Special Conditions: Costruzioni Aeronautiche Tecnam S.P.A.; Model P2012 Airplane; Installation of Rechargeable Lithium Batteries, 17733-17736 [2019-08477]

Download as PDF Federal Register / Vol. 84, No. 81 / Friday, April 26, 2019 / Rules and Regulations P2012 airplane meets the applicable provisions of part 23, as amended by amendment 23–1 through 23–62 thereto. If the Administrator finds that the applicable airworthiness regulations in part 23 do not contain adequate or appropriate safety standards for the Model P2012 airplane because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16. In addition to the applicable airworthiness regulations and special conditions, the Model P2012 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; and the FAA must issue a finding of regulatory adequacy under § 611 of Public Law 92– 574, the ‘‘Noise Control Act of 1972.’’ The FAA issues special conditions, as defined in § 11.19, under § 11.38 and they become part of the type certification basis under § 21.17(a)(2). Special conditions are initially applicable to the 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, the FAA would apply these special conditions to the other model. Novel or Unusual Design Features The Model P2012 airplane will incorporate the following novel or unusual design features: The installation of an Electronic Engine Control (EEC) system. The EEC system is the generic family of electrical/ electronic engine control systems, including full authority digital engine controls, supervisory controls, and derivatives of these. amozie on DSK9F9SC42PROD with RULES Discussion This airplane makes use of an electronic engine control system in addition to a traditional mechanical control system, which is a novel design for this type of airplane. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. Mandating a structured assessment to determine potential installation issues mitigate the concerns that the addition of an electronic engine control does not produce a failure condition not previously considered. Applicability These special conditions are applicable to the Model P2012 airplane. Should Tecnam apply at a later date for a change to the type certificate to include another model incorporating the VerDate Sep<11>2014 16:06 Apr 25, 2019 Jkt 247001 same novel or unusual design feature, the FAA would apply these special conditions to that model as well. Conclusion This action affects only a certain novel or unusual design feature on the Model P2012 airplane. It is not a rule of general applicability. List of Subjects in 14 CFR Part 23 Aircraft, Aviation safety, Signs and symbols. Citation The authority citation for these special conditions is as follows: Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701–44702; Pub. L. 113–53, 127 Stat 584 (49 U.S.C. 44704) note. 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 Tecnam Model P2012 airplane. 1. Installation of Electronic Engine Control System a. For electronic engine control (EEC) system installations, it must be established that no single failure or malfunction or probable combinations of failures of EEC system components will have an effect on the system, as installed in the airplane, that causes the Loss of Power Control (LOPC) probability of the system to exceed those allowed in part 33 certification. b. Electronic engine control system installations must be evaluated for environmental and atmospheric conditions, including lightning and High Intensity Radiated Fields (HIRF). The EEC system lightning and HIRF effects that result in LOPC should be considered catastrophic. c. The components of the installation must be constructed, arranged, and installed to ensure their continued safe operation between normal inspections or overhauls. d. Functions incorporated into any electronic engine control that make it part of any equipment, systems or installation whose functions are beyond that of basic engine control, and which may also introduce system failures and malfunctions, are not exempt from § 23.1309 and must be shown to meet part 23 levels of safety as derived from § 23.1309. Part 33 certification data, if applicable, may be used to show compliance with any part 23 requirements. If part 33 data is used to substantiate compliance with part 23 requirements, then the part 23 applicant PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 17733 must be able to provide this data for its showing of compliance. Note: The term ‘‘probable’’ in the context of ‘‘probable combination of failures’’ does not have the same meaning as used for a safety assessment process. The term ‘‘probable’’ in ‘‘probable combination of failures’’ means ‘‘foreseeable,’’ or those failure conditions anticipated to occur one or more times during the operational life of each airplane. Issued in Kansas City, Missouri, on April 22, 2019. William Schinstock, Acting Manager, Small Airplane Standards Branch, Policy and Innovation Division, Aircraft Certification Service. [FR Doc. 2019–08476 Filed 4–25–19; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 23 [Docket No. FAA–2019–0301; Special Conditions No. 23–293–SC] Special Conditions: Costruzioni Aeronautiche Tecnam S.P.A.; Model P2012 Airplane; Installation of Rechargeable Lithium Batteries Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; request for comments. AGENCY: These special conditions are issued for the Costruzioni Aeronautiche Tecnam S.P.A., Model P2012 airplane. These airplanes will have a novel or unusual design feature associated with the installation of a rechargeable lithium battery. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. DATES: The effective date of these special conditions is April 26, 2019. We must receive your comments by May 28, 2019. ADDRESSES: Send comments identified by docket number FAA–2019–0301 using any of the following methods: • Federal eRegulations Portal: Go to https://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 SUMMARY: E:\FR\FM\26APR1.SGM 26APR1 17734 Federal Register / Vol. 84, No. 81 / Friday, April 26, 2019 / Rules and Regulations Building Ground Floor, Washington, DC 20590–0001. • Hand Delivery 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 https://regulations.gov, including any personal information the commenter provides. Using the search function of the docket website, 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). Docket: Background documents or comments received may be read at https://www.regulations.gov at any time. Follow the online instructions for accessing the docket or go to the 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: Ruth Hirt, Federal Aviation Administration, Aircraft Certification Service, Small Airplane Directorate, AIR–694, 901 Locust, Room 301, Kansas City, MO; telephone (816) 329–4108; facsimile (816)-329 4090. SUPPLEMENTARY INFORMATION: amozie on DSK9F9SC42PROD with RULES Reason for No Prior Notice and Comment Before Adoption The FAA has determined, in accordance with 5 U.S. Code §§ 553(b)(3)(B) and 553(d)(3), that notice and opportunity for prior public comment are unnecessary because substantially identical special conditions have been subjected to the public comment process in several prior instances such that the FAA is satisfied that new comments are unlikely. For the same reason, the FAA finds that good cause exists for making these special conditions effective upon issuance. 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. VerDate Sep<11>2014 16:46 Apr 25, 2019 Jkt 247001 Special conditions No. Company/airplane model 23–15–01–SC 1 23–16–02–SC 2 23–288–SC 3 ..... Kestrel Aircraft Company/Model K–350. Pilatus Aircraft, Ltd, Models PC12, PC–12/45, and PC–12/ 47. St. Louis Helicopter, LLC, Textron Aviation Models B300, B300C, B300C(MC–12W), and B300C (UC–12W). 1 https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/0/39B156C006EB842E8625 7EF3004BB13C?OpenDocument& Highlight=installation%20of%20rechargeable %20lithium%20battery. 2 https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/0/5A2FEC165CB49130 86258019005C34E2?OpenDocument&Highlight=23278-sc. 3 https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/0/B2D62B06A314D7418625 8282005F5E04?OpenDocument&Highlight=23-288sc. Comments Invited 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 on or before the closing date for comments. We will consider comments filed late if it is possible to do so without incurring expense or delay. We may change these special conditions based on the comments we receive. Background On March 13, 2018, Costruzioni Aeronautiche Tecnam S.P.A. (Tecnam) applied for FAA validation of its type certificate for its new Model P2012 airplane. The airplane is a normal category, metallic, non-pressurized, high wing, monoplane that will seat nine passengers and two flightcrew. Two wing mounted Lycoming Model TEO–540–C1A piston engines driving four blade variable pitch constant speed MT-Propellers USA, Inc. Model MTV– 14–B–C–F/CF195–30b propellers power the airplane. The airplane has fixed tricycle landing gear, a Garmin G1000 NXi avionics suite, and a maximum takeoff weight of 7,937 pounds. The Model P2012 has rechargeable lithium batteries installed for higher energy density instead of the nickel-cadmium (Ni-Cd) or lead-acid rechargeable batteries. The current regulatory requirements for part 23 airplanes do not contain adequate requirements for use of rechargeable lithium batteries in airborne applications. This type of battery possesses certain failure and operational characteristics with maintenance requirements that differ PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 significantly from that of the nickelcadmium (Ni-Cd) and lead-acid rechargeable batteries approved in § 23.1553, amendment 23–62 or earlier, for other normal, utility, acrobatic, and commuter category airplanes. Therefore, the FAA is issuing this special condition to address— • All characteristics of the rechargeable lithium batteries and their installation that could affect safe operation of the Model P2012 airplane; and • Appropriate Instructions for Continued Airworthiness (ICA) that include maintenance requirements to ensure the availability of electrical power from the batteries when needed. Type Certification Basis Under the provisions of § 21.17, Tecnam must show that the Model P2012 airplane meets the applicable provisions of part 23, as amended by amendment 23–1 through 23–62 thereto. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 23) do not contain adequate or appropriate safety standards for the Model P2012 airplane because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16. In addition to the applicable airworthiness regulations and special conditions, the Model P2012 airplane 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; and the FAA must issue a finding of regulatory adequacy under § 611 of Public Law 92– 574, the ‘‘Noise Control Act of 1972.’’ The FAA issues special conditions, as defined in § 11.19, under § 11.38 and they become part of the type certification basis under § 21.17(a)(2). Special conditions are initially applicable to the models 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, the FAA would apply these special conditions to the other model. Novel or Unusual Design Features The Model P2012 airplane will incorporate the following novel or unusual design features: The installation of a rechargeable lithium battery—intended as energy storage for the airplane—will power the essential load for continued safe flight and landing if the electrical generating system fails. E:\FR\FM\26APR1.SGM 26APR1 Federal Register / Vol. 84, No. 81 / Friday, April 26, 2019 / Rules and Regulations amozie on DSK9F9SC42PROD with RULES Discussion The applicable regulations governing the installation of batteries in general aviation airplanes were derived from Civil Air Regulations (CAR) 3 as part of the recodification that established 14 CFR part 23. The battery requirements identified in § 23.1353 were a rewording of the CAR requirements. Subsequent rulemaking activities—resulting from increased incidents of Ni-Cd battery fire or failures—added § 23.1353(f) and (g), amendments 23–20 and 23–21, respectively. The FAA did not envision the introduction of lithium battery installations when these regulations were published. The proposed use of rechargeable lithium batteries prompted the FAA to review the adequacy of these existing regulations. We determined the existing regulations do not adequately address the safety of lithium battery installations. Current experience with rechargeable lithium batteries in commercial or general aviation is limited. However, other users of this technology—ranging from personal computers, to wireless telephone manufacturers, to the electric vehicle industry—have noted safety problems with rechargeable lithium batteries. These problems, as described in the following paragraphs, include overcharging, over-discharging, flammability of cell components, cell internal defects, and hazards resulting from exposure to extreme temperatures. 1. Overcharging. In general, rechargeable lithium batteries are significantly more susceptible than their Ni-Cd or lead-acid counterparts to thermal runaway, which is an internal failure that can result in self-sustaining increases in temperature and pressure. This is especially true for overcharging, which causes heating and destabilization of the components of the cell, leading to the formation (by plating) of highly unstable metallic lithium. The metallic lithium can ignite, resulting in a self-sustaining fire or explosion. Finally, the severity of thermal runaway due to overcharging increases with increasing battery capacity due to the higher amount of electrolyte in large batteries. 2. Over-discharging. Discharge of some types of rechargeable lithium battery cells beyond the manufacturer’s recommended specification can cause corrosion of the electrodes of the cell, resulting in loss of battery capacity that cannot be reversed by recharging. This loss of capacity may not be detected by the simple voltage measurements commonly available to flight crews as a means of checking battery status—a VerDate Sep<11>2014 16:06 Apr 25, 2019 Jkt 247001 problem shared with Ni-Cd batteries. In addition, over-discharging has the potential to lead to an unsafe condition (creation of dendrites that could result in internal short circuit during the recharging cycle). 3. Flammability of Cell Components. Unlike Ni-Cd and lead-acid batteries, some types of rechargeable lithium batteries use liquid electrolytes that are flammable. The electrolyte can serve as a source of fuel for an external fire, if there is a breach of the battery container. 4. Cell Internal Defects. The rechargeable lithium batteries and rechargeable battery systems have a history of undetected cell internal defects. These defects may or may not be detected during normal operational evaluation, test, and validation. This may lead to an unsafe condition during in-service operation. 5. Extreme Temperatures. Exposure to an extreme temperature environment has the potential to create major hazards. Care must be taken to ensure that the lithium battery remains within the manufacturer’s recommended specification. Applicability As discussed above, these special conditions are applicable to the Model P2012 airplane. Should Tecnam apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, the FAA would apply these special conditions to that model as well. Conclusion This action affects only certain novel or unusual design features on the Model P2012 airplane. It is not a rule of general applicability. List of Subjects in 14 CFR Part 23 Aircraft, Aviation safety, Signs and symbols. Citation The authority citation for these special conditions is as follows: Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701–44702, 44704, Pub. L. 113–53, 127 Stat 584 (49 U.S.C. 44704) note The Special Conditions Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued, in lieu of the requirements in § 23.1353 (a), (b), (c), (d), and (e), amendment 23–62, as part of the type certification basis for the Tecnam Model P2012 airplane. PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 17735 Installation of Lithium Battery Lithium battery installations must be designed and installed as follows: (1) Safe cell temperatures and pressures must be maintained during— i. Normal operations; ii. Any probable failure conditions of charging or discharging or battery monitoring system; and iii. Any failure of the charging or battery monitoring system shown to not be extremely remote. (2) The rechargeable lithium battery installation must be designed to preclude explosion and fire in the event of a failure under (1)(ii) and (1)(iii) above. (3) Design of the rechargeable lithium batteries must preclude the occurrence of self-sustaining, uncontrolled increases in temperature or pressure. (4) No explosive or toxic gasses emitted by any rechargeable lithium battery in normal operation or as the result of any failure of the battery charging system, monitoring system, or battery installation, which is shown to not be extremely remote, may accumulate in hazardous quantities within the airplane. (5) Installations of rechargeable lithium batteries must meet the requirements of § 23.863(a) through (d), amendment 23–34. (6) No corrosive fluids or gases that may escape from any rechargeable lithium battery may damage surrounding structure or any adjacent systems, equipment, electrical wiring, or the airplane in such a way as to cause a major or more severe failure condition, in accordance with § 23.1309, amendment 23–62. (7) Each rechargeable lithium battery installation must have provisions to prevent any hazardous effect on structure or essential systems that may be caused by the maximum amount of heat the battery can generate during a short circuit of the battery or of its individual cells. (8) Rechargeable lithium battery installations must have a system to automatically control the charging rate of the battery to prevent battery overheating and overcharging, and either: i. A battery temperature sensing and over-temperature warning system with a means for automatically disconnecting the battery from its charging source in the event of an over-temperature condition; or ii. A battery failure sensing and warning system with a means for automatically disconnecting the battery from its charging source in the event of battery failure. E:\FR\FM\26APR1.SGM 26APR1 17736 Federal Register / Vol. 84, No. 81 / Friday, April 26, 2019 / Rules and Regulations (9) Any rechargeable lithium battery installation, the function of which is required for safe operation of the aircraft, must incorporate a monitoring and warning feature that will provide an indication to the appropriate flight crewmembers whenever the state of charge of the batteries has fallen below levels considered acceptable for dispatch of the aircraft. Note 1 to paragraph (9): Reference § 23.1353(h) for dispatch consideration. Note 2 to paragraph (10): Maintenance requirements include procedures that check battery capacity, charge degradation at manufacturer’s recommended inspection intervals, and replace batteries at manufacturer’s recommended replacement schedule/time to prevent age-related degradation. Note 3 to paragraph (10): The term ‘‘sufficiently charged’’ means that the battery must retain enough charge, expressed in ampere-hours, to ensure that the battery cells will not be damaged. A battery cell may be damaged by low charge (i.e., below certain level), resulting in a reduction in the ability to charge and retain a full charge. This reduction would be greater than the reduction that may result from normal operational degradation. amozie on DSK9F9SC42PROD with RULES Note 4 to paragraph (10): Replacement battery in spares storage may be subject to prolonged storage at a low state of charge. Issued in Kansas City, Missouri, on April 22, 2019. William Schinstock, Acting Manager, Small Airplane Standards Branch, Policy and Innovation Division, Aircraft Certification Service. BILLING CODE 4910–13–P VerDate Sep<11>2014 16:06 Apr 25, 2019 Jkt 247001 Federal Aviation Administration 14 CFR Part 71 [Docket No. FAA–2019–0039; Airspace Docket No. 19–AGL–4] RIN 2120–AA66 Amendment of Class E Airspace; Connersville and Richmond, IN Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: (10) The Instructions for Continued Airworthiness (ICA) required by § 23.1529 must contain maintenance requirements to ensure that the battery has been sufficiently charged at appropriate intervals specified by the battery manufacturer and the equipment manufacturer that contain the rechargeable lithium battery or rechargeable lithium battery system. The lithium rechargeable batteries and lithium rechargeable battery systems must not degrade below specified ampere-hour levels sufficient to power the aircraft system. The ICA must also contain procedures for the maintenance of replacement batteries to prevent the installation of batteries that have degraded charge retention ability or other damage due to prolonged storage at a low state of charge. Replacement batteries must be of the same manufacturer and part number as approved by the FAA. [FR Doc. 2019–08477 Filed 4–25–19; 8:45 am] DEPARTMENT OF TRANSPORTATION This action modifies Class E airspace extending upward from 700 feet above the surface at Mettel Field Airport, Connersville, IN, and Richmond Municipal Airport, Richmond, IN. This action is due to an airspace review caused by the decommissioning of the Richmond VHF omnidirectional range (VOR), which provided navigation information to the instrument procedures at these airports, as part of the VOR Minimum Operational Network (MON) Program. The geographic coordinates of the airports are also being updated to coincide with the FAA’s aeronautic database. Airspace redesign is necessary for the safety and management of instrument flight rules (IFR) operations at these airports. DATES: Effective 0901 UTC, August 15, 2019. 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 7400.11C, Airspace Designations and Reporting Points, and subsequent amendments can be viewed online at https://www.faa.gov/ air_traffic/publications/. For further information, you can contact the Airspace Policy Group, Federal Aviation Administration, 800 Independence Avenue SW, Washington, DC 20591; telephone: (202) 267–8783. The Order is also available for inspection at the National Archives and Records Administration (NARA). For information on the availability of FAA Order 7400.11C at NARA, call (202) 741–6030, or go to https:// www.archives.gov/federal-register/cfr/ ibr-locations.html. FAA Order 7400.11, Airspace Designations and Reporting Points, is published yearly and effective on September 15. FOR FURTHER INFORMATION CONTACT: Jeffrey Claypool, Federal Aviation SUMMARY: PO 00000 Frm 00008 Fmt 4700 Sfmt 4700 Administration, Operations Support Group, Central Service Center, 10101 Hillwood Parkway, Fort Worth, TX 76177; telephone (817) 222–5711. SUPPLEMENTARY INFORMATION: Authority for This Rulemaking The FAA’s authority to issue rules regarding aviation safety is found in Title 49 of the United States Code. 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. This rulemaking is promulgated under the authority described in Subtitle VII, Part A, Subpart I, Section 40103. Under that section, the FAA is charged with prescribing regulations to assign the use of airspace necessary to ensure the safety of aircraft and the efficient use of airspace. This regulation is within the scope of that authority as it amends Class E airspace extending upward from 700 feet above the surface at Mettel Field Airport, Connersville, IN, and Richmond Municipal Airport, Richmond, IN, to support IFR operations at these airports. History The FAA published a notice of proposed rulemaking in the Federal Register (84 FR 5014; February 20, 2019) for Docket No. FAA–2019–0039 to amend Class E airspace extending upward from 700 feet above the surface at Mettel Field Airport, Connersville, IN, and Richmond Municipal Airport, Richmond, IN. Interested parties were invited to participate in this rulemaking effort by submitting written comments on the proposal to the FAA. One comment was received, and the FAA provides the following response. Class E airspace extending from 700 feet above the surface of an airport is provided for transition to and from the terminal or en route environment within the National Airspace System. The size and design of this airspace is determined by FAA Order 7400.2M, Procedures for Handling Airspace Matters, and takes both instrument and visual flight rules approach and departure procedures at the airports into consideration. The design of the airspace provides the transitional airspace required without absorbing more of the Class G airspace than is required. In the cases of Mettel Field Airport, Connersville, IN, and Richmond Municipal Airport, Richmond, IN, Class E airspace extending upward from 700 feet above the surface already exists at both airports and no additional airspace is included in the proposal. The airspace E:\FR\FM\26APR1.SGM 26APR1

Agencies

[Federal Register Volume 84, Number 81 (Friday, April 26, 2019)]
[Rules and Regulations]
[Pages 17733-17736]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-08477]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 23

[Docket No. FAA-2019-0301; Special Conditions No. 23-293-SC]


Special Conditions: Costruzioni Aeronautiche Tecnam S.P.A.; Model 
P2012 Airplane; Installation of Rechargeable Lithium Batteries

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final special conditions; request for comments.

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

SUMMARY: These special conditions are issued for the Costruzioni 
Aeronautiche Tecnam S.P.A., Model P2012 airplane. These airplanes will 
have a novel or unusual design feature associated with the installation 
of a rechargeable lithium battery. The applicable airworthiness 
regulations do not contain adequate or appropriate safety standards for 
this design feature. These special conditions contain the additional 
safety standards the Administrator considers necessary to establish a 
level of safety equivalent to that established by the existing 
airworthiness standards.

DATES: The effective date of these special conditions is April 26, 
2019.
    We must receive your comments by May 28, 2019.

ADDRESSES: Send comments identified by docket number FAA-2019-0301 
using any of the following methods:
     Federal eRegulations Portal: Go to https://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

[[Page 17734]]

Building Ground Floor, Washington, DC 20590-0001.
     Hand Delivery 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 https://regulations.gov, including any personal information 
the commenter provides. Using the search function of the docket 
website, 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).
    Docket: Background documents or comments received may be read at 
https://www.regulations.gov at any time. Follow the online instructions 
for accessing the docket or go to the 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: Ruth Hirt, Federal Aviation 
Administration, Aircraft Certification Service, Small Airplane 
Directorate, AIR-694, 901 Locust, Room 301, Kansas City, MO; telephone 
(816) 329-4108; facsimile (816)-329 4090.

SUPPLEMENTARY INFORMATION:

Reason for No Prior Notice and Comment Before Adoption

    The FAA has determined, in accordance with 5 U.S. Code Sec. Sec.  
553(b)(3)(B) and 553(d)(3), that notice and opportunity for prior 
public comment are unnecessary because substantially identical special 
conditions have been subjected to the public comment process in several 
prior instances such that the FAA is satisfied that new comments are 
unlikely. For the same reason, the FAA finds that good cause exists for 
making these special conditions effective upon issuance. 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.

------------------------------------------------------------------------
         Special conditions No.               Company/airplane model
------------------------------------------------------------------------
23-15-01-SC \1\........................  Kestrel Aircraft Company/Model
                                          K-350.
23-16-02-SC \2\........................  Pilatus Aircraft, Ltd, Models
                                          PC12, PC-12/45, and PC-12/47.
23-288-SC \3\..........................  St. Louis Helicopter, LLC,
                                          Textron Aviation Models B300,
                                          B300C, B300C(MC-12W), and
                                          B300C (UC-12W).
------------------------------------------------------------------------
\1\ https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/0/39B156C006EB842E86257EF3004BB13C?OpenDocument&Highlight=installation%20of%20rechargeable%20lithium%20battery.
\2\ https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/0/5A2FEC165CB4913086258019005C34E2?OpenDocument&Highlight=23-278-sc.
\3\ https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgSC.nsf/0/B2D62B06A314D74186258282005F5E04?OpenDocument&Highlight=23-288-sc.

Comments Invited

    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 on or before the closing 
date for comments. We will consider comments filed late if it is 
possible to do so without incurring expense or delay. We may change 
these special conditions based on the comments we receive.

Background

    On March 13, 2018, Costruzioni Aeronautiche Tecnam S.P.A. (Tecnam) 
applied for FAA validation of its type certificate for its new Model 
P2012 airplane. The airplane is a normal category, metallic, non-
pressurized, high wing, monoplane that will seat nine passengers and 
two flightcrew. Two wing mounted Lycoming Model TEO-540-C1A piston 
engines driving four blade variable pitch constant speed MT-Propellers 
USA, Inc. Model MTV-14-B-C-F/CF195-30b propellers power the airplane. 
The airplane has fixed tricycle landing gear, a Garmin G1000 NXi 
avionics suite, and a maximum takeoff weight of 7,937 pounds. The Model 
P2012 has rechargeable lithium batteries installed for higher energy 
density instead of the nickel-cadmium (Ni-Cd) or lead-acid rechargeable 
batteries.
    The current regulatory requirements for part 23 airplanes do not 
contain adequate requirements for use of rechargeable lithium batteries 
in airborne applications. This type of battery possesses certain 
failure and operational characteristics with maintenance requirements 
that differ significantly from that of the nickel-cadmium (Ni-Cd) and 
lead-acid rechargeable batteries approved in Sec.  23.1553, amendment 
23-62 or earlier, for other normal, utility, acrobatic, and commuter 
category airplanes. Therefore, the FAA is issuing this special 
condition to address--
     All characteristics of the rechargeable lithium batteries 
and their installation that could affect safe operation of the Model 
P2012 airplane; and
     Appropriate Instructions for Continued Airworthiness (ICA) 
that include maintenance requirements to ensure the availability of 
electrical power from the batteries when needed.

Type Certification Basis

    Under the provisions of Sec.  21.17, Tecnam must show that the 
Model P2012 airplane meets the applicable provisions of part 23, as 
amended by amendment 23-1 through 23-62 thereto.
    If the Administrator finds that the applicable airworthiness 
regulations (i.e., 14 CFR part 23) do not contain adequate or 
appropriate safety standards for the Model P2012 airplane because of a 
novel or unusual design feature, special conditions are prescribed 
under the provisions of Sec.  21.16.
    In addition to the applicable airworthiness regulations and special 
conditions, the Model P2012 airplane 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; and the FAA must issue a 
finding of regulatory adequacy under Sec.  611 of Public Law 92-574, 
the ``Noise Control Act of 1972.''
    The FAA issues special conditions, as defined in Sec.  11.19, under 
Sec.  11.38 and they become part of the type certification basis under 
Sec.  21.17(a)(2).
    Special conditions are initially applicable to the models 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, the FAA would apply these special conditions to 
the other model.

Novel or Unusual Design Features

    The Model P2012 airplane will incorporate the following novel or 
unusual design features: The installation of a rechargeable lithium 
battery--intended as energy storage for the airplane--will power the 
essential load for continued safe flight and landing if the electrical 
generating system fails.

[[Page 17735]]

Discussion

    The applicable regulations governing the installation of batteries 
in general aviation airplanes were derived from Civil Air Regulations 
(CAR) 3 as part of the recodification that established 14 CFR part 23. 
The battery requirements identified in Sec.  23.1353 were a rewording 
of the CAR requirements. Subsequent rulemaking activities--resulting 
from increased incidents of Ni-Cd battery fire or failures--added Sec.  
23.1353(f) and (g), amendments 23-20 and 23-21, respectively. The FAA 
did not envision the introduction of lithium battery installations when 
these regulations were published.
    The proposed use of rechargeable lithium batteries prompted the FAA 
to review the adequacy of these existing regulations. We determined the 
existing regulations do not adequately address the safety of lithium 
battery installations.
    Current experience with rechargeable lithium batteries in 
commercial or general aviation is limited. However, other users of this 
technology--ranging from personal computers, to wireless telephone 
manufacturers, to the electric vehicle industry--have noted safety 
problems with rechargeable lithium batteries. These problems, as 
described in the following paragraphs, include overcharging, over-
discharging, flammability of cell components, cell internal defects, 
and hazards resulting from exposure to extreme temperatures.
    1. Overcharging. In general, rechargeable lithium batteries are 
significantly more susceptible than their Ni-Cd or lead-acid 
counterparts to thermal runaway, which is an internal failure that can 
result in self-sustaining increases in temperature and pressure. This 
is especially true for overcharging, which causes heating and 
destabilization of the components of the cell, leading to the formation 
(by plating) of highly unstable metallic lithium. The metallic lithium 
can ignite, resulting in a self-sustaining fire or explosion. Finally, 
the severity of thermal runaway due to overcharging increases with 
increasing battery capacity due to the higher amount of electrolyte in 
large batteries.
    2. Over-discharging. Discharge of some types of rechargeable 
lithium battery cells beyond the manufacturer's recommended 
specification can cause corrosion of the electrodes of the cell, 
resulting in loss of battery capacity that cannot be reversed by 
recharging. This loss of capacity may not be detected by the simple 
voltage measurements commonly available to flight crews as a means of 
checking battery status--a problem shared with Ni-Cd batteries. In 
addition, over-discharging has the potential to lead to an unsafe 
condition (creation of dendrites that could result in internal short 
circuit during the recharging cycle).
    3. Flammability of Cell Components. Unlike Ni-Cd and lead-acid 
batteries, some types of rechargeable lithium batteries use liquid 
electrolytes that are flammable. The electrolyte can serve as a source 
of fuel for an external fire, if there is a breach of the battery 
container.
    4. Cell Internal Defects. The rechargeable lithium batteries and 
rechargeable battery systems have a history of undetected cell internal 
defects. These defects may or may not be detected during normal 
operational evaluation, test, and validation. This may lead to an 
unsafe condition during in-service operation.
    5. Extreme Temperatures. Exposure to an extreme temperature 
environment has the potential to create major hazards. Care must be 
taken to ensure that the lithium battery remains within the 
manufacturer's recommended specification.

Applicability

    As discussed above, these special conditions are applicable to the 
Model P2012 airplane. Should Tecnam apply at a later date for a change 
to the type certificate to include another model incorporating the same 
novel or unusual design feature, the FAA would apply these special 
conditions to that model as well.

Conclusion

    This action affects only certain novel or unusual design features 
on the Model P2012 airplane. It is not a rule of general applicability.

List of Subjects in 14 CFR Part 23

    Aircraft, Aviation safety, Signs and symbols.

Citation

    The authority citation for these special conditions is as follows:

    Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704, 
Pub. L. 113-53, 127 Stat 584 (49 U.S.C. 44704) note

The Special Conditions

    Accordingly, pursuant to the authority delegated to me by the 
Administrator, the following special conditions are issued, in lieu of 
the requirements in Sec.  23.1353 (a), (b), (c), (d), and (e), 
amendment 23-62, as part of the type certification basis for the Tecnam 
Model P2012 airplane.

Installation of Lithium Battery

    Lithium battery installations must be designed and installed as 
follows:
    (1) Safe cell temperatures and pressures must be maintained 
during--
    i. Normal operations;
    ii. Any probable failure conditions of charging or discharging or 
battery monitoring system; and
    iii. Any failure of the charging or battery monitoring system shown 
to not be extremely remote.
    (2) The rechargeable lithium battery installation must be designed 
to preclude explosion and fire in the event of a failure under (1)(ii) 
and (1)(iii) above.
    (3) Design of the rechargeable lithium batteries must preclude the 
occurrence of self-sustaining, uncontrolled increases in temperature or 
pressure.
    (4) No explosive or toxic gasses emitted by any rechargeable 
lithium battery in normal operation or as the result of any failure of 
the battery charging system, monitoring system, or battery 
installation, which is shown to not be extremely remote, may accumulate 
in hazardous quantities within the airplane.
    (5) Installations of rechargeable lithium batteries must meet the 
requirements of Sec.  23.863(a) through (d), amendment 23-34.
    (6) No corrosive fluids or gases that may escape from any 
rechargeable lithium battery may damage surrounding structure or any 
adjacent systems, equipment, electrical wiring, or the airplane in such 
a way as to cause a major or more severe failure condition, in 
accordance with Sec.  23.1309, amendment 23-62.
    (7) Each rechargeable lithium battery installation must have 
provisions to prevent any hazardous effect on structure or essential 
systems that may be caused by the maximum amount of heat the battery 
can generate during a short circuit of the battery or of its individual 
cells.
    (8) Rechargeable lithium battery installations must have a system 
to automatically control the charging rate of the battery to prevent 
battery overheating and overcharging, and either:
    i. A battery temperature sensing and over-temperature warning 
system with a means for automatically disconnecting the battery from 
its charging source in the event of an over-temperature condition; or
    ii. A battery failure sensing and warning system with a means for 
automatically disconnecting the battery from its charging source in the 
event of battery failure.

[[Page 17736]]

    (9) Any rechargeable lithium battery installation, the function of 
which is required for safe operation of the aircraft, must incorporate 
a monitoring and warning feature that will provide an indication to the 
appropriate flight crewmembers whenever the state of charge of the 
batteries has fallen below levels considered acceptable for dispatch of 
the aircraft.

    Note 1 to paragraph (9): Reference Sec.  23.1353(h) for dispatch 
consideration.

    (10) The Instructions for Continued Airworthiness (ICA) required by 
Sec.  23.1529 must contain maintenance requirements to ensure that the 
battery has been sufficiently charged at appropriate intervals 
specified by the battery manufacturer and the equipment manufacturer 
that contain the rechargeable lithium battery or rechargeable lithium 
battery system. The lithium rechargeable batteries and lithium 
rechargeable battery systems must not degrade below specified ampere-
hour levels sufficient to power the aircraft system. The ICA must also 
contain procedures for the maintenance of replacement batteries to 
prevent the installation of batteries that have degraded charge 
retention ability or other damage due to prolonged storage at a low 
state of charge. Replacement batteries must be of the same manufacturer 
and part number as approved by the FAA.

    Note 2 to paragraph (10): Maintenance requirements include 
procedures that check battery capacity, charge degradation at 
manufacturer's recommended inspection intervals, and replace 
batteries at manufacturer's recommended replacement schedule/time to 
prevent age-related degradation.


    Note 3 to paragraph (10): The term ``sufficiently charged'' 
means that the battery must retain enough charge, expressed in 
ampere-hours, to ensure that the battery cells will not be damaged. 
A battery cell may be damaged by low charge (i.e., below certain 
level), resulting in a reduction in the ability to charge and retain 
a full charge. This reduction would be greater than the reduction 
that may result from normal operational degradation.


    Note 4 to paragraph (10): Replacement battery in spares storage 
may be subject to prolonged storage at a low state of charge.


    Issued in Kansas City, Missouri, on April 22, 2019.
William Schinstock,
Acting Manager, Small Airplane Standards Branch, Policy and Innovation 
Division, Aircraft Certification Service.
[FR Doc. 2019-08477 Filed 4-25-19; 8:45 am]
BILLING CODE 4910-13-P
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