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Start Printed Page 50235
AGENCY:
Federal Aviation Administration (FAA), DOT.
ACTION:
Final rule.
SUMMARY:
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes. This AD was prompted by reports of burned Boeing Material Specification (BMS) 8-39 urethane foam, which is a material with fire-retardant properties that deteriorate with age. This AD requires replacing certain BMS 8-39 foam pads with Nomex felt in certain areas, removing certain BMS 8-39 foam pads in a certain area (which includes a general visual inspection to find BMS 8-39 foam pads), and inspecting the corner seals to determine if the corner seals were replaced, and replacing affected corner seals. This AD also prohibits the installation of BMS 8-39 urethane foam seal in certain locations. The FAA is issuing this AD to address the unsafe condition on these products.
DATES:
This AD is effective September 20, 2022.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of September 20, 2022.
ADDRESSES:
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; internet www.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 www.regulations.gov by searching for and locating Docket No. FAA-2021-1177.
Examining the AD Docket
You may examine the AD docket at www.regulations.gov by searching for and locating Docket No. FAA-2021-1177; 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.
Start Further InfoFOR FURTHER INFORMATION CONTACT:
Julie Linn, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3584; email: julie.linn@faa.gov.
End Further Info End Preamble Start Supplemental InformationSUPPLEMENTARY 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 certain The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes. The NPRM published in the Federal Register on January 31, 2022 (87 FR 4828). The NPRM was prompted by reports of burned BMS 8-39 urethane foam, which is a material with fire-retardant properties that deteriorate with age. In the NPRM, the FAA proposed to require replacing certain BMS 8-39 foam pads with Nomex felt in certain areas, removing certain BMS 8-39 foam pads in a certain area (which includes a general visual inspection to find BMS 8-39 foam pads), and inspecting the corner seals to determine if the corner seals were replaced, and replacing affected corner seals. The FAA is issuing this AD to address degraded BMS 8-39 urethane foam used in seals, which may fail to maintain sufficient halon concentrations in the cargo compartments to extinguish or contain fire or smoke, and may result in penetration of smoke or fire into the flight compartment, leading to possible loss of control of the airplane.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from Air Line Pilots Association, International (ALPA) and United Airlines, who supported the NPRM without change.
The FAA received additional comments from Aviation Partners Boeing (APB) and another individual. The following presents the comments received on the NPRM and the FAA's response to the comments.
Effect of Winglets on Accomplishment of the Proposed Actions
APB stated that the installation of winglets per Supplemental Type Certificate (STC) ST01920SE does not affect compliance with the mandated actions in the proposed rule.
The FAA agrees with the commenter. Therefore, the installation of STC ST01920SE does not affect the ability to accomplish the actions required by this AD. The FAA has not changed this AD in this regard.
Request for Clarification of the Safe Life-Limit of BMS 8-39 Urethane Foam
An individual commenter requested information related to how long it takes for BMS 8-39 foam pads to become flammable, and, if the foam is relatively new and retains its fire retardant properties, the commenter wondered if the BMS 8-39 foam should still be replaced. Conversely, the commenter questioned whether the situation was serious enough to ground airplanes.
The FAA agrees to clarify. According to Boeing, the self-extinguishing and physical properties of the BMS 8-39 urethane foam can degrade after five to ten years, and this degraded material can be an unacceptable fuel source for a fire if exposed to an ignition source. In developing an appropriate compliance time, the FAA considered the safety implications, parts availability, and normal maintenance schedules for timely accomplishment of replacement of the BMS 8-39 urethane foam. Further, the FAA arrived at the Start Printed Page 50236 proposed compliance time with operator and manufacturer concurrence. In consideration of all of these factors, the FAA determined that the compliance time, as proposed, represents an appropriate interval in which the BMS 8-39 urethane foam can be replaced in a timely manner within the fleet, while still maintaining an adequate level of safety. No airplanes would need to be grounded to address this unsafe condition. The FAA has not changed the AD in this regard.
Request for Clarification of Cost
An individual commenter requested clarification regarding who bears the cost for the BMS 8-39 foam replacement: airplane operators or the manufacturer.
The FAA agrees to clarify. In Boeing Special Attention Service Bulletin 767-25-0381, Revision 4, dated April 26, 2021, the manufacturer indicated that no warranty remedies exist for the required actions. Therefore, the airplane operators are responsible for the costs, and any warranty remedies or adjustments in the cost of accomplishing this AD must be arranged between the manufacturer and the operator. The FAA does not have any control over the costs associated with this AD. The FAA has not changed the AD in this regard.
Conclusion
The FAA reviewed the relevant data, considered any 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 Special Attention Service Bulletin 767-25-0381, Revision 4, dated April 26, 2021. This service information specifies, among other actions, procedures for replacing certain BMS 8-39 foam pads with Nomex felt in the forward and aft crown area, removing certain BMS 8-39 foam pads in the crown area (which includes a general visual inspection to find BMS 8-39 foam pads) for certain airplanes, inspecting the corner seals to determine if the corner seals were replaced, and replacing affected corner seals. The required actions depend on requirements for use and location of the BMS 8-39 urethane foam in the airplane. 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 396 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
Action Labor cost Parts cost Cost per product Cost on U.S. operators Inspection (1 airplane) 33 work-hours × $85 per hour = $2,805 $0 $2,805 $2,805 Replacement of foam pad with Nomex felt (361 airplanes) 29 work-hours × $85 per hour = $2,465 Negligible * 2,465 889,865 Removal (34 airplanes) 29 work-hours × $85 per hour = $2,465 0 2,465 83,810 * Parts are Nomex felt, adhesive, and tapes. There are no kits for this required action. 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 this replacement:
On-Condition Costs
Action Labor cost Parts cost Cost per product Replacement of corner seals 1 work-hour × $85 per hour = $85 Up to $3,848 Up to $3,933. 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.
Start List of SubjectsList 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, Start Printed Page 50237 the FAA amends 14 CFR part 39 as follows:
Start PartPART 39—AIRWORTHINESS DIRECTIVES
End Part Start Amendment Part1. The authority citation for part 39 continues to read as follows:
End Amendment Part[Amended]2. The FAA amends § 39.13 by adding the following new airworthiness directive:
End Amendment Part2022-13-10 The Boeing Company: Amendment 39-22096; Docket No. FAA-2021-1177; Project Identifier AD-2021-00570-T.
(a) Effective Date
This airworthiness directive (AD) is effective September 20, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes, certificated in any category, identified as Group 1, Configuration 4; Group 2, 3, 12, and 13, Configuration 3; Group 14, Configuration 1 and 3; Group 15, Configuration 2; and Group 17, Configuration 3 and 4; in Boeing Special Attention Service Bulletin 767-25-0381, Revision 4, dated April 26, 2021.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/furnishings.
(e) Unsafe Condition
This AD was prompted by reports of burned Boeing Material Specification (BMS) 8-39 urethane foam, and a report from the airplane manufacturer that airplanes were assembled with seals throughout various areas of the airplane (including flight deck and cargo compartments) made of BMS 8-39 urethane foam, a material with fire-retardant properties that deteriorate with age. The FAA is issuing this AD to address degraded BMS 8-39 urethane foam used in seals, which may fail to maintain sufficient halon concentrations in the cargo compartments to extinguish or contain fire or smoke, and may result in penetration of smoke or fire into the flight compartment, leading to possible loss of control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified, unless already done.
(g) Required Actions
Within 72 months after the effective date of this AD, do the applicable actions specified in paragraph (g)(1), (2), (3), or (4) of this AD in accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin 767-25-0381, Revision 4, dated April 26, 2021.
(1) For Group 1, Configuration 4, airplanes; and Group 2, 3, 12, and 13, Configuration 3, airplanes: Replace BMS 8-39 foam pads in the forward and aft crown area with Nomex felt.
(2) For Group 14, Configuration 1 and 3, airplanes; and Group 15, Configuration 2, airplanes: Remove BMS 8-39 foam pads in the crown area.
(3) For Group 17, Configuration 3, airplanes: Replace BMS 8-39 foam pads in the forward and aft crown area with Nomex felt, inspect the corner seals to determine if the corner seals were replaced and if any corner seals were not replaced, within 72 months after the effective date of this AD, replace affected corner seals.
(4) For Group 17, Configuration 4, airplanes: Inspect the corner seals to determine if the corner seals were replaced and if any corner seals were not replaced, within 72 months after the effective date of this AD, replace affected corner seals.
(h) Parts Installation Prohibition
As of the effective date of this AD, no person may install a BMS 8-39 urethane foam seal on any airplane in any location identified in Boeing Special Attention Service Bulletin 767-25-0381, Revision 4, dated April 26, 2021.
(i) 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 (j) of this AD. Information may be emailed to: 9-ANMSeattle-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.
(j) Related Information
For more information about this AD, contact Julie Linn, Aerospace Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3584; email: julie.linn@faa.gov.
(k) 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 Special Attention Service Bulletin 767-25-0381, Revision 4, dated April 26, 2021.
(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; internet www.myboeingfleet.com.
(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.
Start SignatureIssued on June 13, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service.
[FR Doc. 2022-17436 Filed 8-15-22; 8:45 am]
BILLING CODE 4910-13-P
Document Information
- Effective Date:
- 9/20/2022
- Published:
- 08/16/2022
- Department:
- Federal Aviation Administration
- Entry Type:
- Rule
- Action:
- Final rule.
- Document Number:
- 2022-17436
- Dates:
- This AD is effective September 20, 2022.
- Pages:
- 50235-50237 (3 pages)
- Docket Numbers:
- Docket No. FAA-2021-1177, Project Identifier AD-2021-00570-T, Amendment 39-22096, AD 2022-13-10
- RINs:
- 2120-AA64: Airworthiness Directives
- RIN Links:
- https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
- Topics:
- Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
- PDF File:
- 2022-17436.pdf
- Supporting Documents:
- » Airworthiness Directives: The Boeing Company Airplanes
- » Supporting AD Document
- » Airworthiness Directives: The Boeing Company Airplanes
- CFR: (1)
- 14 CFR 39.13