Airworthiness Directives; Dowty Propellers Propellers, 1774 [C1-2013-30882]

Download as PDF 1774 Federal Register / Vol. 79, No. 7 / Friday, January 10, 2014 / Proposed Rules FIGURE 1 TO PARAGRAPH (G) OF THIS AD: ENGINE SHUT-OFF VALVE (FUEL SPAR VALVE) MOV ACTUATOR INSPECTION—Continued AWL No. Task Interval Applicability Description 1. Make sure both Engine Control Switches are in the CUTOFF position. 2. Inspect the left engine fuel spar valve actuator located in the left rear spar. a. Verify the manual override handle on the engine fuel spar valve actuator is in the CLOSED position. b. Repair or replace any MOV actuator that is not in the CLOSED position (refer to Boeing Airplane Maintenance Manual, 28– 22–02). 3. Inspect the right engine fuel spar valve actuator located in the right rear spar. a. Verify the manual override handle on the engine fuel spar valve actuator is in the CLOSED position. b. Repair or replace any MOV actuator that is not in the CLOSED position (refer to Boeing Airplane Maintenance Manual, 28– 22–02). DEPARTMENT OF TRANSPORTATION (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle Aircraft Certification Office (ACO) FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. 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 paragraph (j) of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. mstockstill on DSK4VPTVN1PROD with PROPOSALS (h) No Alternative Actions and Intervals After accomplishment of the maintenance or inspection program revision required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions or intervals are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (i)(1) of this AD. Airworthiness Directives; Dowty Propellers Propellers (j) Related Information For more information about this AD, contact Rebel Nichols, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: (425) 917–6509; fax: (425) 917–6590; email: rebel.nichols@faa.gov. Federal Aviation Administration Issued in Renton, Washington, on December 30, 2013. John P. Piccola, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. Airworthiness Directives; Austro Engine GmbH Engines [FR Doc. 2014–00234 Filed 1–9–14; 8:45 am] BILLING CODE 4910–13–P VerDate Mar<15>2010 16:33 Jan 09, 2014 Jkt 232001 Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2008–1088; Directorate Identifier 2008–NE–15–AD] RIN 2120–AA64 Correction In proposed rule document 2013– 30882, appearing on pages 78290– 78292, in the issue of Thursday, December 26, 2013, make the following correction: On page 78290, in the first column, the subject heading is corrected to read as set forth above. [FR Doc. C1–2013–30882 Filed 1–9–14; 8:45 am] BILLING CODE 1505–01–D DEPARTMENT OF TRANSPORTATION 14 CFR Part 39 [Docket No. FAA–2013–0164; Directorate Identifier 2013–NE–10–AD] RIN 2120–AA64 Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 We propose to supersede airworthiness directive (AD) 2013–14– 08 that applies to all Austro Engine GmbH model E4 engines. AD 2013–14– 08 requires removing from service certain part number (P/N) waste gate controllers. Since we issued AD 2013– 14–08 we received several reports of power loss events due to fracture of the waste gate controller lever. This proposed AD would require removing certain P/N waste gate controllers from service. We are proposing this AD to prevent failure of the waste gate controller lever, which could lead to damage to one or more engines, loss of thrust control, and damage to the airplane. DATES: We must receive comments on this proposed AD by March 11, 2014. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. • Fax: 202–493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this AD, contact Austro Engine GmbH, Rudolf-Diesel-Strasse 11, A–2700 Weiner Neustadt, Austria; phone: +43 2622 23000; fax: +43 2622 23000–2711; Internet: www.austroengine.at. You may SUMMARY: E:\FR\FM\10JAP1.SGM 10JAP1

Agencies

[Federal Register Volume 79, Number 7 (Friday, January 10, 2014)]
[Proposed Rules]
[Page 1774]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: C1-2013-30882]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-1088; Directorate Identifier 2008-NE-15-AD]
RIN 2120-AA64


Airworthiness Directives; Dowty Propellers Propellers

Correction

    In proposed rule document 2013-30882, appearing on pages 78290-
78292, in the issue of Thursday, December 26, 2013, make the following 
correction:
    On page 78290, in the first column, the subject heading is 
corrected to read as set forth above.

[FR Doc. C1-2013-30882 Filed 1-9-14; 8:45 am]
BILLING CODE 1505-01-D