Nachrichten für Luftfahrer 2006 Teil II (weicht ggf. von Druckversion ab)
Do— Of— For— (2) If any midpivot bolt of the spring beam of the inboard side of the outboard struts is found in
(2) A general visual inspection The anti-rotation Damage (i.e., wear, nicks, gouges, or cracks) the incorrect position and if no damage is found on that bolt during any inspection required by
tabs of the midpivot or any missing tab. paragraph (f) of this AD.
bolt access doors.
(3) A general visual inspection The midpivot bolts Correct position or damage (i.e., nicks, Parts Installation
gouges, or cracks).
(4) An ultrasonic inspection The midpivot bolts Cracks. (i) As of the effective date of this AD, no person may install, on any airplane, a midpivot access
door, part number 65B89670-339, 65B89670-340, 654U6624-356, or 654U6624-357, unless it has
Note 1: There is a discrepancy in Step 2 of Figure 13, Sheet 2, of Boeing Alert Service Bulletin been inspected in accordance with paragraphs (f)(1) and (f)(2) of this AD and found to have the
747-54A2225, dated February 16, 2006. The ''MORE DATA'' column of the table incorrectly correct part number for the door location, no damage, and no damaged or missing anti-rotation tab.
describes the anti-rotation slot installation as being ''horizontal and are perpendicular to the strut skin
aft edge.'' The correct description is ''vertical and are parallel to the strut skin aft edge.'' No Reporting
Installation of a Placard and Corrective Actions (j) Although the service bulletin referenced in this AD specifies to submit certain information to
the manufacturer, this AD does not include that requirement.
(g) Before further flight after doing the inspections required by paragraph (f) of this AD, do the
applicable actions specified in Table 2 of this AD in accordance with the Accomplishment Alternative Methods of Compliance (AMOCs)
Instructions of Boeing Alert Service Bulletin 747-54A2225, dated February 16, 2006.
(k)(1) The Manager, Seattle Aircraft Certification Office (ACO), FAA, has the authority to
TABLE 2.—INSTALLATION OF A PLACARD AND CORRECTIVE ACTION approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the
If— And if— Then—
AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate
(1) Any midpivot bolt access Its anti-rotation tabs are Install a placard on the midpivot Holding District Office.
door has the correct part present, are in the correct access door. (3) An AMOC that provides an acceptable level of safety may be used for any repair required by
number and no damage. position, and have no damage. this AD, if it is approved by an Authorized Representative for the Boeing Commercial Airplanes
(2) Any midpivot bolt access Its anti-rotation tabs are Change the midpivot access door or Delegation Option Authorization Organization who has been authorized by the Manager, Seattle
door has the incorrect part present, are in the incorrect replace it with a new or serviceable ACO, to make those findings. For a repair method to be approved, the repair must meet the
number and no damage. position, and have no damage. access door, and install a placard certification basis of the airplane, and the approval must specifically refer to this AD.
on the midpivot access door.
(3) Any midpivot bolt access None Replace the midpivot access door Material Incorporated by Reference
door has the incorrect part with a new or serviceable door and
number, any damage, or any install a placard on the door. (1) You must use Boeing Alert Service Bulletin 747-54A2225, dated February 16, 2006, to
damaged or missing anti- perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of
rotation tab. the Federal Register approved the incorporation by reference of this document in accordance with 5
(4) Any midpivot bolt is in the It has no damage No further action is required by this U.S.C. 552(a) and 1 CFR part 51. Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle,
correct position paragraph. WA 98124-2207, for a copy of this service information. You may review copies at the Docket
(5) Any midpivot bolt is in the It has no damage Correct the midpivot bolt position. Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Room PL-401,
incorrect position Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives
Any midpivot bolt has any None Replace the midpivot bolt with a and Records Administration (NARA). For information on the availability of this material at the
damage new bolt. NARA, call (202) 741-6030, or go to
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Replacement of Midpivot Bolt
Issued in Renton, Washington, on May 26, 2006.
(h) If any condition in paragraph (h)(1) or (h)(2) of this AD is found on any outboard strut, Jeffrey E. Duven,
within 24 months after doing the inspections required by paragraph (f) of this AD, replace the Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
midpivot bolt of the spring beam of the inboard side of that outboard strut with a new midpivot bolt, [FR Doc. 06-5125 Filed 6-6-06; 8:45 am]
in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 747-54A2225, BILLING CODE 4910-13-P
dated February 16, 2006.
(1) If any midpivot bolt access door of the spring beam of the inboard side of the outboard struts
is found in the incorrect position (i.e., the midpivot bolt access door has the incorrect part number or
its anti-rotation tabs are in the incorrect position) and if no damage is found on that bolt during any
inspection required by paragraph (f) of this AD.
7 8
Lufttüchtigkeitsanweisung
LTA-Nr.: D-2006-224
EASA AIRWORTHINESS DIRECTIVE
Luftfahrt-Bundesamt
Datum der Bekanntgabe: 16.08.2006
Muster: Airbus AD der ausländischen Behörde:
A330 EASA AD 2006-0224 vom 27.07.2006 AD No.: 2006 – 0224
Geräte-Nr.: Technische Mitteilungen des Herstellers:
2849 AIRBUS A330 Certification Maintenance Requirements Issue 19,
Referenznummer 955.2074/93 mit EASA-Zulassung,
Referenznummer EASA.A.C.03878, vom 22.06.2006. Date: 27 July 2006
Betroffenes Luftfahrtgerät:
No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with the
Airbus requirements of that Airworthiness Directive unless otherwise agreed with the Authority of the State of Registry.
A330
Type Approval Holder’s Name : Type/Model designation(s) :
- Baureihen: Alle
AIRBUS SAS A330 Aircraft
- Werk-Nrn.: Alle
TCDS Number : EASA A.004
Betrifft:
Festlegung neuer Forderungen für Wartung und Instandhaltung in dem Dokument ''Certification Foreign AD : None
Maintenance Requirements (CMR)'', Airbus-Referenznummer 955.2074/93.
Maßnahmen: Supersedure : None
Detaillierte Informationen über die durchzuführenden Maßnahmen sind der oben genannten EASA
Airworthiness Directive und der genannten technischen Mitteilung des Herstellers zu entnehmen.
Alle erforderlichen Maßnahmen zur Abstellung des technischen Mangels müssen ordnungsgemäß, Time Limits - Airworthiness Limitations - Certification
vollständig und innerhalb der vorgesehen Fristen auf Basis der genannten Bezugsdokumente durchge- ATA 05
Maintenance Requirements (CMR)
führt werden. Alle Abweichungen von den Maßnahmen und Fristen dieser Lufttüchtigkeitsanweisung
bedürfen der vorherigen Zustimmung durch das Luftfahrt-Bundesamt.
Fristen: Manufacturer(s): AIRBUS (formerly AIRBUS INDUSTRIE)
Alle anzuwendenden Fristen sind der oben genannten EASA Airworthiness Directive zu entnehmen.
Die Laufzeit aller anzuwendenden Fristen beginnt mit dem Datum der Inkraftsetzung der genannten Applicability: AIRBUS A330 aircraft, all certified models, all serial numbers.
EASA Airworthiness Directive.
Diese Lufttüchtigkeitsanweisung entspricht hinsichtlich der durchzuführenden Maßnahmen und Fristen der Reason: The certification requirements for systems are provided in AIRBUS A330
EASA AD 2006-0224 vom 27.07.2006 Airworthiness Limitation Section (ALS) Part 3 Document (Certification
Durch die vorgenannten Mängel ist die Lufttüchtigkeit des Luftfahrtgerätes derart beeinträchtigt, daß es nach Ablauf der genannten Fristen Maintenance Requirements - CMR). This A330 CMR document is
nur in Betrieb genommen werden darf, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind. Im Interesse der referenced 955.2074/93 and approved by the European Aviation Safety
Sicherheit des Luftverkehrs, das in diesem Fall das Interesse des Adressaten am Aufschub der angeordneten Maßnahmen überwiegt, ist es
erforderlich, die sofortige Vollziehung dieser LTA anzuordnen.
Agency (EASA).
This Airworthiness Directive (AD) mandates the A330 CMR requirements
Rechtsbehelfsbelehrung:
Gegen diese Verfügung kann innerhalb eines Monats nach Bekanntgabe Widerspruch eingelegt werden. Der Widerspruch ist schriftlich oder as defined in AIRBUS document 955.2074/93 issue 19 which:
zur Niederschrift beim Luftfahrt-Bundesamt, Hermann-Blenk-Str. 26, 38108 Braunschweig einzulegen.
introduces the impact of increasing the Design Service Goal
LTAs werden auch im Internet unter http://www.lba.de publiziert (DSG) for the Weight Variant 50 series,
***
adds new CMR tasks with more restrictive limitations associated
with modifications and new DSG,
changes status of one task from Two Star to One Star with
interval extension.
The issue 19 of the A330 CMR document introduces more restrictive
requirements for aircraft configuration already in service.
1/2
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Lufttüchtigkeitsanweisung
LTA-Nr.: D-2006-225
Effective Date: 11 August 2006
Luftfahrt-Bundesamt
Compliance: From the effective date of this AD, it is mandatory to adhere to the
Datum der Bekanntgabe: 16.08.2006
requirements defined in the AIRBUS A330 Certification Maintenance Muster: Boeing AD der ausländischen Behörde:
Requirements document referenced 955.2074/93 at issue 19. BOEING 737 FAA AD 2006-12-06 Amdt. 39-14631
For any new CMR task introduced by A330 CMR Document Issue 19 the BOEING 747
associated interval is to be counted from the effective date of this AD. BOEING 757
For CMR task that has been revised by A330 CMR Document Issue 19 BOEING 767
the interval is to be counted from the previous performance of the task. BOEING 777
Geräte-Nr.: Technische Mitteilungen des Herstellers:
Ref. Publications: AIRBUS A330 CMR issue 19 referenced 955.2074/93 approved on 22
2823, 2832, 2845, 2851, 2863 Boeing Service Bulletin 737-25-1438 Revision 1 vom 11.11.2004
June 2006 under Ref. EASA.A.C.03878
Boeing Service Bulletin 737-25-1439 Revision 3 vom 11.11.2004
or later approved revisions. Boeing Service Bulletin 747-25-3264 Revision 1 vom 11.11.2004
Boeing Service Bulletin 747-25-3275 Revision 1 vom 04.04.2002
Remarks : 1. If requested and appropriately substantiated the responsible EASA Boeing Service Bulletin 757-25-0238 Revision 2 vom 11.11.2004
manager for the related product has the authority to accept Alternative Boeing Service Bulletin 767-25-0297 Revision 1 vom 11.11.2004
Methods of Compliance (AMOCs) for this AD. Boeing Service Bulletin 777-25-0180 Revision 1 vom 11.11.2004
2. This AD was posted as PAD 06-172 for consultation on 30 June 2006
with a comment period until 14 July 2006. The comment Response Betroffenes Luftfahrtgerät:
Document can be found at http://ad.easa.eu.int/.
Boeing
3. Enquiries regarding this Airworthiness Directive should be referred to BOEING 737, BOEING 747, BOEING 757, BOEING 767, BOEING 777
Mr. M. Capaccio, Airworthiness Directive Focal Point - Certification
Directorate, EASA. E-mail: ADs@easa.europa.eu - Baureihen: 737-300, -400, -500, -700 und -800, 747-400 und -400F, 757-200, 767-300, 777-300
4. For any question concerning the technical content of the requirements
in this AD, please contact AIRBUS SAS –Airworthiness Office - EAL - Werk-Nrn.: Alle
Fax: +33 5 61 93 45 80. -- ausgerüstet mit DRIESSEN Aircraft Interior Systems Bordküchen
oder
-- ausgerüstet mit SHOWA Aircraft Industries Bordküchen
Betrifft:
AUSRÜSTUNG/EINRICHTUNGEN (ATA: 25): Bordküchen - Schutzumwicklung der Küchenverkabelung
Maßnahmen:
Detaillierte Informationen über die durchzuführenden Maßnahmen sind der oben genannten FAA Airworthiness
Directive (AD) und den genannten technischen Mitteilungen des Herstellers zu entnehmen. Alle erforderlichen
Maßnahmen zur Abstellung des technischen Mangels müssen ordnungsgemäß, vollständig und innerhalb der
vorgesehen Fristen auf Basis der genannten Bezugsdokumente durchgeführt werden. Alle Abweichungen von
den Maßnahmen und Fristen dieser Lufttüchtigkeitsanweisung bedürfen der vorherigen Zustimmung durch das
Luftfahrt-Bundesamt.
Fristen:
Alle anzuwendenden Fristen sind der oben genannten FAA Airworthiness Directive (AD) zu entnehmen. Die
Laufzeit aller anzuwendenden Fristen beginnt mit dem Datum der Inkraftsetzung der genannten FAA
Airworthiness Directive (AD).
Diese Lufttüchtigkeitsanweisung entspricht hinsichtlich der durchzuführenden Maßnahmen und Fristen der
FAA AD 2006-12-06 Amdt. 39-14631
Durch die vorgenannten Mängel ist die Lufttüchtigkeit des Luftfahrtgerätes derart beeinträchtigt, daß es nach Ablauf der genannten Fristen
nur in Betrieb genommen werden darf, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind. Im Interesse der
Sicherheit des Luftverkehrs, das in diesem Fall das Interesse des Adressaten am Aufschub der angeordneten Maßnahmen überwiegt, ist es
erforderlich, die sofortige Vollziehung dieser LTA anzuordnen.
Rechtsbehelfsbelehrung:
Gegen diese Verfügung kann innerhalb eines Monats nach Bekanntgabe Widerspruch eingelegt werden. Der Widerspruch ist schriftlich oder
zur Niederschrift beim Luftfahrt-Bundesamt, Hermann-Blenk-Str. 26, 38108 Braunschweig einzulegen.
LTAs werden auch im Internet unter http://www.lba.de publiziert
***
2/2
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TABLE 1.—SERVICE BULLETINS AND SPECIAL ATTENTION SERVICE BULLETINS
AIRWORTHINESS DIRECTIVE U.S. Department
of Transportation Model and service information Revision level Date
www.faa.gov/aircraft/safety/alerts/ Federal Aviation (1) Boeing Special Attention Service Bulletin 737–25– 1 November 11, 2004.
Administration 1438, for Model 737–300, –400, and –500 series airplanes.
www.gpoaccess.gov/fr/advanced.html
(2) Boeing Service Bulletin 737–25–1439, for Model 737– 3 November 11, 2004.
2006-12-06 Boeing: Amendment 39-14631. Docket No. FAA-2005-22628; Directorate Identifier 700 and –800 series airplanes
2005-NM-056-AD. (3) Boeing Special Attention Service Bulletin 747–25– 1 November 11, 2004.
3264, for Model 747–400 series airplanes
Effective Date (4) Boeing Service Bulletin 747–25–3275, for Model 747– 1 April 4, 2002.
400F series airplanes
(a) This AD becomes effective July 12, 2006. (5) Boeing Special Attention 757–25–0238, for Model 757– 2 November 11, 2004.
200 series airplanes
Affected ADs (6) Boeing Special Attention Service Bulletin 767–25– 1 November 11, 2004.
0297, for Model 767–300 series airplanes
(b) None. (7) Boeing Special Attention Service Bulletin 1 November 1 November 11, 2004.
777–25–0180 for Model 777–300 series airplanes.
Applicability
Note 2: The service bulletins and special attention service bulletins specified in Table 1 of this
(c) This AD applies to Boeing transport category airplanes equipped with certain Driessen AD reference Driessen Aircraft Interior Systems Service Bulletin 25-442, Revision E, dated April 29,
Aircraft Interior Systems or Showa Aircraft Industries galleys, certificated in any category; as 2004; and Showa Aircraft Industry Service Bulletin 25-30-111, dated December 11, 2000; as
identified in paragraphs (c)(1) through (c)(5) inclusive of this AD. applicable; as additional sources of service information.
(1) Model 737-300, -400, -500, -700, and -800 series airplanes;
(2) Model 747-400 and 747-400F series airplanes; If Certain Galleys Are Not Installed
(3) Model 757-200 series airplanes;
(4) Model 767-300 series airplanes; and (g) If no galley is installed having any P/N identified in the service information specified in
(5) Model 777-300 series airplanes. paragraph (f) of this AD, no further action is required by this AD.
Unsafe Condition If Certain Galleys Are Installed
(d) This AD results from testing and reports from the manufacturer indicating unacceptable (h) If any galley is installed having any P/N identified in the service information specified in
flammability properties of wire wrapping installed in certain galleys and closets. We are issuing this paragraph (f) of this AD: Within 72 months after the effective date of this AD, replace the spiral
AD to prevent fire propagation or smoke in the cabin area due to electrical arcing or sparking and protective wrapping of the electrical cables of the galley with new spiral protective wrapping that has
ignition of the spiral wire wrapping. been shown to meet certain flammability testing requirements, in accordance with the applicable
service information specified in paragraph (f) of this AD.
Compliance
Credit for Previous Replacement
(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. (i) Replacement of the spiral protective wrapping of the electrical cables of any galley with new
spiral protective wrapping that has been shown to meet certain flammability testing requirements, in
Note 1: For clarification and for the purposes of this AD, the use of the term ''galley'' also accordance with the service information listed in the Table 2 of this AD, prior to the effective date of
includes the terms ''buffet'' and ''closet'' that are referenced in certain service information specified in this AD, is acceptable for compliance with the requirements of paragraph (h) of this AD.
this AD.
TABLE 2.—PREVIOUS ACCOMPLISHMENT
Determination of Part Installation Boeing service information Revision level Date
(1) Special Attention Service Bulletin 737–25–1438 Original March 15, 2001.
(f) Within 72 months after the effective date of this AD, inspect the galleys to determine if any of (2) Special Attention Service Bulletin 737–25–1439 Original March 15, 2001.
the part numbers (P/Ns) installed are identified in the applicable service information specified in (3) Special Attention Service Bulletin 737–25–1439 1 August 2, 2001.
Table 1 of this AD. Instead of inspecting the galleys to determine if the P/Ns are installed, a review of (4) Service Bulletin 737–25–1439 2 December 19, 2001.
airplane maintenance records is acceptable if the P/Ns can be positively determined from that review. (5) Special Attention Service Bulletin 747–25–3264 Original March 15, 2001.
(6) Special Attention Service Bulletin 747–25–3275 Original March 15, 2001.
7 8
Boeing service information Revision level Date Lufttüchtigkeitsanweisung
(7) Special Attention Service Bulletin 757–25–0238 Original March 15, 2001. LTA-Nr.: D-2006-227
(8) Special Attention Service Bulletin 757–25–0238 1 November 15, 2001.
(9) Special Attention Service Bulletin 767–25–0297 Original March 15, 2001. Luftfahrt-Bundesamt
Datum der Bekanntgabe: 17.08.2006
(10) Special Attention Service Bulletin 777–25–0180 Original March 15, 2001.
Muster: Airbus AD der ausländischen Behörde:
A340 EASA AD 2006-0225 vom 21.07.2006
Alternative Methods of Compliance (AMOCs)
Geräte-Nr.: Technische Mitteilungen des Herstellers:
(j)(1) The Manager, Seattle Aircraft Certification Office (ACO), FAA, has the authority to 2850 AIRBUS A340 Certification Maintenance Requirements Issue 14,
Referenznummer 955.3019/92 mit EASA-Zulassung,
approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. Referenznummer EASA.A.414, vom 24.04.2006.
(2) Before using any AMOC approved in accordance with 14 CFR 39.19 on any airplane to
which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Betroffenes Luftfahrtgerät:
Certificate Holding District Office.
Airbus
Material Incorporated by Reference A340
- Baureihen: Alle
(k) You must use the applicable service information in Table 3 of this AD to perform the actions
that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register - Werk-Nrn.: Alle
approved the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and
1 CFR part 51. Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124- Betrifft:
2207, for a copy of this service information. You may review copies at the Docket Management Festlegung neuer Forderungen für Wartung und Instandhaltung in dem Dokument ''Certification
Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Room PL-401, Nassif Maintenance Requirements (CMR)'', Airbus-Referenznummer 955.3019/92.
Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and
Records Administration (NARA). For information on the availability of this material at the NARA, Maßnahmen:
Detaillierte Informationen über die durchzuführenden Maßnahmen sind der oben genannten EASA
call (202) 741-6030, or go to Airworthiness Directive und der genannten technischen Mitteilung des Herstellers zu entnehmen.
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. Alle erforderlichen Maßnahmen zur Abstellung des technischen Mangels müssen ordnungsgemäß,
vollständig und innerhalb der vorgesehen Fristen auf Basis der genannten Bezugsdokumente durchge-
TABLE 3.—MATERIAL INCORPORATED BY REFERENCE führt werden. Alle Abweichungen von den Maßnahmen und Fristen dieser Lufttüchtigkeitsanweisung
bedürfen der vorherigen Zustimmung durch das Luftfahrt-Bundesamt.
Service information Revision level Date
(1) Boeing Special Attention Service Bulletin 737–25–1438 1 November 11, 2004. Fristen:
(2) Boeing Service Bulletin 737–25–1439 3 November 11, 2004. Alle anzuwendenden Fristen sind der oben genannten EASA Airworthiness Directive zu entnehmen.
(3) Boeing Special Attention Service Bulletin 747–25–3264 1 November 11, 2004. Die Laufzeit aller anzuwendenden Fristen beginnt mit dem Datum der Inkraftsetzung der genannten
(4) Boeing Service Bulletin 747–25–3275 1 April 4, 2002. EASA Airworthiness Directive.
(5) Boeing Special Attention Service Bulletin 757–25–0238 2 November 11, 2004. Diese Lufttüchtigkeitsanweisung entspricht hinsichtlich der durchzuführenden Maßnahmen und Fristen der
(6) Boeing Special Attention Service Bulletin 767–25–0297 1 November 11, 2004. EASA AD 2006-0225 vom 21.07.2006
(7) Boeing Special Attention Service Bulletin 777–25–0180 1 November 11, 2004. Durch die vorgenannten Mängel ist die Lufttüchtigkeit des Luftfahrtgerätes derart beeinträchtigt, daß es nach Ablauf der genannten Fristen
nur in Betrieb genommen werden darf, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind. Im Interesse der
Sicherheit des Luftverkehrs, das in diesem Fall das Interesse des Adressaten am Aufschub der angeordneten Maßnahmen überwiegt, ist es
Issued in Renton, Washington, on May 30, 2006. erforderlich, die sofortige Vollziehung dieser LTA anzuordnen.
Jeffrey E. Duven, Rechtsbehelfsbelehrung:
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. Gegen diese Verfügung kann innerhalb eines Monats nach Bekanntgabe Widerspruch eingelegt werden. Der Widerspruch ist schriftlich oder
zur Niederschrift beim Luftfahrt-Bundesamt, Hermann-Blenk-Str. 26, 38108 Braunschweig einzulegen.
[FR Doc. 06-5120 Filed 6-6-06; 8:45 am]
BILLING CODE 4910-13-P LTAs werden auch im Internet unter http://www.lba.de publiziert
***
9
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EASA AIRWORTHINESS DIRECTIVE
The issue 14 of the A340 CMR document introduces more restrictive
requirements for aircraft configuration already in service.
AD No.: 2006 – 0225 Effective Date: 04 August 2006
Compliance: From the effective date of this AD, it is mandatory to adhere to the
requirements defined in the AIRBUS A340 Certification Maintenance
Requirements document referenced 955.3019/92 at issue 14.
Date: 21 July 2006
For any new CMR task introduced by A340 CMR Document Issue 14
the associated interval is to be counted from the effective date of this
AD.
No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with the
requirements of that Airworthiness Directive unless otherwise agreed with the Authority of the State of Registry. For CMR tasks, that have been revised by A340 CMR Document Issue
14 the interval is to be counted from the previous performance of the
Type Approval Holder’s Name : Type/Model designation(s) : task.
AIRBUS SAS A340 Aircraft
Grace periods:
TCDS Number : EASA A.015
In order to allow for a proper rescheduling of the associated
maintenance tasks the following grace periods are granted for the first
Foreign AD : None time of performance of the tasks after this AD becomes effective:
Supersedure : None
x MSI 21.28.00 and 21.43.00:
At the effective date of this AD, for aircraft that have exceeded
or are close to exceed the more restrictive limitations of the
Time Limits - Airworthiness Limitations - Certification CMRs in MSI 21.28.00 and 21.43.00, accomplishment of the
ATA 05
Maintenance Requirements (CMR) task must be performed no later than 2500FH from previous
accomplishment.
x MSI 28.24.00:
Manufacturer: AIRBUS (formerly AIRBUS INDUSTRIE)
At the effective date of this AD, for aircraft having more than
2700 FH since the last accomplishment of maintenance task
Applicability: AIRBUS A340 aircraft, all certified models, all serial numbers. related to MSI 28.24.00, accomplishment of the task must be
performed no later than 800 FH from the effective date of this
Reason: The certification requirements for systems are provided in AIRBUS A340 AD.
Airworthiness Limitation Section (ALS) Part 3 Document (Certification
Maintenance Requirements - CMR). This A340 CMR document is Ref. Publications: AIRBUS A340 CMR issue 14 referenced 955.3019/92 approved on
referenced 955.3019/92 and approved by the European Aviation Safety April 24, 2006 under Ref. EASA.A.414
Agency (EASA). or later approved revisions.
This Airworthiness Directive (AD) mandates the A340 CMR
requirements as defined in AIRBUS document 955.3019/92 issue 14 Remarks : 1. If requested and appropriately substantiated the responsible EASA
which: manager for the related product has the authority to accept
Alternative Methods of Compliance (AMOCs) for this AD.
- introduces a new model A340-643,
2. This AD was posted as PAD 06-173 for consultation on 30 June
- introduces the impact of increasing the Design Service Goal
2006 with a comment period until 14 July 2006. No comment was
(DSG) for the Weight Variant 50 series,
raised during consultation period.
- revises the applicability of some tasks,
3. Enquiries regarding this Airworthiness Directive should be referred to
- adds new CMR tasks associated with modifications and new Mr. M. Capaccio, Airworthiness Directive Focal Point - Certification
DSG, Directorate, EASA. E-mail: ADs@easa.europa.eu
- revises some CMR tasks with more restrictive intervals, 4. For any question concerning the technical content of the
requirements in this AD, please contact AIRBUS SAS –Airworthiness
- deletes CMR status from some tasks. Office - EAL Fax: +33 5 61 93 45 80.
1/2 2/2
Lufttüchtigkeitsanweisung
LTA-Nr.: D-2006-228 AIRWORTHINESS DIRECTIVE U.S. Department
of Transportation
www.faa.gov/aircraft/safety/alerts/ Federal Aviation
Luftfahrt-Bundesamt Administration
Datum der Bekanntgabe: 17.08.2006 www.gpoaccess.gov/fr/advanced.html
Muster: Boeing AD der ausländischen Behörde:
BOEING 747 FAA AD 2006-12-10 Amdt. 39-14635
2006-12-10 Boeing: Amendment 39-14635. Docket No. FAA-2005-23250; Directorate Identifier
2005-NM-150-AD.
Geräte-Nr.: Technische Mitteilungen des Herstellers:
2832 Boeing Service Bulletin 747-35-2114 vom 19.12.2002 Effective Date
Betroffenes Luftfahrtgerät: (a) This AD becomes effective July 17, 2006.
Boeing
BOEING 747 Affected ADs
- Baureihen: 747-400 (b) None.
Applicability
- Werk-Nrn.: Gemäß Boeing Service Bulletin 747-35-2114
(Line-Nrn. 1186 bis 1303)
(c) This AD applies to Boeing Model 747-400 series airplanes, certificated in any category, as
identified in Boeing Special Attention Service Bulletin 747-35-2114, dated December 19, 2002.
Betrifft:
SAUERSTOFFANLAGE (ATA: 35): Sauerstoffanlage für die Besatzung - Traggerüst der Sauerstoffflaschen Unsafe Condition
Maßnahmen: (d) This AD results from a report indicating that certain oxygen cylinder supports may not have
Detaillierte Informationen über die durchzuführenden Maßnahmen sind der oben genannten FAA Airworthiness
Directive (AD) und den genannten technischen Mitteilungen des Herstellers zu entnehmen. Alle erforderlichen
been properly heat-treated. We are issuing this AD to prevent failure of the oxygen cylinder support
Maßnahmen zur Abstellung des technischen Mangels müssen ordnungsgemäß, vollständig und innerhalb der under the most critical flight load conditions, which could cause the oxygen cylinder to come loose
vorgesehen Fristen auf Basis der genannten Bezugsdokumente durchgeführt werden. Alle Abweichungen von and leak oxygen. Leakage of oxygen could result in oxygen being unavailable for the flightcrew or
den Maßnahmen und Fristen dieser Lufttüchtigkeitsanweisung bedürfen der vorherigen Zustimmung durch das could result in a fire hazard in the vicinity of the leakage.
Luftfahrt-Bundesamt.
Compliance
Fristen:
Alle anzuwendenden Fristen sind der oben genannten FAA Airworthiness Directive (AD) zu entnehmen. Die
Laufzeit aller anzuwendenden Fristen beginnt mit dem Datum der Inkraftsetzung der genannten FAA (e) You are responsible for having the actions required by this AD performed within the
Airworthiness Directive (AD). compliance times specified, unless the actions have already been done.
Diese Lufttüchtigkeitsanweisung entspricht hinsichtlich der durchzuführenden Maßnahmen und Fristen der Inspection and Corrective Action
FAA AD 2006-12-10 Amdt. 39-14635
Durch die vorgenannten Mängel ist die Lufttüchtigkeit des Luftfahrtgerätes derart beeinträchtigt, daß es nach Ablauf der genannten Fristen
nur in Betrieb genommen werden darf, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind. Im Interesse der (f) Within 18 months after the effective date of this AD, except as provided by paragraph (g) of
Sicherheit des Luftverkehrs, das in diesem Fall das Interesse des Adressaten am Aufschub der angeordneten Maßnahmen überwiegt, ist es
erforderlich, die sofortige Vollziehung dieser LTA anzuordnen.
this AD: Inspect the support bracket of the crew oxygen cylinder installation to determine the
manufacturing date marked on the support, and do the corrective action as applicable, by doing all of
Rechtsbehelfsbelehrung:
Gegen diese Verfügung kann innerhalb eines Monats nach Bekanntgabe Widerspruch eingelegt werden. Der Widerspruch ist schriftlich oder
the actions in accordance with the Accomplishment Instructions of Boeing Special Attention Service
zur Niederschrift beim Luftfahrt-Bundesamt, Hermann-Blenk-Str. 26, 38108 Braunschweig einzulegen. Bulletin 747-35-2114, dated December 19, 2002. Corrective action, if applicable, must be done
LTAs werden auch im Internet unter http://www.lba.de publiziert
before further flight after the inspection.
***
(g) If the configuration of the crew oxygen cylinder installation is changed from a one-cylinder
to a two-cylinder configuration: Do the actions required by paragraph (f) of this AD before further
flight after the change in configuration, or within 18 months after the effective date of this AD,
whichever is later.
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Parts Installation Lufttüchtigkeitsanweisung
LTA-Nr.: D-2006-229
(h) On or after the effective date of this AD, no person may install an oxygen cylinder support
bracket having part number 65B68258-2 and having a manufacturing date between 10/01/98 and Luftfahrt-Bundesamt
03/09/01 inclusive (meaning, a manufacturing date of 10/01/98 or later and 03/09/01 or earlier). Datum der Bekanntgabe: 17.08.2006
Muster: Boeing AD der ausländischen Behörde:
Alternative Methods of Compliance (AMOCs) BOEING 737 FAA AD 2006-12-11 Amdt. 39-14636
Geräte-Nr.: Technische Mitteilungen des Herstellers:
(i)(1) The Manager, Seattle Aircraft Certification Office, FAA, has the authority to approve 2823 Boeing Service Bulletin 737-28-1199 Revision 1 vom 15.12.2005
AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with 14 CFR 39.19 on any airplane to Betroffenes Luftfahrtgerät:
which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office. Boeing
BOEING 737
Material Incorporated by Reference
- Baureihen: 737-600, -700, -700C, -800 und -900
(j) You must use Boeing Special Attention Service Bulletin 747-35-2114, dated December 19,
2002, to perform the actions that are required by this AD, unless the AD specifies otherwise. The - Werk-Nrn.: Gemäß Boeing Service Bulletin 737-28-1199 Revision 1
Director of the Federal Register approved the incorporation by reference of this document in (Line-Nrn. 1 bis 1348)
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Boeing Commercial Airplanes, P.O.
Box 3707, Seattle, Washington 98124-2207, for a copy of this service information. You may review
Betrifft:
copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street KRAFTSTOFFANLAGE (ATA: 28): Kraftstoffabsperrventile für die Triebwerke - Elektrische Verkabelung und
SW., Room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the Kabelschutzrohre im hinteren Bereich der Triebwerkgondelträger
National Archives and Records Administration (NARA). For information on the availability of this
material at the NARA, call (202) 741-6030, or go to Maßnahmen:
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. Detaillierte Informationen über die durchzuführenden Maßnahmen sind der oben genannten FAA Airworthiness
Directive (AD) und den genannten technischen Mitteilungen des Herstellers zu entnehmen. Alle erforderlichen
Maßnahmen zur Abstellung des technischen Mangels müssen ordnungsgemäß, vollständig und innerhalb der
Issued in Renton, Washington, on May 31, 2006. vorgesehen Fristen auf Basis der genannten Bezugsdokumente durchgeführt werden. Alle Abweichungen von
Kalene C. Yanamura, den Maßnahmen und Fristen dieser Lufttüchtigkeitsanweisung bedürfen der vorherigen Zustimmung durch das
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. Luftfahrt-Bundesamt.
[FR Doc. 06-5209 Filed 6-9-06; 8:45 am]
BILLING CODE 4910-13-P Fristen:
Alle anzuwendenden Fristen sind der oben genannten FAA Airworthiness Directive (AD) zu entnehmen. Die
Laufzeit aller anzuwendenden Fristen beginnt mit dem Datum der Inkraftsetzung der genannten FAA
Airworthiness Directive (AD).
Diese Lufttüchtigkeitsanweisung entspricht hinsichtlich der durchzuführenden Maßnahmen und Fristen der
FAA AD 2006-12-11 Amdt. 39-14636
Durch die vorgenannten Mängel ist die Lufttüchtigkeit des Luftfahrtgerätes derart beeinträchtigt, daß es nach Ablauf der genannten Fristen
nur in Betrieb genommen werden darf, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind. Im Interesse der
Sicherheit des Luftverkehrs, das in diesem Fall das Interesse des Adressaten am Aufschub der angeordneten Maßnahmen überwiegt, ist es
erforderlich, die sofortige Vollziehung dieser LTA anzuordnen.
Rechtsbehelfsbelehrung:
Gegen diese Verfügung kann innerhalb eines Monats nach Bekanntgabe Widerspruch eingelegt werden. Der Widerspruch ist schriftlich oder
zur Niederschrift beim Luftfahrt-Bundesamt, Hermann-Blenk-Str. 26, 38108 Braunschweig einzulegen.
LTAs werden auch im Internet unter http://www.lba.de publiziert
***
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Alternative Methods of Compliance (AMOCs)
AIRWORTHINESS DIRECTIVE U.S. Department
of Transportation
Federal Aviation (h)(1) The Manager, Seattle Aircraft Certification Office, FAA, has the authority to approve
www.faa.gov/aircraft/safety/alerts/
Administration AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.
www.gpoaccess.gov/fr/advanced.html
(2) Before using any AMOC approved in accordance with 14 CFR 39.19 on any airplane to
which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards
2006-12-11 Boeing: Amendment 39-14636. Docket No. FAA-2005-20626; Directorate Identifier
Certificate Holding District Office.
2004-NM-243-AD.
Material Incorporated by Reference
Effective Date
(i) You must use Boeing Special Attention Service Bulletin 737-28-1199, Revision 1, dated
(a) This AD becomes effective July 17, 2006.
December 15, 2005, to perform the actions that are required by this AD, unless the AD specifies
otherwise. The Director of the Federal Register approved the incorporation by reference of this
Affected ADs
document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Boeing Commercial
Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207, for a copy of this service information.
(b) None.
You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400
Seventh Street SW., Room PL-401, Nassif Building, Washington, DC; on the Internet at
Applicability
http://dms.dot.gov; or at 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
(c) This AD applies to Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes;
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
certificated in any category; as listed in Boeing Special Attention Service Bulletin 737-28-1199,
Revision 1, dated December 15, 2005.
Issued in Renton, Washington, on May 31, 2006.
Kalene C. Yanamura,
Unsafe Condition
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 06-5205 Filed 6-9-06; 8:45 am]
(d) This AD was prompted by a report that an operator discovered many small chafe marks and
BILLING CODE 4910-13-P
exposed shield braid on fuel shutoff valve wires routed through a conduit in the wing. We are issuing
this AD to prevent exposed wires that could provide an ignition source in a flammable leakage zone
and possibly lead to an uncontrolled fire or explosion.
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.
Parts Replacement
(f) Within 36 months after the effective date of this AD, replace the fuel shutoff valve wires and
conduit assemblies in the left and right engine strut aft fairing areas with new fuel shutoff valve wires
and conduit assemblies, by accomplishing all the actions in accordance with the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 737-28-1199, Revision 1, dated December
15, 2005.
Actions Accomplished Using Prior Version of Service Information
(g) Actions accomplished before the effective date of this AD in accordance with Special
Attention Service Bulletin 737-28-1199, dated September 9, 2004, are considered acceptable for
compliance with the applicable action specified in this AD.
6 7
Lufttüchtigkeitsanweisung
LTA-Nr.: D-2006-230 AIRWORTHINESS DIRECTIVE U.S. Department
of Transportation
www.faa.gov/aircraft/safety/alerts/ Federal Aviation
Luftfahrt-Bundesamt Datum der Bekanntgabe: 18.08.2006 www.gpoaccess.gov/fr/advanced.html Administration
Muster: Raytheon AD der ausländischen Behörde:
BAe 125 FAA AD 2006-12-20 Amdt. 39-14646 2006-12-20 Raytheon Aircraft Company: Amendment 39-14646. Docket No. FAA-2006-25011;
Geräte-Nr.: Technische Mitteilungen des Herstellers: Directorate Identifier 2006-NM-118-AD.
2507 Raytheon Service Bulletin SB 24-3793 vom Mai 2006
Effective Date
Betroffenes Luftfahrtgerät:
(a) This AD becomes effective July 3, 2006.
Raytheon
BAe 125 Affected ADs
- Baureihen: HS 125 SERIES 700A,
HS 125 SERIES 700B, (b) None.
BAe 125-800A, Applicability
BAe 125-800B,
Hawker 800, (c) This AD applies to the Raytheon airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of
Hawker 800XP,
this AD, certificated in any category.
BAe 125-1000A, (1) Model HS.125 series 700A and 700B airplanes, on which Raytheon Modification 252885 has
BAe 125-1000B, been incorporated or British Aerospace 125 Service Bulletin SB 24-239-2885 has been accomplished.
Hawker 1000 (2) All Model BAe.125 series 800A (including variants C-29A and U-125), 800B, 1000A, and
1000B airplanes.
und die Militärversionen der BAe 125-800A (C29A und U-125) und Hawker 800 (U-125A)
(3) All Model Hawker 800 (including variant U-125A) and 1000 airplanes; and Model Hawker
- Werk-Nrn.: 257001 bis 258768 und 259003 bis 259052 800XP airplanes, serial numbers 1 through 258768 inclusive.
-- ausgenommen sind HS 125-700A und -700B Flugzeuge OHNE Modifikation 252885 Unsafe Condition
(Service Bulletin SB 24-239-2885)
(d) This AD results from reports that certain current limiters have opened within two to four
Betrifft:
STROMVERSORGUNG (ATA: 24): UAM100 Strombegrenzer der PE, PS1 und PS2 Stromschienenversorgung
hours after installation. We are issuing this AD to prevent loss of all primary electrical power, which
could result in the airplane operating only under emergency power.
Maßnahmen:
Detaillierte Informationen über die durchzuführenden Maßnahmen sind der oben genannten FAA Airworthiness Compliance
Directive (AD) und den genannten technischen Mitteilungen des Herstellers zu entnehmen. Alle erforderlichen
Maßnahmen zur Abstellung des technischen Mangels müssen ordnungsgemäß, vollständig und innerhalb der (e) You are responsible for having the actions required by this AD performed within the
vorgesehen Fristen auf Basis der genannten Bezugsdokumente durchgeführt werden. Alle Abweichungen von
compliance times specified, unless the actions have already been done.
den Maßnahmen und Fristen dieser Lufttüchtigkeitsanweisung bedürfen der vorherigen Zustimmung durch das
Luftfahrt-Bundesamt.
Resistance Measurement and Replacement if Necessary
Fristen:
Alle anzuwendenden Fristen sind der oben genannten FAA Airworthiness Directive (AD) zu entnehmen. Die (f) Within 30 days or 25 flight hours after the effective date of this AD, whichever occurs first:
Laufzeit aller anzuwendenden Fristen beginnt mit dem Datum der Inkraftsetzung der genannten FAA Measure the resistance of the applicable current limiters, part number (P/N) UAM100, in accordance
Airworthiness Directive (AD). with paragraph 3.A.(2) of the Accomplishment Instructions of Raytheon Service Bulletin SB 24-
Diese Lufttüchtigkeitsanweisung entspricht hinsichtlich der durchzuführenden Maßnahmen und Fristen der 3793, dated May 2006. The applicable current limiters are listed in Table 1 of the service bulletin. If
FAA AD 2006-12-20 Amdt. 39-14646 the measured resistance of a current limiter is less than 0.46 milliohms or greater than 0.56
Durch die vorgenannten Mängel ist die Lufttüchtigkeit des Luftfahrtgerätes derart beeinträchtigt, daß es nach Ablauf der genannten Fristen milliohms, before further flight, replace the part with a new part in accordance with the service
nur in Betrieb genommen werden darf, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind. Im Interesse der
Sicherheit des Luftverkehrs, das in diesem Fall das Interesse des Adressaten am Aufschub der angeordneten Maßnahmen überwiegt, ist es bulletin. The new part must not be from picking tag purchase order (PO) 4501760749 or PO
erforderlich, die sofortige Vollziehung dieser LTA anzuordnen. 4501743706 and must be the correct resistance in the range of 0.46 milliohms to 0.56 milliohms.
Rechtsbehelfsbelehrung:
Gegen diese Verfügung kann innerhalb eines Monats nach Bekanntgabe Widerspruch eingelegt werden. Der Widerspruch ist schriftlich oder
zur Niederschrift beim Luftfahrt-Bundesamt, Hermann-Blenk-Str. 26, 38108 Braunschweig einzulegen.
LTAs werden auch im Internet unter http://www.lba.de publiziert
***
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