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2021-05-17 ROCKWELL COLLINS, INC.: Amendment 39-21460; Docket No. FAA-2020-0883; Project Identifier 2019-CE-034-AD.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective April 29, 2021.

(b) AFFECTED ADS

    This AD replaces AD 2019-12-09,  Amendment 39-19664 (84 FR 32260, July
    8, 2019) (AD 2019-12-09).

(c) APPLICABILITY

    This AD applies to Rockwell Collins, Inc.,  (Rockwell Collins)  Flight
    Display System Application  FDSA-6500  part  numbers  (P/Ns) 810-0234-
    1H0001, 810-0234-1H0002, 810-0234-1H0003,  810-0234-2H0001,  810-0234-
    2C0001, 810-0234-2C0002, and 810-0234-4B0001.  These  applications are
    installed  on,  but not limited to,  Bombardier Inc. Model CL-600-2B16
    (604 variant) airplanes  and  Textron Aviation Inc. Models 525B, B200,
    B200C, B200CGT, B200GT, B300, B300C and C90GTi airplanes, certificated
    in any category.

(d) SUBJECT

    Joint Aircraft System Component (JASC) Code 3400, NAVIGATION SYSTEM.

(e) UNSAFE CONDITION

    This  AD  was  prompted by  a conflict  between the  traffic collision
    avoidance system (TCAS) primary  display indications and aural  alerts
    during a resolution advisory (RA) scenario. The FAA is issuing this AD
    to prevent  conflicting TCAS  information, which  could result  in the
    pilot under-correcting or over-correcting  and may lead to  inadequate
    aircraft separation and a mid-air collision.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) ACTIONS

(1) Within 30 days after July 23, 2019  (the effective date of AD 2019-12-
    09), do the following:

(i) Revise the airplane flight manual  (AFM)  or  AFM supplement (AFMS) by
    adding the following text to the Limitations section:  For TCAS II in-
    stallations,  during flight,  do not operate TCAS in the "TA/RA" mode;
    TCAS may only be operated in "TA Only" mode.

(ii) Fabricate a placard  for each aircraft primary flight display,  using
     at least 1/8 inch letters, with the following text: TCAS Flight Ops -
     TA Only mode (TA/RA mode prohibited).

(iii) Install the placard  on the bottom  of each  aircraft primary flight
      display bezel  in the area depicted  in figure 1 to paragraph (g)(1)
      (iii) of this AD.

Note 1 to paragraph (g)(1): In "TA/RA" mode, the TA stands for traffic ad-
visory and RA stands for resolution advisory.

                           ILLUSTRATION (Figure 1)

(2) In addition to the provisions of 14 CFR 43.3 and 43.7, the actions re-
    quired by paragraphs (g)(1)(i) through (iii)  of  this  AD may be per-
    formed by the owner/operator (pilot) holding  at least a private pilot
    certificate and must be entered into the aircraft records showing com-
    pliance with this AD in accordance with 14 CFR 43.9(a)(1) through  (4)
    and 14 CFR 91.417(a)(2)(v).  The record must be maintained as required
    by 14 CFR 91.417.  This  authority is not applicable to aircraft being
    operated under 14 CFR part 119.

(3) Within 12 months after the effective date of this AD, upgrade the FDSA
    -6500 field loadable software for your airplane as listed in the table
    in Section C  and  by following the instructions  in Section F of Roc-
    kwell Collins Service Information Letter FDSA-6500-19-1,  Revision No.
    2, dated June 12, 2019.

(4) The airplane flight manual revision and placards required by paragraph
    (g)(1) of this AD may be removed after completing the software upgrade
    required by paragraph (g)(3) of this AD.

(5) As of the effective date of this AD, do not install a Rockwell Collins
    Flight Display System Application FDSA-6500  P/N 810-0234-1H0001, 810-
    0234-1H0002, 810-0234-1H0003,  810-0234-2H0001,  810-0234-2C0001, 810-
    0234-2C0002, or 810-0234-4B0001 on any airplane.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The  Manager,  Wichita ACO Branch,  FAA,  has the authority to approve
    AMOCs for this AD,  if requested  using the procedures found in 14 CFR
    39.19. In  accordance with  14 CFR  39.19, send  your request  to your
    principal  inspector  or  local Flight  Standards District  Office, as
    appropriate. If  sending information  directly to  the manager  of the
    certification  office,  send it to the attention of the person identi-
    fied in Related Information.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector,  or  lacking a principal inspector,  the manager of the local
    flight standards district office/certificate holding district office.

(i) RELATED INFORMATION

    For more information  about  this  AD,  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.

(j) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference (IBR) of the service information listed  in  this  paragraph
    under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable  to do the actions
    required by this AD, unless the AD specifies otherwise.

(i) Rockwell Collins  Service Information Letter FDSA-6500-19-1,  Revision
    No. 2, dated June 12, 2019.

(ii) [Reserved]

(3) For Rockwell Collins service information  identified in this AD,  con-
    tact 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

(4) You may view this service information at FAA,  Airworthiness  Products
    Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106.
    For information on the availability of this material at the FAA,  call
    (816) 329-4148.

(5) You may view this service information  that is incorporated  by refer-
    ence at the National Archives and Records Administration  (NARA).  For
    information  on  the availability  of  this material  at  NARA, email:
    fedreg.legal@nara.gov,  or  go  to:  https://www.archives.gov/federal-
    register/cfr/ibr-locations.html.

Issued  on  February 25, 2021.  Gaetano A. Sciortino,  Deputy Director for
Strategic Initiatives,  Compliance & Airworthiness Division, Aircraft Cer-
tification Service.

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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0883; Project Identifier 2019-CE-034-AD; Amendment
39-21460; AD 2021-05-17]
RIN 2120-AA64

Airworthiness Directives; Rockwell Collins, Inc. Flight Display
System Application

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

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 indications and aural alerts that may occur during a resolution
advisory (RA) scenario. This AD retains the requirements of AD 2019-12-
09 until a software upgrade is completed. The FAA is issuing this AD to
address the unsafe condition on these products.

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 view this service information at the Airworthiness Products
Section, Operational Safety Branch, FAA, 901 Locust, Kansas City, MO
64106. For information on the availability of this material at the FAA,
call (816) 329-4148. It is also available at https://www.regulations.gov
by searching for and locating Docket No. FAA-2020-0883.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2020-0883; or in person at
Docket Operations between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket contains this final rule, any
comments received, and other information. The address for Docket
Operations is U.S. Department of Transportation, Docket Operations, M-
30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue
SE, Washington, DC 20590.

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

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2019-12-09, Amendment 39-19664 (84 FR
32260, July 8, 2019), (AD 2019-12-09). AD 2019-12-09 applied to certain
part-numbered Rockwell Collins FDSA-6500 flight display system
applications that may be installed on, but not limited to, Bombardier
Inc. Model CL-600-2B16 (604 variant) airplanes and Textron Aviation
Inc. Models 525B, B200, B200C, B200CGT, B200GT, B300, B300C, and C90GTi
airplanes. The NPRM published in the Federal Register on December 14,
2020 (85 FR 80686).
AD 2019-12-09 prohibited operation with the TCAS in TA/RA mode by
requiring a revision to the Limitations section of the airplane flight
manual (AFM) or AFM supplement (AFMS) and by fabricating and installing
a placard on each aircraft primary flight display. AD 2019-12-09
resulted from a report that a conflict could occur between the TCAS
primary cockpit display indications and the aural alerts during an RA
scenario. The FAA issued AD 2019-12-09 as an interim action to address
the immediate urgency to prevent the pilot from over-correcting or
under-correcting for aircraft separation, which may result in a mid-air
collision.
In the NPRM, the FAA proposed to retain the actions of AD 2019-12-
09 and install updated software on the flight data system applications
within 12 months. Once the software is upgraded, the FAA proposed to
allow removal of the limitations and placard. Because the requirements
proposed in the NPRM had a longer compliance time, the FAA provided the
public an opportunity to comment. The FAA is issuing this AD to address
the unsafe condition on these products.

Discussion of Final Airworthiness Directive Comments

The FAA received no comments on the NPRM or on the determination of
the costs.

Conclusion

The FAA reviewed the relevant data and determined that air safety
requires adoption of the AD as proposed. Accordingly, the FAA is
issuing this AD to address the unsafe condition on these products. This
AD is adopted as proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Rockwell Collins Service Information Letter FDSA-
6500-19-1, Revision No. 2, dated June 12, 2019. This service
information letter contains information regarding hardware and software
compatibility for the FDSA-6500 flight display system and provides
software download instructions. This service information is reasonably
available because the interested parties have access to it through
their normal course of business or by the means identified in
ADDRESSES.

Costs of Compliance

The FAA estimates that this AD affects 932 FDSA-6500 flight display
system applications installed on 311 airplanes worldwide. The FAA has
no way of knowing the number of FDSA-6500 applications installed on
airplanes of U.S. Registry. The estimated cost on U.S. operators
reflects the maximum possible cost based on worldwide applications.
The FAA estimates the following costs to comply with this AD:

Estimated Costs

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Revise the Limitations section of the AFM or AFMS. .5 work-hour x $85 per hour = $42.50 Not applicable $42.50 (per airplane) Up to $13,217.50
Fabricate and install a placard. .5 work-hour x $85 per hour = $42.50 Negligible $42.50 (per primary flight display) Up to $39,610
FDSA-6500 software upgrade 1 work-hour x $85 per hour = $85 Not applicable $85 (per primary flight display) Up to $79,220

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected operators.

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.

Regulatory Findings

The FAA has determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

The Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by:

a. Removing Airworthiness Directive 2019-12-09, Amendment 39-19664 (84
FR 32260, July 8, 2019); and

b. Adding the following new airworthiness directive: