Airworthiness Directives; Bombardier, Inc. Airplanes, 58827-58829 [2016-20376]
Download as PDF
Federal Register / Vol. 81, No. 166 / Friday, August 26, 2016 / Rules and Regulations
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
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
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 inservice 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
ˆ
Bombardier, Inc., 400 Cote-Vertu Road
´
West, Dorval, Quebec 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: ac.yul@aero.bombardier.com;
Internet: https://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 https://
www.regulations.gov by searching for
and locating Docket No. FAA–2016–
3990.
ehiers on DSK5VPTVN1PROD with RULES
SUMMARY:
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2016–
VerDate Sep<11>2014
14:39 Aug 25, 2016
Jkt 238001
58827
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:
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.
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:
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 highaltitude 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.
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.
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
You may examine the MCAI in the
AD docket on the Internet at https://
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.
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:
• Are consistent with the intent that
was proposed in the NPRM for
correcting the unsafe condition; and
• 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
E:\FR\FM\26AUR1.SGM
26AUR1
58828
Federal Register / Vol. 81, No. 166 / Friday, August 26, 2016 / Rules and Regulations
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
Action
Labor cost
Cost per
product
Cost on U.S.
operators
AFM revision ....................................
1 work-hour × $85 per hour = $85 ............................................................
$85
$19,550
ehiers on DSK5VPTVN1PROD with RULES
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.
VerDate Sep<11>2014
14:39 Aug 25, 2016
Jkt 238001
List of Subjects in 14 CFR Part 39
(f) Compliance
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Comply with this AD within the
compliance times specified, unless already
done.
(g) Airplane Flight Manual (AFM) Revision
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
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 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.
PO 00000
Frm 00020
Fmt 4700
Sfmt 4700
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 DAOauthorized signature.
E:\FR\FM\26AUR1.SGM
26AUR1
Federal Register / Vol. 81, No. 166 / Friday, August 26, 2016 / Rules and Regulations
(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
https://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
ˆ
this AD, contact Bombardier, Inc., 400 Cote´
Vertu Road West, Dorval, Quebec 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:
ac.yul@aero.bombardier.com; Internet:
https://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: https://
www.archives.gov/federal-register/cfr/ibrlocations.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
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
ehiers on DSK5VPTVN1PROD with RULES
[Docket No. FAA–2016–6983; Directorate
Identifier 2016–CE–012–AD; Amendment
39–18618; AD 2016–17–05]
RIN 2120–AA64
Airworthiness Directives; RUAG
Aerospace Services GmbH Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
AGENCY:
VerDate Sep<11>2014
14:39 Aug 25, 2016
Jkt 238001
ACTION:
Final rule.
We are superseding
Airworthiness Directive (AD) 2009–13–
04 for RUAG Aerospace Services GmbH
Models 228–100, 228–101, 228–200,
228–201, 228–202, and 228–212
airplanes. This AD results from
mandatory continuing airworthiness
information (MCAI) issued by an
aviation authority of another country to
identify and correct an unsafe condition
on an aviation product. The MCAI
describes the unsafe condition as
excessive wear on the guide pin of the
power lever or condition lever, which
could cause functional loss of the flight
idle stop. We are issuing this AD to
require actions to address the unsafe
condition on these products.
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 the AD
as of September 30, 2016.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2016–
6983; or in person at the 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 service information identified in
this AD, contact RUAG Aerospace
Services GmbH, Dornier 228 Customer
Support, P.O. Box 1253, 82231
Wessling, Federal Republic of Germany,
telephone: +49 (0) 8153–30–2280; fax:
+49 (0) 8153–30–3030; email:
custsupport.dornier228@ruag.com;
Internet: https://www.ruag.com/. You
may review copies of the referenced
service information at the FAA, Small
Airplane Directorate, 901 Locust,
Kansas City, Missouri 64106. For
information on the availability of this
material at the FAA, call (816) 329–
4148. It is also available on the Internet
at https://www.regulations.gov by
searching for Docket No. FAA–2016–
6983.
FOR FURTHER INFORMATION CONTACT: Karl
Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4123; fax: (816)
329–4090; email: karl.schletzbaum@
faa.gov.
SUPPLEMENTARY INFORMATION:
SUMMARY:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
PO 00000
Frm 00021
Fmt 4700
Sfmt 4700
58829
apply to RUAG Aerospace Services
GmbH Models 228–100, 228–101, 228–
200, 228–201, 228–202, and 228–212
airplanes. That NPRM was published in
the Federal Register on June 1, 2016 (81
FR 34927), and proposed to supersede
AD 2009–13–04, Amendment 39–15943
(74 FR 29116; June 19, 2009) (‘‘AD
2009–13–04’’).
The NPRM proposed to correct an
unsafe condition for the specified
products and was based on mandatory
continuing airworthiness information
(MCAI) originated by an aviation
authority of another country. The MCAI
(EASA AD No.: 2009–0031R1) states
that:
Excessive wear on a guide pin of a power
lever was detected during inspections. The
failure of a power lever or condition lever
guide pin could cause functional loss of the
flight idle stop.
This condition, if not corrected, could lead
to inadvertent activation of the beta mode in
flight, possibly resulting in loss of control of
the aeroplane.
Prompted by this finding, RUAG issued
Alert Service Bulletin (ASB) ASB–228–279 to
provide inspection instructions.
Consequently, EASA issued AD 2009–0031
to require repetitive detailed inspections of
the guide pins of the power levers and
condition levers, and replacement of any pin
that exceeds the allowable wear-limits.
Since that AD was issued, further analysis
has determined that the inspection interval,
in case of no pin replacement, can be
extended and RUAG published Revision 1 of
ASB–228–279, which also included landings
(expressed in this AD as flight cycles—FC) as
a determining factor.
For the reason described above, this AD
revises EASA AD 2009–0031, amending the
compliance times without changing the
technical requirements, and also introducing
some editorial changes for standardization.
EASA revised the MCAI (EASA AD
No.: 2009–0031R2) to incorporate
changes to the applicability. The FAA
had already incorporated these changes
in the NPRM so no changes to the final
rule are necessary.
The MCAI can be found in the AD
docket on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2016–
6983.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM (74
FR 29116; June 19, 2009) or on the
determination of the cost to the public.
Conclusion
We reviewed the relevant data and
determined that air safety and the
public interest require adopting the AD
as proposed except for minor editorial
E:\FR\FM\26AUR1.SGM
26AUR1
Agencies
[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: ac.yul@aero.bombardier.com;
Internet: https://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 https://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 https://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 https://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:
Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
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 https://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:
ac.yul@aero.bombardier.com; Internet: https://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: https://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