Nachrichten für Luftfahrer 2010 Teil II (weicht ggf. von Druckversion ab)
Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
T23 LTA-Sachgebiet
38144 Braunschweig
D-2010-315 Fax: +49-531-2355-725
Table 2–Material Incorporated by Reference
email: ad@lba.de
Document Revision Date BOEING Datum der Bekanntgabe: 22.11.2010
Bombardier Service Bulletin 40-26-05 2 May 4, 2009 Betroffenes Luftfahrtgerät:
Bombardier Service Bulletin 45-26-9 2 May 4, 2009 Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: The Boeing Company
Hersteller: The Boeing Company
(1) The Director of the Federal Register approved the incorporation by reference of the service Muster: BOEING 757,
information contained in Table 2 of this AD under 5 U.S.C. 552(a) and 1 CFR part 51. BOEING 767
Baureihen: 757-200, 757-200CB, 757-200PF und 757-300,
(2) For service information identified in this AD, contact Learjet, Inc., One Learjet Way, 767-200, 767-300, 767-300F und 767-400ER
Wichita, Kansas 67209-2942; telephone 316-946-2000; fax 316-946-2220; e-mail Werknummern: Alle
ac.ict@aero.bombardier.com; Internet http://www.bombardier.com. - ausgenommen sind Boeing 757 Flugzeuge ab der Line-Nummer 1051.
(3) You may review copies of the service information at the FAA, Transport Airplane Gerätenummer: 2845, 2851, EASA.IM.A.035
Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this
Revisionsstand:
material at the FAA, call 425-227-1221. Originalausgabe
(4) You may also review copies of the service information that is incorporated by reference at the
National Archives and Records Administration (NARA). For information on the availability of this Airworthiness Directive der ausländischen Behörde:
material at an NARA facility, call 202-741-6030, or go to FAA AD 2010-23-03 - Amdt. 39-16492
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Betrifft:
(ATA 28) Fuel (FQIS) - Engine Indication and Crew Alerting System (EICAS) - Repetitive Tests
Issued in Renton, Washington, on October 5, 2010.
Ali Bahrami, Maßnahmen und Fristen:
Manager, Transport Airplane Directorate, Aircraft Certification Service. Detaillierte Informationen über die durchzuführenden Maßnahmen sind der genannten FAA Airworthiness Directive
[FR Doc. 2010-25599 Filed 10-13-10; 8:45 am] und den genannten technischen Mitteilungen des Herstellers zu entnehmen. Alle erforderlichen Maßnahmen zur
Abstellung des technischen Mangels müssen ordnungsgemäß, vollständig und innerhalb der vorgesehenen Fristen
BILLING CODE 4910-13-P auf Basis der genannten Bezugsdokumente durchgeführt werden. Alle Abweichungen von den Maßnahmen und
Fristen dieser Lufttüchtigkeitsanweisung bedürfen der vorherigen Zustimmung durch das Luftfahrt-Bundesamt.
Alle anzuwendenden Fristen sind der genannten FAA Airworthiness Directive zu entnehmen. Die Laufzeit aller
anzuwendenden Fristen beginnt mit dem Datum der Inkraftsetzung der genannten FAA Airworthiness Directive.
Diese Lufttüchtigkeitsanweisung entspricht hinsichtlich der durchzuführenden Maßnahmen und Fristen der
FAA AD 2010-23-03 - Amdt. 39-16492.
Zugehörige technische Dokumente:
1. Boeing Service Bulletin 757-28-0121 vom 18.08.2010
2. Boeing Service Bulletin 767-28-0106 vom 25.08.2010
Die sofortige Vollziehung dieses Bescheides wird gemäß § 80 Absatz 2 Satz 1 Nr. 4 der Verwaltungsgerichtsordnung (VwGO) angeordnet.
Begründung
Durch die vorgenannten Mängel ist die Lufttüchtigkeit des Luftfahrtgerätes derart beeinträchtigt, dass es nach Ablauf der genannten Fristen nur in Betrieb genom-
men 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 Lufttüchtigkeitsanweisung
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. Ein eventueller Widerspruch hat keine aufschiebende Wirkung. Das Verwaltungsge-
richt Braunschweig, Am Wendentor 7, 38100 Braunschweig, kann auf Antrag nach § 80 Abs. 5 VwGO die aufschiebende Wirkung jedoch ganz oder teilweise wie-
derherstellen bzw. anordnen.
6
D-2010-315 Seite 1 von 1 536/2010
[Federal Register: November 5, 2010 (Volume 75, Number 214)] • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground
[Rules and Regulations] Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590.
[Page 68177-68179] • Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30, West Building
From the Federal Register Online via GPO Access [wais.access.gpo.gov] Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590,
[DOCID:fr05no10-5] between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this AD, contact Boeing Commercial Airplanes, Attention:
–––––––––––––––––––––––––––––––––– Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207;
telephone 206-544-5000, extension 1, fax 206-766-5680; e-mail me.boecom@boeing.com; Internet
DEPARTMENT OF TRANSPORTATION https://www.myboeingfleet.com. You may review copies of the referenced service information at the
FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information
Federal Aviation Administration on the availability of this material at the FAA, call 425-227-1221.
14 CFR Part 39 Examining the AD Docket
[Docket No. FAA-2010-1040; Directorate Identifier 2010-NM-207-AD; Amendment 39-16492; You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at
AD 2010-23-03] the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and
RIN 2120-AA64 other information. The street address for the Docket Office (phone: 800-647-5527) is in the
ADDRESSES section. Comments will be available in the AD docket shortly after receipt.
Airworthiness Directives; The Boeing Company Model 757 and 767 Airplanes
FOR FURTHER INFORMATION CONTACT: Tak Kobayashi, Aerospace Engineer, Propulsion
AGENCY: Federal Aviation Administration (FAA), DOT. Branch, ANM-140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 917-6499; fax (425) 917-6590; e-mail:
ACTION: Final rule; request for comments. takahisa.kobayashi@faa.gov.
–––––––––––––––––––––––––––––––––– SUPPLEMENTARY INFORMATION:
SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above. This Discussion
AD requires repetitive testing for correct functioning of the engine indication and crew alerting
system (EICAS) to ensure that it receives both the LOW FUEL and FUEL CONFIG discrete signals We received a report from an operator of a Model 757-200 series airplane that the engine
from the fuel quantity processor unit, and alerts the flightcrew of a low fuel situation, and if the test indication and crew alerting system (EICAS) failed to alert the flightcrew of an improper fuel system
fails, troubleshooting to find wire faults and damaged equipment, and corrective actions if necessary. configuration during flight. Later in that flight, the EICAS failed to alert the flightcrew that the fuel in
This AD was prompted by a report that the EICAS failed to alert the flightcrew of an improper fuel the left- and right-hand main tanks was depleted below the minimum of 2,200 pounds. The EICAS
system configuration during flight. Later in that flight, the EICAS failed to alert the flightcrew that receives both the LOW FUEL and FUEL CONFIG discrete signals from the fuel quantity processor
the fuel in the left- and right-hand main tanks was depleted below the minimum of 2,200 pounds. We unit to display certain messages to alert the flightcrew. When the center fuel tank pump switches are
are issuing this AD to detect and correct a single latent failure of the FUEL CONFIG discrete signal, off with more than 200 pounds of fuel in the center tank the EICAS should display the FUEL
which disables both the FUEL CONFIG and LOW FUEL messages. Such failure, combined with a CONFIG advisory message. When the fuel in either main tank is below 2,200 pounds, the EICAS
flightcrew error in configuring the fuel system, could lead to depletion of the fuel in the main tanks should display the LOW FUEL caution message. The EICAS design allows a single latent failure of
and possible flame out of both engines. A dual engine flame out could result in inaccessibility of the the FUEL CONFIG discrete signal, which disables both the FUEL CONFIG and LOW FUEL
remaining fuel in the center tank due to loss of electrical power to the pumps, consequent messages. Such failure, combined with a flightcrew error in configuring the fuel system, could lead to
unrecoverable dual engine shutdown, and forced landing of the airplane. depletion of the fuel in the main tanks and possible flame out of both engines. A dual engine flame
out could result in inaccessibility of the remaining fuel in the center tank due to loss of electrical
DATES: This AD is effective November 22, 2010. power to the pumps, consequent unrecoverable dual engine shutdown, and forced landing of the
The Director of the Federal Register approved the incorporation by reference of certain airplane.
publications listed in the AD as of November 22, 2010. The fuel quantity indicating system (FQIS), EICAS, and large format display system (LFDS)
We must receive comments on this AD by December 20, 2010. installed on Model 757-200 series airplanes are similar to the systems installed on Model 767
airplanes. Therefore, Model 767 airplanes are also subject to the identified unsafe condition and are
ADDRESSES: You may send comments by any of the following methods: included in the applicability of this AD.
• Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for
submitting comments.
• Fax: 202-493-2251.
1 2
Relevant Service Information section. Include ''Docket No. FAA-2010-1040; Directorate Identifier 2010-NM-207-AD;'' at the
beginning of your comments. We specifically invite comments on the overall regulatory, economic,
We reviewed Boeing Special Attention Service Bulletins 757-28-0121, dated August 18, 2010; environmental, and energy aspects of this AD. We will consider all comments received by the closing
and 767-28-0106, dated August 25, 2010. The service information describes procedures for repetitive date and may amend this AD because of those comments.
testing for correct functioning of the EICAS, and if the test fails, troubleshooting to find wire faults, We will post all comments we receive, without change, to http://www.regulations.gov, including
bent connector pins, or damaged equipment. Boeing Special Attention Service Bulletin 757-28-0121, any personal information you provide. We will also post a report summarizing each substantive
dated August 18, 2010, also specifies procedures for corrective actions if any wire fault or damaged verbal contact we receive about this AD.
equipment (including bent connector pins) is found. The corrective actions include repairing or
replacing affected wires and damaged equipment (including bent connector pins). Costs of Compliance
FAA's Determination We estimate that this AD affects 686 Model 757 airplanes and 425 Model 767 airplanes of U.S.
registry.
We are issuing this AD because we evaluated all the relevant information and determined the We estimate the following costs to comply with this AD:
unsafe condition described previously is likely to exist or develop in other products of these same
type designs. Estimated costs
Action Labor cost Parts cost Cost per Cost on U.S. operators
AD Requirements
product
This AD requires accomplishing the actions specified in the service information described EICAS test 1 work-hour X N/A $85 per test $58,310 (for Model 757
previously, except as discussed under ''Difference Between the AD and the Service Information.'' $85 per hour = cycle airplanes)
$85 per test cycle $36,125 (for Model 767
Difference Between the AD and the Service Information
airplanes)
Boeing Special Attention Service Bulletins 767-28-0106, dated August 25, 2010, does not
specify instructions on how to repair certain conditions, but this AD would require repairing those We have received no definitive data that would enable us to provide a cost estimate for the on-
conditions in one of the following ways: condition actions specified in this AD.
• In accordance with a method that we approve; or
• Using data that meet the certification basis of the airplane, and that have been approved by the Authority for this Rulemaking
Boeing Commercial Airplanes Organization Designation Authorization (ODA) whom we
have authorized to make those findings. 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
Interim Action 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,
We consider this AD interim action. The manufacturer is currently developing a modification Section 44701: ''General requirements.'' Under that section, Congress charges the FAA with
that will address the unsafe condition identified in this AD. Once this modification is developed, promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices,
approved, and available, we might consider additional rulemaking. 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
FAA's Justification and Determination of the Effective Date to exist or develop on products identified in this rulemaking action.
An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found Regulatory Findings
that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule
because if the EICAS malfunctions, the flightcrew will not be alerted of a low fuel situation, which This AD will not have federalism implications under Executive Order 13132. This AD will not
could result in depletion of the fuel in the main tanks and consequent unrecoverable dual engine have a substantial direct effect on the States, on the relationship between the national government and
shutdown and forced landing of the airplane. Therefore, we find that notice and opportunity for prior the States, or on the distribution of power and responsibilities among the various levels of
public comment are impracticable and that good cause exists for making this amendment effective in government.
less than 30 days. For the reasons discussed above, I certify that this AD:
(1) Is not a ''significant regulatory action'' under Executive Order 12866,
Comments Invited (2) Is not a ''significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034,
February 26, 1979),
This AD is a final rule that involves requirements affecting flight safety and was not preceded by (3) Will not affect intrastate aviation in Alaska, and
notice and an opportunity for public comment. However, we invite you to send any written data, (4) Will not have a significant economic impact, positive or negative, on a substantial number of
views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES small entities under the criteria of the Regulatory Flexibility Act.
3 4
List of Subjects in 14 CFR Part 39
AIRWORTHINESS DIRECTIVE
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. FAA
www.faa.gov/aircraft/safety/alerts/
Aviation Safety
www.gpoaccess.gov/fr/advanced.html
Adoption of the Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part
39 as follows: 2010-23-03 The Boeing Company: Amendment 39-16492; Docket No. FAA-2010-1040;
Directorate Identifier 2010-NM-207-AD.
PART 39–AIRWORTHINESS DIRECTIVES
Effective Date
1. The authority citation for part 39 continues to read as follows:
(a) This AD is effective November 22, 2010.
Authority: 49 U.S.C. 106(g), 40113, 44701.
Affected ADs
§ 39.13 [Amended]
(b) None.
2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD):
Applicability
(c) This AD applies to The Boeing Company Model 757-200, 200CB, -200PF, and -300 series
airplanes, line numbers 1 through 1050 inclusive, and all Model 767-200, -300, -300F, and -400ER
series airplanes; certificated in any category.
Subject
(d) Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code
28: Fuel.
Unsafe Condition
(e) This AD was prompted by a report that the EICAS failed to alert the flightcrew of an
improper fuel system configuration during flight. Later in that flight the EICAS failed to alert the
flightcrew that the fuel in the left- and right-hand main tanks was depleted below the minimum of
2,200 pounds. We are issuing this AD to detect and correct a single latent failure of the FUEL
CONFIG discrete signal, which disables both the FUEL CONFIG and LOW FUEL messages. Such
failure, combined with a flightcrew error in configuring the fuel system, could lead to depletion of the
fuel in the main tanks and possible flame out of both engines. A dual engine flame out could result in
inaccessibility of the remaining fuel in the center tank due to loss of electrical power to the pumps,
consequent unrecoverable dual engine shutdown, and forced landing of the airplane.
Compliance
(f) Comply with this AD within the compliance times specified, unless already done.
Repetitive Tests
(g) Within 100 flight hours after the effective date of this AD: Do a test for correct functioning of
the EICAS to ensure that it receives both the LOW FUEL and FUEL CONFIG discrete signals from
the fuel quantity processor unit, in accordance with the Accomplishment Instructions of Boeing
Special Attention Service Bulletin 757-28-0121, dated August 18, 2010; or Boeing Special Attention
5 6
Service Bulletin 767-28-0106, dated August 25, 2010; as applicable. Repeat the test thereafter at (2) For service information identified in this AD, contact Boeing Commercial Airplanes,
intervals not to exceed 100 flight hours. Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-
2207; telephone 206-544-5000, extension 1, fax 206-766-5680; e-mail me.boecom@boeing.com;
Corrective Actions If Necessary Internet https://www.myboeingfleet.com.
(3) You may review copies of the service information at the FAA, Transport Airplane
(h) If any test required by paragraph (g) of this AD fails, before further flight, troubleshoot to Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this
find any wire faults, and damaged equipment (including bent connector pins), in accordance with the material at the FAA, call 425-227-1221.
Accomplishment Instructions of Boeing Special Attention Service Bulletin 757-28-0121, dated (4) You may also review copies of the service information that is incorporated by reference at the
August 18, 2010; or Boeing Special Attention Service Bulletin 767-28-0106, dated August 25, 2010; National Archives and Records Administration (NARA). For information on the availability of this
as applicable. material at an NARA facility, call 202-741-6030, or go to http://www.archives.gov/federal_register/
code_of_federal_regulations/ibr_locations.html.
(i) If, during any troubleshooting required by paragraph (h) of this AD, any wire fault or
damaged equipment (including bent connector pins) is found, before further flight, do the applicable Issued in Renton, Washington, on October 20, 2010.
actions specified in paragraph (i)(1) or (i)(2) of this AD. Michael Kaszycki,
(1) For airplanes identified in Boeing Special Attention Service Bulletin 757-28-0121, dated Acting Manager, Transport Airplane Directorate,
August 18, 2010: Repair or replace affected wires and equipment (including bent connector pins), in Aircraft Certification Service.
accordance with the Accomplishment Instructions of Boeing Special Attention Service Bulletin 757-
28-0121, dated August 18, 2010.
(2) For airplanes identified in Boeing Special Attention Service Bulletin 767-28-0106, dated
August 25, 2010: Do corrective actions using a method approved by the Manager, Seattle Aircraft
Certification Office (ACO), FAA.
Note 1: Guidance on doing corrective actions can be found in Chapter 28, Subject 28-41-00,
Section July, of the Boeing 767 Fault Isolation Manual (FIM).
Alternative Methods of Compliance (AMOCs)
(j)(1) The Manager, Seattle ACO, FAA, has the authority to approve AMOCs for this AD, if
requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your
request to your principal inspector or local Flight Standards District Office, as appropriate. If sending
information directly to the manager of the ACO, send it to the attention of the person identified in the
Related Information section of this AD. Information may be e-mailed to: 9-ANM-Seattle-ACO-
AMOC-Requests@faa.gov.
(2) Before using any approved AMOC, notify your Principal Maintenance Inspector or Principal
Avionics Inspector, as appropriate, or lacking a principal inspector, your local Flight Standards
District Office.
Related Information
(k) For more information about this AD, contact Tak Kobayashi, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle ACO, 1601 Lind Avenue, SW., Renton, Washington
98057-3356; telephone (425) 917-6499; fax (425) 917-6590; e-mail takahisa.kobayashi@faa.gov.
Material Incorporated by Reference
(l) You must use Boeing Special Attention Service Bulletin 757-28-0121, dated August 18,
2010; or Boeing Special Attention Service Bulletin 767-28-0106, dated August 25, 2010; as
applicable; to do the actions required by this AD, unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the incorporation by reference of this service
information under 5 U.S.C. 552(a) and 1 CFR part 51.
7 8
AIRWORTHINESS DIRECTIVES
In the following, the Luftfahrt-Bundesamt publishes Airworthiness Directives referring to aeronautical products of
German production or to foreign aeronautical products for which the LBA on the basis of own findings arranged
for the issuance of an Airworthiness Directive. Only in the a.m. cases will Airworthiness Directives be translated
and published in the following.
In accordance with § 14 of Aircraft Operations Order (NfL II-26/70) the following Airworthiness Directives (LTA’s)
will be notified.
After the effective date of an AD, an aeronautical product concerned by the AD may no longer be operated except
for the purpose of accomplishment of the actions prescribed, until the prescribed actions have properly been
accomplished.
The Service Bulletins issued by manufacturers are the reason for the publication of these ADs and thus become a
constituent part of these Airworthiness Directives. We expressly point out that subsequent changes to the Service
Bulletins do not automatically belong to these ADs.
Accomplishment and Log Book Entry:
The actions are to be accomplished and certified by an organisation approved in accordance with § 2 (2) No. 3 of
the Approval of Aeronautical Products Order (LuftGerPV). The regulations relating to the operating records to be
kept in accordance with § 15 Aircraft Operations Order and JAR-OPS 1 shall be adhered to.
AD-No. Title German Type Certificate No.
Amendments:
-none-
New Issues:
-none-
LTA´s / AD´s and Technical Notes are published on the internet at http://www.lba.de
Note:
1) Please pay attention to the fact that in the title of an AD, the number is followed by the manufacturer’s
normal name in short form (without indicating the legal form). It is the name of the type supporting
organisation competent at the date of the issue of the AD. In the future, former type support
organisations or manufacturers will no longer be indicated in the title of the AD. If there are doubts as to
the applicability of an AD, a check by means of the LBA Type Certificate Data Sheet should be
conducted. This number is indicated in the certification documents or on the type plate of the
aeronautical product.
2) As a result of the EU-wide standardisation of Airworthiness Directives, the numbering system of German
ADs has been changed. All AD numbers hereafter will be preceded by the German country code ”D-”.
This change also applies to previous ADs to be changed from 01.01.2004 (e.g. D-2004-…, or D-1998-
…). Revised ADs will be hereafter marked consecutively with “R” (Revision) (e.g. D-1998-…R1).
NACHRICHTEN FÜR LUFTFAHRER
58. JAHRGANG LANGEN, 16. DEZEMBER 2010 NfL II 69 / 10
Bekanntmachung gemäß § 33 (7) LuftVZO, Regierung von Oberbayern
Managementsystem DQS-zertifiziert nach DIN EN ISO 9001:2000
Büro der Nachrichten für Luftfahrer
NACHRICHTEN FÜR LUFTFAHRER
58. JAHRGANG LANGEN, 16. DEZEMBER 2010 NfL II 70 / 10
Bekanntmachung gemäß § 24 e Absatz 1
Luftverkehrs-Zulassungs-Ordnung
(LuftVZO)
Managementsystem DQS-zertifiziert nach DIN EN ISO 9001:2000
Büro der Nachrichten für Luftfahrer
