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). 

(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. 

(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. 

(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. 

Issued in Renton, Washington, on 

December 30, 2013. 

John P. Piccola, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2014–00234 Filed 1–9–14; 8:45 am] 

BILLING CODE 4910–13–P 

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 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0164; Directorate 

Identifier 2013–NE–10–AD] 

RIN 2120–AA64 

Airworthiness Directives; Austro 

Engine GmbH Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: 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 

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