AD 2022-24-11

76413 Federal Register / Vol. 87, No. 239 / Wednesday, December 14, 2022 / Rules and Regulations Validation 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 responsible Flight Standards Office, as appropriate. If sending information directly to the International Validation Branch, send it to the attention of the person identified in paragraph (k) of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, International Validation Branch, FAA; or ANAC; or ANAC’s authorized Designee. If approved by the ANAC Designee, the approval must include the Designee’s authorized signature. (k) Additional Information For more information about this AD, contact Hassan Ibrahim, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206–231– 3653; email Hassan.M.Ibrahim@faa.gov. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Age ˆncia Nacional de Aviac ¸a ˜o Civil (ANAC) AD 2022–06–01, effective June 30, 2022; corrected July 8, 2022. (ii) [Reserved] (3) For ANAC AD 2022–06–01, contact National Civil Aviation Agency (ANAC), Aeronautical Products Certification Branch (GGCP), Rua Dr. Orlando Feirabend Filho, 230—Centro Empresarial Aquarius—Torre B—Andares 14 a 18, Parque Residencial Aquarius, CEP 12.246–190—Sa ˜o Jose ´ dos Campos—SP, Brazil; telephone 55 (12) 3203– 6600; email: pac@anac.gov.br; internet anac.gov.br/en/. You may find this ANAC AD on the ANAC website at sistemas.anac.gov.br/certificacao/DA/ DAE.asp. (4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. (5) You may view this material that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibr- locations.html. Issued on November 18, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–27021 Filed 12–13–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–0799; Project Identifier AD–2022–00611–T; Amendment 39–22251; AD 2022–24–11] RIN 2120–AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule. SUMMARY : The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 787–8, 787–9, and 787–10 airplanes. This AD was prompted by a report indicating that foreign object debris (FOD) could have been introduced during rework of certain engine fire shutoff switches (EFSSs). This AD requires determining the serial number of the left and right EFSS and replacing affected parts. This AD also limits the installation of affected parts under certain conditions. The FAA is issuing this AD to address the unsafe condition on these products. DATES : This AD is effective January 18, 2023. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 18, 2023. ADDRESSES : AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2022–0799; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. Material Incorporated by Reference: • For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110–SK57, Seal Beach, CA 90740–5600; telephone 562–797–1717; website myboeingfleet.com. • You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. It is also available at regulations.gov under Docket No. FAA– 2022–0799. FOR FURTHER INFORMATION CONTACT : Tak Kobayashi, Aerospace Engineer, Propulsion Section, FAA Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone: 206–231– 3553; email Takahisa.Kobayashi@ faa.gov. SUPPLEMENTARY INFORMATION : Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all The Boeing Company Model 787–8, 787–9, and 787–10 airplanes. The NPRM published in the Federal Register on July 8, 2022 (87 FR 40747). The NPRM was prompted by a report indicating that FOD could have been introduced during rework of certain EFSSs. In the NPRM, the FAA proposed to require determining the serial number of the left and right EFSSs and replacing affected parts. The FAA also proposed to limit the installation of affected parts under certain conditions. The FAA is issuing this AD to address FOD in an EFSS, which, if not addressed, could result in a latent failure and loss of intended functions, including the inability to pull the engine fire handle and uncommanded activation of the engine fuel shutoff function. The inability to pull the engine fire handle when an engine fire is detected could lead to an uncontrolled engine fire and subsequent wing failure, and uncommanded activation of the fuel shutoff function for an engine, combined with in-flight shutdown of the remaining engine, could lead to total loss of engine thrust. Discussion of Final Airworthiness Directive Comments The FAA received comments from The Airline Pilots Association, International (ALPA) and United Airlines who both supported the NPRM without change. The FAA received additional comments from Qatar Airways and Boeing. The following presents the comments received on the NPRM and the FAA’s response. VerDate Sep<11>2014 16:00 Dec 13, 2022 Jkt 259001 PO 00000 Frm 00009 Fmt 4700 Sfmt 4700 E:\FR\FM\14DER1.SGM 14DER1 lotter on DSK11XQN23PROD with RULES1

76414 Federal Register / Vol. 87, No. 239 / Wednesday, December 14, 2022 / Rules and Regulations Request for Guidance if an EFSS Has Two Labels Qatar Airways requested the FAA’s guidance regarding how to handle an EFSS having two identification labels. The commenter explained that it has done ‘‘spot checks’’ of EFSS spares and discovered parts with both ‘‘pre- modification’’ and ‘‘post-modification’’ nameplates/labels. The commenter stated that having two identification labels on the EFSS could create confusion and lead to erroneous updating of airplane records, leading to a possible non-compliance with the final AD. The commenter indicated that the EFSS manufacturer should be able to provide the list of EFSS parts that have both ‘‘pre-modification’’ and ‘‘post-modification’’ labels. The FAA acknowledges that some EFSSs could have both ‘‘pre- modification’’ and ‘‘post-modification’’ labels, which could be confusing. However, having both labels on a part would not affect an operator’s ability to comply with the requirements of this AD. This AD requires determining the serial number of the left EFSS having P/ N 417000–104 and the right EFSS having P/N 417000–105, and replacing any EFSS that has an affected serial number with an EFSS that does not have an affected serial number, or with an EFSS that has an affected serial number but is marked with ‘‘Inspection Record SB D533–1X–003.’’ The ‘‘post- modification’’ label on an EFSS specifies the part number, either P/N 417000–104 or PN 417000–105. The serial number remains the same regardless of modification. The modification referred to on the EFSS labels addresses the requirements of AD 2021–02–06, Amendment 39– 21389 (86 FR 10790, February 23, 2021), which required replacement of EFSSs having P/Ns 417000–101 and 417000– 102 with EFSSs having P/Ns 417000– 104 and 417000–105, respectively. This modification was made to EFSSs having P/Ns 417000–101 and 417000–102, followed by re-identification of those part numbers as P/Ns 417000–104 and 417000–105. It addresses a design issue that caused a latent failure of the EFSS and is not the subject of this AD. When this modification was accomplished at a sub-tier supplier, however, FOD could have been introduced inside the EFSS, and this FOD issue is the subject of this AD. The FAA has not changed this AD in response to this comment. Request To Clarify Affected Airplanes Boeing requested a revision to the FAA’s Determination section in the NPRM, which stated that the unsafe condition is ‘‘likely to exist or develop on other products of the same type design.’’ Boeing recommends that the NPRM instead clarify that the unsafe condition is ‘‘contained to only 787–8, 787–9, and 787–10 airplanes having certain line numbers identified to be impacted by the unsafe condition.’’ Boeing asserted that the nonconformance applies only to a specific group of EFSS serial numbers that were affected at the rework site, and is not endemic to the type design. The FAA acknowledges that FOD inside the EFSS is not endemic to the type design since it was introduced during rework at a sub-tier supplier. However, because the Determination section in the preamble of the NPRM is not repeated in this AD, the FAA cannot provide the clarification requested by the commenter. Furthermore, the affected EFSS serial numbers can be installed on any Model 787 airplane, therefore the unsafe condition is not limited to certain Model 787–8, 787–9, and 787–10 airplane line numbers. The FAA has not changed this AD in response to this comment. Conclusion The FAA reviewed the relevant data, considered the comments received, and determined that air safety requires adopting this AD as proposed. Except for minor editorial changes, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator. Related Service Information Under 1 CFR Part 51 The FAA reviewed Boeing Alert Requirements Bulletin B787–81205– SB260010–00 RB, Issue 001, dated May 2, 2022. This service information specifies procedures for determining the serial number of the left EFSS having P/ N 417000–104 and the right EFSS having P/N 417000–105, and replacing any EFSS having an affected serial number with an EFSS that does not have an affected serial number, or with an EFSS that has an affected serial number but is marked with ‘‘Inspection Record SB D533–1X–003.’’ 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 ADDRESSES . Costs of Compliance The FAA estimates that this AD affects 132 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: E STIMATED C OSTS Action Labor cost Parts cost Cost per product Cost on U.S. operators Determination of EFSS serial number ............ 1 work-hour × $85 per hour = $85 ................. $0 $85 $11,220 The FAA estimates the following costs to do any necessary replacements that would be required based on the results of the inspection. The agency has no way of determining the number of aircraft that might need these replacements: O N -C ONDITION C OSTS Action Labor cost Parts cost Cost per product Replacement of EFSS ............................. 2 work-hours × $85 per hour = $170 ...... $9,685 $9,855 (for one EFSS). VerDate Sep<11>2014 16:00 Dec 13, 2022 Jkt 259001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\14DER1.SGM 14DER1 lotter on DSK11XQN23PROD with RULES1

76415 Federal Register / Vol. 87, No. 239 / Wednesday, December 14, 2022 / Rules and Regulations Authority for This Rulemaking Title 49 of the United States Code specifies the FAA’s authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency’s authority. The FAA is issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: General requirements. Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Will not affect intrastate aviation in Alaska, and (3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES ■ 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] ■ 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2022–24–11 The Boeing Company: Amendment 39–22251; Docket No. FAA–2022–0799; Project Identifier AD– 2022–00611–T. (a) Effective Date This airworthiness directive (AD) is effective January 18, 2023. (b) Affected ADs None. (c) Applicability This AD applies to all The Boeing Company Model 787–8, 787–9, and 787–10 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 26, Fire protection. (e) Unsafe Condition This AD was prompted by a report indicating that foreign object debris (FOD) could have been introduced during rework of certain engine fire shutoff switches (EFSSs). The FAA is issuing this AD to address FOD in an EFSS, which if not addressed, could result in a latent failure and loss of intended functions, including the inability to pull the engine fire handle and uncommanded activation of the engine fuel shutoff function. The inability to pull the engine fire handle when an engine fire is detected could lead to an uncontrolled engine fire and subsequent wing failure, and uncommanded activation of the fuel shutoff function for an engine, combined with in-flight shutdown of the remaining engine, could lead to total loss of engine thrust. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before the effective date of this AD: Except as specified by paragraph (h) of this AD, at the applicable time specified in the ‘‘Compliance’’ paragraph of Boeing Alert Requirements Bulletin B787–81205– SB260010–00 RB, Issue 001, dated May 2, 2022, do all applicable actions identified in, and in accordance with, the Accomplishment Instructions of Boeing Alert Requirements Bulletin B787–81205–SB260010–00 RB, Issue 001, dated May 2, 2022. Note 1 to paragraph (g): Guidance for accomplishing the actions required by this AD can be found in Boeing Alert Service Bulletin B787–81205–SB260010–00, Issue 001, dated May 2, 2022, which is referred to in Boeing Alert Requirements Bulletin B787– 81205–SB260010–00 RB, Issue 001, dated May 2, 2022. (h) Exceptions to Service Information Specifications Where the Compliance Time column of the table in the ‘‘Compliance’’ paragraph of Boeing Alert Requirements Bulletin B787– 81205–SB260010–00 RB, Issue 001, dated May 2, 2022, uses the phrase ‘‘the Issue 001 date of Requirements Bulletin B787–81205– SB260010–00 RB,’’ this AD requires using ‘‘the effective date of this AD.’’ (i) Parts Installation Limitation For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued after the effective date of this AD: As of the effective date of this AD, no person may install a left EFSS P/N 417000–104 or a right EFSS P/N 417000–105, having a serial number specified in Boeing Alert Requirements Bulletin B787–81205–SB260010–00 RB, Issue 001, dated May 2, 2022, unless that EFSS is marked with ‘‘Inspection Record SB D533– 1X–003.’’ (j) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph (k) of this AD. Information may be emailed to: 9-ANM- Seattle-ACO-AMOC-Requests@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (3) An AMOC that provides an acceptable level of safety may be used for any repair, modification, or alteration required by this AD if it is approved by The Boeing Company Organization Designation Authorization (ODA) that has been authorized by the Manager, Seattle ACO Branch, FAA, to make those findings. To be approved, the repair method, modification deviation, or alteration deviation must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (k) Related Information For more information about this AD, contact Tak Kobayashi, Aerospace Engineer, Propulsion Section, FAA Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone: 206–231–3553; email Takahisa.Kobayashi@faa.gov. (l) 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) Boeing Alert Requirements Bulletin B787–81205–SB260010–00 RB, Issue 001, dated May 2, 2022. (ii) [Reserved] (3) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110–SK57, Seal Beach, CA 90740–5600; telephone 562–797–1717; website myboeingfleet.com. VerDate Sep<11>2014 16:00 Dec 13, 2022 Jkt 259001 PO 00000 Frm 00011 Fmt 4700 Sfmt 4700 E:\FR\FM\14DER1.SGM 14DER1 lotter on DSK11XQN23PROD with RULES1

76416 Federal Register / Vol. 87, No. 239 / Wednesday, December 14, 2022 / Rules and Regulations (4) You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibr- locations.html. Issued on November 16, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–27020 Filed 12–13–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–1165; Project Identifier MCAI–2022–00700–T; Amendment 39–22254; AD 2022–24–14] RIN 2120–AA64 Airworthiness Directives; Airbus SAS Airplanes AGENCY : Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION : Final rule. SUMMARY : The FAA is superseding Airworthiness Directive (AD) 2020–12– 11, which applied to all Airbus SAS Model A319–111, –112, –113, –114, –115, –151N, and –153N airplanes; Model A320–251N, –252N, –253N, –271N, –272N, and –273N airplanes; and Model A321–251N, –251NX, –252N, –252NX, –253N, –253NX, –271N, –271NX, –272N, and –272NX airplanes. AD 2020–12–11 required revising the existing airplane flight manual (AFM) to limit the use of speed brakes in certain airplane configurations, as specified in a European Union Aviation Safety Agency (EASA) AD. This AD was prompted by a non-stabilized approach followed by an automatic go-around that led to an airplane pitch-up attitude and resulted in an auto-pilot disconnection. This AD continues to require the actions in AD 2020–12–11 and also requires, for certain airplanes, installing updated FG 3G standard software for the FMGC, and prohibits the installation of affected FG standards, as specified in an EASA AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES : This AD is effective January 18, 2023. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 18, 2023. ADDRESSES : AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2022–1165; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. Material Incorporated by Reference: • For material incorporated by reference in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; website easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. It is also available in the AD docket at regulations.gov under Docket No. FAA– 2022–1165. FOR FURTHER INFORMATION CONTACT : Hye Yoon Jang, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 817–222–5584; email Hye.Yoon.Jang@ faa.gov. SUPPLEMENTARY INFORMATION : Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2020–12–11, Amendment 39–19920 (85 FR 41177, July 9, 2020) (AD 2020–12–11). AD 2020–12–11 applied to all Airbus SAS Model A319–111, –112, –113, –114, –115, –151N, and –153N airplanes; Model A320–251N, –252N, –253N, –271N, –272N, and –273N airplanes; and Model A321–251N, –251NX, –252N, –252NX, –253N, –253NX, –271N, –271NX, –272N, and –272NX airplanes. AD 2020–12–11 required revising the existing airplane flight manual (AFM) and applicable corresponding operational procedures to limit the use of speed brakes in certain airplane configurations. The FAA issued AD 2020–12–11 to address certain airplane configurations, which could result in auto-pilot disconnection and high angle of attack, and consequent increased workload for the flightcrew during a critical phase of flight, and possible loss of control of the airplane. The NPRM published in the Federal Register on September 19, 2022 (87 FR 57150). The NPRM was prompted by AD 2022–0096, dated May 31, 2022, issued by EASA (EASA AD 2022–0096) (referred to after this as the MCAI). The MCAI states that a non-stabilized approach followed by an automatic go- around led to an airplane pitch-up attitude and resulted in an auto-pilot disconnection. The development of updated FG 3G standard software for the flight management and guidance computer (FMGC) will address certain airplane configurations that could result in autopilot disconnection and high angle of attack, and consequent increased workload for the flightcrew during a critical phase of flight, and possible loss of control of the airplane. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2022–1165. In the NPRM, the FAA proposed to continue to require revising the existing airplane flight manual (AFM) and applicable corresponding operational procedures to limit the use of speed brakes in certain airplane configurations. The NPRM also proposed to require installing updated FG 3G standard software for certain airplanes, and to prohibit the installation of affected FG standards, as specified in EASA AD 2022–0096. The FAA is issuing this AD to address certain airplane configurations that could result in auto-pilot disconnection and high angle of attack, and consequent increased workload for the flightcrew during a critical phase of flight, and possible loss of control of the airplane. Discussion of Final Airworthiness Directive Comments The FAA received comments from Air Line Pilots Association, International, who supported the NPRM without change. Conclusion This product has been approved by the aviation authority of another country and is approved for operation in the United States. Pursuant to the FAA’s bilateral agreement with this State of Design Authority, it has notified the FAA of the unsafe condition described VerDate Sep<11>2014 16:00 Dec 13, 2022 Jkt 259001 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\14DER1.SGM 14DER1 lotter on DSK11XQN23PROD with RULES1