Filtered Flight Data; Technical Correction and Extension of Comment Period, 67115-67117 [E8-26856]
Download as PDF
Federal Register / Vol. 73, No. 220 / Thursday, November 13, 2008 / Proposed Rules
67115
Actions
Compliance
Procedures
(4) If, as a result of any inspection required by
paragraph (e)(3) of this AD, you find any displacement or damage of clamps or hoses,
replace any damaged clamps and hoses.
(5) Do not install any intercooler SF01170004–
0.
Before further flight, after the inspection required by paragraph (e)(3) of this AD where
you found any displacement or damage of
clamps or hoses.
As of the effective date of this AD ...................
Follow SMA SAFRAN Group Service Bulletin
SB–C182–75–004, Revision No. Basic
Issue, dated July 8, 2008.
Special Flight Permit
DEPARTMENT OF TRANSPORTATION
(SNPRM; 73 FR 47857, August 15,
2008), the FAA was contacted by
members of the industry seeking
clarification of our intent and the scope
of specific provisions. A summary of
that meeting has been placed in the
docket for this rule.
Issues raised at the meeting caused us
to realize that the intent of the rule as
stated in the preamble is inconsistent
with the proposed rule text. We are
restating the intent here and providing
revised proposed rule text.
While this preamble discussion uses
part 121 as its reference, it also applies
to parts 125 and 135 and their
comparable sections. During our review,
we also discovered that the SNPRM
change to a separate section (proposed
§ 121.346) caused us to inadvertently
omit an applicability reference for
airplanes covered under § 121.344a. We
have added that reference as part of this
correction.
The definition of filtering, proposed
§ 121.346(a), remains as it was in the
SNPRM. Comments should address that
section of the proposed rule as
published in the SNPRM.
Proposed § 121.346(b) now states that
any parameter required to be recorded
may be filtered as long as the recorded
signal value continues to meet the
requirements of Appendix M.
Paragraph (c) contains a list of
parameters that we consider critical
from the standpoint of accuracy and
accident investigation when complying
with the required accuracy under the
expanded definition of dynamic
conditions in Appendix M. This list has
not changed from the SNPRM. If any
parameter in the paragraph (c) list is
being filtered, and the filtered, recorded
data do not meet Appendix M, then the
certificate holder must choose one of the
following courses of action:
• Remove the filtering; or
• Demonstrate by test and analysis
that the original sensor signal value can
be reconstructed from the recorded
filtered data. If an operator attempts to
show by test and analysis that the data
can be reconstructed but the tests and
analyses fail, or the results cannot be
repeated, the filtering must be removed.
The restructured language of the rule
text has obviated the need for the
second list of parameters. They are
(f) Under 14 CFR part 39.23, we are
limiting the special flight permits for this AD
by the following conditions:
(1) Before flight, an inspection of hoses and
clamps by a properly certificated mechanic
reveals no damaged or disconnected hoses or
clamps; and
(2) You fly by the most direct route to the
site where the AD can be performed.
Alternative Methods of Compliance
(AMOCs)
(g) The Manager, Atlanta Aircraft
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19. Send information to Attn: Don O.
Young, Aerospace Engineer, ACE–118A,
Atlanta ACO, One Crown Center, 1895
Phoenix Blvd., Suite 450, Atlanta, Georgia
30349; telephone: (770) 703–6079; fax: (770)
703–6097. Before using any approved AMOC
on any airplane to which the AMOC applies,
notify your appropriate principal inspector
(PI) in the FAA Flight Standards District
Office (FSDO), or lacking a PI, your local
FSDO.
Related Information
(h) To get copies of the service information
referenced in this AD, contact SMA Customer
Service, 10–12 Rue Didier Daurat, 18021
Bourges, France; telephone: +33 (0) 2 48 67
56 00; fax: +33 (0) 2 48 50 01 41; E-mail:
customer_services@smasr.com; Web: https://
www.smaengines.com. To view the AD
docket, go to U.S. Department of
Transportation, Docket Operations, M–30,
West Building Ground Floor, Room W12–
140, 1200 New Jersey Avenue, SE.,
Washington, DC 20590, or on the Internet at
https://www.regulations.gov.
Issued in Kansas City, Missouri, on
November 6, 2008.
James E. Jackson,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E8–26910 Filed 11–12–08; 8:45 am]
erowe on PROD1PC64 with PROPOSALS-1
BILLING CODE 4910–13–P
Federal Aviation Administration
14 CFR Parts 121, 125 and 135
[Docket No. FAA–2006–26135; Notice No.
08–08]
RIN 2120–AI79
Filtered Flight Data; Technical
Correction and Extension of Comment
Period
Federal Aviation
Administration (FAA), DOT.
ACTION: Supplemental notice of
proposed rulemaking (SNPRM);
correction and extension of comment
period.
AGENCY:
SUMMARY: The FAA is correcting an
SNPRM published in the Federal
Register on August 15, 2008, regarding
filtered flight data. Questions from
industry caused us to conclude that the
intent expressed in the preamble is
inconsistent with the proposed rule
language. This document will clarify
our intent and the rule language. We are
also extending the comment period to
allow for consideration of this
clarification by all interested parties.
DATES: The comment period will close
December 29, 2008.
FOR FURTHER INFORMATION CONTACT: For
technical questions concerning this
proposed rule contact Brian A. Verna,
Avionics Systems Branch, Aircraft
Certification Service, AIR–130, Federal
Aviation Administration, 800
Independence Avenue, SW.,
Washington, DC 20591; telephone (202)
385–4643; fax (202) 385–4651; e-mail
brian.verna@faa.gov. For legal questions
concerning this proposed rule contact
Karen L. Petronis, Senior Attorney for
Regulations, Regulations Division,
Office of the Chief Counsel, AGC–200,
Federal Aviation Administration, 800
Independence Avenue, SW.,
Washington, DC 20591; telephone (202)
267–3073; fax 202–267–7971; e-mail
karen.petronis@faa.gov.
Background
Following the publication of a
supplemental notice of proposed
rulemaking on filtered flight data
VerDate Aug<31>2005
14:38 Nov 12, 2008
Jkt 217001
PO 00000
Frm 00006
Fmt 4702
Sfmt 4702
Not Applicable.
E:\FR\FM\13NOP1.SGM
13NOP1
67116
Federal Register / Vol. 73, No. 220 / Thursday, November 13, 2008 / Proposed Rules
already covered by paragraph (b); they
may be filtered as long as the recorded
signal value meets Appendix M. We
presume that these parameters are
already in compliance with Appendix
M since that compliance is required by
the 1997 rule changes.
The compliance paragraph has been
redesignated as (d), and has been
changed to include the correct
paragraph references; compliance time
remains unchanged.
All other provisions of the proposed
rule, including the definition of
filtering, remain as proposed in the
SNPRM published on August 15, 2008.
Because of the confusion generated by
the SNPRM language published in
August, we are extending the comment
period for the rule as corrected until
December 29, 2008.
Correction
PART 121—OPERATING
REQUIREMENTS: DOMESTIC, FLAG,
AND SUPPLEMENTAL OPERATIONS
1. On page 47867, in the first column,
remove proposed § 121.346(b) and (c)
and add in their place corrected
paragraphs (b), (c) and (d) to read as
follows:
§ 121.346
Flight recorders—filtered data.
erowe on PROD1PC64 with PROPOSALS-1
*
*
*
*
*
(b) An original sensor signal for any
flight recorder parameter required to be
recorded under § 121.344 of this part
may be filtered only if the recorded
signal value continues to meet the
requirements of Appendix B or M of this
part, as applicable.
(c) For a parameter described in
§ 121.344(a)(1) through (7), (9), (11)
through (18), (26), (32), (42), (43), (68),
(70), (77), or (88), or the corresponding
parameter in Appendix B of this part, if
the recorded signal value is filtered and
does not meet the requirements of
Appendix B or M of this part, as
applicable, the certificate holder must:
(1) Remove the filtering and ensure
that the recorded signal value meets the
requirements of Appendix B or M of this
part; or
(2) Demonstrate by test and analysis
that the original sensor signal value can
be reconstructed from the recorded data.
This demonstration requires that:
(i) The FAA determine that the
procedure submitted by the certificate
holder as its compliance with paragraph
(c)(2) of this section is repeatable; and
(ii) The certificate holder maintain
documentation of the procedure
required to reconstruct the original
sensor signal value.
(d) Compliance. After (four years from
effective date), no aircraft flight data
VerDate Aug<31>2005
14:38 Nov 12, 2008
Jkt 217001
recording system may filter any
parameter listed in paragraph (c) of this
section that does not meet the
requirements of Appendix M or B of this
part unless the certificate holder
possesses test and analysis procedures
that have been approved by the FAA.
The procedures must be submitted to
the FAA no later than the completion of
the next heavy maintenance check after
[six months after effective date] but not
later than [two years after the effective
date].
2. On page 48767 in the second
column, add amendatory instruction 2a
to amend section 121.344a(e) to read as
follows:
2a. Amend § 121.344a by revising
paragraph (e) to read as follows:
§ 121.344a Digital flight data recorders for
10–19 seat airplanes.
* * *
(e) All airplanes subject to this section
are also subject to the requirements and
exceptions stated in §§ 121.344(g)
through (k) and 121.346 of this part.
*
*
*
*
*
PART 125—CERTIFICATION AND
OPERATIONS: AIRPLANES HAVING A
SEATING CAPACITY OF 20 OR MORE
PASSENGERS OR A MAXIMUM
PAYLOAD CAPACITY OF 6,000
POUNDS OR MORE; AND RULES
GOVERNING PERSONS ON BOARD
SUCH AIRCRAFT
3. On page 47867, in the second
column, remove proposed § 125.228(b)
and (c) and add in their place corrected
paragraphs (b), (c) and (d) to read as
follows:
§ 125.228
Flight recorders—filtered data.
*
*
*
*
*
(b) An original sensor signal for any
flight recorder parameter required to be
recorded under § 125.226 of this part
may be filtered only if the recorded
signal value continues to meet the
requirements of Appendix D or E of this
part, as applicable.
(c) For a parameter described in
§ 125.226 (a)(1) through (7), (9), (11)
through (18), (26), (32), (42), (43), (68),
(70), (77), or (88), or the corresponding
parameter in Appendix D of this part if
the recorded signal value is filtered and
does not meet the requirements of
Appendix D or E of this part, as
applicable, the certificate holder must:
(1) Remove the filtering and ensure
that the recorded signal value meets the
requirements of Appendix D or E of this
part; or
(2) Demonstrate by test and analysis
that the original sensor signal value can
be reconstructed from the recorded data.
This demonstration requires that:
PO 00000
Frm 00007
Fmt 4702
Sfmt 4702
(i) The FAA determine that the
procedure submitted by the certificate
holder as its compliance with paragraph
(c)(2) of this section is repeatable; and
(ii) The certificate holder maintain
documentation of the procedure
required to reconstruct the original
sensor signal value.
(d) Compliance. After (four years from
effective date), no aircraft flight data
recording system may filter any
parameter listed in paragraph (c) of this
section that does not meet the
requirements of Appendix D or E of this
part unless the certificate holder
possesses test and analysis procedures
that have been approved by the FAA.
The procedures must be submitted to
the FAA no later than the completion of
the next heavy maintenance check after
[six months after effective date] but not
later than [two years after the effective
date].
PART 135—OPERATING
REQUIREMENTS: COMMUTER AND
ON DEMAND OPERATIONS AND
RULES GOVERNING PERSONS ON
BOARD SUCH AIRCRAFT
4. On page 47868, in the first column,
remove proposed § 135.156(b) and (c)
and add in their place corrected
paragraphs (b), (c) and (d) to read as
follows:
§ 135.156
Flight recorders—filtered data.
*
*
*
*
*
(b) An original sensor signal for any
flight recorder parameter required to be
recorded under § 135.152 of this part
may be filtered only if the recorded
signal value continues to meet the
requirements of Appendix F of this part,
as applicable.
(c) For a parameter described in
§ 135.152(h)(1) through (7), (9), (11)
through (18), (26), (32), (42), (43), (68),
(70), (77), or (88), if the recorded signal
value is filtered and does not meet the
requirements of Appendix F of this part,
as applicable, the certificate holder
must:
(1) Remove the filtering and ensure
that the recorded signal value meets the
requirements of Appendix F of this part;
or
(2) Demonstrate by test and analysis
that the original sensor signal value can
be reconstructed from the recorded data.
This demonstration requires that:
(i) The FAA determine that the
procedure submitted by the certificate
holder as its compliance with paragraph
(c)(2) of this section is repeatable; and
(ii) The certificate holder maintain
documentation of the procedure
required to reconstruct the original
sensor signal value.
E:\FR\FM\13NOP1.SGM
13NOP1
Federal Register / Vol. 73, No. 220 / Thursday, November 13, 2008 / Proposed Rules
(d) Compliance. After (four years from
effective date), no aircraft flight data
recording system may filter any
parameter listed in paragraph (c) of this
section that does not meet the
requirements of Appendix F of this part
unless the certificate holder possesses
test and analysis procedures that have
been approved by the FAA. The
procedures must be submitted to the
FAA no later than the completion of the
next heavy maintenance check after [six
months after effective date] but not later
than [two years after the effective date].
Issued in Washington, DC, on November 6,
2008.
Pamela Hamilton-Powell,
Director, Office of Rulemaking.
[FR Doc. E8–26856 Filed 11–12–08; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Highway Administration
23 CFR Parts 620, 635, 636, and 710
[FHWA Docket No. FHWA–2008–0136]
RIN 2125–AF29
Fair Market Value and Design-Build
Amendments
Federal Highway
Administration (FHWA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM); re-opening of comment period.
erowe on PROD1PC64 with PROPOSALS-1
AGENCY:
SUMMARY: The FHWA is re-opening the
comment period for the notice of
proposed rulemaking (NPRM) and
request for comments, which was
published on October 8, 2008, at 73 FR
58908. That NPRM proposes to amend
existing regulations to clarify that fair
market value must be negotiated for and
received under a concession agreement,
and to amend the design-build
regulations to allow contracting
agencies to incorporate unsuccessful
proposers’ ideas into a contract upon
payment of a stipend.
The original comment period closed
on November 7, 2008. The extension is
based on the FHWA’s desire to receive
the fullest and most comprehensive
comments possible from the broadest
group of stakeholders. During the
comment period, the FHWA received
requests for additional time to analyze
and submit comments regarding the
rulemaking. The FHWA recognizes that
VerDate Aug<31>2005
14:38 Nov 12, 2008
Jkt 217001
those interested in commenting on this
important program may not have had
the opportunity to provide comments
and that the comment period should be
reopened. Therefore, the comment
period is being reopened until
November 21, 2008, which will provide
those interested in commenting
additional time to discuss, evaluate, and
submit responses to the docket.
DATES: Comments must be received on
or before November 21, 2008. Late-filed
comments will be considered to the
extent practicable.
ADDRESSES: Mail or hand deliver
comments to Docket Management
Facility: U.S. Department of
Transportation, 1200 New Jersey
Avenue, SE., Washington, DC 20590–
0001, submit comments electronically at
https://www.regulations.gov, or fax
comments to (202) 493–2251.
All comments should include the
docket number that appears in the
heading of this document. All
comments received will be available for
examination and copying at the above
address from 9 a.m. to 5 p.m., e.t.,
Monday through Friday, except Federal
holidays. Those desiring notification of
receipt of comments must include a selfaddressed, stamped postcard or may
print the acknowledgment page that
appears after submitting comments
electronically. Anyone is able to search
the electronic form of all comments in
any one of our dockets by the name of
the individual submitting the comment
(or signing the comment, if submitted
on behalf of an association, business, or
labor union). You may review the DOT’s
complete Privacy Act Statement in the
Federal Register published on April 11,
2000 (Volume 65, Number 70, Pages
19477–78) or you may visit https://
DocketsInfo.dot.gov.
FOR FURTHER INFORMATION CONTACT: Mr.
Marcus J. Lemon, Chief Counsel, Mr.
Michael Harkins, Office of Chief
Counsel, or Mr. Steve Rochlis, Office of
Chief Counsel, (202) 366–0740, Federal
Highway Administration, 1200 New
Jersey Avenue SE., Washington, DC
20590–0001. Office hours are from 7:45
a.m. to 4:15 p.m., e.t., Monday through
Friday, except Federal holidays.
SUPPLEMENTARY INFORMATION:
Electronic Access and Filing
You may submit or retrieve comments
online through the Federal eRulemaking
portal at www.regulations.gov. It is
PO 00000
Frm 00008
Fmt 4702
Sfmt 4702
67117
available 24 hours each day, 365 days
each year. Please follow the instructions
online for more information and help.
An electronic copy of this document
may also be downloaded by accessing
the Office of the Federal Register’s home
page at: https://www.archives.gov and the
Government Printing Office’s Web page
at: https://www.access.gpo.gov/nara.
Background
On October 8, 2008, the FHWA
published an NPRM proposing to
require State departments of
transportation (DOT) and other public
authorities to negotiate for and obtain
fair market value as part of any
concession agreement involving a
facility acquired or constructed with
Federal-aid highway funds; to amend
FHWA regulations to permit public
agencies to compete against private
entities for the right to obtain a
concession agreement involving such
facilities; and to amend the design-build
regulations to permit contracting
agencies to incorporate unsuccessful
offerors’ ideas into a design-build
contract upon the acceptance of a
stipend.
The original comment period for the
NPRM closes on November 7, 2008.
During the comment period, the FHWA
received requests for additional time to
analyze and submit comments regarding
the rulemaking. The FHWA recognizes
that additional time will allow
interested parties a broader and more
comprehensive review and discussion
of the proposed regulations; and then,
allow the development and submission
of complete responses to the docket. To
allow time for interested parties to
submit comprehensive comments, the
comment period is being reopened until
November 21, 2008.
Authority: Secs. 1503 and 1604 of Pub. L.
109–59, 119 Stat. 1144; Secs. 1215(b) and
1307 of Pub. L. 105–178, 112 Stat. 107; Secs.
1012(b) and 1041(a), Pub. L. 102–240, 105
Stat. 1914; 23 U.S.C. 101 (note), 107, 108,
109, 111, 112, 113, 114, 116, 119, 128, 129,
133, 142(f), 156, 166, 204, 210, 308, 315, 318
and 323; 31 U.S.C. 6505; 42 U.S.C. 2000d et
seq., 3334, 4601 et seq.; 23 CFR 1.32; 49 CFR
1.48, 18.31, and parts 21 and 24;
Issued on: November 6, 2008.
Thomas J. Madison, Jr.,
Federal Highway Administrator.
[FR Doc. E8–26936 Filed 11–12–08; 8:45 am]
BILLING CODE 4910–22–P
E:\FR\FM\13NOP1.SGM
13NOP1
Agencies
[Federal Register Volume 73, Number 220 (Thursday, November 13, 2008)]
[Proposed Rules]
[Pages 67115-67117]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-26856]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Parts 121, 125 and 135
[Docket No. FAA-2006-26135; Notice No. 08-08]
RIN 2120-AI79
Filtered Flight Data; Technical Correction and Extension of
Comment Period
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Supplemental notice of proposed rulemaking (SNPRM); correction
and extension of comment period.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an SNPRM published in the Federal
Register on August 15, 2008, regarding filtered flight data. Questions
from industry caused us to conclude that the intent expressed in the
preamble is inconsistent with the proposed rule language. This document
will clarify our intent and the rule language. We are also extending
the comment period to allow for consideration of this clarification by
all interested parties.
DATES: The comment period will close December 29, 2008.
FOR FURTHER INFORMATION CONTACT: For technical questions concerning
this proposed rule contact Brian A. Verna, Avionics Systems Branch,
Aircraft Certification Service, AIR-130, Federal Aviation
Administration, 800 Independence Avenue, SW., Washington, DC 20591;
telephone (202) 385-4643; fax (202) 385-4651; e-mail
brian.verna@faa.gov. For legal questions concerning this proposed rule
contact Karen L. Petronis, Senior Attorney for Regulations, Regulations
Division, Office of the Chief Counsel, AGC-200, Federal Aviation
Administration, 800 Independence Avenue, SW., Washington, DC 20591;
telephone (202) 267-3073; fax 202-267-7971; e-mail
karen.petronis@faa.gov.
Background
Following the publication of a supplemental notice of proposed
rulemaking on filtered flight data (SNPRM; 73 FR 47857, August 15,
2008), the FAA was contacted by members of the industry seeking
clarification of our intent and the scope of specific provisions. A
summary of that meeting has been placed in the docket for this rule.
Issues raised at the meeting caused us to realize that the intent
of the rule as stated in the preamble is inconsistent with the proposed
rule text. We are restating the intent here and providing revised
proposed rule text.
While this preamble discussion uses part 121 as its reference, it
also applies to parts 125 and 135 and their comparable sections. During
our review, we also discovered that the SNPRM change to a separate
section (proposed Sec. 121.346) caused us to inadvertently omit an
applicability reference for airplanes covered under Sec. 121.344a. We
have added that reference as part of this correction.
The definition of filtering, proposed Sec. 121.346(a), remains as
it was in the SNPRM. Comments should address that section of the
proposed rule as published in the SNPRM.
Proposed Sec. 121.346(b) now states that any parameter required to
be recorded may be filtered as long as the recorded signal value
continues to meet the requirements of Appendix M.
Paragraph (c) contains a list of parameters that we consider
critical from the standpoint of accuracy and accident investigation
when complying with the required accuracy under the expanded definition
of dynamic conditions in Appendix M. This list has not changed from the
SNPRM. If any parameter in the paragraph (c) list is being filtered,
and the filtered, recorded data do not meet Appendix M, then the
certificate holder must choose one of the following courses of action:
Remove the filtering; or
Demonstrate by test and analysis that the original sensor
signal value can be reconstructed from the recorded filtered data. If
an operator attempts to show by test and analysis that the data can be
reconstructed but the tests and analyses fail, or the results cannot be
repeated, the filtering must be removed.
The restructured language of the rule text has obviated the need
for the second list of parameters. They are
[[Page 67116]]
already covered by paragraph (b); they may be filtered as long as the
recorded signal value meets Appendix M. We presume that these
parameters are already in compliance with Appendix M since that
compliance is required by the 1997 rule changes.
The compliance paragraph has been redesignated as (d), and has been
changed to include the correct paragraph references; compliance time
remains unchanged.
All other provisions of the proposed rule, including the definition
of filtering, remain as proposed in the SNPRM published on August 15,
2008. Because of the confusion generated by the SNPRM language
published in August, we are extending the comment period for the rule
as corrected until December 29, 2008.
Correction
PART 121--OPERATING REQUIREMENTS: DOMESTIC, FLAG, AND SUPPLEMENTAL
OPERATIONS
1. On page 47867, in the first column, remove proposed Sec.
121.346(b) and (c) and add in their place corrected paragraphs (b), (c)
and (d) to read as follows:
Sec. 121.346 Flight recorders--filtered data.
* * * * *
(b) An original sensor signal for any flight recorder parameter
required to be recorded under Sec. 121.344 of this part may be
filtered only if the recorded signal value continues to meet the
requirements of Appendix B or M of this part, as applicable.
(c) For a parameter described in Sec. 121.344(a)(1) through (7),
(9), (11) through (18), (26), (32), (42), (43), (68), (70), (77), or
(88), or the corresponding parameter in Appendix B of this part, if the
recorded signal value is filtered and does not meet the requirements of
Appendix B or M of this part, as applicable, the certificate holder
must:
(1) Remove the filtering and ensure that the recorded signal value
meets the requirements of Appendix B or M of this part; or
(2) Demonstrate by test and analysis that the original sensor
signal value can be reconstructed from the recorded data. This
demonstration requires that:
(i) The FAA determine that the procedure submitted by the
certificate holder as its compliance with paragraph (c)(2) of this
section is repeatable; and
(ii) The certificate holder maintain documentation of the procedure
required to reconstruct the original sensor signal value.
(d) Compliance. After (four years from effective date), no aircraft
flight data recording system may filter any parameter listed in
paragraph (c) of this section that does not meet the requirements of
Appendix M or B of this part unless the certificate holder possesses
test and analysis procedures that have been approved by the FAA. The
procedures must be submitted to the FAA no later than the completion of
the next heavy maintenance check after [six months after effective
date] but not later than [two years after the effective date].
2. On page 48767 in the second column, add amendatory instruction
2a to amend section 121.344a(e) to read as follows:
2a. Amend Sec. 121.344a by revising paragraph (e) to read as
follows:
Sec. 121.344a Digital flight data recorders for 10-19 seat airplanes.
* * *
(e) All airplanes subject to this section are also subject to the
requirements and exceptions stated in Sec. Sec. 121.344(g) through (k)
and 121.346 of this part.
* * * * *
PART 125--CERTIFICATION AND OPERATIONS: AIRPLANES HAVING A SEATING
CAPACITY OF 20 OR MORE PASSENGERS OR A MAXIMUM PAYLOAD CAPACITY OF
6,000 POUNDS OR MORE; AND RULES GOVERNING PERSONS ON BOARD SUCH
AIRCRAFT
3. On page 47867, in the second column, remove proposed Sec.
125.228(b) and (c) and add in their place corrected paragraphs (b), (c)
and (d) to read as follows:
Sec. 125.228 Flight recorders--filtered data.
* * * * *
(b) An original sensor signal for any flight recorder parameter
required to be recorded under Sec. 125.226 of this part may be
filtered only if the recorded signal value continues to meet the
requirements of Appendix D or E of this part, as applicable.
(c) For a parameter described in Sec. 125.226 (a)(1) through (7),
(9), (11) through (18), (26), (32), (42), (43), (68), (70), (77), or
(88), or the corresponding parameter in Appendix D of this part if the
recorded signal value is filtered and does not meet the requirements of
Appendix D or E of this part, as applicable, the certificate holder
must:
(1) Remove the filtering and ensure that the recorded signal value
meets the requirements of Appendix D or E of this part; or
(2) Demonstrate by test and analysis that the original sensor
signal value can be reconstructed from the recorded data. This
demonstration requires that:
(i) The FAA determine that the procedure submitted by the
certificate holder as its compliance with paragraph (c)(2) of this
section is repeatable; and
(ii) The certificate holder maintain documentation of the procedure
required to reconstruct the original sensor signal value.
(d) Compliance. After (four years from effective date), no aircraft
flight data recording system may filter any parameter listed in
paragraph (c) of this section that does not meet the requirements of
Appendix D or E of this part unless the certificate holder possesses
test and analysis procedures that have been approved by the FAA. The
procedures must be submitted to the FAA no later than the completion of
the next heavy maintenance check after [six months after effective
date] but not later than [two years after the effective date].
PART 135--OPERATING REQUIREMENTS: COMMUTER AND ON DEMAND OPERATIONS
AND RULES GOVERNING PERSONS ON BOARD SUCH AIRCRAFT
4. On page 47868, in the first column, remove proposed Sec.
135.156(b) and (c) and add in their place corrected paragraphs (b), (c)
and (d) to read as follows:
Sec. 135.156 Flight recorders--filtered data.
* * * * *
(b) An original sensor signal for any flight recorder parameter
required to be recorded under Sec. 135.152 of this part may be
filtered only if the recorded signal value continues to meet the
requirements of Appendix F of this part, as applicable.
(c) For a parameter described in Sec. 135.152(h)(1) through (7),
(9), (11) through (18), (26), (32), (42), (43), (68), (70), (77), or
(88), if the recorded signal value is filtered and does not meet the
requirements of Appendix F of this part, as applicable, the certificate
holder must:
(1) Remove the filtering and ensure that the recorded signal value
meets the requirements of Appendix F of this part; or
(2) Demonstrate by test and analysis that the original sensor
signal value can be reconstructed from the recorded data. This
demonstration requires that:
(i) The FAA determine that the procedure submitted by the
certificate holder as its compliance with paragraph (c)(2) of this
section is repeatable; and
(ii) The certificate holder maintain documentation of the procedure
required to reconstruct the original sensor signal value.
[[Page 67117]]
(d) Compliance. After (four years from effective date), no aircraft
flight data recording system may filter any parameter listed in
paragraph (c) of this section that does not meet the requirements of
Appendix F of this part unless the certificate holder possesses test
and analysis procedures that have been approved by the FAA. The
procedures must be submitted to the FAA no later than the completion of
the next heavy maintenance check after [six months after effective
date] but not later than [two years after the effective date].
Issued in Washington, DC, on November 6, 2008.
Pamela Hamilton-Powell,
Director, Office of Rulemaking.
[FR Doc. E8-26856 Filed 11-12-08; 8:45 am]
BILLING CODE 4910-13-P