Airworthiness Directives; Dornier Luftfahrt GmbH Airplanes, 35485-35488 [2014-14336]
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Federal Register / Vol. 79, No. 120 / Monday, June 23, 2014 / Rules and Regulations
component history card or equivalent record
and assign a life limit of 5,000 hours TIS by
following the Accomplishment Instructions,
Part IV, of ASB 407–01–48.
(ii) Within 25 hours TIS or 30 days,
whichever occurs first, prepare the tailboom
for daily visual checks and recurring
inspections and inspect the tailboom for a
crack by following the Accomplishment
Instructions, Part II, Steps 1.a) through 1.f),
of Bell ASB 407–07–80, dated August 27,
2007 (ASB 407–07–80).
(iii) Thereafter, before the first flight of
each day, clean the area on the tailboom
where paint has been removed at the upper
and lower attachment support areas of the
horizontal stabilizer and visually check that
area of the tailboom for a crack.
(iv) Within 100 hours TIS and thereafter at
intervals not to exceed 100 hours TIS, using
a 10X or higher power magnifying glass,
inspect each tailboom for a loose rivet, a
crack, skin corrosion, or any other damage,
by following the Accomplishment
Instructions, Part IV, Steps 1 through 6, of
ASB 407–07–80, except this AD does not
require you to contact Bell. If there is
corrosion within an allowable tolerance,
repair each area of corrosion.
(3) If there is a crack, before further flight,
replace the tailboom.
(4) If there is no crack, make sure both of
the inspection area surfaces are dry and
protect each reworked area with a thin coat
of clear coating.
(5) The actions required by paragraphs
(f)(1)(i)(A) and (f)(2)(iii) of this AD may be
performed by the owner/operator (pilot)
holding at least a private pilot certificate and
must be entered into the aircraft records
showing compliance with this AD in
accordance with 14 CFR 43.9 (a)(1) through
(4) and 91.417(a)(2)(v). This record must be
maintained as required by 14 CFR 91.417,
121.380, or 135.439.
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(g) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Safety Management
Group, FAA, may approve AMOCs for this
AD. Send your proposal to: Sharon Miles,
Aviation Safety Engineer, Regulations and
Policy Group, Rotorcraft Directorate, FAA,
2601 Meacham Blvd., Fort Worth, Texas
76137; telephone (817) 222–5110; email
sharon.y.miles@faa.gov.
(2) For operations conducted under a 14
CFR part 119 operating certificate or under
14 CFR part 91, subpart K, we suggest that
you notify your principal inspector, or
lacking a principal inspector, the manager of
the local flight standards district office or
certificate holding district office before
operating any aircraft complying with this
AD through an AMOC.
(h) Additional Information
(1) Bell Alert Service Bulletin No. 407–99–
26, Revision B, dated June 14, 2001, which
is not incorporated by reference, contains
additional information about the subject of
this AD. For this service information, contact
Bell Helicopter Textron Canada, 12,800 Rue
de l’Avenir, Mirabel, Quebec J7J1R4,
telephone (450) 437 2862 or (800) 363–8023,
fax (450) 433–0272 or at https://www.bell
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customer.com/files/. You may review service
information at the FAA, Office of the
Regional Counsel, Southwest Region, 2601
Meacham Blvd., Room 663, Fort Worth,
Texas 76137.
(2) The subject of this AD is addressed in
Transport Canada Civil Aviation (TCCA) AD
No. CF–2008–04, dated January 11, 2008.
You may view the TCCA AD on the Internet
at https://www.regulations.gov in Docket No.
FAA–2013–0574.
DEPARTMENT OF TRANSPORTATION
(i) Subject
Joint Aircraft Service Component (JASC)
Code is 5300: Rotorcraft Tail Boom, and
5302: Middle Section.
Airworthiness Directives; Dornier
Luftfahrt GmbH Airplanes
AGENCY:
(j) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(3) The following service information was
approved for IBR on July 28, 2014.
(i) Bell Helicopter Textron Alert Service
Bulletin (ASB) No. 407–01–48, Revision C,
dated August 27, 2007.
(ii) Bell Helicopter Textron ASB No. 407–
07–80, dated August 27, 2007.
(4) The following service information was
approved for IBR on April 17, 2003 (68 FR
11967, March 13, 2003).
(i) Bell Helicopter Textron ASB No. 407–
99–26, Revision C, dated February 28, 2002.
(ii) Bell Helicopter Textron Technical
Bulletin No. 407–01–33, dated August 29,
2001.
(5) For Bell service information identified
in this AD, contact Bell Helicopter Textron
Canada, 12,800 Rue de l’Avenir, Mirabel,
Quebec J7J1R4, telephone (450) 437–2862 or
(800) 363–8023, fax (450) 433–0272 or at
https://www.bellcustomer.com/files/.
(6) You may view this service information
at FAA, Office of the Regional Counsel,
Southwest Region, 2601 Meacham Blvd.,
Room 663, Fort Worth, Texas 76137. For
information on the availability of this
material at the FAA, call (817) 222–5110.
(7) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
(202) 741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Fort Worth, Texas, on May 21,
2014.
Lance T. Gant,
Acting Directorate Manager, Rotorcraft
Directorate, Aircraft Certification Service.
[FR Doc. 2014–13263 Filed 6–20–14; 8:45 am]
BILLING CODE 4910–13–P
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Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2013–1056; Directorate
Identifier 2013–CE–046–AD; Amendment
39–17849; AD 2014–10–02]
RIN 2120–AA64
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
We are superseding
airworthiness directive (AD) 2006–11–
19 for Dornier Luftfahrt GmbH Model
Dornier 228–100, 228–101, 228–200,
228–201, 228–202, and 228–212
airplanes. This AD results from
mandatory continuing airworthiness
information (MCAI) issued by an
aviation authority of another country to
identify and correct an unsafe condition
on an aviation product. The MCAI
describes the unsafe condition as chafed
or damaged wiring on the flight deck
overhead panels (5VE and 6VE). We are
issuing this AD to require actions to
address the unsafe condition on these
products.
SUMMARY:
This AD is effective July 28,
2014.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of July 28, 2014.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2013–
1056; or in person at the Docket
Management Facility, U.S. Department
of Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue SE., Washington, DC 20590.
For service information identified in
this AD, contact RUAG Aerospace
Services GmbH, Dornier 228 Customer
Support, P.O. Box 1253, 82231
Wessling, Germany; telephone: +49 (0)
8153–30 2220; fax: +49 (0) 8153–30
4258; email: custsupport.dornier228@
ruag.com; Internet: https://
www.ruag.com/en/Aviation/Aviation_
Home. You may view this referenced
service information at the FAA, Small
Airplane Directorate, 901 Locust,
Kansas City, Missouri 64106. For
information on the availability of this
material at the FAA, call (816) 329–
4148.
DATES:
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Federal Register / Vol. 79, No. 120 / Monday, June 23, 2014 / Rules and Regulations
Karl
Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4146; fax: (816)
329–4090; email: karl.schletzbaum@
faa.gov.
SUPPLEMENTARY INFORMATION:
For the reasons described above, this AD
retains the requirements of EASA AD D–
2005–438, which is superseded, and requires
the implementation of the life limits and
maintenance actions as specified in the
TLMCM (TM–TLMCM–090305–ALL
respectively TM–TLMCM–228–00002–
150610) for zone 321 overhead panels 5VE/
6VE.
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to add an AD that would apply
to Dornier Luftfahrt GmbH Model
DORNIER LUFTFAHRT GmbH Models
Dornier 228–100, 228–101, 228–200,
228–201, 228–202, and 228–212
airplanes. The NPRM was published in
the Federal Register on December 23,
2013 (78 FR 77380), and proposed to
supersede AD 2006–11–19, Amendment
39–14624 (71 FR 32268; June 5, 2006).
Since we issued AD 2006–11–19,
Amendment 39–14624 (71 FR 32268;
June 5, 2006), DORNIER LUFTFAHRT
GmbH changed the compliance time
between repetitive inspections and
incorporated those inspections into the
Time Limits/Maintenance Checks
Manual (TLMCM).
The NPRM proposed to correct an
unsafe condition for the specified
products and was based on mandatory
continuing airworthiness information
(MCAI) originated by an aviation
authority of another country. The MCAI
states that:
The MCAI can be found in the AD
docket on the Internet at: https://
www.regulations.gov/
#!documentDetail;D=FAA-2013-10560002.
After the NPRM was issued, we
identified that we inadvertently omitted
the calendar time compliance for the
inspections of the wiring in the flight
deck overhead panels. We issued a
supplemental notice of proposed
rulemaking (SNPRM) to propose adding
the calendar time compliance for the
inspections of the wiring in the flight
deck overhead panels. The SNPRM was
published in the Federal Register on
March 4, 2014 (79 FR 12131).
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FOR FURTHER INFORMATION CONTACT:
RUAG Aerospace Services GmbH issued
Time Limits/Maintenance Checks Manual
(TLMCM) TM–TLMCM–090305–ALL,
Revision 5 dated 20 March 2011 respectively
TM–TLMCM–228–00002–150610, Revision 1
dated 03 March 2011, listing component life
limits and describing maintenance
instructions for the Dornier 228 type design.
The Document TM–TLMCM–228–00002–
150610 is valid for airplane SN 8300 and up
and other airplane SN modified according to
CN–228–247. The instructions contained in
that manual have been identified as
mandatory actions for continued
airworthiness.
In 2005, chafed wiring was found on 5VE
Panel due to lost adhesive of the TY–RAP
holder and subsequent vibration of the cable
harness.
To address this potential unsafe condition,
RUAG issued All Operators Telefax (AOT)
No. AOT–228–24–028 and Temporary
Revision (TR) 05–05 of the TLMCM
introducing repetitive of the cockpit
overhead panels 5VE and 6VE and,
depending on findings, corrective actions(s).
Subsequently, LBA issued AD D–2005–438
(EASA approval 2005–6430) to require those
actions.
Since that AD was issued, the instructions
of TR 05–05 have been incorporated into
TM–TLMCM–090305–ALL, Revision 5 dated
20 March 2011 respectively into TM–
TLMCM–228–00002–150610, Revision 1
dated 03 March 2011.
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Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the SNPRM
(79 FR 12131, March 4, 2014) or on the
determination of the cost to the public.
Conclusion
We reviewed the relevant data and
determined that air safety and the
public interest require adopting the AD
as proposed except for minor editorial
changes. We have determined that these
minor changes:
• Are consistent with the intent that
was proposed in the SNPRM (79 FR
12131, March 4, 2014) for correcting the
unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the SNPRM (79 FR 12131,
March 4, 2014).
Costs of Compliance
We estimate that this AD will affect
17 products of U.S. registry. We also
estimate that it will take about 2 workhours per product to comply with the
basic requirements of this AD. The
average labor rate is $85 per work-hour.
Based on these figures, we estimate
the cost of the proposed AD on U.S.
operators to be $2,890 or $170 per
product.
In addition, we estimate that any
necessary follow-on actions would take
about 3 work-hours and require parts
costing $1,000, for a cost of $1,255 per
product. We have no way of
determining the number of products
that may need these actions.
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Authority for This Rulemaking
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 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, Section 44701:
General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, 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 to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We determined that this AD will not
have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Is not a ‘‘significant rule’’ under
the DOT Regulatory Policies and
Procedures (44 FR 11034, February 26,
1979),
(3) Will not affect intrastate aviation
in Alaska, and
(4) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2013–
1056; or in person at the Docket
Management Facility between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket
contains the NPRM/SNPRM, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Office
(telephone (800) 647–5527) is in the
ADDRESSES section. Comments will be
available in the AD docket shortly after
receipt.
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Federal Register / Vol. 79, No. 120 / Monday, June 23, 2014 / Rules and Regulations
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing Amendment 39–14624 (71 FR
32268; June 5, 2006) and adding the
following new AD:
■
2014–10–02 Dornier Luftfahrt GmbH:
Amendment 39–17849; Docket No.
FAA–2013–1056; Directorate Identifier
2013–CE–046–AD.
(a) Effective Date
This airworthiness directive (AD) becomes
effective July 28, 2014.
(b) Affected ADs
This AD supersedes AD 2006–11–19,
Amendment 39–14624 (71 FR 32268; June 5,
2006).
(c) Applicability
This AD applies to Dornier Luftfahrt GmbH
Dornier Models 228–100, 228–101, 228–200,
228–201, 228–202, and 228–212 airplanes, all
serial numbers, certificated in any category.
(d) Subject
Air Transport Association of America
(ATA) Code 5: Time Limits.
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(e) Reason
This AD was prompted by mandatory
continuing airworthiness information (MCAI)
originated by an aviation authority of another
country to identify and correct an unsafe
condition on an aviation product. The MCAI
describes the unsafe condition as chafed or
damaged wiring on the flight deck overhead
panels (5VE and 6VE). We are issuing this
AD to prevent chafing and damage to the
wiring in the flight deck overhead panels,
which could result in short-circuiting of
related wiring and possibly lead to electrical
failure of affected systems and potential fire
in the flight deck.
(f) Actions and Compliance
Unless already done, do the following
actions in paragraphs (f)(1) through (f)(3) of
this AD:
(1) Within the next 600 hours time-inservice (TIS) after July 28, 2014 (the effective
date of this AD) or within the next 12 months
after July 28, 2014 (the effective date of this
AD), whichever occurs first, and repetitively
thereafter at intervals not to exceed 600 hours
TIS or 12 months, whichever occurs first,
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inspect the wiring in the flight deck overhead
panels, 5VE and 6VE, for chafing, damage,
and/or incorrect installation (wire tie
attachment holders). For the inspection, refer
to:
(i) Zone 321 on page 5, dated May 1, 2006,
in section 05–22–10, Zonal Inspection
Program, in Chapter 05, Time Limits/
Maintenance Checks—General, in RUAG
Aerospace Services GmbH Dornier 228 Time
Limits/Maintenance Checks Manual
(TLMCM), TM–TLMCM–090305–ALL,
Revision 5, March 20, 2011;
(ii) Zone 321 on page 5, dated May 1, 2006,
in section 05–26–10, Low Utilization Zonal
Inspection Program, in Chapter 05, Time
Limits/Maintenance Checks—General, in
RUAG Aerospace Services GmbH Dornier
228 Time Limits/Maintenance Checks
Manual (TLMCM), TM–TLMCM–090305–
ALL, Revision 5, March 20, 2011;
(iii) Pages 1 through 10, Overhead Panel
5VE—Description, dated November 25, 2009,
in subject 31–10–07, of Chapter 31,
Indicating/Recording Systems, in RUAG
Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM–AMM–
228–00014–080184, Revision 3, October 30,
2012;
(iv) Pages 201 through 208, Overhead Panel
5VE—Maintenance Practices, dated
November 25, 2009, in subject 31–10–07, of
Chapter 31, Indicating/Recording Systems, in
RUAG Aerospace Services GmbH Dornier
228 Airplane Maintenance Manual, TM–
AMM–228–00014–080184, Revision 3,
October 30, 2012;
(v) Pages 1 and 2, Overhead Panel 6VE—
Description, in subject 31–10–08, dated
November 25, 2009, of Chapter 31,
Indicating/Recording Systems, in RUAG
Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM–AMM–
228–00014–080184, Revision 3, October 30,
2012;
(vi) Pages 201 through 204, Overhead Panel
6VE—Maintenance Practices, in subject 31–
10–08, dated November 25, 2009, of Chapter
31, Indicating/Recording Systems, in RUAG
Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM–AMM–
228–00014–080184, Revision 3, October 30,
2012.
(2) If any chafed or damaged wires are
found during any inspection required in
paragraph (f)(1) of this AD, before further
flight, repair the affected wire(s) and assure
correct installation of the wiring in the flight
deck overhead panels by reattaching or
replacing the wire tie attachment holders and
securing any loose wires to the wire tie
attachment holders with plastic wire ties
following:
(i) Pages 1 through 10, Overhead Panel
5VE—Description, dated November 25, 2009,
in subject 31–10–07, of Chapter 31,
Indicating/Recording Systems, in RUAG
Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM–AMM–
228–00014–080184, Revision 3, October 30,
2012;
(ii) Pages 201 through 208, Overhead Panel
5VE—Maintenance Practices, dated
November 25, 2009, in subject 31–10–07, of
Chapter 31, Indicating/Recording Systems, in
RUAG Aerospace Services GmbH Dornier
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35487
228 Airplane Maintenance Manual, TM–
AMM–228–00014–080184, Revision 3,
October 30, 2012;
(iii) Pages 1 and 2, Overhead Panel 6VE—
Description, in subject 31–10–08, dated
November 25, 2009, of Chapter 31,
Indicating/Recording Systems, in RUAG
Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM–AMM–
228–00014–080184, Revision 3, October 30,
2012;
(iv) Pages 201 through 204, Overhead Panel
6VE—Maintenance Practices, in subject 31–
10–08, dated November 25, 2009, of Chapter
31, Indicating/Recording Systems, in RUAG
Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM–AMM–
228–00014–080184, Revision 3, October 30,
2012.
(3) To comply with the actions of this AD,
you may insert a copy of this AD or a copy
of the required actions of this AD into the
instructions for continued airworthiness
section of the FAA-approved maintenance
program (e.g., maintenance manual). This
action may be done by an owner/operator
(pilot) holding at least a private pilot
certificate and must be entered into the
airplane records showing compliance with
this AD in accordance with 14 CFR 43.9
(a)(1)(4) and 14 CFR 91.417(a)(2)(v). The
record must be maintained as required by 14
CFR 91.173 or 135.439.
(g) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Standards Office,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. Send information to
ATTN: Karl Schletzbaum, Aerospace
Engineer, FAA, Small Airplane Directorate,
901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329–4146; fax: (816)
329–4090; email: karl.schletzbaum@faa.gov.
Before using any approved AMOC on any
airplane to which the AMOC applies, notify
your appropriate principal inspector (PI) in
the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement
in this AD to obtain corrective actions from
a manufacturer or other source, use these
actions if they are FAA-approved. Corrective
actions are considered FAA-approved if they
are approved by the State of Design Authority
(or their delegated agent). You are required
to assure the product is airworthy before it
is returned to service.
(h) Related Information
Refer to MCAI European Aviation Safety
Agency (EASA) AD No.: 2013–0244, dated
October 4, 2013, for related information. You
may examine the MCAI on the Internet at
https://www.regulations.gov/
#!documentDetail;D=FAA-2013-1056-0002.
(i) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
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Federal Register / Vol. 79, No. 120 / Monday, June 23, 2014 / Rules and Regulations
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) Chapter 05, Time Limits/Maintenance
Checks—General, in RUAG Aerospace
Services GmbH Dornier 228 Time Limits/
Maintenance Checks Manual (TLMCM), TM–
TLMCM–090305–ALL, Revision 5, March 20,
2011:
(A) Page 5, in section 05–22–10, Zonal
Inspection Program, dated May 1, 2006;
(B) Page 5, in section 05–26–10, Low
Utilization Zonal Inspection Program, dated
May 1, 2006.
(ii) Chapter 31, Indicating/Recording
Systems, in RUAG Aerospace Services GmbH
Dornier 228 Airplane Maintenance Manual,
TM–AMM–228–00014–080184, Revision 3,
October 30, 2012:
(A) Pages 1 through 10, Overhead Panel
5VE—Description, in subject 31–10–07,
dated November 25, 2009;
(B) Pages 201 through 208, Overhead Panel
5VE—Maintenance Practices, in subject 31–
10–07, dated November 25, 2009;
(C) Pages 1 and 2, Overhead Panel 6VE—
Description, in subject 31–10–08, dated
November 25, 2009;
(D) Pages 201 through 204, Overhead Panel
6VE—Maintenance Practices, in subject 31–
10–08, dated November 25, 2009.
(3) For service information identified in
this AD, contact RUAG Aerospace Services
GmbH, Dornier 228 Customer Support, P.O.
Box 1253, 82231 Wessling, Germany;
telephone: +49 (0) 8153–30 2220; fax: +49 (0)
8153–30 4258; email:
custsupport.dornier228@ruag.com; Internet:
https://www.ruag.com/en/Aviation/Aviation_
Home.
(4) You may view this referenced service
information at the FAA, Small Airplane
Directorate, 901 Locust, Kansas City,
Missouri 64106. For information on the
availability of this material at the FAA, call
(816) 329–4148.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 93
[Docket No.: FAA–2010–0302; Amdt. No.
93–98]
RIN 2120–AK46
The Extension of the Expiration Date of
the New York North Shore Helicopter
Route
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
[FR Doc. 2014–14336 Filed 6–20–14; 8:45 am]
The action amends the
expiration date of the final rule
requiring pilots flying civil helicopters
under Visual Flight Rules to use the
New York North Shore Helicopter Route
when operating along the north shore of
Long Island, New York. The current rule
expires on August 6, 2014. The FAA
finds it necessary to extend this rule for
an additional two years to preserve the
current operating environment in order
to determine whether the mandatory use
of this route should be made permanent.
The FAA will conduct notice and
comment rulemaking on the permanent
use of this route. A limited extension of
the current rule provides needed time to
conduct the appropriate analysis to
assess the rule’s impact and proper
rulemaking procedures.
DATES: This final rule is effective August
6, 2014, through August 6, 2016.
FOR FURTHER INFORMATION CONTACT: For
technical questions concerning this
action, contact David Maddox, Airspace
Regulation and ATC Procedures Group,
AJV–113, Federal Aviation
Administration, 800 Independence
Avenue SW., Washington, DC 20591;
telephone 202–267- 8783; email
david.maddox@faa.gov.
For legal questions concerning this
action, contact Lorelei Peter,
International Law, Legislation and
Regulations Division, AGC–200, Office
of the Chief Counsel, Federal Aviation
Administration, 800 Independence
Avenue SW., Washington, DC 20591;
telephone 202–267–3073; email
Lorelei.Peter@faa.gov.
SUPPLEMENTARY INFORMATION:
BILLING CODE 4910–13–P
Authority for This Rulemaking
pmangrum on DSK3VPTVN1PROD with RULES
Issued in Kansas City, Missouri, on June
13, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
SUMMARY:
The FAA’s authority to issue rules on
aviation safety is found in Title 49 of the
United States Code. Subtitle I, Section
106 describes the authority of the FAA
Administrator. Subtitle VII, Aviation
Programs, describes in more detail the
scope of the agency’s authority.
VerDate Mar<15>2010
14:40 Jun 20, 2014
Jkt 232001
PO 00000
Frm 00010
Fmt 4700
Sfmt 4700
The FAA has broad authority and
responsibility to regulate the operation
of aircraft, the use of the navigable
airspace and to establish safety
standards for and regulate the
certification of airmen, aircraft, and air
carriers. (49 U.S.C. 40104 et seq.,
40103(b)). The FAA’s authority for this
rule is contained in 49 U.S.C. 40103 and
44715. Under section 40103, the
Administrator of the FAA has authority
to ‘‘prescribe air traffic regulations on
the flight of aircraft (including
regulations on safe altitudes) for * * *
(B) protecting individuals and property
on the ground. (49 U.S.C. 40103(b)(2)).
In addition, section 44715(a), provides
that to ‘‘relieve and protect the public
health and welfare from aircraft noise,’’
the Administrator of the FAA, ‘‘as he
deems necessary, shall prescribe * * *
(ii) regulations to control and abate
aircraft noise * * *.’’
I. Background
In response to concerns from local
residents regarding noise from
helicopters operating over Long Island,
the FAA adopted the New York North
Shore Helicopter Route final rule (77 FR
39911). The rule is based on a voluntary
Visual Flight Rule (VFR) route that was
developed by the FAA working with the
Eastern Region Helicopter Council. The
rule requires civil helicopter pilots
operating under VFR, whose route of
flight takes them over the north shore of
Long Island between the VPLYD
waypoint and Orient point, to use the
North Shore Helicopter Route, as
published in the New York Helicopter
Chart.1 The rule permits pilots to
deviate from the route and altitude
requirements when necessary for safety,
weather conditions, or transitioning to
or from a destination or point of
landing. The rule was promulgated to
maximize use of the route as published
in order to secure and improve upon
decreased levels of noise that had been
voluntarily achieved.
The current rule terminates on August
6, 2014. The FAA limited the duration
of the rule because at the time of
promulgation the FAA did not know the
current rate of compliance with the
voluntary route or the circumstances
surrounding an operator’s decision to
not use the route. The FAA concluded
that ‘‘There is no reason to retain this
rule if the FAA determines that it is not
actually improving the noise situation
along the north shore of Long Island.’’ 2
Accordingly, the agency decided that
1 The voluntary route originally was added to the
Helicopter Route Chart for New York on May 8,
2008.
2 See 77 FR 39918.
E:\FR\FM\23JNR1.SGM
23JNR1
]]>Agencies
[Federal Register Volume 79, Number 120 (Monday, June 23, 2014)]
[Rules and Regulations]
[Pages 35485-35488]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-14336]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-1056; Directorate Identifier 2013-CE-046-AD;
Amendment 39-17849; AD 2014-10-02]
RIN 2120-AA64
Airworthiness Directives; Dornier Luftfahrt GmbH Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are superseding airworthiness directive (AD) 2006-11-19 for
Dornier Luftfahrt GmbH Model Dornier 228-100, 228-101, 228-200, 228-
201, 228-202, and 228-212 airplanes. This AD results from mandatory
continuing airworthiness information (MCAI) issued by an aviation
authority of another country to identify and correct an unsafe
condition on an aviation product. The MCAI describes the unsafe
condition as chafed or damaged wiring on the flight deck overhead
panels (5VE and 6VE). We are issuing this AD to require actions to
address the unsafe condition on these products.
DATES: This AD is effective July 28, 2014.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of July 28, 2014.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2013-
1056; or in person at the Docket Management Facility, U.S. Department
of Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.
For service information identified in this AD, contact RUAG
Aerospace Services GmbH, Dornier 228 Customer Support, P.O. Box 1253,
82231 Wessling, Germany; telephone: +49 (0) 8153-30 2220; fax: +49 (0)
8153-30 4258; email: custsupport.dornier228@ruag.com; Internet: https://www.ruag.com/en/Aviation/Aviation_Home. You may view this referenced
service information at the FAA, Small Airplane Directorate, 901 Locust,
Kansas City, Missouri 64106. For information on the availability of
this material at the FAA, call (816) 329-4148.
[[Page 35486]]
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090; email:
karl.schletzbaum@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to add an AD that would apply to Dornier Luftfahrt GmbH Model
DORNIER LUFTFAHRT GmbH Models Dornier 228-100, 228-101, 228-200, 228-
201, 228-202, and 228-212 airplanes. The NPRM was published in the
Federal Register on December 23, 2013 (78 FR 77380), and proposed to
supersede AD 2006-11-19, Amendment 39-14624 (71 FR 32268; June 5,
2006).
Since we issued AD 2006-11-19, Amendment 39-14624 (71 FR 32268;
June 5, 2006), DORNIER LUFTFAHRT GmbH changed the compliance time
between repetitive inspections and incorporated those inspections into
the Time Limits/Maintenance Checks Manual (TLMCM).
The NPRM proposed to correct an unsafe condition for the specified
products and was based on mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country. The MCAI states that:
RUAG Aerospace Services GmbH issued Time Limits/Maintenance
Checks Manual (TLMCM) TM-TLMCM-090305-ALL, Revision 5 dated 20 March
2011 respectively TM-TLMCM-228-00002-150610, Revision 1 dated 03
March 2011, listing component life limits and describing maintenance
instructions for the Dornier 228 type design. The Document TM-TLMCM-
228-00002-150610 is valid for airplane SN 8300 and up and other
airplane SN modified according to CN-228-247. The instructions
contained in that manual have been identified as mandatory actions
for continued airworthiness.
In 2005, chafed wiring was found on 5VE Panel due to lost
adhesive of the TY-RAP holder and subsequent vibration of the cable
harness.
To address this potential unsafe condition, RUAG issued All
Operators Telefax (AOT) No. AOT-228-24-028 and Temporary Revision
(TR) 05-05 of the TLMCM introducing repetitive of the cockpit
overhead panels 5VE and 6VE and, depending on findings, corrective
actions(s). Subsequently, LBA issued AD D-2005-438 (EASA approval
2005-6430) to require those actions.
Since that AD was issued, the instructions of TR 05-05 have been
incorporated into TM-TLMCM-090305-ALL, Revision 5 dated 20 March
2011 respectively into TM-TLMCM-228-00002-150610, Revision 1 dated
03 March 2011.
For the reasons described above, this AD retains the
requirements of EASA AD D-2005-438, which is superseded, and
requires the implementation of the life limits and maintenance
actions as specified in the TLMCM (TM-TLMCM-090305-ALL respectively
TM-TLMCM-228-00002-150610) for zone 321 overhead panels 5VE/6VE.
The MCAI can be found in the AD docket on the Internet at: https://www.regulations.gov/#!documentDetail;D=FAA-2013-1056-0002.
After the NPRM was issued, we identified that we inadvertently
omitted the calendar time compliance for the inspections of the wiring
in the flight deck overhead panels. We issued a supplemental notice of
proposed rulemaking (SNPRM) to propose adding the calendar time
compliance for the inspections of the wiring in the flight deck
overhead panels. The SNPRM was published in the Federal Register on
March 4, 2014 (79 FR 12131).
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the SNPRM (79 FR 12131, March 4,
2014) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting the AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
SNPRM (79 FR 12131, March 4, 2014) for correcting the unsafe condition;
and
Do not add any additional burden upon the public than was
already proposed in the SNPRM (79 FR 12131, March 4, 2014).
Costs of Compliance
We estimate that this AD will affect 17 products of U.S. registry.
We also estimate that it will take about 2 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour.
Based on these figures, we estimate the cost of the proposed AD on
U.S. operators to be $2,890 or $170 per product.
In addition, we estimate that any necessary follow-on actions would
take about 3 work-hours and require parts costing $1,000, for a cost of
$1,255 per product. We have no way of determining the number of
products that may need these actions.
Authority for This Rulemaking
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
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, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, 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 to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation in Alaska, and
(4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2013-
1056; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains the NPRM/SNPRM, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (telephone (800) 647-5527) is in the ADDRESSES section. Comments
will be available in the AD docket shortly after receipt.
[[Page 35487]]
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by removing Amendment 39-14624 (71 FR
32268; June 5, 2006) and adding the following new AD:
2014-10-02 Dornier Luftfahrt GmbH: Amendment 39-17849; Docket No.
FAA-2013-1056; Directorate Identifier 2013-CE-046-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective July 28,
2014.
(b) Affected ADs
This AD supersedes AD 2006-11-19, Amendment 39-14624 (71 FR
32268; June 5, 2006).
(c) Applicability
This AD applies to Dornier Luftfahrt GmbH Dornier Models 228-
100, 228-101, 228-200, 228-201, 228-202, and 228-212 airplanes, all
serial numbers, certificated in any category.
(d) Subject
Air Transport Association of America (ATA) Code 5: Time Limits.
(e) Reason
This AD was prompted by mandatory continuing airworthiness
information (MCAI) originated by an aviation authority of another
country to identify and correct an unsafe condition on an aviation
product. The MCAI describes the unsafe condition as chafed or
damaged wiring on the flight deck overhead panels (5VE and 6VE). We
are issuing this AD to prevent chafing and damage to the wiring in
the flight deck overhead panels, which could result in short-
circuiting of related wiring and possibly lead to electrical failure
of affected systems and potential fire in the flight deck.
(f) Actions and Compliance
Unless already done, do the following actions in paragraphs
(f)(1) through (f)(3) of this AD:
(1) Within the next 600 hours time-in-service (TIS) after July
28, 2014 (the effective date of this AD) or within the next 12
months after July 28, 2014 (the effective date of this AD),
whichever occurs first, and repetitively thereafter at intervals not
to exceed 600 hours TIS or 12 months, whichever occurs first,
inspect the wiring in the flight deck overhead panels, 5VE and 6VE,
for chafing, damage, and/or incorrect installation (wire tie
attachment holders). For the inspection, refer to:
(i) Zone 321 on page 5, dated May 1, 2006, in section 05-22-10,
Zonal Inspection Program, in Chapter 05, Time Limits/Maintenance
Checks--General, in RUAG Aerospace Services GmbH Dornier 228 Time
Limits/Maintenance Checks Manual (TLMCM), TM-TLMCM-090305-ALL,
Revision 5, March 20, 2011;
(ii) Zone 321 on page 5, dated May 1, 2006, in section 05-26-10,
Low Utilization Zonal Inspection Program, in Chapter 05, Time
Limits/Maintenance Checks--General, in RUAG Aerospace Services GmbH
Dornier 228 Time Limits/Maintenance Checks Manual (TLMCM), TM-TLMCM-
090305-ALL, Revision 5, March 20, 2011;
(iii) Pages 1 through 10, Overhead Panel 5VE--Description, dated
November 25, 2009, in subject 31-10-07, of Chapter 31, Indicating/
Recording Systems, in RUAG Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM-AMM-228-00014-080184, Revision 3,
October 30, 2012;
(iv) Pages 201 through 208, Overhead Panel 5VE--Maintenance
Practices, dated November 25, 2009, in subject 31-10-07, of Chapter
31, Indicating/Recording Systems, in RUAG Aerospace Services GmbH
Dornier 228 Airplane Maintenance Manual, TM-AMM-228-00014-080184,
Revision 3, October 30, 2012;
(v) Pages 1 and 2, Overhead Panel 6VE--Description, in subject
31-10-08, dated November 25, 2009, of Chapter 31, Indicating/
Recording Systems, in RUAG Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM-AMM-228-00014-080184, Revision 3,
October 30, 2012;
(vi) Pages 201 through 204, Overhead Panel 6VE--Maintenance
Practices, in subject 31-10-08, dated November 25, 2009, of Chapter
31, Indicating/Recording Systems, in RUAG Aerospace Services GmbH
Dornier 228 Airplane Maintenance Manual, TM-AMM-228-00014-080184,
Revision 3, October 30, 2012.
(2) If any chafed or damaged wires are found during any
inspection required in paragraph (f)(1) of this AD, before further
flight, repair the affected wire(s) and assure correct installation
of the wiring in the flight deck overhead panels by reattaching or
replacing the wire tie attachment holders and securing any loose
wires to the wire tie attachment holders with plastic wire ties
following:
(i) Pages 1 through 10, Overhead Panel 5VE--Description, dated
November 25, 2009, in subject 31-10-07, of Chapter 31, Indicating/
Recording Systems, in RUAG Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM-AMM-228-00014-080184, Revision 3,
October 30, 2012;
(ii) Pages 201 through 208, Overhead Panel 5VE--Maintenance
Practices, dated November 25, 2009, in subject 31-10-07, of Chapter
31, Indicating/Recording Systems, in RUAG Aerospace Services GmbH
Dornier 228 Airplane Maintenance Manual, TM-AMM-228-00014-080184,
Revision 3, October 30, 2012;
(iii) Pages 1 and 2, Overhead Panel 6VE--Description, in subject
31-10-08, dated November 25, 2009, of Chapter 31, Indicating/
Recording Systems, in RUAG Aerospace Services GmbH Dornier 228
Airplane Maintenance Manual, TM-AMM-228-00014-080184, Revision 3,
October 30, 2012;
(iv) Pages 201 through 204, Overhead Panel 6VE--Maintenance
Practices, in subject 31-10-08, dated November 25, 2009, of Chapter
31, Indicating/Recording Systems, in RUAG Aerospace Services GmbH
Dornier 228 Airplane Maintenance Manual, TM-AMM-228-00014-080184,
Revision 3, October 30, 2012.
(3) To comply with the actions of this AD, you may insert a copy
of this AD or a copy of the required actions of this AD into the
instructions for continued airworthiness section of the FAA-approved
maintenance program (e.g., maintenance manual). This action may be
done by an owner/operator (pilot) holding at least a private pilot
certificate and must be entered into the airplane records showing
compliance with this AD in accordance with 14 CFR 43.9 (a)(1)(4) and
14 CFR 91.417(a)(2)(v). The record must be maintained as required by
14 CFR 91.173 or 135.439.
(g) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Office, FAA, has the authority to approve AMOCs for this
AD, if requested using the procedures found in 14 CFR 39.19. Send
information to ATTN: Karl Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090;
email: karl.schletzbaum@faa.gov. Before using any approved AMOC on
any airplane to which the AMOC applies, notify your appropriate
principal inspector (PI) in the FAA Flight Standards District Office
(FSDO), or lacking a PI, your local FSDO.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(h) Related Information
Refer to MCAI European Aviation Safety Agency (EASA) AD No.:
2013-0244, dated October 4, 2013, for related information. You may
examine the MCAI on the Internet at https://www.regulations.gov/#!documentDetail;D=FAA-2013-1056-0002.
(i) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
[[Page 35488]]
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Chapter 05, Time Limits/Maintenance Checks--General, in RUAG
Aerospace Services GmbH Dornier 228 Time Limits/Maintenance Checks
Manual (TLMCM), TM-TLMCM-090305-ALL, Revision 5, March 20, 2011:
(A) Page 5, in section 05-22-10, Zonal Inspection Program, dated
May 1, 2006;
(B) Page 5, in section 05-26-10, Low Utilization Zonal
Inspection Program, dated May 1, 2006.
(ii) Chapter 31, Indicating/Recording Systems, in RUAG Aerospace
Services GmbH Dornier 228 Airplane Maintenance Manual, TM-AMM-228-
00014-080184, Revision 3, October 30, 2012:
(A) Pages 1 through 10, Overhead Panel 5VE--Description, in
subject 31-10-07, dated November 25, 2009;
(B) Pages 201 through 208, Overhead Panel 5VE--Maintenance
Practices, in subject 31-10-07, dated November 25, 2009;
(C) Pages 1 and 2, Overhead Panel 6VE--Description, in subject
31-10-08, dated November 25, 2009;
(D) Pages 201 through 204, Overhead Panel 6VE--Maintenance
Practices, in subject 31-10-08, dated November 25, 2009.
(3) For service information identified in this AD, contact RUAG
Aerospace Services GmbH, Dornier 228 Customer Support, P.O. Box
1253, 82231 Wessling, Germany; telephone: +49 (0) 8153-30 2220; fax:
+49 (0) 8153-30 4258; email: custsupport.dornier228@ruag.com;
Internet: https://www.ruag.com/en/Aviation/Aviation_Home.
(4) You may view this referenced service information at the FAA,
Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106.
For information on the availability of this material at the FAA,
call (816) 329-4148.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on June 13, 2014.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2014-14336 Filed 6-20-14; 8:45 am]
BILLING CODE 4910-13-P
