Special Conditions: Dassault Falcon 2000 Series Airplanes; Aircell Airborne Satcom Equipment Consisting of a Wireless Handset and Associated Base Station, With Lithium Battery Installations, 70285-70287 [E8-27538]
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70285
Proposed Rules
Federal Register
Vol. 73, No. 225
Thursday, November 20, 2008
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
FOR FURTHER INFORMATION CONTACT:
DEPARTMENT OF TRANSPORTATION
Nazih Khaouly, FAA, 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:
Federal Aviation Administration
Comments Invited
14 CFR Part 25
[Docket No. NM395; Notice No. 25–08–07–
SC]
Special Conditions: Dassault Falcon
2000 Series Airplanes; Aircell Airborne
Satcom Equipment Consisting of a
Wireless Handset and Associated Base
Station, With Lithium Battery
Installations
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed special
conditions.
rwilkins on PROD1PC63 with PROPOSALS
AGENCY:
SUMMARY: This action proposes special
conditions for the Dassault Falcon 2000
series airplanes. These airplanes, as
modified by Aircell LLC, will have a
novel or unusual design feature
associated with the Aircell airborne
satcom equipment (ASE) which use
lithium battery technology. The
applicable airworthiness regulations do
not contain adequate or appropriate
safety standards for this design feature.
These proposed 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.
DATES: We must receive your comments
by January 5, 2009.
ADDRESSES: You must mail two copies
of your comments to: Federal Aviation
Administration, Transport Airplane
Directorate, Attention: Rules Docket
(ANM–113), Docket No. NM395, 1601
Lind Avenue, SW., Renton, Washington
98057–3356. You may deliver two
copies to the Transport Airplane
Directorate at the above address. You
must mark your comments: Docket No.
NM395. You can inspect comments in
the Rules Docket weekdays, except
federal holidays, between 7:30 a.m. and
4 p.m.
VerDate Aug<31>2005
18:25 Nov 19, 2008
Jkt 217001
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 ask that you send
us two copies of written comments.
We will file in the docket all
comments we receive as well as a report
summarizing each substantive public
contact with FAA personnel about these
special conditions. You can inspect the
docket before and after the comment
closing date. If you wish to review the
docket in person, go to the address in
the ADDRESSES section of this preamble
between 7:30 a.m. and 4 p.m., Monday
through Friday, except federal holidays.
We will consider all comments we
receive by 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.
If you want us to let you know we
received your comments on this
proposal, send us a pre-addressed,
stamped postcard on which the docket
number appears. We will stamp the date
on the postcard and mail it back to you.
Background
On March 15, 2007, Aircell LLC,
applied for a type design change to an
existing STC (ST01388WI–D), to install
additional equipment on Dassault
Falcon 2000 series airplanes. This
installation adds components to the
existing airplane installation to include
a low power Wi-Fi handset containing
a single cell lithium polymer
rechargeable battery. The battery
identified for application in this design
is a low capacity, single cell lithium
polymer rechargeable battery, with a
nominal capacity of 1400mAh and a
nominal voltage of 3.7V. The battery has
a weight of 26.5 grams. The battery has
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Sfmt 4702
been Underwriters Laboratories, Inc.
(UL) tested and qualified by DO–160E in
the Aircell handset (P12857). The
design is supported by a System Safety
Assessment/Functional Hazard
Assessment (SSA/FHA) analysis. The
Aircell Wi-Fi handset, which is a
component of the Aircell ASE, consists
of a wireless handset and associated
base station (cradle and charging unit),
both with protective circuits and fuse
devices which provide multiple levels
of redundant protection from hazards,
such as overcharging or discharging.
The lithium battery is installed in the
handset.
A lithium battery has certain failure,
operational, and maintenance
characteristics that differ significantly
from those of the nickel-cadmium and
lead-acid rechargeable batteries
currently approved for installation on
large transport category airplanes. The
FAA is proposing these special
conditions to require that (1) all
characteristics of the lithium batteries
and their installations that could affect
safe operation of the Dassault Falcon
2000 are addressed, and (2) appropriate
continued airworthiness instructions,
which include maintenance
requirements, are established to ensure
the availability of electrical power from
the batteries when needed.
At present, there is limited experience
with use of rechargeable lithium
batteries in applications involving
commercial aviation. However, other
users of this technology, ranging from
wireless telephone manufacturers to the
electric vehicle industry, have noted
safety problems with lithium batteries.
These problems include overcharging,
over-discharging, and flammability of
cell components.
1. Overcharging
In general, lithium batteries are
significantly more susceptible to
internal failures that can result in selfsustaining increases in temperature and
pressure (i.e., thermal runaway) than
their nickel-cadmium or lead-acid
counterparts. This is especially true for
overcharging that 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
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70286
Federal Register / Vol. 73, No. 225 / Thursday, November 20, 2008 / Proposed Rules
used as spares are maintained in an
appropriate state of charge.
increases with increasing battery
capacity due to the higher amount of
electrolyte in large batteries.
rwilkins on PROD1PC63 with PROPOSALS
2. Over-Discharging
Discharge of some types of lithium
batteries beyond a certain voltage
(typically 2.4 volts) 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 flightcrews as a
means of checking battery status—a
problem shared with nickel-cadmium
batteries.
3. Flammability of Cell Components
Unlike nickel-cadmium and lead-acid
batteries, some types of 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.
These problems experienced by users
of lithium batteries raise concern about
the use of these batteries in commercial
aviation. Accordingly, the proposed use
of lithium batteries in the Aircell ASE
on Dassault Falcon 2000 series aircraft
has prompted the FAA to review the
adequacy of existing regulations in Title
14 Code of Federal Regulations (14 CFR)
part 25. Our review indicates that the
existing regulations do not adequately
address several failure, operational, and
maintenance characteristics of lithium
batteries that could affect the safety and
reliability of lithium battery
installations.
The intent of these special conditions
is to establish appropriate airworthiness
standards for lithium batteries in
Dassault Falcon 2000 series aircraft,
modified Aircell LLC, and to ensure, as
required by § 25.601, that these battery
installations are not hazardous or
unreliable. Accordingly, these special
conditions include the following
requirements:
• Those provisions of § 25.1353
which are applicable to lithium
batteries.
• The flammable fluid fire protection
provisions of § 25.863.
In the past, this regulation was not
applied to batteries of transport category
airplanes, since the electrolytes used in
lead-acid and nickel-cadmium batteries
are not flammable.
• New requirements to address the
hazards of overcharging and overdischarging that are unique to lithium
batteries.
• New Instructions for Continuous
Airworthiness that include maintenance
requirements to ensure that batteries
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18:25 Nov 19, 2008
Jkt 217001
Type Certification Basis
Under the provisions of 14 CFR
21.101, Aircell LLC must show that the
Dassault Falcon 2000 series airplanes, as
changed, continue to meet the
applicable provisions of the regulations
incorporated by reference in Type
Certificate No. Type Certificate A50NM,
Revision 3, or the applicable regulations
in effect on the date of application for
the change. The regulations
incorporated by reference in the type
certificate are commonly referred to as
the ‘‘original type certification basis.’’
The certification basis for Dassault
Falcon 2000 is listed in Type Certificate
A50NM, Revision 3, dated September
21, 2004. In addition, the certification
basis includes certain special conditions
and exemptions that are not relevant to
these special conditions. Also, if the
regulations incorporated by reference do
not provide adequate standards with
respect to the change, the applicant
must comply with certain regulations in
effect on the date of application for the
change.
If the Administrator finds that the
applicable airworthiness regulations
(i.e., part 25, as amended) do not
contain adequate or appropriate safety
standards for Dassault Aviation Falcon
2000 series airplanes because of a novel
or unusual design feature, special
conditions are prescribed under the
provisions of 14 CFR 21.16.
In addition to the applicable
airworthiness regulations and special
conditions, the Dassault Falcon 2000
series airplanes 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, under § 11.38,
and they become part of the type
certification basis in accordance with
§ 21.101.
Special conditions are initially
applicable to the models for which they
are issued. Should Aircell LLC apply for
a supplemental type certificate to
modify any other model included on
Type Certificate No. A50NM to
incorporate the same or similar novel or
unusual design feature, these special
conditions would also apply to the other
model.
Novel or Unusual Design Features
The Dassault Aviation Falcon 2000
series airplanes, as modified by Aircell
LLC, to include the Aircell ASE which
will use lithium battery technology, will
incorporate a novel or unusual design
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Fmt 4702
Sfmt 4702
feature. Because of rapid improvements
in airplane technology, 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
of safety equivalent to that established
by the existing airworthiness standards.
The Aircell Access system will
include lithium battery installations.
The application of a rechargeable
lithium battery is a novel or unusual
design feature in transport category
airplanes. This type of battery has
certain failure, operational, and
maintenance characteristics that differ
significantly from those of the nickelcadmium and lead-acid rechargeable
batteries currently approved for
installation on large transport category
airplanes. The FAA issues these special
conditions to require that (1) all
characteristics of the lithium battery and
its installation that could affect safe
operation of the satellite communication
system are addressed, and (2)
appropriate maintenance requirements
are established to ensure that electrical
power is available from the batteries
when it is needed.
Applicability
As discussed above, these special
conditions are applicable to the Dassault
Aviation 2000 series airplanes as
modified by Aircell LLC. Should Aircell
LLC apply at a later date for a
supplemental type certificate to modify
any other model included on Type
Certificate No. A28NM to incorporate
the same novel or unusual design
feature, these special conditions would
apply to that model as well.
Conclusion
This action affects only certain novel
or unusual design features of the
Dassault Aviation 2000 series airplanes
as modified by Aircell LLC. It is not a
rule of general applicability and affects
only the applicant which applied to the
FAA for approval of these features 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:
Authority: 49 U.S.C. 106(g), 40113, 44701,
44702, 44704.
The Proposed Special Conditions
Accordingly, the Federal Aviation
Administration (FAA) proposes the
following special conditions as part of
the type certification basis for the
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rwilkins on PROD1PC63 with PROPOSALS
Federal Register / Vol. 73, No. 225 / Thursday, November 20, 2008 / Proposed Rules
Dassault Aviation 2000 series airplanes,
modified by Aircell LLC in lieu of the
requirements of § 25.1353(c)(1) through
(c)(4), Amendment 25–113.
Lithium batteries and battery
installations on Dassault Aviation 2000
series airplanes must be designed and
installed as follows:
1. Safe cell temperatures and
pressures must be maintained during
any foreseeable charging or discharging
condition and during any failure of the
charging or battery monitoring system
not shown to be extremely remote. The
lithium battery installation must
preclude explosion in the event of those
failures.
2. Design of the lithium batteries must
preclude the occurrence of selfsustaining, uncontrolled increases in
temperature or pressure.
3. No explosive or toxic gases emitted
by any lithium battery in normal
operation or as the result of any failure
of the battery charging system,
monitoring system, or battery
installation which is not shown to be
extremely remote may accumulate in
hazardous quantities within the
airplane.
4. Installations of lithium batteries
must meet the requirements of
§ 25.863(a) through (d).
5. No corrosive fluids or gases that
may escape from any lithium battery
may damage surrounding structure or
any adjacent systems, equipment, or
electrical wiring of the airplane in such
a way as to cause a major or more severe
failure condition, in accordance with
§ 25.1309(b) and applicable regulatory
guidance.
6. Each lithium battery installation
must have provisions to prevent any
hazardous effect on structure or
essential systems caused by the
maximum amount of heat the battery
can generate during a short circuit of the
battery or of its individual cells.
7. Lithium battery installations must
have a system to control the charging
rate of the battery automatically, so as
to prevent battery overheating or
overcharging, and,
(a) 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
(b) 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.
8. Any lithium battery installation
whose function is required for safe
operation of the airplane must
incorporate a monitoring and warning
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18:25 Nov 19, 2008
Jkt 217001
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 airplane.
9. The Instructions for Continued
Airworthiness required by § 25.1529
must contain maintenance requirements
to assure that the lithium battery is
sufficiently charged at appropriate
intervals specified by the battery
manufacturer. The Instructions for
Continued Airworthiness must also
contain procedures for the maintenance
of lithium batteries in spares storage to
prevent the replacement of batteries
whose function is required for safe
operation of the airplane with batteries
that have experienced degraded charge
retention ability or other damage due to
prolonged storage at a low state of
charge. Precautions should be included
in the Instructions for Continued
Airworthiness maintenance instructions
to prevent mishandling of the lithium
battery which could result in shortcircuit or other unintentional damage
that could result in personal injury or
property damage.
Note 1: The term ‘‘sufficiently charged’’
means that the battery will retain enough of
a charge, expressed in ampere-hours, to
ensure that the battery cells will not be
damaged. A battery cell may be damaged by
lowering the charge below a point where
there is 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 2: These special conditions are not
intended to replace § 25.1353(c), Amendment
25–113 in the certification basis of the Aircell
LLC supplemental type certificate. These
special conditions apply only to lithium
batteries and their installations. The
requirements of § 25.1353(c), Amendment
25–113 remain in effect for batteries and
battery installations on the Aircell LLC
supplemental type certificate that do not use
lithium batteries.
Compliance with the requirements of
these special conditions must be shown
by test or analysis, with the concurrence
of the Fort Worth Special Certification
Office.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–27538 Filed 11–19–08; 8:45 am]
BILLING CODE 4910–13–P
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70287
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2008–1102; Airspace
Docket No. 08–AGL–8]
Proposed Establishment of Class D
Airspace; Branson, MO
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking.
AGENCY:
SUMMARY: This action proposes to
establish Class D airspace at Branson
Airport, Branson, MO. The
establishment of an air traffic control
tower has made this action necessary for
the safety of Instrument Flight Rule
(IFR) operations at Branson Airport.
DATES: 0901 UTC. Comments must be
received on or before January 5, 2009.
ADDRESSES: Send comments on this
proposal to the U.S. Department of
Transportation, Docket Operations, 1200
New Jersey Avenue, SE., West Building
Ground Floor, Room W12–140,
Washington, DC 20590–0001. You must
identify the docket number FAA–2008–
1102/Airspace Docket No. 08–AGL–8, at
the beginning of your comments. You
may also submit comments through the
Internet at https://www.regulations.gov.
You may review the public docket
containing the proposal, any comments
received, and any final disposition in
person in the Dockets Office between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The
Docket Office (telephone 1–800–647–
5527) is on the ground floor of the
building at the above address.
FOR FURTHER INFORMATION CONTACT:
Scott Enander, Central Service Area,
Operations Support Group, Federal
Aviation Administration, Southwest
Region, 2601 Meacham Blvd., Fort
Worth, TX 76193–0530; telephone: (817)
222–5582.
SUPPLEMENTARY INFORMATION:
Comments Invited
Interested parties are invited to
participate in this proposed rulemaking
by submitting such written data, views,
or arguments, as they may desire.
Comments that provide the factual basis
supporting the views and suggestions
presented are particularly helpful in
developing reasoned regulatory
decisions on the proposal. Comments
are specifically invited on the overall
regulatory, aeronautical, economic,
environmental, and energy-related
aspects of the proposal.
Communications should identify both
E:\FR\FM\20NOP1.SGM
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Agencies
[Federal Register Volume 73, Number 225 (Thursday, November 20, 2008)]
[Proposed Rules]
[Pages 70285-70287]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-27538]
========================================================================
Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
========================================================================
Federal Register / Vol. 73, No. 225 / Thursday, November 20, 2008 /
Proposed Rules
[[Page 70285]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM395; Notice No. 25-08-07-SC]
Special Conditions: Dassault Falcon 2000 Series Airplanes;
Aircell Airborne Satcom Equipment Consisting of a Wireless Handset and
Associated Base Station, With Lithium Battery Installations
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed special conditions.
-----------------------------------------------------------------------
SUMMARY: This action proposes special conditions for the Dassault
Falcon 2000 series airplanes. These airplanes, as modified by Aircell
LLC, will have a novel or unusual design feature associated with the
Aircell airborne satcom equipment (ASE) which use lithium battery
technology. The applicable airworthiness regulations do not contain
adequate or appropriate safety standards for this design feature. These
proposed 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.
DATES: We must receive your comments by January 5, 2009.
ADDRESSES: You must mail two copies of your comments to: Federal
Aviation Administration, Transport Airplane Directorate, Attention:
Rules Docket (ANM-113), Docket No. NM395, 1601 Lind Avenue, SW.,
Renton, Washington 98057-3356. You may deliver two copies to the
Transport Airplane Directorate at the above address. You must mark your
comments: Docket No. NM395. You can inspect comments in the Rules
Docket weekdays, except federal holidays, between 7:30 a.m. and 4 p.m.
FOR FURTHER INFORMATION CONTACT: Nazih Khaouly, FAA, 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:
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 ask
that you send us two copies of written comments.
We will file in the docket all comments we receive as well as a
report summarizing each substantive public contact with FAA personnel
about these special conditions. You can inspect the docket before and
after the comment closing date. If you wish to review the docket in
person, go to the address in the ADDRESSES section of this preamble
between 7:30 a.m. and 4 p.m., Monday through Friday, except federal
holidays.
We will consider all comments we receive by 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.
If you want us to let you know we received your comments on this
proposal, send us a pre-addressed, stamped postcard on which the docket
number appears. We will stamp the date on the postcard and mail it back
to you.
Background
On March 15, 2007, Aircell LLC, applied for a type design change to
an existing STC (ST01388WI-D), to install additional equipment on
Dassault Falcon 2000 series airplanes. This installation adds
components to the existing airplane installation to include a low power
Wi-Fi handset containing a single cell lithium polymer rechargeable
battery. The battery identified for application in this design is a low
capacity, single cell lithium polymer rechargeable battery, with a
nominal capacity of 1400mAh and a nominal voltage of 3.7V. The battery
has a weight of 26.5 grams. The battery has been Underwriters
Laboratories, Inc. (UL) tested and qualified by DO-160E in the Aircell
handset (P12857). The design is supported by a System Safety
Assessment/Functional Hazard Assessment (SSA/FHA) analysis. The Aircell
Wi-Fi handset, which is a component of the Aircell ASE, consists of a
wireless handset and associated base station (cradle and charging
unit), both with protective circuits and fuse devices which provide
multiple levels of redundant protection from hazards, such as
overcharging or discharging. The lithium battery is installed in the
handset.
A lithium battery has certain failure, operational, and maintenance
characteristics that differ significantly from those of the nickel-
cadmium and lead-acid rechargeable batteries currently approved for
installation on large transport category airplanes. The FAA is
proposing these special conditions to require that (1) all
characteristics of the lithium batteries and their installations that
could affect safe operation of the Dassault Falcon 2000 are addressed,
and (2) appropriate continued airworthiness instructions, which include
maintenance requirements, are established to ensure the availability of
electrical power from the batteries when needed.
At present, there is limited experience with use of rechargeable
lithium batteries in applications involving commercial aviation.
However, other users of this technology, ranging from wireless
telephone manufacturers to the electric vehicle industry, have noted
safety problems with lithium batteries. These problems include
overcharging, over-discharging, and flammability of cell components.
1. Overcharging
In general, lithium 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. This is especially true for
overcharging that 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
[[Page 70286]]
increases with increasing battery capacity due to the higher amount of
electrolyte in large batteries.
2. Over-Discharging
Discharge of some types of lithium batteries beyond a certain
voltage (typically 2.4 volts) 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 flightcrews as a means of
checking battery status--a problem shared with nickel-cadmium
batteries.
3. Flammability of Cell Components
Unlike nickel-cadmium and lead-acid batteries, some types of
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.
These problems experienced by users of lithium batteries raise
concern about the use of these batteries in commercial aviation.
Accordingly, the proposed use of lithium batteries in the Aircell ASE
on Dassault Falcon 2000 series aircraft has prompted the FAA to review
the adequacy of existing regulations in Title 14 Code of Federal
Regulations (14 CFR) part 25. Our review indicates that the existing
regulations do not adequately address several failure, operational, and
maintenance characteristics of lithium batteries that could affect the
safety and reliability of lithium battery installations.
The intent of these special conditions is to establish appropriate
airworthiness standards for lithium batteries in Dassault Falcon 2000
series aircraft, modified Aircell LLC, and to ensure, as required by
Sec. 25.601, that these battery installations are not hazardous or
unreliable. Accordingly, these special conditions include the following
requirements:
Those provisions of Sec. 25.1353 which are applicable to
lithium batteries.
The flammable fluid fire protection provisions of Sec.
25.863.
In the past, this regulation was not applied to batteries of
transport category airplanes, since the electrolytes used in lead-acid
and nickel-cadmium batteries are not flammable.
New requirements to address the hazards of overcharging
and over-discharging that are unique to lithium batteries.
New Instructions for Continuous Airworthiness that include
maintenance requirements to ensure that batteries used as spares are
maintained in an appropriate state of charge.
Type Certification Basis
Under the provisions of 14 CFR 21.101, Aircell LLC must show that
the Dassault Falcon 2000 series airplanes, as changed, continue to meet
the applicable provisions of the regulations incorporated by reference
in Type Certificate No. Type Certificate A50NM, Revision 3, or the
applicable regulations in effect on the date of application for the
change. The regulations incorporated by reference in the type
certificate are commonly referred to as the ``original type
certification basis.''
The certification basis for Dassault Falcon 2000 is listed in Type
Certificate A50NM, Revision 3, dated September 21, 2004. In addition,
the certification basis includes certain special conditions and
exemptions that are not relevant to these special conditions. Also, if
the regulations incorporated by reference do not provide adequate
standards with respect to the change, the applicant must comply with
certain regulations in effect on the date of application for the
change.
If the Administrator finds that the applicable airworthiness
regulations (i.e., part 25, as amended) do not contain adequate or
appropriate safety standards for Dassault Aviation Falcon 2000 series
airplanes because of a novel or unusual design feature, special
conditions are prescribed under the provisions of 14 CFR 21.16.
In addition to the applicable airworthiness regulations and special
conditions, the Dassault Falcon 2000 series airplanes 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,
under Sec. 11.38, and they become part of the type certification basis
in accordance with Sec. 21.101.
Special conditions are initially applicable to the models for which
they are issued. Should Aircell LLC apply for a supplemental type
certificate to modify any other model included on Type Certificate No.
A50NM to incorporate the same or similar novel or unusual design
feature, these special conditions would also apply to the other model.
Novel or Unusual Design Features
The Dassault Aviation Falcon 2000 series airplanes, as modified by
Aircell LLC, to include the Aircell ASE which will use lithium battery
technology, will incorporate a novel or unusual design feature. Because
of rapid improvements in airplane technology, 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 of safety equivalent to that established by the
existing airworthiness standards.
The Aircell Access system will include lithium battery
installations. The application of a rechargeable lithium battery is a
novel or unusual design feature in transport category airplanes. This
type of battery has certain failure, operational, and maintenance
characteristics that differ significantly from those of the nickel-
cadmium and lead-acid rechargeable batteries currently approved for
installation on large transport category airplanes. The FAA issues
these special conditions to require that (1) all characteristics of the
lithium battery and its installation that could affect safe operation
of the satellite communication system are addressed, and (2)
appropriate maintenance requirements are established to ensure that
electrical power is available from the batteries when it is needed.
Applicability
As discussed above, these special conditions are applicable to the
Dassault Aviation 2000 series airplanes as modified by Aircell LLC.
Should Aircell LLC apply at a later date for a supplemental type
certificate to modify any other model included on Type Certificate No.
A28NM to incorporate the same novel or unusual design feature, these
special conditions would apply to that model as well.
Conclusion
This action affects only certain novel or unusual design features
of the Dassault Aviation 2000 series airplanes as modified by Aircell
LLC. It is not a rule of general applicability and affects only the
applicant which applied to the FAA for approval of these features 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:
Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.
The Proposed Special Conditions
Accordingly, the Federal Aviation Administration (FAA) proposes the
following special conditions as part of the type certification basis
for the
[[Page 70287]]
Dassault Aviation 2000 series airplanes, modified by Aircell LLC in
lieu of the requirements of Sec. 25.1353(c)(1) through (c)(4),
Amendment 25-113.
Lithium batteries and battery installations on Dassault Aviation
2000 series airplanes must be designed and installed as follows:
1. Safe cell temperatures and pressures must be maintained during
any foreseeable charging or discharging condition and during any
failure of the charging or battery monitoring system not shown to be
extremely remote. The lithium battery installation must preclude
explosion in the event of those failures.
2. Design of the lithium batteries must preclude the occurrence of
self-sustaining, uncontrolled increases in temperature or pressure.
3. No explosive or toxic gases emitted by any lithium battery in
normal operation or as the result of any failure of the battery
charging system, monitoring system, or battery installation which is
not shown to be extremely remote may accumulate in hazardous quantities
within the airplane.
4. Installations of lithium batteries must meet the requirements of
Sec. 25.863(a) through (d).
5. No corrosive fluids or gases that may escape from any lithium
battery may damage surrounding structure or any adjacent systems,
equipment, or electrical wiring of the airplane in such a way as to
cause a major or more severe failure condition, in accordance with
Sec. 25.1309(b) and applicable regulatory guidance.
6. Each lithium battery installation must have provisions to
prevent any hazardous effect on structure or essential systems caused
by the maximum amount of heat the battery can generate during a short
circuit of the battery or of its individual cells.
7. Lithium battery installations must have a system to control the
charging rate of the battery automatically, so as to prevent battery
overheating or overcharging, and,
(a) 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
(b) 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.
8. Any lithium battery installation whose function is required for
safe operation of the airplane 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 airplane.
9. The Instructions for Continued Airworthiness required by Sec.
25.1529 must contain maintenance requirements to assure that the
lithium battery is sufficiently charged at appropriate intervals
specified by the battery manufacturer. The Instructions for Continued
Airworthiness must also contain procedures for the maintenance of
lithium batteries in spares storage to prevent the replacement of
batteries whose function is required for safe operation of the airplane
with batteries that have experienced degraded charge retention ability
or other damage due to prolonged storage at a low state of charge.
Precautions should be included in the Instructions for Continued
Airworthiness maintenance instructions to prevent mishandling of the
lithium battery which could result in short-circuit or other
unintentional damage that could result in personal injury or property
damage.
Note 1: The term ``sufficiently charged'' means that the battery
will retain enough of a charge, expressed in ampere-hours, to ensure
that the battery cells will not be damaged. A battery cell may be
damaged by lowering the charge below a point where there is 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 2: These special conditions are not intended to replace
Sec. 25.1353(c), Amendment 25-113 in the certification basis of the
Aircell LLC supplemental type certificate. These special conditions
apply only to lithium batteries and their installations. The
requirements of Sec. 25.1353(c), Amendment 25-113 remain in effect
for batteries and battery installations on the Aircell LLC
supplemental type certificate that do not use lithium batteries.
Compliance with the requirements of these special conditions must
be shown by test or analysis, with the concurrence of the Fort Worth
Special Certification Office.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-27538 Filed 11-19-08; 8:45 am]
BILLING CODE 4910-13-P