81 FR 26102 - Airworthiness Directives; Bombardier, Inc. Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 84 (May 2, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 84 (May 2, 2016)
| Page Range | 26102-26103 | |
| FR Document | 2016-09791 |
[Federal Register Volume 81, Number 84 (Monday, May 2, 2016)] [Rules and Regulations] [Pages 26102-26103] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-09791] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-4814; Directorate Identifier 2015-NM-105-AD; Amendment 39-18502; AD 2016-09-04] RIN 2120-AA64 Airworthiness Directives; Bombardier, Inc. Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. This AD was prompted by the discovery of a number of incorrectly calibrated angle of attack (AOA) transducers installed in the stall protection system. This AD requires replacement of incorrectly calibrated AOA transducers. We are issuing this AD to detect and replace incorrectly calibrated AOA transducers; incorrect calibration of the transducers could result in late activation of the stick pusher. DATES: This AD is effective June 6, 2016. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of June 6, 2016. ADDRESSES: For service information identified in this final rule, contact Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval, Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855- 7401; email [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-2015- 4814. 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-2015- 4814; 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 address for the Docket Office (phone: 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: Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7318; fax 516-794-5531. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100&440) airplanes. The NPRM published in the Federal Register on November 17, 2015 (80 FR 71749) (``the NPRM''). The NPRM was prompted by the discovery of a number of incorrectly calibrated AOA transducers installed in the stall protection system. The NPRM proposed to require replacement of incorrectly calibrated AOA transducers. We are issuing this AD to detect and replace incorrectly calibrated AOA transducers; incorrect calibration of the transducers could result in late activation of the stick pusher. Transport Canada Civil Aviation (TCCA), which is the aviation authority for Canada, has issued Canadian AD CF-2015-17, effective July 16, 2015 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. The MCAI states: It was discovered that a number of [angle of attack] AOA transducers installed on Bombardier CL-600-2B19 aeroplanes were incorrectly calibrated due to a quality control problem at both the production and repair facilities. Incorrect calibration of the AOA transducer could result in a late activation of the stick pusher. This [Canadian] AD mandates the replacement of the incorrectly calibrated AOA transducer. 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-2015- 4814. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM 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 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 We reviewed Bombardier Service Bulletin 601R-27-164, dated March 30, 2015. The service information describes procedures for replacement of incorrectly calibrated AOA transducers. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section. Costs of Compliance We estimate that this AD affects 575 airplanes of U.S. registry. We also estimate that it would take about 4 work-hours per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Required parts would cost about $10,000 per product. Based on these figures, we estimate the cost of this AD on U.S. operators to be $5,945,500, or $10,340 per product. 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 [[Page 26103]] 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) Is not a ``significant rule'' under 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): 2016-09-04 Bombardier, Inc.: Amendment 39-18502; Docket No. FAA- 2015-4814; Directorate Identifier 2015-NM-105-AD. (a) Effective Date This AD is effective June 6, 2016. (b) Affected ADs None. (c) Applicability This AD applies to Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category, serial numbers 7003 through 7067 inclusive, 7069 through 7990 inclusive, and 8000 through 8999 inclusive. (d) Subject Air Transport Association (ATA) of America Code 27, Flight Controls. (e) Reason This AD was prompted by the discovery of a number of incorrectly calibrated angle of attack (AOA) transducers installed in the stall protection system. We are issuing this AD to detect and replace incorrectly calibrated AOA transducers; incorrect calibration of the transducers could result in late activation of the stick pusher. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Replacement For AOA transducers identified in paragraph 1.A., ``Effectivity,'' of Bombardier Service Bulletin 601R-27-164, dated March 30, 2015: Within 2,500 flight hours or 12 months, whichever occurs first after the effective date of this AD, replace the AOA transducers with correctly calibrated AOA transducers, in accordance with the Accomplishment Instructions of Bombardier Service Bulletin 601R-27-164, dated March 30, 2015. (h) Parts Installation Prohibition As of the effective date of this AD, no person may install, on any airplane, an AOA transducer having a part number or serial number listed in paragraph 1.A., ``Effectivity,'' of Bombardier Service Bulletin 601R-27-164, dated March 30, 2015. (i) 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: Program Manager, Continuing Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; fax 516-794-5531. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD. (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, New York ACO, ANE-170, FAA; or Transport Canada Civil Aviation (TCCA); or Bombardier, Inc.'s TCCA Design Approval Organization (DAO). If approved by the DAO, the approval must include the DAO-authorized signature. (j) Related Information For more information about this AD, contact Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York ACO, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7318; fax 516-794-5531. (k) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Bombardier Service Bulletin 601R-27-164, dated March 30, 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; telephone 514-855-5000; fax 514-855- 7401; email [email protected]; Internet http://www.bombardier.com. (4) You may view this service information at 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 April 20, 2016. John P. Piccola, Jr., Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-09791 Filed 4-29-16; 8:45 am] BILLING CODE 4910-13-P
![26102 Federal Register / Vol. 81, No. 84 / Monday, May 2, 2016 / Rules and Regulations
Issued in Renton, Washington, on April 20, www.regulations.gov by searching for You may examine the MCAI in the
2016. and locating Docket No. FAA–2015– AD docket on the Internet at http://
John P. Piccola, Jr., 4814; or in person at the Docket www.regulations.gov by searching for
Acting Manager, Transport Airplane Management Facility between 9 a.m. and locating Docket No. FAA–2015–
Directorate, Aircraft Certification Service. and 5 p.m., Monday through Friday, 4814.
[FR Doc. 2016–09800 Filed 4–29–16; 8:45 am] except Federal holidays. The AD docket
Comments
BILLING CODE 4910–13–P contains this AD, the regulatory
evaluation, any comments received, and We gave the public the opportunity to
other information. The address for the participate in developing this AD. We
DEPARTMENT OF TRANSPORTATION Docket Office (phone: 800–647–5527) is received no comments on the NPRM or
Docket Management Facility, U.S. on the determination of the cost to the
Federal Aviation Administration Department of Transportation, Docket public.
Operations, M–30, West Building Conclusion
14 CFR Part 39 Ground Floor, Room W12–140, 1200
[Docket No. FAA–2015–4814; Directorate New Jersey Avenue SE., Washington, We reviewed the relevant data and
Identifier 2015–NM–105–AD; Amendment DC 20590. determined that air safety and the
39–18502; AD 2016–09–04] public interest require adopting this AD
FOR FURTHER INFORMATION CONTACT: as proposed, except for minor editorial
RIN 2120–AA64 Cesar Gomez, Aerospace Engineer, changes. We have determined that these
Airframe and Mechanical Systems minor changes:
Airworthiness Directives; Bombardier, Branch, ANE–171, FAA, New York
Inc. Airplanes • Are consistent with the intent that
Aircraft Certification Office (ACO), 1600 was proposed in the NPRM for
AGENCY: Federal Aviation Stewart Avenue, Suite 410, Westbury, correcting the unsafe condition; and
Administration (FAA), DOT. NY 11590; telephone 516–228–7318; fax • Do not add any additional burden
ACTION: Final rule. 516–794–5531. upon the public than was already
SUPPLEMENTARY INFORMATION: proposed in the NPRM.
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain Discussion Related Service Information Under 1
Bombardier, Inc. Model CL–600–2B19 CFR Part 51
We issued a notice of proposed
(Regional Jet Series 100 & 440) We reviewed Bombardier Service
rulemaking (NPRM) to amend 14 CFR
airplanes. This AD was prompted by the Bulletin 601R–27–164, dated March 30,
part 39 by adding an AD that would
discovery of a number of incorrectly 2015. The service information describes
calibrated angle of attack (AOA) apply to certain Bombardier, Inc. Model
CL–600–2B19 (Regional Jet Series procedures for replacement of
transducers installed in the stall incorrectly calibrated AOA transducers.
protection system. This AD requires 100&440) airplanes. The NPRM
published in the Federal Register on This service information is reasonably
replacement of incorrectly calibrated available because the interested parties
AOA transducers. We are issuing this November 17, 2015 (80 FR 71749) (‘‘the
NPRM’’). The NPRM was prompted by have access to it through their normal
AD to detect and replace incorrectly course of business or by the means
calibrated AOA transducers; incorrect the discovery of a number of incorrectly
calibrated AOA transducers installed in identified in the ADDRESSES section.
calibration of the transducers could
result in late activation of the stick the stall protection system. The NPRM Costs of Compliance
pusher. proposed to require replacement of
incorrectly calibrated AOA transducers. We estimate that this AD affects 575
DATES: This AD is effective June 6, 2016. We are issuing this AD to detect and airplanes of U.S. registry.
The Director of the Federal Register replace incorrectly calibrated AOA We also estimate that it would take
approved the incorporation by reference transducers; incorrect calibration of the about 4 work-hours per product to
of a certain publication listed in this AD transducers could result in late comply with the basic requirements of
as of June 6, 2016. activation of the stick pusher. this AD. The average labor rate is $85
ADDRESSES: For service information per work-hour. Required parts would
Transport Canada Civil Aviation
identified in this final rule, contact cost about $10,000 per product. Based
(TCCA), which is the aviation authority
Bombardier, Inc., 400 Côte-Vertu Road on these figures, we estimate the cost of
for Canada, has issued Canadian AD
West, Dorval, Québec H4S 1Y9, Canada; this AD on U.S. operators to be
CF–2015–17, effective July 16, 2015
telephone 514–855–5000; fax 514–855– $5,945,500, or $10,340 per product.
(referred to after this as the Mandatory
7401; email
Continuing Airworthiness Information, Authority for This Rulemaking
thd.crj@aero.bombardier.com; Internet
or ‘‘the MCAI’’), to correct an unsafe Title 49 of the United States Code
http://www.bombardier.com. You may
condition for certain Bombardier, Inc. specifies the FAA’s authority to issue
view this referenced service information
Model CL–600–2B19 (Regional Jet rules on aviation safety. Subtitle I,
at the FAA, Transport Airplane
Series 100 & 440) airplanes. The MCAI section 106, describes the authority of
Directorate, 1601 Lind Avenue SW.,
states: the FAA Administrator. Subtitle VII:
Renton, WA. For information on the
availability of this material at the FAA, It was discovered that a number of [angle Aviation Programs, describes in more
call 425–227–1221. It is also available of attack] AOA transducers installed on detail the scope of the Agency’s
on the Internet at http:// Bombardier CL–600–2B19 aeroplanes were authority.
mstockstill on DSK3G9T082PROD with RULES
incorrectly calibrated due to a quality control We are issuing this rulemaking under
www.regulations.gov by searching for problem at both the production and repair
and locating Docket No. FAA–2015– the authority described in Subtitle VII,
facilities. Incorrect calibration of the AOA
4814. transducer could result in a late activation of
Part A, Subpart III, Section 44701:
the stick pusher. ‘‘General requirements.’’ Under that
Examining the AD Docket section, Congress charges the FAA with
This [Canadian] AD mandates the
You may examine the AD docket on replacement of the incorrectly calibrated promoting safe flight of civil aircraft in
the Internet at http:// AOA transducer. air commerce by prescribing regulations
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![Federal Register / Vol. 81, No. 84 / Monday, May 2, 2016 / Rules and Regulations 26103
for practices, methods, and procedures numbers 7003 through 7067 inclusive, 7069 (j) Related Information
the Administrator finds necessary for through 7990 inclusive, and 8000 through For more information about this AD,
safety in air commerce. This regulation 8999 inclusive. contact Cesar Gomez, Aerospace Engineer,
is within the scope of that authority (d) Subject Airframe and Mechanical Systems Branch,
because it addresses an unsafe condition ANE–171, FAA, New York ACO, 1600
Air Transport Association (ATA) of
that is likely to exist or develop on Stewart Avenue, Suite 410, Westbury, NY
America Code 27, Flight Controls.
11590; telephone 516–228–7318; fax 516–
products identified in this rulemaking
(e) Reason 794–5531.
action.
This AD was prompted by the discovery of (k) Material Incorporated by Reference
Regulatory Findings a number of incorrectly calibrated angle of
attack (AOA) transducers installed in the (1) The Director of the Federal Register
This AD will not have federalism stall protection system. We are issuing this approved the incorporation by reference
implications under Executive Order AD to detect and replace incorrectly (IBR) of the service information listed in this
13132. This AD will not have a calibrated AOA transducers; incorrect paragraph under 5 U.S.C. 552(a) and 1 CFR
substantial direct effect on the States, on calibration of the transducers could result in part 51.
the relationship between the national late activation of the stick pusher. (2) You must use this service information
government and the States, or on the as applicable to do the actions required by
(f) Compliance this AD, unless the AD specifies otherwise.
distribution of power and (i) Bombardier Service Bulletin 601R–27–
Comply with this AD within the
responsibilities among the various compliance times specified, unless already 164, dated March 30, 2015.
levels of government. done. (ii) Reserved.
For the reasons discussed above, I (3) For service information identified in
certify that this AD: (g) Replacement this AD, contact Bombardier, Inc., 400 Côte-
(1) Is not a ‘‘significant regulatory For AOA transducers identified in Vertu Road West, Dorval, Québec H4S 1Y9,
action’’ under Executive Order 12866, paragraph 1.A., ‘‘Effectivity,’’ of Bombardier Canada; telephone 514–855–5000; fax 514–
(2) Is not a ‘‘significant rule’’ under Service Bulletin 601R–27–164, dated March 855–7401; email
30, 2015: Within 2,500 flight hours or 12 thd.crj@aero.bombardier.com; Internet http://
DOT Regulatory Policies and Procedures months, whichever occurs first after the www.bombardier.com.
(44 FR 11034, February 26, 1979), effective date of this AD, replace the AOA (4) You may view this service information
(3) Will not affect intrastate aviation transducers with correctly calibrated AOA at FAA, Transport Airplane Directorate, 1601
in Alaska, and transducers, in accordance with the Lind Avenue SW., Renton, WA. For
(4) Will not have a significant Accomplishment Instructions of Bombardier information on the availability of this
economic impact, positive or negative, Service Bulletin 601R–27–164, dated March material at the FAA, call 425–227–1221.
on a substantial number of small entities 30, 2015. (5) You may view this service information
under the criteria of the Regulatory (h) Parts Installation Prohibition that is incorporated by reference at the
Flexibility Act. National Archives and Records
As of the effective date of this AD, no
Administration (NARA). For information on
List of Subjects in 14 CFR Part 39 person may install, on any airplane, an AOA
the availability of this material at NARA, call
transducer having a part number or serial
202–741–6030, or go to: http://
Air transportation, Aircraft, Aviation number listed in paragraph 1.A.,
‘‘Effectivity,’’ of Bombardier Service Bulletin www.archives.gov/federal-register/cfr/ibr-
safety, Incorporation by reference, locations.html.
Safety. 601R–27–164, dated March 30, 2015.
Issued in Renton, Washington, on April 20,
Adoption of the Amendment (i) Other FAA AD Provisions
2016.
The following provisions also apply to this John P. Piccola, Jr.,
Accordingly, under the authority AD:
delegated to me by the Administrator, (1) Alternative Methods of Compliance Acting Manager, Transport Airplane
the FAA amends 14 CFR part 39 as (AMOCs): The Manager, New York Aircraft Directorate, Aircraft Certification Service.
follows: Certification Office (ACO), ANE–170, FAA, [FR Doc. 2016–09791 Filed 4–29–16; 8:45 am]
has the authority to approve AMOCs for this BILLING CODE 4910–13–P
PART 39—AIRWORTHINESS AD, if requested using the procedures found
DIRECTIVES in 14 CFR 39.19. In accordance with 14 CFR
39.19, send your request to your principal DEPARTMENT OF TRANSPORTATION
■ 1. The authority citation for part 39 inspector or local Flight Standards District
continues to read as follows: Office, as appropriate. If sending information
Federal Aviation Administration
directly to the ACO, send it to ATTN:
Authority: 49 U.S.C. 106(g), 40113, 44701. Program Manager, Continuing Operational
Safety, FAA, New York ACO, 1600 Stewart 14 CFR Part 39
§ 39.13 [Amended] Avenue, Suite 410, Westbury, NY 11590; [Docket No. FAA–2015–3970; Directorate
■ 2. The FAA amends § 39.13 by adding telephone 516–228–7300; fax 516–794–5531. Identifier 2015–SW–006–AD; Amendment
the following new airworthiness Before using any approved AMOC, notify 39–18497; AD 2016–08–20]
your appropriate principal inspector, or
directive (AD): lacking a principal inspector, the manager of RIN 2120–AA64
2016–09–04 Bombardier, Inc.: Amendment the local flight standards district office/
39–18502; Docket No. FAA–2015–4814; certificate holding district office. The AMOC Airworthiness Directives; Airbus
Directorate Identifier 2015–NM–105–AD. approval letter must specifically reference Helicopters (Previously Eurocopter
this AD. France)
(a) Effective Date (2) Contacting the Manufacturer: For any
This AD is effective June 6, 2016. requirement in this AD to obtain corrective AGENCY: Federal Aviation
mstockstill on DSK3G9T082PROD with RULES
actions from a manufacturer, the action must Administration (FAA), DOT.
(b) Affected ADs be accomplished using a method approved
None. by the Manager, New York ACO, ANE–170, ACTION: Final rule.
FAA; or Transport Canada Civil Aviation
(c) Applicability (TCCA); or Bombardier, Inc.’s TCCA Design SUMMARY: We are superseding
This AD applies to Bombardier, Inc. Model Approval Organization (DAO). If approved by airworthiness directive (AD) 2014–12–
CL–600–2B19 (Regional Jet Series 100 & 440) the DAO, the approval must include the 51 for Airbus Helicopters (previously
airplanes, certificated in any category, serial DAO-authorized signature. Eurocopter France) Model EC130B4 and
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Document Created: 2016-04-30 13:34:43
Document Modified: 2016-04-30 13:34:43
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule. | |
| Dates | This AD is effective June 6, 2016. | |
| Contact | Cesar Gomez, Aerospace Engineer, Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7318; fax 516-794-5531. | |
| FR Citation | 81 FR 26102 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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