Airworthiness Directives; Dowty Propellers Propellers, 1774 [C1-2013-30882]
Download as PDF
<![CDATA[
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
https://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]
-----------------------------------------------------------------------
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
