83 FR 16792 - Airworthiness Directives; Saab AB, Saab Aeronautics (Formerly Known as Saab AB, Saab Aerosystems) Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 74 (April 17, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 74 (April 17, 2018)
| Page Range | 16792-16794 | |
| FR Document | 2018-07636 |
[Federal Register Volume 83, Number 74 (Tuesday, April 17, 2018)] [Proposed Rules] [Pages 16792-16794] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-07636] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0271; Product Identifier 2017-NM-111-AD] RIN 2120-AA64 Airworthiness Directives; Saab AB, Saab Aeronautics (Formerly Known as Saab AB, Saab Aerosystems) Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to supersede Airworthiness Directive (AD) 2016-13- 06, which applies to certain Saab AB, Saab Aeronautics Model 340A (SAAB/SF340A) and SAAB 340B airplanes. AD 2016-13-06 requires a revision of the applicable airplane flight manual (AFM), repetitive inspections of the horizontal stabilizer de-icing boots, and applicable corrective actions. Since we issued AD 2016-13-06, the manufacturer has developed an improved de-icing boot. This proposed AD would continue to require a revision of the applicable AFM, repetitive inspections of the horizontal stabilizer de-icing boots, and applicable corrective actions. This proposed AD would also require replacement of single stitched de-icing boots with improved double stitched boots, and re- identification of the modified horizontal stabilizer leading edge. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by June 1, 2018. 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 NPRM, contact Saab AB, Saab Aeronautics, SE-581 88, Link[ouml]ping, Sweden; telephone: +46 13 18 5591; fax: +46 13 18 4874; email: saab340techsupport@saabgroup.com; internet: http://www.saabgroup.com. You may view this referenced service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. 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-2018- 0271; 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 Operations office (telephone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3220. 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-2018-0271; Product Identifier 2017-NM-111-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 based on 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 We issued AD 2016-13-06, Amendment 39-18570 (81 FR 41432, June 27, 2016) (``AD 2016-13-06''), for certain Saab AB, Saab Aeronautics Model 340A (SAAB/SF340A) and SAAB 340B airplanes. AD 2016-13-06 was prompted by reports of ruptured horizontal stabilizer de-icing boots. AD 2016- 13-06 requires a revision of the applicable AFM, repetitive inspections of the horizontal stabilizer de-icing boots, and applicable corrective actions. We issued AD 2016-13-06 to detect and correct damage of the de-icing boot; such damage could lead to a ruptured boot, severe vibrations, and possible reduced control of the airplane. Since we issued AD 2016-13-06, the manufacturer has developed an improved de-icing boot, reinforced through double stitch lines. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2017-0144, dated August 9, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Saab AB, Saab Aeronautics Model 340A (SAAB/SF340A) and SAAB 340B airplanes. The MCAI states: Several occurrences were reported of rupture of the horizontal stabilizer de-icing boot in flight. In some of the reported events, the de-icing boot had formed a large open scoop. This condition, if not detected and corrected, could lead to complete loss of the de-icing function within its associated zone and severe vibrations, possibly resulting in reduced control of the aeroplane. To address this potential unsafe condition, Saab AB, Aeronautics (hereafter referred to as ``Saab'' in this [EASA] AD) issued Alert Operations Bulletin (AOB) No. 12 and AOB No. 23 as temporary measures, recommending to select Flaps 0 for landing in the event of a suspected rupture of the de-icing boot on the horizontal stabilizer. In addition, Saab issued SB [Service Bulletin] 340-30- 094 providing instructions for inspection of de-icing boots. [[Page 16793]] Consequently, EASA issued AD 2015-0129 [which corresponds to FAA AD 2016-13-06] to require amendment of the applicable Aircraft Flight Manual (AFM), repetitive inspections of the horizontal stabilizer de-icing boots and, depending on findings, accomplishment of applicable corrective action(s). Since that [EASA] AD was issued, Saab developed an improved de- icing boot, reinforced through double stitch lines, and issued SB 340-30-095 providing instructions for boot replacement. For the reason described above, this [EASA] AD retains the requirements of EASA AD 2015-0129, which is superseded, and requires replacement of single stitched de-icing boots, installed on the left-hand (LH) and right-hand (RH) horizontal stabilizer, with improved double stitched boots, and re-identification of the modified horizontal stabilizer leading edge. 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-2018- 0271. Related Service Information Under 1 CFR Part 51 Saab AB, Saab Aeronautics has issued the following service information. Service Bulletin 340-30-094, dated March 27, 2015. This service information describes procedures for repetitive detailed inspections of the de-icing boots installed on the horizontal stabilizers, and repair and replacement of damaged de-icing boots. Service Bulletin 340-30-095, dated April 3, 2017. This service information describes procedures for replacement of single stitched de-icing boots with improved double stitched boots, and re- identification of the modified horizontal stabilizer leading edge. Saab AB, Saab Aeronautics has also issued the following AFMs, which describe performance limitations and general data. These AFMs are distinct since they apply to different airplane models in different configurations. AFM 340A 001, Revision 57, dated March 27, 2015. AFM 340B 001, Revision 35, dated March 27, 2015. AFM 340B 010, Revision 28, dated March 27, 2015. 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. FAA's Determination and Requirements of This Proposed AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of these same type designs. Costs of Compliance We estimate that this proposed AD affects 51 airplanes of U.S. registry. The actions required by AD 2016-13-06, and retained in this proposed AD take about 6 work-hours per product, at an average labor rate of $85 per work-hour. Based on these figures, the estimated cost of the actions that are required by AD 2016-13-06 is $510 per product. In addition, we estimate that any necessary follow-on actions required by AD 2016-13-06, and retained in this proposed AD take about 6 work-hours and require parts costing $9,500, for a cost of $10,010 per product. We have no way of determining the number of aircraft that might need these actions. We also estimate that it would take about 6 work-hours per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Required parts would cost about $13,500 per product. Based on these figures, we estimate the cost of this proposed AD on U.S. operators to be $714,510, or $14,010 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 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 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 transport category airplanes to the Director of the System Oversight Division. 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 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 removing Airworthiness Directive (AD) 2016-13-06, Amendment 39-18570 (81 FR 41432, June 27, 2016), and adding the following new AD: Saab AB, Saab Aeronautics (Formerly Known as Saab AB, Saab Aerosystems): Docket No. FAA-2018-0271; Product Identifier 2017-NM- 111-AD. (a) Comments Due Date We must receive comments by June 1, 2018. [[Page 16794]] (b) Affected ADs This AD replaces AD 2016-13-06, Amendment 39-18570 (81 FR 41432, June 27, 2016) (``AD 2016-13-06''). (c) Applicability This AD applies to Saab AB, Saab Aeronautics (formerly known as Saab AB, Saab Aerosystems) airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2), of this AD. (1) Saab AB, Saab Aeronautics Model 340A (SAAB/SF340A) airplanes, serial numbers 004 through 138 inclusive, if Saab modification 1462 has been embodied in production, or Saab Service Bulletin 340-55-008 has been embodied in service, except those that have also embodied Saab modification 1793 in production, or Saab Service Bulletin 340-55-010 in service; and serial numbers 139 through 159 inclusive. (2) Saab AB, Saab Aeronautics Model SAAB 340B airplanes, serial numbers 160 through 459 inclusive. (d) Subject Air Transport Association (ATA) of America Code 30, Ice and rain protection. (e) Reason This AD was prompted by reports of ruptured horizontal stabilizer de-icing boots. We are issuing this AD to detect and correct ruptured horizontal stabilizer de-icing boots, which could lead to complete loss of the de-icing function within its associated zone and severe vibrations, possibly resulting in reduced control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Revision of the Airplane Flight Manual (AFM), With No Changes This paragraph restates the requirements of paragraph (g) of AD 2016-13-06, with no changes. Within 30 days after August 1, 2016 (the effective date of AD 2016-13-06), revise the ``Abnormal Procedures'' section of the applicable Saab 340 AFM to incorporate the revision specified in paragraphs (g)(1) through (g)(3) of this AD. (1) For Saab AB, Saab Aeronautics Model 340A (SAAB/SF340A) airplanes, revise AFM 340A 001 by incorporating Revision 57, dated March 27, 2015. (2) For Saab AB, Saab Aeronautics Model SAAB 340B airplanes, revise AFM 340B 001 by incorporating Revision 35, dated March 27, 2015. (3) For Saab AB, Saab Aeronautics Model SAAB 340B airplanes with extended wing tips, revise AFM 340B 010 by incorporating Revision 28, dated March 27, 2015. (h) Retained Inspection/Replacement, With No Changes This paragraph restates the requirements of paragraph (h) of AD 2016-13-06, with no changes. Within 400 flight hours or 6 months, whichever occurs first after August 1, 2016 (the effective date of AD 2016-13-06), do a detailed inspection for damage of the horizontal stabilizer de-icing boots, and existing repairs of horizontal stabilizer de-icing boots, in accordance with the Accomplishment Instructions of Saab Service Bulletin 340-30-094, dated March 27, 2015. Repeat the inspection thereafter at intervals not to exceed 400 flight hours. If, during any inspection required by this paragraph, any damage or existing repair outside the limits specified in Saab Service Bulletin 340-30-094, dated March 27, 2015, is found, before further flight, repair or replace the horizontal stabilizer de-icing boots, in accordance with the Accomplishment Instructions of Saab Service Bulletin 340-30-094, dated March 27, 2015. Repair or replacement on an airplane of the horizontal stabilizer de-icing boots, as required by this paragraph, does not constitute terminating action for the repetitive inspections required by this paragraph for that airplane. (i) New Requirement of This AD: Modification Within 18 months after the effective date of this AD, modify the airplane by replacing the single stitched de-icing boots installed on the left-hand (LH) and right-hand (RH) horizontal stabilizers with double stitched de-icing boots and re-identify the LH and RH horizontal stabilizer leading edge, in accordance with the Accomplishment Instructions of Saab Service Bulletin 340-30-095, dated April 3, 2017. (j) Terminating Action Modification of the airplane as required by paragraph (i) of this AD, constitutes terminating action for the repetitive inspections required by paragraph (h) of this AD, for that airplane. (k) Other FAA AD Provisions (1) Alternative Methods of Compliance (AMOCs): The Manager, International Section, Transport Standards 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 request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Section, send it to the attention of the person identified in paragraph (l)(2) of this AD. Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 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. (2) Contacting the Manufacturer: As of the effective date of this AD, 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, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or Saab AB, Saab Aeronautics EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (l) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2017-0144, dated August 9, 2017, for related information. This MCAI may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0271. (2) For more information about this AD, contact Shahram Daneshmandi, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3220. (3) For service information identified in this AD, contact Saab AB, Saab Aeronautics, SE-581 88, Link[ouml]ping, Sweden; telephone: +46 13 18 5591; fax: +46 13 18 4874; email: saab340techsupport@saabgroup.com; internet: http://www.saabgroup.com. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. Issued in Des Moines, Washington, on March 30, 2018. Chris Spangenberg, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-07636 Filed 4-16-18; 8:45 am] BILLING CODE 4910-13-P
![16792 Federal Register / Vol. 83, No. 74 / Tuesday, April 17, 2018 / Proposed Rules
on the internet at http://www.regulations.gov the modified horizontal stabilizer 2018–0271; Product Identifier 2017–
by searching for and locating Docket No. leading edge. We are proposing this AD NM–111–AD’’ at the beginning of your
FAA–2018–0277. to address the unsafe condition on these comments. We specifically invite
(2) For more information about this AD, products. comments on the overall regulatory,
contact Dan Rodina, Aerospace Engineer,
International Section, Transport Standards DATES: We must receive comments on economic, environmental, and energy
Branch, FAA, 2200 South 216th St., Des this proposed AD by June 1, 2018. aspects of this proposed AD. We will
Moines, WA 98198; telephone and fax 206– ADDRESSES: You may send comments,
consider all comments received by the
231–3225. using the procedures found in 14 CFR closing date and may amend this
(3) For service information identified in 11.43 and 11.45, by any of the following proposed AD based on those comments.
this AD, contact Airbus SAS, Airworthiness We will post all comments we
methods:
Office—EAW, 1 Rond Point Maurice receive, without change, to http://
Bellonte, 31707 Blagnac Cedex, France;
• Federal eRulemaking Portal: Go to
www.regulations.gov, including any
telephone +33 5 61 93 36 96; fax +33 5 61 http://www.regulations.gov. Follow the
personal information you provide. We
93 44 51; email account.airworth-eas@ instructions for submitting comments.
• Fax: 202–493–2251. will also post a report summarizing each
airbus.com; internet http://www.airbus.com. substantive verbal contact we receive
You may view this service information at the • Mail: U.S. Department of
FAA, Transport Standards Branch, 2200 Transportation, Docket Operations, M– about this proposed AD.
South 216th St., Des Moines, WA. For 30, West Building Ground Floor, Room Discussion
information on the availability of this W12–140, 1200 New Jersey Avenue SE,
material at the FAA, call 206–231–3195. We issued AD 2016–13–06,
Washington, DC 20590. Amendment 39–18570 (81 FR 41432,
Issued in Des Moines, Washington, on • Hand Delivery: Deliver to Mail June 27, 2016) (‘‘AD 2016–13–06’’), for
March 30, 2018. address above between 9 a.m. and 5 certain Saab AB, Saab Aeronautics
Chris Spangenberg, p.m., Monday through Friday, except Model 340A (SAAB/SF340A) and SAAB
Acting Director, System Oversight Division, Federal holidays. 340B airplanes. AD 2016–13–06 was
Aircraft Certification Service. For service information identified in prompted by reports of ruptured
[FR Doc. 2018–07626 Filed 4–16–18; 8:45 am] this NPRM, contact Saab AB, Saab horizontal stabilizer de-icing boots. AD
BILLING CODE 4910–13–P Aeronautics, SE–581 88, Linköping, 2016–13–06 requires a revision of the
Sweden; telephone: +46 13 18 5591; fax: applicable AFM, repetitive inspections
+46 13 18 4874; email: of the horizontal stabilizer de-icing
DEPARTMENT OF TRANSPORTATION saab340techsupport@saabgroup.com; boots, and applicable corrective actions.
internet: http://www.saabgroup.com. We issued AD 2016–13–06 to detect and
Federal Aviation Administration You may view this referenced service correct damage of the de-icing boot;
information at the FAA, Transport such damage could lead to a ruptured
14 CFR Part 39 Standards Branch, 2200 South 216th St., boot, severe vibrations, and possible
[Docket No. FAA–2018–0271; Product Des Moines, WA. For information on the reduced control of the airplane.
Identifier 2017–NM–111–AD] availability of this material at the FAA, Since we issued AD 2016–13–06, the
call 206–231–3195. manufacturer has developed an
RIN 2120–AA64
Examining the AD Docket improved de-icing boot, reinforced
Airworthiness Directives; Saab AB, through double stitch lines.
You may examine the AD docket on The European Aviation Safety Agency
Saab Aeronautics (Formerly Known as the internet at http://
Saab AB, Saab Aerosystems) (EASA), which is the Technical Agent
www.regulations.gov by searching for for the Member States of the European
Airplanes and locating Docket No. FAA–2018– Union, has issued EASA AD 2017–0144,
AGENCY: Federal Aviation 0271; or in person at the Docket dated August 9, 2017 (referred to after
Administration (FAA), DOT. Management Facility between 9 a.m. this as the Mandatory Continuing
and 5 p.m., Monday through Friday, Airworthiness Information, or ‘‘the
ACTION: Notice of proposed rulemaking
except Federal holidays. The AD docket MCAI’’), to correct an unsafe condition
(NPRM).
contains this proposed AD, the for certain Saab AB, Saab Aeronautics
SUMMARY: We propose to supersede regulatory evaluation, any comments Model 340A (SAAB/SF340A) and SAAB
Airworthiness Directive (AD) 2016–13– received, and other information. The 340B airplanes. The MCAI states:
06, which applies to certain Saab AB, street address for the Docket Operations
office (telephone: 800–647–5527) is in Several occurrences were reported of
Saab Aeronautics Model 340A (SAAB/ rupture of the horizontal stabilizer de-icing
SF340A) and SAAB 340B airplanes. AD the ADDRESSES section. Comments will boot in flight. In some of the reported events,
2016–13–06 requires a revision of the be available in the AD docket shortly the de-icing boot had formed a large open
applicable airplane flight manual after receipt. scoop.
(AFM), repetitive inspections of the FOR FURTHER INFORMATION CONTACT: This condition, if not detected and
horizontal stabilizer de-icing boots, and Shahram Daneshmandi, Aerospace corrected, could lead to complete loss of the
Engineer, International Section, de-icing function within its associated zone
applicable corrective actions. Since we and severe vibrations, possibly resulting in
issued AD 2016–13–06, the Transport Standards Branch, FAA, 2200 reduced control of the aeroplane.
manufacturer has developed an South 216th St., Des Moines, WA 98198; To address this potential unsafe condition,
improved de-icing boot. This proposed telephone and fax: 206–231–3220. Saab AB, Aeronautics (hereafter referred to as
amozie on DSK30RV082PROD with PROPOSALS
AD would continue to require a revision SUPPLEMENTARY INFORMATION: ‘‘Saab’’ in this [EASA] AD) issued Alert
of the applicable AFM, repetitive Operations Bulletin (AOB) No. 12 and AOB
inspections of the horizontal stabilizer Comments Invited No. 23 as temporary measures,
de-icing boots, and applicable corrective recommending to select Flaps 0 for landing
We invite you to send any written
in the event of a suspected rupture of the de-
actions. This proposed AD would also relevant data, views, or arguments about icing boot on the horizontal stabilizer. In
require replacement of single stitched this proposal. Send your comments to addition, Saab issued SB [Service Bulletin]
de-icing boots with improved double an address listed under the ADDRESSES 340–30–094 providing instructions for
stitched boots, and re-identification of section. Include ‘‘Docket No. FAA– inspection of de-icing boots.
VerDate Sep<11>2014 17:36 Apr 16, 2018 Jkt 244001 PO 00000 Frm 00006 Fmt 4702 Sfmt 4702 E:\FR\FM\17APP1.SGM 17APP1](https://thefederalregister.org/doc/83_FR_16866/page/1.svg)
![Federal Register / Vol. 83, No. 74 / Tuesday, April 17, 2018 / Proposed Rules 16793
Consequently, EASA issued AD 2015–0129 Design Authority, we have been notified of ADs is normally a function of the
[which corresponds to FAA AD 2016–13–06] of the unsafe condition described in the Compliance and Airworthiness
to require amendment of the applicable MCAI and service information Division, but during this transition
Aircraft Flight Manual (AFM), repetitive referenced above. We are proposing this period, the Executive Director has
inspections of the horizontal stabilizer de-
icing boots and, depending on findings,
AD because we evaluated all pertinent delegated the authority to issue ADs
accomplishment of applicable corrective information and determined an unsafe applicable to transport category
action(s). condition exists and is likely to exist or airplanes to the Director of the System
Since that [EASA] AD was issued, Saab develop on other products of these same Oversight Division.
developed an improved de-icing boot, type designs.
reinforced through double stitch lines, and
Regulatory Findings
issued SB 340–30–095 providing instructions Costs of Compliance
We determined that this proposed AD
for boot replacement. We estimate that this proposed AD would not have federalism implications
For the reason described above, this affects 51 airplanes of U.S. registry.
[EASA] AD retains the requirements of EASA under Executive Order 13132. This
The actions required by AD 2016–13– proposed AD would not have a
AD 2015–0129, which is superseded, and 06, and retained in this proposed AD
requires replacement of single stitched de- substantial direct effect on the States, on
take about 6 work-hours per product, at the relationship between the national
icing boots, installed on the left-hand (LH)
and right-hand (RH) horizontal stabilizer, an average labor rate of $85 per work- Government and the States, or on the
with improved double stitched boots, and re- hour. Based on these figures, the distribution of power and
identification of the modified horizontal estimated cost of the actions that are responsibilities among the various
stabilizer leading edge. required by AD 2016–13–06 is $510 per levels of government.
You may examine the MCAI in the product.
In addition, we estimate that any For the reasons discussed above, I
AD docket on the internet at http:// certify this proposed regulation:
necessary follow-on actions required by
www.regulations.gov by searching for
AD 2016–13–06, and retained in this 1. Is not a ‘‘significant regulatory
and locating Docket No. FAA–2018–
proposed AD take about 6 work-hours action’’ under Executive Order 12866;
0271.
and require parts costing $9,500, for a 2. Is not a ‘‘significant rule’’ under the
Related Service Information Under cost of $10,010 per product. We have no DOT Regulatory Policies and Procedures
1 CFR Part 51 way of determining the number of (44 FR 11034, February 26, 1979);
Saab AB, Saab Aeronautics has issued aircraft that might need these actions. 3. Will not affect intrastate aviation in
the following service information. We also estimate that it would take
Alaska; and
• Service Bulletin 340–30–094, dated about 6 work-hours per product to
comply with the basic requirements of 4. Will not have a significant
March 27, 2015. This service economic impact, positive or negative,
information describes procedures for this proposed AD. The average labor
rate is $85 per work-hour. Required on a substantial number of small entities
repetitive detailed inspections of the de- under the criteria of the Regulatory
icing boots installed on the horizontal parts would cost about $13,500 per
product. Based on these figures, we Flexibility Act.
stabilizers, and repair and replacement
of damaged de-icing boots. estimate the cost of this proposed AD on List of Subjects in 14 CFR Part 39
• Service Bulletin 340–30–095, dated U.S. operators to be $714,510, or
April 3, 2017. This service information $14,010 per product. Air transportation, Aircraft, Aviation
describes procedures for replacement of safety, Incorporation by reference,
Authority for This Rulemaking Safety.
single stitched de-icing boots with
improved double stitched boots, and re- Title 49 of the United States Code
The Proposed Amendment
identification of the modified horizontal specifies the FAA’s authority to issue
stabilizer leading edge. rules on aviation safety. Subtitle I, Accordingly, under the authority
Saab AB, Saab Aeronautics has also section 106, describes the authority of delegated to me by the Administrator,
issued the following AFMs, which the FAA Administrator. ‘‘Subtitle VII: the FAA proposes to amend 14 CFR part
describe performance limitations and Aviation Programs,’’ describes in more 39 as follows:
general data. These AFMs are distinct detail the scope of the Agency’s
since they apply to different airplane authority. PART 39—AIRWORTHINESS
models in different configurations. We are issuing this rulemaking under DIRECTIVES
• AFM 340A 001, Revision 57, dated the authority described in ‘‘Subtitle VII,
March 27, 2015. Part A, Subpart III, Section 44701: ■ 1. The authority citation for part 39
• AFM 340B 001, Revision 35, dated General requirements.’’ Under that continues to read as follows:
March 27, 2015. section, Congress charges the FAA with Authority: 49 U.S.C. 106(g), 40113, 44701.
• AFM 340B 010, Revision 28, dated promoting safe flight of civil aircraft in
March 27, 2015. air commerce by prescribing regulations § 39.13 [Amended]
This service information is reasonably for practices, methods, and procedures ■ 2. The FAA amends § 39.13 by
available because the interested parties the Administrator finds necessary for removing Airworthiness Directive (AD)
have access to it through their normal safety in air commerce. This regulation 2016–13–06, Amendment 39–18570 (81
course of business or by the means is within the scope of that authority FR 41432, June 27, 2016), and adding
identified in the ADDRESSES section. because it addresses an unsafe condition the following new AD:
amozie on DSK30RV082PROD with PROPOSALS
that is likely to exist or develop on
FAA’s Determination and Requirements products identified in this rulemaking Saab AB, Saab Aeronautics (Formerly
of This Proposed AD action. Known as Saab AB, Saab Aerosystems):
This AD is issued in accordance with Docket No. FAA–2018–0271; Product
This product has been approved by
Identifier 2017–NM–111–AD.
the aviation authority of another authority delegated by the Executive
country, and is approved for operation Director, Aircraft Certification Service, (a) Comments Due Date
in the United States. Pursuant to our as authorized by FAA Order 8000.51C. We must receive comments by June 1,
bilateral agreement with the State of In accordance with that order, issuance 2018.
VerDate Sep<11>2014 17:36 Apr 16, 2018 Jkt 244001 PO 00000 Frm 00007 Fmt 4702 Sfmt 4702 E:\FR\FM\17APP1.SGM 17APP1](https://thefederalregister.org/doc/83_FR_16866/page/2.svg)
![16794 Federal Register / Vol. 83, No. 74 / Tuesday, April 17, 2018 / Proposed Rules
(b) Affected ADs icing boots, in accordance with the information. This MCAI may be found in the
This AD replaces AD 2016–13–06, Accomplishment Instructions of Saab Service AD docket on the internet at http://
Amendment 39–18570 (81 FR 41432, June Bulletin 340–30–094, dated March 27, 2015. www.regulations.gov by searching for and
27, 2016) (‘‘AD 2016–13–06’’). Repeat the inspection thereafter at intervals locating Docket No. FAA–2018–0271.
not to exceed 400 flight hours. If, during any (2) For more information about this AD,
(c) Applicability inspection required by this paragraph, any contact Shahram Daneshmandi, Aerospace
This AD applies to Saab AB, Saab damage or existing repair outside the limits Engineer, International Section, Transport
Aeronautics (formerly known as Saab AB, specified in Saab Service Bulletin 340–30– Standards Branch, FAA, 2200 South 216th
Saab Aerosystems) airplanes, certificated in 094, dated March 27, 2015, is found, before St., Des Moines, WA 98198; telephone and
any category, identified in paragraphs (c)(1) further flight, repair or replace the horizontal fax: 206–231–3220.
and (c)(2), of this AD. stabilizer de-icing boots, in accordance with (3) For service information identified in
(1) Saab AB, Saab Aeronautics Model 340A the Accomplishment Instructions of Saab this AD, contact Saab AB, Saab Aeronautics,
(SAAB/SF340A) airplanes, serial numbers Service Bulletin 340–30–094, dated March SE–581 88, Linköping, Sweden; telephone:
004 through 138 inclusive, if Saab 27, 2015. Repair or replacement on an +46 13 18 5591; fax: +46 13 18 4874; email:
modification 1462 has been embodied in airplane of the horizontal stabilizer de-icing saab340techsupport@saabgroup.com;
production, or Saab Service Bulletin 340–55– boots, as required by this paragraph, does not internet: http://www.saabgroup.com. You
008 has been embodied in service, except constitute terminating action for the may view this service information at the
those that have also embodied Saab repetitive inspections required by this FAA, Transport Standards Branch, 2200
modification 1793 in production, or Saab paragraph for that airplane. South 216th St., Des Moines, WA. For
Service Bulletin 340–55–010 in service; and (i) New Requirement of This AD: information on the availability of this
serial numbers 139 through 159 inclusive. Modification material at the FAA, call 206–231–3195.
(2) Saab AB, Saab Aeronautics Model
Within 18 months after the effective date Issued in Des Moines, Washington, on
SAAB 340B airplanes, serial numbers 160
of this AD, modify the airplane by replacing March 30, 2018.
through 459 inclusive.
the single stitched de-icing boots installed on Chris Spangenberg,
(d) Subject the left-hand (LH) and right-hand (RH) Acting Director, System Oversight Division,
Air Transport Association (ATA) of horizontal stabilizers with double stitched Aircraft Certification Service.
America Code 30, Ice and rain protection. de-icing boots and re-identify the LH and RH
[FR Doc. 2018–07636 Filed 4–16–18; 8:45 am]
horizontal stabilizer leading edge, in
(e) Reason accordance with the Accomplishment BILLING CODE 4910–13–P
This AD was prompted by reports of Instructions of Saab Service Bulletin 340–30–
ruptured horizontal stabilizer de-icing boots. 095, dated April 3, 2017.
We are issuing this AD to detect and correct DEPARTMENT OF TRANSPORTATION
(j) Terminating Action
ruptured horizontal stabilizer de-icing boots,
which could lead to complete loss of the de- Modification of the airplane as required by Federal Aviation Administration
icing function within its associated zone and paragraph (i) of this AD, constitutes
severe vibrations, possibly resulting in terminating action for the repetitive 14 CFR Part 39
reduced control of the airplane. inspections required by paragraph (h) of this
AD, for that airplane. [Docket No. FAA–2018–0142; Product
(f) Compliance Identifier 2018–NE–04–AD]
(k) Other FAA AD Provisions
Comply with this AD within the
compliance times specified, unless already (1) Alternative Methods of Compliance RIN 2120–AA64
done. (AMOCs): The Manager, International
Section, Transport Standards Branch, FAA, Airworthiness Directives; General
(g) Retained Revision of the Airplane Flight has the authority to approve AMOCs for this Electric Company CF34–8E Engines
Manual (AFM), With No Changes AD, if requested using the procedures found
This paragraph restates the requirements of in 14 CFR 39.19. In accordance with 14 CFR AGENCY: Federal Aviation
paragraph (g) of AD 2016–13–06, with no 39.19, send your request to your principal Administration (FAA), DOT.
changes. Within 30 days after August 1, 2016 inspector or local Flight Standards District ACTION: Notice of proposed rulemaking
(the effective date of AD 2016–13–06), revise Office, as appropriate. If sending information (NPRM).
the ‘‘Abnormal Procedures’’ section of the directly to the International Section, send it
applicable Saab 340 AFM to incorporate the to the attention of the person identified in SUMMARY: We propose to adopt a new
revision specified in paragraphs (g)(1) paragraph (l)(2) of this AD. Information may airworthiness directive (AD) for all
through (g)(3) of this AD. be emailed to: 9-ANM-116-AMOC- General Electric Company (GE) CF34–8E
(1) For Saab AB, Saab Aeronautics Model REQUESTS@faa.gov. Before using any turbofan engines. This proposed AD was
340A (SAAB/SF340A) airplanes, revise AFM approved AMOC, notify your appropriate
prompted by a report from GE regarding
340A 001 by incorporating Revision 57, principal inspector, or lacking a principal
dated March 27, 2015. inspector, the manager of the local flight a quality escape of nonconforming
(2) For Saab AB, Saab Aeronautics Model standards district office/certificate holding thrust reverser fire seals. This proposed
SAAB 340B airplanes, revise AFM 340B 001 district office. AD would require a one-time inspection
by incorporating Revision 35, dated March (2) Contacting the Manufacturer: As of the of the gap between the core cowl seal
27, 2015. effective date of this AD, for any requirement and the pylon seal of the thrust reverser
(3) For Saab AB, Saab Aeronautics Model in this AD to obtain corrective actions from for correct gap width, and replacement
SAAB 340B airplanes with extended wing a manufacturer, the action must be of the seals, if needed. We are proposing
tips, revise AFM 340B 010 by incorporating accomplished using a method approved by
this AD to address the unsafe condition
Revision 28, dated March 27, 2015. the Manager, International Section, Transport
Standards Branch, FAA; or the European on these products.
(h) Retained Inspection/Replacement, With Aviation Safety Agency (EASA); or Saab AB, DATES: We must receive comments on
No Changes this proposed AD by June 1, 2018.
amozie on DSK30RV082PROD with PROPOSALS
Saab Aeronautics EASA Design Organization
This paragraph restates the requirements of Approval (DOA). If approved by the DOA, ADDRESSES: You may send comments,
paragraph (h) of AD 2016–13–06, with no the approval must include the DOA- using the procedures found in 14 CFR
changes. Within 400 flight hours or 6 authorized signature.
months, whichever occurs first after August 11.43 and 11.45, by any of the following
1, 2016 (the effective date of AD 2016–13– (l) Related Information methods:
06), do a detailed inspection for damage of (1) Refer to Mandatory Continuing • Federal eRulemaking Portal: Go to
the horizontal stabilizer de-icing boots, and Airworthiness Information (MCAI) EASA AD http://www.regulations.gov. Follow the
existing repairs of horizontal stabilizer de- 2017–0144, dated August 9, 2017, for related instructions for submitting comments.
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Document Created: 2018-04-17 02:53:10
Document Modified: 2018-04-17 02:53:10
| 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 June 1, 2018. | |
| Contact | Shahram Daneshmandi, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3220. | |
| FR Citation | 83 FR 16792 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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