Transcript Automatic Dependent Surveillance-Broadcast (ADS-B)

Federal Aviation
Administration
ADS-B Out Avionics
Equipage &
Installation Guidance
Presented to: HAI Expo Meeting
Presented by: Tim Shaver (AFS-360)
John Fisher (AIR-132)
Date: March 03, 2015
Agenda
Tim Shaver (AFS-360) (Flight Standards)
• Equipage Update
• STC/TC Approvals
• Field Approvals
• ADS-B Focus Team
John Fisher (AIR-132) (Surveillance Policy)
• ADS-B Compliance Monitor
• Post Installation Performance Statistics
• Common Installation Issues
• Wrap Up
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Equipage Update
NEED AND UPDATE
FOR THIS SLIDE
8000
9663 total includes US & foreign V2 equipped aircraft
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Equipage Update
Approx: 8995 US Aircraft Equipped (2/24/15)
GA
Biz
5%
Commercial
Helo
4%
10%
81%
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FAA-Approved V2 ADS-B Out Avionics, 1 of 4
as of 23-Feb-2015
Surveillance
Manufacturer
Model #
Exelis /
FreeFlight
FDL-978TXG
ACSS
XS-950
* multiple STC dates; only earliest shown
Approved Position Source(s)
RCI GLU-920 , RCI GLU-925
RCI GLU-920
Thales TLS8755-01-0101A/0102B
RCI GPS-4000S
Aircraft
Approval Date
AML
Approved
VEHICLE
May 2012
Massport
767, 747, A300, MD11
A320
A330
757
STC Jan 2012*
STC Jul 2012
STC Aug 2012
STC Jul 2014
Yes
No
No
No
XS-852
CMC CMA-4024-1 SBAS
Embraer 145, Learjet
45, Hawker 800, and
Citation X
Jan 2012
No
Trig-Avionics
TT-31
FreeFlight WAAS 1201
Accord Technology NexNav™ Mini
Garmin GNS 400W/500W series
Trig TN70
Mooney M20B-M20G,
M20J & M20K
STC May 2012*
Yes
FreeFlight
FDL-978TX
FreeFlight WAAS 1201
Agusta Westland 139
Cessna 172S
STC Jun 2012*
No
Yes
Honeywell
ISP-80A.1
Honeywell ADIRU Part#’s
HG2030BE02, BE03 or BE04
A380
EASA TC
Jul 2012
Yes via
Production
FreeFlight WAAS 1201
King Air C-90A,
Aviat/Pitts (aerobatic)
S-76A/B/C (all
variants)
STC Nov 2012*
No (King Air)
Yes (Pitts)
No (S-76x)
Honeywell
Trig-Avionics
TT-22
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FAA-Approved V2 ADS-B Out Avionics, 2 of 4
as of 23-Feb-2015
Surveillance
Manufacturer
Garmin
* multiple dates; only earliest shown
Model #
Approved Position Source(s)
GDL-88
GTX-23
GTX-33x w/ES
GTX-330x
GTX-3000
Garmin GTN 625/635/650,
GTN 725/750, GPS 400W,
GNC 420W/420AW, GNS
430W/430AW, GPS 500W/530W
(w/ or w/o TAWS)
(GTX models require
appropriate S/W rev)
(all require appropriate S/W rev)
Approval Date
AML
Approved
STC Dec 2012*
Yes
Multiple
Gulfstream
models^
TC amendment
Dec 2014
Yes via
Production or
Aircraft Service
Change (ASC)
Aircraft
King Air C-90
Honeywell
MRC XPDR
w/ADS-B Out
CMC CMA-3024 SBAS GNSSU
MK II and
CMA-4024 SBAS GNSSU
Agusta
Westland 139
EASA TC
Feb 2013
Yes via
Production
Honeywell
XS-858B
P/N 7517402-970
Honeywell GPS module (made
by CMC), P/N 245-604067-100
Gulfstream
450/550
TC amendment
Feb 2013
Yes via
Production or
ASC
Falcon
Mar 2013*
No
Falcon F7X
Apr 2013
No
King Air C-90
STC Apr 2013
No
Honeywell
FreeFlight
XS-858B
P/N:7017401-970
FDL-1090-TX
CMC GNSS/MMR, P/N 245604067-100
Honeywell GNSS/MMR VIDL-G,
P/N: 7026208-804
FreeFlight WAAS 1201 (either
external or integrated in FDL978-XVR)
2000EX/S,
F900X
^ these are “dual out” installations (ADS-B Out on both UAT and 1090) of GDL-88 and GTX-330
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FAA-Approved V2 ADS-B Out Avionics, 3 of 4
as of 23-Feb-2015
* multiple dates; only earliest shown
Surveillance
Manufacturer
Model #
Approved Position Source(s)
Aircraft
FDL-978-XVR
FreeFlight WAAS 1201 (either
external or integrated in FDL978-XVR)
Bell-206
FreeFlight
Fixed Wing
N/A
N/A
Feb 2014
No
S-92A
TC Feb 2014
Yes via Production
S-76C, S-92A
STC Mar 2014*
No
Approval Date
AML Approved
No
STC Feb 2014*
Yes
Avidyne
AXP340
Rockwell
TDR-94/94D550/551
Universal UNS-1Fw
BendixKing
KT-74
Accord Technology NexNav™ Mini
FreeFlight WAAS 1201
GNS 400W/500W series
M20C
STC Mar 2014
Yes
Honeywell
KXP 2290A
Honeywell KGS200
PC-12/47E
EASA TC
Apr 2014
Yes via Production
NavWorx
ADS600-B
Accord Technology NexNav™ Mini
Piper
PA-32RT
STC Jun 2014
Yes
Rockwell
TDR-94/94D501
N/A
N/A
Oct 2014
N/A
Rockwell
TSS-4100
N/A
N/A
Oct 2014
N/A
Note:“N/A” indicates equipment has received TSOA, but has not received any other certification
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FAA-Approved V2 ADS-B Out Avionics, 4 of 4
as of 23-Feb-2015
* multiple dates; only earliest shown
Surveillance
Manufacturer
Model #
Approved Position Source(s)
Aircraft
Approval Date
AML Approved
ACSS
NXT-800
RCI GLU-925
767
TC Nov 2014
Yes via Production
Garmin
GTX-330ES
Garmin GNS-430W
AS350
Dec 2014
No
L-3 Aviation
Products
NGT-2000/2500
Integrated in NGT-2000/2500
only
Cirrus SR-22
Jan 2015
Yes
Note:“N/A” indicates equipment has received TSOA, but has not received any other certification
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FAA-Sponsored Projects that will result in
Version 2 ADS-B Out Avionics
Surveillance
Manufacturer
Model #
FreeFlight
FDL-978XVR
Rockwell
TPR 901205
Planned Position
Source(s)
FreeFlight WAAS
1201 (either external
or integrated in FDL978-XVR)
RCI GLU 925-001
RCI GLU 925-330
Aircraft
Planned STC
Availability
Operator
Rotorcraft
models other
than Bell 206
Mid-2015
Approximately
40 rotorcraft in
Alaska
737-700/800/900
(aka “737NG”)
Boeing Service
Bulletin Q1 2016*
United
Boeing provided UAL with a Service Bulletin to wire 737NG for ADS-B Version 2 in 2013; UAL has wired 45
aircraft as of 28-Oct-2014 and plans to have 51 aircraft wired by 31-Dec-2014
All Boeing production aircraft have wiring provisions installed for ADS-B Version 2 as follows:
737NGs beginning with Line Number 4522 (YS115, 03-Jun-2013)
747-8 beginning with Line Number 1490 (RC510, 07-Oct-2013)
767 beginning with Line Number 1063 (VT558, 10-Oct-2013)
777 beginning with Line Number 1132 (WE166, 01-Aug-2013)
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FAA-Approved Version 2 ADS-B In Avionics
as of 23-Feb-2015
* multiple dates; only earliest shown
Manufacturer
Model #
Aircraft
STC Date
AML Approved
Honeywell
TPA-100B
B747-400
June 2011
No
Honeywell
TPA-100B
A330/340
A318/319/320/321
Dec 2011**
Yes via Production
ACSS
TCAS3000SP
A330/340
A318/319/320/321
Dec 2011**
Yes via Production
ACSS
TCAS3000SP
B767-300, A330
May 2012*
No
Garmin
GDL-88
King Air C-90
Dec 2012
Yes
NavWorx
ADS600-B
N/A
Jul 2013
No
FreeFlight
FDL-978-XVR
Bell 206
Fixed Wing
STC Feb 2014*
No
Yes
L-3 Aviation
Products
NGT-2000/2500
Cirrus SR-22
STC Jan 2015
Yes
Note:“N/A” indicates equipment has received TSOA, but has not received any other certification
**Airbus ATSAW (with and without ITP) received EASA approval in May 2011 as TC amendment; all
A330/340s produced since Jan 2011 and all Airbus single-aisle aircraft produced since mid-2011 are
ATSAW/ITP-capable
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FAA-Sponsored Projects that will result in
Version 2 ADS-B In Avionics
Manufacturer
Model #
Aircraft
FreeFlight
FDL-978XVR
Rotorcraft
models other
than Bell 206
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Planned STC
Availability
Mid-2015
Operator
Approximately 40
rotorcraft in Alaska
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Field Approval (Policy Memo)
• Previous ADS-B policy restricted approvals
for ADS-B Out systems to:
– Type Certificate (TC)
– Amended TC
– Supplemental Type Certificate (STC)
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Field Approval (Policy Memo)
• Current policy memo allows for field
approvals under specific conditions
– Released October 10, 2012
– ADS-B Installation Policy Memorandum can be
found on the FAA Regulatory and Guidance Website
http://rgl.faa.gov/Regulatory_and_Guidance_Library/rg
Policy.nsf/0/A80D6DB0C3EE5ABA86257A940057FAC
8?OpenDocument&Highlight=ads-b
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Field Approval (Policy Memo)
• In order to obtain a field approval the
applicant must ensure:
– The ADS-B Out equipment (1090ES/UAT), GNSS
position sensor, and interconnect wiring are identical
to previously approved design under TC, amended
TC, or STC
– The installation is performed in accordance with the
equipment manufacturer’s installation guidance
– The installation is performed in accordance with AC
20-165A Chapter 3 and 4
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Field Approval (Policy Memo)
• All other aspects of the installation qualify
for installation under 14 CFR part 43
• ADS-B installation policy memo released
Oct 10, 2012 supersedes all previous
versions
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AFS ADS-B Focus Team (AFT)
• AFT Overview:
– Foster the consistent interpretation and application of
ADS-B related regulations, policy, and guidance to
support effective and efficient equipage and continuous
compliance of avionics performance standards
– Comprised of HQ SMEs from AFS, AIR and ATO
• AFT Activities:
– Provide SME support to FAA field offices and aviation
community during ADS-B mandate equipage
– Coordinate resolution of issues arising during avionics
installation approvals
– Collaborate with manufacturers to address installation
and avionics performance issues
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John Fisher (AIR-132)
• ADS-B Compliance
Monitor
• Post Installation
Performance Statistics
• Common Installation
Issues
• Wrap Up
Federal Aviation
Administration
ADS-B Compliance Monitor
• Primary purpose
– Support FAA Flight Standards with compliance &
enforcement of 14 CFR §91.225 and §91.227
– Monitor & record all ADS-B Out aircraft operations in
the NAS & generate reports based on compliance of
§91.227 requirements
• Secondary purpose
– Support installation testing
– Support aircraft certification test flight process for
new approvals
– Monitor ADS-B equipage and growth
– Support avionics performance trend analysis
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ADS-B Compliance Monitor
• Generates two types of reports
– Compliance reports
– Certification reports
• Compliance report for field approvals and post
installation performance certification
– E-mail: [email protected]
• Certification report for certification of ADS-B
systems per AC 20-165A section 4-3 a (1)
– E-mail: [email protected]
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ADS-B Compliance Monitor
• Organizes ADS-B data into flight operations
• Generates compliance reports for all ADS-B
monitored operations
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ADS-B Compliance Monitor
• Identifies aircraft that do not comply with
equipment performance requirements in
§91.227
– Checks integrity & accuracy of positioning §91.227(c):
• Compliant NIC, NACp, NACv, SIL, SDA
• Validation also performed against primary and secondary
surveillance systems
– Checks for required message elements §91.227(d):
• Lat/long, velocity, baro & geo alt, Mode 3/A, Flight ID, ICAO
24-bit address, Emitter Category, Length/Width code, etc.
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ADS-B Compliance Monitor
• Performs reasonableness checks
(Kinematics) on position, velocity, altitude
• Identifies Flight ID, Mode 3/A, and Mode S
address issues/mismatches
• Accumulates ADS-B OUT/IN equipage data
• Assists in identifying issues common to a
manufacturer or part number
• A sample Compliance Report can be found
at the end of this presentation (click here)
• Provides graphic representation of data
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ADS-B Compliance Monitor
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ADS-B Compliance Monitor
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ADS-B Compliance Monitor
• When is a failure not a failure?
– FAA-provided ADS-B Aircraft Operation Compliance
Report may highlight failures of 0.1% - 2.0% in red.
These seem to be related to brief data dropouts due
to maneuver induced antenna shading.
– IF these are not deemed as system failures
corrective action may not be required
This content provided by: Garmin
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ADS-B Compliance Monitor
• When is a failure not a failure?
– Altitude source turned off during flight? The CM will
report no Baro Alt and likely an associated integrity
failure
This content provided by: Garmin
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Post Installation Performance Statistics
• Approximately 20% of rule equipped aircraft
do not fully comply with §91.227 equipment
performance requirements
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Common Installation Issues
• Mode 3/A issues, no transmit or UAT code
disagrees with transponder code
– Majority are GDL 88s with UAT Call Sign ID Logic
disabled
• Missing Flight ID
– Not entered during install or by pilot on subsequent flts
• Software compatibility
– Can cause multiple issues including non-compliant
SIL/SDA/NIC/NACp/NACv
– Ensure transmitter & GPS software are at correct
version level following installation
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Common Installation Issues
• Emitter category
– High number of “Light” aircraft (<15,500 lbs.) are
configured to transmit as “Small” (>15,500 lbs.)
– Emitter category 6 (High Performance) is for fighters
• Baro/Geo drop/spike
– Installation error fixed with software coding
• Mode S address errors
– Results in “No Data Found” when requesting CM
report for specific N-number
– Entry errors during initial configuration, Owner/Nnumber change
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Common Installation Issues (Mode 3/A)
• GDL 88 UAT Call Sign ID Logic Configuration
– The GDL 88 Call Sign ID Logic must be enabled,
allowing the pilot-entered Mode 3/A Code to be
transmitted. If not enabled, the Compliance Report
will indicate a Mode 3/A failure of 100%*
* = In dual band installs GDL 88 UAT plus GTX w/ES transponder, failure may be only 50%
This content provided by: Garmin
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Common Installation Issues (Mode 3/A)
• GDL 88 UAT Call Sign ID Logic Configuration
– For GDL 88 and GTN 6xx/7xx installations
• The UAT Call Sign ID Logic is enabled in the GTN’s
Configuration Mode
– For other GDL 88 installations
• The UAT Call Sign ID Logic is enabled using Garmin’s PC
Install Tool
This content provided by: Garmin
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Common Installation Issues (SW)
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Common Installation Issues (SW)
2300 feet
8/10/1/3/2
18:05:59.535
NIC:8 NACp:10 NACv:1
SIL:3 SDA:2
Balt:5675ft / Galt:2525ft
Failed:
- Integrity / Accuracy
- Kinematic Checks
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Common Installation Issues (Baro)
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Common Installation Issues (Baro)
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Common Installation Issues
• Aircraft reporting wrong ICAO addresses
• Go to: http://registry.faa.gov/aircraftinquiry/
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Common Installation Issues
• Aircraft reporting wrong ICAO addresses
Be sure to always use Hex
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Common Installation Issues
• The majority of compliance failures that we
have seen thus far have been caused by
improper configuration of the equipment
• There are two transponder settings and one
UAT setting that are frequently
misconfigured
• The incorrect settings usually result in a
100% failure rate of one of the performance
criteria, and hence are easy to identify
This content provided by: Garmin
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Common Installation Issues
• GTX 23/33/33D/330/330D w/ES GPS Source
Configuration
– The RS-232 serial output of the Garmin GTN 6xx/7xx
unit or GNS 4xxW/5xxW must be configured to one of
the special ‘+’ formats to provide compliant GPS source
data. If not, the Compliance Report will indicate failure*
of NIC, NACp, NACv, NIC_SVT, and NACp_SVT
* = In dual band installs GDL 88 UAT plus GTX w/ES transponder, failure may be only 50%
This content provided by: Garmin
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Common Installation Issues
• GTX 23/33/33D/330/330D w/ES GPS Integrity
Configuration
– The transponder GPS Integrity config setting must be
1E-7 when the transponder is connected to a GTN
6xx/7xx unit or a GNS 4xxW/5xxW unit. If configured
wrong Compliance Report will indicate 100% SIL failure*
* = In dual band installs GDL 88 UAT plus GTX w/ES transponder, failure may be only 50%
This content provided by: Garmin
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Common Installation Issues
• Corrective Actions
– FAA, (AIR, SBS and AFS), providing information,
supporting outreach programs related to ADS-B
• Support seminars/briefings @ trade & industry events
• Coordination of related articles in trade & industry
publications
• https://www.faa.gov/nextgen/implementation/programs/adsb/
– ADS-B Avionics Check
• [email protected]
– Investigate compliance issues worked as a team effort
• Operators and installers contacted by AFS
• Manufacturers contacted by AIR
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Wrap Up
Tim Shaver (AFS-360)
• Equipage Update
• STC/TC Approvals
• Field Approvals
• ADS-B Focus Team
John Fisher (AIR-132)
• ADS-B Compliance Monitor
• Post Installation Performance Statistics
• Common Installation Issues
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Questions?
Jim Marks
Aviation Safety Inspector (Avionics)
ADS-B Focus Team Lead
Flight Standards Service, Avionics Branch (AFS-360)
[email protected]
John Fisher
Transportation Industry Analyst
Systems and Equipment Standards Branch (AIR-132)
[email protected]
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Back up slides – Useful Links
• Regulation and Guidance Library:
– http://rgl.faa.gov/
• Compliance report (post installation)
– [email protected]
• Certification report (first of kind)
– [email protected]
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Back up slides – Sample Report Page 1 - 2
Click here to return
to slide 22
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Back up slides – Sample Report Page 3 - 4
Click here to return
to slide 22
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Back up slides – Sample Report Page 5 - 6
Click here to return
to slide 22
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