[PDF] Display TCAS Fly-To Cue Update - Software Download Instructions





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Display TCAS Fly-To Cue Update - Software Download Instructions

The new FDSA-6500 and APCT-3700 software files may be obtained as described below Refer to Table 1 to reference existing/new FDSA-6500 and APCT-3700 part numbers • Initial delivery of the files will be electronic with the delivery of the Compact Disc (CD)s to follow approximately 2-3 weeks later

  • Summary

    The FAA is superseding Airworthiness Directive (AD) AD 2019-12-09 for certain Rockwell Collins, Inc. (Rockwell Collins) FDSA-6500 flight display system applications installed on airplanes. AD 2019-12-09 imposed operating limitations on the traffic collision avoidance system (TCAS). AD 2019-12-09 was prompted by conflict between the TCAS display ind...

  • Dates

    This AD is effective April 29, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 29, 2021.

  • Addresses

    For service information identified in this final rule, contact Rockwell Collins at Collins Aviation Services, 400 Collins Road NE, M/S 164-100, Cedar Rapids, IA 52498-0001; phone: (319) 295-9258; fax: (319) 295-4351; email: techmanuals@rockwellcollins.com; website: https://www.rockwellcollins.com/?Services and Support/Publications.aspx. You may vie...

  • For Further Information Contact

    Nhien Hoang, Aviation Safety Engineer, Wichita ACO Branch, FAA, 1801 Airport Road, Wichita, KS 67209; phone: (316) 946-4157; fax: (316) 946-4107; email: Nhien.Hoang@faa.gov or Wichita-COS@faa.gov.

  • Supplementary Information

    Background

  • List of Subjects in 14 CFR Part 39

    Air transportation

ServiceInf ormationLetter523-0826420-201000

ServiceInf ormationLetterFDSA-6500-19-1

REVISIONNO .2DISPLAYTCASFL Y-TOCUEU PDATE-SOFTWARE DOW NLOADINSTRUC TION S

TRANSMITTALINFORMATIONSUMMAR Y

S ummary Thisi srevis ion 2of Ser viceInformation Letter(SIL)FDSA-6500-19-1fortheFDSA-65 00Flight

DisplayS oftwareApplication.

Thisr evisio

n updatesSections D. andE.,andadds SectionF .

Blackbars in themargins indicatethec hange.

Replace revision1withthis re vision.

ServiceInformationLetterRevis

ionHistory

REVISIONDATEOFRELE AS E

InitialR eleaseJune3, 2019

Revision1June4, 2019

Revision2June12,201

ExportClassific ationNumberfort hisdocum entis7E994. DUE TOTHEU SG OVERNMENT'SI MPLEMENTATIONOFEXPORTCONTR OLREFORM(ECR),ALLEXPORT DA TAPRO VIDED IN THISPUBLIC ATIONISCURRENT ASOFTHE LASTREVISIONDATE ANDMAY BESU BJECT TOCH AN GEBYROCKW ELL COLLINS.T HEREFORE,PLEASEBEAD VISEDTHATY OUAR EENCOU RAGEDT OVALIDATE THEACCURACYOF THEDATA

PRIOR TOAN YFUTUREEXPOR TACTIVITYR ELATINGTOT HESEPUBLICATIONS.© 2019Roc kwellCollins.Allrights reserved.

Jun3 /19FDSA-6500-19-1

2-Jun12/19 Page1of10

Service Information Letter

Software License and General Conditions of Sale

For each software license procured, the Software License for Equipment Specific Software, reproduced below, shall apply.

Software License for Equipment Specific Software

Software delivered hereunder, either embedded in equipment described herein or specifically designed for use in or with such

equipment, is copyrighted by the seller and shall remain the sole and exclusive property of seller. Seller grants the buyer a perpetual,

worldwide, non-exclusive license to use the software only in or with the equipment. The buyer shall not copy, modify, or disassemble

the software, or permit others to do so. Buyer shall not transfer thelicense granted hereby or possessionof the software except as part

of or with the equipment, such transfer being subject to the restrictions contained herein. Seller may terminate this license upon written

notice for violation of any of the terms of the foregoing license.

Should the customer have any questions concerning the scope of permitted use, please contact your Rockwell Customer Service Engineer.

Rockwell Collins' General Conditions of Sale 074-8431-866 (Rev 04/15) are incorporated herein by reference.

Jun 3/19FDSA-6500-19-1

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Service Information Letter

A. Effectivity

The information in this SIL is applicable to the FDSA-6500 Flight Display Software

Application listed in the following table.

UNIT NOMENCLATUREROCKWELL COLLINS

PART NUMBER (CPN)

FDSA-6500 Flight Display Software Application810-0234-1H0001 FDSA-6500 Flight Display Software Application 810-0234-1H0002 FDSA-6500 Flight Display Software Application 810-0234-1H0003 FDSA-6500 Flight Display Software Application810-0234-2C0001 FDSA-6500 Flight Display Software Application 810-0234-2C0002 FDSA-6500 Flight Display Software Application 810-0234-2H0001 FDSA-6500 Flight Display Software Application810-0234-4B0001

B. Issue Summary

(1) The Traffic Collision Avoidance System (TCAS) Fly-To Cue indication on the primary cockpit dis plays may conflict with other TCAS system information (e.g. aural cues) during a Resolution Advisory (RA) scenario. Specifically, the TCAS Fly-To Cue vertical position on the Attitude Direction Indicator (ADI) pitch tape is displayed relative t o the aircraft horizon line instead of the aircraft symbol. The potential conflict between displayed indications and TCAS aural cues could adversely affect the pilot decision-making process and may lead the pilot to over/under-correct which may result in u nintended reduction in aircraft separation. (2) The TCAS Line Replaceable Unit (LRU) outputs are correct, and compliant with requirements, and the aural call-outs for the pilot are correct. The issue has been isolated to the FDSA-6500 software where the command data from the TCAS equipment is being translated incorrectly prior to display of TCAS Resolution Advisory pitch indications on the AFD-3700.

C. Replacement Effectivity

(1) The following table shows the replacement FDSA-6500 software CPNs for each version that is obsolete due to the TCAS non-compliance.

PLATFORM OBSOLETE CPN REPLACEMENT CPN

King AirC90, B200 & B300810-0234-1H0001810-0234-1H0101 King Air C90, B200 & B300 810-0234-1H0002 810-0234-1H0102 King Air C90, B200 & B300 810-0234-1H0003 810-0234-1H0103 PL II King Air B200 & B300810-0234-2H0001810-0234-2H0101

Jun 3/19FDSA-6500-19-1

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Service Information Letter

PLATFORM OBSOLETE CPN REPLACEMENT CPN

Cessna CJ3810-0234-2C0001

810-0234-2C0002810-0234-2C0102

Challenger CL-604810-0234-4B0001810-0234-4B0101

(2) For APCT-3700, ICIT-3700, and KIT-3700 software part numbers, refer to aircraft platform specific information in Section F.

D. Supplemental

Type Certificate (STC) and Service Bulletin (SB) Availability Notification will be sent to operators once the STCs and SBs are available. In the interim, contact the R ockwell Collins Customer Support Center to obtain status on the STC and/or

SB specific to each aircraft platform.

Rockwell Col

lins Avionics Support Center

319.295.5000

AvionicsSupport@Collins.com

E. Software Download Instructions

(1) Textron King Air C90, B200 and B300.

This sectio

n applies to Textron King Air Production delivered aircraft with Pro Line

Fusion

and King Air Pro Line 21 to Pro Line Fusion retrofit aircraft modified by Rockwell Collins STCs SA01769WI, SA01784WI, SA01792WI, and SA01857WI. • Both FDSA-6500 and Integrated Modular Avionics (IMA) Configuration Index Table (ICIT)-3700 software files will be available on the Textron portal (Refer to the foll owing instructions to download onto a Universal Serial Bus (USB)). Along with the required FDSA-6500 and ICIT-3700 software, a copy of the Certificate of Conformance (CoC) and/or Airworthiness Approval Tag (8130-3) will be ava ilable for each part number to support your installation.

Jun 3/19FDSA-6500-19-1

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Service Information Letter

• For both Textron Production delivered and retrofit King Air aircraft with Pro Line

Fusion

referto Rockwell Collins Approved Model List (AML) STC SA01922WI document number RCA-3158, Modification Instructions, refer to Table 1 to reference existing/new FDSA-6500 and ICIT part numbers. • Additionally , Textron Production delivered aircraft with Pro Line Fusion may refer to Textron SB MTB-34-02 for existing/replacement loadset. • The new FDSA-6500 and ICIT-3700 software may be obtained by accessing the Textron p ortal at http://txtavsupport.com and following the instructions. 1 . Log on to your customer account at http://txtavsupport.com. 2 . Once logged in, select the applicable King Air model on the left side of the page. 3 . Under "Avionics", select the link "Rockwell Collins Pro Line Fusion

Support".

4 . Use the pull down menus to find your model and serial number. 5 . Refer to Section F. for USB preparation and software load reference instruction s. N OTE:Additional instructions can be obtained in the following manuals.

PUBLICATION TITLE PART NUMBER

Pro Line Fusion

for King Air Aircraft

Maintenance Manual523-0824677

Pro Line Fusion

for Aftermarket Installation Manual523-0821905 B300 Aircraft Maintenance Manual 434-590169-0009 Rev B1 C90GTi Aircraft Maintenance Manual 434-590171-0009 Rev A3 B200GT Aircraft Maintenance Manual434-590168-0009 Rev B0 (2) Cessna CJ3. This section applies to all CJ3 aircraft updated via STC SA11219SC. The new FDSA-6500 and APCT-3700, software files may be obtained as described below.

Refer to T

able 1 to reference existing/new FDSA-6500 and APCT-3700 part numbers. • Initial delivery of the files will be electronic with the delivery of the Compact Disc (CD)s to f ollow approximately 2-3 weeks later. No Purchase Order (PO) will be required to obtain the CDs. • Updated software will be made available on the Rockwell Collins Aftermarket web portal fo r download onto a USB memory device. • Rockwell Collins Customer Support Engineers will reach out to each operator to ensure access to the web portal and walk them through the update.

• Refer to S

ection F. for USB preparation and software load reference instructions.

Jun 3/19FDSA-6500-19-1

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Service Information Letter

(3) Pro Line II to Pro Line Fusion

Retrofit King Air.

This section ap

plies to all Pro Line II King Air B200 and B300 aircraft that were updated via STC SA11136SC. The new FDSA-6500 and KIT-3700, software files may be obtained as described below. Refer to Table 1 to reference existing/new

FDSA-6500 and

ICIT part numbers.

• Initial delivery of the files will be electronic with the delivery of the CDs to follow approximate ly 2-3 weeks later. No Purchase Order (PO) will be required to obtain the CDs. • Updated software will be made available on the Rockwell Collins Aftermarket web portal for do wnload onto a USB memory device. • Operators should download and refer to the document titled "Pro Line II to

Fusion

King Air ICIT and Audio Storage & Playback Unit (ASPU) Software Config

Matrix.pdf"

, available on the web portal, to determine the specific files to be downloaded from the web portal for their aircraft. Please note that the KIT-3700 CD will contain all possible files, not just those for a specific aircraft. • Rockwell Co llins Customer Support Engineers will reach out to each operator to ensure access to the web portal and walk them through the update. • Refer to Section F. for USB preparation and software load reference instructions. (4) Challenger 604.
This section applies to all Challenger 604 aircraft that have been updated via ST04356CH. The new FDSA-6500 and ICIT-3700 software may be obtained as described b elow. Refer to Table 1 to reference existing/new FDSA-6500 and ICIT part numbers. • Operators should contact Nextant to obtain the aircraft service bulletin and have a USB memory device shipped to them. The USB memory device is a Parts Manufacturer Approval (PMA) approved part that is required in order to update the software o n the aircraft. The USB memory device has the same Part Number as the ICIT-3700 contained within it, which is NT0016-ICIT-0100-B. This device contains the software needed to update a Challenger 604 to resolve the TCAS

Fly-To Cu

e indication on the primary flight deck displays. • The instructions for installation on the aircraft are available in the aircraft service bulletin SB-31-2019-02. • Operator s should call Nextant Customer Support at 216.797.8416 to have the USB memory device mailed to them and to obtain instructions on how to download the aircraft service bulletin. • Refer to S ection F. for software load reference instructions.

Jun 3/19FDSA-6500-19-1

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Service Information Letter

F. Software Installation Instructions

Prepare USB and install software as follows:

• Identify the IC IT installed on the aircraft in the System Configuration. N OTE:For CJ3 operators use APCT-3700 in place of ICIT. (1) Access OMS. (2) On the Maint pa ge, select the Basic (Bsc)/Advanced (Adv) mode icon until the Adv icon is highlighted. (3) Select the System tab d. (4) On the IMA Syst em Configuration page Configuration Index Nameplate area will show the electronic nameplate of the IMA Configuration Index Table (ICIT). Refer to

Figure 1.

IMA System Configuration Page

Figure 1

(5) Refer t o Table 1 to determine new ICIT and FDSA 6500.

Jun 3/19FDSA-6500-19-1

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Service Information Letter

(6) Transfer the applicable software listed in Table 1 to a USB Flash drive. (a) Format the USB M emory flash drive as follows: 1 . Insert the target USB flash drive into a free USB port in the PC. 2 . Open Windows File Explorer and select the USB drive. 3 . Right mouse click and select the Format menu option. 4 . Make sure FAT32 (Default) shows in the File system drop down menu. In the

Allocation un

it size drop down menu, select Default allocation size. Use of the Volume label field and Format options field is not required. Select Start. (b) The USB flash drive is formatted. (7) Install softw are identified in Table 1 per applicable AMM/ASM - The following steps are provided for clarification/simplification only. (a) Prepare/Load USB flash drive with required software (b) Set the Data L oad Enable switch to ON. (c) Enable the Automated Field Load. 1 . Production King Air and PL21 to KA Fusion, insert field loadable shorting plug in the back of the center pedestal. 2 . Aftermarket PL 2 to KA Fusion, locate the Automated Field Load enable switch in the Pilots side nose avionics bay set the switch to ON. 3 . CJ3 locate the Automated Field Load enable switch in the Pilots side nose avionics bay set the switch to ON. 4 . CL604, locate the Automated Field Load enable switch behind the Pilots seat,settheswitchtoON. (d) Cycle the power on the AFD-3700 unit requiring field load (all three (3)). (e) Insert the p repared USB flash drive into the AFD front bezel USB port. (f) The Target Status messages will update during field load to indicate progress. (g) Upon successful field load completion the Target Status will state Complete for each targe t. (h) Remove the USB flash drive from the AFD front bezel USB port (i) Using the reversionary switch for the display being loaded, power off the display. (j) Set the Dat a Load Enable switch to OFF.

Jun 3/19FDSA-6500-19-1

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Service Information Letter

(k) Using the reversionary switch for the display being loaded, power on the display. (l) Wait one (1) mi nute for the display to draw in the configuration data from the

Aircraft Personality Module.

(m) As the display powers up (after the splash screen), watch the center of the

FDSA-6500-19

-1 Page 8 display for the copyright statement. The third line will be the configuration the display is set for. For example, King Air B300, CL604, etc. (n) Repeat Steps F.(7)(j) thru F.(7)(m) if third line is not displayed. (o) Repeat Step F .(7)(b) through Step F.(7)(n) to field load the remaining AFD-3700 units. (p) Disable the Automated Field Load. (8) Software ver ification Repeat Steps F.(6)(a) thru F.(7)(d) and verify new ICIT was loaded T numbers.

ICIT PART NUMBER

INSTALLED P

RIOR TO

AIRCRAFT MODTYPE NUMBER

TO INSTALLPART NUMBERS TO

INSTALL

ICITRCA-5429-100 or

434-31001

1-0013

434-310011-0001 or

RCA-5177-

001 or

RCA-5168-001 or

RCA-5205-001

FDSA-6500 810-0234-1H0101

ICITRCA-5429-101 or

101-3303-0013

101-3303-0009

FDSA-6500 810-0234-1H0101

ICITRCA-5429-102 or

434-310011-0015

434-310011-0003

FDSA-6500 810-0234-1H0101

ICITRCA-5429-200 or

434-310011-0017

434-310011-0005 or

RCA-5177-002 or

RCA-5168-002 or

RCA-520

5-002FDSA-6500 810-0234-1H0102

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