Published 2022-07-07 · Federal Register document 2022-14274
Airworthiness Directives; Bombardier, Inc., Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. This AD was prompted by reports of the loss of all air data system information provided to the flightcrew during flight; the air data system information was recovered as the airplane descended to lower altitudes. This AD requires revising the existing airplane flight manual (AFM) to update the Unreliable Airspeed and Landing Distance Factor emergency procedures, which provide instructions for the flightcrew to stabilize the airspeed and altitude. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:11.345539+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2022-c0cc5a172b1306fa
- Source row
- results[230]
- Raw source SHA-256
- c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2022-13-05
- Effective date printed in this edition
- 2022-08-11
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective August 11, 2022.
Exact source excerpt. Text positions 14344–14433, end exclusive, in the original decoded publication. SHA-256: a0e8e4c9d55c905d2eeccc84eb5d9ee34b33c577e1dc658a1d54ad904dbbb4b9
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 14433–14462, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-700-1A10 and BD-
700-1A11 airplanes, certificated in any category, serial numbers (S/
Ns) 9002 through 9998 inclusive, and S/Ns 60001 through 60027
inclusive.
Exact source excerpt. Text positions 14462–14692, end exclusive, in the original decoded publication. SHA-256: b3afb504f167b88979f367947a0b90b599df79fbe6ba57671d03bdcc24d055cd
Subject
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
Exact source excerpt. Text positions 14692–14774, end exclusive, in the original decoded publication. SHA-256: 0542bcd80d4296f1663f9c1a9ee6733c7599b54c556ebcd2abd87a0d6015adff
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by reports of the loss of all air data
system information provided to the flightcrew during flight; the air
data system information was recovered as the airplanes descended to
lower altitudes. The FAA is issuing this AD to address loss of all
air data system information, which could lead to loss of continued
safe flight and landing of the airplane.
Exact source excerpt. Text positions 14774–15178, end exclusive, in the original decoded publication. SHA-256: 6532b128c82b900c4a78057d836141303fb4e441727ca00264f9dfca2093cd4d
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 15178–15280, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Revision of the Existing Airplane Flight Manual (AFM)
(g) Revision of the Existing Airplane Flight Manual (AFM)
Within 30 days after the effective date of this AD: Revise the
existing AFM to incorporate the information specified in the AFM
sections and supplements, as applicable, of the AFM revisions
specified in figure 1 to paragraph (g) of this AD.
[[Page 40432]]
[GRAPHIC] [TIFF OMITTED] TR07JY22.002
[[Page 40433]]
[GRAPHIC] [TIFF OMITTED] TR07JY22.003
[[Page 40434]]
[GRAPHIC] [TIFF OMITTED] TR07JY22.004
Exact source excerpt. Text positions 15280–15757, end exclusive, in the original decoded publication. SHA-256: 7d53449c1e607ec8be9777e9c1d9a5430a1f159ef439115b64f13dacbf05e488
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 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
[[Page 40435]]
request to your principal inspector or responsible Flight Standards
Office, as appropriate. If sending information directly to the
manager of the certification office, send it to ATTN: Program
Manager, Continuing Operational Safety, FAA, New York ACO Branch,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-
228-7300. Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, 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.
Exact source excerpt. Text positions 15757–17014, end exclusive, in the original decoded publication. SHA-256: 36da6fdfeaa3b42eef270e6ac2ada1c53a239b284eb3a43931bb9ffbbbe96e0b
Related Information
(i) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) TCCA AD CF-2020-50, dated November 20, 2020, for related
information. This MCAI may be found in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-
2022-0453.
(2) For more information about this AD, contact Chirayu Gupta,
Aerospace Engineer, Mechanical Systems and Administrative Services
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email [email protected].
Exact source excerpt. Text positions 17014–17584, end exclusive, in the original decoded publication. SHA-256: 2ca79e95a4c00a3d7ea1c484da984724eda90286b6bfcbb5c8afb6c85d517790
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) Unreliable Airspeed procedure, Section 03-12, Primary Flight
Displays, Chapter 3--Emergency Procedures, of the Bombardier Global
Express Airplane Flight Manual (AFM), Publication No. CSP 700-1,
Revision 107, dated February 22, 2021.
Note 1 to paragraph (j)(2)(i): For obtaining the procedures
specified in paragraphs (j)(2)(i) and (ii) of this AD for Bombardier
Global Express AFM, Publication No. CSP 700-1, use Document
Identification No. GL 700 AFM-1.
(ii) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global Express AFM, Publication No. CSP 700-1, Revision
107, dated February 22, 2021.
(iii) Unreliable Airspeed procedure, Section 03-12, Primary
Flight Displays, Chapter 3--Emergency Procedures, of the Bombardier
Global Express AFM, Publication No. CSP 700-1A, Revision 107, dated
February 22, 2021.
Note 2 to paragraph (j)(2)(iii): For obtaining the procedures
specified in paragraphs (j)(2)(iii) and (iv) of this AD for
Bombardier Global Express AFM, Publication No. CSP 700-1A, use
Document Identification No. GL 700 AFM-1A.
(iv) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global Express AFM, Publication No. CSP 700-1A, Revision
107, dated February 22, 2021.
(v) Unreliable Airspeed procedure, Section 03-12, Primary Flight
Displays, Chapter 3--Emergency Procedures, of the Bombardier Global
5000 AFM, Publication No. CSP 700-5000-1, Revision 68, dated
February 22, 2021.
Note 3 to paragraph (j)(2)(v): For obtaining the procedures
specified in paragraphs (j)(2)(v) and (vi) of this AD for Bombardier
Global 5000 AFM, Publication No. CSP 700-5000-1, use Document
Identification No. GL 5000 AFM.
(vi) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 5000 AFM, Publication No. CSP 700-5000-1, Revision
68, dated February 22, 2021.
(vii) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
5000 Featuring Global Vision Flight Deck AFM, Publication No. CSP
700-5000-1V, Revision 37, dated February 22, 2021.
Note 4 to paragraph (j)(2)(vii): For obtaining the procedures
specified in paragraphs (j)(2)(vii) and (viii) of this AD for
Bombardier Global 5000 Featuring Global Vision Flight Deck AFM,
Publication No. CSP 700-5000-1V, use Document Identification No. GL
5000 GVFD AFM.
(viii) Instruments procedure, Landing Distance Factors section,
of the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 5000 Featuring Global Vision Flight Deck AFM,
Publication No. CSP 700-5000-1V, Revision 37, dated February 22,
2021.
(ix) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
5500 AFM, Publication No. CSP 700-5500-1, Revision 8, dated November
11, 2020.
Note 5 to paragraph (j)(2)(ix): For obtaining the procedure
specified in paragraph (j)(2)(ix) of this AD for Bombardier Global
5500 AFM, Publication No. CSP 700-5500-1, use Document
Identification No. GL 5500 AFM.
(x) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
6000 AFM, Publication No. CSP 700-1V, Revision 37, dated February
22, 2021.
Note 6 to paragraph (j)(2)(x): For obtaining the procedures
specified in paragraphs (j)(2)(x) and (xi) of this AD for Bombardier
Global 6000 AFM, Publication No. CSP 700-1V, use Document
Identification No. GL 6000 AFM.
(xi) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 6000 AFM, Publication No. CSP 700-1V, Revision 37,
dated February 22, 2021.
(xii) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
6500 AFM, Publication No. CSP 700-6500-1, Revision 8, dated November
11, 2020.
Note 7 to paragraph (j)(2)(xii): For obtaining the procedure
specified in paragraph (j)(2)(xii) of this AD for Bombardier Global
6500 AFM, Publication No. CSP 700-6500-1, use Document
Identification No. GL 6500 AFM.
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 1-514-855-2999; email [email protected]; internet
https://www.bombardier.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(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, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 17584–23561, end exclusive, in the original decoded publication. SHA-256: dd23c3dac9f510a7b8f0f048f4e79751cf1143d20175cfb529f99f7d932b2a37
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 2022-13-05 · 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: 1b496b27b646278effb0b187734a992e3d7baed2085cd402313f5666683813e2. Source manifest: 9779748964510c3cf4f11db9b2b7a5010d06b24072e9a2948b00879875944605.
Official source · 2022-07-07
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 87, Number 129 (Thursday, July 7, 2022)]
[Rules and Regulations]
[Pages 40429-40435]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-14274]
========================================================================
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.
========================================================================
Federal Register / Vol. 87, No. 129 / Thursday, July 7, 2022 / Rules
and Regulations
[[Page 40429]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0453; Project Identifier MCAI-2020-01557-T;
Amendment 39-22091; AD 2022-13-05]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes.
This AD was prompted by reports of the loss of all air data system
information provided to the flightcrew during flight; the air data
system information was recovered as the airplane descended to lower
altitudes. This AD requires revising the existing airplane flight
manual (AFM) to update the Unreliable Airspeed and Landing Distance
Factor emergency procedures, which provide instructions for the
flightcrew to stabilize the airspeed and altitude. The FAA is issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective August 11, 2022.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of August 11,
2022.
ADDRESSES: For service information identified in this final rule,
contact Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 1-514-855-2999; email [email protected]; internet
https://www.bombardier.com. You may view this service information at
the FAA, Airworthiness Products Section, Operational Safety Branch,
2200 South 216th St., Des Moines, WA. For information on the
availability of this material at the FAA, call 206-231-3195. It is also
available on the internet at https://www.regulations.gov by searching
for and locating Docket No. FAA-2022-0453.
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-2022-
0453; 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: Chirayu Gupta, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7300; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued TCCA AD CF-2020-50, dated November 20,
2020 (TCCA AD CF-2020-50) (also referred to after this as the Mandatory
Continuing Airworthiness Information, or the MCAI), to correct an
unsafe condition for certain Bombardier, Inc., Model BD-700-1A10 and
BD-700-1A11 airplanes. You may examine the MCAI in the AD docket at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2022-0453.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to for certain Bombardier,
Inc., Model BD-700-1A10 and BD-700-1A11 airplanes. The NPRM published
in the Federal Register on April 11, 2022 (87 FR 21047). The NPRM was
prompted by reports of the loss of all air data system information
provided to the flightcrew during flight; the air data system
information was recovered as the airplane descended to lower altitudes.
The NPRM proposed to require revising the existing AFM to update the
Unreliable Airspeed and Landing Distance Factor emergency procedures,
which provide instructions for the flightcrew to stabilize the airspeed
and altitude. The FAA is issuing this AD to address loss of all air
data system information, which could lead to loss of continued safe
flight and landing of the airplane. See the MCAI for additional
background information.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
The FAA reviewed the relevant data and determined that air safety
requires adopting this AD as proposed. Except for minor editorial
changes, this AD is adopted as proposed in the NPRM. None of the
changes will increase the economic burden on any operator. Accordingly,
the FAA is issuing this AD to address the unsafe condition on these
products.
Related Service Information Under 1 CFR Part 51
Bombardier has issued the following service information. This
service information describes procedures for stabilizing the airspeed
and altitude of the airplane. These documents are distinct since they
apply to different airplane models.
<bullet> Unreliable Airspeed procedure, Section 03-12, Primary
Flight Displays, Chapter 3--Emergency Procedures, of the Bombardier
Global Express AFM, Publication No. CSP 700-1, Revision 107, dated
February 22, 2021. (For obtaining the procedures for Bombardier Global
Express AFM, Publication No. CSP 700-1, use Document Identification No.
GL 700 AFM-1.)
<bullet> Instruments procedure, Landing Distance Factors section,
of the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global Express AFM, Publication No. CSP 700-1, Revision 107,
dated February 22, 2021. (For obtaining the
[[Page 40430]]
procedures for Bombardier Global Express AFM, Publication No. CSP 700-
1, use Document Identification No. GL 700 AFM-1.)
<bullet> Unreliable Airspeed procedure, Section 03-12, Primary
Flight Displays, Chapter 3--Emergency Procedures, of the Bombardier
Global Express AFM, Publication No. CSP 700-1A, Revision 107, dated
February 22, 2021. (For obtaining the procedures for Bombardier Global
Express AFM, Publication No. CSP 700-1A, use Document Identification
No. GL 700 AFM-1A.)
<bullet> Instruments procedure, Landing Distance Factors section,
of the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global Express AFM, Publication No. CSP 700-1A, Revision
107, dated February 22, 2021. (For obtaining the procedures for
Bombardier Global Express AFM, Publication No. CSP 700-1A, use Document
Identification No. GL 700 AFM-1A.)
<bullet> Unreliable Airspeed procedure, Section 03-12, Primary
Flight Displays, Chapter 3--Emergency Procedures, of the Bombardier
Global 5000 AFM, Publication No. CSP 700-5000-1, Revision 68, dated
February 22, 2021. (For obtaining the procedures for Bombardier Global
5000 AFM, Publication No. CSP 700-5000-1, use Document Identification
No. GL 5000 AFM.)
<bullet> Instruments procedure, Landing Distance Factors section,
of the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 5000 AFM, Publication No. CSP 700-5000-1, Revision
68, dated February 22, 2021. (For obtaining the procedures for
Bombardier Global 5000 AFM, Publication No. CSP 700-5000-1, use
Document Identification No. GL 5000 AFM.)
<bullet> Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global 5000
Featuring Global Vision Flight Deck AFM, Publication No. CSP 700-5000-
1V, Revision 37, dated February 22, 2021. (For obtaining the procedures
for Bombardier Global 5000 Featuring Global Vision Flight Deck AFM,
Publication No. CSP 700-5000-1V, use Document Identification No. GL
5000 GVFD AFM.)
<bullet> Instruments procedure, Landing Distance Factors section,
of the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 5000 Featuring Global Vision Flight Deck AFM,
Publication No. CSP 700-5000-1V, Revision 37, dated February 22, 2021.
(For obtaining the procedures for Bombardier Global 5000 Featuring
Global Vision Flight Deck AFM, Publication No. CSP 700-5000-1V, use
Document Identification No. GL 5000 GVFD AFM.)
<bullet> Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global 5500
AFM, Publication No. CSP 700-5500-1, Revision 8, dated November 11,
2020. (For obtaining the procedures for Bombardier Global 5500 AFM,
Publication No. CSP 700-5500-1, use Document Identification No. GL 5500
AFM.)
<bullet> Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global 6000
AFM, Publication No. CSP 700-1V, Revision 37, dated February 22, 2021.
(For obtaining the procedures for Bombardier Global 6000 AFM,
Publication No. CSP 700-1V, use Document Identification No. GL 6000
AFM.)
<bullet> Instruments procedure, Landing Distance Factors section,
of the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 6000 AFM, Publication No. CSP 700-1V, Revision 37,
dated February 22, 2021. (For obtaining the procedures for Bombardier
Global 6000 AFM, Publication No. CSP 700-1V, use Document
Identification No. GL 6000 AFM.)
<bullet> Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures of the Bombardier Global 6500
AFM, Publication No. CSP 700-6500-1, Revision 8, dated November 11,
2020. (For obtaining the procedures for Bombardier Global 6500 AFM,
Publication No. CSP 700-6500-1, use Document Identification No. GL 6500
AFM.)
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
The FAA estimates that this AD affects 395 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85............................. $0 $85 $33,575
----------------------------------------------------------------------------------------------------------------
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
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,
[[Page 40431]]
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
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:
2022-13-05 Bombardier, Inc.: Amendment 39-22091; Docket No. FAA-
2022-0453; Project Identifier MCAI-2020-01557-T.
(a) Effective Date
This airworthiness directive (AD) is effective August 11, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc., Model BD-700-1A10 and BD-
700-1A11 airplanes, certificated in any category, serial numbers (S/
Ns) 9002 through 9998 inclusive, and S/Ns 60001 through 60027
inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 34, Navigation.
(e) Unsafe Condition
This AD was prompted by reports of the loss of all air data
system information provided to the flightcrew during flight; the air
data system information was recovered as the airplanes descended to
lower altitudes. The FAA is issuing this AD to address loss of all
air data system information, which could lead to loss of continued
safe flight and landing of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Revision of the Existing Airplane Flight Manual (AFM)
Within 30 days after the effective date of this AD: Revise the
existing AFM to incorporate the information specified in the AFM
sections and supplements, as applicable, of the AFM revisions
specified in figure 1 to paragraph (g) of this AD.
[[Page 40432]]
[GRAPHIC] [TIFF OMITTED] TR07JY22.002
[[Page 40433]]
[GRAPHIC] [TIFF OMITTED] TR07JY22.003
[[Page 40434]]
[GRAPHIC] [TIFF OMITTED] TR07JY22.004
(h) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York 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
[[Page 40435]]
request to your principal inspector or responsible Flight Standards
Office, as appropriate. If sending information directly to the
manager of the certification office, send it to ATTN: Program
Manager, Continuing Operational Safety, FAA, New York ACO Branch,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-
228-7300. Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, 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.
(i) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) TCCA AD CF-2020-50, dated November 20, 2020, for related
information. This MCAI may be found in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-
2022-0453.
(2) For more information about this AD, contact Chirayu Gupta,
Aerospace Engineer, Mechanical Systems and Administrative Services
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7300; email [email protected].
(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) Unreliable Airspeed procedure, Section 03-12, Primary Flight
Displays, Chapter 3--Emergency Procedures, of the Bombardier Global
Express Airplane Flight Manual (AFM), Publication No. CSP 700-1,
Revision 107, dated February 22, 2021.
Note 1 to paragraph (j)(2)(i): For obtaining the procedures
specified in paragraphs (j)(2)(i) and (ii) of this AD for Bombardier
Global Express AFM, Publication No. CSP 700-1, use Document
Identification No. GL 700 AFM-1.
(ii) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global Express AFM, Publication No. CSP 700-1, Revision
107, dated February 22, 2021.
(iii) Unreliable Airspeed procedure, Section 03-12, Primary
Flight Displays, Chapter 3--Emergency Procedures, of the Bombardier
Global Express AFM, Publication No. CSP 700-1A, Revision 107, dated
February 22, 2021.
Note 2 to paragraph (j)(2)(iii): For obtaining the procedures
specified in paragraphs (j)(2)(iii) and (iv) of this AD for
Bombardier Global Express AFM, Publication No. CSP 700-1A, use
Document Identification No. GL 700 AFM-1A.
(iv) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global Express AFM, Publication No. CSP 700-1A, Revision
107, dated February 22, 2021.
(v) Unreliable Airspeed procedure, Section 03-12, Primary Flight
Displays, Chapter 3--Emergency Procedures, of the Bombardier Global
5000 AFM, Publication No. CSP 700-5000-1, Revision 68, dated
February 22, 2021.
Note 3 to paragraph (j)(2)(v): For obtaining the procedures
specified in paragraphs (j)(2)(v) and (vi) of this AD for Bombardier
Global 5000 AFM, Publication No. CSP 700-5000-1, use Document
Identification No. GL 5000 AFM.
(vi) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 5000 AFM, Publication No. CSP 700-5000-1, Revision
68, dated February 22, 2021.
(vii) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
5000 Featuring Global Vision Flight Deck AFM, Publication No. CSP
700-5000-1V, Revision 37, dated February 22, 2021.
Note 4 to paragraph (j)(2)(vii): For obtaining the procedures
specified in paragraphs (j)(2)(vii) and (viii) of this AD for
Bombardier Global 5000 Featuring Global Vision Flight Deck AFM,
Publication No. CSP 700-5000-1V, use Document Identification No. GL
5000 GVFD AFM.
(viii) Instruments procedure, Landing Distance Factors section,
of the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 5000 Featuring Global Vision Flight Deck AFM,
Publication No. CSP 700-5000-1V, Revision 37, dated February 22,
2021.
(ix) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
5500 AFM, Publication No. CSP 700-5500-1, Revision 8, dated November
11, 2020.
Note 5 to paragraph (j)(2)(ix): For obtaining the procedure
specified in paragraph (j)(2)(ix) of this AD for Bombardier Global
5500 AFM, Publication No. CSP 700-5500-1, use Document
Identification No. GL 5500 AFM.
(x) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
6000 AFM, Publication No. CSP 700-1V, Revision 37, dated February
22, 2021.
Note 6 to paragraph (j)(2)(x): For obtaining the procedures
specified in paragraphs (j)(2)(x) and (xi) of this AD for Bombardier
Global 6000 AFM, Publication No. CSP 700-1V, use Document
Identification No. GL 6000 AFM.
(xi) Instruments procedure, Landing Distance Factors section, of
the Emergency Procedures section of Supplement 20--Operations at
Airport Elevations Above 10,000 Feet, Chapter 7--Supplements, of the
Bombardier Global 6000 AFM, Publication No. CSP 700-1V, Revision 37,
dated February 22, 2021.
(xii) Unreliable Airspeed procedure, Section 03-12, Instruments
System, Chapter 3--Emergency Procedures, of the Bombardier Global
6500 AFM, Publication No. CSP 700-6500-1, Revision 8, dated November
11, 2020.
Note 7 to paragraph (j)(2)(xii): For obtaining the procedure
specified in paragraph (j)(2)(xii) of this AD for Bombardier Global
6500 AFM, Publication No. CSP 700-6500-1, use Document
Identification No. GL 6500 AFM.
(3) For service information identified in this AD, contact
Bombardier Business Aircraft Customer Response Center, 400
C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada;
telephone 1-514-855-2999; email [email protected]; internet
https://www.bombardier.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(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, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on June 13, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-14274 Filed 7-6-22; 8:45 am]
BILLING CODE 4910-13-P
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