18 November 15 | Start Time – End Time (3:00 – 4:30pm)
PRESENTED BY:
Arnold Oldach / Gary Heckler

•   Quick Summary of near term world wide mandates
•   ADS-B Overview and Implications
•   Mandates and AIPs
•   Reminder of what’s a Transponder
•   ADS-B Summary and current compliance conditions
•   SA=ON vs SA=OFF (AWARE)
•   What is FANS
•   The Components and Implications
•   Falcon 2000 Configurations and considerations
•   How to get to FANS
•   How to get to ADS-B
•   Rockwell Collins Falcon 2000/EX Summary
2

Prior- years 2013 2014 2015 2016 2017 2018 2019 2020+
Link 2000+ Mandate ( ATN Baseline 1)
-ANSP Readiness is now February 2018
-Retrofit and Forward Mandate are now Feburary
2020
-Eurocontrol has posted exemption list.
FAA CVR Datalink Recording
-April 2012 for Part 91
-When ATC datalink upgraded
ANSP Readiness: February 2018
NAT Region – FANS 1/A
-February 2013
-Two Core Tracks: FL360 – FL390
NAT Region – FANS 1/A
-February 2015
-All Tracks: FL350 – FL390
NAT Region – FANS 1/A
-December 2017
-All NAT Region: FL350 – FL390
NAT Region – FANS 1/A
-January 2020
-All NAT Region: FL290 and Above
3

Prior- years 2013 2014 2015 2016 2017 2018 2019 2020+
Gulf of Mexico
ADS-B Out Helos
Hudson Bay
FL 350 - FL400
Australia
Retrofit FL290
SIN + Indonesia
Retrofit FL290
Hong Kong
PBN Routes-FL290
Hong Kong
HKG FIR-FL290
Australia
SA Aware GNSS
Europe
Forward Fit
Retrofit
US
F/F and Retrofit
Mexico
F/F and Retrofit
DO-260A or B
DO-260 or B
DO-260, A or B
DO-260, A or B
DO-260, A or B
DO-260, A or B
DO-260B TSOC 129 SA=ON allowed
DO-260B SBAS (TSO C145) GNSS preferred, SA=AWARE allowed, SA=ON requires use of SAPT Tool
DO-260B Proposed: Follows US Mandate Requirements, including UAT for GA <18,0000 4

ADS-B Overview and Implications

n
Retrofit  mandates:
•   Hudson  Bay:    Dec  2012
•   Australia:    02  Feb  17,  all  IFR  flights/all   flight  levels
•   China  TesVng  (Shanya  FIR  L642/M771)
•   Hong  Kong:    Along  L642/M771  today,   delayed  phase  2  (all  areas)  –unVl  08  Dec  16
•   Singapore:    12  Dec  13  (Select  Airways)
•   Europe:    7  Jun  20
•   Indonesia:    25  Jun  15
•   Sri  Lanka:    01  Sep  15
•   Taiwan:    Now  31  Dec  16
•   Vietnam:    12  Dec  13  (Select  Airways)
•   India  (Aerion  ADS-­‐B  underway)
•   Mexico  (2020):    Plan  to  follow  US  Model
Resources
AIP-­‐Canada
ACAO  82.1,  3,  5
NOTAM
(AIC)  09/11 ,
AIC  14/10  ,  AIP  SUP  254/13
AIP  Sup  10/14
AIC    A02/14
AIP  Sup  08/14
AIP  Sup  A09/13
•   Forward  Fit  mandates:
–   Europe:    0  8Jun  16
–   Australia:  Dec  2013
–   US:      Jan  20  (FF  and  R/F)

A
T
Mode S Mode A Mode C DO-260 DO-260A
4 digits ID
4 digits ID
Altitude
Flight ID
Selected altitude
Mach number
Roll angle
Track angle
Track angle rate
TAS/IAS/GS/VS
MODE S
(ELS and EHS)
GPS position
Flight ID
Velocity
NUC
GPS position
Flight ID
Velocity
NIC and NACp
DO-260B
GPS position
Flight ID
Velocity
Changed how
NIC, NACp and SIL are set
Length/Width
…

ADS-B
A UTOMATIC D EPENDENT S URVEILLANCE
•   Flight Number
•   Position
•   Relative Altitude
•   Vertical Tendency
•   Distance
•   Heading
•   Ground Speed
•   Indicated Air Speed

S
ADS-B A
6600  a/c   4400  a/c   1000  a/c   2100  a/c
•   Transponder Demand
–   Estimated Demand based on dual installation - 85,736 transponders
•   Translates into over 40,000 transponders to upgrade or replace
–   GPS Issues for US need to be addressed
•   Though there is now an exemption
–   FAA is forecasting over 150,000 aircraft including GA
Es#mated  Fleets
Air  Transport
Regional
Business
Military
Transport/Tankers
Aircrab  Est.
Ac#ve  A/C
14,  100
6,939
16,684
5,145
42,868
The mandate is TODAY! There are approximately 1,500 days left until January 2020.

W
’
U
10.6%
Haven’t Given Much
Thought
26.8%
Thinking About
Preparing
26.8%
Compliance
Planned &
Budgeted
22.1%
13.7%
Compliance is a work in progress
Compliance is complete
10
Source - Honeywell

What is FANS 1/A

•   Context Management Application (CMA)/ATC Facilities Notification (AFN)
•   Aircraft announces to ATC Facility readiness to begin data link communication
•   Provides aircraft information and capability to ATC Facility
•   Establishes Agreement on services, features, functions and requirements
•   Facilitates ATS communication across FIR boundaries

•   CPDLC is the application that contains the actual uplink and downlink messages used between the pilot and the controller
•   Text messages (Pilot to controller interchange
–   Confirm Assigned Level, Estimate Time Arrival (ETA), Descend to XXX FL, etc
•   Loading uplinks to FMS flight plan
•   Routes and route modifications
–   Direct clearances
–   Offset clearances
–   Crossing constraints Integrated
Application in FMS
•   Validation of data in requests
–   Against route / navigation data base
•   Validation of uplinks
–   Against route / Navigation data base
Please note: the list of message above are examples, but not the complete list.

•   Automatic Dependent Surveillance – Contract (Automatically Generated by the FMS)
•   Periodic Contracts
–   Content—Basic ADS Group and any number of On-Request Groups
–   Interval—64 seconds to over an hour (1:08:16)
•   On-Request Groups
–   Included at specified reporting intervals
–   Each On-Request Group may be included at different intervals
•   Event Contracts
•   Waypoint Change
•   Lateral Deviation
•   Basic Group Content
Altitude Range Change
Vertical Rate Change
–   Aircraft Current 4-D Position
»   Latitude, Longitude, Altitude, Time at which position was determined
–   Figure of Merit
»   Accuracy of position determination

What is Link 2000+
Protected Mode CPDLC / ATN Baseline 1 (ATN B1)

•   Link 2000+ Implementation
–   ATN applications are not integrated with the FMS
–   ACARS Router to support AOC (ACARS) Messages
•   ACARS Routing & mobility management
–   VDL Mode 2 Sub Network and ATN Router
•   ATN Routing & mobility management
–   CPDLC and CMA only
–   Sub-set of the ATN CPDLC Message set
–   65 CPDLC Uplinks
–   27 CPDLC Downlinks
•   Mandated Domestic European Airspace
–   Designed to be implemented on large number of aircraft
–   FMS Integration not considered
–   Implemented to deal with immediate ATC Voice congestion
FMS Integration is not required.

•   Messages are categorized into four main groups
1.
Data Link Initiation Capability (part of Context Management)
•   Provides the necessary information to establish a connection and enable CPDLC
2.
ATC Communication Management (ACM)
•   Provides automated assistance to the aircrew and controllers for transferring ATC communications from one sector to another
3.
ATC Clearances (ACL)
•   Enables the controller to send ‘strategic’ en-route clearances for altitude, heading, speed, direct route, and rate of climb
•   Provides the crew with the capability of requesting deviations in altitude, heading, speed
4.
ATC Microphone Check (AMC)
•   Provides controllers with the capability to uplink an instruction to the aircraft to check that they are not inadvertently blocking a given voice channel

How to Get to FANS and Link 2000+

•   For FANS 1/A
–   Upgraded FMS to provide ADS-C capability
•   Might include MCDU and Display System Upgrade
–   Communications Management Unit
•   Which enables Datalink Routing and Messaging
–   Dedicated VHF Radio connected to CMU and Audio Control Panel
•   For Domestic US FANS the FAA wants you to have a VHF Data Radio
(VDR) which is VDL Mode 2 compliant
–   Satcom System (Iridium, Aero H+, SBB) for Oceanic Operations
–   Datalink Recording Rule – Though an exemption for some aircraft
•   Flight Plan Filling requirements, AFM updates, Crew Training
•   What to do with the datalink equipment beyond FANS and ATC Datalink?
–   Are there services that an ARINC or SITA may be able to provide over the datalink systems? 19

L
2000+ (PM CPDLC) B
•   Communications Management Unit
–   Capable of hosting both the ATN Router and PM CPDLC Applications
–   Capable of supporting the VDL Mode 2 VHF Data Radio Interface
•   Link 2000+ CMU Software
–   ATN Software
•   ATN Router
•   CPDLC Protected Mode
–   Datalink Recording capable
•   VHF Data Radio (VDL Mode 2)
–   Manufacturer specific and linked to CMU choice
•   MCDU / Pilot Interface Unit
–   Specific to aircraft type and upgrade path
•   TBD by Aircraft Manufacturer and/or datalink product vendor

Falcon 2000 Summary
Or What’s the Problem?

T
( THERE ’ S JUST NOT ONE CONFIGURATION )
1998 Falcon 2000
2006 Falcon 2000
2004 Falcon 2000

Some Examples of Offerings

(Through 3 rd Party Service Bulletins)
Iridium Satcom - CG 220A - FANS datalink and Satcom Voice
Install 1ea. ICG Iridium transceiver
Install 1ea. Iridium antenna
Install 2ea. ICG corded handsets
STC, Engineering, Installation, and Labor
Rockwell Collins Datalink System – For FANS Support
Install 3rd VHF-422 VHF Radio for datalink if required
Survey aircraft and install if needed, including audio control panel for 3 rd radio selection
Install 1ea. CMU-4000 or CMU-1000 Communications Management Unitt
Install 1ea. ECU Rockwell Collins configuration unit
STC, Engineering, Installation, AFM Updates, and Labor
24

Rockwell Collins WAAS/LPV is required for FANS
Collins FMC-6100 WAAS/LPV
Delete 2ea. Collins FMC
Delete 4ea. Display units
Delete 2ea. flight control computers
Delete 4ea. IOC cards
Delete 2ea. GPS antennas
Delete 1ea. PCD-3000 Data transfer Unit
Delete 2ea. GPS-4000A
Install 1ea. DBU-5010 Data Transfer Unit
• Install 4ea. IOC-4000 cards
• Install 2ea. FMC-6000 Flight Management Computers
• Install 2ea. GPS-4000S SBAS GNSS Sensor
• Install 2ea. GPS/WAAS antennas
• Install 4ea. EFD-4077 display units
• Install 2ea. FCC-4002 flight control
• STCs, Engineering, Installation, AFM Updates, and Labor
25

Rockwell Collins WAAS/LPV is required for FANS
If you are planning on WAAS /LPV FMS operations, then you may want to consider the following:
Collins AHRS-3000A
•Delete 1ea. AHC-85E - 3rd reference unit
•Install 1ea. AHC-3000A AHRS computer
•Install 1ea. ECU external compensation unit
•Install Labor, engineering, STC, 8110s, 337
Note: Recommend if either #1 or #2 IRS is lost, LPV approach not allowed. This AHRS upgrade provides for redundant operation
Aircraft is still not FANS compliant – Need FMS Integrated Package from Rockwell Collins.
But you can fly LPV approaches. And your GPS is FAA Mandate ADS-B Out compliant.

(FMS Integration and Aircraft Integration)
Rockwell Collins (Challenger 604 Example)
27

(FMS Integration and Aircraft Integration)
Rockwell Collins (Challenger 604 Example)
28

Rockwell Collins Marketing Bulletin: Ref. No. BRS-150183.01M
29

ADS-B Compliance
Third Party S/Bs are Possible

•   For ADS-B Out
–   Upgrade or replace the Mode S Transponder
•   Upgrades and replacement available from many manufacturers
•   Though replacements must be interoperable with your TCAS II system
–   GPS (GNSS) Sensor - Example: GPS-4000, 4000A are SA=ON
•   Either Replaced or file for exemption with the FAA
•   Though an SA=ON (GPS-4000/4000A) will require the use of the FAA
SAPT GNSS availability tool
•   Flight Plan Filing to indicate ADS-B Capable
–   Item 10B in the 2012 ICAO Flight Plan
•   Certified Installation Required
•   No LOA required
31

GPS E
S
•   For docket, applicants need to post their exemption requests here:
–   http://www.regulations.gov/#!docketDetail;D=FAA-2015-0971
•   The FAA Decision Memo is at:
–   http://www.regulations.gov/contentStreamer?
documentId=FAA-2015-0971-0010&attachmentNumber=1&disposition=attachment&con tentType=pdf
•   The exemption is number 12555

TCAS 7.1
Rockwell Collins has AML STC ST01794WI. This uses the TTR-4100.
RCI has several dealers getting EASA certification for the Falcon 2000.
ADS-B Out (DO-260B)
Dassault Falcon jet has a ADSB solution for Pro Line 4 and 21 aircraft using the Rockwell
Collins TDR-94D.
Rockwell Collins is in the process of updating our Pro Line 4 to 21 STC to
include integrated ADS-B annunciations.
STC update is coming soon.
FANS
Dassault Falcon jet is doing a FANS STC for the Falcon 2000 that are equipped with Pro
Line 21.
The solution is built around the Rockwell Collins CMU-1000.
33

Back Up

SBAS C
Source:  FAA
35

S
A
•   Intentional Degrading of SPS C/A Code for
Non-Military GPS Users
–   Controlled by the US Gov’t
•   Discontinued by Order of the US President
May 2 nd, 2000
•   All Non-Military Civil Aviation GPS
Receivers Prior to May 2 nd , 2000 Assumed the Error Would be Present (SA=ON)
–   Currently, better accuracy is being achieved, but receiver estimates of accuracy and integrity assume SA is on
•   SA=Off / SA Aware GPS Receivers. Aware of current status of SA
–   Higher availability
–   Better accuracy and integrity limits
Position In Commercial GPS
Before After
GPS Receivers that are “SA Aware” Provide Higher Availability of an Operationally
Required Level of Position Accuracy & Integrity Performance