out DO-260 A Change 2 (Extended Squitter) TSO C 166 Updated to DO-181 D (ED-73 C) and TSO C 112 c (ETSO C 112 c) DO-160 D Elementary Surveillance & Enhanced Surveillance ADS-B Out DO 260 B TSO C 166 b DO-181 E (ED-73 C) and TSO C 112 d (ETSO C 112 c) Interface standard 718 A-4 DO-160 G DO 260 B Development Underway. Certification planned for 3 rd Qtr 2013 © Copyright 2011 Rockwell Collins, Inc. All rights reserved.

Integrated Transponder • Business and Regional Aircraft TSS-4100 -4 MCU TCAS, Traffic Computer, XPDR • Air Transport Aircraft ISS-2100 -8 MCU TCAS function/Traffic Computer Transponder, Weather Radar and Terrain Warning functions DO 260 -B 4 th Quarter 2013 © Copyright 2011 Rockwell Collins, Inc. All rights reserved. 11

ADS-B In (Traffic Computer) © Copyright 2011 Rockwell Collins, Inc. All rights reserved.

TCAS with Traffic Computer Summary Next Generation TCAS and Traffic Computer Product Line Developments – TTR-2100 is Plug and Play with the TTR-921 – All products are Traffic Computer Capable – Using a common traffic computer architecture – Product line ADS-B In applications development • Though will require display customization for each aircraft type TSS-4100 -4 MCU TCAS, Traffic Computer, XPDR TTR-4100 Business, Regional & Helicopter aircraft -4 MCU TCAS, Traffic Computer, TTR-2100 -6 MCU Federated TCAS II Traffic Computer ISS-2100 -8 MCU TCAS function/Traffic Computer Transponder, Weather Radar and Terrain Warning functions Airbus/Boeing in Production Aircraft Common Traffic Computer and Traffic Apps. Boeing 787/C 919 Common Traffic Computer Design enables re-use of ADS-B In Applications © Copyright 2011 Rockwell Collins, Inc. All rights reserved. 13

TTR-921 versus TTR-2100 Physical Changes TTR-921 Front View © Copyright 2011 Rockwell Collins, Inc.

Fusion Symbology Evaluation The Complexity and Difficulty of Displaying Aircraft Targets © Copyright 2011

Fusion Symbology Evaluation Selected -No Flight ID -Data Block Displayed © Copyright 2011 Rockwell

Fusion - TCAS RA Event Fusion Symbology Evaluation TA Symbol with directionality RA Symbol with directionality -TBD/Under study © Copyright 2011 Rockwell Collins, Inc. All rights reserved. Focus on TCAS event -Minimize ADS-B Information 17

Airport Surface with Traffic ANZ 139 Range: 3 NM Speed: 150 KTS Selected Aircraft

GNSS Requirements © Copyright 2011 Rockwell Collins, Inc. All rights reserved.

GLU Status • Current GLU-925 (SA = Aware) • • • ILS (Category IIIB) Compliant with DO-229 D (without SBAS) – TSO 145 A without SBAS Provides NIC ≥ 7 (99. 9% availability) Accommodates Category I GLS • GLS Category I Certified on Airbus & Boeing aircraft Supports SIL = 3 for ADS-B Out • System Integrity Limit FLS (FMS Landing System) Capability • Airbus platforms only • Current GLU-920 (SA = On) – ILS (Cat IIIB) – Compliant with TSO-C 129 A • SA=On – SA=Off Service Bulletin available today (Boeing) • Compliant with TSO-C 129 A • Will provide NIC ≥ 7 (99. 9% availability) • Will not accommodate SBAS, GLS, or Galileo • Upgrade of GLU-920 to GLU-925 – SB 503 converts 920 to GLS 925 (Boeing) – SB 504 converts 920 to Non-GLS 925 (Boeing) – SB 505 converts the 920 to SA=Off (Aware) GLS = GNSS Landing System GLU = GNSS Landing Unit SA = Selective Availability SB = Service Bulletin TSO = Technical Standard Order A 350 Will Integrate SBAS (WAAS) Capability into the MMR © Copyright 2011 Rockwell Collins, Inc. All rights reserved. 20