Special Conditions: Boeing Model 787-8 Airplane; Overhead Crew Rest Compartment, 75-81 [E9-31117]
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75
Proposed Rules
Federal Register
Vol. 75, No. 1
Monday, January 4, 2010
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.
Staff, Transport Airplane Directorate,
Aircraft Certification Service, 1601 Lind
Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2136;
facsimile (425) 227–1320.
SUPPLEMENTARY INFORMATION:
Comments Invited
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM412 Special Conditions No.
25–09–08–SC]
Special Conditions: Boeing Model 787–
8 Airplane; Overhead Crew Rest
Compartment
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AGENCY: Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed special
conditions.
SUMMARY: This action proposes special
conditions for the Boeing Model 787–8
airplane. This airplane will have novel
or unusual design features associated
with installation of an overhead crew
rest compartment. 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. Additional
special conditions will be issued for
other novel or unusual design features
of the Boeing Model 787–8 airplanes.
DATES: We must receive your comments
by February 18, 2010.
ADDRESSES: You must mail two copies
of your comments to: Federal Aviation
Administration, Transport Airplane
Directorate, Attn: Rules Docket (ANM–
113), Docket No. NM412, 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.
NM412. 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: Jeff
Gardlin, FAA, Airframe/Cabin Safety
Branch, ANM–115, Transport Standards
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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
concerning 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 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.
If you want us to acknowledge receipt
of your comments on this proposal,
include with your comments a selfaddressed, stamped postcard on which
you have written the docket number.
We will stamp the date on the postcard
and mail it back to you.
Background
On March 28, 2003, The Boeing
Commercial Airplane Group (hereafter
referred to as ‘‘Boeing’’) applied for an
FAA type certificate for its new Boeing
Model 787–8 passenger airplane. The
company applied for an extension of
time for the type certificate on March 9,
2009, and was granted that extension on
March 13, 2009. The Boeing Model 787–
8 airplane will be an all-new, twoengine jet transport airplane with a twoaisle cabin. The maximum takeoff
weight will be 476,000 pounds, with a
maximum passenger count of 381
passengers.
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Type Certification Basis
Under provisions of Title 14 Code of
Federal Regulations (14 CFR) 21.17,
Boeing must show that the Boeing
Model 787–8 airplane (hereafter referred
to as ‘‘the 787’’) meets the applicable
provisions of 14 CFR part 25, as
amended by Amendments 25–1 through
25–117, 25–120, 25–124, 25–125 and
25–128, except that § 25.1309 remains at
Amendment 25–117 for cargo fire
protection systems. 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 787 because of a novel
or unusual design feature, special
conditions are prescribed under the
provisions of § 21.16.
In addition to complying with the
applicable airworthiness regulations
and special conditions, the 787 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. In
addition, the FAA must issue a finding
of regulatory adequacy pursuant to
section 611 of Public Law 92–574, the
‘‘Noise Control Act of 1972.’’
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
§ 21.17(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 features, the special conditions
would also apply to the other model
under provisions of § 21.101.
Novel or Unusual Design Features
Crew rest compartments have been
installed and certificated on several
Boeing airplane models in locations as
varied as the main passenger seating
area, the overhead space above the main
passenger cabin seating area, and below
the passenger cabin seating area within
the cargo compartment. In each case, the
Administrator has determined that the
applicable regulations (i.e., 14 CFR part
25) did not provide all of the necessary
requirements because each installation
had unique features by virtue of its
design, location, and use on the
airplane. When the Administrator finds
that the applicable airworthiness
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regulations do not contain adequate or
appropriate safety standards because of
a novel or unusual design feature,
special conditions are prescribed under
the provisions of § 21.16. The special
conditions contain safety standards that
the Administrator considers necessary
to establish a level of safety equivalent
to that established by the existing
airworthiness standards.
Most recently, for the Boeing Model
777 series airplanes, the FAA has issued
Special Conditions No. 25–230–SC,
dated April 9, 2003, for overhead crew
rest (OCR) compartments allowed to be
occupied during flight, and Special
Conditions No. 25–260–SC, dated April
14, 2004, for overhead flight crew rest
(OFCR) compartments allowed to be
occupied during taxi, takeoff, and
landing (TT&L), as well as during flight.
The OCR compartment on the 787
identified by Boeing as an overhead
flight attendant rest is located above the
main passenger cabin, adjacent to Door
4, and will be accessed from the main
deck by stairs through a vestibule. This
OCR compartment will contain six
private berths, an emergency hatch that
opens directly into the main passenger
cabin area, a smoke detection system, an
oxygen system, and various occupant
amenities. This OCR compartment will
only be occupied by trained crew
members in flight. It will not be
occupied during taxi, takeoff, or
landing.
This 787 OCR compartment is unique
to part 25 because of its design, location,
and use on the airplane. Because of the
novel or unusual features associated
with installation of this compartment,
special conditions are considered
necessary to provide a level of safety
equal to that established by the
airworthiness regulations.
Certification engineers evaluate such
an installation with respect to the
interior and assess it in accordance with
the certification basis of the airplane.
However, part 25 does not provide all of
the requirements for crew rest
compartments within the overhead area
of the passenger compartment. These
proposed special conditions do not
negate the need to address other
applicable part 25 regulations.
Operational Evaluations and Approval
These proposed special conditions
outline requirements for OCR
compartment design approvals
administered by the FAA’s Aircraft
Certification Service. Prior to
operational use of an OCR compartment,
the FAA’s Flight Standards Service
must evaluate and approve the ‘‘basic
suitability’’ of the compartment for crew
occupation. Additionally, if an operator
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wishes to use an OCR compartment as
‘‘sleeping quarters,’’ the compartment
must undergo an additional evaluation
and approval (reference 14 CFR
121.485(a), 121.523(b), and
135.269(b)(5)). Compliance with these
proposed special conditions does not
ensure that the applicant has
demonstrated compliance with the
requirements of parts 121 or 135.
To obtain an operational evaluation,
the type certificate holder must contact
the appropriate aircraft evaluation group
(AEG) in the Flight Standards Service
and request a ‘‘basic suitability’’
evaluation or a ‘‘sleeping quarters’’
evaluation of its OCR compartment. The
results of these evaluations should be
documented in a 787 flight
standardization board (FSB) report
appendix. Individual operators may
reference these standardized evaluations
in discussions with their FAA principal
operating inspector (POI) as the basis for
an operational approval, in lieu of an
on-site operational evaluation.
Any changes to the approved OCR
compartment configuration that affect
crewmember emergency egress or any
other procedures affecting safety of the
occupying crewmembers or related
emergency training will require reevaluation and approval. The applicant
for an OCR compartment design change
that affects egress, safety procedures, or
training is responsible for notifying the
FAA’s AEG that a new compartment
evaluation is required. The results of a
re-evaluation should also be
documented in a 787 FSB report
appendix.
Procedures must be developed to
ensure that a crewmember entering the
OCR compartment through the stairway/
vestibule to fight a fire will examine the
stairway/vestibule and the adjacent
galley or lavatory areas (if installed) for
the source of the fire before entering the
remaining areas of the compartment.
This is intended to ensure that the
source of the fire is not between the
crewmember and the entrance to the
OCR compartment. If a fire source is not
immediately evident to the firefighter,
the firefighter should check for potential
fire sources at areas closest to the OCR
compartment entrance first, then
proceed to check areas in such a manner
that the fire source, when found, will
not be between the firefighter and his or
her way to get out of the compartment.
Procedures describing methods for
searching the OCR compartment for fire
source(s) must be transmitted to
operators for incorporation into their
training programs and appropriate
operational manuals.
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Discussion of Proposed Special
Conditions
These proposed special conditions
would initially apply to an OCR
compartment installed adjacent to the
Door 4 exits on the 787. These proposed
special conditions would supplement
14 CFR part 25. Except as noted below,
these proposed special conditions for
the 787 closely resemble Boeing 777
Special Conditions No. 25–230–SC.
Proposed Special Conditions No. 4
and 14 contain requirements for the exit
signs that must be provided in the OCR
compartment. Symbols that satisfy the
equivalent level of safety finding
established for the 787 may be used in
lieu of the text required by
§ 25.812(b)(1)(i). The FAA expects that
crewmembers will learn the meaning of
any symbolic exit sign as a part of their
training in evacuation procedures.
Proposed Special Condition No. 13
contains requirements for supplemental
oxygen systems. Special Conditions No.
25–260–SC, for the overhead flightcrew
rest compartments, required that each
berth be provided with two oxygen
masks. This was intended to address the
case where a person not in a berth was
moving around in the crew rest
compartment and needed quick access
to the oxygen. For the designs used in
the model 777, this requirement was
sufficient. However, for the 787, the
requirement to have two masks per
berth may not always meet the objective
of having masks available to persons
who are in transition within the
compartment. Therefore, the wording of
this proposed special condition has
been modified to better state the
objective rather than specify that two
masks be provided per berth. In
addition, the requirement to have
adequate illumination to retrieve the
mask, while implied previously, is
made explicit in this proposal.
Proposed Special Condition No. 17
contains the requirement for materials
used in the construction of the OCR
compartment and states that § 25.853 as
amended by Amendment 25–116 is the
appropriate regulation. Amendment 25–
116 is the latest amendment level for
§ 25.853.
Compliance with these proposed
special conditions does not relieve the
applicant from the existing airplane
certification basis requirements. One
particular area of concern is that the
installation of OCR compartments
leaves a smaller compartment volume
within the overhead area of the airplane.
The applicant must comply with the
pressurized compartment loads
requirements of § 25.365(e), (f), and (g)
for the OCR compartment, as well as for
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any other airplane compartments whose
decompression characteristics are
affected by the installation of an OCR
compartment. Compliance with § 25.813
emergency exit access requirements
must be demonstrated for all phases of
flight during which occupants will be
present.
Section 25.813(e) prohibits
installation of interior doors between
passenger compartments, but the FAA
has historically found crew rest doors to
be acceptable, because crew rests are not
passenger compartments. Proposed
Special Conditions No. 1 and 14 provide
requirements for crew rest doors which
are considered to provide an
appropriate level of safety to OCR
compartment occupants.
Sections 25.1443, 25.1445, and
25.1447 contain oxygen requirements
for flight crew, passengers, and cabin
attendants. Crewmembers occupying the
OCR compartment are not on duty, and
therefore are considered passengers in
determining compliance with these
oxygen regulations.
Applicability
As discussed above, these proposed
special conditions are applicable to the
787. Should Boeing apply at a later date
for a change to the type certificate to
include another model incorporating the
same novel or unusual design features,
these proposed special conditions
would apply to that model as well.
Conclusion
This action affects only certain novel
or unusual design features of the 787. It
is not a rule of general applicability.
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.
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The Proposed Special Conditions
Accordingly, the Federal Aviation
Administration (FAA) proposes the
following special conditions as part of
the type certification basis for the
Boeing Model 787–8 airplanes with an
overhead crew rest (OCR) compartment
installed above the main passenger
cabin adjacent to an exit door.
1. Occupancy of the OCR
compartment is limited to the total
number of installed bunks and seats in
each compartment. There must be an
approved seat or berth able to withstand
the maximum flight loads when
occupied for each occupant permitted in
the OCR compartment. Maximum
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occupancy in the OCR compartment is
six.
(a) There must be appropriate
placards, inside and outside each
entrance to the OCR compartment, to
indicate:
(1) The maximum number of
occupants allowed.
(2) That occupancy is restricted to
crewmembers who are trained in the
evacuation procedures for the OCR
compartment.
(3) That occupancy is prohibited
during taxi, take-off, and landing.
(4) That smoking is prohibited in the
OCR compartment.
(5) That stowage in the OCR
compartment area is limited to crew
personal luggage. The stowage of cargo
or passenger baggage is not allowed.
(b) There must be at least one ashtray
on the inside and one ashtray on the
outside of any entrance to the overhead
crew rest compartment.
(c) For times when there is no flight
attendant present in the area around the
door to the OCR compartment, and also
in the event of an emergency, there must
be a means to prevent passengers from
entering the OCR compartment.
(d) There must be a means for any
door installed between the OCR
compartment and the passenger cabin to
be quickly opened from inside the
compartment, even when crowding
occurs at each side of the door.
(e) For all doors installed, there must
be a means to preclude anyone from
being trapped inside the OCR
compartment. If a locking mechanism is
installed, it must be capable of being
unlocked from the outside without the
aid of special tools. The lock must not
prevent opening from the inside of the
compartment at any time.
(f) The means of opening doors and
hatches to the OCR compartment must
be simple and obvious. In addition,
doors or hatches that separate the
overhead crew rest compartment from
the main deck must not adversely affect
evacuation of occupants on the main
deck (slowing evacuation by
encroaching into aisles, for example) or
cause injury to those occupants during
opening or while opened.
2. There must be at least two
emergency evacuation routes which
could be used by each occupant of the
OCR compartment to rapidly evacuate
to the main cabin. These evacuation
routes must be able to be closed from
the main passenger cabin after
evacuation. In addition—
(a) The routes must be located with
sufficient separation within the OCR
compartment to minimize the
possibility of an event either inside or
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outside of the crew rest compartment
rendering both routes inoperative.
Compliance with requirements of
Proposed Special Condition No. 2(a)
may be shown by inspection or by
analysis. Regardless of which method is
used, the maximum acceptable distance
between crew rest compartment outlets
is 60 feet.
Compliance by Inspection
Inspection may be used to show
compliance with proposed Special
Condition No. 2(a). An inspection
finding that an OCR compartment has
evacuation routes located so that each
occupant of the seats and berths has an
unobstructed route to at least one of the
crew rest compartment outlets,
regardless of the location of a fire,
would be reason for a finding of
compliance. A fire within a berth that
only blocks the occupant of that berth
from exiting the berth need not be
considered. Therefore, crew rest
compartment outlets that are located at
absolute opposite ends (i.e., adjacent to
opposite end walls) of the OCR
compartment would require no further
review or analysis with regard to exit
separation.
Compliance by Analysis
Analysis must show that the OCR
compartment configuration and interior
features allow all occupants of the OCR
compartment to escape the
compartment in the event of a hazard
inside or outside of the compartment.
Elements to consider in this
evaluation are as follows:
(1) Fire inside or outside the OCR
compartment, considered separately,
and the design elements used to reduce
the available fuel for the fire.
(2) Design elements used to reduce
fire ignition sources in the OCR
compartment.
(3) Distribution and quantity of
emergency equipment within the OCR
compartment.
(4) Structural failure or deformation of
components that could block access to
the available evacuation routes (e.g.,
seats, folding berths, contents of
stowage compartments, etc.).
(5) An incapacitated person blocking
the evacuation routes.
(6) Any other foreseeable hazard not
identified above that could cause the
evacuation routes to be compromised.
Analysis must consider design
features affecting access to the
evacuation routes. Possibilities for
design components affecting evacuation
that should be considered include, but
are not limited to, seat back break over,
rigid structure that reduces access from
one part of the compartment to another,
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and items known to be the cause of
potential hazards. Factors that also
should be considered are availability of
emergency equipment to address fire
hazards, availability of communications
equipment, supplemental restraint
devices to retain items of mass that, if
broken loose, could hinder evacuation,
and load path isolation between
components containing evacuation
routes.
Analysis of fire threats should be used
in determining placement of required
fire extinguishers and protective
breathing equipment (PBE). This
analysis should consider the possibility
of fire in any location in the OCR
compartment. The location and quantity
of PBE equipment and fire extinguishers
should allow occupants located in any
approved seats or berths access to the
equipment necessary to fight a fire in
the OCR compartment.
The intent of this proposed special
condition is to provide sufficient exit
route separation. Therefore the exit
separation analysis described above
should not be used to approve crew rest
compartment outlets that have less
physical separation (measured between
the centroid of each exit opening) than
the minimums prescribed below, unless
compensating features are identified
and submitted to the FAA for evaluation
and approval.
For OCR compartments with one
outlet located near the forward or aft
end of the compartment (as measured by
having the centroid of the exit opening
within 20 percent of the forward or aft
end of the total overhead crew rest
compartment length) the outlet
separation from one outlet to the other
should not be less than 50 percent of the
total OCR compartment length.
For OCR compartments with neither
required crew rest compartment outlet
located near the forward or aft end of
the compartment (as measured by not
having the centroid of either outlet
opening within 20 percent of the
forward or aft end of the total OCR
compartment length) the outlet
separation from one outlet to the other
should not be less than 30 percent of the
total OCR compartment length.
(b) The routes must be designed to
minimize the possibility of blockage,
which might result from fire,
mechanical or structural failure, or
persons standing below or against the
crew rest compartment outlets. One of
the two OCR evacuation routes should
not be located where, during times
when occupancy is allowed, normal
movement by passengers occurs (i.e.,
main aisle, cross aisle or galley
complex, for example) that would
impede egress from the OCR
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compartment. If an evacuation route is
in an area where normal movement of
passengers occurs, it must be
demonstrated that passengers would not
impede egress to the main deck. If there
is low headroom at or near the
evacuation route, provisions must be
made to prevent or to protect occupants
of the OCR compartment from head
injury. Use of evacuation routes must
not be dependent on any powered
device. If a crew rest compartment
outlet is over an area where there are
passenger seats, a maximum of five
passengers may be displaced from their
seats temporarily during the process of
evacuating an incapacitated person(s). If
such an evacuation procedure involves
the evacuee stepping on seats, the seats
must not be damaged to the extent that
they would not be acceptable for
occupancy during an emergency
landing.
(c) Emergency evacuation procedures,
including procedures for emergency
evacuation of an incapacitated occupant
from the OCR compartment, must be
established. The applicant must
transmit all of these procedures to the
operator for incorporation into its
training programs and appropriate
operational manuals.
(d) There must be a limitation in the
airplane flight manual or other suitable
means to require that crewmembers be
trained in use of the OCR evacuation
routes.
3. There must be a means of
evacuating an incapacitated person
(representative of a ninety-fifth
percentile male) from the OCR
compartment to the passenger cabin
floor.
(a) Such an evacuation must be
demonstrated for all evacuation routes.
A crewmember (a total of one assistant
within the OCR compartment) may
provide assistance in the evacuation.
Additional assistance may be provided
by up to three persons in the main
passenger compartment. These
additional assistants must be standing
on the floor while providing assistance.
For evacuation routes with stairways,
the additional assistants may ascend up
to one half the elevation change from
the main deck to the OCR compartment,
or to the first landing, whichever is
lower.
4. The following signs and placards
must be provided in the OCR
compartment, and they must meet the
following criteria:
(a) At least one exit sign, located near
each exit, meeting the emergency
lighting requirements of
§ 25.812(b)(1)(i). One allowable
exception would be a sign with reduced
background area of no less than 5.3
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square inches (excluding the letters),
provided that it is installed so that the
material surrounding the exit sign is
light in color (e.g., white, cream, light
beige, for example). If the material
surrounding the exit sign is not light in
color, a sign with a minimum of a oneinch-wide background border around
the letters would also be acceptable.
Another allowable exception is a sign
with a symbol that the FAA has
determined to be equivalent for use as
an exit sign in an OCR compartment.
(b) An appropriate placard located
near each exit defining the location of
and operating instructions for each
evacuation route.
(c) Placards must be readable from a
distance of 30 inches under emergency
lighting conditions.
(d) The exit handles and evacuation
path operating instruction placards
must be illuminated to at least 160
microlamberts under emergency lighting
conditions.
5. There must be a means in the event
of failure of the aircraft’s main power
system, or of the normal OCR
compartment lighting system, for
emergency illumination to be
automatically provided for the OCR
compartment.
(a) This emergency illumination must
be independent of the main lighting
system.
(b) The sources of general cabin
illumination may be common to both
the emergency and the main lighting
systems if the power supply to the
emergency lighting system is
independent of the power supply to the
main lighting system.
(c) The illumination level must be
sufficient to allow occupants of the OCR
compartment to locate and move to the
main passenger cabin floor by means of
each evacuation route.
(d) The illumination level must be
sufficient, with the privacy curtains in
the closed position, for each occupant of
the crew rest compartment to locate a
deployed oxygen mask.
6. There must be means for two-way
voice communications between
crewmembers on the flight deck and
occupants of the OCR compartment.
There must also be two-way
communications between occupants of
the OCR compartment and each flight
attendant station in the passenger cabin
required per § 25.1423(g) to have a
public address system microphone . In
addition, the public address system
must include provisions to provide only
the relevant information to the
crewmembers in the OCR compartment
(for example fire in flight, aircraft
depressurization, preparation of the
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compartment occupants for landing,
etc.).
7. There must be a means for manual
activation of an aural emergency alarm
system, audible during normal and
emergency conditions, to enable
crewmembers on the flight deck and at
each pair of required floor level
emergency exits to alert occupants of
the overhead crew rest OCR
compartment of an emergency situation.
Use of a public address or crew
interphone system will be acceptable,
provided an adequate means of
differentiating between normal and
emergency communications is
incorporated. The system must be
powered in flight, after the shutdown or
failure of all engines and auxiliary
power units, for a period of at least ten
minutes.
8. There must be a means, readily
detectable by seated or standing
occupants of the OCR compartment, to
indicate when seat belts should be
fastened. If there are no seats in the OCR
compartment, at least one means must
be provided to cover anticipated
turbulence (e.g., sufficient handholds).
Seat belt type restraints must be
provided for berths and must be
compatible for the sleeping attitude
during cruise conditions. There must be
a placard on each berth requiring that
seat belts be fastened when occupied. If
compliance with any of the other
requirements of these proposed special
conditions is predicated on specific
head location, there must be a placard
identifying that head position.
9. In lieu of the requirements
specified in § 25.1439(a) pertaining to
isolated compartments, and to provide a
level of safety equivalent to that
provided to occupants of an isolated
galley, the following equipment must be
provided in the OCR compartment:
(a) At least one approved hand-held
fire extinguisher appropriate for the
kinds of fires likely to occur.
(b) Two PBE devices suitable for
firefighting, or one PBE for each handheld fire extinguisher, whichever is
greater. All PBE devices must be
approved to Technical Standard Order
(TSO)–C116 or equivalent.
(c) One flashlight.
Note: Additional PBE devices and fire
extinguishers in specific locations, beyond
the minimum numbers prescribed in
Proposed Special Condition No. 9, may be
required as a result of the egress analysis
accomplished to satisfy Proposed Special
Condition No. 2(a).
10. A smoke or fire detection system
(or systems) must be provided that
monitors each occupiable area within
the OCR compartment, including those
areas partitioned by curtains or doors.
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Flight tests must be conducted to show
compliance with this requirement. If a
fire occurs, each system (or systems)
must provide:
(a) A visual indication to the
flightdeck within one minute after the
start of a fire.
(b) An aural warning in the OCR
compartment.
(c) A warning in the main passenger
cabin. This warning must be readily
detectable by a flight attendant, taking
into consideration the positioning of
flight attendants throughout the main
passenger compartment during various
phases of flight.
11. The OCR compartment must be
designed so that fires within the
compartment can be controlled without
a crewmember having to enter the
compartment, or the design of the access
provisions must allow crewmembers
equipped for firefighting to have
unrestricted access to the compartment.
The time for a crewmember on the main
deck to react to the fire alarm, don the
firefighting equipment, and gain access
to the OCR compartment must not
exceed the time it takes for the
compartment to become filled with
smoke, making it difficult to locate the
fire source. Approved procedures
describing methods for searching the
OCR for fire sources(s) must be
established. These procedures must be
transmitted to the operator for
incorporation into its training programs
and appropriate operational manuals.
12. There must be a means provided
to exclude hazardous quantities of
smoke or extinguishing agent
originating in the OCR compartment
from entering any other compartment
occupied by crewmembers or
passengers. The effectiveness of this
means must include the time periods
during evacuation of the OCR
compartment and, if applicable, the
time during which crewmembers are
accessing the OCR compartment to
manually fight a fire. Smoke entering
any other compartment occupied by
crewmembers or passengers when the
access to the OCR compartment is
opened, during an emergency
evacuation, must dissipate within five
minutes after the access to the OCR
compartment is closed.
(a) Hazardous quantities of smoke
may not enter any other compartment
occupied by crewmembers or
passengers during access to the OCR
compartment to manually fight a fire.
The amount of smoke entrained by a
firefighter exiting the OCR compartment
through the access is not considered
hazardous. During the one-minute
smoke detection time, penetration of a
small quantity of smoke from the OCR
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79
compartment into an occupied area is
acceptable. Flight tests must be
conducted to show compliance with
this requirement.
(b) There must be a provision in the
firefighting procedures to ensure that all
door(s) and hatch(es) at the crew rest
compartment outlets are closed after
evacuation of the compartment and
during firefighting to minimize smoke
and extinguishing agent entering other
occupiable compartments.
(c) If a built-in fire extinguishing
system is to be used instead of manual
firefighting, the fire extinguishing
system must be designed so that no
hazardous quantities of extinguishing
agent will enter other compartments
occupied by passengers or crew. The
system must have adequate capacity to
suppress a fire considering the fire
threat, the volume of the compartment,
and the ventilation rate.
(1) The system must have sufficient
extinguishing agent to provide an initial
knockdown and suppression
environment per the minimum
performance standards that have been
established for the agent being used. In
addition, certification flight testing will
verify the acceptable duration that the
suppression environment can be
maintained.
(2) If the capacity of the extinguishing
system does not provide effective fire
suppression that will last for the
duration of flight from the farthest point
in route to the nearest suitable landing
site expected in service, an additional
manual firefighting procedure must be
established. For the built-in
extinguishing system, the time duration
for effective fire suppression must be
established and documented in the
firefighting procedures in the airplane
flight manual. If the duration of time for
demonstrated effective fire suppression
provided by the built-in extinguishing
agent will be exceeded, the firefighting
procedures must instruct the crew to:
(i) Enter the OCR compartment at the
time that demonstrated fire suppression
effectiveness will be exceeded.
(ii) Check for and extinguish any
residual fire.
(iii) Confirm that the fire is out.
(b) For a manual hand-held bottle
extinguishing system (designed as the
sole means to fight a fire or to
supplement a built-in extinguishing
system of limited suppression duration)
for the OCR:
(1) There must be a limitation in the
airplane flight manual or other suitable
means requiring that crewmembers be
trained in the firefighting procedures.
(2) The compartment design must
allow crewmembers equipped for
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firefighting to have unrestricted access
to all parts of the compartment.
(3) The time for a crewmember on the
main deck to react to the fire alarm, don
the firefighting equipment, and gain
access to the OCR compartment must
not exceed the time it would take for the
compartment to become filled with
smoke, thus making it difficult to locate
the fire source.
13. There must be a supplemental
oxygen system within the crew rest
compartment as follows:
(a) There must be at least one mask for
each seat and berth in the crew rest
compartment.
(b) If a destination area (such as a
changing area) is provided in the OCR
compartment, there must be an oxygen
mask readily available for each
occupant who can reasonably be
expected to be in the destination area
(with the maximum number of required
masks within the destination area being
limited to the placarded maximum
occupancy of the crew rest).
(c) There must also be an oxygen
mask readily accessible to each
occupant who can reasonably be
expected to be moving from the main
cabin into the OCR compartment,
moving around within the OCR
compartment, or moving from the OCR
compartment to the main cabin.
(d) The system must provide an aural
and visual alert to warn occupants of
the OCR compartment to don oxygen
masks in the event of decompression.
The aural and visual alerts must activate
concurrently with deployment of the
oxygen masks in the passenger cabin. To
compensate for sleeping occupants, the
aural alert must be heard in each section
of the OCR compartment and must
sound continuously for a minimum of
five minutes or until a reset switch
within the OCR compartment is
activated. A visual alert that informs
occupants that they must don an oxygen
mask must be visible in each section.
(e) There must also be a means by
which oxygen masks can be manually
deployed from the flight deck.
(f) Approved procedures must be
established for OCR occupants in the
event of decompression. These
procedures must be transmitted to the
operator for incorporation into their
training programs and appropriate
operational manuals.
(g) The supplemental oxygen system
for the OCR compartment must meet the
same 14 CFR part 25 regulations as the
supplemental oxygen system for the
passenger cabin occupants except for
the 10 percent additional masks
requirement of 14 CFR 25.1447(c)(1).
(h) The illumination level of the
normal OCR compartment lighting
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17:10 Dec 31, 2009
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system must automatically be sufficient
for each occupant of the compartment to
locate a deployed oxygen mask.
14. The following requirements apply
to OCR compartments that are divided
into several sections by the installation
of curtains or partitions:
(a) A placard is required adjacent to
each curtain that visually divides or
separates, for privacy purposes, the OCR
compartment into small sections. The
placard must require that the curtain(s)
remains open when the private section
it creates is unoccupied. The vestibule
section adjacent to the stairway is not
considered a private area and, therefore,
does not require a placard.
(b) For each section of the OCR
compartment created by the installation
of a curtain, the following requirements
of these proposed special conditions
must be met with the curtain open or
closed:
(1) No smoking placard requirement
(Proposed Special Condition No. 1).
(2) Emergency illumination
requirement (Proposed Special
Condition No. 5).
(3) Emergency alarm system
requirement (Proposed Special
Condition No. 7).
(4) Seat belt fasten signal or return to
seat signal as applicable requirement
(Proposed Special Condition No. 8).
(5) Smoke or fire detection system
requirement (Proposed Special
Condition No. 10).
(6) Oxygen system requirement
(Proposed Special Condition No. 13).
(c) Overhead crew rest compartments
that are visually divided to the extent
that evacuation could be affected must
have exit signs directing occupants to
the primary stairway outlet. The exit
signs must be provided in each separate
section of the OCR compartment, except
for curtained bunks, and must meet
requirements of § 25.812(b)(1)(i). An exit
sign with reduced background area or a
symbolic exit sign as described in
Proposed Special Condition No. 4(a)
may be used to meet this requirement.
(d) For sections within an OCR
compartment created by the installation
of a rigid partition with a door
physically separating the sections, the
following requirements of these
proposed special conditions must be
met with the door open or closed:
(1) There must be a secondary
evacuation route from each section to
the main deck, or alternatively, the
applicant must show that any door
between the sections has been designed
to preclude anyone from being trapped
inside the compartment. Removal of an
incapacitated occupant within this area
must be considered. A secondary
evacuation route from a small room
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Fmt 4702
Sfmt 4702
designed for only one occupant for a
short time duration, such as a changing
area or lavatory, is not required, but
removal of an incapacitated occupant
from within such a small room must be
considered.
(2) Any door between the sections
must be shown to be openable when
crowded against, even when crowding
occurs at each side of the door.
(3) There may be no more than one
door between any seat or berth and the
primary stairway exit.
(4) In each section there must be exit
signs meeting requirements of
§ 25.812(b)(1)(i), or shown to have an
equivalent level of safety, that direct
occupants to the primary stairway exit.
An exit sign with reduced background
area or a symbolic exit sign as described
in Proposed Special Condition No. 4(a)
may be used to meet this requirement.
(e) For each smaller section within the
main OCR compartment created by the
installation of a partition with a door,
the following requirements of these
proposed special conditions must be
met with the door open or closed:
(1) No smoking placards requirement
(Proposed Special Condition No. 1).
(2) Emergency illumination
requirement (Proposed Special
Condition No. 5).
(3) Two-way voice communication
requirement (Proposed Special
Condition No. 6).
(4) Emergency alarm system
requirement (Proposed Special
Condition No. 7).
(5) Seat belt fasten signal or return to
seat signal as applicable requirement
(Proposed Special Condition No. 8).
(6) Emergency firefighting and
protective equipment requirement
(Proposed Special Condition No. 9).
(7) Smoke or fire detection system
requirement (Proposed Special
Condition No. 10).
(8) Oxygen system requirement
(Proposed Special Condition No. 13).
15. The requirements for two-way
voice communication with the flight
deck and provisions for emergency
firefighting and protective equipment do
not apply to lavatories or other small
areas that are not intended to be
occupied for extended periods of time.
16. If a waste disposal receptacle is
fitted in the OCR compartment, it must
be equipped with an automatic fire
extinguisher that meets the performance
requirements of § 25.854(b).
17. Materials (including finishes or
decorative surfaces applied to the
materials) must comply with
flammability requirements of § 25.853(a)
as amended by Amendment 25–116.
Mattresses must comply with the
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Federal Register / Vol. 75, No. 1 / Monday, January 4, 2010 / Proposed Rules
flammability requirements of § 25.853(c)
as amended by Amendment 25–116.
18. The addition of a lavatory within
the OCR compartment would require
the lavatory to meet the same
requirements as those for a lavatory
installed on the main deck except with
regard to Proposed Special Condition
No. 10 for smoke detection.
19. Each stowage compartment in the
OCR compartment must be completely
enclosed. All enclosed stowage
compartments within the OCR
compartment that are not limited to
stowage of emergency equipment or
airplane-supplied equipment (i.e.,
bedding) must meet the design criteria
given in the table below. Enclosed
stowage compartments greater than 200
ft3 in interior volume are not addressed
by this proposed special condition. The
81
in-flight accessibility of very large
enclosed stowage compartments and the
subsequent impact on the
crewmembers’ ability to effectively
reach any part of the compartment with
the contents of a hand fire extinguisher
will require additional fire protection
considerations similar to those required
for inaccessible compartments such as
Class C cargo compartments.
DESIGN CRITERIA FOR ENCLOSED STOWAGE COMPARTMENTS NOT LIMITED TO STOWAGE OF EMERGENCY OR AIRPLANESUPPLIED EQUIPMENT
Applicability of fire protection requirements by interior volume
Fire protection features
Less than 25 cubic feet
Compliant Materials of Construction1
Smoke or Fire Detectors 2 .............
Liner 3 .............................................
Fire Location Detector 4 .................
25 Cubic feet to less than 57
cubic feet
57 Cubic feet to
200 cubic feet
Yes ................................................
Yes ................................................
Yes.
No .................................................
No .................................................
No .................................................
Yes ................................................
Conditional ....................................
Yes ................................................
Yes.
Yes.
Yes.
1 Compliant
Materials of Construction
The material used to construct each enclosed stowage compartment must at least be fire resistant and must meet the flammability standards
established for interior components (i.e., 14 CFR part 25 Appendix F, parts I, IV, and V) per the requirements of § 25.853. For compartments less
than 25 ft.3 in interior volume, the design must ensure the ability to contain a fire likely to occur within the compartment under normal use.
2 Smoke or Fire Detectors
Enclosed stowage compartments equal to or exceeding 25 ft.3 in interior volume must be provided with a smoke or fire detection system to ensure that a fire can be detected within a one-minute detection time. Flight tests must be conducted to show compliance with this requirement.
Each system (or systems) must provide:
(a) A visual indication in the flight deck within one minute after the start of a fire.
(b) An aural warning in the overhead crew rest compartment.
(c) A warning in the main passenger cabin. This warning must be readily detectable by a flight attendant, taking into consideration the positioning of flight attendants throughout the main passenger compartment during various phases of flight.
3 Liner
If it can be shown that the material used to construct the stowage compartment meets the flammability requirements of a liner for a Class B
cargo compartment (i.e., § 25.855 at Amendment 25–116, and Appendix F, part I, paragraph (a)(2)(ii)), then no liner would be required for enclosed stowage compartments equal to or greater than 25 ft.3 but less than 57 ft.3 in interior volume. For all enclosed stowage compartments
equal to or greater than 57 ft.3 in interior volume but less than or equal to 200 ft.3, a liner must be provided that meets the requirements of
§ 25.855 for a Class B cargo compartment.
4 Fire Location Detector
If an OCR compartment has enclosed stowage compartments exceeding 25 ft.3 interior volume that are located separately from the other stowage compartments (located, for example, away from one central location, such as the entry to the OCR compartment or a common area within
the OCR compartment, where the other stowage compartments are), that OCR compartment would require additional fire protection features
and/or devices to assist the firefighter in determining the location of a fire.
Issued in Renton, Washington, on
December 28, 2009.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E9–31117 Filed 12–31–09; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
pwalker on DSK8KYBLC1PROD with PROPOSALS
14 CFR Part 25
[Docket No. NM411 Special Conditions No.
25–09–07–SC]
Special Conditions: Boeing Model 787–
8 Airplane; Overhead Flightcrew Rest
Compartment Occupiable During Taxi,
Take-Off, and Landing
AGENCY: Federal Aviation
Administration (FAA), DOT.
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19:15 Dec 31, 2009
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ACTION: Notice of proposed special
conditions.
SUMMARY: This action proposes special
conditions for the Boeing Model 787–8
airplane. This airplane will have novel
or unusual design features associated
with an overhead flightcrew rest (OFCR)
compartment, which is proposed to be
occupiable during taxi, take-off, and
landing (TT&L). 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. Additional
special conditions will be issued for
other novel or unusual design features
of the Boeing Model 787–8 airplanes.
PO 00000
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DATES: We must receive your comments
by February 18, 2010.
ADDRESSES: You must mail two copies
of your comments to: Federal Aviation
Administration, Transport Airplane
Directorate, Attn: Rules Docket (ANM–
113), Docket No. NM411, 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.
NM411. 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: Jeff
Gardlin, FAA, Airframe/Cabin Safety
Branch, ANM–115, Transport Standards
Staff, Transport Airplane Directorate,
Aircraft Certification Service, 1601 Lind
Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2136;
facsimile (425) 227–1320.
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Agencies
[Federal Register Volume 75, Number 1 (Monday, January 4, 2010)]
[Proposed Rules]
[Pages 75-81]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-31117]
========================================================================
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. 75, No. 1 / Monday, January 4, 2010 /
Proposed Rules
[[Page 75]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM412 Special Conditions No. 25-09-08-SC]
Special Conditions: Boeing Model 787-8 Airplane; Overhead Crew
Rest Compartment
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed special conditions.
-----------------------------------------------------------------------
SUMMARY: This action proposes special conditions for the Boeing Model
787-8 airplane. This airplane will have novel or unusual design
features associated with installation of an overhead crew rest
compartment. 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. Additional special conditions will be issued for other novel
or unusual design features of the Boeing Model 787-8 airplanes.
DATES: We must receive your comments by February 18, 2010.
ADDRESSES: You must mail two copies of your comments to: Federal
Aviation Administration, Transport Airplane Directorate, Attn: Rules
Docket (ANM-113), Docket No. NM412, 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. NM412. 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: Jeff Gardlin, FAA, Airframe/Cabin
Safety Branch, ANM-115, Transport Standards Staff, Transport Airplane
Directorate, Aircraft Certification Service, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056; telephone (425) 227-2136; facsimile
(425) 227-1320.
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
concerning 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 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.
If you want us to acknowledge receipt of your comments on this
proposal, include with your comments a self-addressed, stamped postcard
on which you have written the docket number. We will stamp the date on
the postcard and mail it back to you.
Background
On March 28, 2003, The Boeing Commercial Airplane Group (hereafter
referred to as ``Boeing'') applied for an FAA type certificate for its
new Boeing Model 787-8 passenger airplane. The company applied for an
extension of time for the type certificate on March 9, 2009, and was
granted that extension on March 13, 2009. The Boeing Model 787-8
airplane will be an all-new, two-engine jet transport airplane with a
two-aisle cabin. The maximum takeoff weight will be 476,000 pounds,
with a maximum passenger count of 381 passengers.
Type Certification Basis
Under provisions of Title 14 Code of Federal Regulations (14 CFR)
21.17, Boeing must show that the Boeing Model 787-8 airplane (hereafter
referred to as ``the 787'') meets the applicable provisions of 14 CFR
part 25, as amended by Amendments 25-1 through 25-117, 25-120, 25-124,
25-125 and 25-128, except that Sec. 25.1309 remains at Amendment 25-
117 for cargo fire protection systems. 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 787 because of
a novel or unusual design feature, special conditions are prescribed
under the provisions of Sec. 21.16.
In addition to complying with the applicable airworthiness
regulations and special conditions, the 787 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. In addition, the FAA must
issue a finding of regulatory adequacy pursuant to section 611 of
Public Law 92-574, the ``Noise Control Act of 1972.''
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. 21.17(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 features, the special conditions would also apply to the
other model under provisions of Sec. 21.101.
Novel or Unusual Design Features
Crew rest compartments have been installed and certificated on
several Boeing airplane models in locations as varied as the main
passenger seating area, the overhead space above the main passenger
cabin seating area, and below the passenger cabin seating area within
the cargo compartment. In each case, the Administrator has determined
that the applicable regulations (i.e., 14 CFR part 25) did not provide
all of the necessary requirements because each installation had unique
features by virtue of its design, location, and use on the airplane.
When the Administrator finds that the applicable airworthiness
[[Page 76]]
regulations do not contain adequate or appropriate safety standards
because of a novel or unusual design feature, special conditions are
prescribed under the provisions of Sec. 21.16. The special conditions
contain safety standards that the Administrator considers necessary to
establish a level of safety equivalent to that established by the
existing airworthiness standards.
Most recently, for the Boeing Model 777 series airplanes, the FAA
has issued Special Conditions No. 25-230-SC, dated April 9, 2003, for
overhead crew rest (OCR) compartments allowed to be occupied during
flight, and Special Conditions No. 25-260-SC, dated April 14, 2004, for
overhead flight crew rest (OFCR) compartments allowed to be occupied
during taxi, takeoff, and landing (TT&L), as well as during flight.
The OCR compartment on the 787 identified by Boeing as an overhead
flight attendant rest is located above the main passenger cabin,
adjacent to Door 4, and will be accessed from the main deck by stairs
through a vestibule. This OCR compartment will contain six private
berths, an emergency hatch that opens directly into the main passenger
cabin area, a smoke detection system, an oxygen system, and various
occupant amenities. This OCR compartment will only be occupied by
trained crew members in flight. It will not be occupied during taxi,
takeoff, or landing.
This 787 OCR compartment is unique to part 25 because of its
design, location, and use on the airplane. Because of the novel or
unusual features associated with installation of this compartment,
special conditions are considered necessary to provide a level of
safety equal to that established by the airworthiness regulations.
Certification engineers evaluate such an installation with respect
to the interior and assess it in accordance with the certification
basis of the airplane. However, part 25 does not provide all of the
requirements for crew rest compartments within the overhead area of the
passenger compartment. These proposed special conditions do not negate
the need to address other applicable part 25 regulations.
Operational Evaluations and Approval
These proposed special conditions outline requirements for OCR
compartment design approvals administered by the FAA's Aircraft
Certification Service. Prior to operational use of an OCR compartment,
the FAA's Flight Standards Service must evaluate and approve the
``basic suitability'' of the compartment for crew occupation.
Additionally, if an operator wishes to use an OCR compartment as
``sleeping quarters,'' the compartment must undergo an additional
evaluation and approval (reference 14 CFR 121.485(a), 121.523(b), and
135.269(b)(5)). Compliance with these proposed special conditions does
not ensure that the applicant has demonstrated compliance with the
requirements of parts 121 or 135.
To obtain an operational evaluation, the type certificate holder
must contact the appropriate aircraft evaluation group (AEG) in the
Flight Standards Service and request a ``basic suitability'' evaluation
or a ``sleeping quarters'' evaluation of its OCR compartment. The
results of these evaluations should be documented in a 787 flight
standardization board (FSB) report appendix. Individual operators may
reference these standardized evaluations in discussions with their FAA
principal operating inspector (POI) as the basis for an operational
approval, in lieu of an on-site operational evaluation.
Any changes to the approved OCR compartment configuration that
affect crewmember emergency egress or any other procedures affecting
safety of the occupying crewmembers or related emergency training will
require re-evaluation and approval. The applicant for an OCR
compartment design change that affects egress, safety procedures, or
training is responsible for notifying the FAA's AEG that a new
compartment evaluation is required. The results of a re-evaluation
should also be documented in a 787 FSB report appendix.
Procedures must be developed to ensure that a crewmember entering
the OCR compartment through the stairway/vestibule to fight a fire will
examine the stairway/vestibule and the adjacent galley or lavatory
areas (if installed) for the source of the fire before entering the
remaining areas of the compartment. This is intended to ensure that the
source of the fire is not between the crewmember and the entrance to
the OCR compartment. If a fire source is not immediately evident to the
firefighter, the firefighter should check for potential fire sources at
areas closest to the OCR compartment entrance first, then proceed to
check areas in such a manner that the fire source, when found, will not
be between the firefighter and his or her way to get out of the
compartment. Procedures describing methods for searching the OCR
compartment for fire source(s) must be transmitted to operators for
incorporation into their training programs and appropriate operational
manuals.
Discussion of Proposed Special Conditions
These proposed special conditions would initially apply to an OCR
compartment installed adjacent to the Door 4 exits on the 787. These
proposed special conditions would supplement 14 CFR part 25. Except as
noted below, these proposed special conditions for the 787 closely
resemble Boeing 777 Special Conditions No. 25-230-SC.
Proposed Special Conditions No. 4 and 14 contain requirements for
the exit signs that must be provided in the OCR compartment. Symbols
that satisfy the equivalent level of safety finding established for the
787 may be used in lieu of the text required by Sec. 25.812(b)(1)(i).
The FAA expects that crewmembers will learn the meaning of any symbolic
exit sign as a part of their training in evacuation procedures.
Proposed Special Condition No. 13 contains requirements for
supplemental oxygen systems. Special Conditions No. 25-260-SC, for the
overhead flightcrew rest compartments, required that each berth be
provided with two oxygen masks. This was intended to address the case
where a person not in a berth was moving around in the crew rest
compartment and needed quick access to the oxygen. For the designs used
in the model 777, this requirement was sufficient. However, for the
787, the requirement to have two masks per berth may not always meet
the objective of having masks available to persons who are in
transition within the compartment. Therefore, the wording of this
proposed special condition has been modified to better state the
objective rather than specify that two masks be provided per berth. In
addition, the requirement to have adequate illumination to retrieve the
mask, while implied previously, is made explicit in this proposal.
Proposed Special Condition No. 17 contains the requirement for
materials used in the construction of the OCR compartment and states
that Sec. 25.853 as amended by Amendment 25-116 is the appropriate
regulation. Amendment 25-116 is the latest amendment level for Sec.
25.853.
Compliance with these proposed special conditions does not relieve
the applicant from the existing airplane certification basis
requirements. One particular area of concern is that the installation
of OCR compartments leaves a smaller compartment volume within the
overhead area of the airplane. The applicant must comply with the
pressurized compartment loads requirements of Sec. 25.365(e), (f), and
(g) for the OCR compartment, as well as for
[[Page 77]]
any other airplane compartments whose decompression characteristics are
affected by the installation of an OCR compartment. Compliance with
Sec. 25.813 emergency exit access requirements must be demonstrated
for all phases of flight during which occupants will be present.
Section 25.813(e) prohibits installation of interior doors between
passenger compartments, but the FAA has historically found crew rest
doors to be acceptable, because crew rests are not passenger
compartments. Proposed Special Conditions No. 1 and 14 provide
requirements for crew rest doors which are considered to provide an
appropriate level of safety to OCR compartment occupants.
Sections 25.1443, 25.1445, and 25.1447 contain oxygen requirements
for flight crew, passengers, and cabin attendants. Crewmembers
occupying the OCR compartment are not on duty, and therefore are
considered passengers in determining compliance with these oxygen
regulations.
Applicability
As discussed above, these proposed special conditions are
applicable to the 787. Should Boeing apply at a later date for a change
to the type certificate to include another model incorporating the same
novel or unusual design features, these proposed special conditions
would apply to that model as well.
Conclusion
This action affects only certain novel or unusual design features
of the 787. It is not a rule of general applicability.
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 Boeing Model 787-8 airplanes with an overhead crew rest (OCR)
compartment installed above the main passenger cabin adjacent to an
exit door.
1. Occupancy of the OCR compartment is limited to the total number
of installed bunks and seats in each compartment. There must be an
approved seat or berth able to withstand the maximum flight loads when
occupied for each occupant permitted in the OCR compartment. Maximum
occupancy in the OCR compartment is six.
(a) There must be appropriate placards, inside and outside each
entrance to the OCR compartment, to indicate:
(1) The maximum number of occupants allowed.
(2) That occupancy is restricted to crewmembers who are trained in
the evacuation procedures for the OCR compartment.
(3) That occupancy is prohibited during taxi, take-off, and
landing.
(4) That smoking is prohibited in the OCR compartment.
(5) That stowage in the OCR compartment area is limited to crew
personal luggage. The stowage of cargo or passenger baggage is not
allowed.
(b) There must be at least one ashtray on the inside and one
ashtray on the outside of any entrance to the overhead crew rest
compartment.
(c) For times when there is no flight attendant present in the area
around the door to the OCR compartment, and also in the event of an
emergency, there must be a means to prevent passengers from entering
the OCR compartment.
(d) There must be a means for any door installed between the OCR
compartment and the passenger cabin to be quickly opened from inside
the compartment, even when crowding occurs at each side of the door.
(e) For all doors installed, there must be a means to preclude
anyone from being trapped inside the OCR compartment. If a locking
mechanism is installed, it must be capable of being unlocked from the
outside without the aid of special tools. The lock must not prevent
opening from the inside of the compartment at any time.
(f) The means of opening doors and hatches to the OCR compartment
must be simple and obvious. In addition, doors or hatches that separate
the overhead crew rest compartment from the main deck must not
adversely affect evacuation of occupants on the main deck (slowing
evacuation by encroaching into aisles, for example) or cause injury to
those occupants during opening or while opened.
2. There must be at least two emergency evacuation routes which
could be used by each occupant of the OCR compartment to rapidly
evacuate to the main cabin. These evacuation routes must be able to be
closed from the main passenger cabin after evacuation. In addition--
(a) The routes must be located with sufficient separation within
the OCR compartment to minimize the possibility of an event either
inside or outside of the crew rest compartment rendering both routes
inoperative.
Compliance with requirements of Proposed Special Condition No. 2(a)
may be shown by inspection or by analysis. Regardless of which method
is used, the maximum acceptable distance between crew rest compartment
outlets is 60 feet.
Compliance by Inspection
Inspection may be used to show compliance with proposed Special
Condition No. 2(a). An inspection finding that an OCR compartment has
evacuation routes located so that each occupant of the seats and berths
has an unobstructed route to at least one of the crew rest compartment
outlets, regardless of the location of a fire, would be reason for a
finding of compliance. A fire within a berth that only blocks the
occupant of that berth from exiting the berth need not be considered.
Therefore, crew rest compartment outlets that are located at absolute
opposite ends (i.e., adjacent to opposite end walls) of the OCR
compartment would require no further review or analysis with regard to
exit separation.
Compliance by Analysis
Analysis must show that the OCR compartment configuration and
interior features allow all occupants of the OCR compartment to escape
the compartment in the event of a hazard inside or outside of the
compartment.
Elements to consider in this evaluation are as follows:
(1) Fire inside or outside the OCR compartment, considered
separately, and the design elements used to reduce the available fuel
for the fire.
(2) Design elements used to reduce fire ignition sources in the OCR
compartment.
(3) Distribution and quantity of emergency equipment within the OCR
compartment.
(4) Structural failure or deformation of components that could
block access to the available evacuation routes (e.g., seats, folding
berths, contents of stowage compartments, etc.).
(5) An incapacitated person blocking the evacuation routes.
(6) Any other foreseeable hazard not identified above that could
cause the evacuation routes to be compromised.
Analysis must consider design features affecting access to the
evacuation routes. Possibilities for design components affecting
evacuation that should be considered include, but are not limited to,
seat back break over, rigid structure that reduces access from one part
of the compartment to another,
[[Page 78]]
and items known to be the cause of potential hazards. Factors that also
should be considered are availability of emergency equipment to address
fire hazards, availability of communications equipment, supplemental
restraint devices to retain items of mass that, if broken loose, could
hinder evacuation, and load path isolation between components
containing evacuation routes.
Analysis of fire threats should be used in determining placement of
required fire extinguishers and protective breathing equipment (PBE).
This analysis should consider the possibility of fire in any location
in the OCR compartment. The location and quantity of PBE equipment and
fire extinguishers should allow occupants located in any approved seats
or berths access to the equipment necessary to fight a fire in the OCR
compartment.
The intent of this proposed special condition is to provide
sufficient exit route separation. Therefore the exit separation
analysis described above should not be used to approve crew rest
compartment outlets that have less physical separation (measured
between the centroid of each exit opening) than the minimums prescribed
below, unless compensating features are identified and submitted to the
FAA for evaluation and approval.
For OCR compartments with one outlet located near the forward or
aft end of the compartment (as measured by having the centroid of the
exit opening within 20 percent of the forward or aft end of the total
overhead crew rest compartment length) the outlet separation from one
outlet to the other should not be less than 50 percent of the total OCR
compartment length.
For OCR compartments with neither required crew rest compartment
outlet located near the forward or aft end of the compartment (as
measured by not having the centroid of either outlet opening within 20
percent of the forward or aft end of the total OCR compartment length)
the outlet separation from one outlet to the other should not be less
than 30 percent of the total OCR compartment length.
(b) The routes must be designed to minimize the possibility of
blockage, which might result from fire, mechanical or structural
failure, or persons standing below or against the crew rest compartment
outlets. One of the two OCR evacuation routes should not be located
where, during times when occupancy is allowed, normal movement by
passengers occurs (i.e., main aisle, cross aisle or galley complex, for
example) that would impede egress from the OCR compartment. If an
evacuation route is in an area where normal movement of passengers
occurs, it must be demonstrated that passengers would not impede egress
to the main deck. If there is low headroom at or near the evacuation
route, provisions must be made to prevent or to protect occupants of
the OCR compartment from head injury. Use of evacuation routes must not
be dependent on any powered device. If a crew rest compartment outlet
is over an area where there are passenger seats, a maximum of five
passengers may be displaced from their seats temporarily during the
process of evacuating an incapacitated person(s). If such an evacuation
procedure involves the evacuee stepping on seats, the seats must not be
damaged to the extent that they would not be acceptable for occupancy
during an emergency landing.
(c) Emergency evacuation procedures, including procedures for
emergency evacuation of an incapacitated occupant from the OCR
compartment, must be established. The applicant must transmit all of
these procedures to the operator for incorporation into its training
programs and appropriate operational manuals.
(d) There must be a limitation in the airplane flight manual or
other suitable means to require that crewmembers be trained in use of
the OCR evacuation routes.
3. There must be a means of evacuating an incapacitated person
(representative of a ninety-fifth percentile male) from the OCR
compartment to the passenger cabin floor.
(a) Such an evacuation must be demonstrated for all evacuation
routes. A crewmember (a total of one assistant within the OCR
compartment) may provide assistance in the evacuation. Additional
assistance may be provided by up to three persons in the main passenger
compartment. These additional assistants must be standing on the floor
while providing assistance. For evacuation routes with stairways, the
additional assistants may ascend up to one half the elevation change
from the main deck to the OCR compartment, or to the first landing,
whichever is lower.
4. The following signs and placards must be provided in the OCR
compartment, and they must meet the following criteria:
(a) At least one exit sign, located near each exit, meeting the
emergency lighting requirements of Sec. 25.812(b)(1)(i). One allowable
exception would be a sign with reduced background area of no less than
5.3 square inches (excluding the letters), provided that it is
installed so that the material surrounding the exit sign is light in
color (e.g., white, cream, light beige, for example). If the material
surrounding the exit sign is not light in color, a sign with a minimum
of a one-inch-wide background border around the letters would also be
acceptable. Another allowable exception is a sign with a symbol that
the FAA has determined to be equivalent for use as an exit sign in an
OCR compartment.
(b) An appropriate placard located near each exit defining the
location of and operating instructions for each evacuation route.
(c) Placards must be readable from a distance of 30 inches under
emergency lighting conditions.
(d) The exit handles and evacuation path operating instruction
placards must be illuminated to at least 160 microlamberts under
emergency lighting conditions.
5. There must be a means in the event of failure of the aircraft's
main power system, or of the normal OCR compartment lighting system,
for emergency illumination to be automatically provided for the OCR
compartment.
(a) This emergency illumination must be independent of the main
lighting system.
(b) The sources of general cabin illumination may be common to both
the emergency and the main lighting systems if the power supply to the
emergency lighting system is independent of the power supply to the
main lighting system.
(c) The illumination level must be sufficient to allow occupants of
the OCR compartment to locate and move to the main passenger cabin
floor by means of each evacuation route.
(d) The illumination level must be sufficient, with the privacy
curtains in the closed position, for each occupant of the crew rest
compartment to locate a deployed oxygen mask.
6. There must be means for two-way voice communications between
crewmembers on the flight deck and occupants of the OCR compartment.
There must also be two-way communications between occupants of the OCR
compartment and each flight attendant station in the passenger cabin
required per Sec. 25.1423(g) to have a public address system
microphone . In addition, the public address system must include
provisions to provide only the relevant information to the crewmembers
in the OCR compartment (for example fire in flight, aircraft
depressurization, preparation of the
[[Page 79]]
compartment occupants for landing, etc.).
7. There must be a means for manual activation of an aural
emergency alarm system, audible during normal and emergency conditions,
to enable crewmembers on the flight deck and at each pair of required
floor level emergency exits to alert occupants of the overhead crew
rest OCR compartment of an emergency situation. Use of a public address
or crew interphone system will be acceptable, provided an adequate
means of differentiating between normal and emergency communications is
incorporated. The system must be powered in flight, after the shutdown
or failure of all engines and auxiliary power units, for a period of at
least ten minutes.
8. There must be a means, readily detectable by seated or standing
occupants of the OCR compartment, to indicate when seat belts should be
fastened. If there are no seats in the OCR compartment, at least one
means must be provided to cover anticipated turbulence (e.g.,
sufficient handholds). Seat belt type restraints must be provided for
berths and must be compatible for the sleeping attitude during cruise
conditions. There must be a placard on each berth requiring that seat
belts be fastened when occupied. If compliance with any of the other
requirements of these proposed special conditions is predicated on
specific head location, there must be a placard identifying that head
position.
9. In lieu of the requirements specified in Sec. 25.1439(a)
pertaining to isolated compartments, and to provide a level of safety
equivalent to that provided to occupants of an isolated galley, the
following equipment must be provided in the OCR compartment:
(a) At least one approved hand-held fire extinguisher appropriate
for the kinds of fires likely to occur.
(b) Two PBE devices suitable for firefighting, or one PBE for each
hand-held fire extinguisher, whichever is greater. All PBE devices must
be approved to Technical Standard Order (TSO)-C116 or equivalent.
(c) One flashlight.
Note: Additional PBE devices and fire extinguishers in specific
locations, beyond the minimum numbers prescribed in Proposed Special
Condition No. 9, may be required as a result of the egress analysis
accomplished to satisfy Proposed Special Condition No. 2(a).
10. A smoke or fire detection system (or systems) must be provided
that monitors each occupiable area within the OCR compartment,
including those areas partitioned by curtains or doors. Flight tests
must be conducted to show compliance with this requirement. If a fire
occurs, each system (or systems) must provide:
(a) A visual indication to the flightdeck within one minute after
the start of a fire.
(b) An aural warning in the OCR compartment.
(c) A warning in the main passenger cabin. This warning must be
readily detectable by a flight attendant, taking into consideration the
positioning of flight attendants throughout the main passenger
compartment during various phases of flight.
11. The OCR compartment must be designed so that fires within the
compartment can be controlled without a crewmember having to enter the
compartment, or the design of the access provisions must allow
crewmembers equipped for firefighting to have unrestricted access to
the compartment. The time for a crewmember on the main deck to react to
the fire alarm, don the firefighting equipment, and gain access to the
OCR compartment must not exceed the time it takes for the compartment
to become filled with smoke, making it difficult to locate the fire
source. Approved procedures describing methods for searching the OCR
for fire sources(s) must be established. These procedures must be
transmitted to the operator for incorporation into its training
programs and appropriate operational manuals.
12. There must be a means provided to exclude hazardous quantities
of smoke or extinguishing agent originating in the OCR compartment from
entering any other compartment occupied by crewmembers or passengers.
The effectiveness of this means must include the time periods during
evacuation of the OCR compartment and, if applicable, the time during
which crewmembers are accessing the OCR compartment to manually fight a
fire. Smoke entering any other compartment occupied by crewmembers or
passengers when the access to the OCR compartment is opened, during an
emergency evacuation, must dissipate within five minutes after the
access to the OCR compartment is closed.
(a) Hazardous quantities of smoke may not enter any other
compartment occupied by crewmembers or passengers during access to the
OCR compartment to manually fight a fire. The amount of smoke entrained
by a firefighter exiting the OCR compartment through the access is not
considered hazardous. During the one-minute smoke detection time,
penetration of a small quantity of smoke from the OCR compartment into
an occupied area is acceptable. Flight tests must be conducted to show
compliance with this requirement.
(b) There must be a provision in the firefighting procedures to
ensure that all door(s) and hatch(es) at the crew rest compartment
outlets are closed after evacuation of the compartment and during
firefighting to minimize smoke and extinguishing agent entering other
occupiable compartments.
(c) If a built-in fire extinguishing system is to be used instead
of manual firefighting, the fire extinguishing system must be designed
so that no hazardous quantities of extinguishing agent will enter other
compartments occupied by passengers or crew. The system must have
adequate capacity to suppress a fire considering the fire threat, the
volume of the compartment, and the ventilation rate.
(1) The system must have sufficient extinguishing agent to provide
an initial knockdown and suppression environment per the minimum
performance standards that have been established for the agent being
used. In addition, certification flight testing will verify the
acceptable duration that the suppression environment can be maintained.
(2) If the capacity of the extinguishing system does not provide
effective fire suppression that will last for the duration of flight
from the farthest point in route to the nearest suitable landing site
expected in service, an additional manual firefighting procedure must
be established. For the built-in extinguishing system, the time
duration for effective fire suppression must be established and
documented in the firefighting procedures in the airplane flight
manual. If the duration of time for demonstrated effective fire
suppression provided by the built-in extinguishing agent will be
exceeded, the firefighting procedures must instruct the crew to:
(i) Enter the OCR compartment at the time that demonstrated fire
suppression effectiveness will be exceeded.
(ii) Check for and extinguish any residual fire.
(iii) Confirm that the fire is out.
(b) For a manual hand-held bottle extinguishing system (designed as
the sole means to fight a fire or to supplement a built-in
extinguishing system of limited suppression duration) for the OCR:
(1) There must be a limitation in the airplane flight manual or
other suitable means requiring that crewmembers be trained in the
firefighting procedures.
(2) The compartment design must allow crewmembers equipped for
[[Page 80]]
firefighting to have unrestricted access to all parts of the
compartment.
(3) The time for a crewmember on the main deck to react to the fire
alarm, don the firefighting equipment, and gain access to the OCR
compartment must not exceed the time it would take for the compartment
to become filled with smoke, thus making it difficult to locate the
fire source.
13. There must be a supplemental oxygen system within the crew rest
compartment as follows:
(a) There must be at least one mask for each seat and berth in the
crew rest compartment.
(b) If a destination area (such as a changing area) is provided in
the OCR compartment, there must be an oxygen mask readily available for
each occupant who can reasonably be expected to be in the destination
area (with the maximum number of required masks within the destination
area being limited to the placarded maximum occupancy of the crew
rest).
(c) There must also be an oxygen mask readily accessible to each
occupant who can reasonably be expected to be moving from the main
cabin into the OCR compartment, moving around within the OCR
compartment, or moving from the OCR compartment to the main cabin.
(d) The system must provide an aural and visual alert to warn
occupants of the OCR compartment to don oxygen masks in the event of
decompression. The aural and visual alerts must activate concurrently
with deployment of the oxygen masks in the passenger cabin. To
compensate for sleeping occupants, the aural alert must be heard in
each section of the OCR compartment and must sound continuously for a
minimum of five minutes or until a reset switch within the OCR
compartment is activated. A visual alert that informs occupants that
they must don an oxygen mask must be visible in each section.
(e) There must also be a means by which oxygen masks can be
manually deployed from the flight deck.
(f) Approved procedures must be established for OCR occupants in
the event of decompression. These procedures must be transmitted to the
operator for incorporation into their training programs and appropriate
operational manuals.
(g) The supplemental oxygen system for the OCR compartment must
meet the same 14 CFR part 25 regulations as the supplemental oxygen
system for the passenger cabin occupants except for the 10 percent
additional masks requirement of 14 CFR 25.1447(c)(1).
(h) The illumination level of the normal OCR compartment lighting
system must automatically be sufficient for each occupant of the
compartment to locate a deployed oxygen mask.
14. The following requirements apply to OCR compartments that are
divided into several sections by the installation of curtains or
partitions:
(a) A placard is required adjacent to each curtain that visually
divides or separates, for privacy purposes, the OCR compartment into
small sections. The placard must require that the curtain(s) remains
open when the private section it creates is unoccupied. The vestibule
section adjacent to the stairway is not considered a private area and,
therefore, does not require a placard.
(b) For each section of the OCR compartment created by the
installation of a curtain, the following requirements of these proposed
special conditions must be met with the curtain open or closed:
(1) No smoking placard requirement (Proposed Special Condition No.
1).
(2) Emergency illumination requirement (Proposed Special Condition
No. 5).
(3) Emergency alarm system requirement (Proposed Special Condition
No. 7).
(4) Seat belt fasten signal or return to seat signal as applicable
requirement (Proposed Special Condition No. 8).
(5) Smoke or fire detection system requirement (Proposed Special
Condition No. 10).
(6) Oxygen system requirement (Proposed Special Condition No. 13).
(c) Overhead crew rest compartments that are visually divided to
the extent that evacuation could be affected must have exit signs
directing occupants to the primary stairway outlet. The exit signs must
be provided in each separate section of the OCR compartment, except for
curtained bunks, and must meet requirements of Sec. 25.812(b)(1)(i).
An exit sign with reduced background area or a symbolic exit sign as
described in Proposed Special Condition No. 4(a) may be used to meet
this requirement.
(d) For sections within an OCR compartment created by the
installation of a rigid partition with a door physically separating the
sections, the following requirements of these proposed special
conditions must be met with the door open or closed:
(1) There must be a secondary evacuation route from each section to
the main deck, or alternatively, the applicant must show that any door
between the sections has been designed to preclude anyone from being
trapped inside the compartment. Removal of an incapacitated occupant
within this area must be considered. A secondary evacuation route from
a small room designed for only one occupant for a short time duration,
such as a changing area or lavatory, is not required, but removal of an
incapacitated occupant from within such a small room must be
considered.
(2) Any door between the sections must be shown to be openable when
crowded against, even when crowding occurs at each side of the door.
(3) There may be no more than one door between any seat or berth
and the primary stairway exit.
(4) In each section there must be exit signs meeting requirements
of Sec. 25.812(b)(1)(i), or shown to have an equivalent level of
safety, that direct occupants to the primary stairway exit. An exit
sign with reduced background area or a symbolic exit sign as described
in Proposed Special Condition No. 4(a) may be used to meet this
requirement.
(e) For each smaller section within the main OCR compartment
created by the installation of a partition with a door, the following
requirements of these proposed special conditions must be met with the
door open or closed:
(1) No smoking placards requirement (Proposed Special Condition No.
1).
(2) Emergency illumination requirement (Proposed Special Condition
No. 5).
(3) Two-way voice communication requirement (Proposed Special
Condition No. 6).
(4) Emergency alarm system requirement (Proposed Special Condition
No. 7).
(5) Seat belt fasten signal or return to seat signal as applicable
requirement (Proposed Special Condition No. 8).
(6) Emergency firefighting and protective equipment requirement
(Proposed Special Condition No. 9).
(7) Smoke or fire detection system requirement (Proposed Special
Condition No. 10).
(8) Oxygen system requirement (Proposed Special Condition No. 13).
15. The requirements for two-way voice communication with the
flight deck and provisions for emergency firefighting and protective
equipment do not apply to lavatories or other small areas that are not
intended to be occupied for extended periods of time.
16. If a waste disposal receptacle is fitted in the OCR
compartment, it must be equipped with an automatic fire extinguisher
that meets the performance requirements of Sec. 25.854(b).
17. Materials (including finishes or decorative surfaces applied to
the materials) must comply with flammability requirements of Sec.
25.853(a) as amended by Amendment 25-116. Mattresses must comply with
the
[[Page 81]]
flammability requirements of Sec. 25.853(c) as amended by Amendment
25-116.
18. The addition of a lavatory within the OCR compartment would
require the lavatory to meet the same requirements as those for a
lavatory installed on the main deck except with regard to Proposed
Special Condition No. 10 for smoke detection.
19. Each stowage compartment in the OCR compartment must be
completely enclosed. All enclosed stowage compartments within the OCR
compartment that are not limited to stowage of emergency equipment or
airplane-supplied equipment (i.e., bedding) must meet the design
criteria given in the table below. Enclosed stowage compartments
greater than 200 ft\3\ in interior volume are not addressed by this
proposed special condition. The in-flight accessibility of very large
enclosed stowage compartments and the subsequent impact on the
crewmembers' ability to effectively reach any part of the compartment
with the contents of a hand fire extinguisher will require additional
fire protection considerations similar to those required for
inaccessible compartments such as Class C cargo compartments.
Design Criteria for Enclosed Stowage Compartments Not Limited to Stowage of Emergency or Airplane-Supplied
Equipment
----------------------------------------------------------------------------------------------------------------
Applicability of fire protection requirements by interior volume
--------------------------------------------------------------------------
Fire protection features 25 Cubic feet to less 57 Cubic feet to 200
Less than 25 cubic feet than 57 cubic feet cubic feet
----------------------------------------------------------------------------------------------------------------
Compliant Materials of Yes.................... Yes.................... Yes.
Construction\1\
Smoke or Fire Detectors \2\.......... No..................... Yes.................... Yes.
Liner \3\............................ No..................... Conditional............ Yes.
Fire Location Detector \4\........... No..................... Yes.................... Yes.
----------------------------------------------------------------------------------------------------------------
\1\ Compliant Materials of Construction
The material used to construct each enclosed stowage compartment must at least be fire resistant and must meet
the flammability standards established for interior components (i.e., 14 CFR part 25 Appendix F, parts I, IV,
and V) per the requirements of Sec. 25.853. For compartments less than 25 ft.\3\ in interior volume, the
design must ensure the ability to contain a fire likely to occur within the compartment under normal use.
\2\ Smoke or Fire Detectors
Enclosed stowage compartments equal to or exceeding 25 ft.\3\ in interior volume must be provided with a smoke
or fire detection system to ensure that a fire can be detected within a one-minute detection time. Flight
tests must be conducted to show compliance with this requirement. Each system (or systems) must provide:
(a) A visual indication in the flight deck within one minute after the start of a fire.
(b) An aural warning in the overhead crew rest compartment.
(c) A warning in the main passenger cabin. This warning must be readily detectable by a flight attendant, taking
into consideration the positioning of flight attendants throughout the main passenger compartment during
various phases of flight.
\3\ Liner
If it can be shown that the material used to construct the stowage compartment meets the flammability
requirements of a liner for a Class B cargo compartment (i.e., Sec. 25.855 at Amendment 25-116, and Appendix
F, part I, paragraph (a)(2)(ii)), then no liner would be required for enclosed stowage compartments equal to
or greater than 25 ft.\3\ but less than 57 ft.\3\ in interior volume. For all enclosed stowage compartments
equal to or greater than 57 ft.\3\ in interior volume but less than or equal to 200 ft.\3\, a liner must be
provided that meets the requirements of Sec. 25.855 for a Class B cargo compartment.
\4\ Fire Location Detector
If an OCR compartment has enclosed stowage compartments exceeding 25 ft.\3\ interior volume that are located
separately from the other stowage compartments (located, for example, away from one central location, such as
the entry to the OCR compartment or a common area within the OCR compartment, where the other stowage
compartments are), that OCR compartment would require additional fire protection features and/or devices to
assist the firefighter in determining the location of a fire.
Issued in Renton, Washington, on December 28, 2009.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-31117 Filed 12-31-09; 8:45 am]
BILLING CODE 4910-13-P