Review of Existing Regulations, 34999-35006 [E7-12285]
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Federal Register / Vol. 72, No. 122 / Tuesday, June 26, 2007 / Rules and Regulations
27. The authority citation for part 37
continues to read as follows:
I
Authority: 5 U.S.C. 301 and 10 U.S.C. 113.
28. Section 37.130 is amended by
revising paragraph (b)(1) to read as
follows:
I
§ 37.130 Which other parts of the DoD
Grant and Agreement Regulations apply to
TIAs?
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(b) * * *
(1) Part 1125 (2 CFR part 1125) on
nonprocurement debarment and
suspension, which applies because it
covers nonprocurement instruments in
general;
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I 29. Appendix D to part 37 is amended
by revising the introductory text and
paragraphs A, B, B.1, B.3, and B.5 to
read as follows:
Appendix D to Part 37—What Common
National Policy Requirements May
Apply and Need To Be Included in
TIAs?
Whether your TIA is a cooperative
agreement or another type of assistance
transaction, as discussed in Appendix B to
this part, the terms and conditions of the
agreement must provide for recipients’
compliance with applicable Federal statutes
and regulations. This appendix lists some of
the more common requirements to aid you in
identifying ones that apply to your TIA. The
list is not intended to be all-inclusive,
however, and you may need to consult legal
counsel to verify whether there are others
that apply in your situation (e.g., due to a
provision in the appropriations act for the
specific funds that you are using or due to
a statute or rule that applies to a particular
program or type of activity).
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A. Certifications
One requirement that applies to all TIAs
currently requires you to obtain a
certification at the time of proposal. That
requirement is in a Governmentwide
common rule about lobbying prohibitions,
which is implemented by the DoD at 32 CFR
part 28. The prohibitions apply to all
financial assistance. Appendix A to 32 CFR
part 22 includes a sample provision that you
may use, to have proposers incorporate the
certification by reference into their proposals.
B. Assurances That Apply to All TIAs
DoD policy is to use a certification, as
described in the preceding paragraph, only
for a national policy requirement that
specifically requires one. The usual approach
to communicating other national policy
requirements to recipients is to incorporate
them as award terms or conditions, or
assurances. Appendix B to 32 CFR part 22
lists national policy requirements that
commonly apply to grants and cooperative
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agreements. It also has suggested language for
assurances to incorporate the requirements in
award documents. Of those requirements, the
following six apply to all TIAs:
1. Requirements concerning debarment and
suspension in the OMB guidance in 2 CFR
part 180, as implemented by the DoD at 2
CFR part 1125. The requirements apply to all
nonprocurement transactions.
DEPARTMENT OF TRANSPORTATION
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PART 37—TECHNOLOGY
INVESTMENT AGREEMENTS
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34999
AGENCY:
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3. Prohibitions on discrimination on the
basis of race, color, or national origin in Title
VI of the Civil Rights Act of 1964 (42 U.S.C.
2000d, et seq.). These apply to all financial
assistance. They require recipients to flow
down the prohibitions to any subrecipients
performing a part of the substantive research
program (as opposed to suppliers from whom
recipients purchase goods or services). For
further information, see item a. under the
heading ‘‘Nondiscrimination’’ in Appendix B
to 32 CFR part 22.
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5. Prohibitions on discrimination on the
basis of handicap, in section 504 of the
Rehabilitation Act of 1973 (29 U.S.C. 794).
They apply to all financial assistance and
require flow down to subrecipients. For
further information, see item e.1. under the
heading ‘‘Nondiscrimination’’ in Appendix B
to 32 CFR part 22.
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30. Appendix E to part 37 is amended
by revising paragraph B.2 to read as
follows:
I
Appendix E to Part 37—What
Provisions May a Participant Need To
Include When Purchasing Goods or
Services Under a TIA?
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B. * * *
2. Debarment and suspension. A contract
award with an amount expected to equal or
exceed $25,000 and certain other contract
awards (see 2 CFR 1125.220, which
implements OMB guidance in 2 CFR
180.220) shall not be made to parties listed
on the Governmentwide Excluded Parties
List System, in accordance with the DoD
adoption at 2 CFR part 1125 of the OMB
guidance implementing E.O.s 12549 (3 CFR,
1986 Comp., p. 189) and 12689 (3 CFR, 1989
Comp., p. 235), ‘‘Debarment and
Suspension.’’ The Excluded Parties List
System accessible on the Internet at
www.epls.gov contains the names of parties
debarred, suspended, or otherwise excluded
by agencies, as well as parties declared
ineligible under statutory or regulatory
authority other than E.O. 12549.
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Dated: June 18, 2007.
L.M. Bynum,
Alternate OSD Federal Register Liaison
Officer, Department of Defense.
[FR Doc. 07–3086 Filed 6–25–07; 8:45 am]
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Federal Aviation Administration
14 CFR Chapters I and III
[Docket No.: FAA–2004–17168]
Review of Existing Regulations
Federal Aviation
Administration (FAA), DOT.
ACTION: Disposition of comments on
existing regulations.
SUMMARY: The FAA is notifying the
public of the outcome of our periodic
review of existing regulations. This
notice summarizes the public comments
we received and our responses to them.
This action is part of our effort to make
our regulatory program more effective
and less burdensome.
FOR FURTHER INFORMATION CONTACT:
Patrick W. Boyd, Office of Rulemaking,
ARM–23, Federal Aviation
Administration, 800 Independence
Avenue, SW., Washington, DC 20591;
telephone (202) 267–7320.
SUPPLEMENTARY INFORMATION:
Background
Under section 5 of Executive Order
12866, Regulatory Planning and Review,
each agency must develop a program to
periodically review its existing
regulations to determine if they should
be changed or eliminated (58 FR 51735,
October 4, 1993). The purposes of the
review are to make the agency’s
regulatory program more effective in
achieving the regulatory objectives and
less burdensome. The FAA conducts its
review on a three-year cycle.
On February 25, 2004, we published
a notice in the Federal Register asking
the public to tell us which regulations
we should amend, remove, or simplify
(69 FR 8575). The notice stated that we
would consider the comments and
adjust our regulatory priorities
consistent with our statutory
responsibilities. The notice also stated
we would publish a summary of the
comments and an explanation of how
we would act on them.
Summary of Comments
In response to the February 2004
notice, we received 97 comments from
30 different commenters. For
comparison, we received 476 comments
during the previous review and 82
comments the time before that. We
received comments from citizens,
private pilots, commercial pilots, and
representatives of interest groups and
commercial entities. The interest groups
that filed comments include the Air
Transport Association, the Allied Pilots
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Association, the Experimental Aircraft
Association, the National Air Carrier
Association, and the Regional Airline
Association. The commercial entities
that filed comments include ABX Air,
Inc.; Alteon Training; Apex Aviation
Corporation; Boeing Commercial
Airplanes; General Electric Aircraft
Engines; Honeywell Engines, Systems
and Services; Morris Research, Inc.; the
Orange County (Ca.) Flight Center;
Southwest Airlines; and World Airways.
Our February 2004 request for
comments asked that commenters
identify three regulations that we
should amend or remove. This is to
enable us to focus on commenters’ high
priority concerns. Most commenters
limited themselves to three or fewer
comments. However, the Air Transport
Association filed 21 comments, while
Southwest Airlines and the National Air
Carrier Association filed 5 each.
Our February 2004 request for
comments also asked the public to
direct comments about 14 CFR parts 125
and 135 to the working group that is
conducting a separate review of those
parts to avoid any duplication of effort.
We appreciate that commenters
complied with this request. For the first
time, the regulatory review included 14
CFR Chapter III, the regulations
governing commercial space
transportation. However, we did not
receive any comments on these
regulations.
Response to Comments
We have organized the comments in
four groups:
• Comments that we have already
addressed,
• Comments that we are addressing,
• Comments that we will address,
and
• Comments that we will not address
at this time.
Readers should note that, in this
document, when we say we ‘‘are
addressing’’ a comment, we do not
mean we will necessarily address a
comment exactly as proposed by a
commenter. We reserve the right to
‘‘address’’ comments in a way that is in
accord with our statutory authority,
balances competing interests, and
fosters a safe and efficient civil aviation
system. We have carefully considered
issues raised by commenters and are
taking, or will take, action to address
those issues, as discussed below, but we
do not guarantee the outcome of our
action will always correspond to the
commenters’ views. With regard to
comments that we will not address now,
readers should note that, while we
disagree with some of the comments, in
other cases we simply cannot take
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action now due to competing priorities
and limited resources.
Comments That We Have Already
Addressed
We have already addressed 23 of the
97 comments. One individual
commenter asked us to amend the
medical examination requirement to
require pilots to report only new
medical examinations that occurred
after the last application date. Response:
We have already included this in the
instructions printed on the form.
Southwest Airlines asked us to
restructure the environmental
assessment process for routine airspace
and airport expansion. Response: On
June 8, 2004, we issued revised FAA
Order No. 1050.1E, entitled,
‘‘Environmental Impacts: Policies and
Procedures.’’ The order establishes a
categorical exclusion from National
Environmental Policy Act requirements
for these changes.
The Air Transport Association asked
that, before undertaking new regulatory
reviews, we conduct a thorough analysis
of the accomplishments of the previous
review. Response: We already do this as
part of the review of existing regulations
and through the reviews conducted
under section 610 of the Regulatory
Flexibility Act.
The Air Transport Association also
asked that the FAA conduct a rigorous
evaluation of the need and impact of
every proposed regulation. Response:
Existing laws and Executive Orders
already require this. For example, the
National Environmental Policy Act
requires analysis of the environmental
impact of Federal actions, and Executive
Order 12866, Regulatory Review,
requires analysis of the costs and
benefits of proposed regulatory actions.
An individual commenter asked that
the FAA control air pollution, aircraft
noise, and crashes and prevent pilots
who are under the influence of illegal
substances from operating aircraft.
Response: We already have regulations
in place for these purposes, including
14 CFR part 34 (air pollution), part 36
(noise), and part 61 (drug and alcohol
testing).
An individual commenter asked that
we allow general aviation operations at
the Ronald Reagan Washington National
Airport. Response: While the airport
was closed to general aviation as part of
the security measures adopted in the
aftermath of the terrorist attacks on
September 11, 2001, the Transportation
Security Administration (TSA) has since
reopened the airport to general aviation
operations that meet specific security
criteria (70 FR 41585, July 19, 2005).
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ABX Air recommended removing
from 14 CFR part 39 airworthiness
directive 91–08–51, amendment 39–
7031. This amendment requires certain
actions for aircraft equipped with a
Honeywell flight management system
that had a navigational database. The
AD became effective on June 24, 1991
and had a compliance period of 72
hours. Response: We agree with the
commenter and withdrew AD 91–08–51
on October 5, 2005.
We received four comments on 14
CFR 91.205(b)(12) and 121.353 asking
us to require pyrotechnic signaling
devices only for aircraft used in
extended over-water operations.
Response: On December 27, 2004, we
published a final rule that removes the
requirement for a pyrotechnic signaling
device for aircraft operated for hire over
water and beyond power-off gliding
distance from shore for air carriers
operating under Part 121 unless it is
part of a required life raft. All other
operators will continue to be required to
have onboard one pyrotechnic signaling
device if they operate aircraft for hire
over water and beyond power-off
gliding distance from shore (69 FR
77596).
World Airways asked us to amend 14
CFR 121.311(e)(2) to allow certain
passengers the ability to keep their seats
reclined if they do not obstruct others’
access to the aisle or emergency exits.
Response: Paragraph (e)(2) is an
exception to the requirement in
paragraph (e) that no certificate holder
may take off or land an airplane unless
each passenger seat back is in the
upright position. Paragraph (e)(2) states
that paragraph (e) does not apply to
seats on which cargo or persons who are
unable to sit erect for a medical reason
are carried in accordance with
procedures in the certificate holder’s
manual if the seat back does not
obstruct any passenger’s access to the
aisle or to any emergency exit. Thus, we
see no need to amend the regulation
since it already allows the flexibility the
commenter is seeking.
Three commenters, including World
Airways, the National Air Carrier
Association and the Air Transport
Association, filed four comments on the
topic of supplemental oxygen.
Specifically, they requested we change
14 CFR 121.333(c)(3) and 91. 211(b)(2)
to allow for a quick seat swap or quick
leave by one pilot without requiring the
remaining pilot to put on an oxygen
mask. Response: On November 10, 2005,
we published a direct final rule to
address these comments (70 FR 68330).
The direct final rule procedure involves
issuing a final rule with request for
comments. If we receive any adverse
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comment, we withdraw the rule before
it becomes effective. We may then issue
a notice of proposed rulemaking. We
received an adverse comment from the
National Transportation Safety Board
stating that we relied on data that did
not represent actual pilot performance
under realistic decompression
conditions. See Docket No. FAA–2005–
22915. For this reason, we withdrew the
final rule on January 11, 2006 (71 FR
1688). We don’t plan any further action
at this time.
The Air Transport Association asked
that we amend 14 CFR 121.368 by
adopting its comments dated May 5,
2003, on inspection procedures.
Response: Chapter 10, Volume 3 of FAA
Order No. 8300.10, Airworthiness
Inspectors’ Handbook, addresses these
comments.
The Air Transport Association also
commented on supplemental
inspections, 14 CFR 121.370a. This rule
requires all aircraft in operation after
December 20, 2010, to have a
maintenance program that includes
damage-tolerance based inspections and
procedures. The Association asked that
we adopt its comments on inspection
procedures dated May 5, 2003 (Docket
No. FAA 1999–5401). The regulation
imposes an undue burden on operators
and may also duplicate other existing
regulatory requirements. Response:
These comments were addressed in the
aging aircraft safety final rule, which
was published on February 5, 2005 (70
FR 5517).
The Air Transport Association asked
for confirmation that 14 CFR 121.393(b)
allows a pilot to substitute for a flight
attendant during an intermediate stop.
Response: Existing paragraph (b)(2)
allows the certificate holder to
substitute for the required flight
attendants other persons qualified in the
emergency evacuation procedures for
that aircraft as required in 14 CFR
121.417 if these persons are identified to
the passengers. So the answer is a
qualified ‘‘yes.’’ A pilot could substitute
for a flight attendant during an
intermediate stop. The pilot would have
to be qualified in the aircraft’s
emergency evacuation procedures and
would have to be identified to the
passengers.
We received three comments on our
regulations governing mechanical
reliability reports (14 CFR 121.703). The
Air Transport Association
recommended that we require reporting
only of significant occurrences and
within 72 hours after the aircraft has
returned to service, rather than 72 hours
after the occurrence. Southwest Airlines
asked us to remove service difficulty
reporting requirements that have been
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previously tracked by individual
carriers. The Regional Airline
Association asked that we offer air
carriers the option to refrain from
submitting mechanical reliability
reports. Response: This issue was the
subject of a final rule we published on
December 30, 2003 (68 FR 75380), with
a request for comments. We
subsequently delayed the effective date
of the final rule to give us time to
consider the comments. On December
29, 2005, we withdrew the final rule to
re-examine the Service Difficulty Report
(SDR) program. In the same document,
we adopted several amendments that
improve the functioning of the SDR
program (70 FR 76974). These
amendments include increasing the
time for submitting an SDR from 72
hours to 96 hours after an event occurs
that requires an SDR. This change gives
certificate holders additional time to
prepare the SDR and should reduce the
number of supplemental SDRs that need
to be filed.
One commenter representing General
Electric Aircraft Engines asked that we
amend 14 CFR part 187 to correspond
with laws passed by Congress that
eliminate some fees. The fees that are
the subject of the comment are for
certification services performed outside
the United States. Response: We
decided in 1997 not to charge these
particular fees. Part 187 does not require
the agency to charge these fees. It only
establishes a method for calculating
them.
Comments That We Are Addressing
We are in the process of addressing 13
of the 97 comments. General Electric
Aircraft Engines commented on the
parts manufacturer approval regulations
in 14 CFR parts 21 and 45. The
comment urged FAA to issue for public
comment the most recent version of the
document originally prepared by the
Parts and Production Certification
Working Group of the Aviation
Rulemaking Advisory Committee in
February 1999. Response: We have
incorporated the working group’s
recommendations into an ongoing
rulemaking project to revise 14 CFR
parts 21 and 45.
Another representative of General
Electric Aircraft Engines made several
comments on 14 CFR part 21,
Certification Procedures for Products
and Parts. One comment urged us to
address international consortium
arrangements in part 21 by allowing
multiple international production
authorizations. Another comment
recommended allowing and recognizing
work on complete products that is done
by one production certificate (PC)
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35001
holder at another PC holder’s facility
without requiring formal extension of
the PC. A third comment asked us to
clarify exactly when an engine or
propeller is submitted for airworthiness
certification or approval. A
representative of Honeywell Engines,
Systems and Services also commented
on part 21. One comment asked us to
remove 14 CFR 21.325(b)(3), which
limits export airworthiness approvals to
products manufactured and located in
the United States. The commenter
believes that this regulation is
unnecessary and costly and does not
support a global manufacturing
environment. Honeywell stated that it
should be the production approval
holder’s responsibility to make sure
products meet the approved design, and
the place of production should not
matter. Another comment urged
elimination of 14 CFR 21.147, which
requires the holder of a production
certificate to notify us of each change to
the quality control system that may
affect the inspection, conformity, or
airworthiness of the product. In the
commenter’s view, this requirement is
burdensome, unnecessary, and subject
to varying interpretation. Response: All
of these comments are being addressed
in an ongoing project to amend part 21
that was published for public comment
on October 5, 2006 (71 FR 58913). The
comment period closed on February 5,
2007, and we are now in the process of
analyzing the comments.
An individual commenter proposed
that we require separate exit doors for
passengers and flight crewmembers to
prevent hijacking of commercial
airliners. Response: The existing
regulations require a reinforced flight
deck door that significantly reduces the
risk of forced entry onto the flight deck.
For airplanes of 20 passengers or
greater, the regulations already prescribe
separate emergency exits for passengers
and flightcrew. It would not be feasible
to retrofit the existing commercial
airline fleet with separate exit doors.
Further, a separate project is addressing
suspicious activity or security breaches
in the cabin. On September 21, 2005, we
issued a notice of proposed rulemaking
concerning flightdeck door monitoring
and crew discreet alerting systems (70
FR 55492). This proposal would require
a means to monitor the door area
outside the flightdeck and a means to
discretely notify the flightcrew of
threats. The comment period closed on
November 21, 2005, and we are in the
process of preparing the final rule. The
existing regulations and this proposal,
when it is finalized, will help address
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the commenter’s concern about
hijacking.
A representative of Alteon Training
commented there is a pressing need
within the industry to update,
standardize, and harmonize the various
regulations and documents relating to
airman and crewmember training. There
are multiple documents that include
qualification and training requirements
for pilots, flight instructors, simulator
instructors, check airmen, and training
evaluators. Many of the sources of
information are in conflict with one
another. These documents include 14
CFR parts 61, 91, 135, 121, and 142;
various Practical Test Standards;
Operations Inspector’s Handbooks; and
several FAA forms. Response: These
comments are being addressed by the
Flight Simulation final rule, published
on October 30, 2006 (71 FR 63391) and
by an upcoming proposal to amend
subparts N and O of 14 CFR part 121.
One individual recommended we
abolish or amend 14 CFR 121.383(c),
which prohibits people aged 60 and
older from serving as commercial pilots.
According to the commenter, the rule is
baseless, discriminatory, and deprives
the U.S. airline industry of some of its
most able and experienced pilots.
Response: On January 30, 2007, the
Administrator announced that the FAA
will propose a raise in the mandatory
retirement age for U.S. commercial
pilots from 60 to 65. The FAA plans to
have an NPRM out by the end of
calendar year 2007. The public,
industry, and individual pilots will then
have the opportunity to comment.
Another of the Air Transport
Association’s comments concerns
crewmember requirements at stops
where passengers remain on board, 14
CFR 121.393. The Association asked us
to confirm that flight attendants may
leave the aircraft to conduct passengerrelated business as long as the engines
are shut down and at least one floor
level exit is open when staffing is
reduced in accordance with 14 CFR
121.393(b). The reason is that allowing
flight attendants to step onto the jet
bridge at intermediate stops facilitates
communication with ground personnel,
reduces delays, and otherwise promotes
the efficient use of personnel on through
flights. Response: A rulemaking team
has been established, is considering the
issues, and will recommend the best
way to proceed.
Another Air Transport Association
comment concerns crewmember
emergency training, 14 CFR
121.417(c)(2)(ii)(B). The Association
recommended elimination of the
requirement that recurrent training must
include a module on transferring each
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type of slide or raft pack from one door
to another. The Association believes it
is impractical to expect that a
crewmember would be able to complete
the complex series of steps required to
remove a slide or raft from one exit and
install it in another in a post-ditching
situation. Response: This issue is being
addressed in an ongoing rulemaking
project to revise subparts N and O of 14
CFR part 121.
The Air Transport Association also
requested a change to 14 CFR 121.434
to allow the check pilot to step away
during flight without a replacement and
allow the pilot in training to remain at
the controls under certain
circumstances. Response: This comment
is being addressed by an upcoming
proposal to amend subparts N and O of
14 CFR part 121.
The Boeing Company commented
regarding 14 CFR 25.777, Cockpit
controls, and 14 CFR 25.779, Motion
and effect of cockpit controls. According
to the commenter, 14 CFR 25.777(b)
states the direction of movement of
cockpit controls must meet the
requirements of 14 CFR 25.779.
However, that regulation explicitly
addresses only a certain list of controls,
leaving other controls subject to implicit
coverage. The commenter urged us to
revise the requirements to either list all
controls or include language describing
how to show compliance for nonlisted
controls. In the commenter’s view, the
recommended change would improve
the efficiency of the production
approval process without compromising
aviation safety. Response: A rulemaking
team has been established, is
considering the issues, and will
recommend the best way to proceed.
Comments That We Will Address
We plan to address 13 of the
comments. ABX Air commented there
are overlaps between 14 CFR 121.370,
121.370a, the proposed widespread
fatigue damage rule, and various
airworthiness directives on the subject
of aging aircraft. The commenter
recommends forming a committee to
coordinate and eliminate duplication
between these items. Response: The
FAA recently performed a
comprehensive review of the Aging
Airplane Program. Among other things,
our review identified overlapping and
redundant requirements in certain
rulemaking initiatives, such as those
identified by the commenter. Based on
this, we developed ways to eliminate
duplication between the rulemaking
initiatives. A public notice entitled
‘‘Fuel Tank Safety Compliance
Extension and Aging Airplane Program
Update,’’ which was issued on July 30,
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2004, summarized the FAA’s
conclusions and plans (69 FR 45936).
These plans should address the
recommendation made by the
commenter.
The Air Transport Association
recommended we adopt the rulemaking
recommendations of the Clarification of
Major/Minor Repairs or Alterations
Working Group of the Aviation
Rulemaking Advisory Committee
(ARAC). This change would address a
controversial enforcement and
compliance issue. Response: The
recently formed Aviation Safety Repairs
and Alterations Team is conducting a
thorough evaluation of all comments we
have received on this issue, including
the ARAC recommendations. The team
plans to make recommendations for
changes to existing policies and
development of new policies.
We received 11 comments from
several commenters on various aspects
of flight time limitations and rest
requirements, which are found in 14
CFR 121.471 to 525. Some of the
commenters wanted us to guarantee that
flight crewmembers get enough rest and
to base rest requirements on time on
duty rather than on flight time. Some
suggested specific language that would
require crewmembers to have at least 10
consecutive hours of rest after
completing a flight. Another commenter
suggested that we restrict the ability of
carriers to reduce rest time by allowing
reduced rest time only when delays
occur that are beyond the carriers’
control. Alternatively, one commenter
asked us to consider the rest periods
during duty in setting the rest-time
requirements. Response: In 1995, the
FAA published a comprehensive notice
of proposed rulemaking addressing duty
period limitations, flight time
limitations, and rest requirements for
flight crewmembers. We received a large
number of comments. We intend to
address these issues and are currently
considering our next action.
Comments That We Will Not Address at
This Time
We received 48 comments that we
will not address at this time. We have
arranged this section in numerical order
of the regulation cited by the
commenters, except that we discuss
general or overarching comments up
front.
The Regional Airline Association
made a comment about recent
rulemaking proposals. The Association
believes FAA policy seems to support
the notion that certain advisory material
currently contained in Advisory
Circulars should instead be placed into
the appendices of the FAA regulations.
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The justification is not that the FAA
wants the industry to conform to only
‘‘one means of compliance,’’ but that
advisory material placed into an
appendix will somehow be easier to
revise. The association believes we
should use appendices sparingly and
not to establish requirements. Response:
It is true that we have recently adopted
Quality Performance Standards (QPS)
appendices that contain both regulatory
and informational material. We have
two reasons for doing so. Much of the
material in the QPS appendices is
regulatory and properly belongs in the
regulations. Secondly, we believe this is
a user-friendly approach. By having the
advisory material close to the QPS
requirements in one document, people
will not have to refer to several
documents to learn both what is
required and a recommended way of
complying.
We received two comments on 14
CFR part 1, which contains definitions
of terms used throughout our
regulations. The National Air Carrier
Association proposed we revise part 1 to
include definitions of ‘‘accepted,’’
‘‘airworthy,’’ ‘‘competent,’’ and
‘‘repair.’’ Response: We disagree with
the comment. These particular terms are
used in a number of different
circumstances in the regulations, and it
would not be possible to write allpurpose definitions.
The other comment on part 1 came
from a representative of GE Aircraft
Engines who urged us to amend part 1
to include definitions of words used in
our regulations that have a meaning
different from that given in the
dictionary. We do not believe this is
appropriate. Terms are included in part
1 or in individual regulations because
they have specialized meanings.
An individual commenter suggested
the cost of the requirements for flotation
equipment (14 CFR 25.801) and
crewmember training in ditching
procedures (14 CFR 121.417) are not
offset by any benefits in lives saved or
injuries prevented. Response: These
requirements have been in place for
many years. While we acknowledge the
number of ditching incidents is low, we
do not have any information that the
relatively minor cost of these
requirements exceeds the benefits they
would provide in the event ditching
became necessary.
The same commenter questioned
whether it is necessary to supply oxygen
to the passenger cabin in the event of an
emergency. Response: Between 1959
and 1996, there were about 40 reported
decompression events in the worldwide
fleet of large transport category
airplanes over 60,000 pounds. Airplanes
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are being approved to operate at everincreasing altitudes, which increases the
risk to passengers should a cabin
decompression occur. The FAA believes
it is necessary to supply oxygen to the
passenger cabin in the event of an
emergency because any cabin
decompression is a serious matter that
could lead to permanent injury or death
due to lack of oxygen. While these
events are rare, we believe the
emergency oxygen systems play a
significant role in ensuring the wellbeing of passengers.
An individual proposed that we
eliminate the vertical burn test
requirement for seat cushions in 14 CFR
25.853(c). In the commenter’s view, this
is a costly requirement that is not
necessary due to advances in
technology. Response: We do not
necessarily disagree with the comment,
but due to other ongoing projects, it is
not an immediate priority. Southwest
Airlines proposed we eliminate 14 CFR
25.853(g) and 121.215(d), which contain
requirements to provide lavatory
ashtrays and no-smoking signs in the
aircraft cabin. According to the
commenter, these requirements are
unnecessary since smoking has been
banned on commercial flights in the
U.S. for almost 20 years and
announcements to this effect are made
throughout each flight. Response: We
disagree with the comment. Even
though smoking is prohibited, there are
still smokers, and the lavatory ashtrays
provide a safe place to extinguish illegal
smoking material. We also believe the
sign or placard requirement provides a
continuous reminder to passengers of
the ban on smoking. This is especially
important on longer flights.
ABX Air stated there is a conflict
between 14 CFR 25.857 and 121.583
with regard to carrying supernumeraries
aboard a cargo airplane. The commenter
recommended changing 14 CFR
25.857(e) to allow the supernumeraries
identified in 14 CFR 121.583 to be
carried aboard airplanes with a Class E
cargo compartment. In the commenter’s
view, the change would eliminate the
need for individual exemptions.
Response: Because the kinds of
supernumeraries identified in part 121
are varied, and the duties they may
perform during flight are also varied, it
is not a straightforward matter to
include them all in part 25. We find it
appropriate to use the exemption
process to consider each case on merit
and may initiate rulemaking action as
appropriate at some future time.
A representative of General Electric
Aircraft Engines recommends we
rescind 14 CFR 25.901(b)(2) as obsolete,
impossible to interpret consistently, and
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having no well-defined means of
compliance. This regulation requires the
components of each powerplant
installation to be constructed, arranged,
and installed to ensure their continued
safe operation between normal
inspections or overhauls. According to
the commenter, engines are currently
overhauled when a departure from
normal operation is observed, not
according to a specific time interval.
Also, the current large commercial
transport fleet operates at an extremely
high level of propulsion system
reliability. Response: We acknowledge
that a literal application of this rule at
the component level has long since
given way to the realities of meeting the
intent of the requirement at the airplane
system level. This regulation prohibits
intentionally exposing the airplane to
practically preventable powerplant
installation failures. Consequently, we
do not agree the regulation is no longer
useful or effective. While we plan no
immediate action on this issue, we may
consider rulemaking in the future to
update the requirement and provide
standardized compliance guidance, as
resources and priorities allow.
The Boeing Company commented that
14 CFR 25.1353, Electrical equipment
and installations, and 14 CFR 25.1431,
Electronic equipment should be revised
to clarify what is meant by ‘‘electronic’’
versus ‘‘electrical.’’ The lack of a clear
distinction between the terms has posed
problems and duplicated efforts during
aircraft certification activities. At times,
the commenter has shown compliance
with both regulations, when compliance
with only one is sufficient. To remedy
the problem, the commenter suggested
we revise 14 CFR 25.1353 to clarify that
it pertains to equipment directly related
to generation and distribution of
primary electrical power. The
commenter also recommended we
revise 14 CFR 25.1431 to clarify that it
pertains to all other electrically powered
equipment. Response: Existing
§ 25.1353 applies to both electronic and
electrical equipment. While § 25.1353(c)
references storage batteries, the
regulation is not limited to power
generation and distribution functions.
For example § 25.1353(a), (b), and (d)
apply to all electrical and electronic
equipment. Existing § 25.1431 clearly
states that it applies to radio and
electronic equipment. We are not aware
of any misunderstanding of how this
regulation applies to the aircraft
certification process. For these reasons,
we do not believe the recommended
changes are necessary.
General Electric Aircraft Engines filed
four comments on 14 CFR part 33,
which contains the airworthiness
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standards for aircraft engines. The
commenter believes § 33.17, Fire
prevention, does not take account of fire
protection zones as used at the aircraft
level for engine certification. As a result,
the commenter recommends we revise
the regulation to allow for the actual
installations, with the installation
assumptions documented in the
installation manual. Response: We agree
that § 33.17 does not address fire zone
definitions. We consider fire zones and
aircraft-level installation assessments to
be outside the scope of the engine
certification process and are addressed
during aircraft certification. Changes to
part 33 are not appropriate.
The commenter recommended we
revise 14 CFR 33.87, Endurance test, to
allow the use of other test cycles based
on submittal of acceptable data. The
commenter notes that the test cycle was
defined when engine architecture and
control systems were simpler and may
not provide the best current test for a
specific change or application.
Response: The test cycle of § 33.87 and
its associated test conditions have been
revised in the four decades since we
adopted them. There have been two
major revisions to the regulation
(Amendments 6 and 10) to
accommodate the increasing complexity
of the engine, airframe, and their
interface. The purpose of the endurance
test is to show a level of engine
operability and durability within the
approved engine ratings and limitations
and to contribute to an acceptable level
of safety for aircraft gas turbine engines.
An alternate test cycle may not be as
reliable as the one specified in § 33.87.
However, our regulations do provide a
means for evaluating alternatives and
approving those that provide an
equivalent level of safety (14 CFR
21.21).
Concerning 14 CFR 33.88, Engine
overtemperature test, the commenter
stated that the requirement was
originally a 5-minute uncooled rotor
integrity demonstration (reference
AC33–3). As implemented by
Amendment 6, it became a 30-minute
test which was found to be overly severe
because of flowpath limitations.
Amendment 10 changed the duration
back to 5 minutes but also changed the
focus from a rotor integrity
demonstration to an overall hot section
durability demonstration. There is little
evidence that cooled rotors are
significantly influenced by a 75 degrees
F increase in gas path temperature,
making this requirement superfluous
from a safety standpoint. Further there
is no direct Joint Aviation
Requirements—Engines (JAR–E) or
Certification Specification—Engines
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(CS–E) corollary. JAR–E 700 and CS–E
700, Excess Operating Conditions, is the
closest related requirement, and it only
comes into play if the conditions of
speed and temperature can arise.
Response: The engine overtemperature
test is intended to ensure that turbine
engine hot sections can safely
accommodate overtemperature events,
which history has shown do occur.
Many years of successful service
experience provide the necessary
validation for the overtemperature
requirement. We agree there is no direct
JAR–E or CS–E corollary for this
requirement. The FAA and the
European Aviation Safety Authority
continue to work cooperatively toward
harmonized regulations, as appropriate.
Concerning 14 CFR 33.97, Thrust
reversers, the commenter recommended
a revision to address the difference
between fan (cold structure) and core
(hot structure) reversers. The
commenter also pointed out the
endurance and calibration tests are
almost never performed with the
reversers installed. More often than not,
simulated service cycles satisfy the
requirement of § 33.97(a). Response: We
agree there have been a number of
instances where the endurance,
calibration, operation, and vibration
tests are run without the reverser
installed. We evaluate these instances
on a case-by-case basis for compliance.
We may consider a change to § 33.97(a)
to remove the strict requirement of
running tests with the reverser installed;
expand the scope of which block tests
require an engine and thrust reverser
compatibility evaluation; and allow
alternate considerations, other than
tests, for these evaluations in the future
as workload and resources permit.
ABX Air filed four comments on
specific airworthiness directives (AD).
In each case, the commenter suggested
the AD was obsolete and should be
withdrawn. Withdrawing the AD would
eliminate the cost of tracking and
maintaining records. Response: In one
case, we agree with the suggestion and
discussed the issue earlier in this
document under the heading
‘‘Comments we have already
addressed.’’ Two of the comments
concern ADs that require modification
of certain protective breathing
equipment mask assemblies. Without
more information about how
cancellation of these ADs would relieve
the burden on the commenter, we are
unable to evaluate the merits of these
recommendations. The fourth comment
concerns AD 84–18–07, Amendment
39–4915, which requires inspection of
certain discharge cartridges for
erroneously placed aluminum foil in the
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electrical connector pins. Response: We
would like to point out that this AD
does not apply to components installed
on foreign-registered aircraft. It is
possible that a U.S. carrier could buy an
aircraft that has one of these
components installed and has not
complied with this AD. Thus, the
possibility exists that withdrawal of this
AD could lead to an unsafe condition.
For this reason, we disagree with the
comment.
The Air Transport Association
suggested we amend the appropriate
section of 14 CFR part 39 to allow the
FAA Certificate Management Office
(CMO) to approve minor changes or
deviations from the means of
compliance specified in an
Airworthiness Directive. Currently,
§ 39.19 requires an operator to send a
proposed alternate means of compliance
through its principal inspector to the
manager of the office that issued the AD
for review and approval. According to
the commenter, allowing the CMO to
approve minor deviations would
streamline the process and reduce
aircraft and engine downtime.
Response: We disagree with the
proposal. Alternative means of
compliance to an AD need to be
reviewed by an engineer familiar with
the technical information in the type
design to assure the objective of the AD
is attained.
A representative of General Electric
Aircraft Engines recommended that we
amend 14 CFR 43.3(j) to allow a
manufacturer to perform maintenance
on any aircraft, aircraft engine,
propeller, or part thereof manufactured
by him under a type or production
certificate without needing any other
certificate or authorization. Currently,
the regulations allow a manufacturer to
either rebuild or alter, but not to
perform maintenance on those items. In
the commenter’s view, requiring a
manufacturer to hold a repair station
license to perform maintenance on the
manufacturer’s own products adds an
administrative burden on the
manufacturer and diverts FAA resources
away from critical safety functions.
Response: We disagree with the
comment. The holder of a production
certificate has demonstrated the
capability to produce accurate copies of
a particular design, but has made no
showing about the ability to perform
various kinds of maintenance. To allow
a manufacturer, based on a production
certificate, to perform maintenance
without determining the manufacturer
meets the repair station criteria of 14
CFR part 145 would not be prudent and
would not contribute to safety.
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The same representative of General
Electric Aircraft Engines also filed a
comment on 14 CFR part 45,
Identification and registration marking.
The commenter recommended we
coordinate with the Department of
Defense (DoD) to make the DoD’s unique
item identification and the FAA part
marking requirements the same for
products used in both military and civil
aviation. Response: We do not disagree
with the comment. Currently, DoD is
developing its marking requirements.
We are monitoring their activities and
may consider rulemaking once we have
a clear picture of what they will require.
The Experimental Aircraft
Association filed a comment on 14 CFR
47.33(c), which contains the
requirements for registering aircraft not
previously registered anywhere. The
Association recommends we allow an
applicant for registration of an aircraft
built from a kit to file either a bill of sale
or an invoice from the manufacturer.
Currently, the regulation requires a bill
of sale. In the Association’s view, this
requirement is burdensome because
most kit manufacturers do not provide
a bill of sale. Response: Invoices do not
themselves provide proof of ownership.
Proof of ownership should include
language that shows a sale took place
and the signature of the seller. For this
reason, we do accept some invoices if
they have a signature for the
manufacturer and some wording such as
‘‘sold to [name of buyer].’’
An individual commenter
recommended that we eliminate the
requirement in 14 CFR 61.23 that
private pilots hold a third-class medical
certificate. In its place, the commenter
suggested we accept a driver’s license
and require the private pilot to consult
an aviation medical examiner if an
illness occurs that might reasonably be
expected to affect the ability to fly.
Response: Out of a concern for the
potential safety impact of the change
given the large number of private pilots,
and in the absence of any data to
support the change, we are not inclined
to change the rule at this time.
A representative of World Airways
objected to the requirements of 14 CFR
61.18, 63.14, and 65.14 concerning
security disqualification. These
regulations require the FAA to deny a
pilot certificate when the Transportation
Security Administration (TSA) has
notified the FAA in writing that an
individual poses a security threat. The
commenter believes it is inappropriate
for FAA to deny a certificate based
solely on the recommendation of
another organization. The commenter
suggested the FAA set up an
independent review process to prevent
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Jkt 211001
the careers of aviation professionals
from being unjustly terminated by
unilateral action of the TSA. Response:
We disagree with the comment.
Congress has given TSA legal authority
to make these determinations. It is
beyond the scope of FAA’s authority to
establish a separate mechanism that
duplicates TSA’s duties. Although in
this one particular area there is a
separation of duties, FAA and TSA are
working closely and cooperating to
ensure a safe and secure aviation
system.
We received several comments on 14
CFR part 91, which contains our general
operating and flight rules. A
representative of Apex Aviation
proposed that we amend 14 CFR
91.117(c) by adding the words ‘‘under
VFR’’ after the word ‘‘aircraft.’’ The
commenter believes the change would
allow operation of an aircraft under IFR
at up to 250 knots in certain areas. In
the commenter’s view, the current
regulation unnecessarily slows traffic
flow, may interfere with sequencing of
aircraft by air traffic control, and costs
money and wastes fuel by extending
flight time. Response: All IFR traffic is
under air traffic control, which can
specify any speed less than 250 knots
that may be necessary. We believe the
commenter may have misunderstood
the regulation. The speed restrictions in
the existing rule do not distinguish
between VFR and IFR. The speed
restrictions are based on the flight
altitude or airspace designation.
A representative of World Airways
also commented on 14 CFR 91.117(c),
asking that it either be eliminated or
restricted to VFR aircraft not in contact
with air traffic control. In the
commenter’s view, the existing
limitation may serve a purpose for
keeping the closure speeds of aircraft
not in contact with air traffic control to
a minimum, but for those who routinely
operate below Class B airspace in
contact with, or at the direction of, air
traffic control, this restriction is
unnecessary. In fact, it has the potential
to degrade safety due to pilot distraction
while trying to determine the lateral
limits of Class B airspace when on an
IFR flight plan. Response: The
maximum allowable speed is governed
by aircraft altitude or airspace
designation. There is an exception
where the minimum safe airspeed for a
particular operation is greater than the
maximum prescribed by the rule. In this
case, the aircraft may be operated at that
minimum, and air traffic control should
be advised.
One individual commenter suggested
we update 14 CFR 91.207, Emergency
locator transmitters, to include the new
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35005
406MHz emergency locator transmitter.
The change should include actual
decoding and reading of the
transmitter’s identification number and
GPS location by independent test
equipment to verify the transmitter is
sending the correct information through
its antenna. Response: We disagree with
the comment. Approved emergency
locator transmitters are specified in
technical standard orders (TSOs), which
are more easily updated than
regulations. The 406 MHz transmitter is
included in TSO–C126, which was last
updated on December 8, 2006.
Another individual commenter
suggested we create an exception from
14 CFR 91.207 to allow turbojet aircraft
to use portable emergency locator
transmitters, rather than requiring the
transmitters to be attached to the
aircraft. Response: We disagree with the
comment. The requirement for
transmitters to be attached to the aircraft
ensures they are on board for every
flight and automatically activate when
needed.
A representative of Morris Research,
Inc, proposed that we amend 14 CFR
91.213(a)(2) to allow operation of
turbine-powered aircraft under part 91
using the FAA-approved master
minimum equipment list for that type of
aircraft as the approved minimum
equipment list without having to get a
letter of authorization from the FAA.
Among its reasons for the proposed
change, the commenter noted that it is
burdensome to require each turbinepowered aircraft operated under part 91
to get a letter of authorization to operate
with the most insignificant inoperative
equipment, such as a passenger reading
light. Response: While we do not
necessarily disagree with the comment,
due to resources allocated to other
projects, this is not a high priority.
The National Air Carrier Association
recommended that we eliminate the
requirement that the FAA review and
approve wet leases before a certificate
holder conducts operations involving a
wet lease (14 CFR 119.53). The
Association considers this requirement
unnecessary, costly, and burdensome. It
suggested that providing the wet lease
agreement to the FAA before or after the
operation allows the FAA to provide
adequate surveillance over operational
control. Response: We are not
persuaded that this requirement is
unnecessary. In a wet lease situation,
the party exercising operational control
is held responsible for the safety and
regulatory compliance of the flights
conducted under the wet lease. It is not
in the public interest to allow
operations to be conducted under a wet
lease (without the FAA having an
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opportunity to review the wet lease and
determine beforehand which party has
operational control) if the party alleging
to have operational control is later
found not to be responsible for the
safety and regulatory compliance of the
flights.
There were nine comments filed by
the Air Transport Association on 14
CFR part 121 that may have merit, but
we are unable to devote resources to a
rulemaking project at this time. We do
not view these recommended changes as
being higher priority than the
rulemaking projects already in progress.
These comments include the following:
• Amend 14 CFR 121.335, Equipment
standards, to eliminate the reference to
an obsolete regulation;
• Amend 14 CFR 121.367,
Maintenance, preventive maintenance,
and alterations programs, by revising
the introductory language to consolidate
the regulatory requirements;
• Amend 14 CFR 121.613, Dispatch
or flight release under IFR or over the
top, to allow a flight to be released
without meeting the required approach
minimums at the destination if an
alternate airport is given in the dispatch
release;
• Amend 14 CFR 121.619, Alternate
airport for destination, to reflect current
aircraft and airport approach
capabilities;
• Amend 14 CFR 121.619 to reduce
minimums from 2,000 to 1,000 feet and
from three miles to one mile visibility
during the period from one hour before
to one hour after estimated time of
arrival;
• Amend 14 CFR 121.621, Alternate
airport for destination, to either remove
or extend the current six-hour time limit
on no-alternate operations;
• Amend 14 CFR 121.645, Fuel
supply, to eliminate the requirement
that fuel loads for international aircraft
operations include an extra 10 percent
of the total flight time;
• Amend 14 CFR 121.652, Landing
weather minimums, to eliminate the
reduced landing weather minimums for
less experienced pilots when an
autopilot or head-up guidance is used
(the National Air Carrier Association
also filed a comment on this topic); and
• Amend 14 CFR 121.655,
Applicability of reported weather
minimums, to allow some flexibility
when the reported visibility in the main
body of the weather report is less than
four miles.
The National Air Carrier Association
suggested we delete 14 CFR 121.139,
Requirements for manual aboard
aircraft, in its entirety. This regulation,
in part, requires certificate holders
conducting supplemental operations to
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Jkt 211001
carry appropriate parts of the printed
manual on each airplane when away
from the principal base of operations. If
the manual is not in printed form, it
requires the airplane to carry a
compatible reading device. The
commenters believe this is an
unnecessary requirement given the state
of technology today. Response: Our
view is that the information in the
manual must be available wherever the
aircraft goes. For this reason, we are not
inclined to change the regulation.
A representative of the Orange County
(CA) Flight Center suggested we amend
one of the flight training requirements of
14 CFR 141.79 to allow use of a flight
training device to accomplish the
recurrent proficiency check required by
paragraph (d)(2). The commenter
suggested allowing the flight training
device on a rotational basis at schools
that have an approved instrument
course that requires use of the flight
training device. Response: While we do
not necessarily disagree with the
comment, due to resources allocated to
other projects, it is not a high priority.
A representative of Honeywell
Engines, Systems and Services
suggested we change 14 CFR
145.153(b)(1), which requires
certificated U.S. repair stations to
employ supervisors who are certificated
under 14 CFR part 65. The commenter
feels this requirement is burdensome,
unnecessary, and costly and suggests
that a technical lead could ensure that
employees performing the work are
capable. Response: We believe that
supervisors must be certified to ensure
they can direct the activities of workers
who may not be at the journeyman
level. For this reason, we are not
inclined to change the regulation.
The Boeing Company suggested a
change to 14 CFR 183.29(i), which
prohibits an acoustical engineering
representative (AER) from determining a
type design change is not an acoustical
change. In the commenter’s view, this
limit is not consistent with how we
manage other designated engineering
representatives. It also requires
applicants to provide a significant
amount of information to FAA to enable
us to determine how a type design
change should be certified for noise.
Removing this limit could improve
efficiency without adversely affecting
safety. Response: We disagree with the
comment. An AER is authorized only to
determine the noise test, test data, and
associated analyses comply with the
applicable regulations. A determination
that a type design change is an
acoustical change is not a compliance
determination and would not be
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appropriate for an AER, even if the limit
were not spelled out in the regulation.
Conclusion
The FAA finds that reviewing public
comments on our regulations helps us
in assessing the effectiveness of our
regulatory agenda and adjusting the
agenda when necessary. As a result of
this review, we have identified many
issues of importance to the industry and
other interested parties. Some of these
issues, we are pleased to note, we either
have already addressed or are currently
addressing. In addition, the review
offers us a general understanding of
industry’s and the public’s concerns
about our regulations. We intend to
continue to request public comments on
a three-year cycle to identify any
necessary changes to our regulatory
program. We plan to issue a notice
requesting public comments for our next
review later this year.
Issued in Washington, DC, on June 19,
2007.
Nicholas A. Sabatini,
Associate Administrator for Aviation Safety.
[FR Doc. E7–12285 Filed 6–25–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 97
[Docket No. 30556 Amdt. No. 3223]
Standard Instrument Approach
Procedures, Weather Takeoff
Minimums; Miscellaneous
Amendments
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: This amendment establishes,
amends, suspends, or revokes Standard
Instrument Approach Procedures
(SIAPs) and/or Weather Takeoff
Minimums for operations at certain
airports. These regulatory actions are
needed because of the adoption of new
or revised criteria, or because of changes
occurring in the National Airspace
System, such as the commissioning of
new navigational facilities, addition of
new obstacles, or changes in air traffic
requirements. These changes are
designed to provide safe and efficient
use of the navigable airspace and to
promote safe flight operations under
instrument flight rules at the affected
airports.
This rule is effective June 26,
2007. The compliance date for each
DATES:
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Agencies
[Federal Register Volume 72, Number 122 (Tuesday, June 26, 2007)]
[Rules and Regulations]
[Pages 34999-35006]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-12285]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Chapters I and III
[Docket No.: FAA-2004-17168]
Review of Existing Regulations
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Disposition of comments on existing regulations.
-----------------------------------------------------------------------
SUMMARY: The FAA is notifying the public of the outcome of our periodic
review of existing regulations. This notice summarizes the public
comments we received and our responses to them. This action is part of
our effort to make our regulatory program more effective and less
burdensome.
FOR FURTHER INFORMATION CONTACT: Patrick W. Boyd, Office of Rulemaking,
ARM-23, Federal Aviation Administration, 800 Independence Avenue, SW.,
Washington, DC 20591; telephone (202) 267-7320.
SUPPLEMENTARY INFORMATION:
Background
Under section 5 of Executive Order 12866, Regulatory Planning and
Review, each agency must develop a program to periodically review its
existing regulations to determine if they should be changed or
eliminated (58 FR 51735, October 4, 1993). The purposes of the review
are to make the agency's regulatory program more effective in achieving
the regulatory objectives and less burdensome. The FAA conducts its
review on a three-year cycle.
On February 25, 2004, we published a notice in the Federal Register
asking the public to tell us which regulations we should amend, remove,
or simplify (69 FR 8575). The notice stated that we would consider the
comments and adjust our regulatory priorities consistent with our
statutory responsibilities. The notice also stated we would publish a
summary of the comments and an explanation of how we would act on them.
Summary of Comments
In response to the February 2004 notice, we received 97 comments
from 30 different commenters. For comparison, we received 476 comments
during the previous review and 82 comments the time before that. We
received comments from citizens, private pilots, commercial pilots, and
representatives of interest groups and commercial entities. The
interest groups that filed comments include the Air Transport
Association, the Allied Pilots
[[Page 35000]]
Association, the Experimental Aircraft Association, the National Air
Carrier Association, and the Regional Airline Association. The
commercial entities that filed comments include ABX Air, Inc.; Alteon
Training; Apex Aviation Corporation; Boeing Commercial Airplanes;
General Electric Aircraft Engines; Honeywell Engines, Systems and
Services; Morris Research, Inc.; the Orange County (Ca.) Flight Center;
Southwest Airlines; and World Airways.
Our February 2004 request for comments asked that commenters
identify three regulations that we should amend or remove. This is to
enable us to focus on commenters' high priority concerns. Most
commenters limited themselves to three or fewer comments. However, the
Air Transport Association filed 21 comments, while Southwest Airlines
and the National Air Carrier Association filed 5 each.
Our February 2004 request for comments also asked the public to
direct comments about 14 CFR parts 125 and 135 to the working group
that is conducting a separate review of those parts to avoid any
duplication of effort. We appreciate that commenters complied with this
request. For the first time, the regulatory review included 14 CFR
Chapter III, the regulations governing commercial space transportation.
However, we did not receive any comments on these regulations.
Response to Comments
We have organized the comments in four groups:
Comments that we have already addressed,
Comments that we are addressing,
Comments that we will address, and
Comments that we will not address at this time.
Readers should note that, in this document, when we say we ``are
addressing'' a comment, we do not mean we will necessarily address a
comment exactly as proposed by a commenter. We reserve the right to
``address'' comments in a way that is in accord with our statutory
authority, balances competing interests, and fosters a safe and
efficient civil aviation system. We have carefully considered issues
raised by commenters and are taking, or will take, action to address
those issues, as discussed below, but we do not guarantee the outcome
of our action will always correspond to the commenters' views. With
regard to comments that we will not address now, readers should note
that, while we disagree with some of the comments, in other cases we
simply cannot take action now due to competing priorities and limited
resources.
Comments That We Have Already Addressed
We have already addressed 23 of the 97 comments. One individual
commenter asked us to amend the medical examination requirement to
require pilots to report only new medical examinations that occurred
after the last application date. Response: We have already included
this in the instructions printed on the form.
Southwest Airlines asked us to restructure the environmental
assessment process for routine airspace and airport expansion.
Response: On June 8, 2004, we issued revised FAA Order No. 1050.1E,
entitled, ``Environmental Impacts: Policies and Procedures.'' The order
establishes a categorical exclusion from National Environmental Policy
Act requirements for these changes.
The Air Transport Association asked that, before undertaking new
regulatory reviews, we conduct a thorough analysis of the
accomplishments of the previous review. Response: We already do this as
part of the review of existing regulations and through the reviews
conducted under section 610 of the Regulatory Flexibility Act.
The Air Transport Association also asked that the FAA conduct a
rigorous evaluation of the need and impact of every proposed
regulation. Response: Existing laws and Executive Orders already
require this. For example, the National Environmental Policy Act
requires analysis of the environmental impact of Federal actions, and
Executive Order 12866, Regulatory Review, requires analysis of the
costs and benefits of proposed regulatory actions.
An individual commenter asked that the FAA control air pollution,
aircraft noise, and crashes and prevent pilots who are under the
influence of illegal substances from operating aircraft. Response: We
already have regulations in place for these purposes, including 14 CFR
part 34 (air pollution), part 36 (noise), and part 61 (drug and alcohol
testing).
An individual commenter asked that we allow general aviation
operations at the Ronald Reagan Washington National Airport. Response:
While the airport was closed to general aviation as part of the
security measures adopted in the aftermath of the terrorist attacks on
September 11, 2001, the Transportation Security Administration (TSA)
has since reopened the airport to general aviation operations that meet
specific security criteria (70 FR 41585, July 19, 2005).
ABX Air recommended removing from 14 CFR part 39 airworthiness
directive 91-08-51, amendment 39-7031. This amendment requires certain
actions for aircraft equipped with a Honeywell flight management system
that had a navigational database. The AD became effective on June 24,
1991 and had a compliance period of 72 hours. Response: We agree with
the commenter and withdrew AD 91-08-51 on October 5, 2005.
We received four comments on 14 CFR 91.205(b)(12) and 121.353
asking us to require pyrotechnic signaling devices only for aircraft
used in extended over-water operations. Response: On December 27, 2004,
we published a final rule that removes the requirement for a
pyrotechnic signaling device for aircraft operated for hire over water
and beyond power-off gliding distance from shore for air carriers
operating under Part 121 unless it is part of a required life raft. All
other operators will continue to be required to have onboard one
pyrotechnic signaling device if they operate aircraft for hire over
water and beyond power-off gliding distance from shore (69 FR 77596).
World Airways asked us to amend 14 CFR 121.311(e)(2) to allow
certain passengers the ability to keep their seats reclined if they do
not obstruct others' access to the aisle or emergency exits. Response:
Paragraph (e)(2) is an exception to the requirement in paragraph (e)
that no certificate holder may take off or land an airplane unless each
passenger seat back is in the upright position. Paragraph (e)(2) states
that paragraph (e) does not apply to seats on which cargo or persons
who are unable to sit erect for a medical reason are carried in
accordance with procedures in the certificate holder's manual if the
seat back does not obstruct any passenger's access to the aisle or to
any emergency exit. Thus, we see no need to amend the regulation since
it already allows the flexibility the commenter is seeking.
Three commenters, including World Airways, the National Air Carrier
Association and the Air Transport Association, filed four comments on
the topic of supplemental oxygen. Specifically, they requested we
change 14 CFR 121.333(c)(3) and 91. 211(b)(2) to allow for a quick seat
swap or quick leave by one pilot without requiring the remaining pilot
to put on an oxygen mask. Response: On November 10, 2005, we published
a direct final rule to address these comments (70 FR 68330). The direct
final rule procedure involves issuing a final rule with request for
comments. If we receive any adverse
[[Page 35001]]
comment, we withdraw the rule before it becomes effective. We may then
issue a notice of proposed rulemaking. We received an adverse comment
from the National Transportation Safety Board stating that we relied on
data that did not represent actual pilot performance under realistic
decompression conditions. See Docket No. FAA-2005-22915. For this
reason, we withdrew the final rule on January 11, 2006 (71 FR 1688). We
don't plan any further action at this time.
The Air Transport Association asked that we amend 14 CFR 121.368 by
adopting its comments dated May 5, 2003, on inspection procedures.
Response: Chapter 10, Volume 3 of FAA Order No. 8300.10, Airworthiness
Inspectors' Handbook, addresses these comments.
The Air Transport Association also commented on supplemental
inspections, 14 CFR 121.370a. This rule requires all aircraft in
operation after December 20, 2010, to have a maintenance program that
includes damage-tolerance based inspections and procedures. The
Association asked that we adopt its comments on inspection procedures
dated May 5, 2003 (Docket No. FAA 1999-5401). The regulation imposes an
undue burden on operators and may also duplicate other existing
regulatory requirements. Response: These comments were addressed in the
aging aircraft safety final rule, which was published on February 5,
2005 (70 FR 5517).
The Air Transport Association asked for confirmation that 14 CFR
121.393(b) allows a pilot to substitute for a flight attendant during
an intermediate stop. Response: Existing paragraph (b)(2) allows the
certificate holder to substitute for the required flight attendants
other persons qualified in the emergency evacuation procedures for that
aircraft as required in 14 CFR 121.417 if these persons are identified
to the passengers. So the answer is a qualified ``yes.'' A pilot could
substitute for a flight attendant during an intermediate stop. The
pilot would have to be qualified in the aircraft's emergency evacuation
procedures and would have to be identified to the passengers.
We received three comments on our regulations governing mechanical
reliability reports (14 CFR 121.703). The Air Transport Association
recommended that we require reporting only of significant occurrences
and within 72 hours after the aircraft has returned to service, rather
than 72 hours after the occurrence. Southwest Airlines asked us to
remove service difficulty reporting requirements that have been
previously tracked by individual carriers. The Regional Airline
Association asked that we offer air carriers the option to refrain from
submitting mechanical reliability reports. Response: This issue was the
subject of a final rule we published on December 30, 2003 (68 FR
75380), with a request for comments. We subsequently delayed the
effective date of the final rule to give us time to consider the
comments. On December 29, 2005, we withdrew the final rule to re-
examine the Service Difficulty Report (SDR) program. In the same
document, we adopted several amendments that improve the functioning of
the SDR program (70 FR 76974). These amendments include increasing the
time for submitting an SDR from 72 hours to 96 hours after an event
occurs that requires an SDR. This change gives certificate holders
additional time to prepare the SDR and should reduce the number of
supplemental SDRs that need to be filed.
One commenter representing General Electric Aircraft Engines asked
that we amend 14 CFR part 187 to correspond with laws passed by
Congress that eliminate some fees. The fees that are the subject of the
comment are for certification services performed outside the United
States. Response: We decided in 1997 not to charge these particular
fees. Part 187 does not require the agency to charge these fees. It
only establishes a method for calculating them.
Comments That We Are Addressing
We are in the process of addressing 13 of the 97 comments. General
Electric Aircraft Engines commented on the parts manufacturer approval
regulations in 14 CFR parts 21 and 45. The comment urged FAA to issue
for public comment the most recent version of the document originally
prepared by the Parts and Production Certification Working Group of the
Aviation Rulemaking Advisory Committee in February 1999. Response: We
have incorporated the working group's recommendations into an ongoing
rulemaking project to revise 14 CFR parts 21 and 45.
Another representative of General Electric Aircraft Engines made
several comments on 14 CFR part 21, Certification Procedures for
Products and Parts. One comment urged us to address international
consortium arrangements in part 21 by allowing multiple international
production authorizations. Another comment recommended allowing and
recognizing work on complete products that is done by one production
certificate (PC) holder at another PC holder's facility without
requiring formal extension of the PC. A third comment asked us to
clarify exactly when an engine or propeller is submitted for
airworthiness certification or approval. A representative of Honeywell
Engines, Systems and Services also commented on part 21. One comment
asked us to remove 14 CFR 21.325(b)(3), which limits export
airworthiness approvals to products manufactured and located in the
United States. The commenter believes that this regulation is
unnecessary and costly and does not support a global manufacturing
environment. Honeywell stated that it should be the production approval
holder's responsibility to make sure products meet the approved design,
and the place of production should not matter. Another comment urged
elimination of 14 CFR 21.147, which requires the holder of a production
certificate to notify us of each change to the quality control system
that may affect the inspection, conformity, or airworthiness of the
product. In the commenter's view, this requirement is burdensome,
unnecessary, and subject to varying interpretation. Response: All of
these comments are being addressed in an ongoing project to amend part
21 that was published for public comment on October 5, 2006 (71 FR
58913). The comment period closed on February 5, 2007, and we are now
in the process of analyzing the comments.
An individual commenter proposed that we require separate exit
doors for passengers and flight crewmembers to prevent hijacking of
commercial airliners. Response: The existing regulations require a
reinforced flight deck door that significantly reduces the risk of
forced entry onto the flight deck. For airplanes of 20 passengers or
greater, the regulations already prescribe separate emergency exits for
passengers and flightcrew. It would not be feasible to retrofit the
existing commercial airline fleet with separate exit doors. Further, a
separate project is addressing suspicious activity or security breaches
in the cabin. On September 21, 2005, we issued a notice of proposed
rulemaking concerning flightdeck door monitoring and crew discreet
alerting systems (70 FR 55492). This proposal would require a means to
monitor the door area outside the flightdeck and a means to discretely
notify the flightcrew of threats. The comment period closed on November
21, 2005, and we are in the process of preparing the final rule. The
existing regulations and this proposal, when it is finalized, will help
address
[[Page 35002]]
the commenter's concern about hijacking.
A representative of Alteon Training commented there is a pressing
need within the industry to update, standardize, and harmonize the
various regulations and documents relating to airman and crewmember
training. There are multiple documents that include qualification and
training requirements for pilots, flight instructors, simulator
instructors, check airmen, and training evaluators. Many of the sources
of information are in conflict with one another. These documents
include 14 CFR parts 61, 91, 135, 121, and 142; various Practical Test
Standards; Operations Inspector's Handbooks; and several FAA forms.
Response: These comments are being addressed by the Flight Simulation
final rule, published on October 30, 2006 (71 FR 63391) and by an
upcoming proposal to amend subparts N and O of 14 CFR part 121.
One individual recommended we abolish or amend 14 CFR 121.383(c),
which prohibits people aged 60 and older from serving as commercial
pilots. According to the commenter, the rule is baseless,
discriminatory, and deprives the U.S. airline industry of some of its
most able and experienced pilots. Response: On January 30, 2007, the
Administrator announced that the FAA will propose a raise in the
mandatory retirement age for U.S. commercial pilots from 60 to 65. The
FAA plans to have an NPRM out by the end of calendar year 2007. The
public, industry, and individual pilots will then have the opportunity
to comment.
Another of the Air Transport Association's comments concerns
crewmember requirements at stops where passengers remain on board, 14
CFR 121.393. The Association asked us to confirm that flight attendants
may leave the aircraft to conduct passenger-related business as long as
the engines are shut down and at least one floor level exit is open
when staffing is reduced in accordance with 14 CFR 121.393(b). The
reason is that allowing flight attendants to step onto the jet bridge
at intermediate stops facilitates communication with ground personnel,
reduces delays, and otherwise promotes the efficient use of personnel
on through flights. Response: A rulemaking team has been established,
is considering the issues, and will recommend the best way to proceed.
Another Air Transport Association comment concerns crewmember
emergency training, 14 CFR 121.417(c)(2)(ii)(B). The Association
recommended elimination of the requirement that recurrent training must
include a module on transferring each type of slide or raft pack from
one door to another. The Association believes it is impractical to
expect that a crewmember would be able to complete the complex series
of steps required to remove a slide or raft from one exit and install
it in another in a post-ditching situation. Response: This issue is
being addressed in an ongoing rulemaking project to revise subparts N
and O of 14 CFR part 121.
The Air Transport Association also requested a change to 14 CFR
121.434 to allow the check pilot to step away during flight without a
replacement and allow the pilot in training to remain at the controls
under certain circumstances. Response: This comment is being addressed
by an upcoming proposal to amend subparts N and O of 14 CFR part 121.
The Boeing Company commented regarding 14 CFR 25.777, Cockpit
controls, and 14 CFR 25.779, Motion and effect of cockpit controls.
According to the commenter, 14 CFR 25.777(b) states the direction of
movement of cockpit controls must meet the requirements of 14 CFR
25.779. However, that regulation explicitly addresses only a certain
list of controls, leaving other controls subject to implicit coverage.
The commenter urged us to revise the requirements to either list all
controls or include language describing how to show compliance for
nonlisted controls. In the commenter's view, the recommended change
would improve the efficiency of the production approval process without
compromising aviation safety. Response: A rulemaking team has been
established, is considering the issues, and will recommend the best way
to proceed.
Comments That We Will Address
We plan to address 13 of the comments. ABX Air commented there are
overlaps between 14 CFR 121.370, 121.370a, the proposed widespread
fatigue damage rule, and various airworthiness directives on the
subject of aging aircraft. The commenter recommends forming a committee
to coordinate and eliminate duplication between these items. Response:
The FAA recently performed a comprehensive review of the Aging Airplane
Program. Among other things, our review identified overlapping and
redundant requirements in certain rulemaking initiatives, such as those
identified by the commenter. Based on this, we developed ways to
eliminate duplication between the rulemaking initiatives. A public
notice entitled ``Fuel Tank Safety Compliance Extension and Aging
Airplane Program Update,'' which was issued on July 30, 2004,
summarized the FAA's conclusions and plans (69 FR 45936). These plans
should address the recommendation made by the commenter.
The Air Transport Association recommended we adopt the rulemaking
recommendations of the Clarification of Major/Minor Repairs or
Alterations Working Group of the Aviation Rulemaking Advisory Committee
(ARAC). This change would address a controversial enforcement and
compliance issue. Response: The recently formed Aviation Safety Repairs
and Alterations Team is conducting a thorough evaluation of all
comments we have received on this issue, including the ARAC
recommendations. The team plans to make recommendations for changes to
existing policies and development of new policies.
We received 11 comments from several commenters on various aspects
of flight time limitations and rest requirements, which are found in 14
CFR 121.471 to 525. Some of the commenters wanted us to guarantee that
flight crewmembers get enough rest and to base rest requirements on
time on duty rather than on flight time. Some suggested specific
language that would require crewmembers to have at least 10 consecutive
hours of rest after completing a flight. Another commenter suggested
that we restrict the ability of carriers to reduce rest time by
allowing reduced rest time only when delays occur that are beyond the
carriers' control. Alternatively, one commenter asked us to consider
the rest periods during duty in setting the rest-time requirements.
Response: In 1995, the FAA published a comprehensive notice of proposed
rulemaking addressing duty period limitations, flight time limitations,
and rest requirements for flight crewmembers. We received a large
number of comments. We intend to address these issues and are currently
considering our next action.
Comments That We Will Not Address at This Time
We received 48 comments that we will not address at this time. We
have arranged this section in numerical order of the regulation cited
by the commenters, except that we discuss general or overarching
comments up front.
The Regional Airline Association made a comment about recent
rulemaking proposals. The Association believes FAA policy seems to
support the notion that certain advisory material currently contained
in Advisory Circulars should instead be placed into the appendices of
the FAA regulations.
[[Page 35003]]
The justification is not that the FAA wants the industry to conform to
only ``one means of compliance,'' but that advisory material placed
into an appendix will somehow be easier to revise. The association
believes we should use appendices sparingly and not to establish
requirements. Response: It is true that we have recently adopted
Quality Performance Standards (QPS) appendices that contain both
regulatory and informational material. We have two reasons for doing
so. Much of the material in the QPS appendices is regulatory and
properly belongs in the regulations. Secondly, we believe this is a
user-friendly approach. By having the advisory material close to the
QPS requirements in one document, people will not have to refer to
several documents to learn both what is required and a recommended way
of complying.
We received two comments on 14 CFR part 1, which contains
definitions of terms used throughout our regulations. The National Air
Carrier Association proposed we revise part 1 to include definitions of
``accepted,'' ``airworthy,'' ``competent,'' and ``repair.'' Response:
We disagree with the comment. These particular terms are used in a
number of different circumstances in the regulations, and it would not
be possible to write all-purpose definitions.
The other comment on part 1 came from a representative of GE
Aircraft Engines who urged us to amend part 1 to include definitions of
words used in our regulations that have a meaning different from that
given in the dictionary. We do not believe this is appropriate. Terms
are included in part 1 or in individual regulations because they have
specialized meanings.
An individual commenter suggested the cost of the requirements for
flotation equipment (14 CFR 25.801) and crewmember training in ditching
procedures (14 CFR 121.417) are not offset by any benefits in lives
saved or injuries prevented. Response: These requirements have been in
place for many years. While we acknowledge the number of ditching
incidents is low, we do not have any information that the relatively
minor cost of these requirements exceeds the benefits they would
provide in the event ditching became necessary.
The same commenter questioned whether it is necessary to supply
oxygen to the passenger cabin in the event of an emergency. Response:
Between 1959 and 1996, there were about 40 reported decompression
events in the worldwide fleet of large transport category airplanes
over 60,000 pounds. Airplanes are being approved to operate at ever-
increasing altitudes, which increases the risk to passengers should a
cabin decompression occur. The FAA believes it is necessary to supply
oxygen to the passenger cabin in the event of an emergency because any
cabin decompression is a serious matter that could lead to permanent
injury or death due to lack of oxygen. While these events are rare, we
believe the emergency oxygen systems play a significant role in
ensuring the well-being of passengers.
An individual proposed that we eliminate the vertical burn test
requirement for seat cushions in 14 CFR 25.853(c). In the commenter's
view, this is a costly requirement that is not necessary due to
advances in technology. Response: We do not necessarily disagree with
the comment, but due to other ongoing projects, it is not an immediate
priority. Southwest Airlines proposed we eliminate 14 CFR 25.853(g) and
121.215(d), which contain requirements to provide lavatory ashtrays and
no-smoking signs in the aircraft cabin. According to the commenter,
these requirements are unnecessary since smoking has been banned on
commercial flights in the U.S. for almost 20 years and announcements to
this effect are made throughout each flight. Response: We disagree with
the comment. Even though smoking is prohibited, there are still
smokers, and the lavatory ashtrays provide a safe place to extinguish
illegal smoking material. We also believe the sign or placard
requirement provides a continuous reminder to passengers of the ban on
smoking. This is especially important on longer flights.
ABX Air stated there is a conflict between 14 CFR 25.857 and
121.583 with regard to carrying supernumeraries aboard a cargo
airplane. The commenter recommended changing 14 CFR 25.857(e) to allow
the supernumeraries identified in 14 CFR 121.583 to be carried aboard
airplanes with a Class E cargo compartment. In the commenter's view,
the change would eliminate the need for individual exemptions.
Response: Because the kinds of supernumeraries identified in part 121
are varied, and the duties they may perform during flight are also
varied, it is not a straightforward matter to include them all in part
25. We find it appropriate to use the exemption process to consider
each case on merit and may initiate rulemaking action as appropriate at
some future time.
A representative of General Electric Aircraft Engines recommends we
rescind 14 CFR 25.901(b)(2) as obsolete, impossible to interpret
consistently, and having no well-defined means of compliance. This
regulation requires the components of each powerplant installation to
be constructed, arranged, and installed to ensure their continued safe
operation between normal inspections or overhauls. According to the
commenter, engines are currently overhauled when a departure from
normal operation is observed, not according to a specific time
interval. Also, the current large commercial transport fleet operates
at an extremely high level of propulsion system reliability. Response:
We acknowledge that a literal application of this rule at the component
level has long since given way to the realities of meeting the intent
of the requirement at the airplane system level. This regulation
prohibits intentionally exposing the airplane to practically
preventable powerplant installation failures. Consequently, we do not
agree the regulation is no longer useful or effective. While we plan no
immediate action on this issue, we may consider rulemaking in the
future to update the requirement and provide standardized compliance
guidance, as resources and priorities allow.
The Boeing Company commented that 14 CFR 25.1353, Electrical
equipment and installations, and 14 CFR 25.1431, Electronic equipment
should be revised to clarify what is meant by ``electronic'' versus
``electrical.'' The lack of a clear distinction between the terms has
posed problems and duplicated efforts during aircraft certification
activities. At times, the commenter has shown compliance with both
regulations, when compliance with only one is sufficient. To remedy the
problem, the commenter suggested we revise 14 CFR 25.1353 to clarify
that it pertains to equipment directly related to generation and
distribution of primary electrical power. The commenter also
recommended we revise 14 CFR 25.1431 to clarify that it pertains to all
other electrically powered equipment. Response: Existing Sec. 25.1353
applies to both electronic and electrical equipment. While Sec.
25.1353(c) references storage batteries, the regulation is not limited
to power generation and distribution functions. For example Sec.
25.1353(a), (b), and (d) apply to all electrical and electronic
equipment. Existing Sec. 25.1431 clearly states that it applies to
radio and electronic equipment. We are not aware of any
misunderstanding of how this regulation applies to the aircraft
certification process. For these reasons, we do not believe the
recommended changes are necessary.
General Electric Aircraft Engines filed four comments on 14 CFR
part 33, which contains the airworthiness
[[Page 35004]]
standards for aircraft engines. The commenter believes Sec. 33.17,
Fire prevention, does not take account of fire protection zones as used
at the aircraft level for engine certification. As a result, the
commenter recommends we revise the regulation to allow for the actual
installations, with the installation assumptions documented in the
installation manual. Response: We agree that Sec. 33.17 does not
address fire zone definitions. We consider fire zones and aircraft-
level installation assessments to be outside the scope of the engine
certification process and are addressed during aircraft certification.
Changes to part 33 are not appropriate.
The commenter recommended we revise 14 CFR 33.87, Endurance test,
to allow the use of other test cycles based on submittal of acceptable
data. The commenter notes that the test cycle was defined when engine
architecture and control systems were simpler and may not provide the
best current test for a specific change or application. Response: The
test cycle of Sec. 33.87 and its associated test conditions have been
revised in the four decades since we adopted them. There have been two
major revisions to the regulation (Amendments 6 and 10) to accommodate
the increasing complexity of the engine, airframe, and their interface.
The purpose of the endurance test is to show a level of engine
operability and durability within the approved engine ratings and
limitations and to contribute to an acceptable level of safety for
aircraft gas turbine engines. An alternate test cycle may not be as
reliable as the one specified in Sec. 33.87. However, our regulations
do provide a means for evaluating alternatives and approving those that
provide an equivalent level of safety (14 CFR 21.21).
Concerning 14 CFR 33.88, Engine overtemperature test, the commenter
stated that the requirement was originally a 5-minute uncooled rotor
integrity demonstration (reference AC33-3). As implemented by Amendment
6, it became a 30-minute test which was found to be overly severe
because of flowpath limitations. Amendment 10 changed the duration back
to 5 minutes but also changed the focus from a rotor integrity
demonstration to an overall hot section durability demonstration. There
is little evidence that cooled rotors are significantly influenced by a
75 degrees F increase in gas path temperature, making this requirement
superfluous from a safety standpoint. Further there is no direct Joint
Aviation Requirements--Engines (JAR-E) or Certification Specification--
Engines (CS-E) corollary. JAR-E 700 and CS-E 700, Excess Operating
Conditions, is the closest related requirement, and it only comes into
play if the conditions of speed and temperature can arise. Response:
The engine overtemperature test is intended to ensure that turbine
engine hot sections can safely accommodate overtemperature events,
which history has shown do occur. Many years of successful service
experience provide the necessary validation for the overtemperature
requirement. We agree there is no direct JAR-E or CS-E corollary for
this requirement. The FAA and the European Aviation Safety Authority
continue to work cooperatively toward harmonized regulations, as
appropriate.
Concerning 14 CFR 33.97, Thrust reversers, the commenter
recommended a revision to address the difference between fan (cold
structure) and core (hot structure) reversers. The commenter also
pointed out the endurance and calibration tests are almost never
performed with the reversers installed. More often than not, simulated
service cycles satisfy the requirement of Sec. 33.97(a). Response: We
agree there have been a number of instances where the endurance,
calibration, operation, and vibration tests are run without the
reverser installed. We evaluate these instances on a case-by-case basis
for compliance. We may consider a change to Sec. 33.97(a) to remove
the strict requirement of running tests with the reverser installed;
expand the scope of which block tests require an engine and thrust
reverser compatibility evaluation; and allow alternate considerations,
other than tests, for these evaluations in the future as workload and
resources permit.
ABX Air filed four comments on specific airworthiness directives
(AD). In each case, the commenter suggested the AD was obsolete and
should be withdrawn. Withdrawing the AD would eliminate the cost of
tracking and maintaining records. Response: In one case, we agree with
the suggestion and discussed the issue earlier in this document under
the heading ``Comments we have already addressed.'' Two of the comments
concern ADs that require modification of certain protective breathing
equipment mask assemblies. Without more information about how
cancellation of these ADs would relieve the burden on the commenter, we
are unable to evaluate the merits of these recommendations. The fourth
comment concerns AD 84-18-07, Amendment 39-4915, which requires
inspection of certain discharge cartridges for erroneously placed
aluminum foil in the electrical connector pins. Response: We would like
to point out that this AD does not apply to components installed on
foreign-registered aircraft. It is possible that a U.S. carrier could
buy an aircraft that has one of these components installed and has not
complied with this AD. Thus, the possibility exists that withdrawal of
this AD could lead to an unsafe condition. For this reason, we disagree
with the comment.
The Air Transport Association suggested we amend the appropriate
section of 14 CFR part 39 to allow the FAA Certificate Management
Office (CMO) to approve minor changes or deviations from the means of
compliance specified in an Airworthiness Directive. Currently, Sec.
39.19 requires an operator to send a proposed alternate means of
compliance through its principal inspector to the manager of the office
that issued the AD for review and approval. According to the commenter,
allowing the CMO to approve minor deviations would streamline the
process and reduce aircraft and engine downtime. Response: We disagree
with the proposal. Alternative means of compliance to an AD need to be
reviewed by an engineer familiar with the technical information in the
type design to assure the objective of the AD is attained.
A representative of General Electric Aircraft Engines recommended
that we amend 14 CFR 43.3(j) to allow a manufacturer to perform
maintenance on any aircraft, aircraft engine, propeller, or part
thereof manufactured by him under a type or production certificate
without needing any other certificate or authorization. Currently, the
regulations allow a manufacturer to either rebuild or alter, but not to
perform maintenance on those items. In the commenter's view, requiring
a manufacturer to hold a repair station license to perform maintenance
on the manufacturer's own products adds an administrative burden on the
manufacturer and diverts FAA resources away from critical safety
functions. Response: We disagree with the comment. The holder of a
production certificate has demonstrated the capability to produce
accurate copies of a particular design, but has made no showing about
the ability to perform various kinds of maintenance. To allow a
manufacturer, based on a production certificate, to perform maintenance
without determining the manufacturer meets the repair station criteria
of 14 CFR part 145 would not be prudent and would not contribute to
safety.
[[Page 35005]]
The same representative of General Electric Aircraft Engines also
filed a comment on 14 CFR part 45, Identification and registration
marking. The commenter recommended we coordinate with the Department of
Defense (DoD) to make the DoD's unique item identification and the FAA
part marking requirements the same for products used in both military
and civil aviation. Response: We do not disagree with the comment.
Currently, DoD is developing its marking requirements. We are
monitoring their activities and may consider rulemaking once we have a
clear picture of what they will require.
The Experimental Aircraft Association filed a comment on 14 CFR
47.33(c), which contains the requirements for registering aircraft not
previously registered anywhere. The Association recommends we allow an
applicant for registration of an aircraft built from a kit to file
either a bill of sale or an invoice from the manufacturer. Currently,
the regulation requires a bill of sale. In the Association's view, this
requirement is burdensome because most kit manufacturers do not provide
a bill of sale. Response: Invoices do not themselves provide proof of
ownership. Proof of ownership should include language that shows a sale
took place and the signature of the seller. For this reason, we do
accept some invoices if they have a signature for the manufacturer and
some wording such as ``sold to [name of buyer].''
An individual commenter recommended that we eliminate the
requirement in 14 CFR 61.23 that private pilots hold a third-class
medical certificate. In its place, the commenter suggested we accept a
driver's license and require the private pilot to consult an aviation
medical examiner if an illness occurs that might reasonably be expected
to affect the ability to fly. Response: Out of a concern for the
potential safety impact of the change given the large number of private
pilots, and in the absence of any data to support the change, we are
not inclined to change the rule at this time.
A representative of World Airways objected to the requirements of
14 CFR 61.18, 63.14, and 65.14 concerning security disqualification.
These regulations require the FAA to deny a pilot certificate when the
Transportation Security Administration (TSA) has notified the FAA in
writing that an individual poses a security threat. The commenter
believes it is inappropriate for FAA to deny a certificate based solely
on the recommendation of another organization. The commenter suggested
the FAA set up an independent review process to prevent the careers of
aviation professionals from being unjustly terminated by unilateral
action of the TSA. Response: We disagree with the comment. Congress has
given TSA legal authority to make these determinations. It is beyond
the scope of FAA's authority to establish a separate mechanism that
duplicates TSA's duties. Although in this one particular area there is
a separation of duties, FAA and TSA are working closely and cooperating
to ensure a safe and secure aviation system.
We received several comments on 14 CFR part 91, which contains our
general operating and flight rules. A representative of Apex Aviation
proposed that we amend 14 CFR 91.117(c) by adding the words ``under
VFR'' after the word ``aircraft.'' The commenter believes the change
would allow operation of an aircraft under IFR at up to 250 knots in
certain areas. In the commenter's view, the current regulation
unnecessarily slows traffic flow, may interfere with sequencing of
aircraft by air traffic control, and costs money and wastes fuel by
extending flight time. Response: All IFR traffic is under air traffic
control, which can specify any speed less than 250 knots that may be
necessary. We believe the commenter may have misunderstood the
regulation. The speed restrictions in the existing rule do not
distinguish between VFR and IFR. The speed restrictions are based on
the flight altitude or airspace designation.
A representative of World Airways also commented on 14 CFR
91.117(c), asking that it either be eliminated or restricted to VFR
aircraft not in contact with air traffic control. In the commenter's
view, the existing limitation may serve a purpose for keeping the
closure speeds of aircraft not in contact with air traffic control to a
minimum, but for those who routinely operate below Class B airspace in
contact with, or at the direction of, air traffic control, this
restriction is unnecessary. In fact, it has the potential to degrade
safety due to pilot distraction while trying to determine the lateral
limits of Class B airspace when on an IFR flight plan. Response: The
maximum allowable speed is governed by aircraft altitude or airspace
designation. There is an exception where the minimum safe airspeed for
a particular operation is greater than the maximum prescribed by the
rule. In this case, the aircraft may be operated at that minimum, and
air traffic control should be advised.
One individual commenter suggested we update 14 CFR 91.207,
Emergency locator transmitters, to include the new 406MHz emergency
locator transmitter. The change should include actual decoding and
reading of the transmitter's identification number and GPS location by
independent test equipment to verify the transmitter is sending the
correct information through its antenna. Response: We disagree with the
comment. Approved emergency locator transmitters are specified in
technical standard orders (TSOs), which are more easily updated than
regulations. The 406 MHz transmitter is included in TSO-C126, which was
last updated on December 8, 2006.
Another individual commenter suggested we create an exception from
14 CFR 91.207 to allow turbojet aircraft to use portable emergency
locator transmitters, rather than requiring the transmitters to be
attached to the aircraft. Response: We disagree with the comment. The
requirement for transmitters to be attached to the aircraft ensures
they are on board for every flight and automatically activate when
needed.
A representative of Morris Research, Inc, proposed that we amend 14
CFR 91.213(a)(2) to allow operation of turbine-powered aircraft under
part 91 using the FAA-approved master minimum equipment list for that
type of aircraft as the approved minimum equipment list without having
to get a letter of authorization from the FAA. Among its reasons for
the proposed change, the commenter noted that it is burdensome to
require each turbine-powered aircraft operated under part 91 to get a
letter of authorization to operate with the most insignificant
inoperative equipment, such as a passenger reading light. Response:
While we do not necessarily disagree with the comment, due to resources
allocated to other projects, this is not a high priority.
The National Air Carrier Association recommended that we eliminate
the requirement that the FAA review and approve wet leases before a
certificate holder conducts operations involving a wet lease (14 CFR
119.53). The Association considers this requirement unnecessary,
costly, and burdensome. It suggested that providing the wet lease
agreement to the FAA before or after the operation allows the FAA to
provide adequate surveillance over operational control. Response: We
are not persuaded that this requirement is unnecessary. In a wet lease
situation, the party exercising operational control is held responsible
for the safety and regulatory compliance of the flights conducted under
the wet lease. It is not in the public interest to allow operations to
be conducted under a wet lease (without the FAA having an
[[Page 35006]]
opportunity to review the wet lease and determine beforehand which
party has operational control) if the party alleging to have
operational control is later found not to be responsible for the safety
and regulatory compliance of the flights.
There were nine comments filed by the Air Transport Association on
14 CFR part 121 that may have merit, but we are unable to devote
resources to a rulemaking project at this time. We do not view these
recommended changes as being higher priority than the rulemaking
projects already in progress. These comments include the following:
Amend 14 CFR 121.335, Equipment standards, to eliminate
the reference to an obsolete regulation;
Amend 14 CFR 121.367, Maintenance, preventive maintenance,
and alterations programs, by revising the introductory language to
consolidate the regulatory requirements;
Amend 14 CFR 121.613, Dispatch or flight release under IFR
or over the top, to allow a flight to be released without meeting the
required approach minimums at the destination if an alternate airport
is given in the dispatch release;
Amend 14 CFR 121.619, Alternate airport for destination,
to reflect current aircraft and airport approach capabilities;
Amend 14 CFR 121.619 to reduce minimums from 2,000 to
1,000 feet and from three miles to one mile visibility during the
period from one hour before to one hour after estimated time of
arrival;
Amend 14 CFR 121.621, Alternate airport for destination,
to either remove or extend the current six-hour time limit on no-
alternate operations;
Amend 14 CFR 121.645, Fuel supply, to eliminate the
requirement that fuel loads for international aircraft operations
include an extra 10 percent of the total flight time;
Amend 14 CFR 121.652, Landing weather minimums, to
eliminate the reduced landing weather minimums for less experienced
pilots when an autopilot or head-up guidance is used (the National Air
Carrier Association also filed a comment on this topic); and
Amend 14 CFR 121.655, Applicability of reported weather
minimums, to allow some flexibility when the reported visibility in the
main body of the weather report is less than four miles.
The National Air Carrier Association suggested we delete 14 CFR
121.139, Requirements for manual aboard aircraft, in its entirety. This
regulation, in part, requires certificate holders conducting
supplemental operations to carry appropriate parts of the printed
manual on each airplane when away from the principal base of
operations. If the manual is not in printed form, it requires the
airplane to carry a compatible reading device. The commenters believe
this is an unnecessary requirement given the state of technology today.
Response: Our view is that the information in the manual must be
available wherever the aircraft goes. For this reason, we are not
inclined to change the regulation.
A representative of the Orange County (CA) Flight Center suggested
we amend one of the flight training requirements of 14 CFR 141.79 to
allow use of a flight training device to accomplish the recurrent
proficiency check required by paragraph (d)(2). The commenter suggested
allowing the flight training device on a rotational basis at schools
that have an approved instrument course that requires use of the flight
training device. Response: While we do not necessarily disagree with
the comment, due to resources allocated to other projects, it is not a
high priority.
A representative of Honeywell Engines, Systems and Services
suggested we change 14 CFR 145.153(b)(1), which requires certificated
U.S. repair stations to employ supervisors who are certificated under
14 CFR part 65. The commenter feels this requirement is burdensome,
unnecessary, and costly and suggests that a technical lead could ensure
that employees performing the work are capable. Response: We believe
that supervisors must be certified to ensure they can direct the
activities of workers who may not be at the journeyman level. For this
reason, we are not inclined to change the regulation.
The Boeing Company suggested a change to 14 CFR 183.29(i), which
prohibits an acoustical engineering representative (AER) from
determining a type design change is not an acoustical change. In the
commenter's view, this limit is not consistent with how we manage other
designated engineering representatives. It also requires applicants to
provide a significant amount of information to FAA to enable us to
determine how a type design change should be certified for noise.
Removing this limit could improve efficiency without adversely
affecting safety. Response: We disagree with the comment. An AER is
authorized only to determine the noise test, test data, and associated
analyses comply with the applicable regulations. A determination that a
type design change is an acoustical change is not a compliance
determination and would not be appropriate for an AER, even if the
limit were not spelled out in the regulation.
Conclusion
The FAA finds that reviewing public comments on our regulations
helps us in assessing the effectiveness of our regulatory agenda and
adjusting the agenda when necessary. As a result of this review, we
have identified many issues of importance to the industry and other
interested parties. Some of these issues, we are pleased to note, we
either have already addressed or are currently addressing. In addition,
the review offers us a general understanding of industry's and the
public's concerns about our regulations. We intend to continue to
request public comments on a three-year cycle to identify any necessary
changes to our regulatory program. We plan to issue a notice requesting
public comments for our next review later this year.
Issued in Washington, DC, on June 19, 2007.
Nicholas A. Sabatini,
Associate Administrator for Aviation Safety.
[FR Doc. E7-12285 Filed 6-25-07; 8:45 am]
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