Airworthiness Directives; McDonnell Douglas Model DC-8-33 and -43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; and Model DC-8-50, -60, -60F, -70, and -70F Series Airplanes, 20713-20715 [05-7684]
Download as PDF
<![CDATA[
Federal Register / Vol. 70, No. 76 / Thursday, April 21, 2005 / Rules and Regulations
20713
Actions
Compliance
Procedures
(5) Incorporate changes in the FAA-approved
sailplane flight manual (SFM).
(i) The owner/operator holding at least a private
pilot certificate as authorized by section 43.7
of the Federal Aviation Regulations (14 CFR
43.7) may do the flight manual changes requirement of this AD.
(ii) Make an entry in the aircraft records showing compliance with this portion of the AD following section 43.9 of the Federal Aviation
Regulations (14 CFR 43.9).
Before further flight after the modifications required by paragraphs (e)(1), (e)(2), (e)(3),
and (e)(4) of this AD.
For sailplanes with a SOLO 2625 engine: Follow DG Flugzeugbau GmbH Technical Note
No. 873/26, dated November 12, 2001; For
sailplanes with a Mid-West AE 50T engine:
Follow DG Flugzeugbau GmbH Technical
Note No. 873/27, dated November 29,
2001.
(6) Do not install any SOLO 2625 engine or
Mid-West AE 50T engine unless the modifications required by paragraphs (e)(1),
(e)(2), (e)(3), and (e)(4) of this AD have been
done.
As of June 6, 2005 (the effective date of this
AD).
Not Applicable.
May I Request an Alternative Method of
Compliance?
(f) You may request a different method of
compliance or a different compliance time
for this AD by following the procedures in 14
CFR 39.19. Unless FAA authorizes otherwise,
send your request to your principal
inspector. The principal inspector may add
comments and will send your request to the
Manager, Standards Office, FAA. For
information on any already approved
alternative methods of compliance, contact
Greg Davison, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4130; facsimile: (816)
329–4090.
Issued in Kansas City, Missouri, on April
12, 2005.
Nancy C. Lane,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–7790 Filed 4–20–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–20135; Directorate
Identifier 2003–NM–231–AD; Amendment
39–14060; AD 2005–08–08]
Does This AD Incorporate Any Material by
Reference?
RIN 2120–AA64
(g) You must do the actions required by
this AD following the instructions in DG
Flugzeugbau GmbH Technical Note No. 873/
26, dated November 12, 2001, and DG
Flugzeugbau GmbH Technical Note No. 873/
27, dated November 29, 2001. The Director
of the Federal Register approved the
incorporation by reference of this service
bulletin in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51. You may get a copy from
DG Flugzeugbau, Postbox 41 20, D–76625
Bruchsal, Federal Republic of Germany;
telephone: 011–49 7257–890; facsimile: 011–
49 7257–8922. You may review copies at
FAA, Central Region, Office of the Regional
Counsel, 901 Locust, Room 506, Kansas City,
Missouri 64106; or at the National Archives
and Records Administration (NARA). For
information on the availability of this
material at NARA, call (202) 741–6030, or go
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Airworthiness Directives; McDonnell
Douglas Model DC–8–33 and –43
Airplanes; Model DC–8F–54 and DC–
8F–55 Airplanes; and Model DC–8–50,
–60, –60F, –70, and –70F Series
Airplanes
Is There Other Information That Relates to
This Subject?
(h) German AD Number 2002–083, dated
April 4, 2002, also addresses the subject of
this AD.
VerDate jul<14>2003
16:25 Apr 20, 2005
Jkt 205001
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is superseding an
existing airworthiness directive (AD),
which applies to certain McDonnell
Douglas series airplanes. That AD
currently requires repetitive inspections
of the electrical connectors of the
explosive cartridge wiring of the engine
fire extinguisher containers to verify if
the identification number labels are
installed and legible; repetitive
electrical tests of all explosive cartridge
wiring of the engine fire extinguisher
containers to verify proper installation
and function; and corrective actions if
necessary. This new AD requires an
inspection of the emergency shut off
wire assembly; installation of lanyards
on the electrical connectors for the
PO 00000
Frm 00021
Fmt 4700
Sfmt 4700
engine fire extinguishing agent
containers and for the auxiliary power
unit fire extinguishing agent containers
if applicable; and related investigative/
corrective actions, as applicable. This
AD is prompted by reports of crosswired electrical connectors of the engine
fire extinguishing agent containers. We
are issuing this AD to detect and correct
cross-wired electrical connectors of the
fire extinguishing system, which could
release fire extinguishing agent into the
incorrect engine nacelle in the event of
an engine fire.
DATES: This AD becomes effective May
26, 2005.
The incorporation by reference of a
certain publication listed in the AD is
approved by the Director of the Federal
Register as of May 26, 2005.
On December 20, 2001 (66 FR 63157,
December 5, 2001), the Director of the
Federal Register approved the
incorporation by reference of a certain
other publication listed in the AD.
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, Long Beach
Division, 3855 Lakewood Boulevard,
Long Beach, California 90846,
Attention: Data and Service
Management, Dept. C1–L5A (D800–
0024).
Docket: The AD docket contains the
proposed AD, comments, and any final
disposition. You can examine the AD
docket on the Internet at https://
dms.dot.gov, or in person at the Docket
Management Facility office between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The
Docket Management Facility office
(telephone (800) 647–5227) is located on
the plaza level of the Nassif Building at
the U.S. Department of Transportation,
400 Seventh Street SW., room PL–401,
Washington, DC. This docket number is
FAA–2005–20135; the directorate
E:\FR\FM\21APR1.SGM
21APR1
20714
Federal Register / Vol. 70, No. 76 / Thursday, April 21, 2005 / Rules and Regulations
identifier for this docket is 2003–NM–
231–AD.
FOR FURTHER INFORMATION CONTACT:
William S. Bond, Aerospace Engineer,
Propulsion Branch, ANM–140L, FAA,
Los Angeles Aircraft Certification
Office, 3960 Paramount Boulevard,
Lakewood, California 90712–4137;
telephone (562) 627–5253; fax (562)
627–5210.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend part 39 of the
Federal Aviation Regulations (14 CFR
part 39) with an AD to supersede AD
2001–25–01, amendment 39–12553 (66
FR 63157, December 5, 2001). The
existing AD applies to certain
McDonnell Douglas Model DC–8–33
and –43 airplanes; Model DC–8F–54
and DC–8F–55 airplanes; and Model
DC–8–50, –60, –60F, –70, and –70F
series airplanes. The proposed AD was
published in the Federal Register on
January 28, 2005 (70 FR 4055), to
continue to require repetitive
inspections of the electrical connectors
of the explosive cartridge wiring of the
engine fire extinguisher containers to
verify if the identification number labels
are installed and legible; repetitive
electrical tests of all explosive cartridge
wiring of the engine fire extinguisher
containers to verify proper installation
and function; and corrective actions if
necessary. That action also proposed to
require an inspection of the emergency
shut off wire assembly; installation of
lanyards on the electrical connectors for
the engine fire extinguishing agent
containers and for the auxiliary power
unit (APU) fire extinguishing agent
containers if applicable; and related
investigative/corrective actions, as
applicable.
Comments
We provided the public the
opportunity to participate in the
development of this AD. No comments
have been submitted on the proposed
AD or on the determination of the cost
to the public.
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD as proposed.
Costs of Compliance
There are about 233 airplanes of the
affected design in the worldwide fleet.
The following table provides the
estimated costs, using an average labor
rate of $65 per hour, for U.S. operators
to comply with this AD.
ESTIMATED COSTS
Work
hours
Action
Inspection of the electrical connectors of the explosive
cartridge wiring and electrical test of all explosive cartridge wiring (required by AD 2001–25–01).
General visual inspection of the emergency shut off wire
assembly (new action).
Installation of lanyards on electrical connectors for engine
fire extinguishing agent containers (new action).
Installation of lanyards on electrical APU connectors for
APU fire extinguishing agent containers if applicable
(new action).
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
Section 106, describes the authority of
the FAA Administrator. Subtitle VII,
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in subtitle VII,
part A, subpart III, section 44701,
‘‘General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We have determined that this AD will
not have federalism implications under
VerDate jul<14>2003
16:25 Apr 20, 2005
Jkt 205001
Parts
Cost per airplane
Frm 00022
Fleet cost
3
$0 ...........................
$195, per inspection/
testing cycle.
177
$34,515
1
$0 ...........................
177
11,505
4
$58 (For engine
firex).
$52 (For APU firex)
$65, per inspection
cycle.
$318 ...........................
177
56,268
$117 ...........................
177
20,709
1
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the National Government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this AD. See the ADDRESSES section for
a location to examine the regulatory
evaluation.
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Number of
U.S.registered
airplanes
Fmt 4700
Sfmt 4700
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing amendment 39–12553 (66 FR
63157, December 5, 2001), and by adding
the following new airworthiness
directive (AD):
I
2005–08–08 McDonnell Douglas:
Amendment 39–14060. Docket No.
FAA–2005–20135; Directorate Identifier
2003–NM–231–AD.
E:\FR\FM\21APR1.SGM
21APR1
Federal Register / Vol. 70, No. 76 / Thursday, April 21, 2005 / Rules and Regulations
Effective Date
New Requirements of This AD
(a) This AD becomes effective May 26,
2005.
Inspection and Installation
Affected ADs
(b) This AD supersedes AD 2001–25–01,
amendment 39–12553 (66 FR 63157,
December 5, 2001).
Applicability
(c) This AD applies to McDonnell Douglas
Model DC–8–33, DC–8–43, DC–8–51, DC–8–
52, DC–8–53, DC–8F–54, DC–8–55, DC–8F–
55, DC–8–61, DC–8–61F, DC–8–62, DC–8–
62F, DC–8–63, DC–8–63F, DC–8–71, DC–8–
71F, DC–8–72, DC–8–72F, DC–8–73, and DC–
8–73F airplanes; certificated in any category;
as identified in Boeing Service Bulletin DC8–
26–047, Revision 1, dated September 4, 2003.
Unsafe Condition
(d) This AD was prompted by reports of
cross-wired electrical connectors of the
engine fire extinguishing agent containers.
We are issuing this AD to detect and correct
cross-wired electrical connectors of the fire
extinguishing system, which could release
fire extinguishing agent into the incorrect
engine nacelle in the event of an engine fire.
Compliance
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
Restatement of Requirements of AD 2001–
25–01
Repetitive Inspections and Tests, and
Corrective Action(s), if Necessary
(f) Within 30 days after December 20, 2001
(the effective date of AD 2001–25–01,
amendment 39–12553), do the action(s)
specified in paragraphs (f)(1) and (f)(2) of this
AD, in accordance with Boeing Alert Service
Bulletin DC8–26A046, dated November 7,
2001.
(1) Do an inspection of the electrical
connectors of the explosive cartridge wiring
of the engine fire extinguisher containers to
verify if the identification number labels are
installed and legible. If any identification
number label is missing or is not legible,
before further flight, install a label or replace
the label with a new label, as applicable.
Repeat the inspection after each maintenance
action for the Firex Discharge system.
(2) Do an electrical test of all explosive
cartridge wiring of the engine fire
extinguisher containers to verify proper
installation and function, using the cockpit
warning lamps. If the lamp fails to
illuminate, before further flight, troubleshoot
and repair the wiring of the Firex Discharge
system. Repeat the test after each
maintenance action for the Firex Discharge
system.
Note 1: Inspections, tests, and corrective
actions, if necessary, done per Boeing
BOECOM M–7200–01–02632, dated
November 5, 2001, before December 20, 2001
(the effective date of AD 2001–25–01,
amendment 39–12553), are considered
acceptable for compliance with the
requirements of paragraph (f) of this AD.
VerDate jul<14>2003
16:25 Apr 20, 2005
Jkt 205001
(g) Within 18 months of the effective date
of this AD, do a general visual inspection of
the emergency shut off wire assembly to
determine if the length of wire harness AAG
at P1–510 can be connected to R5–74 and to
determine if the length of wire harness ABG
at P1–511 can be connected to R5–73; and,
before further flight, do the corrective action,
as applicable; by accomplishing all of the
actions specified in paragraph B.1.b. of the
Accomplishment Instructions of Boeing
Service Bulletin DC8–26–047, Revision 1,
dated September 4, 2003.
Note 2: For the purposes of this AD, a
general visual inspection is defined as: ‘‘A
visual examination of an interior or exterior
area, installation, or assembly to detect
obvious damage, failure, or irregularity. This
level of inspection is made from within
touching distance unless otherwise specified.
A mirror may be necessary to enhance visual
access to all exposed surfaces in the
inspection area. This level of inspection is
made under normally available lighting
conditions such as daylight, hangar lighting,
flashlight, or droplight and may require
removal or opening of access panels or doors.
Stands, ladders, or platforms may be required
to gain proximity to the area being checked.’’
(h) Within 18 months of the effective date
of this AD, install lanyards on the electrical
connectors for the engine fire extinguishing
agent containers in the left and right wing
front spar; and, before further flight, do all
the related investigative/corrective actions, as
applicable; by accomplishing all of the
actions specified in paragraph B.1.c. of the
Accomplishment Instructions of Boeing
Service Bulletin DC8–26–047, Revision 1,
dated September 4, 2003.
Installation if Applicable
(i) For airplanes equipped with an
auxiliary power unit (APU) installation in the
forward cargo compartment at station
Y=640.000: Within 18 months of the effective
date of this AD, install lanyards on the
electrical connectors for the APU fire
extinguishing agent containers; and, before
further flight, do all the related investigative/
corrective actions, as applicable; by
accomplishing all of the actions specified in
paragraph B.2. of the Accomplishment
Instructions of Boeing Service Bulletin DC8–
26–047, Revision 1, dated September 4, 2003.
20715
Alternative Methods of Compliance
(AMOCs)
(l) The Manager, Los Angeles Aircraft
Certification Office, FAA, has the authority to
approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
Material Incorporated by Reference
(m) You must use Boeing Service Bulletin
DC8–26–047, Revision 1, dated September 4,
2003; and Boeing Alert Service Bulletin DC8–
26A046, dated November 7, 2001; as
applicable; to perform the actions that are
required by this AD, unless the AD specifies
otherwise.
(1) The incorporation by reference of
Boeing Service Bulletin DC8–26–047,
Revision 1, dated September 4, 2003, is
approved by the Director of the Federal
Register, in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51.
(2) The incorporation by reference of
Boeing Alert Service Bulletin DC8–26A046,
dated November 7, 2001, was approved
previously by the Director of the Federal
Register as of December 20, 2001 (66 FR
63157, December 5, 2001).
(3) To get copies of the service information,
contact Boeing Commercial Airplanes, Long
Beach Division, 3855 Lakewood Boulevard,
Long Beach, California 90846, Attention:
Data and Service Management, Dept. C1–L5A
(D800–0024. To view the AD docket, go to
the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh
Street SW., room PL–401, Nassif Building,
Washington, DC. To review copies of the
service information, go to the National
Archives and Records Administration
(NARA). For information on the availability
of this material at the NARA, call (202) 741–
6030, or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on April 11,
2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–7684 Filed 4–20–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Terminating Action
(j) Accomplishment of the actions specified
in paragraphs (g) and (h) of this AD
terminates the repetitive inspections and
electrical tests required by paragraph (f) of
this AD.
[Docket No. FAA–2004–19522; Directorate
Identifier 2004–CE–36–AD; Amendment 39–
14064; AD 2005–08–12]
RIN 2120–AA64
Credit for Previous Service Bulletin
(k) Actions done before the effective date
of this AD in accordance with Boeing Service
Bulletin DC8–26–047, dated April 2, 2003,
are acceptable for compliance with the
corresponding requirements in paragraphs
(g), (h), and (i) of this AD.
PO 00000
Frm 00023
Fmt 4700
Sfmt 4700
Airworthiness Directives; CENTRAIR
101 Series Gliders
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA adopts a new
airworthiness directive (AD) for certain
E:\FR\FM\21APR1.SGM
21APR1
]]>Agencies
[Federal Register Volume 70, Number 76 (Thursday, April 21, 2005)]
[Rules and Regulations]
[Pages 20713-20715]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-7684]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20135; Directorate Identifier 2003-NM-231-AD;
Amendment 39-14060; AD 2005-08-08]
RIN 2120-AA64
Airworthiness Directives; McDonnell Douglas Model DC-8-33 and -43
Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; and Model DC-8-50, -
60, -60F, -70, and -70F Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding an existing airworthiness directive
(AD), which applies to certain McDonnell Douglas series airplanes. That
AD currently requires repetitive inspections of the electrical
connectors of the explosive cartridge wiring of the engine fire
extinguisher containers to verify if the identification number labels
are installed and legible; repetitive electrical tests of all explosive
cartridge wiring of the engine fire extinguisher containers to verify
proper installation and function; and corrective actions if necessary.
This new AD requires an inspection of the emergency shut off wire
assembly; installation of lanyards on the electrical connectors for the
engine fire extinguishing agent containers and for the auxiliary power
unit fire extinguishing agent containers if applicable; and related
investigative/corrective actions, as applicable. This AD is prompted by
reports of cross-wired electrical connectors of the engine fire
extinguishing agent containers. We are issuing this AD to detect and
correct cross-wired electrical connectors of the fire extinguishing
system, which could release fire extinguishing agent into the incorrect
engine nacelle in the event of an engine fire.
DATES: This AD becomes effective May 26, 2005.
The incorporation by reference of a certain publication listed in
the AD is approved by the Director of the Federal Register as of May
26, 2005.
On December 20, 2001 (66 FR 63157, December 5, 2001), the Director
of the Federal Register approved the incorporation by reference of a
certain other publication listed in the AD.
ADDRESSES: For service information identified in this AD, contact
Boeing Commercial Airplanes, Long Beach Division, 3855 Lakewood
Boulevard, Long Beach, California 90846, Attention: Data and Service
Management, Dept. C1-L5A (D800-0024).
Docket: The AD docket contains the proposed AD, comments, and any
final disposition. You can examine the AD docket on the Internet at
https://dms.dot.gov, or in person at the Docket Management Facility
office between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the U.S.
Department of Transportation, 400 Seventh Street SW., room PL-401,
Washington, DC. This docket number is FAA-2005-20135; the directorate
[[Page 20714]]
identifier for this docket is 2003-NM-231-AD.
FOR FURTHER INFORMATION CONTACT: William S. Bond, Aerospace Engineer,
Propulsion Branch, ANM-140L, FAA, Los Angeles Aircraft Certification
Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137;
telephone (562) 627-5253; fax (562) 627-5210.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend part 39 of the
Federal Aviation Regulations (14 CFR part 39) with an AD to supersede
AD 2001-25-01, amendment 39-12553 (66 FR 63157, December 5, 2001). The
existing AD applies to certain McDonnell Douglas Model DC-8-33 and -43
airplanes; Model DC-8F-54 and DC-8F-55 airplanes; and Model DC-8-50, -
60, -60F, -70, and -70F series airplanes. The proposed AD was published
in the Federal Register on January 28, 2005 (70 FR 4055), to continue
to require repetitive inspections of the electrical connectors of the
explosive cartridge wiring of the engine fire extinguisher containers
to verify if the identification number labels are installed and
legible; repetitive electrical tests of all explosive cartridge wiring
of the engine fire extinguisher containers to verify proper
installation and function; and corrective actions if necessary. That
action also proposed to require an inspection of the emergency shut off
wire assembly; installation of lanyards on the electrical connectors
for the engine fire extinguishing agent containers and for the
auxiliary power unit (APU) fire extinguishing agent containers if
applicable; and related investigative/corrective actions, as
applicable.
Comments
We provided the public the opportunity to participate in the
development of this AD. No comments have been submitted on the proposed
AD or on the determination of the cost to the public.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD as proposed.
Costs of Compliance
There are about 233 airplanes of the affected design in the
worldwide fleet. The following table provides the estimated costs,
using an average labor rate of $65 per hour, for U.S. operators to
comply with this AD.
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Number of
Work U.S.-
Action hours Parts Cost per airplane registered Fleet cost
airplanes
----------------------------------------------------------------------------------------------------------------
Inspection of the electrical 3 $0........................ $195, per 177 $34,515
connectors of the explosive inspection/
cartridge wiring and testing cycle.
electrical test of all
explosive cartridge wiring
(required by AD 2001-25-01).
General visual inspection of 1 $0........................ $65, per 177 11,505
the emergency shut off wire inspection cycle.
assembly (new action).
Installation of lanyards on 4 $58 (For engine firex).... $318............. 177 56,268
electrical connectors for
engine fire extinguishing
agent containers (new action).
Installation of lanyards on 1 $52 (For APU firex)....... $117............. 177 20,709
electrical APU connectors for
APU fire extinguishing agent
containers if applicable (new
action).
----------------------------------------------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
subtitle VII, part A, subpart III, section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the National Government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD. See the ADDRESSES section for a location to
examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
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2. The FAA amends Sec. 39.13 by removing amendment 39-12553 (66 FR
63157, December 5, 2001), and by adding the following new airworthiness
directive (AD):
2005-08-08 McDonnell Douglas: Amendment 39-14060. Docket No. FAA-
2005-20135; Directorate Identifier 2003-NM-231-AD.
[[Page 20715]]
Effective Date
(a) This AD becomes effective May 26, 2005.
Affected ADs
(b) This AD supersedes AD 2001-25-01, amendment 39-12553 (66 FR
63157, December 5, 2001).
Applicability
(c) This AD applies to McDonnell Douglas Model DC-8-33, DC-8-43,
DC-8-51, DC-8-52, DC-8-53, DC-8F-54, DC-8-55, DC-8F-55, DC-8-61, DC-
8-61F, DC-8-62, DC-8-62F, DC-8-63, DC-8-63F, DC-8-71, DC-8-71F, DC-
8-72, DC-8-72F, DC-8-73, and DC-8-73F airplanes; certificated in any
category; as identified in Boeing Service Bulletin DC8-26-047,
Revision 1, dated September 4, 2003.
Unsafe Condition
(d) This AD was prompted by reports of cross-wired electrical
connectors of the engine fire extinguishing agent containers. We are
issuing this AD to detect and correct cross-wired electrical
connectors of the fire extinguishing system, which could release
fire extinguishing agent into the incorrect engine nacelle in the
event of an engine fire.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Restatement of Requirements of AD 2001-25-01
Repetitive Inspections and Tests, and Corrective Action(s), if
Necessary
(f) Within 30 days after December 20, 2001 (the effective date
of AD 2001-25-01, amendment 39-12553), do the action(s) specified in
paragraphs (f)(1) and (f)(2) of this AD, in accordance with Boeing
Alert Service Bulletin DC8-26A046, dated November 7, 2001.
(1) Do an inspection of the electrical connectors of the
explosive cartridge wiring of the engine fire extinguisher
containers to verify if the identification number labels are
installed and legible. If any identification number label is missing
or is not legible, before further flight, install a label or replace
the label with a new label, as applicable. Repeat the inspection
after each maintenance action for the Firex Discharge system.
(2) Do an electrical test of all explosive cartridge wiring of
the engine fire extinguisher containers to verify proper
installation and function, using the cockpit warning lamps. If the
lamp fails to illuminate, before further flight, troubleshoot and
repair the wiring of the Firex Discharge system. Repeat the test
after each maintenance action for the Firex Discharge system.
Note 1: Inspections, tests, and corrective actions, if
necessary, done per Boeing BOECOM M-7200-01-02632, dated November 5,
2001, before December 20, 2001 (the effective date of AD 2001-25-01,
amendment 39-12553), are considered acceptable for compliance with
the requirements of paragraph (f) of this AD.
New Requirements of This AD
Inspection and Installation
(g) Within 18 months of the effective date of this AD, do a
general visual inspection of the emergency shut off wire assembly to
determine if the length of wire harness AAG at P1-510 can be
connected to R5-74 and to determine if the length of wire harness
ABG at P1-511 can be connected to R5-73; and, before further flight,
do the corrective action, as applicable; by accomplishing all of the
actions specified in paragraph B.1.b. of the Accomplishment
Instructions of Boeing Service Bulletin DC8-26-047, Revision 1,
dated September 4, 2003.
Note 2: For the purposes of this AD, a general visual inspection
is defined as: ``A visual examination of an interior or exterior
area, installation, or assembly to detect obvious damage, failure,
or irregularity. This level of inspection is made from within
touching distance unless otherwise specified. A mirror may be
necessary to enhance visual access to all exposed surfaces in the
inspection area. This level of inspection is made under normally
available lighting conditions such as daylight, hangar lighting,
flashlight, or droplight and may require removal or opening of
access panels or doors. Stands, ladders, or platforms may be
required to gain proximity to the area being checked.''
(h) Within 18 months of the effective date of this AD, install
lanyards on the electrical connectors for the engine fire
extinguishing agent containers in the left and right wing front
spar; and, before further flight, do all the related investigative/
corrective actions, as applicable; by accomplishing all of the
actions specified in paragraph B.1.c. of the Accomplishment
Instructions of Boeing Service Bulletin DC8-26-047, Revision 1,
dated September 4, 2003.
Installation if Applicable
(i) For airplanes equipped with an auxiliary power unit (APU)
installation in the forward cargo compartment at station Y=640.000:
Within 18 months of the effective date of this AD, install lanyards
on the electrical connectors for the APU fire extinguishing agent
containers; and, before further flight, do all the related
investigative/corrective actions, as applicable; by accomplishing
all of the actions specified in paragraph B.2. of the Accomplishment
Instructions of Boeing Service Bulletin DC8-26-047, Revision 1,
dated September 4, 2003.
Terminating Action
(j) Accomplishment of the actions specified in paragraphs (g)
and (h) of this AD terminates the repetitive inspections and
electrical tests required by paragraph (f) of this AD.
Credit for Previous Service Bulletin
(k) Actions done before the effective date of this AD in
accordance with Boeing Service Bulletin DC8-26-047, dated April 2,
2003, are acceptable for compliance with the corresponding
requirements in paragraphs (g), (h), and (i) of this AD.
Alternative Methods of Compliance (AMOCs)
(l) The Manager, Los Angeles Aircraft Certification Office, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19.
Material Incorporated by Reference
(m) You must use Boeing Service Bulletin DC8-26-047, Revision 1,
dated September 4, 2003; and Boeing Alert Service Bulletin DC8-
26A046, dated November 7, 2001; as applicable; to perform the
actions that are required by this AD, unless the AD specifies
otherwise.
(1) The incorporation by reference of Boeing Service Bulletin
DC8-26-047, Revision 1, dated September 4, 2003, is approved by the
Director of the Federal Register, in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51.
(2) The incorporation by reference of Boeing Alert Service
Bulletin DC8-26A046, dated November 7, 2001, was approved previously
by the Director of the Federal Register as of December 20, 2001 (66
FR 63157, December 5, 2001).
(3) To get copies of the service information, contact Boeing
Commercial Airplanes, Long Beach Division, 3855 Lakewood Boulevard,
Long Beach, California 90846, Attention: Data and Service
Management, Dept. C1-L5A (D800-0024. To view the AD docket, go to
the Docket Management Facility, U.S. Department of Transportation,
400 Seventh Street SW., room PL-401, Nassif Building, Washington,
DC. To review copies of the service information, go to the National
Archives and Records Administration (NARA). For information on the
availability of this material at the NARA, call (202) 741-6030, or
go to https://www.archives.gov/federal_register/code_of_federal_
regulations/ibr_locations.html.
Issued in Renton, Washington, on April 11, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-7684 Filed 4-20-05; 8:45 am]
BILLING CODE 4910-13-P
