81 FR 18804 - Airworthiness Directives; M7 Aerospace LLC Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 63 (April 1, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 63 (April 1, 2016)
| Page Range | 18804-18806 | |
| FR Document | 2016-07371 |
[Federal Register Volume 81, Number 63 (Friday, April 1, 2016)] [Proposed Rules] [Pages 18804-18806] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-07371] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-5431; Directorate Identifier 2015-CE-044-AD] RIN 2120-AA64 Airworthiness Directives; M7 Aerospace LLC Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for M7 Aerospace LLC Models SA26-AT, SA26-T, SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes. This proposed AD was prompted by reports of multiple cracks in the steel horizontal tube of the cockpit control column. This proposed AD would require inspection of the cockpit control column horizontal tube with repair or replacement as necessary of the cockpit control column. We are proposing this AD to correct the unsafe condition on these products. DATES: We must receive comments on this proposed AD by May 16, 2016. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact M7 Aerospace LLC, 10823 NE Entrance Road, San Antonio, Texas 78216; phone: (210) 824-9421; fax: (210) 804-7766; Internet: http://www.elbitsystems-us.com; email: [email protected]. You may view this referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call 816-329-4148. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 5431; 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 proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office [[Page 18805]] (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Andrew McAnaul, Aerospace Engineer, FAA, ASW-143 (c/o San Antonio MIDO), 10100 Reunion Place, Suite 650, San Antonio, Texas 78216; phone: (210) 308-3365; fax: (210) 308-3370; email: [email protected]. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-5431; Directorate Identifier 2015-CE-044-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD because of those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion The FAA received reports of multiple cracks in the cockpit control column horizontal tube at the corners of the access panel cutout, at the pulley bolt welds, and at the elevator arm weld in the steel horizontal tube of the control column on M7 Aerospace SA26, SA226, and SA227 airplanes. This condition, if not corrected, could result in partial or complete control column failure with partial or complete loss of pitch and/or roll control. Related Service Information Under 1 CFR Part 51 We reviewed M7 Aerospace LLC SA26 Series Service Bulletin (SB) 26- 27-002, M7 Aerospace LLC SA226 Series SB 226-27-078, M7 Aerospace LLC SA227 Series SB 227-27-058, and M7 Aerospace LLC SA227 Series SB CC7- 27-030, all dated October 8, 2015. The service information describes procedures for inspection of the cockpit control column horizontal tube for cracks and repair or replacement of the cockpit control column as necessary. All of the related 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 of this NPRM. FAA's Determination and Requirements of the Proposed AD We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of these same type designs. Proposed AD Requirements This proposed AD would require repetitive inspections of the cockpit control column horizontal tube for cracks and repair or replacement of the cockpit control column as necessary. Differences Between This Proposed AD and the Service Information We have revised the compliance times of the proposed AD to differ from service information. We have determined we have met the safety intent with the revised compliance times while allowing for clarity. The compliance times in the proposed AD action would take precedence over those in the service bulletin. Costs of Compliance We estimate that this proposed AD affects 350 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Inspection........................ 12 work-hours x $85 Not applicable...... $1,020 $357,000 per hour = $1,020. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary repairs/ replacements that would be required based on the results of the proposed inspection. We have no way of determining the number of airplanes that might need these repairs/replacements: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Repair cracks........................... 2 work-hours x $85 per Not applicable............ $170 hour = $170. Replace parts........................... 16 work-hours x $85 per $5,000.................... 6,360 hour = $1,360. ---------------------------------------------------------------------------------------------------------------- Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the [[Page 18806]] distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify this proposed regulation: (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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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): M7 Aerospace LLC: Docket No. FAA-2016-5431; Directorate Identifier 2015-CE-044-AD. (a) Comments Due Date We must receive comments by May 16, 2016. (b) Affected ADs None. (c) Applicability This AD applies to M7 Aerospace LLC Models SA26-AT, SA26-T, SA226-AT, SA226-T, SA226-T(B), SA226-TC, SA227-AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes, all serial numbers, certificated in any category. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 2700, Flight Controls. (e) Unsafe Condition This AD was prompted by reports of multiple cracks in the steel horizontal tube of the cockpit control column. We are issuing this AD to require repetitive inspections of the cockpit control column horizontal tube with repair or replacement, as necessary, of the cockpit control column. We are proposing this AD to correct the unsafe condition on these products. (f) Compliance Comply with paragraphs (g)(1) through (g)(2) of this AD using the following service bulletins within the compliance times specified below, unless already done: (1) For Models SA26-T and SA26-AT: M7 Aerospace LLC Service Bulletin (SB) 26-27-002, dated October 8, 2015; (2) For Models SA226-AT, SA226-T, SA226-T(B), and SA226-TC: M7 Aerospace LLC SB 226-27-078, dated October 8, 2015; (3) For Models SA227-AC(C-26A), SA227-AT, SA227-BC(C-26A), and SA227-TT: M7 Aerospace LLC SB 227-27-058, dated October 8, 2015; or (4) For Models SA227-CC and SA227-DC (C-26B): M7 Aerospace LLC SB CC7-27-030, dated October 8, 2015. (g) Actions (1) For all airplanes: Within the next 2,000 hours time-in- service (TIS) after the effective date of this AD or no later than when the airplane accumulates 20,000 hours TIS, whichever occurs later, do an initial inspection of the cockpit control column horizontal tube for cracks following paragraph 2.B. of the Accomplishment Instructions of the service bulletins identified in paragraphs (f)(1), (f)(2), (f)(3), or (f)(4) of this AD, as applicable; and repetitively inspect as follows: (i) For airplanes with less than 35,000 hours TIS as of the effective date of this AD: Repetitively inspect the cockpit control column horizontal tube for cracks every 5,000 hours TIS until the airplane reaches 35,000 hours TIS at which time do the inspection within 2,000 hours TIS from the last inspection or within the next 100 hours TIS, whichever occurs later, and then thereafter at intervals not to exceed 2,000 hours TIS. (ii) For airplanes with 35,000 hours TIS or more as of the effective date of this AD: Repetitively inspect the cockpit control column horizontal tube for cracks every 2,000 hours TIS. (2) For all airplanes: If any cracks are found following the inspections required in paragraphs (g)(1), (g)(1)(i), or (g)(1)(ii), as applicable, before further flight, repair the control column following paragraph 2.C. of the Accomplishment Instructions of the service bulletins identified in paragraphs (f)(1), (f)(2), (f)(3), or (f)(4) of this AD. (h) Paperwork Reduction Act Burden Statement A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Fort Worth Airplane Certification Office, 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 manager of the ACO, send it to the attention of the person identified in paragraph (j) of this AD. (2) 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. (j) Related Information (1) For more information about this AD, contact Andrew McAnaul, Aerospace Engineer, FAA, ASW-143 (c/o San Antonio MIDO), 10100 Reunion Place, Suite 650, San Antonio, Texas 78216; phone: (210) 308-3365; fax: (210) 308-3370; email: [email protected]. (2) For service information identified in this AD, contact M7 Aerospace LLC, 10823 NE Entrance Road, San Antonio, Texas 78216; phone: (210) 824-9421; fax: (210) 804-7766; Internet: http://www.elbitsystems-us.com; email: [email protected]. You may view this referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call 816-329-4148. Issued in Kansas City, Missouri, on March 28, 2016. Jacqueline Jambor, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-07371 Filed 3-31-16; 8:45 am] BILLING CODE 4910-13-P
![18804 Federal Register / Vol. 81, No. 63 / Friday, April 1, 2016 / Proposed Rules
TABLE 2—CURRENT DAIRY BOARD REPRESENTATION BASED ON AVERAGE U.S. TOTAL SOLIDS AND AVERAGE IMPORTED
TOTAL SOLIDS
Average total
Average total milk solids
Current number
milk solids represented per
of board seats
(lbs.) board member
(lbs.)
Domestic Producer .......................................................................................................... 23,461,555,556 36 651,709,877
Importer ............................................................................................................................ 589,296,653 2 294,648,327
Based on the calculations, it is member, to accurately represent the producer members. Table 2 reflects the
proposed that Dairy Board importer volume of imported total milk solids proposed changes.
member representation be reduced from compared to the volume of total solids
2 importer members to 1 importer represented by each of the 36 domestic
TABLE 3—PROPOSED DAIRY BOARD REPRESENTATION BASED ON U.S. TOTAL SOLIDS AND IMPORTED TOTAL SOLIDS
Average total
Average total milk solids
Current number
milk solids represented per
of board seats
(lbs.) board member
(lbs.)
Domestic Producer .......................................................................................................... 23,461,555,556 36 651,709,877
Importer ............................................................................................................................ 589,296,653 1 589,296,653
A 30-day comment period is provided DEPARTMENT OF TRANSPORTATION • Federal eRulemaking Portal: Go to
for interested persons to comment on http://www.regulations.gov. Follow the
this proposed rule. One term of office Federal Aviation Administration instructions for submitting comments.
for an importer member will expire on • Fax: 202–493–2251.
October 31, 2016. Thus, a 30-day 14 CFR Part 39 • Mail: U.S. Department of
comment period is provided for a timely Transportation, Docket Operations, M–
[Docket No. FAA–2016–5431; Directorate
announcement of the Dairy Board Identifier 2015–CE–044–AD]
30, West Building Ground Floor, Room
nomination solicitation in 2016. W12–140, 1200 New Jersey Avenue SE.,
RIN 2120–AA64 Washington, DC 20590.
List of Subjects in 7 CFR Part 1150 • Hand Delivery: Deliver to Mail
Airworthiness Directives; M7 address above between 9 a.m. and 5
Dairy products, Milk, Promotion, Aerospace LLC Airplanes p.m., Monday through Friday, except
Research.
AGENCY: Federal Aviation Federal holidays.
For the reasons set forth in the Administration (FAA), DOT. For service information identified in
preamble, it is proposed that 7 CFR part this proposed AD, contact M7
ACTION: Notice of proposed rulemaking
1150 be amended as follows: Aerospace LLC, 10823 NE Entrance
(NPRM). Road, San Antonio, Texas 78216; phone:
PART 1150—DAIRY PROMOTION (210) 824–9421; fax: (210) 804–7766;
SUMMARY: We propose to adopt a new
PROGRAM Internet: http://www.elbitsystems-
airworthiness directive (AD) for M7
Aerospace LLC Models SA26–AT, us.com; email: MetroTech@
■ 1. The authority citation for 7 CFR SA26–T, SA226–AT, SA226–T, SA226– M7Aerospace.com. You may view this
part 1150 continues to read as follows: T(B), SA226–TC, SA227–AC (C–26A), referenced service information at the
Authority: 7 U.S.C. 4501–4514 and 7 SA227–AT, SA227–BC (C–26A), FAA, Small Airplane Directorate, 901
U.S.C. 7401. SA227–CC, SA227–DC (C–26B), and Locust, Kansas City, Missouri 64106.
SA227–TT airplanes. This proposed AD For information on the availability of
■ 2. In § 1150.131, paragraph (c) is this material at the FAA, call 816–329–
was prompted by reports of multiple
revised to read as follows: 4148.
cracks in the steel horizontal tube of the
§ 1150.131 Establishment and cockpit control column. This proposed Examining the AD Docket
membership. AD would require inspection of the You may examine the AD docket on
* * * * * cockpit control column horizontal tube the Internet at http://
(c) One member of the board shall be with repair or replacement as necessary www.regulations.gov by searching for
an importer who is subject to of the cockpit control column. We are and locating Docket No. FAA–2016–
proposing this AD to correct the unsafe
Lhorne on DSK5TPTVN1PROD with PROPOSALS
assessments under § 1150.152(b). 5431; or in person at the Docket
condition on these products. Management Facility between 9 a.m.
* * * * *
DATES: We must receive comments on and 5 p.m., Monday through Friday,
Dated: March 29, 2016. this proposed AD by May 16, 2016. except Federal holidays. The AD docket
Erin Morris, ADDRESSES: You may send comments, contains this proposed AD, the
Associate Administrator. using the procedures found in 14 CFR regulatory evaluation, any comments
[FR Doc. 2016–07413 Filed 3–31–16; 8:45 am] 11.43 and 11.45, by any of the following received, and other information. The
BILLING CODE P methods: street address for the Docket Office
VerDate Sep<11>2014 14:16 Mar 31, 2016 Jkt 238001 PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 E:\FR\FM\01APP1.SGM 01APP1](https://thefederalregister.org/doc/81_FR_18867/page/1.svg)
![18806 Federal Register / Vol. 81, No. 63 / Friday, April 1, 2016 / Proposed Rules
distribution of power and with repair or replacement, as necessary, of instructions, completing and reviewing the
responsibilities among the various the cockpit control column. We are collection of information. All responses to
levels of government. proposing this AD to correct the unsafe this collection of information are mandatory.
condition on these products. Comments concerning the accuracy of this
For the reasons discussed above, I
burden and suggestions for reducing the
certify this proposed regulation: (f) Compliance
burden should be directed to the FAA at: 800
(1) Is not a ‘‘significant regulatory Comply with paragraphs (g)(1) through Independence Ave. SW., Washington, DC
action’’ under Executive Order 12866, (g)(2) of this AD using the following service 20591, Attn: Information Collection
(2) Is not a ‘‘significant rule’’ under bulletins within the compliance times Clearance Officer, AES–200.
the DOT Regulatory Policies and specified below, unless already done:
(1) For Models SA26–T and SA26–AT: M7 (i) Alternative Methods of Compliance
Procedures (44 FR 11034, February 26, (AMOCs)
Aerospace LLC Service Bulletin (SB) 26–27–
1979), 002, dated October 8, 2015;
(3) Will not affect intrastate aviation (1) The Manager, Fort Worth Airplane
(2) For Models SA226–AT, SA226–T, Certification Office, FAA, has the authority to
in Alaska, and SA226–T(B), and SA226–TC: M7 Aerospace approve AMOCs for this AD, if requested
(4) Will not have a significant LLC SB 226–27–078, dated October 8, 2015; using the procedures found in 14 CFR 39.19.
economic impact, positive or negative, (3) For Models SA227–AC(C–26A), SA227– In accordance with 14 CFR 39.19, send your
on a substantial number of small entities AT, SA227–BC(C–26A), and SA227–TT: M7 request to your principal inspector or local
under the criteria of the Regulatory Aerospace LLC SB 227–27–058, dated Flight Standards District Office, as
Flexibility Act. October 8, 2015; or appropriate. If sending information directly
(4) For Models SA227–CC and SA227–DC to the manager of the ACO, send it to the
List of Subjects in 14 CFR Part 39 (C–26B): M7 Aerospace LLC SB CC7–27–030, attention of the person identified in
dated October 8, 2015. paragraph (j) of this AD.
Air transportation, Aircraft, Aviation
safety, Incorporation by reference, (g) Actions (2) Before using any approved AMOC,
notify your appropriate principal inspector,
Safety. (1) For all airplanes: Within the next 2,000 or lacking a principal inspector, the manager
hours time-in-service (TIS) after the effective
The Proposed Amendment of the local flight standards district office/
date of this AD or no later than when the
certificate holding district office.
Accordingly, under the authority airplane accumulates 20,000 hours TIS,
delegated to me by the Administrator, whichever occurs later, do an initial (j) Related Information
the FAA proposes to amend 14 CFR part inspection of the cockpit control column (1) For more information about this AD,
horizontal tube for cracks following contact Andrew McAnaul, Aerospace
39 as follows: paragraph 2.B. of the Accomplishment Engineer, FAA, ASW–143 (c/o San Antonio
Instructions of the service bulletins identified MIDO), 10100 Reunion Place, Suite 650, San
PART 39—AIRWORTHINESS in paragraphs (f)(1), (f)(2), (f)(3), or (f)(4) of
DIRECTIVES Antonio, Texas 78216; phone: (210) 308–
this AD, as applicable; and repetitively 3365; fax: (210) 308–3370; email:
inspect as follows:
■ 1. The authority citation for part 39 andrew.mcanaul@faa.gov.
(i) For airplanes with less than 35,000
continues to read as follows: (2) For service information identified in
hours TIS as of the effective date of this AD:
this AD, contact M7 Aerospace LLC, 10823
Authority: 49 U.S.C. 106(g), 40113, 44701. Repetitively inspect the cockpit control
NE Entrance Road, San Antonio, Texas
column horizontal tube for cracks every
78216; phone: (210) 824–9421; fax: (210)
§ 39.13 [Amended] 5,000 hours TIS until the airplane reaches
804–7766; Internet: http://www.elbitsystems-
■ 2. The FAA amends § 39.13 by adding 35,000 hours TIS at which time do the
us.com; email: MetroTech@
inspection within 2,000 hours TIS from the
the following new airworthiness last inspection or within the next 100 hours
M7Aerospace.com. You may view this
directive (AD): referenced service information at the FAA,
TIS, whichever occurs later, and then
thereafter at intervals not to exceed 2,000 Small Airplane Directorate, 901 Locust,
M7 Aerospace LLC: Docket No. FAA–2016– Kansas City, Missouri 64106. For information
5431; Directorate Identifier 2015–CE– hours TIS.
(ii) For airplanes with 35,000 hours TIS or on the availability of this material at the
044–AD. FAA, call 816–329–4148.
more as of the effective date of this AD:
(a) Comments Due Date Repetitively inspect the cockpit control Issued in Kansas City, Missouri, on March
We must receive comments by May 16, column horizontal tube for cracks every 28, 2016.
2016. 2,000 hours TIS. Jacqueline Jambor,
(2) For all airplanes: If any cracks are
(b) Affected ADs Acting Manager, Small Airplane Directorate,
found following the inspections required in
paragraphs (g)(1), (g)(1)(i), or (g)(1)(ii), as Aircraft Certification Service.
None.
applicable, before further flight, repair the [FR Doc. 2016–07371 Filed 3–31–16; 8:45 am]
(c) Applicability control column following paragraph 2.C. of BILLING CODE 4910–13–P
This AD applies to M7 Aerospace LLC the Accomplishment Instructions of the
Models SA26–AT, SA26–T, SA226–AT, service bulletins identified in paragraphs
SA226–T, SA226–T(B), SA226–TC, SA227– (f)(1), (f)(2), (f)(3), or (f)(4) of this AD. DEPARTMENT OF TRANSPORTATION
AC (C–26A), SA227–AT, SA227–BC (C–26A),
SA227–CC, SA227–DC (C–26B), and SA227– (h) Paperwork Reduction Act Burden
Statement Federal Aviation Administration
TT airplanes, all serial numbers, certificated
in any category. A federal agency may not conduct or
sponsor, and a person is not required to 14 CFR Part 39
(d) Subject respond to, nor shall a person be subject to [Docket No. FAA–2016–4551; Directorate
Joint Aircraft System Component (JASC)/ a penalty for failure to comply with a Identifier 2016–NE–07–AD]
Lhorne on DSK5TPTVN1PROD with PROPOSALS
Air Transport Association (ATA) of America collection of information subject to the
Code 2700, Flight Controls. requirements of the Paperwork Reduction RIN 2120–AA64
Act unless that collection of information
(e) Unsafe Condition displays a current valid OMB Control Airworthiness Directives; Rolls-Royce
This AD was prompted by reports of Number. The OMB Control Number for this Deutschland Ltd & Co KG Turbofan
multiple cracks in the steel horizontal tube information collection is 2120–0056. Public Engines
of the cockpit control column. We are issuing reporting for this collection of information is
this AD to require repetitive inspections of estimated to be approximately 5 minutes per AGENCY:Federal Aviation
the cockpit control column horizontal tube response, including the time for reviewing Administration (FAA), DOT.
VerDate Sep<11>2014 14:16 Mar 31, 2016 Jkt 238001 PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 E:\FR\FM\01APP1.SGM 01APP1](https://thefederalregister.org/doc/81_FR_18867/page/3.svg)
Document Created: 2016-04-06 00:07:53
Document Modified: 2016-04-06 00:07:53
| 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 | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by May 16, 2016. | |
| Contact | Andrew McAnaul, Aerospace Engineer, FAA, ASW-143 (c/o San Antonio MIDO), 10100 Reunion Place, Suite 650, San Antonio, Texas 78216; phone: (210) 308-3365; fax: (210) 308-3370; email: [email protected] | |
| FR Citation | 81 FR 18804 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR