[Federal Register Volume 76, Number 196 (Tuesday, October 11, 2011)]
[Rules and Regulations]
[Pages 62603-62604]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-25504]
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Rules and Regulations
Federal Register
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Federal Register / Vol. 76, No. 196 / Tuesday, October 11, 2011 /
Rules and Regulations
[[Page 62603]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM465; Special Conditions No. 25-446-SC]
Special Conditions: The Boeing Company, Model 747-8; Upper Deck
Occupancy
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; request for comments.
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SUMMARY: These special conditions are issued for the Boeing Model 747-8
airplane. These airplanes will have novel or unusual design features
associated with upper deck occupancy. The applicable airworthiness
regulations do not contain adequate or appropriate safety standards for
this design feature. These special conditions contain the additional
safety standards that the Administrator considers necessary to
establish a level of safety equivalent to that established by the
existing airworthiness standards.
DATES: The effective date of these special conditions is September 28,
2011. We must receive your comments by November 25, 2011.
ADDRESSES: You must mail two copies of your comments to: Federal
Aviation Administration, Transport Airplane Directorate, Attn: Rules
Docket (ANM-113), Docket No. NM465, 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. NM465. You can inspect comments in the Rules Docket
weekdays, except Federal holidays, between 7:30 a.m. and 4:00 p.m.
FOR FURTHER INFORMATION CONTACT: Jayson Claar, FAA, Airframe and 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) 227-1232.
SUPPLEMENTARY INFORMATION: The FAA has determined that notice of, and
opportunity for prior public comment on, these special conditions are
impracticable because these procedures would significantly delay
issuance of the design approval and thus delivery of the affected
aircraft. In addition, the substance of these special conditions has
been subject to the public comment process in several prior instances
with no substantive comments received. The FAA therefore finds that
good cause exists for making these special conditions effective upon
issuance.
Comments Invited
We invite interested people to take part in this rulemaking by
sending written comments, data, or views. The most helpful comments
reference a specific portion of the special conditions, explain the
reason for any recommended change, and include supporting data. We ask
that you send us two copies of written comments.
We will file in the docket all comments we receive, as well as a
report summarizing each substantive public contact with FAA personnel
about these special conditions. You can inspect the docket before and
after the comment closing date. If you wish to review the docket in
person, go to the address in the ADDRESSES section of this preamble
between 7:30 a.m. and 4 p.m., Monday through Friday, except Federal
holidays.
We will consider all comments we receive by the closing date for
comments. We may change these special conditions based on the comments
we receive.
If you want us to acknowledge receipt of your comments on these
special conditions, 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 November 4, 2005, The Boeing Company applied for an amendment to
Type Certificate Number A20WE to include the new Model 747-8 passenger
airplane. The Model 747-8 is a derivative of the 747-400. The Model
747-8 is a four-engine jet transport airplane that will have a maximum
takeoff weight of 975,000 pounds, new General Electric GEnx-2B67
engines, and the capacity to carry 605 passengers.
The Model 747-8 design offers seating capacity on two separate
decks: The main deck with a maximum passenger capacity of 495 and the
upper deck with a maximum passenger capacity of 110. Occupants can move
between decks via a staircase located near door 2 on the main deck of
the airplane in the forward part of the cabin. The staircase is located
in the aft end of the upper deck passenger compartment. The regulations
do not adequately address a passenger airplane with separate decks for
passenger occupancy, thus the FAA considers this to be a novel design,
and special conditions are required.
Type Certification Basis
Under the provisions of Title 14 Code of Federal Regulations (14
CFR) 21.101, Boeing must show that the Model 747-8 (hereafter referred
to as the 747-8) meets the applicable provisions of 14 CFR part 25, as
amended by Amendments 25-1 through 25-117, except for earlier
amendments as agreed upon by the FAA. These regulations will be
incorporated into Type Certificate No. A20WE after type certification
approval of the 747-8.
If the Administrator finds that the applicable airworthiness
regulations (i.e., part 25) do not contain adequate or appropriate
safety standards for the 747-8 because of a novel or unusual design
feature, special conditions are prescribed under the provisions of
Sec. 21.16.
Special conditions are initially applicable to the 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, or should any other model already included on
the same type certificate be modified to incorporate the same novel or
unusual design features, these special conditions would also apply to
the other model.
In addition to the applicable airworthiness regulations and special
conditions, the 747-8 must comply with the fuel vent and exhaust
emission requirements of 14 CFR part 34 and the
[[Page 62604]]
noise certification requirements of 14 CFR part 36.
The FAA issues special conditions, as defined in Sec. 11.19, in
accordance with Sec. 11.38, and they become part of the type-
certification basis under Sec. 21.101.
Novel or Unusual Design Features
The Boeing Model 747-8 will incorporate the following novel or
unusual design features: seating capacity on two separate decks, a main
deck with a maximum passenger capacity of 495 and an upper deck with a
maximum passenger capacity of 110, and a staircase to facilitate
occupant movement between the decks.
Discussion
The regulations governing the certification of the 747-8 do not
adequately address the certification requirements for a two-deck
passenger airplane. The Airbus A380-800 and all of the earlier Boeing
747 passenger airplane models were certified with seating capacity on
two separate decks. When the seating capacity of the upper deck of the
Boeing 747 exceeded 24 passengers, the FAA issued Special Condition No.
25-61-NW-1 for a maximum seating capacity of 32 passengers on the upper
deck for take-off and landing. A second set of special conditions,
Special Condition No. 25-71-NW-3, was issued to include airplanes up to
a maximum seating capacity of 45 passengers on the upper deck for take-
off and landing. The second set of special conditions was modified to
address airplanes with a maximum seating capacity of 110 passengers on
the upper deck for take-off and landing. Special Conditions No. 25-326-
SC for the Airbus A380-800 allowed a seating capacity on two separate
decks: The main deck with a maximum passenger capacity of 542 and the
upper deck with a maximum passenger capacity of 308. Although these
previously issued special conditions provided a starting point for
developing the 747-8 special conditions, the 747-8 special conditions
are specific to the unique aspects of this airplane's design.
The upper deck of the 747-8 has one pair of exits at station 690,
which is located approximately in the forward one-third of the upper
deck passenger cabin. The stairway between the main deck and the upper
deck is located in the aft end of the upper deck passenger compartment.
Depending on the interior arrangement of the upper deck, access to the
pair of exits on the upper deck can be reduced. This pair of exits
could be rated as Type A, Type C, or Type I exits. These exit
configurations and stairway evacuation route are not addressed in the
regulations.
Current regulations do not address the design of the emergency
lighting system(s) for two-deck airplanes including the separation of
the systems between the two decks and the operational requirements of
the systems when considering a single transverse vertical separation of
the fuselage during a crash landing.
Additionally, with a two-deck airplane, there are concerns with
communications between the two decks and between each deck and the
flight deck.
The FAA issued a set of special conditions for the 747-8, Special
Conditions No. 25-430-SC, specifying the design requirements of the
stairway connecting the main and upper decks, including structural
design, placement within the airplane, lighting, and signage.
The following special conditions address additional elements to
support evacuation between decks of the 747-8 airplane in an in-flight
emergency.
Applicability
As discussed above, these special conditions are applicable to the
Model 747-8. 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, the special conditions would apply to that
model as well.
Conclusion
This action affects only certain novel or unusual design features
on Model 747-8 airplanes. It is not a rule of general applicability.
The substance of these special conditions has been subjected to the
notice and comment period in several prior instances and has been
derived without substantive change from those previously issued. It is
unlikely that prior public comment would result in a significant change
from the substance contained herein. Therefore, because a delay would
significantly affect the certification of the airplane, which is
imminent, the FAA has determined that prior public notice and comment
are unnecessary and impracticable, and good cause exists for adopting
these special conditions upon issuance. The FAA is requesting comments
to allow interested persons to submit views that may not have been
submitted in response to the prior opportunities for comment described
above.
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 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 Boeing Model 747-8 airplanes.
1. Passenger Emergency Exits
(a) The upper deck passenger occupancy is limited to 110 with one
pair of Type A exits. If, due to the interior arrangement, the upper
deck exits are rated as Type I, the upper deck passenger occupancy is
limited to 45. If, due to the interior arrangement, the upper deck
exits are rated as Type C, the upper deck passenger occupancy is
limited to 55. The centerline of these exits is located at station 690
on the upper deck.
2. Emergency Lighting System
(a) The upper deck emergency lighting system power supplies must be
independent of the main deck emergency lighting system power supplies.
(b) The upper deck emergency lighting system must be designed so
that, after any single transverse vertical separation of the fuselage
during a crash landing, not more than 25 percent of all required
electrically illuminated emergency lights in the upper deck are
rendered inoperative, in addition to the upper deck emergency lights
that are directly damaged by separation.
3. Inter-deck Communication
(a) An intercom and a two-way alerting means between passenger
decks and between each passenger deck and the flightdeck must be
provided that meet the following requirements:
(1) They must remain operable in the event of the loss of the main
power supply.
(2) They must be capable of providing crewmembers on all decks an
immediate indication of emergency situation on any deck.
Issued in Renton, Washington, on September 28, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-25504 Filed 10-7-11; 8:45 am]
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