Published 2016-08-26 · Federal Register document 2016-20376
Airworthiness Directives; Bombardier, Inc. Airplanes
Publication summary
We are adopting a new airworthiness directive (AD) for all Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series 705) and CL- 600-2D24 (Regional Jet Series 900) airplanes. This AD was prompted by two in-service incidents reported on Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes regarding a loss of all air data information in the flight deck. This AD requires revision of the airplane flight manual (AFM) to provide procedures to guide the crew to stabilize the airplane's airspeed and attitude for continued safe flight. We are issuing this AD to prevent loss of air data information that may affect continued safe flight.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:51.853224+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2016-48fe8cb6c57c00b7
- Source row
- results[282]
- Raw source SHA-256
- 48fe8cb6c57c00b74623eb2b71ad0abe73b95a424a8ac83fecd389da4d1e3a81
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2016-17-09
- Effective date printed in this edition
- 2016-09-30
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective September 30, 2016.
Exact source excerpt. Text positions 11484–11550, end exclusive, in the original decoded publication. SHA-256: 6614de790949d2598fc5c33ec2bcad9615e5a08b3ce8e68cd04fde474380471f
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 11550–11579, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to all Bombardier, Inc. Model CL-600-2D15
(Regional Jet Series 705) and CL-600-2D24 (Regional Jet Series 900)
airplanes, certificated in any category.
Exact source excerpt. Text positions 11579–11772, end exclusive, in the original decoded publication. SHA-256: 48aceff730af7aaa47a2ffcb4732cf528a5f49572a933cfe685915f702b193e9
Subject
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
Exact source excerpt. Text positions 11772–11854, end exclusive, in the original decoded publication. SHA-256: 0542bcd80d4296f1663f9c1a9ee6733c7599b54c556ebcd2abd87a0d6015adff
Reason
(e) Reason
This AD was prompted by reports of two in-service incidents on
Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, &
702) airplanes regarding a loss of all air data information in the
flight deck. We are issuing this AD to prevent air data information
loss that may affect continued safe flight.
Exact source excerpt. Text positions 11854–12185, end exclusive, in the original decoded publication. SHA-256: e9ebbb8a2f36c839ae7e23df9356dddb3922ba6648e808b9bd3f98a417abc976
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 12185–12287, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Airplane Flight Manual (AFM) Revision
(g) Airplane Flight Manual (AFM) Revision
Within 30 days after the effective date of this AD, revise the
Emergency Procedures section of the AFM to include the information
in Emergency Procedure 1., Unreliable Airspeed, of Section 03-19,
Emergency Procedures--Unreliable Airspeed, of Chapter 3, Emergency
Procedures, in Volume 1 of the Bombardier CRJ Series Regional Jet
CL-600-2D15 and CL-600-2D24 AFM CSP C-012, Revision 11A, dated May
25, 2015.
Exact source excerpt. Text positions 12287–12747, end exclusive, in the original decoded publication. SHA-256: 26cbd5b623d6a5eb78cf5a8d722cdb94a984eb0db583e042f420a0a60ef2f962
Other FAA AD Provisions
(h) 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 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 ACO, send it to ATTN: Assata Dessaline, Aerospace
Engineer, Avionics and Services Branch, ANE 172, FAA, New York ACO,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-
228-7301; 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, Engine and Propeller Directorate, 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.
[[Page 58829]]
Exact source excerpt. Text positions 12747–14190, end exclusive, in the original decoded publication. SHA-256: 0f4454dab088e67ab300a90bd27f1b4405c5ad5550f01f5f25151ead8144f1f7
Related Information
(i) Related Information
Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian AD CF-2015-08, dated 28 April, 2015, for related
information. This MCAI may be found in the AD docket on the Internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2016-3990.
Exact source excerpt. Text positions 14190–14500, end exclusive, in the original decoded publication. SHA-256: f6e923987ea43f5d7fc645b54909bf77001237e7d7651a70bbe4d7c3ea9d2a59
Material Incorporated by Reference
(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 this AD specifies otherwise.
(i) Section 03-19, Emergency Procedures--Unreliable Airspeed, of
Chapter 3, Emergency Procedures, in Volume 1 of the Bombardier CRJ
Series Regional Jet CL-600-2D15 and CL-600-2D24 Airplane Flight
Manual CSP C-012, Revision 11A, dated May 25, 2015.
(ii) Reserved.
(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; Widebody Customer Response Center
North America toll-free telephone: 1-866-538-1247 or direct-dial
telephone: 1-514-855-2999; fax 514-855-7401; email:
[email protected]; Internet: http://www.bombardier.com.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 14500–16011, end exclusive, in the original decoded publication. SHA-256: 7efc619d4027072e01db6fc385e340f4375274b2de3333b94ec900446859011f
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2016-17-09 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: cc76da58e0e5a6e28abf6e243d576e823dcef8da51fdcbdc5c4c6c8148419672. Source manifest: b63e6629ed4145db65bf369947a922a1c20c9ae4bbe2876386237124d342f586.
Official source · 2016-08-26
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 81, Number 166 (Friday, August 26, 2016)]
[Rules and Regulations]
[Pages 58827-58829]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-20376]
[[Page 58827]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-3990; Directorate Identifier 2015-NM-153-AD;
Amendment 39-18622; AD 2016-17-09]
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 all
Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series 705) and CL-
600-2D24 (Regional Jet Series 900) airplanes. This AD was prompted by
two in-service incidents reported on Bombardier, Inc. Model CL-600-2C10
(Regional Jet Series 700, 701, & 702) airplanes regarding a loss of all
air data information in the flight deck. This AD requires revision of
the airplane flight manual (AFM) to provide procedures to guide the
crew to stabilize the airplane's airspeed and attitude for continued
safe flight. We are issuing this AD to prevent loss of air data
information that may affect continued safe flight.
DATES: This AD is effective September 30, 2016.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of September
30, 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; Widebody Customer Response Center North
America toll-free telephone: 1-866-538-1247 or direct-dial telephone:
1-514-855-2999; fax 514-855-7401; email: [email protected];
Internet: http://www.bombardier.com. 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 http://www.regulations.gov by searching for and
locating Docket No. FAA-2016-3990.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
3990; 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 all Bombardier, Inc. Model
CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24 (Regional Jet
Series 900) airplanes. The NPRM published in the Federal Register on
March 4, 2016 (81 FR 11467) (``the NPRM''). The NPRM was prompted by
two in-service incidents reported on Bombardier, Inc. Model CL-600-2C10
(Regional Jet Series 700, 701, & 702) airplanes regarding a loss of all
air data information in the flight deck. The NPRM proposed to require
revision of the airplane flight manual (AFM) to provide procedures to
guide the crew to stabilize the airplane's airspeed and attitude for
continued safe flight. We are issuing this AD to prevent loss of air
data information that may affect continued safe flight.
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2015-08, dated April
28, 2015 (referred to after this as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for all Bombardier, Inc. Model CL-600-2D15 (Regional Jet
Series 705) and CL-600-2D24 (Regional Jet Series 900) airplanes. The
MCAI states:
Two in-service incidents have been reported on CL-600-2C10
aeroplanes regarding a loss of all air data information in the
cockpit. The air data information was recovered as the aeroplane
descended to lower altitudes. An investigation determined that the
root cause in both events was high altitude icing (ice crystal
contamination). If not addressed, this condition may affect
continued safe flight.
Due to similarities in the air data systems, such events could
happen on all Bombardier CRJ models, CL-600-2B19, CL-600-2C10, CL-
600-2D15, CL-600-2D24 and CL-600-2E25. Therefore, the corrective
actions for these models will be mandated once their respective
Airplane Flight Manual (AFM) revisions become available.
This [Canadian] AD mandates the incorporation of AFM procedures
to guide the crew to stabilize the aeroplanes airspeed and attitude
for continued safe flight.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
3990.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM and
the FAA's response to each comment.
Request for Further Investigation
The Air Line Pilots Association stated that the AFM revision will
not address the root cause of the high-altitude icing (ice crystal
contamination), and requested that further investigation be done for
the ice crystal contamination issue and remedies be provided in
addition to the AFM amendments.
We agree that the AFM revision will not address the root cause of
the high-altitude icing (ice crystal contamination). The manufacturer
is investigating the issue, but there is no timetable for a final
resolution. Should the manufacturer develop modifications to prevent
this problem, the FAA will consider further rulemaking. The
incorporation of the AFM procedures is meant to be used to guide the
crew on how to stabilize the airplane airspeed and altitude for
continued safe flight in icing conditions. However, further
investigation into this matter extends beyond the scope of this AD.
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 except for minor editorial changes. We have
determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
Bombardier, Inc. has issued Emergency Procedure 1., Unreliable
[[Page 58828]]
Airspeed, of Section 03-19, Emergency Procedures--Unreliable Airspeed,
of Chapter 3, Emergency Procedures, in Volume 1 of the Bombardier CRJ
Series Regional Jet CL-600-2D15 and CL-600-2D24 Airplane Flight Manual
CSP C-012, Revision 11A, dated May 25, 2015. The service information
describes procedures to guide the crew to stabilize the airplane's
airspeed and attitude for continued safe flight. 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.
Interim Action
Required actions in this AD apply only to Bombardier, Inc. Model
CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24 (Regional Jet
Series 900) airplanes. We may consider issuing further rulemaking on
the other Bombardier airplane models identified previously.
Costs of Compliance
We estimate that this AD affects 230 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 product operators
----------------------------------------------------------------------------------------------------------------
AFM revision.............................. 1 work-hour x $85 per hour = $85.. $85 $19,550
----------------------------------------------------------------------------------------------------------------
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):
2016-17-09 Bombardier, Inc.: Amendment 39-18622; Docket No. FAA-
2016-3990; Directorate Identifier 2015-NM-153-AD.
(a) Effective Date
This AD is effective September 30, 2016.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Bombardier, Inc. Model CL-600-2D15
(Regional Jet Series 705) and CL-600-2D24 (Regional Jet Series 900)
airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
(e) Reason
This AD was prompted by reports of two in-service incidents on
Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, &
702) airplanes regarding a loss of all air data information in the
flight deck. We are issuing this AD to prevent air data information
loss that may affect continued safe flight.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Airplane Flight Manual (AFM) Revision
Within 30 days after the effective date of this AD, revise the
Emergency Procedures section of the AFM to include the information
in Emergency Procedure 1., Unreliable Airspeed, of Section 03-19,
Emergency Procedures--Unreliable Airspeed, of Chapter 3, Emergency
Procedures, in Volume 1 of the Bombardier CRJ Series Regional Jet
CL-600-2D15 and CL-600-2D24 AFM CSP C-012, Revision 11A, dated May
25, 2015.
(h) 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 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 ACO, send it to ATTN: Assata Dessaline, Aerospace
Engineer, Avionics and Services Branch, ANE 172, FAA, New York ACO,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 516-
228-7301; 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, Engine and Propeller Directorate, 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.
[[Page 58829]]
(i) Related Information
Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian AD CF-2015-08, dated 28 April, 2015, for related
information. This MCAI may be found in the AD docket on the Internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2016-3990.
(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 this AD specifies otherwise.
(i) Section 03-19, Emergency Procedures--Unreliable Airspeed, of
Chapter 3, Emergency Procedures, in Volume 1 of the Bombardier CRJ
Series Regional Jet CL-600-2D15 and CL-600-2D24 Airplane Flight
Manual CSP C-012, Revision 11A, dated May 25, 2015.
(ii) Reserved.
(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; Widebody Customer Response Center
North America toll-free telephone: 1-866-538-1247 or direct-dial
telephone: 1-514-855-2999; fax 514-855-7401; email:
[email protected]; Internet: http://www.bombardier.com.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on August 17, 2016.
Dorr M. Anderson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2016-20376 Filed 8-25-16; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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