83 FR 62701 - Airworthiness Directives; Pacific Aerospace Limited Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 234 (December 6, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 234 (December 6, 2018)
| Page Range | 62701-62702 | |
| FR Document | 2018-26364 |
[Federal Register Volume 83, Number 234 (Thursday, December 6, 2018)] [Rules and Regulations] [Pages 62701-62702] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-26364] [[Page 62701]] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0371; Product Identifier 2018-CE-005-AD; Amendment 39-19504; AD 2018-23-16] RIN 2120-AA64 Airworthiness Directives; Pacific Aerospace Limited Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for Pacific Aerospace Limited Model 750XL 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 insufficient clearance between the pitot tubes and the primary support at the flame arrester intersection. We are issuing this AD to require actions to address the unsafe condition on these products. DATES: This AD is effective January 10, 2019. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of January 10, 2019. ADDRESSES: You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0371; or in person at Docket Operations, 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 Pacific Aerospace Limited, Airport Road, Hamilton, Private Bag 3027, Hamilton 3240, New Zealand; phone: +64 7843 6144; fax: +64 843 6134; email: [email protected]; internet: www.aerospace.co.nz. You may view this referenced service information at the FAA, Policy and Innovation Division, 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 http://www.regulations.gov by searching for Docket No. FAA-2018-0371. FOR FURTHER INFORMATION CONTACT: Mike Kiesov, Aerospace Engineer, FAA, Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; email: [email protected]. 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 Pacific Aerospace Limited Model 750XL airplanes. The NPRM was published in the Federal Register on May 11, 2018 (83 FR 21962). The NPRM proposed to correct an unsafe condition for the specified products and was based on mandatory continuing airworthiness information (MCAI) originated by the Civil Aviation Authority of New Zealand (CAA). The MCAI states: Pacific Aerospace SB PACSB/XL/094 issue 2, dated 20 March 2018 revised to include inspection information, and DCA/750XL/24A updated to introduce the revised SB. The [CAA] AD is prompted by a production inspection of installed pitot static plumbing which identified insufficient clearance between the pitot tubes and the primary support at the flame arrestor intersection. This AD requires inspecting the pitot static tubes for chafing damage, replacing tubing as necessary, installing an additional clamp for pitot static tube support, protecting plumbing with spiralwrap, and ensuring proper clearance between the pitot tubes and the primary support at the flame arrester intersection. The MCAI can be found in the AD docket on the internet at: https://www.regulations.gov/document?D=FAA-2018-0371-0002. 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 the AD as proposed except for minor editorial changes and changes to clarify the reference to the service information. 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 Pacific Aerospace Service Bulletin PACSB/XL/094, Issue 2, dated March 20, 2018. The service information contains procedures for inspecting the pitot static tubing for chafing, replacing tubing as necessary, installing an additional clamp for pitot static tube support, protecting plumbing with spiralwrap, and ensuring proper clearance between the pitot tubes and the primary support at the flame arrester intersection. 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 will affect 22 products of U.S. registry. We also estimate that it would take about 1 work-hour per product to comply with the pitot static tubing inspection and installation of support clamps and spiral wrap required by this AD. The average labor rate is $85 per work-hour. Required parts would cost about $25 per product. Based on these figures, we estimate the cost of the AD on U.S. operators to be $2,420, or $110 per product. In addition, we estimate that any necessary follow-on actions to replace damaged tubing would take about 1 work-hour and require parts costing $25, for a cost of $110 per product. We have no way of determining the number of products that may need these actions. 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. This AD is issued in accordance with authority delegated by the Executive [[Page 62702]] Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to small airplanes, gliders, balloons, airships, domestic business jet transport airplanes, and associated appliances to the Director of the Policy and Innovation Division. 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 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): 2018-23-16 Pacific Aerospace Limited: Amendment 39-19504; Docket No. FAA-2018-0371; Product Identifier 2018-CE-005-AD. (a) Effective Date This AD becomes effective January 10, 2019. (b) Affected ADs None. (c) Applicability This AD applies to Pacific Aerospace Limited Model 750XL airplanes, serial numbers up to and including 200, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 34: Navigation. (e) Reason This AD was prompted by mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and address an unsafe condition on an aviation product. The MCAI describes the unsafe condition as insufficient clearance between the pitot tubes and the primary support at the flame arrester intersection. We are issuing this AD to prevent chafing between the pitot-static plumbing and the flame arrestor, which could lead to damage of the pitot-static lines. (f) Actions and Compliance Unless already done, do the following actions in paragraphs (f)(1) through (3) of this AD. (1) Within 100 hours time-in-service (TIS) after January 10, 2019 (the effective date of this AD) or within 60 days after January 10, 2019 (the effective date of this AD), whichever occurs first, inspect the pitot static tubing adjacent to the flame arrestor for chafing damage. (2) If any chafing damage is found during the inspection required in paragraph (f)(1) of this AD, before further flight, repair or replace any damaged tubing and conduct a pitot and static leak check. (3) Within 100 hours TIS after January 10, 2019 (the effective date of this AD) or within 60 days after January 10, 2019 (the effective date of this AD), whichever occurs first, install an additional support clamp, protect plumbing with spiralwrap, and ensure proper clearance between the pitot tubes and the primary support at the flame arrester intersection. Follow paragraphs (3) through (6) of the Accomplishment Instructions in Pacific Aerospace Service Bulletin PACSB/XL/094, Issue 2, dated March 20, 2018. (g) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Small Airplane Standards Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Mike Kiesov, Aerospace Engineer, FAA, Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329- 4090; email: [email protected]. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must instead be accomplished using a method approved by the Manager, Small Airplane Standards Branch, FAA; or Civil Aviation Authority of New Zealand (CAA). (h) Related Information Refer to MCAI CAA AD DCA/750XL/24A, dated March 22, 2018, for related information. The MCAI can be found in the AD docket on the internet at: https://www.regulations.gov/document?D=FAA-2018-0371-0002. (i) 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) Pacific Aerospace Service Bulletin PACSB/XL/094, Issue 2, dated March 20, 2018. (ii) [Reserved] (3) For service information identified in this AD, contact Pacific Aerospace Limited, Airport Road, Hamilton, Private Bag 3027, Hamilton 3240, New Zealand; phone: +64 7843 6144; fax: +64 843 6134; email: [email protected]; internet: www.aerospace.co.nz. (4) You may view this service information at the FAA, Policy and Innovation Division, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. In addition, you can access this service information on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0371. (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 Kansas City, Missouri, on November 27, 2018. Melvin J. Johnson, Aircraft Certification Service, Deputy Director, Policy and Innovation Division, AIR-601. [FR Doc. 2018-26364 Filed 12-4-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 234 / Thursday, December 6, 2018 / Rules and Regulations 62701
DEPARTMENT OF TRANSPORTATION FOR FURTHER INFORMATION CONTACT: Related Service Information Under 1
Mike Kiesov, Aerospace Engineer, FAA, CFR Part 51
Federal Aviation Administration Small Airplane Standards Branch, 901 We reviewed Pacific Aerospace
Locust, Room 301, Kansas City, Service Bulletin PACSB/XL/094, Issue
14 CFR Part 39 Missouri 64106; telephone: (816) 329– 2, dated March 20, 2018. The service
4144; fax: (816) 329–4090; email: information contains procedures for
[Docket No. FAA–2018–0371; Product mike.kiesov@faa.gov.
Identifier 2018–CE–005–AD; Amendment inspecting the pitot static tubing for
39–19504; AD 2018–23–16] SUPPLEMENTARY INFORMATION: chafing, replacing tubing as necessary,
Discussion installing an additional clamp for pitot
RIN 2120–AA64 static tube support, protecting plumbing
We issued a notice of proposed with spiralwrap, and ensuring proper
Airworthiness Directives; Pacific rulemaking (NPRM) to amend 14 CFR clearance between the pitot tubes and
Aerospace Limited Airplanes part 39 by adding an AD that would the primary support at the flame arrester
apply to Pacific Aerospace Limited intersection. This service information is
AGENCY: Federal Aviation Model 750XL airplanes. The NPRM was
Administration (FAA), Department of reasonably available because the
published in the Federal Register on interested parties have access to it
Transportation (DOT). May 11, 2018 (83 FR 21962). The NPRM through their normal course of business
ACTION: Final rule. proposed to correct an unsafe condition or by the means identified in the
for the specified products and was
SUMMARY: We are adopting a new ADDRESSES section.
based on mandatory continuing
airworthiness directive (AD) for Pacific airworthiness information (MCAI) Costs of Compliance
Aerospace Limited Model 750XL originated by the Civil Aviation
airplanes. This AD results from We estimate that this AD will affect
Authority of New Zealand (CAA). The 22 products of U.S. registry. We also
mandatory continuing airworthiness MCAI states:
information (MCAI) issued by an estimate that it would take about 1
aviation authority of another country to Pacific Aerospace SB PACSB/XL/094 issue work-hour per product to comply with
2, dated 20 March 2018 revised to include the pitot static tubing inspection and
identify and correct an unsafe condition
inspection information, and DCA/750XL/24A installation of support clamps and spiral
on an aviation product. The MCAI updated to introduce the revised SB.
describes the unsafe condition as wrap required by this AD. The average
The [CAA] AD is prompted by a
insufficient clearance between the pitot production inspection of installed pitot static
labor rate is $85 per work-hour.
tubes and the primary support at the plumbing which identified insufficient Required parts would cost about $25 per
flame arrester intersection. We are clearance between the pitot tubes and the product.
issuing this AD to require actions to primary support at the flame arrestor Based on these figures, we estimate
address the unsafe condition on these intersection. the cost of the AD on U.S. operators to
products. This AD requires inspecting the pitot be $2,420, or $110 per product.
static tubes for chafing damage, In addition, we estimate that any
DATES: This AD is effective January 10, necessary follow-on actions to replace
2019. replacing tubing as necessary, installing
an additional clamp for pitot static tube damaged tubing would take about 1
The Director of the Federal Register work-hour and require parts costing
approved the incorporation by reference support, protecting plumbing with
spiralwrap, and ensuring proper $25, for a cost of $110 per product. We
of a certain publication listed in the AD have no way of determining the number
as of January 10, 2019. clearance between the pitot tubes and
the primary support at the flame arrester of products that may need these actions.
ADDRESSES: You may examine the AD
intersection. The MCAI can be found in Authority for This Rulemaking
docket on the internet at http://
the AD docket on the internet at: https://
www.regulations.gov by searching for Title 49 of the United States Code
www.regulations.gov/
and locating Docket No. FAA–2018– specifies the FAA’s authority to issue
document?D=FAA-2018-0371-0002.
0371; or in person at Docket Operations, rules on aviation safety. Subtitle I,
U.S. Department of Transportation, Comments section 106, describes the authority of
Docket Operations, M–30, West We gave the public the opportunity to the FAA Administrator. ‘‘Subtitle VII:
Building Ground Floor, Room W12–140, participate in developing this AD. We Aviation Programs,’’ describes in more
1200 New Jersey Avenue SE, received no comments on the NPRM or detail the scope of the Agency’s
Washington, DC 20590. on the determination of the cost to the authority.
For service information identified in public. We are issuing this rulemaking under
this AD, contact Pacific Aerospace the authority described in ‘‘Subtitle VII,
Limited, Airport Road, Hamilton, Conclusion Part A, Subpart III, Section 44701:
Private Bag 3027, Hamilton 3240, New We reviewed the relevant data and General requirements.’’ Under that
Zealand; phone: +64 7843 6144; fax: +64 determined that air safety and the section, Congress charges the FAA with
843 6134; email: pacific@ public interest require adopting the AD promoting safe flight of civil aircraft in
aerospace.co.nz; internet: as proposed except for minor editorial air commerce by prescribing regulations
www.aerospace.co.nz. You may view changes and changes to clarify the for practices, methods, and procedures
this referenced service information at reference to the service information. We the Administrator finds necessary for
the FAA, Policy and Innovation have determined that these minor safety in air commerce. This regulation
khammond on DSK30JT082PROD with RULES
Division, 901 Locust, Kansas City, changes: is within the scope of that authority
Missouri 64106. For information on the • Are consistent with the intent that because it addresses an unsafe condition
availability of this material at the FAA, was proposed in the NPRM for that is likely to exist or develop on
call (816) 329–4148. It is also available correcting the unsafe condition; and products identified in this rulemaking
on the internet at http:// • Do not add any additional burden action.
www.regulations.gov by searching for upon the public than was already This AD is issued in accordance with
Docket No. FAA–2018–0371. proposed in the NPRM. authority delegated by the Executive
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![62702 Federal Register / Vol. 83, No. 234 / Thursday, December 6, 2018 / Rules and Regulations
Director, Aircraft Certification Service, (a) Effective Date (816) 329–4144; fax: (816) 329–4090; email:
as authorized by FAA Order 8000.51C. This AD becomes effective January 10, mike.kiesov@faa.gov. Before using any
In accordance with that order, issuance 2019. approved AMOC on any airplane to which
of ADs is normally a function of the the AMOC applies, notify your appropriate
(b) Affected ADs principal inspector (PI) in the FAA Flight
Compliance and Airworthiness
Division, but during this transition None. Standards District Office (FSDO), or lacking
period, the Executive Director has a PI, your local FSDO.
(c) Applicability
delegated the authority to issue ADs (2) Contacting the Manufacturer: For any
This AD applies to Pacific Aerospace requirement in this AD to obtain corrective
applicable to small airplanes, gliders, Limited Model 750XL airplanes, serial actions from a manufacturer, the action must
balloons, airships, domestic business jet numbers up to and including 200, instead be accomplished using a method
transport airplanes, and associated certificated in any category.
approved by the Manager, Small Airplane
appliances to the Director of the Policy
(d) Subject Standards Branch, FAA; or Civil Aviation
and Innovation Division. Authority of New Zealand (CAA).
Air Transport Association of America
Regulatory Findings (ATA) Code 34: Navigation. (h) Related Information
We determined that this AD will not (e) Reason Refer to MCAI CAA AD DCA/750XL/24A,
have federalism implications under This AD was prompted by mandatory dated March 22, 2018, for related
Executive Order 13132. This AD will continuing airworthiness information (MCAI) information. The MCAI can be found in the
not have a substantial direct effect on originated by an aviation authority of another AD docket on the internet at: https://
the States, on the relationship between country to identify and address an unsafe www.regulations.gov/document?D=FAA-
the national government and the States, condition on an aviation product. The MCAI 2018-0371-0002.
or on the distribution of power and describes the unsafe condition as insufficient
(i) Material Incorporated by Reference
responsibilities among the various clearance between the pitot tubes and the
levels of government. primary support at the flame arrester (1) The Director of the Federal Register
For the reasons discussed above, I intersection. We are issuing this AD to approved the incorporation by reference
prevent chafing between the pitot-static (IBR) of the service information listed in this
certify this AD:
plumbing and the flame arrestor, which paragraph under 5 U.S.C. 552(a) and 1 CFR
(1) Is not a ‘‘significant regulatory could lead to damage of the pitot-static lines. part 51.
action’’ under Executive Order 12866,
(f) Actions and Compliance (2) You must use this service information
(2) Is not a ‘‘significant rule’’ under as applicable to do the actions required by
the DOT Regulatory Policies and Unless already done, do the following this AD, unless the AD specifies otherwise.
Procedures (44 FR 11034, February 26, actions in paragraphs (f)(1) through (3) of this (i) Pacific Aerospace Service Bulletin
1979), AD.
PACSB/XL/094, Issue 2, dated March 20,
(3) Will not affect intrastate aviation (1) Within 100 hours time-in-service (TIS)
2018.
in Alaska, and after January 10, 2019 (the effective date of
(ii) [Reserved]
(4) Will not have a significant this AD) or within 60 days after January 10,
(3) For service information identified in
2019 (the effective date of this AD),
economic impact, positive or negative, this AD, contact Pacific Aerospace Limited,
whichever occurs first, inspect the pitot static
on a substantial number of small entities tubing adjacent to the flame arrestor for Airport Road, Hamilton, Private Bag 3027,
under the criteria of the Regulatory chafing damage. Hamilton 3240, New Zealand; phone: +64
Flexibility Act. (2) If any chafing damage is found during 7843 6144; fax: +64 843 6134; email: pacific@
the inspection required in paragraph (f)(1) of aerospace.co.nz; internet:
List of Subjects in 14 CFR Part 39 www.aerospace.co.nz.
this AD, before further flight, repair or
Air transportation, Aircraft, Aviation replace any damaged tubing and conduct a (4) You may view this service information
safety, Incorporation by reference, pitot and static leak check. at the FAA, Policy and Innovation Division,
Safety. (3) Within 100 hours TIS after January 10, 901 Locust, Kansas City, Missouri 64106. For
2019 (the effective date of this AD) or within information on the availability of this
Adoption of the Amendment 60 days after January 10, 2019 (the effective material at the FAA, call (816) 329–4148. In
Accordingly, under the authority date of this AD), whichever occurs first, addition, you can access this service
delegated to me by the Administrator, install an additional support clamp, protect information on the internet at http://
the FAA amends 14 CFR part 39 as plumbing with spiralwrap, and ensure proper www.regulations.gov by searching for and
clearance between the pitot tubes and the locating Docket No. FAA–2018–0371.
follows:
primary support at the flame arrester (5) You may view this service information
intersection. Follow paragraphs (3) through that is incorporated by reference at the
PART 39—AIRWORTHINESS
(6) of the Accomplishment Instructions in National Archives and Records
DIRECTIVES Pacific Aerospace Service Bulletin PACSB/ Administration (NARA). For information on
XL/094, Issue 2, dated March 20, 2018. the availability of this material at NARA, call
■ 1. The authority citation for part 39
continues to read as follows: (g) Other FAA AD Provisions 202–741–6030, or go to: http://
www.archives.gov/federal-register/cfr/ibr-
Authority: 49 U.S.C. 106(g), 40113, 44701. The following provisions also apply to this
AD: locations.html.
§ 39.13 [Amended] (1) Alternative Methods of Compliance Issued in Kansas City, Missouri, on
■ 2. The FAA amends § 39.13 by adding (AMOCs): The Manager, Small Airplane November 27, 2018.
Standards Branch, FAA, has the authority to Melvin J. Johnson,
the following new airworthiness
khammond on DSK30JT082PROD with RULES
approve AMOCs for this AD, if requested
directive (AD): using the procedures found in 14 CFR 39.19. Aircraft Certification Service, Deputy
Send information to ATTN: Mike Kiesov, Director, Policy and Innovation Division,
2018–23–16 Pacific Aerospace Limited:
AIR–601.
Amendment 39–19504; Docket No. Aerospace Engineer, FAA, Small Airplane
FAA–2018–0371; Product Identifier Standards Branch, 901 Locust, Room 301, [FR Doc. 2018–26364 Filed 12–4–18; 8:45 am]
2018–CE–005–AD. Kansas City, Missouri 64106; telephone: BILLING CODE 4910–13–P
VerDate Sep<11>2014 16:05 Dec 04, 2018 Jkt 247001 PO 00000 Frm 00014 Fmt 4700 Sfmt 4700 E:\FR\FM\06DER1.SGM 06DER1](https://thefederalregister.org/doc/83_FR_62935/page/2.svg)
Document Created: 2018-12-05 02:35:51
Document Modified: 2018-12-05 02:35:51
| 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 January 10, 2019. | |
| Contact | Mike Kiesov, Aerospace Engineer, FAA, Small Airplane Standards Branch, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; email: [email protected] | |
| FR Citation | 83 FR 62701 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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