Special Conditions: Bombardier Aerospace Inc., Model BD-100-1A10 Airplane; Non-Rechargeable Lithium Battery Installations, 22066-22069 [2017-09661]

Download as PDF 22066 Federal Register / Vol. 82, No. 91 / Friday, May 12, 2017 / Rules and Regulations include any other model that incorporates the same novel or unusual design feature, or should any other model already included on the same type certificate be modified to incorporate the same novel or unusual design feature, these special conditions would also apply to the other model under § 21.101. In addition to the applicable airworthiness regulations and special conditions, the Model BD–700–2A12 and BD–700–2A13 airplanes must comply with the fuel-vent and exhaustemission requirements of 14 CFR part 34, and the noise-certification requirements of 14 CFR part 36. The FAA issues special conditions, as defined in 14 CFR 11.19, in accordance with § 11.38, and they become part of the type certification basis under § 21.101. Novel or Unusual Design Feature The Bombardier Model BD–700–2A12 and BD–700–2A13 airplanes will incorporate a novel or unusual design feature associated with engine-seizure requirements due, in part, to large bypass fans capable of producing much larger and more complex dynamic loads than would other bypass fans. mstockstill on DSK30JT082PROD with RULES Applicability As discussed above, these special conditions are applicable to the Model BD–700–2A12 and BD–700–2A13 airplanes. Should Bombardier apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, these special conditions would apply to the other model as well. Conclusion This action affects only one novel or unusual design feature on Bombardier Model BD–700–2A12 and BD–700– 2A13 airplanes. It is not a rule of general applicability and affects only the applicant who applied to FAA for approval of this feature on the airplane. List of Subjects in 14 CFR Part 25 Aircraft, Aviation safety, Reporting and recordkeeping requirements. The authority citation for these special conditions is as follows: ■ Discussion The limit engine torque load imposed by sudden engine stoppage due to malfunction or structural failure (such as compressor jamming) has been a specific requirement for transportcategory airplanes since 1957. In the past, the design torque loads associated with typical failure scenarios have been estimated by the engine manufacturer and provided to the airframe manufacturer as limit loads. These limit loads were considered simple, pure, torque static loads. It is evident from service history that the engine-failure events that tend to cause the most severe loads are fanblade failures. These events occur much less frequently than the typical ‘‘limit’’ load condition. Regulatory authorities and industry have developed a standardized requirement in the Aviation Rulemaking Advisory Committee (ARAC) forum (Aviation Rulemaking Advisory Committee; Loads and Dynamics Harmonization Working Group [58 FR 13819]). The technical aspects of this requirement have been agreed upon, and the ARAC Loads and Dynamics Harmonization Working Group has accepted them. These special conditions reflect the ARAC recommendation. The ARAC recommendation includes corresponding advisory material, which VerDate Sep<11>2014 is considered an acceptable means of compliance to these special conditions. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. 16:29 May 11, 2017 Jkt 241001 Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704. The Proposed Special Conditions Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the type certification basis for Bombardier Model BD–700– 2A12 and BD–700–2A13 airplanes. In lieu of § 25.361(b) the following special conditions apply: 1. For turbine engine installations, the engine mounts, pylons, and adjacent supporting airframe structure must be designed to withstand 1g level flight loads acting simultaneously with the maximum limit torque loads imposed by each of the following: a. Sudden engine deceleration due to a malfunction that could result in a temporary loss of power or thrust, and b. The maximum acceleration of the engine. 2. For auxiliary power unit (APU) installations, the power unit mounts and adjacent supporting airframe structure must be designed to withstand 1g level flight loads acting simultaneously with the maximum limit torque loads imposed by each of the following: a. Sudden APU deceleration due to malfunction or structural failure; and ■ PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 b. The maximum acceleration of the APU. 3. For engine supporting structure, an ultimate loading condition must be considered that combines 1g flight loads with the transient dynamic loads resulting from: a. The loss of any fan, compressor, or turbine blade; and separately b. Where applicable to a specific engine design, any other engine structural failure that results in higher loads. 4. The ultimate loads developed from the conditions specified in paragraphs 3(a) and 3(b) of these special conditions are to be multiplied by a factor of 1.0 when applied to engine mounts and pylons, and multiplied by a factor of 1.25 when applied to adjacent supporting airframe structure. 5. Any permanent deformation that results from the conditions specified in paragraph 3 must not prevent continued safe flight and landing. Issued in Renton, Washington, on April 27, 2017. Paul Bernado, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017–09663 Filed 5–11–17; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA–2017–0358; Special Conditions No. 25–659–SC] Special Conditions: Bombardier Aerospace Inc., Model BD–100–1A10 Airplane; Non-Rechargeable Lithium Battery Installations Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; request for comment. AGENCY: These special conditions are issued for non-rechargeable lithium battery installations on the Bombardier Aerospace Inc. (Bombardier) Model BD– 100–1A10 airplane. Non-rechargeable lithium batteries are a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport category airplanes. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level SUMMARY: E:\FR\FM\12MYR1.SGM 12MYR1 mstockstill on DSK30JT082PROD with RULES Federal Register / Vol. 82, No. 91 / Friday, May 12, 2017 / Rules and Regulations of safety equivalent to that established by the existing airworthiness standards. DATES: This action is effective on Bombardier on May 12, 2017. We must receive your comments by June 26, 2017. ADDRESSES: Send comments identified by docket number FAA–2017–0358 using any of the following methods: • Federal eRegulations Portal: Go to http://www.regulations.gov/ and follow the online instructions for sending your comments electronically. • Mail: Send comments to Docket Operations, M–30, U.S. Department of Transportation (DOT), 1200 New Jersey Avenue SE., Room W12–140, West Building Ground Floor, Washington, DC 20590–0001. • Hand Delivery or Courier: Take comments to Docket Operations in Room W12–140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. • Fax: Fax comments to Docket Operations at 202–493–2251. Privacy: The FAA will post all comments it receives, without change, to http://www.regulations.gov/, including any personal information the commenter provides. Using the search function of the docket Web site, anyone can find and read the electronic form of all comments received into any FAA docket, including the name of the individual sending the comment (or signing the comment for an association, business, labor union, etc.). DOT’s complete Privacy Act Statement can be found in the Federal Register published on April 11, 2000 (65 FR 19477–19478), as well as at http://DocketsInfo.dot.gov/. Docket: Background documents or comments received may be read at http://www.regulations.gov/ at any time. Follow the online instructions for accessing the docket or go to Docket Operations in Room W12–140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. FOR FURTHER INFORMATION CONTACT: Nazih Khaouly, Airplane and Flight Crew Interface Branch, ANM–111, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone 425–227–2432; facsimile 425–227–1149. SUPPLEMENTARY INFORMATION: Future Requests for Installation of NonRechargeable Lithium Batteries The FAA anticipates that nonrechargeable lithium batteries will be VerDate Sep<11>2014 16:29 May 11, 2017 Jkt 241001 installed in most makes and models of transport category airplanes. We intend to require special conditions for certification projects involving nonrechargeable lithium battery installations to address certain safety issues until we can revise the airworthiness requirements. Applying special conditions to these installations across the range of transport category airplanes will ensure regulatory consistency. Typically, the FAA issues special conditions after receiving an application for type certificate approval of a novel or unusual design feature. However, the FAA has found that the presence of nonrechargeable lithium batteries in certification projects is not always immediately identifiable, since the battery itself may not be the focus of the project. Meanwhile, the inclusion of these batteries has become virtually ubiquitous on in-production transport category airplanes, which shows that there will be a need for these special conditions. Also, delaying the issuance of special conditions until after each design application is received could lead to costly certification delays. Therefore the FAA finds it necessary to issue special conditions applicable to these battery installations on particular makes and models of aircraft. On April 22, 2016, the FAA published special conditions no. 25–612–SC in the Federal Register (81 FR 23573) applicable to Gulfstream Aerospace Corporation for the GVI airplane. Those were the first special conditions the FAA issued for non-rechargeable lithium battery installations. We explained in that document our decision to make those special conditions effective one year after publication in the Federal Register, which is April 22, 2017. In those special conditions, the FAA stated its intention to apply non-rechargeable lithium battery special conditions to design changes on other makes and models applied for after this same date. Section 1205 of the FAA Reauthorization Act of 1996 requires the FAA to consider the extent to which Alaska is not served by transportation modes other than aviation and to establish appropriate regulatory distinctions when modifying airworthiness regulations that affect intrastate aviation in Alaska. In consideration of this requirement and the overall impact on safety, the FAA does not intend to require nonrechargeable lithium battery special conditions for design changes that only replace a 121.5 megahertz (MHz) emergency locator transmitter (ELT) with a 406 MHz ELT that meets PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 22067 Technical Standard Order C126b, or later revision, on transport airplanes operating only in Alaska. This will support our efforts of encouraging operators in Alaska to upgrade to a 406 MHz ELT. These ELTs provide significantly improved accuracy for lifesaving services to locate an accident site in Alaskan terrain. The FAA considers that the safety benefits from upgrading to a 406 MHz ELT for Alaskan operations will outweigh the battery fire risk. Comments Invited The substance of these special conditions has been subjected to the notice and comment period in prior instances and has been derived without substantive change from those previously issued. It is unlikely that prior public comment would result in a significant change from the substance contained herein. Therefore, the FAA has determined that prior public notice and comment are unnecessary and impracticable, and good cause exists for adopting these special conditions upon publication in the Federal Register. The FAA is requesting comments to allow interested persons to submit views that may not have been submitted in response to the prior opportunities for comment described above. We invite interested people to take part in this rulemaking by sending written comments, data, or views. The most helpful comments reference a specific portion of the special conditions, explain the reason for any recommended change, and include supporting data. We will consider all comments we receive by the closing date for comments. We may change these special conditions based on the comments we receive. Background Bombardier holds type certificate no. T00005NY, which provides the certification basis for the BD–100–1A10 airplane. The BD–100–1A10 is a twin engine, transport category airplane with a passenger seating capacity of 16 and a maximum takeoff weight of 38,500 to 40,600 pounds, depending on the specific design. The FAA is issuing these special conditions for non-rechargeable lithium battery installations on the BD–100– 1A10 airplane. The current battery requirements in title 14, Code of Federal Regulations (14 CFR) part 25 are inadequate for addressing an airplane with non-rechargeable lithium batteries. E:\FR\FM\12MYR1.SGM 12MYR1 22068 Federal Register / Vol. 82, No. 91 / Friday, May 12, 2017 / Rules and Regulations Type Certification Basis Under the provisions of 14 CFR 21.101, Bombardier must show that the BD–100–1A10 airplane meets the applicable provisions of the regulations listed in type certificate no. T00005NY or the applicable regulations in effect on the date of application for the change, except for earlier amendments as agreed upon by the FAA. In addition, the certification basis includes certain special conditions, exemptions, or later amended sections that are not relevant to these special conditions. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for the BD–100–1A10 airplane because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16. Special conditions are initially applicable to the airplane model for which they are issued. Should the type certificate for that model be amended later to include any other model that incorporates the same novel or unusual design feature, or should any other model already included on the same type certificate be modified to incorporate the same novel or unusual design feature, these special conditions would also apply to the other model under § 21.101. In addition to the applicable airworthiness regulations and special conditions, the BD–100–1A10 must comply with the fuel vent and exhaust emission requirements of 14 CFR part 34 and the noise certification requirements of 14 CFR part 36. The FAA issues special conditions, as defined in 14 CFR 11.19, in accordance with § 11.38, and they become part of the type certification basis under § 21.101. Novel or Unusual Design Feature mstockstill on DSK30JT082PROD with RULES The novel or unusual design feature is the installation of non-rechargeable lithium batteries. For the purpose of these special conditions, we refer to a battery and battery system as a battery. A battery system consists of the battery and any protective, monitoring, and alerting circuitry or hardware inside or outside of the battery. It also includes vents (where necessary) and packaging. Discussion The FAA derived the current regulations governing installation of batteries in transport category airplanes from Civil Air Regulations (CAR) 4b.625(d) as part of the recodification of CAR 4b that established 14 CFR part 25 VerDate Sep<11>2014 16:29 May 11, 2017 Jkt 241001 in February 1965. This recodification basically reworded the CAR 4b battery requirements, which are currently in § 25.1353(b)(1) through (4). Nonrechargeable lithium batteries are novel and unusual with respect to the state of technology considered when these requirements were codified. These batteries introduce higher energy levels into airplane systems through new chemical compositions in various battery cell sizes and construction. Interconnection of these cells in battery packs introduces failure modes that require unique design considerations, such as provisions for thermal management. Recent events involving rechargeable and non-rechargeable lithium batteries prompted the FAA to initiate a broad evaluation of these energy storage technologies. In January 2013, two independent events involving rechargeable lithium-ion batteries revealed unanticipated failure modes. A National Transportation Safety Board (NTSB) letter to the FAA, dated May 22, 2014, which is available at http:// www.ntsb.gov, filename A–14–032– 036.pdf, describes these events. On July 12, 2013, an event involving a non-rechargeable lithium battery in an emergency locator transmitter installation demonstrated unanticipated failure modes. The United Kingdom’s Air Accidents Investigation Branch Bulletin S5/2013 describes this event. Some known uses of rechargeable and non-rechargeable lithium batteries on airplanes include: • Flight deck and avionics systems such as displays, global positioning systems, cockpit voice recorders, flight data recorders, underwater locator beacons, navigation computers, integrated avionics computers, satellite network and communication systems, communication management units, and remote-monitor electronic linereplaceable units; • Cabin safety, entertainment, and communications equipment, including emergency locator transmitters, life rafts, escape slides, seatbelt air bags, cabin management systems, Ethernet switches, routers and media servers, wireless systems, Internet and in-flight entertainment systems, satellite televisions, remotes, and handsets; • Systems in cargo areas including door controls, sensors, video surveillance equipment, and security systems. Some known potential hazards and failure modes associated with nonrechargeable lithium batteries are: • Internal failures: In general, these batteries are significantly more susceptible to internal failures that can PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 result in self-sustaining increases in temperature and pressure (i.e., thermal runaway) than their nickel-cadmium or lead-acid counterparts. The metallic lithium can ignite, resulting in a selfsustaining fire or explosion. • Fast or imbalanced discharging: Fast discharging or an imbalanced discharge of one cell of a multi-cell battery may create an overheating condition that results in an uncontrollable venting condition, which in turn leads to a thermal event or an explosion. • Flammability: Unlike nickelcadmium and lead-acid batteries, lithium batteries use higher energy and current in an electrochemical system that can be configured to maximize energy storage of lithium. They also use liquid electrolytes that can be extremely flammable. The electrolyte, as well as the electrodes, can serve as a source of fuel for an external fire if the battery casing is breached. Special condition no. 1 of these special conditions requires that each individual cell within a nonrechargeable lithium battery be designed to maintain safe temperatures and pressures. Special condition no. 2 addresses these same issues but for the entire battery. Special condition no. 2 requires the battery be designed to prevent propagation of a thermal event, such as self-sustained, uncontrollable increases in temperature or pressure from one cell to adjacent cells. Special conditions nos. 1 and 2 are intended to ensure that the nonrechargeable lithium battery and its cells are designed to eliminate the potential for uncontrollable failures. However, a certain number of failures will occur due to various factors beyond the control of the battery designer. Therefore, other special conditions are intended to protect the airplane and its occupants if failure occurs. Special conditions 3, 7, and 8 are selfexplanatory. Special condition no. 4 makes it clear that the flammable fluid fire protection requirements of § 25.863 apply to nonrechargeable lithium battery installations. Section 25.863 is applicable to areas of the airplane that could be exposed to flammable fluid leakage from airplane systems. Nonrechargeable lithium batteries contain an electrolyte that is a flammable fluid. Special condition no. 5 requires that each non-rechargeable lithium battery installation not damage surrounding structure or adjacent systems, equipment, or electrical wiring from corrosive fluids or gases that may escape in such a way as to cause a major or more severe failure condition. E:\FR\FM\12MYR1.SGM 12MYR1 Federal Register / Vol. 82, No. 91 / Friday, May 12, 2017 / Rules and Regulations mstockstill on DSK30JT082PROD with RULES While special condition no. 5 addresses corrosive fluids and gases, special condition no. 6 addresses heat. Special condition no. 6 requires that each non-rechargeable lithium battery installation have provisions to prevent any hazardous effect on airplane structure or systems caused by the maximum amount of heat the battery installation can generate due to any failure of it or its individual cells. The means of meeting special conditions nos. 5 and 6 may be the same, but the requirements are independent and address different hazards. These special conditions apply to all non-rechargeable lithium battery installations in lieu of § 25.1353(b)(1) through (4) at Amendment 25–123 or § 25.1353(c)(1) through (4) at earlier amendments. Those regulations remain in effect for other battery installations. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. Applicability These special conditions are applicable to the BD–100–1A10 airplane. Should Bombardier apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, these special conditions would apply to that model as well. These special conditions are only applicable to design changes applied for after the effective date. These special conditions are not applicable to changes to previously certified non-rechargeable lithium battery installations where the only change is either cosmetic or to relocate the installation to improve the safety of the airplane and occupants. Previously certified non-rechargeable lithium battery installations, as used in this paragraph, are those installations approved for certification projects applied for on or before the effective date of these special conditions. A cosmetic change is a change in appearance only, and does not change any function or safety characteristic of the battery installation. These special conditions are also not applicable to unchanged, previously certified nonrechargeable lithium battery installations that are affected by a change in a manner that improves the safety of its installation. The FAA determined that these exclusions are in the public interest because the need to meet all of the special conditions might otherwise deter these design changes that improve safety. VerDate Sep<11>2014 16:29 May 11, 2017 Jkt 241001 Conclusion This action affects only a certain novel or unusual design feature on one model of airplane. It is not a rule of general applicability. The substance of these special conditions has been subjected to the notice and comment period in prior instances and has been derived without substantive change from those previously issued. It is unlikely that prior public comment would result in a significant change from the substance contained herein. Therefore, the FAA has determined that prior public notice and comment are unnecessary and impracticable, and good cause exists for adopting these special conditions upon publication in the Federal Register. The FAA is requesting comments to allow interested persons to submit views that may not have been submitted in response to the prior opportunities for comment described above. List of Subjects in 14 CFR Part 25 Aircraft, Aviation safety, Reporting and record keeping requirements. 22069 6. Have provisions to prevent any hazardous effect on airplane structure or systems caused by the maximum amount of heat it can generate due to any failure of it or its individual cells. 7. Have a failure sensing and warning system to alert the flightcrew if its failure affects safe operation of the airplane. 8. Have a means for the flightcrew or maintenance personnel to determine the battery charge state if the battery’s function is required for safe operation of the airplane. Note: A battery system consists of the battery and any protective, monitoring, and alerting circuitry or hardware inside or outside of the battery. It also includes vents (where necessary) and packaging. For the purpose of these special conditions, a ‘‘battery’’ and ‘‘battery system’’ are referred to as a battery. Issued in Renton, Washington, on April 27, 2017. Paul Bernado, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017–09661 Filed 5–11–17; 8:45 am] The authority citation for these special conditions is as follows: BILLING CODE 4910–13–P Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704. DEPARTMENT OF TRANSPORTATION ■ The Special Conditions ■ Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued as part of the type certification basis for the Bombardier Model BD– 100–1A10 airplane. Non-Rechargeable Lithium Battery Installations In lieu of § 25.1353(b)(1) through (4) at Amendment 25–123 or § 25.1353(c)(1) through (4) at earlier amendments, each non-rechargeable lithium battery installation must: 1. Be designed to maintain safe cell temperatures and pressures under all foreseeable operating conditions to prevent fire and explosion. 2. Be designed to prevent the occurrence of self-sustaining, uncontrollable increases in temperature or pressure. 3. Not emit explosive or toxic gases, either in normal operation or as a result of its failure, that may accumulate in hazardous quantities within the airplane. 4. Meet the requirements of § 25.863. 5. Not damage surrounding structure or adjacent systems, equipment, or electrical wiring from corrosive fluids or gases that may escape in such a way as to cause a major or more severe failure condition. PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 Federal Aviation Administration 14 CFR Part 71 [Docket No. FAA–2016–9494; Airspace Docket No. 16–ASW–19] Amendment of Class E Airspace for Haskell, TX Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: This action modifies Class E airspace extending upward from 700 feet above the surface at Haskell Municipal Airport, Haskell, TX. The decommissioning of the Haskell radio beacon (RBN) and cancellation of RBN approach makes it necessary to implement new area navigation (RNAV) procedures for the safety and management of instrument flight rules (IFR) operations at the airport. This action also updates the geographic coordinates of the airport. DATES: Effective 0901 UTC, September 14, 2017. The Director of the Federal Register approves this incorporation by reference action under Title 1, Code of Federal Regulations, part 51, subject to the annual revision of FAA Order 7400.11 and publication of conforming amendments. ADDRESSES: FAA Order 7400.11A, Airspace Designations and Reporting SUMMARY: E:\FR\FM\12MYR1.SGM 12MYR1

Agencies

[Federal Register Volume 82, Number 91 (Friday, May 12, 2017)]
[Rules and Regulations]
[Pages 22066-22069]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-09661]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 25

[Docket No. FAA-2017-0358; Special Conditions No. 25-659-SC]


Special Conditions: Bombardier Aerospace Inc., Model BD-100-1A10 
Airplane; Non-Rechargeable Lithium Battery Installations

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final special conditions; request for comment.

-----------------------------------------------------------------------

SUMMARY: These special conditions are issued for non-rechargeable 
lithium battery installations on the Bombardier Aerospace Inc. 
(Bombardier) Model BD-100-1A10 airplane. Non-rechargeable lithium 
batteries are a novel or unusual design feature when compared to the 
state of technology envisioned in the airworthiness standards for 
transport category airplanes. The applicable airworthiness regulations 
do not contain adequate or appropriate safety standards for this design 
feature. These special conditions contain the additional safety 
standards that the Administrator considers necessary to establish a 
level

[[Page 22067]]

of safety equivalent to that established by the existing airworthiness 
standards.

DATES: This action is effective on Bombardier on May 12, 2017. We must 
receive your comments by June 26, 2017.

ADDRESSES: Send comments identified by docket number FAA-2017-0358 
using any of the following methods:
     Federal eRegulations Portal: Go to http://www.regulations.gov/ and follow the online instructions for sending 
your comments electronically.
     Mail: Send comments to Docket Operations, M-30, U.S. 
Department of Transportation (DOT), 1200 New Jersey Avenue SE., Room 
W12-140, West Building Ground Floor, Washington, DC 20590-0001.
     Hand Delivery or Courier: Take comments to Docket 
Operations in Room W12-140 of the West Building Ground Floor at 1200 
New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.
     Fax: Fax comments to Docket Operations at 202-493-2251.
    Privacy: The FAA will post all comments it receives, without 
change, to http://www.regulations.gov/, including any personal 
information the commenter provides. Using the search function of the 
docket Web site, anyone can find and read the electronic form of all 
comments received into any FAA docket, including the name of the 
individual sending the comment (or signing the comment for an 
association, business, labor union, etc.). DOT's complete Privacy Act 
Statement can be found in the Federal Register published on April 11, 
2000 (65 FR 19477-19478), as well as at http://DocketsInfo.dot.gov/.
    Docket: Background documents or comments received may be read at 
http://www.regulations.gov/ at any time. Follow the online instructions 
for accessing the docket or go to Docket Operations in Room W12-140 of 
the West Building Ground Floor at 1200 New Jersey Avenue SE., 
Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, 
except Federal holidays.

FOR FURTHER INFORMATION CONTACT: Nazih Khaouly, Airplane and Flight 
Crew Interface Branch, ANM-111, Transport Airplane Directorate, 
Aircraft Certification Service, 1601 Lind Avenue SW., Renton, 
Washington 98057-3356; telephone 425-227-2432; facsimile 425-227-1149.

SUPPLEMENTARY INFORMATION: 

Future Requests for Installation of Non-Rechargeable Lithium Batteries

    The FAA anticipates that non-rechargeable lithium batteries will be 
installed in most makes and models of transport category airplanes. We 
intend to require special conditions for certification projects 
involving non-rechargeable lithium battery installations to address 
certain safety issues until we can revise the airworthiness 
requirements. Applying special conditions to these installations across 
the range of transport category airplanes will ensure regulatory 
consistency.
    Typically, the FAA issues special conditions after receiving an 
application for type certificate approval of a novel or unusual design 
feature. However, the FAA has found that the presence of non-
rechargeable lithium batteries in certification projects is not always 
immediately identifiable, since the battery itself may not be the focus 
of the project. Meanwhile, the inclusion of these batteries has become 
virtually ubiquitous on in-production transport category airplanes, 
which shows that there will be a need for these special conditions. 
Also, delaying the issuance of special conditions until after each 
design application is received could lead to costly certification 
delays. Therefore the FAA finds it necessary to issue special 
conditions applicable to these battery installations on particular 
makes and models of aircraft.
    On April 22, 2016, the FAA published special conditions no. 25-612-
SC in the Federal Register (81 FR 23573) applicable to Gulfstream 
Aerospace Corporation for the GVI airplane. Those were the first 
special conditions the FAA issued for non-rechargeable lithium battery 
installations. We explained in that document our decision to make those 
special conditions effective one year after publication in the Federal 
Register, which is April 22, 2017. In those special conditions, the FAA 
stated its intention to apply non-rechargeable lithium battery special 
conditions to design changes on other makes and models applied for 
after this same date.
    Section 1205 of the FAA Reauthorization Act of 1996 requires the 
FAA to consider the extent to which Alaska is not served by 
transportation modes other than aviation and to establish appropriate 
regulatory distinctions when modifying airworthiness regulations that 
affect intrastate aviation in Alaska. In consideration of this 
requirement and the overall impact on safety, the FAA does not intend 
to require non-rechargeable lithium battery special conditions for 
design changes that only replace a 121.5 megahertz (MHz) emergency 
locator transmitter (ELT) with a 406 MHz ELT that meets Technical 
Standard Order C126b, or later revision, on transport airplanes 
operating only in Alaska. This will support our efforts of encouraging 
operators in Alaska to upgrade to a 406 MHz ELT. These ELTs provide 
significantly improved accuracy for lifesaving services to locate an 
accident site in Alaskan terrain. The FAA considers that the safety 
benefits from upgrading to a 406 MHz ELT for Alaskan operations will 
outweigh the battery fire risk.

Comments Invited

    The substance of these special conditions has been subjected to the 
notice and comment period in prior instances and has been derived 
without substantive change from those previously issued. It is unlikely 
that prior public comment would result in a significant change from the 
substance contained herein. Therefore, the FAA has determined that 
prior public notice and comment are unnecessary and impracticable, and 
good cause exists for adopting these special conditions upon 
publication in the Federal Register. The FAA is requesting comments to 
allow interested persons to submit views that may not have been 
submitted in response to the prior opportunities for comment described 
above.
    We invite interested people to take part in this rulemaking by 
sending written comments, data, or views. The most helpful comments 
reference a specific portion of the special conditions, explain the 
reason for any recommended change, and include supporting data.
    We will consider all comments we receive by the closing date for 
comments. We may change these special conditions based on the comments 
we receive.

Background

    Bombardier holds type certificate no. T00005NY, which provides the 
certification basis for the BD-100-1A10 airplane. The BD-100-1A10 is a 
twin engine, transport category airplane with a passenger seating 
capacity of 16 and a maximum takeoff weight of 38,500 to 40,600 pounds, 
depending on the specific design.
    The FAA is issuing these special conditions for non-rechargeable 
lithium battery installations on the BD-100-1A10 airplane. The current 
battery requirements in title 14, Code of Federal Regulations (14 CFR) 
part 25 are inadequate for addressing an airplane with non-rechargeable 
lithium batteries.

[[Page 22068]]

Type Certification Basis

    Under the provisions of 14 CFR 21.101, Bombardier must show that 
the BD-100-1A10 airplane meets the applicable provisions of the 
regulations listed in type certificate no. T00005NY or the applicable 
regulations in effect on the date of application for the change, except 
for earlier amendments as agreed upon by the FAA. In addition, the 
certification basis includes certain special conditions, exemptions, or 
later amended sections that are not relevant to these special 
conditions.
    If the Administrator finds that the applicable airworthiness 
regulations (i.e., 14 CFR part 25) do not contain adequate or 
appropriate safety standards for the BD-100-1A10 airplane because of a 
novel or unusual design feature, special conditions are prescribed 
under the provisions of Sec.  21.16.
    Special conditions are initially applicable to the airplane model 
for which they are issued. Should the type certificate for that model 
be amended later to include any other model that incorporates the same 
novel or unusual design feature, or should any other model already 
included on the same type certificate be modified to incorporate the 
same novel or unusual design feature, these special conditions would 
also apply to the other model under Sec.  21.101.
    In addition to the applicable airworthiness regulations and special 
conditions, the BD-100-1A10 must comply with the fuel vent and exhaust 
emission requirements of 14 CFR part 34 and the noise certification 
requirements of 14 CFR part 36.
    The FAA issues special conditions, as defined in 14 CFR 11.19, in 
accordance with Sec.  11.38, and they become part of the type 
certification basis under Sec.  21.101.

Novel or Unusual Design Feature

    The novel or unusual design feature is the installation of non-
rechargeable lithium batteries.
    For the purpose of these special conditions, we refer to a battery 
and battery system as a battery. A battery system consists of the 
battery and any protective, monitoring, and alerting circuitry or 
hardware inside or outside of the battery. It also includes vents 
(where necessary) and packaging.

Discussion

    The FAA derived the current regulations governing installation of 
batteries in transport category airplanes from Civil Air Regulations 
(CAR) 4b.625(d) as part of the recodification of CAR 4b that 
established 14 CFR part 25 in February 1965. This recodification 
basically reworded the CAR 4b battery requirements, which are currently 
in Sec.  25.1353(b)(1) through (4). Non-rechargeable lithium batteries 
are novel and unusual with respect to the state of technology 
considered when these requirements were codified. These batteries 
introduce higher energy levels into airplane systems through new 
chemical compositions in various battery cell sizes and construction. 
Interconnection of these cells in battery packs introduces failure 
modes that require unique design considerations, such as provisions for 
thermal management.
    Recent events involving rechargeable and non-rechargeable lithium 
batteries prompted the FAA to initiate a broad evaluation of these 
energy storage technologies. In January 2013, two independent events 
involving rechargeable lithium-ion batteries revealed unanticipated 
failure modes. A National Transportation Safety Board (NTSB) letter to 
the FAA, dated May 22, 2014, which is available at http://www.ntsb.gov, 
filename A-14-032-036.pdf, describes these events.
    On July 12, 2013, an event involving a non-rechargeable lithium 
battery in an emergency locator transmitter installation demonstrated 
unanticipated failure modes. The United Kingdom's Air Accidents 
Investigation Branch Bulletin S5/2013 describes this event.
    Some known uses of rechargeable and non-rechargeable lithium 
batteries on airplanes include:
     Flight deck and avionics systems such as displays, global 
positioning systems, cockpit voice recorders, flight data recorders, 
underwater locator beacons, navigation computers, integrated avionics 
computers, satellite network and communication systems, communication 
management units, and remote-monitor electronic line-replaceable units;
     Cabin safety, entertainment, and communications equipment, 
including emergency locator transmitters, life rafts, escape slides, 
seatbelt air bags, cabin management systems, Ethernet switches, routers 
and media servers, wireless systems, Internet and in-flight 
entertainment systems, satellite televisions, remotes, and handsets;
     Systems in cargo areas including door controls, sensors, 
video surveillance equipment, and security systems.
    Some known potential hazards and failure modes associated with non-
rechargeable lithium batteries are:
     Internal failures: In general, these batteries are 
significantly more susceptible to internal failures that can result in 
self-sustaining increases in temperature and pressure (i.e., thermal 
runaway) than their nickel-cadmium or lead-acid counterparts. The 
metallic lithium can ignite, resulting in a self-sustaining fire or 
explosion.
     Fast or imbalanced discharging: Fast discharging or an 
imbalanced discharge of one cell of a multi-cell battery may create an 
overheating condition that results in an uncontrollable venting 
condition, which in turn leads to a thermal event or an explosion.
     Flammability: Unlike nickel-cadmium and lead-acid 
batteries, lithium batteries use higher energy and current in an 
electrochemical system that can be configured to maximize energy 
storage of lithium. They also use liquid electrolytes that can be 
extremely flammable. The electrolyte, as well as the electrodes, can 
serve as a source of fuel for an external fire if the battery casing is 
breached.
    Special condition no. 1 of these special conditions requires that 
each individual cell within a non-rechargeable lithium battery be 
designed to maintain safe temperatures and pressures. Special condition 
no. 2 addresses these same issues but for the entire battery. Special 
condition no. 2 requires the battery be designed to prevent propagation 
of a thermal event, such as self-sustained, uncontrollable increases in 
temperature or pressure from one cell to adjacent cells.
    Special conditions nos. 1 and 2 are intended to ensure that the 
non-rechargeable lithium battery and its cells are designed to 
eliminate the potential for uncontrollable failures. However, a certain 
number of failures will occur due to various factors beyond the control 
of the battery designer. Therefore, other special conditions are 
intended to protect the airplane and its occupants if failure occurs.
    Special conditions 3, 7, and 8 are self-explanatory.
    Special condition no. 4 makes it clear that the flammable fluid 
fire protection requirements of Sec.  25.863 apply to non-rechargeable 
lithium battery installations. Section 25.863 is applicable to areas of 
the airplane that could be exposed to flammable fluid leakage from 
airplane systems. Non-rechargeable lithium batteries contain an 
electrolyte that is a flammable fluid.
    Special condition no. 5 requires that each non-rechargeable lithium 
battery installation not damage surrounding structure or adjacent 
systems, equipment, or electrical wiring from corrosive fluids or gases 
that may escape in such a way as to cause a major or more severe 
failure condition.

[[Page 22069]]

    While special condition no. 5 addresses corrosive fluids and gases, 
special condition no. 6 addresses heat. Special condition no. 6 
requires that each non-rechargeable lithium battery installation have 
provisions to prevent any hazardous effect on airplane structure or 
systems caused by the maximum amount of heat the battery installation 
can generate due to any failure of it or its individual cells. The 
means of meeting special conditions nos. 5 and 6 may be the same, but 
the requirements are independent and address different hazards.
    These special conditions apply to all non-rechargeable lithium 
battery installations in lieu of Sec.  25.1353(b)(1) through (4) at 
Amendment 25-123 or Sec.  25.1353(c)(1) through (4) at earlier 
amendments. Those regulations remain in effect for other battery 
installations.
    These special conditions contain the additional safety standards 
that the Administrator considers necessary to establish a level of 
safety equivalent to that established by the existing airworthiness 
standards.

Applicability

    These special conditions are applicable to the BD-100-1A10 
airplane. Should Bombardier apply at a later date for a change to the 
type certificate to include another model incorporating the same novel 
or unusual design feature, these special conditions would apply to that 
model as well.
    These special conditions are only applicable to design changes 
applied for after the effective date.
    These special conditions are not applicable to changes to 
previously certified non-rechargeable lithium battery installations 
where the only change is either cosmetic or to relocate the 
installation to improve the safety of the airplane and occupants. 
Previously certified non-rechargeable lithium battery installations, as 
used in this paragraph, are those installations approved for 
certification projects applied for on or before the effective date of 
these special conditions. A cosmetic change is a change in appearance 
only, and does not change any function or safety characteristic of the 
battery installation. These special conditions are also not applicable 
to unchanged, previously certified non-rechargeable lithium battery 
installations that are affected by a change in a manner that improves 
the safety of its installation. The FAA determined that these 
exclusions are in the public interest because the need to meet all of 
the special conditions might otherwise deter these design changes that 
improve safety.

Conclusion

    This action affects only a certain novel or unusual design feature 
on one model of airplane. It is not a rule of general applicability.
    The substance of these special conditions has been subjected to the 
notice and comment period in prior instances and has been derived 
without substantive change from those previously issued. It is unlikely 
that prior public comment would result in a significant change from the 
substance contained herein. Therefore, the FAA has determined that 
prior public notice and comment are unnecessary and impracticable, and 
good cause exists for adopting these special conditions upon 
publication in the Federal Register. The FAA is requesting comments to 
allow interested persons to submit views that may not have been 
submitted in response to the prior opportunities for comment described 
above.

List of Subjects in 14 CFR Part 25

    Aircraft, Aviation safety, Reporting and record keeping 
requirements.


0
The authority citation for these special conditions is as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.

The Special Conditions

0
Accordingly, pursuant to the authority delegated to me by the 
Administrator, the following special conditions are issued as part of 
the type certification basis for the Bombardier Model BD-100-1A10 
airplane.

Non-Rechargeable Lithium Battery Installations

    In lieu of Sec.  25.1353(b)(1) through (4) at Amendment 25-123 or 
Sec.  25.1353(c)(1) through (4) at earlier amendments, each non-
rechargeable lithium battery installation must:
    1. Be designed to maintain safe cell temperatures and pressures 
under all foreseeable operating conditions to prevent fire and 
explosion.
    2. Be designed to prevent the occurrence of self-sustaining, 
uncontrollable increases in temperature or pressure.
    3. Not emit explosive or toxic gases, either in normal operation or 
as a result of its failure, that may accumulate in hazardous quantities 
within the airplane.
    4. Meet the requirements of Sec.  25.863.
    5. Not damage surrounding structure or adjacent systems, equipment, 
or electrical wiring from corrosive fluids or gases that may escape in 
such a way as to cause a major or more severe failure condition.
    6. Have provisions to prevent any hazardous effect on airplane 
structure or systems caused by the maximum amount of heat it can 
generate due to any failure of it or its individual cells.
    7. Have a failure sensing and warning system to alert the 
flightcrew if its failure affects safe operation of the airplane.
    8. Have a means for the flightcrew or maintenance personnel to 
determine the battery charge state if the battery's function is 
required for safe operation of the airplane.

    Note: A battery system consists of the battery and any 
protective, monitoring, and alerting circuitry or hardware inside or 
outside of the battery. It also includes vents (where necessary) and 
packaging. For the purpose of these special conditions, a 
``battery'' and ``battery system'' are referred to as a battery.


    Issued in Renton, Washington, on April 27, 2017.
Paul Bernado,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2017-09661 Filed 5-11-17; 8:45 am]
BILLING CODE 4910-13-P