AD 2016-14-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-600-2B19 (Regional Jet Series 100) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B19 (Regional Jet Series 440) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2C10 (Regional Jet Series 700) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2C10 (Regional Jet Series 701) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2C10 (Regional Jet Series 702) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2D15 (Regional Jet Series 705) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2D24 (Regional Jet Series 900) | Airworthiness Directives; Bombardier, Inc. Airplanes |
| aircraft | Bombardier Inc. | CL-600-2E25 (Regional Jet Series 1000) | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Reports of undesirable changes in the Reference Airspeed (RAS) Bug during flight without pilot input, caused by the flight control computer (FCC) not correctly reading input data from the Input/Output Concentrator, leading to uncommanded pitch changes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the flight control computer (FCC).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440), Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), Model CL-600-2D15 (Regional Jet Series 705), Model CL-600-2D24 (Regional Jet Series 900), and Model CL-600-2E25 (Regional Jet Series 1000) airplanes equipped with a flight control computer (FCC) with part numbers and serial numbers listed in Bombardier Service Bulletin 601R-22-018, Revision A, or Service Bulletin 670BA-22-009.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440), Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), Model CL-600- 2D15 (Regional Jet Series 705), Model CL-600-2D24 (Regional Jet Series 900), and Model CL-600-2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by reports of undesirable changes in the Reference Airspeed (RAS) Bug, occurring during flight without pilot input. This AD requires replacing the flight control computer (FCC). We are issuing this AD to prevent uncommanded pitch changes, which could result in deviation from a safe flight path.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Bombardier, Inc., airplanes, certificated in
any category, identified in paragraphs (c)(1) through (c)(5) of this
AD, all serial numbers, that are equipped with a flight control
computer (FCC) with a part number and serial number listed in
paragraph 1A., ``Effectivity'', of Bombardier Service Bulletin 601R-
22-018, Revision A, dated November 3, 2015; or Service Bulletin
670BA-22-009, dated August 17, 2015; as applicable.
(1) Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes.
(2) Model CL-600-2C10 (Regional Jet Series 700, 701, & 702)
airplanes.
(3) Model CL-600-2D15 (Regional Jet Series 705) airplanes.
(4) Model CL-600-2D24 (Regional Jet Series 900) airplanes.
(5) Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 81, Number 133 (Tuesday, July 12, 2016)]
[Rules and Regulations]
[Pages 44981-44983]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2016-16321]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
Prices of new books are listed in the first FEDERAL REGISTER issue of each
week.
========================================================================
Federal Register / Vol. 81, No. 133 / Tuesday, July 12, 2016 / Rules
and Regulations
[[Page 44981]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-5590; Directorate Identifier 2016-NM-018-AD;
Amendment 39-18588; AD 2016-14-07
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440),
Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), Model CL-600-
2D15 (Regional Jet Series 705), Model CL-600-2D24 (Regional Jet Series
900), and Model CL-600-2E25 (Regional Jet Series 1000) airplanes. This
AD was prompted by reports of undesirable changes in the Reference
Airspeed (RAS) Bug, occurring during flight without pilot input. This
AD requires replacing the flight control computer (FCC). We are issuing
this AD to prevent uncommanded pitch changes, which could result in
deviation from a safe flight path.
DATES: This AD is effective August 16, 2016.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of August 16,
2016.
ADDRESSES: For service information identified in this final rule,
contact Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; email <a href="/cdn-cgi/l/email-protection#93e7fbf7bdf0e1f9d3f2f6e1fcbdf1fcfef1f2e1f7faf6e1bdf0fcfe"><span class="__cf_email__" data-cfemail="fb8f939fd5988991bb9a9e8994d5999496999a899f929e89d5989496">[email protected]</span></a>; Internet. You may view this
referenced service information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the
availability of this material at the FAA, call 425-227-1221. It is also
available on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching
for and locating Docket No. FAA-2016-5590.
Examining the AD Docket
You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No. FAA-2016-
5590; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Office (telephone
800-647-5527) is Docket Management Facility, 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: Assata Dessaline, Aerospace Engineer,
Avionics and Services Branch, ANE-172, FAA, New York Aircraft
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516-228-7301; fax 516-794-5531.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Bombardier, Inc.
Model CL-600-2B19 (Regional Jet Series 100 & 440), Model CL-600-2C10
(Regional Jet Series 700, 701, & 702), Model CL-600-2D15 (Regional Jet
Series 705), Model CL-600-2D24 (Regional Jet Series 900), and Model CL-
600-2E25 (Regional Jet Series 1000) airplanes. The NPRM published in
the Federal Register on April 14, 2016 (81 FR 22037) (``the NPRM'').
The NPRM was prompted by reports of undesirable changes in the RAS Bug,
occurring during flight without pilot input. The NPRM proposed to
require replacing the FCC. We are issuing this AD to prevent
uncommanded pitch changes, which could result in deviation from a safe
flight path.
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2016-02, dated January 20, 2016 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ''the MCAI''), to
correct an unsafe condition for certain Bombardier, Inc. Model CL-600-
2B19 (Regional Jet Series 100 & 440), Model CL-600-2C10 (Regional Jet
Series 700, 701, & 702), Model CL-600-2D15 (Regional Jet Series 705),
Model CL-600-2D24 (Regional Jet Series 900), and Model CL-600-2E25
(Regional Jet Series 1000) airplanes. The MCAI states:
There have been numerous reports of uncommanded changes in the
Reference Airspeed (RAS) Bug during flight. When the Auto Flight
Control System (AFCS) is in a speed mode (CLB, DES, IAS or MACH),
the flight director will show vertical guidance to achieve or
maintain the reference airspeed. If the autopilot is engaged, the
aeroplane will automatically follow that vertical guidance and cause
the aeroplane to pitch up or pitch down. Investigation revealed that
this uncommanded reference airspeed changes were caused by the FCC
that did not correctly read the input data from the Input/Output
Concentrator. If not corrected, these uncommanded pitch changes
could create hazard for continued safe flight. This [Canadian] AD
mandates installation of a new filter to the Input/Output Circuit
Card in the FCC.
Uncommanded pitch changes, if not corrected, could result in
deviation from a safe flight path. Corrective actions include replacing
the FCC. You may examine the MCAI in the AD docket on the Internet at
<a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching for and locating Docket No.
FAA-2016-5590.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comment received. The commenter supported
the NPRM.
Conclusion
We reviewed the relevant data, considered the comment received, and
determined that air safety and the public interest require adopting
this AD as proposed.
[[Page 44982]]
Related Service Information Under 1 CFR Part 51
We reviewed Bombardier Service Bulletin 601R-22-018, Revision A,
dated November 3, 2015; and Service Bulletin 670BA-22-009, dated August
17, 2015. The service information describes procedures for replacing
the FCCs. 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 the ADDRESSES section.
Costs of Compliance
We estimate that this AD affects 1,008 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Replace FCC........................ 3 work-hours x $85 per hour $2,800 $3,055 $3,079,440
= $255 per airplane.
----------------------------------------------------------------------------------------------------------------
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.
We are 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
We 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. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);
3. Will not affect intrastate aviation in Alaska; and
4. 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.
Adoption of 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
0
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]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2016-14-07 Bombardier, Inc. Amendment 39-18588. Docket No. FAA-2016-
5590; Directorate Identifier 2016-NM-018-AD.
(a) Effective Date
This AD is effective August 16, 2016.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., airplanes, certificated in
any category, identified in paragraphs (c)(1) through (c)(5) of this
AD, all serial numbers, that are equipped with a flight control
computer (FCC) with a part number and serial number listed in
paragraph 1A., ``Effectivity'', of Bombardier Service Bulletin 601R-
22-018, Revision A, dated November 3, 2015; or Service Bulletin
670BA-22-009, dated August 17, 2015; as applicable.
(1) Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes.
(2) Model CL-600-2C10 (Regional Jet Series 700, 701, & 702)
airplanes.
(3) Model CL-600-2D15 (Regional Jet Series 705) airplanes.
(4) Model CL-600-2D24 (Regional Jet Series 900) airplanes.
(5) Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 22, Auto Flight.
(e) Reason
This AD was prompted by reports of undesirable changes in the
Reference Airspeed (RAS) Bug, occurring during flight without pilot
input. We are issuing this AD to prevent uncommanded pitch changes,
which could result in deviation from a safe flight path.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Replace the FCC for Certain Airplanes
Within 33 months after the effective date of this AD: Remove the
FCC from the integrated avionic processor system (IAPS) and replace
the FCC, in accordance with the Accomplishment Instructions of the
applicable service information specified in paragraph (g)(1) or
(g)(2) of this AD.
(1) Bombardier Service Bulletin 601R-22-018, Revision A, dated
November 3, 2015; or
(2) Bombardier Service Bulletin 670BA-22-009, dated August 17,
2015.
(h) Parts Installation Limitation
As of 12 months after the effective date of this AD, no person
may install any FCC having a part or serial number identified in
Bombardier Service Bulletin 601R-22-018, Revision A, dated November
3, 2015; or Bombardier Service Bulletin 670BA-22-009, dated August
17, 2015; unless ``SB 50'' is marked on the FCC modification chart
(MOD chart).
(i) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using Bombardier Service Bulletin 601R-22-018, dated
August 17, 2015, as applicable. This service information is not
incorporated by reference in this AD.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office (ACO), ANE-170, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found
[[Page 44983]]
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 New
York ACO, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516-228-7300; fax 516-794-5531. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the local flight
standards district office/certificate holding district office. The
AMOC approval letter must specifically reference this AD.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO,
ANE-170, FAA; or Transport Canada Civil Aviation (TCCA); or
Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If
approved by the DAO, the approval must include the DAO-authorized
signature.
(k) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian Airworthiness Directive CF-2016-02, dated January
20, 2016, for related information. This MCAI may be found in the AD
docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> by searching
for and locating Docket No. FAA-2016-5590.
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (l)(3) and (l)(4) of this AD.
(l) 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 this AD specifies otherwise.
(i) Bombardier Service Bulletin 601R-22-018, Revision A, dated
November 3, 2015.
(ii) Bombardier Service Bulletin 670BA-22-009, dated August 17,
2015.
(3) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; email <a href="/cdn-cgi/l/email-protection#116579753f72637b517074637e3f737e7c737063757874633f727e7c"><span class="__cf_email__" data-cfemail="3d495559135e4f577d5c584f52135f52505f5c4f5954584f135e5250">[email protected]</span></a>; Internet <a href="http://www.bombardier.com">http://www.bombardier.com</a>.
(4) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Renton, Washington, on June 28, 2016.
John P. Piccola, Jr.,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-16321 Filed 7-11-16; 8:45 am]
BILLING CODE 4910-13-P
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