AD 2021-15-04

Airworthiness directive · Electrical Power · Boeing 767-300 Series with STC ST02040SE

Effective
July 14, 2021
Published
July 14, 2021 · 86 FR 37019–37022
Issued
July 8, 2021
Model
767-300 Series
Data sheet
TCDSA1NM
Registered aircraft
191 matched by model
Product
Aircraft · Large airplane
ATA chapter
24 · Electrical power
Amendment
39-21651
Docket
FAA-2021-0566
Project
MCAI-2021-00733-T
Issued as
Final rule; request for comments

Unofficial copy from the Federal Register XML, document 2021-15026. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-300 series airplanes as modified by a certain supplemental type certificate (STC). This AD was prompted by a report that the electrical diagram for the C9066 circuit breaker connection (wiring) for the “Main Deck Oxygen Alert Control” is erroneous and might have resulted in incorrect installation. This AD requires inspecting the wiring connection common to the C9066 circuit breaker and, if necessary, making changes to the wiring connection and testing the main deck oxygen alert system. The FAA is issuing this AD to address the unsafe condition on these products.

The airworthiness directive

2021-15-04 The Boeing Company: Amendment 39-21651; Docket No. FAA-2021-0566; Project Identifier MCAI-2021-00733-T.

(a) Effective Date

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This airworthiness directive (AD) becomes effective July 14, 2021.

(b) Affected ADs

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None.

(c) Applicability

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This AD applies to The Boeing Company Model 767-300 series airplanes, certificated in any category, that have been modified to a Bedek Division Special Freighter (BDSF), in accordance with FAA Supplemental Type Certificate (STC) ST02040SE (the freighter configuration is designated as 767-300BDSF), and which are listed in paragraph 1.A., “Effectivity,” of IAI-Aviation Group Alert Service Bulletin 368-24-098, Revision 1, dated June 2021.

(d) Subject

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Air Transport Association (ATA) of America Code 24, Electrical Power.

(e) Reason

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This AD was prompted by a report that the electrical diagram for the C9066 circuit breaker connection (wiring) for the “Main Deck Oxygen Alert Control” is erroneous and might have resulted in incorrect installation. The FAA is issuing this AD to address potential incorrect installation of the “Main Deck Oxygen Alert Control” circuit breaker, which could result in overheating and burning of the wiring, and consequently, could result in smoke triggering an alarm and causing the crew workload to increase; or could result in a short circuit to adjacent wires causing malfunctions in other systems. Furthermore, since this is a potentially unprotected circuit, if any failure occurs along the length of this circuit it could result in a fire and cause collateral damage to adjacent circuits and affect critical systems necessary for continued safe flight and landing.

(f) Compliance

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Comply with this AD within the compliance times specified, unless already done.

(g) Inspection, Wiring Connection Change, and Test

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Within 10 days after the effective date of this AD, perform a detailed inspection of the wiring connection common to the C9066 circuit breaker to make sure 20 AWG wire is connected to terminal 1 and the BUS is connected to terminal 2, in accordance with steps 1. through 3. of the Accomplishment Instructions of IAI-Aviation Group Alert Service Bulletin 368-24-098, Revision 1, dated June 2021. If 20 AWG wire is not connected to terminal 1 or the BUS is not connected to terminal 2, before further flight, make changes to the wiring connection and test the main deck oxygen alert system, in accordance with steps 4. through 13. of the Accomplishment Instructions of IAI-Aviation Group Alert Service Bulletin 368-24-098, Revision 1, dated June 2021.

(h) No Report

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Although IAI-Aviation Group Alert Service Bulletin 368-24-098, Revision 1, dated June 2021, specifies to report inspection findings, this AD does not require any report.

(i) Alternative Methods of Compliance (AMOCs)

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(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 Related Information. 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.

(j) Related Information

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(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) Civil Aviation Authority of Israel (CAAI) Israeli AD ISR-I-24-2021-6-6R1, dated June 27, 2021, for related information. This MCAI may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0566.

(2) For more information about this AD, contact Brian Hernandez, Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3535; email: Brian.Hernandez@faa.gov.

(k) Material Incorporated by Reference

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(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 this AD specifies otherwise.

(i) IAI-Aviation Group Alert Service Bulletin 368-24-098, Revision 1, dated June 2021.

(ii) [Reserved]

(3) For service information identified in this AD, contact Israel Aerospace Industries, Ltd., Ben Gurion Airport, Israel 70100; telephone 972-39359826; email tmazor@iai.co.il.

(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, email fedreg.legal@nara.gov, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

This AD becomes effective July 14, 2021.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 14, 2021.

The FAA must receive comments on this AD by August 30, 2021.

AddressesPage 1

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 https://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 final rule, contact Israel Aerospace Industries, Ltd., Ben Gurion Airport, Israel 70100; telephone 972-39359826; email tmazor@iai.co.il. You may view this referenced 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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0566.

For further information contactPage 1

Brian Hernandez, Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3535; email: Brian.Hernandez@faa.gov.

BackgroundPage 1

The Civil Aviation Authority of Israel (CAAI), which is the aviation authority for Israel, has issued Israeli AD ISR-I-24-2021-6-6R1, dated June 27, 2021 (also referred to after this as the Mandatory Continuing Airworthiness Information, or the MCAI), to correct an unsafe condition for The Boeing Company Model 767-300 series airplanes, that have been modified to a Bedek Division Special Freighter (BDSF), designated as 767-300BDSF, in accordance with CAAI STC SA218/FAA STC ST02040SE/European Union Aviation Safety Agency (EASA) STC 10028430 (as listed in the appendix of the MCAI). Only FAA STC ST02040SE is approved for U.S. operators. You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0566.

This AD was prompted by a report that the electrical diagram for the C9066 circuit breaker connection (wiring) for the “Main Deck Oxygen Alert Control” is erroneous and might have resulted in incorrect installation. This incorrect installation leads to an unprotected circuit, and therefore any wires or system components that might lie adjacent to the wiring that would normally be protected by the C9066 circuit breaker might be affected. The FAA is issuing this AD to address potential incorrect installation of the “Main Deck Oxygen Alert Control” circuit breaker, which could result in overheating and burning of the wiring, and consequently, could result in smoke triggering an alarm and causing the crew workload to increase; or could result in a short circuit to adjacent wires causing malfunctions in other systems. See the MCAI for additional background information.

Related Service Information Under 1 CFR Part 51Page 2

Israel Aerospace Industries, Ltd., has issued IAI-Aviation Group Alert Service Bulletin 368-24-098, Revision 1, dated June 2021. This service information describes procedures for a visual inspection of the wiring connection common to the C9066 circuit breaker, changes to the wiring connection, if necessary, and a test of the main deck oxygen alert system, if necessary. 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 DeterminationPage 2

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 the State of Design Authority, the FAA has been notified of the unsafe condition described in the MCAI and service information referenced above. The FAA is issuing this AD because the FAA evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of the same type design.

Requirements of This ADPage 2

This AD requires accomplishing the actions specified in the service information described previously.

FAA's Justification and Determination of the Effective DatePage 2

Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5 U.S.C. 551 et seq.) authorizes agencies to dispense with notice and comment procedures for rules when the agency, for “good cause,” finds that those procedures are “impracticable, unnecessary, or contrary to the public interest.” Under this section, an agency, upon finding good cause, may issue a final rule without providing notice and seeking comment prior to issuance. Further, section 553(d) of the APA authorizes agencies to make rules effective in less than thirty days, upon a finding of good cause.

An unsafe condition exists that requires the immediate adoption of this AD without providing an opportunity for public comments prior to adoption. The FAA has found that the risk to the flying public justifies forgoing notice and comment prior to adoption of this rule because incorrect installation of the “Main Deck Oxygen Alert Control” circuit breaker could result in overheating and burning of wiring, and consequently, could result in smoke triggering an alarm and causing the crew workload to increase; or could result in a short circuit to adjacent wires causing malfunctions in other systems. Furthermore, since this is a potentially unprotected circuit, if any failure occurs along the length of this circuit it could result in a fire and cause collateral damage to adjacent circuits and affect critical systems necessary for continued safe flight and landing. Accordingly, notice and opportunity for prior public comment are impracticable and contrary to the public interest pursuant to 5 U.S.C. 553(b)(3)(B). In addition, the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days, for the same reasons the FAA found good cause to forgo notice and comment.

Comments invitedPage 2

The FAA invites you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under ADDRESSES. Include “Docket No. FAA-2021-0566; Project Identifier MCAI-2021-00733-T” at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this final rule because of those comments.

Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this final rule.

Confidential business informationPage 2

CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this AD contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this AD, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as “PROPIN.” The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this AD. Submissions containing CBI should be sent to Brian Hernandez, Aerospace Engineer, Systems and Equipment Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3535; email: Brian.Hernandez@faa.gov. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking.

Regulatory Flexibility Act (RFA)Page 2

The requirements of the RFA do not apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because the FAA has determined that it has good cause to adopt this rule without notice and comment, RFA analysis is not required.

Costs of CompliancePage 2

The FAA estimates that this AD affects 71 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs
ActionLabor costParts costCost per productCost on U.S. operators
Inspection1 work-hour × $85 per hour = $85$0$85$6,035

The FAA estimates the following costs to do any necessary on-condition actions that would be required based on the results of the inspection. The FAA has no way of determining the number of aircraft that might need these actions:

On-Condition Costs
ActionLabor costParts costCost per product
Wiring change and test1 work-hour × $85 per hour = $85$0$85
Authority for This RulemakingPage 3

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 findingsPage 3

The FAA determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.

For the reasons discussed above, I certify that this AD:

(1) Is not a “significant regulatory action” under Executive Order 12866, and

(2) Will not affect intrastate aviation in Alaska.

Adoption of the AmendmentPage 3

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

Adoption of the amendmentPage 3

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 39.13 by adding the following new airworthiness directive:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 191

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Boeing191 aircraft
By year built
19882012
Registered aircraft by year built: 170 aircraft
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19946
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19969
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199819
199915
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20014
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20042
20063
20081
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