Special Conditions: Boeing Model 787-8 Airplane; Reinforced Flightdeck Bulkhead, 40215-40216 [E7-14333]
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Rules and Regulations
Federal Register
Vol. 72, No. 141
Tuesday, July 24, 2007
This section of the FEDERAL REGISTER
contains regulatory documents having general
applicability and legal effect, most of which
are keyed to and codified in the Code of
Federal Regulations, which is published under
50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by
the Superintendent of Documents. Prices of
new books are listed in the first FEDERAL
REGISTER issue of each week.
Appendix II to Part 1201
[Amended]
2. Amend Appendix II to Part 1201 in
item 5. by removing ‘‘250 Montgomery
Street, Suite 400, 4th Floor, San
Francisco, California 941–3401,
Facsmile No.: (415) 705–2945,’’ and
adding, in its place ‘‘201 Mission Street,
Suite 2310, San Francisco, California
94105–1831 Facsmile No.: (415) 904–
0580,’’.
I
Dated: July 18, 2007.
Arlin Winefordner,
Acting Clerk of the Board.
[FR Doc. E7–14293 Filed 7–23–07; 8:45 am]
MERIT SYSTEMS PROTECTION
BOARD
5 CFR Part 1201
BILLING CODE 7400–01–P
Practices and Procedures
AGENCY:
DEPARTMENT OF TRANSPORTATION
Merit Systems Protection
Board.
ACTION:
Federal Aviation Administration
Final rule.
The Merit Systems Protection
Board (MSPB or the Board) is amending
its rules of practice and procedure in
this part to reflect the relocation of its
Western Regional Office.
EFFECTIVE DATE: July 27, 2007.
FOR FURTHER INFORMATION CONTACT:
Matthew Shannon, Acting Clerk of the
Board, (202) 653–7200. The Board is
publishing this rule as a final rule
pursuant to 5 U.S.C. 1204(h).
SUPPLEMENTARY INFORMATION: On July
27, 2007, the Board relocates its Western
Regional Office from 250 Montgomery
Street, Suite 400, 4th Floor, San
Francisco, California 94105–3401, to
201 Mission Street, Suite 2310, San
Francisco, California 94105–1831.
Appendix II of this part is amended to
show the new address. The Western
Regional Office telephone number
changes to (415) 904–6772 and the
facsimile number is changes to (415)
904–0580.
SUMMARY:
List of Subjects in 5 CFR Part 1201
Administrative practice and
procedure, Civil rights, Government
employees.
Accordingly, the Board amends 5 CFR
part 1201 as follows:
pwalker on PROD1PC71 with RULES
I
PART 1201—PRACTICES AND
PROCEDURES
1. The authority citation for part 1201
continues to read as follows:
I
Authority: 5 U.S.C. 1204 and 7701, unless
otherwise noted.
VerDate Aug<31>2005
18:16 Jul 23, 2007
Jkt 211001
14 CFR Part 25
[Docket No. NM372 Special Conditions No.
25–355–SC]
Special Conditions: Boeing Model 787–
8 Airplane; Reinforced Flightdeck
Bulkhead
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions.
AGENCY:
SUMMARY: These special conditions are
issued for the Boeing Model 787–8
airplane. This airplane will have novel
or unusual design features when
compared to the state of technology
envisioned in the airworthiness
standards for transport category
airplanes. The Boeing Model 787–8
airplanes will have a flightdeck
bulkhead incorporating ballistic-and
intrusion-resistant features. While the
regulations include standards for
ballistic-and intrusion-resistant
flightdeck doors, they do not yet
incorporate the same standards for these
features in the bulkhead. Therefore,
special conditions are needed to address
these design features. 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 standards. Additional
special conditions will be issued for
other novel or unusual design features
of the Boeing Model 787–8 airplanes.
EFFECTIVE DATE: August 23, 2007.
FOR FURTHER INFORMATION CONTACT: Jeff
Gardlin, FAA, Airframe/Cabin Safety,
PO 00000
Frm 00001
Fmt 4700
Sfmt 4700
ANM–115, Transport Airplane
Directorate, Aircraft Certification
Service, 1601 Lind Avenue, SW.,
Renton, Washington 98057–3356;
telephone (425) 227–2136; facsimile
(425) 227–1320.
SUPPLEMENTARY INFORMATION:
Background
On March 28, 2003, Boeing applied
for an FAA type certificate for its new
Boeing Model 787–8 passenger airplane.
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 14 Code of
Federal Regulations (CFR) 21.17, Boeing
must show that Boeing Model 787–8
airplanes (hereafter referred to as ‘‘the
787’’) meet the applicable provisions of
14 CFR part 25, as amended by
Amendments 25–1 through 25–117,
except §§ 25.809(a) and 25.812, which
will remain at Amendment 25–115. If
the Administrator finds that the
applicable airworthiness regulations do
not contain adequate or appropriate
safety standards for the 787 because of
a novel or unusual design feature,
special conditions are prescribed under
provisions of 14 CFR 21.16.
In addition to 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 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 § 11.19, under § 11.38 and
they become part of the type
certification basis under § 21.17(a)(2).
Special conditions are initially
applicable to the model for which they
are issued. Should the type certificate
for that model be amended later to
include any other model that
incorporates the same or similar novel
or unusual design feature, the special
conditions would also apply to the other
model under § 21.101.
Novel or Unusual Design Features
The 787 will incorporate a number of
novel or unusual design features.
E:\FR\FM\24JYR1.SGM
24JYR1
40216
Federal Register / Vol. 72, No. 141 / Tuesday, July 24, 2007 / Rules and Regulations
pwalker on PROD1PC71 with RULES
Because of rapid improvements in
airplane technology, the applicable
airworthiness regulations do not contain
adequate or appropriate safety standards
for these design features. These special
conditions for the 787 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.
On January 15, 2002, the FAA issued
14 CFR 25.795(a) (Amendment 25–106),
which specifies that the flightdeck door
of a transport airplane be designed to
resist forcible intrusion by unauthorized
persons and penetration by small arms
fire and fragmentation devices. At the
time it was written, the regulation was
limited to the flightdeck door to
expedite a rapid retrofit of the existing
airplanes required by operating rules to
have a flightdeck door.
In addition to a reinforced flightdeck
door, the 787 will have a flightdeck
bulkhead which is reinforced to resist
intrusion and ballistic penetration. The
regulations do not adequately address
the certification requirements for such a
bulkhead, and appropriate certification
standards are necessary. These special
conditions require that the reinforced
flightdeck bulkhead meet the same
standards as those specified in
§ 25.795(a) for flightdeck doors. These
special conditions contain the minimum
standards that the Administrator
considers necessary to ensure that safety
standards are maintained after the
aircraft enters into service.
On December 21, 2006, the FAA
issued a notice of proposed rulemaking
that proposes amending § 25.795(a) to
require that a flightdeck bulkhead—and
any other accessible barrier separating
the flightcrew compartment from
occupied areas—also be designed to
resist intrusion or penetration. The
methods of compliance described in the
preamble of that notice and associated
draft advisory material could be used to
show compliance with these special
conditions. For the 787, the reinforced
bulkhead may be comprised of
components such as the walls of
adjacent lavatories, galleys, or crew rest
areas. Those components are covered by
these special conditions.
Discussion of Comments
Notice of Proposed Special
Conditions No. 25–07–08–SC for the
787 was published in the Federal
Register on April 12, 2007 (72 FR
18412). One comment was received,
from Air Line Pilots Association,
International (ALPA).
ALPA Comment: ALPA recommended
that the requirements of these special
VerDate Aug<31>2005
17:17 Jul 23, 2007
Jkt 211001
conditions apply to future versions of
the 787, including possible freighter
configurations.
FAA Response: These special
conditions apply to airplanes that
incorporate a reinforced bulkhead. They
are not limited to any particular type of
operation, nor do they impose
operational requirements. Thus, if a
future freighter version did incorporate
a reinforced bulkhead, these special
conditions would apply. These special
conditions are adopted as proposed.
Issued in Renton, Washington, on July 12,
2007.
Stephen P. Boyd,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E7–14333 Filed 7–23–07; 8:45 am]
Applicability
[Docket No. FAA–2007–28749; Directorate
Identifier 2007–NM–079–AD; Amendment
39–15134; AD 2007–15–05]
As discussed above, these 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 on the same type
certificate incorporating the same novel
or unusual design features, these 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:
I
Authority: 49 U.S.C. 106(g), 40113, 44701,
44702, 44704.
The Special Conditions
Accordingly, pursuant to the authority
delegated to me by the Administrator,
the following special conditions are
issued as part of the type certification
basis for the Boeing Model 787–8
airplane.
In addition to the requirements of 14
CFR 25.795(a) governing protection of
the flightdeck door, the following
special conditions apply.
I
The reinforced bulkhead, including
components that comprise the bulkhead,
separating the flightcrew compartment from
occupied areas must be designed to meet the
following standards:
It must resist forcible intrusion by
unauthorized persons and be capable of
withstanding impacts of 300 Joules (221.3
foot-pounds) at critical locations on the
bulkhead as well as a 1113 Newton (250
pound) constant tensile load on accessible
handholds.
It must resist penetration by small arms fire
and fragmentation devices to a level
equivalent to level IIIa of the National
Institute of Justice Standard (NIJ) 0101.04.
PO 00000
Frm 00002
Fmt 4700
Sfmt 4700
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
RIN 2120–AA64
Airworthiness Directives; McDonnell
Douglas Model DC–10–10 and DC–10–
10F Airplanes, Model DC–10–15
Airplanes, Model DC–10–30 and DC–
10–30F (KC–10A and KDC–10)
Airplanes, Model DC–10–40 and DC–
10–40F Airplanes, Model MD–10–10F
and MD–10–30F Airplanes, and Model
MD–11 and MD–11F Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
transport category airplanes identified
above. This AD requires an inspection
to determine if a certain fuel pump
housing electrical connector is installed.
This AD also requires a revision to the
FAA-approved airplane flight manual
(AFM) to advise the flightcrew of the
appropriate procedures for disabling
certain fuel pump electrical circuits
following failure of a fuel pump housing
electrical connector if applicable. This
AD also requires the deactivation of
certain fuel tanks or fuel pumps and the
installation of placards if applicable.
This AD allows the optional
replacement of the fuel pump housing
electrical connectors with new,
improved parts, which would terminate
the AFM revisions, deactivation of
certain fuel tanks and fuel pumps, and
placard installation. This AD results
from a report of two failures of the fuel
pump housing electrical connector. We
are issuing this AD to prevent continued
arcing following a short circuit of the
fuel pump housing electrical connector,
which could damage the conduit that
protects the power lead inside the fuel
tank; this condition could create an
ignition source inside the fuel tank,
which, in combination with flammable
fuel vapors, could result in a fuel tank
E:\FR\FM\24JYR1.SGM
24JYR1
]]>Agencies
[Federal Register Volume 72, Number 141 (Tuesday, July 24, 2007)]
[Rules and Regulations]
[Pages 40215-40216]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-14333]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. NM372 Special Conditions No. 25-355-SC]
Special Conditions: Boeing Model 787-8 Airplane; Reinforced
Flightdeck Bulkhead
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for the Boeing Model 787-8
airplane. This airplane will have novel or unusual design features when
compared to the state of technology envisioned in the airworthiness
standards for transport category airplanes. The Boeing Model 787-8
airplanes will have a flightdeck bulkhead incorporating ballistic-and
intrusion-resistant features. While the regulations include standards
for ballistic-and intrusion-resistant flightdeck doors, they do not yet
incorporate the same standards for these features in the bulkhead.
Therefore, special conditions are needed to address these design
features. 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
standards. Additional special conditions will be issued for other novel
or unusual design features of the Boeing Model 787-8 airplanes.
EFFECTIVE DATE: August 23, 2007.
FOR FURTHER INFORMATION CONTACT: Jeff Gardlin, FAA, Airframe/Cabin
Safety, ANM-115, Transport Airplane Directorate, Aircraft Certification
Service, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-2136; facsimile (425) 227-1320.
SUPPLEMENTARY INFORMATION:
Background
On March 28, 2003, Boeing applied for an FAA type certificate for
its new Boeing Model 787-8 passenger airplane. 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 14 Code of Federal Regulations (CFR) 21.17,
Boeing must show that Boeing Model 787-8 airplanes (hereafter referred
to as ``the 787'') meet the applicable provisions of 14 CFR part 25, as
amended by Amendments 25-1 through 25-117, except Sec. Sec. 25.809(a)
and 25.812, which will remain at Amendment 25-115. If the Administrator
finds that the applicable airworthiness regulations do not contain
adequate or appropriate safety standards for the 787 because of a novel
or unusual design feature, special conditions are prescribed under
provisions of 14 CFR 21.16.
In addition to 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 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 Sec. 11.19, under
Sec. 11.38 and they become part of the type certification basis under
Sec. 21.17(a)(2).
Special conditions are initially applicable to the 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, the special conditions would also
apply to the other model under Sec. 21.101.
Novel or Unusual Design Features
The 787 will incorporate a number of novel or unusual design
features.
[[Page 40216]]
Because of rapid improvements in airplane technology, the applicable
airworthiness regulations do not contain adequate or appropriate safety
standards for these design features. These special conditions for the
787 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.
On January 15, 2002, the FAA issued 14 CFR 25.795(a) (Amendment 25-
106), which specifies that the flightdeck door of a transport airplane
be designed to resist forcible intrusion by unauthorized persons and
penetration by small arms fire and fragmentation devices. At the time
it was written, the regulation was limited to the flightdeck door to
expedite a rapid retrofit of the existing airplanes required by
operating rules to have a flightdeck door.
In addition to a reinforced flightdeck door, the 787 will have a
flightdeck bulkhead which is reinforced to resist intrusion and
ballistic penetration. The regulations do not adequately address the
certification requirements for such a bulkhead, and appropriate
certification standards are necessary. These special conditions require
that the reinforced flightdeck bulkhead meet the same standards as
those specified in Sec. 25.795(a) for flightdeck doors. These special
conditions contain the minimum standards that the Administrator
considers necessary to ensure that safety standards are maintained
after the aircraft enters into service.
On December 21, 2006, the FAA issued a notice of proposed
rulemaking that proposes amending Sec. 25.795(a) to require that a
flightdeck bulkhead--and any other accessible barrier separating the
flightcrew compartment from occupied areas--also be designed to resist
intrusion or penetration. The methods of compliance described in the
preamble of that notice and associated draft advisory material could be
used to show compliance with these special conditions. For the 787, the
reinforced bulkhead may be comprised of components such as the walls of
adjacent lavatories, galleys, or crew rest areas. Those components are
covered by these special conditions.
Discussion of Comments
Notice of Proposed Special Conditions No. 25-07-08-SC for the 787
was published in the Federal Register on April 12, 2007 (72 FR 18412).
One comment was received, from Air Line Pilots Association,
International (ALPA).
ALPA Comment: ALPA recommended that the requirements of these
special conditions apply to future versions of the 787, including
possible freighter configurations.
FAA Response: These special conditions apply to airplanes that
incorporate a reinforced bulkhead. They are not limited to any
particular type of operation, nor do they impose operational
requirements. Thus, if a future freighter version did incorporate a
reinforced bulkhead, these special conditions would apply. These
special conditions are adopted as proposed.
Applicability
As discussed above, these 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 on the same type certificate
incorporating the same novel or unusual design features, these 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.
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 787-8 airplane.
In addition to the requirements of 14 CFR 25.795(a) governing
protection of the flightdeck door, the following special conditions
apply.
The reinforced bulkhead, including components that comprise the
bulkhead, separating the flightcrew compartment from occupied areas
must be designed to meet the following standards:
It must resist forcible intrusion by unauthorized persons and be
capable of withstanding impacts of 300 Joules (221.3 foot-pounds) at
critical locations on the bulkhead as well as a 1113 Newton (250
pound) constant tensile load on accessible handholds.
It must resist penetration by small arms fire and fragmentation
devices to a level equivalent to level IIIa of the National
Institute of Justice Standard (NIJ) 0101.04.
Issued in Renton, Washington, on July 12, 2007.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-14333 Filed 7-23-07; 8:45 am]
BILLING CODE 4910-13-P
