80 FR 34256 - Airworthiness Directives; Avidyne Corporation Integrated Flight Displays
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 115 (June 16, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 115 (June 16, 2015)
| Page Range | 34256-34258 | |
| FR Document | 2015-14645 |
[Federal Register Volume 80, Number 115 (Tuesday, June 16, 2015)] [Rules and Regulations] [Pages 34256-34258] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-14645] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-2191; Directorate Identifier 2015-CE-019-AD; Amendment 39-18183; AD 2015-10-51] RIN 2120-AA64 Airworthiness Directives; Avidyne Corporation Integrated Flight Displays AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for Avidyne Corporation (Avidyne) Integrated Flight Displays (IFDs) part number (P/ N) 700-00083-() loaded with software release 9.3.1.0 or earlier release (referred to as Model R9--10 inch), P/N 700-00171-() loaded with software release 9.2.5.0 or earlier release (referred to as Model R9-- 12 inch), and P/N 700-00182-() loaded with software release 10.0.3.0 or earlier release (referred to as Model IFD540). This emergency AD was sent previously to all known U.S. owners and operators of all aircraft that incorporate the above referenced Avidyne IFDs. This AD requires incorporating an operational limitation into the Limitations section of the airplane flight manual (AFM) or airplane flight manual supplement (AFMS). This AD was prompted by reports of Avidyne IFDs displaying incorrect course deviation indication information during GPS approaches (incorrect display of lateral deviations). We are issuing this AD to correct the unsafe condition on these products. DATES: This AD is effective July 1, 2015 to all persons except those persons to whom it was made immediately effective by Emergency AD 2015- 10-51, issued on May 18, 2015, which contained the requirements of this amendment. We must receive comments on this AD by July 31, 2015. 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. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015- 2191; or in person at the Docket Operations Office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Anthony Pigott, Aerospace Engineer, Boston Aircraft Certification Office, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: (781) 238-7158; fax: (781) 238-7199; email: [email protected]. SUPPLEMENTARY INFORMATION: Discussion On May 18, 2015, we issued Emergency AD 2015-10-51, which requires incorporating an operational limitation into the Limitations section of [[Page 34257]] the airplane flight manual (AFM) or airplane flight manual supplement (AFMS). This emergency AD was sent previously to all known U.S. owners and operators of all aircraft that incorporate Avidyne Corporation (Avidyne) Integrated Flight Displays (IFDs) part number (P/N) 700- 00083-() loaded with software release 9.3.1.0 or earlier release (referred to as Model R9--10 inch), P/N 700-00171-() loaded with software release 9.2.5.0 or earlier release (referred to as Model R9-- 12 inch), and P/N 700-00182-() loaded with software release 10.0.3.0 or earlier release (referred to as Model IFD540). This action was prompted by reports of Avidyne IFDs displaying incorrect course deviation indication information during GPS approaches (incorrect display of lateral deviations). This condition occurs when the airplane is flying in certain approaches, the leg to the Final Approach Fix (FAF) is active, and the leg to the FAF is not aligned with the final approach course (i.e., an angled entry to the FAF). The software of the Avidyne IFDs as referenced above will produce lateral deviations to the final approach course as soon as the leg to the FAF becomes active. Therefore, when the leg does not align with the final approach course, the course deviation indicator (CDI) will show a deviation when, in fact, the aircraft is on the proper course for the active leg. This could result in the pilot making flight decisions that put the aircraft in unsafe flight conditions, flying into airspace that was, by the GPS approach design, to be avoided (terrain, obstacle, traffic, restricted). FAA's Determination We are issuing 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 the same type design. AD Requirements This AD requires incorporating an operational limitation into the Limitations section of the airplane flight manual (AFM) or airplane flight manual supplement (AFMS). The operational limitation will contain the following: Flying a full procedure (non Vector-to-Final) GPS approach, with a course change at the Final Approach Fix (FAF), is prohibited.'' ``Flying a GPS approach, with a Direct-To or with an Omni- Bearing Selector (OBS) leg to the FAF, is prohibited.'' FAA's Determination of the Effective Date An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule because of the Avidyne IFDs displaying incorrect course deviation indication information during GPS approaches (incorrect display of lateral deviations), which could result in the pilot making flight decisions that put the aircraft in unsafe flight conditions, flying into airspace that was, by the GPS approach design, to be avoided (terrain, obstacle, traffic, restricted). Therefore, we find that notice and opportunity for prior public comment are impracticable and that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include Docket Number FAA-2015-2191 and Directorate Identifier 2015-CE-015-AD at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this 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 AD. Costs of Compliance We estimate that this AD affects 324 products installed on airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Incorporate operational .5 work-hour x $85 Not applicable...... $42.50 $13,770 limitations into the Limitations per hour = $42.50. section of the airplane flight manual (AFM) or airplane flight manual supplement. ---------------------------------------------------------------------------------------------------------------- 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 This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska, and (4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. [[Page 34258]] List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S. C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2015-10-51 Avidyne Corporation: Amendment 39-18183; Docket No. FAA- 2015-2191; Directorate Identifier 2015-CE-015-AD. (a) Effective Date This AD is effective July 1, 2015 to all persons except those persons to whom it was made immediately effective by Emergency AD 2015-10-51, issued on May 18, 2015, which contained the requirements of this amendment. (b) Affected ADs None. (c) Applicability Avidyne Corporation (Avidyne) Integrated Flight Displays (IFDs) part number (P/N) 700-00083-() loaded with software release 9.3.1.0 or earlier release (referred to as Model R9--10 inch), P/N 700- 00171-() loaded with software release 9.2.5.0 or earlier release (referred to as Model R9--12 inch), and P/N 700-00182-() loaded with software release 10.0.3.0 or earlier release (referred to as Model IFD540). These IFDs are installed on, but not limited to, airplanes that are certificated in any category and are identified in the following: (1) For Model R9--10 inch: AML STC SA00282BO. This document can be found at: http://rgl.faa.gov/Regulatory_and_Guidance_Library/ rgstc.nsf/0/24d8d8ba6cb57e4f86257d1d0055dec4/$FILE/ SA00282BO_AML.pdf. (2) For Model R9--12 inch: Korea Aerospace Industries KC-100 (currently being type validated by the FAA). (3) For Model IFD540: STC SAA00343BO. This document can be found at: http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgstc.nsf/0/ 5084676a444f3b2b86257d20005d08ab/$FILE/SA00343BO_AML.pdf. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code: 34, Navigation. (e) Unsafe Condition This AD was prompted by reports of Avidyne IFDs displaying incorrect course deviation indication information during GPS approaches (incorrect display of lateral deviations). This condition occurs when the airplane is flying in certain approaches, the leg to the Final Approach Fix (FAF) is active, and the leg to the FAF is not aligned with the final approach course (i.e., an angled entry to the FAF). The software of the Avidyne IFDs as referenced above in the Applicability section, paragraph (c) of this AD, will produce lateral deviations to the final approach course as soon as the leg to the FAF becomes active. Therefore, when the leg does not align with the final approach course, the course deviation indicator (CDI) will show a deviation when, in fact, the aircraft is on the proper course for the active leg. We are issuing this AD to prevent such incorrect display of lateral deviations, which could result in the pilot making flight decisions that put the aircraft in unsafe flight conditions, flying into airspace that was, by the GPS approach design, to be avoided (terrain, obstacle, traffic, restricted). (f) Compliance Unless already done, comply with paragraphs (g)(1) through (g)(4) of this AD, including all subparagraphs. (g) Airplane Flight Manual (AFM) or Airplane Flight Manual Supplement (AFMS) Limitation (1) Before further flight after July 1, 2015 to all persons except those persons to whom it was made immediately effective by Emergency AD 2015-10-51, issued on May 18, 2015, which contained the requirements of this amendment, incorporate the operational limitations listed in paragraphs (g)(1)(i) and (g)(1)(ii) of this AD into the Limitations section of the AFM or AFMS, as applicable. This can be done by inserting a copy of this AD into the Limitations section of the AFM or AFMS. (i) ``Flying a full procedure (non Vector-to-Final) GPS approach, with a course change at the Final Approach Fix (FAF), is prohibited.'' (ii) ``Flying a GPS approach, with a Direct-To or with an Omni- Bearing Selector (OBS) leg to the FAF, is prohibited.'' (2) This action may be done by an owner/operator (pilot) holding at least a private pilot certificate and must be entered into the airplane records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1)(4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.173 or 135.439. (3) Paragraphs (g)(3)(i) and (g)(3)(ii) of this AD provides examples of prohibited and allowed GPS approach per paragraph (g)(1)(i) of this AD: (i) An example of a prohibited GPS approach per paragraph (g)(1)(i) of this AD can be found at: http://aeronav.faa.gov/d-tpp/1505/05597r25.pdf. (ii) An example of an allowed GPS approach per paragraph (g)(1)(i) of this AD can be found at: http://aeronav.faa.gov/d-tpp/1505/00626rz29.pdf. (4) This AD is no longer applicable if software is installed that is different than that referenced in paragraph (c) Applicability of this AD. (h) Special Flight Permit Under 14 CFR 39.23, special flight permits are prohibited for this AD. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Boston Aircraft Certification Office (ACO), 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 For further information about this AD, contact Anthony Pigott, Aerospace Engineer, Boston ACO, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: (781) 238-7158; fax: (781) 238-7199; email: [email protected]. Issued in Kansas City, Missouri, on June 8, 2015. Earl Lawrence, Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-14645 Filed 6-15-15; 8:45 am] BILLING CODE 4910-13-P
![34256 Federal Register / Vol. 80, No. 115 / Tuesday, June 16, 2015 / Rules and Regulations
(2) Boeing Special Attention Service (2) You must use this service information incorporating an operational limitation
Bulletin 777–27–0062, Revision 1, dated as applicable to do the actions required by into the Limitations section of the
October 1, 2009, which is not incorporated this AD, unless the AD specifies otherwise. airplane flight manual (AFM) or
by reference in this AD. (i) Boeing Special Attention Service
airplane flight manual supplement
Bulletin 777–27–0062, Revision 2, dated
(k) Alternative Methods of Compliance January 27, 2014. (AFMS). This AD was prompted by
(AMOCs) (ii) Reserved. reports of Avidyne IFDs displaying
(1) The Manager, Seattle Aircraft (3) For service information identified in incorrect course deviation indication
Certification Office (ACO), FAA, has the this AD, contact Boeing Commercial information during GPS approaches
authority to approve AMOCs for this AD, if Airplanes, Attention: Data & Services (incorrect display of lateral deviations).
requested using the procedures found in 14 Management, P. O. Box 3707, MC 2H–65, We are issuing this AD to correct the
CFR 39.19. In accordance with 14 CFR 39.19, Seattle, WA 98124–2207; telephone 206– unsafe condition on these products.
send your request to your principal inspector 544–5000, extension 1; fax 206–766–5680;
DATES: This AD is effective July 1, 2015
or local Flight Standards District Office, as Internet https://www.myboeingfleet.com.
(4) You may view this service information to all persons except those persons to
appropriate. If sending information directly
to the manager of the ACO, send it to the at FAA, Transport Airplane Directorate, 1601 whom it was made immediately
attention of the person identified in Lind Avenue SW., Renton, WA. For effective by Emergency AD 2015–10–51,
paragraph (l)(1) of this AD. Information may information on the availability of this issued on May 18, 2015, which
be emailed to: 9-ANM-Seattle-ACO-AMOC- material at the FAA, call 425–227–1221. contained the requirements of this
Requests@faa.gov. (5) You may view this service information amendment.
(2) Before using any approved AMOC, that is incorporated by reference at the We must receive comments on this
notify your appropriate principal inspector, National Archives and Records AD by July 31, 2015.
or lacking a principal inspector, the manager Administration (NARA). For information on
the availability of this material at NARA, call ADDRESSES: You may send comments,
of the local flight standards district office/ using the procedures found in 14 CFR
certificate holding district office. 202–741–6030, or go to: http://
www.archives.gov/federal-register/cfr/ibr- 11.43 and 11.45, by any of the following
(3) An AMOC that provides an acceptable
level of safety may be used for any repair locations.html. methods:
required by this AD if it is approved by the Issued in Renton, Washington, on June 3, • Federal eRulemaking Portal: Go to
Boeing Commercial Airplanes Organization 2015. http://www.regulations.gov. Follow the
Designation Authorization (ODA) that has Jeffrey E. Duven, instructions for submitting comments.
been authorized by the Manager, Seattle • Fax: 202–493–2251.
Manager, Transport Airplane Directorate,
ACO, to make those findings. For a repair Aircraft Certification Service.
• Mail: U.S. Department of
method to be approved, the repair must meet Transportation, Docket Operations, M–
[FR Doc. 2015–14174 Filed 6–15–15; 8:45 am]
the certification basis of the airplane, and the 30, West Building Ground Floor, Room
approval must specifically refer to this AD. BILLING CODE 4910–13–P
W12–140, 1200 New Jersey Avenue SE.,
(4) AMOCs approved previously for the Washington, DC 20590.
freeplay measurements of the right and left • Hand Delivery: Deliver to Mail
elevators and rudder tab required by DEPARTMENT OF TRANSPORTATION
address above between 9 a.m. and 5
paragraph (f) of AD 2007–13–05, Amendment
39–15109 (72 FR 33856, June 20, 2007), are Federal Aviation Administration p.m., Monday through Friday, except
approved as AMOCs for the corresponding Federal holidays.
requirements of this AD. 14 CFR Part 39 Examining the AD Docket
(5) AMOCs approved previously for the
freeplay measurements of the rudder [Docket No. FAA–2015–2191; Directorate You may examine the AD docket on
required by paragraph (f) of AD 2007–13–05, Identifier 2015–CE–019–AD; Amendment the Internet at http://
Amendment 39–15109 (72 FR 33856, June 39–18183; AD 2015–10–51] www.regulations.gov by searching for
20, 2007), are not approved as AMOCs for the RIN 2120–AA64 and locating Docket No. FAA–2015–
corresponding requirements of this AD. We 2191; or in person at the Docket
are not aware of any such AMOCs. Airworthiness Directives; Avidyne Operations Office between 9 a.m. and 5
(6) AMOCs approved previously for the Corporation Integrated Flight Displays p.m., Monday through Friday, except
repetitive lubrications required by paragraph
AGENCY: Federal Aviation Federal holidays. The AD docket
(g) of AD 2007–13–05, Amendment 39–15109
(72 FR 33856, June 20, 2007), are approved Administration (FAA), DOT. contains this AD, the regulatory
as AMOCs for the corresponding evaluation, any comments received, and
ACTION: Final rule; request for
requirements of this AD. other information. The street address for
comments. the Docket Operations Office (phone:
(l) Related Information 800–647–5527) is in the ADDRESSES
SUMMARY: We are adopting a new
(1) For more information about this AD, airworthiness directive (AD) for section. Comments will be available in
contact Haytham Alaidy, Aerospace the AD docket shortly after receipt.
Engineer, Airframe Branch, ANM–120S,
Avidyne Corporation (Avidyne)
Integrated Flight Displays (IFDs) part FOR FURTHER INFORMATION CONTACT:
FAA, Seattle Aircraft Certification Office
(ACO), 1601 Lind Avenue SW., Renton, WA number (P/N) 700–00083–() loaded with Anthony Pigott, Aerospace Engineer,
98057–3356; phone: 425–917–6573; fax: 425– software release 9.3.1.0 or earlier release Boston Aircraft Certification Office,
917–6590; email: Haytham.Alaidy@faa.gov. (referred to as Model R9—10 inch), P/ FAA, 12 New England Executive Park,
(2) Service information identified in this N 700–00171–() loaded with software Burlington, MA 01803; phone: (781)
AD that is not incorporated by reference is release 9.2.5.0 or earlier release (referred 238–7158; fax: (781) 238–7199; email:
asabaliauskas on DSK5VPTVN1PROD with RULES
available at the addresses specified in to as Model R9—12 inch), and P/N 700– anthony.pigott@faa.gov.
paragraphs (m)(3) and (m)(4) of this AD. 00182–() loaded with software release SUPPLEMENTARY INFORMATION:
(m) Material Incorporated by Reference 10.0.3.0 or earlier release (referred to as
Model IFD540). This emergency AD was Discussion
(1) The Director of the Federal Register
approved the incorporation by reference sent previously to all known U.S. On May 18, 2015, we issued
(IBR) of the service information listed in this owners and operators of all aircraft that Emergency AD 2015–10–51, which
paragraph under 5 U.S.C. 552(a) and 1 CFR incorporate the above referenced requires incorporating an operational
part 51. Avidyne IFDs. This AD requires limitation into the Limitations section of
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List of Subjects in 14 CFR Part 39 (e) Unsafe Condition referenced in paragraph (c) Applicability of
This AD was prompted by reports of this AD.
Air transportation, Aircraft, Aviation Avidyne IFDs displaying incorrect course (h) Special Flight Permit
safety, Incorporation by reference, deviation indication information during GPS
Safety. approaches (incorrect display of lateral Under 14 CFR 39.23, special flight permits
deviations). This condition occurs when the are prohibited for this AD.
Adoption of the Amendment airplane is flying in certain approaches, the (i) Alternative Methods of Compliance
leg to the Final Approach Fix (FAF) is active, (AMOCs)
Accordingly, under the authority and the leg to the FAF is not aligned with
delegated to me by the Administrator, the final approach course (i.e., an angled (1) The Manager, Boston Aircraft
the FAA amends 14 CFR part 39 as entry to the FAF). The software of the Certification Office (ACO), FAA, has the
follows: Avidyne IFDs as referenced above in the authority to approve AMOCs for this AD, if
Applicability section, paragraph (c) of this requested using the procedures found in 14
PART 39—AIRWORTHINESS AD, will produce lateral deviations to the CFR 39.19. In accordance with 14 CFR 39.19,
final approach course as soon as the leg to send your request to your principal inspector
DIRECTIVES
the FAF becomes active. Therefore, when the or local Flight Standards District Office, as
leg does not align with the final approach appropriate. If sending information directly
■ 1. The authority citation for part 39 to the manager of the ACO, send it to the
course, the course deviation indicator (CDI)
continues to read as follows: will show a deviation when, in fact, the attention of the person identified in
Authority: 49 U.S. C. 106(g), 40113, 44701. aircraft is on the proper course for the active paragraph (j) of this AD.
leg. We are issuing this AD to prevent such (2) Before using any approved AMOC,
§ 39.13 [Amended] incorrect display of lateral deviations, which notify your appropriate principal inspector,
could result in the pilot making flight or lacking a principal inspector, the manager
■ 2. The FAA amends § 39.13 by adding decisions that put the aircraft in unsafe flight of the local flight standards district office/
the following new airworthiness conditions, flying into airspace that was, by certificate holding district office.
directive (AD): the GPS approach design, to be avoided (j) Related Information
(terrain, obstacle, traffic, restricted).
2015–10–51 Avidyne Corporation: For further information about this AD,
Amendment 39–18183; Docket No. (f) Compliance contact Anthony Pigott, Aerospace Engineer,
FAA–2015–2191; Directorate Identifier Unless already done, comply with Boston ACO, FAA, 12 New England
2015–CE–015–AD. paragraphs (g)(1) through (g)(4) of this AD, Executive Park, Burlington, MA 01803;
(a) Effective Date including all subparagraphs. phone: (781) 238–7158; fax: (781) 238–7199;
email: anthony.pigott@faa.gov.
This AD is effective July 1, 2015 to all (g) Airplane Flight Manual (AFM) or
persons except those persons to whom it was Airplane Flight Manual Supplement (AFMS) Issued in Kansas City, Missouri, on June 8,
made immediately effective by Emergency Limitation 2015.
AD 2015–10–51, issued on May 18, 2015, (1) Before further flight after July 1, 2015 Earl Lawrence,
which contained the requirements of this to all persons except those persons to whom Manager, Small Airplane Directorate, Aircraft
amendment. it was made immediately effective by Certification Service.
(b) Affected ADs Emergency AD 2015–10–51, issued on May [FR Doc. 2015–14645 Filed 6–15–15; 8:45 am]
18, 2015, which contained the requirements
None. of this amendment, incorporate the BILLING CODE 4910–13–P
(c) Applicability operational limitations listed in paragraphs
(g)(1)(i) and (g)(1)(ii) of this AD into the
Avidyne Corporation (Avidyne) Integrated Limitations section of the AFM or AFMS, as DEPARTMENT OF TRANSPORTATION
Flight Displays (IFDs) part number (P/N) applicable. This can be done by inserting a
700–00083–() loaded with software release copy of this AD into the Limitations section Federal Aviation Administration
9.3.1.0 or earlier release (referred to as Model of the AFM or AFMS.
R9—10 inch), P/N 700–00171–() loaded with (i) ‘‘Flying a full procedure (non Vector-to- 14 CFR Part 39
software release 9.2.5.0 or earlier release Final) GPS approach, with a course change
(referred to as Model R9—12 inch), and P/N at the Final Approach Fix (FAF), is [Docket No. FAA–2014–0249; Directorate
700–00182–() loaded with software release prohibited.’’ Identifier 2012–NM–211–AD; Amendment
10.0.3.0 or earlier release (referred to as (ii) ‘‘Flying a GPS approach, with a Direct- 39–18180; AD 2015–12–06]
Model IFD540). These IFDs are installed on, To or with an Omni-Bearing Selector (OBS)
but not limited to, airplanes that are RIN 2120–AA64
leg to the FAF, is prohibited.’’
certificated in any category and are identified (2) This action may be done by an owner/
in the following: Airworthiness Directives; Learjet Inc.
operator (pilot) holding at least a private pilot
(1) For Model R9—10 inch: AML STC certificate and must be entered into the Airplanes
SA00282BO. This document can be found at: airplane records showing compliance with AGENCY: Federal Aviation
http://rgl.faa.gov/Regulatory_and_Guidance_ this AD in accordance with 14 CFR Administration (FAA), DOT.
Library/rgstc.nsf/0/24d8d8ba6cb57e 43.9(a)(1)(4) and 14 CFR 91.417(a)(2)(v). The
4f86257d1d0055dec4/$FILE/SA00282BO_ record must be maintained as required by 14 ACTION: Final rule.
AML.pdf. CFR 91.173 or 135.439.
(2) For Model R9—12 inch: Korea (3) Paragraphs (g)(3)(i) and (g)(3)(ii) of this
SUMMARY: We are adopting a new
Aerospace Industries KC–100 (currently AD provides examples of prohibited and airworthiness directive (AD) for certain
being type validated by the FAA). allowed GPS approach per paragraph (g)(1)(i) Learjet Inc. Model 45 airplanes. This AD
(3) For Model IFD540: STC SAA00343BO. of this AD: was prompted by reports of non-
This document can be found at: http:// (i) An example of a prohibited GPS conforming windshield supports (coupe
asabaliauskas on DSK5VPTVN1PROD with RULES
rgl.faa.gov/Regulatory_and_Guidance_ approach per paragraph (g)(1)(i) of this AD rails). This AD requires a general visual
Library/rgstc.nsf/0/ can be found at: http://aeronav.faa.gov/d- inspection of the coupe rails to detect
5084676a444f3b2b86257d20005d08ab/ tpp/1505/05597r25.pdf. gouging and scratches, and to determine
$FILE/SA00343BO_AML.pdf. (ii) An example of an allowed GPS
approach per paragraph (g)(1)(i) of this AD
if a radius has been removed; an
(d) Subject can be found at: http://aeronav.faa.gov/d- ultrasound inspection to measure the
Joint Aircraft System Component (JASC)/ tpp/1505/00626rz29.pdf. dimensions of the lower coupe rails; an
Air Transport Association (ATA) of America (4) This AD is no longer applicable if eddy current inspection to detect cracks
Code: 34, Navigation. software is installed that is different than that of the lower coupe rails; replacement of
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Document Created: 2018-02-22 10:23:09
Document Modified: 2018-02-22 10:23:09
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD is effective July 1, 2015 to all persons except those persons to whom it was made immediately effective by Emergency AD 2015- 10-51, issued on May 18, 2015, which contained the requirements of this amendment. | |
| Contact | Anthony Pigott, Aerospace Engineer, Boston Aircraft Certification Office, FAA, 12 New England Executive Park, Burlington, MA 01803; phone: (781) 238-7158; fax: (781) 238-7199; email: [email protected] | |
| FR Citation | 80 FR 34256 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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