[Federal Register: September 18, 2006 (Volume 71, Number 180)]
[Rules and Regulations]
[Page 54572-54576]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr18se06-4]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM347; Special Conditions No. 25-331-SC]
Special Conditions: Boeing Model 777-200 Series Airplanes;
Forward Lower Lobe Crew Rest Compartment (CRC)
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions.
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SUMMARY: These special conditions are issued for the Boeing Model 777-
200 series airplanes. These airplanes, modified by Aerocon Engineering
Company (AEC), will have a novel or unusual design feature associated
with a forward lower lobe crew rest compartment (CRC). The applicable
airworthiness regulations do not contain adequate or appropriate safety
standards for this design feature. These special conditions contain the
additional safety standards the Administrator considers necessary to
establish a level of safety equivalent to that established by the
existing airworthiness standards.
DATES: Effective Date: The effective date of these special conditions
is September 8, 2006.
FOR FURTHER INFORMATION CONTACT: Jayson Claar, FAA, Airframe/Cabin
Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-
3356; telephone (425) 227-2194; facsimile (425) 227-1320.
SUPPLEMENTARY INFORMATION:
Background
On March 10, 2005, AEC applied for a supplemental type certificate
(STC) to allow installation of a CRC in Boeing 777-200 series
airplanes.
The CRC will be located under the passenger cabin floor in the
forward cargo compartment of Boeing Model 777-200 series airplanes. It
will be the size of three standard airfreight containers, combined, and
will be removable from the cargo compartment. The CRC will be occupied
in flight but not during taxi, takeoff, or landing. No more than ten
crewmembers at a time will be permitted to occupy it. The CRC will have
a smoke detection system, a hand held fire extinguishing system, and an
oxygen system.
The CRC will be accessed from the main deck via a ``stairhouse.''
The floor within the stairhouse has a hatch that leads to stairs which
occupants use to descend into the CRC. This hatch locks automatically
in the open position when fully opened. In addition, there will be an
emergency hatch which opens directly into the main passenger cabin
area. The CRC also has a maintenance access/ground loading door. This
door is intended to be used to allow maintenance personnel and cargo
handlers to enter the CRC from the cargo compartment when the airplane
is not in flight.
Type Certification Basis
Under Sec. 21.101, AEC must show that Boeing Model 777-200 series
airplanes, as changed, continue to meet (1) the applicable provisions
of the regulations incorporated by reference in Type Certificate No.
T00001SE or (2) the applicable regulations in effect on the date of
application for the change. The regulations incorporated by reference
in the type certificate are commonly referred to as the ``original type
certification basis.'' The regulations incorporated by reference in
Type Certificate No. T00001SE are as follows:
The certification basis for Boeing Model 777-200 series airplanes
is 14 CFR part 25, as amended by Amendments 25-1 through 25-82, except
for Sec. 25.571(e)(1) which remains at Amendment 25-71, with
exceptions. Refer to Type Certificate No. T00001SE, as applicable, for
a complete description of the certification basis for this model,
including certain special conditions that are not relevant to these
special conditions.
If the Administrator finds the applicable airworthiness regulations
(i.e., part 25) do not contain adequate or appropriate safety standards
for Boeing Model 777-200 series airplanes because of a novel or unusual
design feature, special conditions are prescribed under Sec. 21.16.
Besides the applicable airworthiness regulations and special
conditions, Boeing Model 777-200 series airplanes must comply with the
fuel vent and exhaust emission requirements of 14 CFR part 34 and the
noise certification requirements of 14 CFR part 36.
The FAA issues special conditions, as defined in Sec. 11.19, under
Sec. 11.38 and they become part of the type certification basis under
Sec. 21.101.
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 or similar
novel or unusual design feature, or should any other model already
included on the same type certificate be modified to incorporate the
same or similar novel or unusual design feature, the special conditions
would also apply to the other model under Sec. 21.101.
Novel or Unusual Design Features
While the installation of a CRC is not a new concept for large
transport category airplanes, each CRC has unique features based on
design, location, and use on the airplane. The CRC is novel in terms of
part 25 in that it will be located below the passenger cabin floor in
the forward cargo compartment of Boeing Model 777-200 series airplanes.
Because of the novel or unusual features associated with the
installation of a CRC, special conditions are considered necessary to
provide a level of safety equal to that established by the
airworthiness regulations incorporated by reference in the type
certificates of these airplanes. These special conditions do not negate
the need to address other applicable part 25 regulations.
Operational Evaluations and Approval
These special conditions specify requirements for design approvals
(i.e., type design changes and STCs) of CRCs administered by the FAA's
Aircraft Certification Service. Before operational use of a CRC, the
FAA's Flight Standards Service, Aircraft Evaluation Group (AEG), must
evaluate and approve the ``basic suitability'' of the CRC for
occupation by crewmembers. If an operator wishes to utilize a CRC as
``sleeping quarters,'' the CRC must undergo an additional operational
[[Page 54573]]
evaluation and approval. The CRC would be evaluated for compliance to
Sec. Sec. 121.485(a) and 121.523(b), with Advisory Circular 121-31,
Flight Crew Sleeping Quarters and Rest Facilities, providing one method
of compliance to these operating regulations.
To obtain an operational evaluation, the supplemental type design
holder must contact the AEG within the Flight Standards Service which
has operational approval authority for the project. In this instance,
it is the Seattle AEG. The supplemental type design holder must request
a ``basic suitability'' evaluation or a ``sleeping quarters''
evaluation of the CRC. The supplemental type design holder may make
these requests concurrently with the demonstration of compliance with
these special conditions.
The results of these evaluations will be documented in the Boeing
Model 777-200 Flight Standardization Board (FSB) Report Appendix. In
discussions with their FAA Principal Operating Inspector (POI),
individual operators may reference these standardized evaluations as
the basis for an operational approval, in lieu of an on-site
operational evaluation.
An operational reevaluation and approval will be required for any
changes to the approved CRC configuration, if the changes affect
procedures for emergency egress of crewmembers, other safety procedures
for crewmembers occupying the CRC, or training related to these
procedures. The applicant for any such change is responsible for
notifying the Seattle AEG that a new CRC evaluation is required.
All instructions for continued airworthiness (ICAW), including
service bulletins, must be submitted to the Seattle AEG for approval
before the FAA issues its approval of the modification.
Discussion of Special Conditions No. 9 and 12
The following clarifies how Special Condition No. 9 should be
understood relative to the requirements of Sec. 25.1439(a):
Amendment 25-38 modified the requirements of Sec. 25.1439(a) by
adding, ``In addition, protective breathing equipment must be installed
in each isolated separate compartment in the airplane, including upper
and lower lobe galleys, in which crewmember occupancy is permitted
during flight for the maximum number of crewmembers expected to be in
the area during any operation.'' The CRC is an isolated separate
compartment, so Sec. 25.1439(a) is applicable. However, the Sec.
25.1439(a) PBE requirements for isolated separate compartments are not
appropriate because the CRC is novel and unusual in terms of the number
of occupants.
In 1976 when Amendment 25-38 was adopted, small galleys were the
only isolated compartments that had been certificated. Two crewmembers
were the maximum expected to occupy those galleys.
These special conditions address a CRC, which can accommodate up to
ten crewmembers. This large number of occupants in an isolated
compartment was not envisioned at the time Amendment 25-38 was adopted.
It is not appropriate for all occupants to don PBE in the event of a
fire because the first action should be to leave the confined space
unless the occupant is fighting the fire. Taking the time to don the
PBE would prolong the time for the emergency evacuation of the
occupants and possibly interfere with efforts to extinguish the fire.
Regarding Special Condition No. 12; the FAA considers that during
the 1-minute smoke detection time, penetration of a small quantity of
smoke from this forward lower lobe CRC design into an occupied area on
this airplane configuration would be acceptable based on the
limitations placed in these special conditions. The FAA considers that
the special conditions place sufficient restrictions in the quantity
and type of material allowed in crew carry-on bags that the threat from
a fire in this remote area would be equivalent to that experienced on
the main cabin.
Discussion of Comments
Notice of proposed special conditions No. 25-06-06SC for the Boeing
Model 777-200 series airplanes was published in the Federal Register on
June 21, 2006 (71 FR 35567). No comments were received, and the special
conditions are adopted as proposed.
Applicability
As discussed above, these special conditions are applicable to
Boeing Model 777-200 series airplanes as modified by the AEC to include
a forward lower lobe CRC. Should AEC apply at a later date for a change
to the STC to include another model listed on the same type certificate
data sheet, incorporating the same or similar novel or unusual design
feature, these special conditions would apply to that model as well.
Under standard practice, the effective date of final special
conditions would be 30 days after the date or publication in the
Federal Register; however, as the certification date for the Boeing
Model 777-200 series airplanes is imminent, the FAA finds that good
cause exists to make these special conditions effective upon issuance.
Conclusion
This action affects only certain novel or unusual design features
on the Boeing Model 777-200 series airplanes. It is not a rule of
general applicability, and it affects only the applicant which applied
to the FAA for approval of these features on the airplane.
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting and recordkeeping
requirements.
0
The authority citation for these special conditions is as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704.
The Special Conditions
0
Accordingly, pursuant to the authority delegated to me by the
Administrator, the following special conditions are issued as part of
the type certification basis for the Boeing Model 777-200 series
airplanes, modified by Aerocon Engineering Company.
1. Occupancy of the forward lower lobe crew rest compartment (CRC)
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 CRC. The maximum occupancy is ten in the CRC.
(a) There must be appropriate placard(s) displayed in a conspicuous
place at each entrance to the CRC 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 CRC;
(3) That occupancy is prohibited during taxi, take-off and landing;
(4) That smoking is prohibited in the CRC;
(5) That hazardous quantities of flammable fluids, explosives, or
other dangerous cargo are prohibited from the CRC.
(6) That stowage in the CRC must be limited to emergency equipment,
airplane-supplied equipment (e.g., bedding), and crew personal luggage;
cargo or passenger baggage is not allowed.
(b) There must be at least one ashtray located conspicuously on or
near the entry side of any entrance to the CRC.
(c) There must be a means to prevent passengers from entering the
compartment in the event of an emergency or when no flight attendant is
present.
[[Page 54574]]
(d) There must be a means for any door installed between the CRC
and passenger cabin to be opened quickly from inside the compartment,
even when crowding occurs at each side of the door.
(e) For all doors installed in the evacuation routes, there must be
a means to preclude anyone from being trapped inside the 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.
2. There must be at least two emergency evacuation routes, each of
which can be used by each occupant of the CRC to rapidly evacuate to
the main cabin. The exit door/hatch for each route must be able to be
closed for the main cabin after evacuation. In addition--
(a) The routes must be located with one at each end of the
compartment, or with two having sufficient separation within the
compartment and between the routes to minimize the possibility of an
event (either inside or outside of the CRC) rendering both routes
inoperative.
(b) The routes must be designed to minimize the possibility of
blockage, which might result from fire, mechanical or structural
failure, or persons standing on top of or against the escape route. If
an evacuation route utilizes an area where normal movement of
passengers occurs, it must be demonstrated that passengers would not
impede egress to the main deck. If a hatch is installed in an
evacuation route, the point at which the evacuation route terminates in
the passenger cabin should not be located where normal movement by
passengers or crew occurs (main aisle, cross aisle, passageway or
galley complex). If such a location cannot be avoided, special
consideration must be taken to ensure that the hatch or door can be
opened when a person, the weight of a ninety-fifth percentile male, is
standing on the hatch or door. The use of evacuation routes must not be
dependent on any powered device. If there is low headroom at or near an
evacuation route, provisions must be made to prevent or to protect
occupants (of the CRC) from head injury.
(c) Emergency evacuation procedures, including the emergency
evacuation of an incapacitated occupant from the CRC, must be
established. All of these procedures must be transmitted to all
operators for incorporation into their training programs and
appropriate operational manuals.
(d) There must be a limitation in the Airplane Flight Manual or
other suitable means requiring that crewmembers be trained in the use
of evacuation routes.
3. There must be a means for the evacuation of an incapacitated
person (representative of a 95th percentile male) from the CRC to the
passenger cabin floor. The evacuation must be demonstrated for all
evacuation routes. A flight attendant or other crewmember (a total of
one assistant within the CRC) may provide assistance in the evacuation.
Additional assistance may be provided by up to three persons in the
main passenger compartment. For evacuation routes having stairways, the
additional assistants may descend down to one half the elevation change
from the main deck to the lower deck compartment, or to the first
landing, whichever is higher.
4. The following signs and placards must be provided in the CRC:
(a) At least one exit sign, located near each exit, meeting the
requirements of Sec. 25.812(b)(1)(i) at Amendment 25-58, except that a
sign with reduced background area of no less than 5.3 square inches
(excluding the letters) may be utilized, provided that it is installed
such that the material surrounding the exit sign is light in color
(e.g., white, cream, light beige). 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;
(b) An appropriate placard located near each exit defining the
location and the operating instructions for each evacuation route;
(c) Placards must be readable from a distance of 30 inches under
emergency lighting conditions; and
(d) The exit handles and evacuation path operating instruction
placards must be illuminated to at least 160 micro lamberts 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 CRC lighting system, for emergency
illumination to be automatically provided for the CRC.
(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 for the occupants of
the CRC to locate and transfer 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 CRC to locate
a deployed oxygen mask.
6. There must be means for two-way voice communications between
crewmembers on the flightdeck and occupants of the CRC. There must also
be public address (PA) system microphones at each flight attendant seat
required to be near a floor level exit in the passenger cabin per Sec.
25.785(h) at Amendment 25-51. The PA system must allow two-way voice
communications between flight attendants and the occupants of the CRC,
except that one microphone may serve more than one exit provided the
proximity of the exits allows unassisted verbal communication between
seated flight attendants.
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 flightdeck and at each pair of required
floor level emergency exits to alert occupants of the CRC 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 for at least ten minutes after the shutdown
or failure of all engines and auxiliary power units (APU) or the
disconnection or failure of all power sources which are dependent on
the continued operation of the engines and APUs.
8. There must be a means, readily detectable by seated or standing
occupants of the CRC, which indicates when seat belts should be
fastened. In the event there are no seats, 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 must be
fastened when occupied. If compliance with any of the other
requirements of these special conditions is predicated on specific head
location, there must be a placard identifying the head position.
9. In lieu of the requirements specified in Sec. 25.1439(a) at
Amendment 25-38 that pertain to isolated compartments and to provide a
level of safety equivalent to that which is provided occupants of a
small isolated
[[Page 54575]]
galley, the following equipment must be provided in the CRC:
(a) At least one approved hand-held fire extinguisher appropriate
for the kinds of fires likely to occur;
(b) Two PBE devices approved to Technical Standard Order (TSO)-C116
or equivalent, suitable for fire fighting, or one PBE for each hand-
held fire extinguisher, whichever is greater; and
(c) One flashlight.
Note: Additional PBEs and fire extinguishers in specific
locations, (beyond the minimum numbers prescribed in Special
Condition No. 9) may be required as a result of any egress analysis
accomplished to satisfy Special Condition No. 2(a).
10. A smoke or fire detection system (or systems) must be provided
that monitors each occupiable area within the CRC, including those
areas partitioned by curtains. Flight tests must be conducted to show
compliance with this requirement. 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 CRC; and
(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 CRC must be designed such 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 fire fighting to have unrestricted access to the compartment. The
time for a crewmember on the main deck to react to the fire alarm, to
don the fire fighting equipment, and to gain access must not exceed the
time for the compartment to become smoke-filled, making it difficult to
locate the fire source.
12. There must be a means provided to exclude hazardous quantities
of smoke or extinguishing agent originating in the CRC from entering
any other compartment occupied by crewmembers or passengers. This means
must include the time periods during the evacuation of the CRC and, if
applicable, when accessing the CRC to manually fight a fire. Smoke
entering any other compartment occupied by crewmembers or passengers
when the access to the CRC is opened, during an emergency evacuation,
must dissipate within five minutes after the access to the CRC is
closed. Hazardous quantities of smoke may not enter any other
compartment occupied by crewmembers or passengers during subsequent
access to manually fight a fire in the CRC (the amount of smoke
entrained by a firefighter exiting the CRC through the access is not
considered hazardous). During the 1-minute smoke detection time,
penetration of a small quantity of smoke from the CRC into an occupied
area is acceptable. Flight tests must be conducted to show compliance
with this requirement.
If a built-in fire extinguishing system is used in lieu of manual
fire fighting, then 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 any fire occurring in the CRC,
considering the fire threat, volume of the compartment and the
ventilation rate.
13. There must be a supplemental oxygen system equivalent to that
provided for main deck passengers for each seat and berth in the CRC.
The system must provide an aural and visual warning to warn the
occupants of the CRC to don oxygen masks in the event of decompression.
The warning must activate before the cabin pressure altitude exceeds
15,000 feet. The aural warning must sound continuously for a minimum of
five minutes or until a reset push button in the CRC is depressed.
Procedures for crew rest occupants to follow in the event of
decompression must be established. These procedures must be transmitted
to the operators for incorporation into their training programs and
appropriate operational manuals.
14. The following requirements apply to CRCs that are divided into
several sections by the installation of curtains or partitions:
(a) To warn sleeping occupants, there must be an aural alert that
can be heard in each section of the CRC and that accompanies automatic
presentation of supplemental oxygen masks. A visual indicator that
occupants must don an oxygen mask is required in each section where
seats or berths are not installed. A minimum of two supplemental oxygen
masks is required for each seat or berth. There must also be a means by
which the oxygen masks can be manually deployed from the flightdeck.
(b) A placard is required adjacent to each curtain that visually
divides or separates, for privacy purposes, the CRC into small
sections. The placard must require that the curtain remains open when
the private section it creates is unoccupied.
(c) For each section of the CRC created by the installation of a
curtain, the following requirements of these special conditions must be
met both with the curtain open and with the curtain closed:
(1) Emergency illumination (Special Condition No. 5);
(2) Emergency alarm system (Special Condition No. 7);
(3) Seat belt fasten signal or return to seat signal as applicable
(Special Condition No. 8); and
(4) The smoke or fire detection system (Special Condition No. 10).
(d) Crew rest compartments visually divided to the extent that
evacuation could be affected must have exit signs that direct occupants
to the primary stairway exit. The exit signs must be provided in each
separate section of the CRC, and must meet the requirements of Sec.
25.812(b)(1)(i) at Amendment 25-58. An exit sign with reduced
background area as described in Special Condition No. 4(a) may be used
to meet this requirement.
(e) For sections within a CRC that are created by the installation
of a partition with a door separating the sections, the following
requirements of these special conditions must be met both with the door
open and with the door closed:
(1) There must be a secondary evacuation route from each section to
the main deck, or alternatively, it must be shown 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 short time duration, such as a
changing area or lavatory, is not required. However, removal of an
incapacitated occupant within this area 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) There must be exit signs in each section meeting the
requirements of Sec. 25.812(b)(1)(i) at Amendment 25-58 that direct
occupants to the primary stairway exit. An exit sign with reduced
background area as described in Special Condition No. 4(a) may be used
to meet this requirement.
(5) Special Conditions No. 5 (emergency illumination), No. 7
(emergency alarm system), No. 8 (fasten seat belt signal or return to
seat signal as applicable) and No. 10 (smoke or fire detection system)
must be met both with the door open and with the door closed.
(6) Special Conditions No. 6 (two-way voice communication) and No.
9
[[Page 54576]]
(emergency fire fighting and protective equipment) must be met
independently for each separate section except for lavatories or other
small areas that are not intended to be occupied for extended periods
of time.
15. Where a waste disposal receptacle is fitted, it must be
equipped with a built-in fire extinguisher designed to discharge
automatically upon occurrence of a fire in the receptacle.
16. Materials (including finishes or decorative surfaces applied to
the materials) must comply with the flammability requirements of Sec.
25.853 at Amendment 25-72. Mattresses must comply with the flammability
requirements of Sec. 25.853(b) and (c) at Amendment 25-72.
17. All lavatories within the CRC are required to meet the same
requirements as those for a lavatory installed on the main deck except
with regard to Special Condition No.10 for smoke detection.
18. When a CRC is installed or enclosed as a removable module in
part of a cargo compartment or is located directly adjacent to a cargo
compartment without an intervening cargo compartment wall, the
following apply:
(a) Any wall of the module (container) forming part of the boundary
of the reduced cargo compartment, subject to direct flame impingement
from a fire in the cargo compartment and including any interface item
between the module (container) and the airplane structure or systems,
must meet the applicable requirements of Sec. 25.855 at Amendment 25-
72.
(b) Means must be provided so that the fire protection level of the
cargo compartment meets the applicable requirements of Sec. 25.855 at
Amendment 25-72, Sec. 25.857 at Amendment 25-60 and Sec. 25.858 at
Amendment 25-54 when the module (container) is not installed.
(c) Use of each emergency evacuation route must not require
occupants of the CRC compartment to enter the cargo compartment in
order to return to the passenger compartment.
(d) The aural warning in Special Condition No. 7 must sound in the
CRC.
19. Means must be provided to prevent access into the Class C cargo
compartment during all airplane flight operations and to ensure that
the maintenance door is closed during all airplane flight operations.
20. All enclosed stowage compartments within the CRC that are not
limited to stowage of emergency equipment or airplane-supplied
equipment (e.g., bedding) must meet the design criteria given in the
table below. As indicated by the table below, this special condition
does not address enclosed stowage compartments greater than 200 ft \3\
in interior volume. 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.
----------------------------------------------------------------------------------------------------------------
Stowage compartment interior volumes
Fire protection features -------------------------------------------------------------------------
less than 25 ft\3\ 25 ft\3\ to 57 ft\3\ 57 ft\3\ to 200 ft\3\
----------------------------------------------------------------------------------------------------------------
Materials of Construction \1\......... Yes.................... Yes.................... Yes.
Detectors \2\......................... No..................... Yes.................... Yes.
Liner \3\............................. No..................... No..................... Yes.
Locating device \4\................... No..................... Yes.................... Yes.
----------------------------------------------------------------------------------------------------------------
\1\ Material 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 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\ 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 flightdeck within one minute after the start of a fire;
(b) An aural warning in the CRC; and
(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, then no liner would be required for enclosed stowage
compartments equal to or greater than 25 ft\3\ in interior volume 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 at Amendment 25-72
for a class B cargo compartment.
\4\ Location Detector Crew rest areas which contain enclosed stowage compartments exceeding 25 ft\3\ interior
volume and which are located away from one central location such as the entry to the crew rest area or a
common area within the crew rest area 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 September 8, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-15380 Filed 9-15-06; 8:45 am]
BILLING CODE 4910-13-P