Airworthiness Directives; Saab Model SAAB SF340A and SAAB 340B Series Airplanes, 10 [04-28653]
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10
Federal Register / Vol. 70, No. 1 / Monday, January 3, 2005 / Rules and Regulations
the existing coats just beyond the abraded
area. Let the area dry for 30 minutes to 1
hour. Then, apply one sealer coat of
Polyurethane MILC85285 TYI CL2, color
Number 27925 (semi-gloss white) per Fed.
Std. 595. Reinstall the blade.
Note 3: BHT–ALL–SPM, chapter 4,
pertains to painting.
(d) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. Contact the Safety Management Group,
FAA, for information about previously
approved alternative methods of compliance.
(e) Special flight permits may be issued by
following 14 CFR 21.197 and 21.199 to
operate the helicopter to a location where the
requirements of this AD can be accomplished
provided you do not find a crack in the paint
during a check or inspection.
(f) This amendment becomes effective
January 18, 2005.
Note 4: The subject of this AD is addressed
in Transport Canada (Canada) Airworthiness
Directive CF–2004–21, dated October 28,
2004.
Issued in Fort Worth, Texas, on December
23, 2004.
Kim Smith,
Acting Manager, Rotorcraft Directorate,
Aircraft Certification Service.
[FR Doc. 04–28628 Filed 12–30–04; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002–NM–182–AD; Amendment
39–13882; AD 2004–24–06]
RIN 2120–AA64
Airworthiness Directives; Saab Model
SAAB SF340A and SAAB 340B Series
Airplanes
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
SUMMARY: This document corrects a
typographical error that appeared in
airworthiness directive (AD) 2004–24–
06 that was published in the Federal
Register on November 30, 2004 (69 FR
69505). The typographical error resulted
in incorrect reference to certain main
landing gear (MLG) part numbers as
retract actuator bracket attachment bolt
(RABAB) part numbers. This AD is
applicable to certain Saab Model SAAB
SF340A and SAAB 340B series
airplanes. This AD requires replacement
of the RABAB of the MLG with a new
RABAB; reidentification of the MLG
shock strut; an inspection for corrosion,
fretting, or other damage of certain
RABABs; and applicable corrective
actions.
VerDate jul<14>2003
14:40 Dec 30, 2004
Jkt 205001
DATES:
Effective January 4, 2005.
FOR FURTHER INFORMATION CONTACT:
DEPARTMENT OF TRANSPORTATION
Dan
Rodina, Aerospace Engineer;
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2125;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Airworthiness Directive (AD) 2004–24–
06, amendment 39–13882, applicable to
certain Saab Model SAAB SF340A and
SAAB 340B series airplanes, was
published in the Federal Register on
November 30, 2004 (69 FR 69505). That
AD requires replacement of the retract
actuator bracket attachment bolt
(RABAB) of the main landing gear
(MLG) with a new RABAB;
reidentification of the MLG shock strut;
an inspection for corrosion, fretting, or
other damage of certain RABABs; and
applicable corrective actions.
As published, the AD contains an
incorrect reference to the old RABAB
part number. Instead of the RABAB part
number, certain MLG assembly part
numbers were listed as RABAB part
numbers.
Since no other part of the regulatory
information has been changed, the final
rule is not being republished in the
Federal Register.
The effective date of this AD remains
January 4, 2005.
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000–NM–409–AD; Amendment
39–13853; AD 2004–22–25]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 767–200, –300, and –300F Series
Airplanes
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
SUMMARY: This document corrects an
error that appeared in airworthiness
directive (AD) 2004–22–25, which was
published in the Federal Register on
November 9, 2004 (69 FR 64839). The
error resulted in the incorrect reference
to cable spacers. This AD is applicable
to certain Boeing Model 767–200, –300,
and –300F series airplanes. This AD
requires a one-time inspection for
discrepancies of all wire bundles,
including certain power feeder cables,
of the electrical system in the forward
cargo compartment ceiling at certain
stations; and corrective actions if
necessary.
DATES: Effective December 14, 2004.
FOR FURTHER INFORMATION CONTACT:
Elias Natsiopoulos, Aerospace Engineer,
Systems and Equipment Branch, ANM–
130S, FAA, Seattle Aircraft Certification
§ 39.13 [Corrected]
Office, 1601 Lind Avenue, SW., Renton,
Washington 98055–4056; telephone
I In the Federal Register of November
(425) 917–6478; fax (425) 917–6590.
30, 2004, on page 69506, make the
following corrections:
SUPPLEMENTARY INFORMATION:
Airworthiness Directive (AD) 2004–22–
I 1. In the first column, following
instruction 2, the airworthiness directive 25, amendment 39–13853, applicable to
certain Boeing Model 767–200, –300,
number ‘‘2004–24–067’’ is corrected to
and –300F series airplanes, was
read ‘‘2004–24–06’’;
published in the Federal Register on
I 2. In the second column, paragraph (c)
November 9, 2004 (69 FR 64839). That
of this AD 2004–24–06 is corrected to
AD requires a one-time inspection for
read as follows:
discrepancies of all wire bundles,
*
*
*
*
*
including certain power feeder cables,
of the electrical system in the forward
(c) As of the effective date of this AD,
cargo compartment ceiling at certain
no person may install a MLG shock
stations; and corrective actions if
strut, part number (P/N) AIR83022–5
necessary.
through –18 inclusive, or P/N
As published, the third cell of
AIR83064–1 through –5 inclusive, on
any airplane; and no person may install paragraph (a)(2)(ii) of Table 1 of AD
a RABAB, P/N AIR124792, on any MLG 2004–22–25 states, ‘‘* * * install
sleeving, lacing tape, cable spacers, and
shock strut.
straps,’’ in accordance with Boeing Alert
*
*
*
*
*
Service Bulletin 767–24A0128, Revision
Issued in Renton, Washington, on
3, dated June 24, 2004 (cited as the
December 21, 2004.
appropriate service information for
Kevin M. Mullin,
accomplishing the required actions). We
Acting Manager, Transport Airplane
incorrectly specified ‘‘cable spacers’’ as
Directorate, Aircraft Certification Service.
part of the installation requirements if
[FR Doc. 04–28653 Filed 12–28–04; 1:42 pm] the clearance between the power feeder
cables and cargo liner standoffs is less
BILLING CODE 4910–13–P
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]]>Agencies
[Federal Register Volume 70, Number 1 (Monday, January 3, 2005)]
[Rules and Regulations]
[Page 10]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 04-28653]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002-NM-182-AD; Amendment 39-13882; AD 2004-24-06]
RIN 2120-AA64
Airworthiness Directives; Saab Model SAAB SF340A and SAAB 340B
Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document corrects a typographical error that appeared in
airworthiness directive (AD) 2004-24-06 that was published in the
Federal Register on November 30, 2004 (69 FR 69505). The typographical
error resulted in incorrect reference to certain main landing gear
(MLG) part numbers as retract actuator bracket attachment bolt (RABAB)
part numbers. This AD is applicable to certain Saab Model SAAB SF340A
and SAAB 340B series airplanes. This AD requires replacement of the
RABAB of the MLG with a new RABAB; reidentification of the MLG shock
strut; an inspection for corrosion, fretting, or other damage of
certain RABABs; and applicable corrective actions.
DATES: Effective January 4, 2005.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer;
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2004-24-06,
amendment 39-13882, applicable to certain Saab Model SAAB SF340A and
SAAB 340B series airplanes, was published in the Federal Register on
November 30, 2004 (69 FR 69505). That AD requires replacement of the
retract actuator bracket attachment bolt (RABAB) of the main landing
gear (MLG) with a new RABAB; reidentification of the MLG shock strut;
an inspection for corrosion, fretting, or other damage of certain
RABABs; and applicable corrective actions.
As published, the AD contains an incorrect reference to the old
RABAB part number. Instead of the RABAB part number, certain MLG
assembly part numbers were listed as RABAB part numbers.
Since no other part of the regulatory information has been changed,
the final rule is not being republished in the Federal Register.
The effective date of this AD remains January 4, 2005.
Sec. 39.13 [Corrected]
0
In the Federal Register of November 30, 2004, on page 69506, make the
following corrections:
0
1. In the first column, following instruction 2, the airworthiness
directive number ``2004-24-067'' is corrected to read ``2004-24-06'';
0
2. In the second column, paragraph (c) of this AD 2004-24-06 is
corrected to read as follows:
* * * * *
(c) As of the effective date of this AD, no person may install a
MLG shock strut, part number (P/N) AIR83022-5 through -18 inclusive, or
P/N AIR83064-1 through -5 inclusive, on any airplane; and no person may
install a RABAB, P/N AIR124792, on any MLG shock strut.
* * * * *
Issued in Renton, Washington, on December 21, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 04-28653 Filed 12-28-04; 1:42 pm]
BILLING CODE 4910-13-P
