AD 2011-21-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Diamond Aircraft Industries GmbH | DA 40 | Airworthiness Directives; Diamond Aircraft Industries GmbH Airplanes With Supplemental Type Certificate (STC) SA03674AT |
Unsafe Condition
Damage around the VCS compressor mounting area found during maintenance inspections, resulting from excessive wear, which could lead to the air conditioner compressor disconnecting in the engine compartment, potentially causing engine stoppage or additional engine damage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Deactivate the VCS system, pull and collar the compressor breaker with a placard stating 'INOP', remove the VCS compressor and associated mounting hardware, and revise the airplane weight and balance.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 100 hours time-in-service after installation of the VCS or within 30 days after November 16, 2011, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Diamond Aircraft Industries GmbH Model DA 40 airplanes, all serial numbers, equipped with vapor cycle system (VCS) cabin air conditioning installed per STC SA03674AT following DER Services Master Document List MDL-2006-020-1, Revisions C, D, E, or F.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for Diamond Aircraft Industries GmbH Model (Diamond) DA 40 airplanes equipped with cabin air conditioning vapor cycle system (VCS) installed per STC SA03674AT held by Premier Aircraft Services (originally held by DER Services, Inc.) following DER Services Master Document List MDL-2006- 020-1, Revision C, dated February 3, 2009; Revision D, dated April 22, 2009; Revision E, dated May 12, 2010; or Revision F, dated July 6, 2010. This AD was prompted by reports of damage around the VCS compressor mounting areas found during maintenance inspections. This AD requires deactivation of the VCS, removal of the compressor and bracket, and revision to the airplane weight and balance. We are issuing this AD to correct the unsafe condition on these products.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to Diamond Aircraft Industries GmbH Model DA 40
airplanes, all serial numbers, that:
(1) Are equipped with vapor cycle system (VCS) cabin air
conditioning installed per Premier Aircraft Service STC SA03674AT
following DER Services Master Document List MDL-2006-020-1, Revision
C, dated February 3, 2009; Revision D, dated April 22, 2009;
Revision E, dated May 12, 2010; or Revision F, dated July 6, 2010;
and
(2) are certificated in any category.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 76, Number 197 (Wednesday, October 12, 2011)]
[Rules and Regulations]
[Pages 63167-63169]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2011-26001]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-0687; Directorate Identifier 2011-CE-017-AD;
Amendment 39-16833; AD 2011-21-10]
RIN 2120-AA64
Airworthiness Directives; Diamond Aircraft Industries GmbH
Airplanes With Supplemental Type Certificate (STC) SA03674AT
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for Diamond
Aircraft Industries GmbH Model (Diamond) DA 40 airplanes equipped with
cabin air conditioning vapor cycle system (VCS) installed per STC
SA03674AT held by Premier Aircraft Services (originally held by DER
Services, Inc.) following DER Services Master Document List MDL-2006-
020-1, Revision C, dated February 3, 2009; Revision D, dated April 22,
2009; Revision E, dated May 12, 2010; or Revision F, dated July 6,
2010. This AD was prompted by reports of damage around the VCS
compressor mounting areas found during maintenance inspections. This AD
requires deactivation of the VCS, removal of the compressor and
bracket, and revision to the airplane weight and balance. We are
issuing this AD to correct the unsafe condition on these products.
DATES: This AD is effective November 16, 2011.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of November 16,
2011.
ADDRESSES: For service information identified in this AD, contact
Premier Aircraft Service, 5540 NW 23 Avenue Hangar 14, Ft. Lauderdale,
FL 33309, telephone: (954) 771-0411; fax: (954) 334-1489; Internet:
<a href="http://www.flypas.com">http://www.flypas.com</a>. You may review copies of the referenced service
information at the FAA, Small Airplane Directorate, 901 Locust St.,
Kansas City, Missouri 64106. For information on the availability of
this material at the FAA, call (816) 329-4148.
Examining the AD Docket
You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a>; 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 this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone: 800-647-5527) is Document 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 FURTHER INFORMATION CONTACT: Hal Horsburgh, Aerospace Engineer,
FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue,
College Park, Georgia 30337; telephone: (404) 474-5553; fax: (404) 474-
5606; e-mail: <a href="/cdn-cgi/l/email-protection#d5bdb4b9fbbdbaa7a6b7a0a7b2bd95b3b4b4fbb2baa3"><span class="__cf_email__" data-cfemail="432b222f6d2b2c3130213631242b032522226d242c35">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM published in the Federal Register on June 28, 2011 (76 FR
37684). That NPRM proposed to require removal of the VCS mount, which
could result in the air conditioner compressor disconnecting in the
engine compartment. This condition could result in engine stoppage or
additional damage to the engine.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (76 FR 37684, June 28,
2011) 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 and the addition of an optional terminating
action after the compressor is removed which will allow for the
reinstallation and reactivation of the air conditioning system. We have
determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (76 FR 37684, June 28, 2011) for correcting the unsafe condition;
and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM.
Costs of Compliance
We estimate that this AD affects 11 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
[[Page 63168]]
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Remove the VCS compressor, 3 work-hours x $85 per Not applicable $255 $2,805
deactivate system, and revise hour = $255.
weight and balance.
----------------------------------------------------------------------------------------------------------------
According to the manufacturer, all of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
individuals. We do not control warranty coverage for affected
individuals. As a result, we have included all costs in our cost
estimate.
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
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 that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under 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.
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 adding the following new airworthiness
directive (AD):
2011-21-10 Diamond Aircraft Industries GmbH Airplanes Equipped With
Supplemental Type Certificate (STC) SA03674AT: Amendment 39-16833;
Docket No. FAA-2011-0687; Directorate Identifier 2011-CE-017-AD.
(a) Effective Date
This AD is effective November 16, 2011.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Diamond Aircraft Industries GmbH Model DA 40
airplanes, all serial numbers, that:
(1) Are equipped with vapor cycle system (VCS) cabin air
conditioning installed per Premier Aircraft Service STC SA03674AT
following DER Services Master Document List MDL-2006-020-1, Revision
C, dated February 3, 2009; Revision D, dated April 22, 2009;
Revision E, dated May 12, 2010; or Revision F, dated July 6, 2010;
and
(2) are certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code 2150, Cabin Cooling
System.
(e) Unsafe Condition
This AD was prompted by reports of damage around the VCS
compressor mounting area found during maintenance inspections. We
are issuing this AD to remove the VCS compressor and mount, as a
result of excessive wear, which could result in the air conditioner
compressor disconnecting in the engine compartment. This condition
could result in engine stoppage or additional damage to the engine.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Within the next 100 hours time-in-service after installation of
the VCS installed per STC SA03674AT held by Premier Aircraft Service
(originally held by DER Services, Inc.) following DER Services
Master Document List MDL-2006-020-1, Revision C, dated February 3,
2009; Revision D, dated April 22, 2009; Revision E, dated May 12,
2010; or Revision F, dated July 6, 2010, or within 30 days after
November 16, 2011 (the effective date of this AD), whichever occurs
later, do the following actions following Premier Aircraft Service
Work Instruction PAS-WI-MSB-40-2011-001, dated March 4, 2011; and
Premier Aircraft Service Mandatory Service Bulletin No. PAS-MSB-40-
2011-001, dated March 4, 2011:
(1) Deactivate the VCS system.
(2) Pull and collar the compressor breaker and place a placard
above the breaker stating ``INOP.''
(3) Remove the VCS compressor and associated mounting hardware.
(4) Revise the airplane weight and balance.
(h) Optional Actions
If all actions in paragraphs (g)(1), (g)(2), (g)(3), and (g)(4)
of this AD have been completed, an optional terminating action
allows you to reinstall the VCS compressor and reactivate the air
conditioning system following Premier Aircraft Service Service
Bulletin No. PAS-SB-40-2011-002, dated August 18, 2011; Seamech
International Inc. Vapor Cycle Air Conditioning with Automatic
Climate Control Instructions for Continued Airworthiness, ASI-
772216A, Revision G, dated August 9, 2011; Seamech International
Inc. Kit Compressor Mounting, Drawing SII 2216155, Revision D, dated
July 21, 2011; and DER Services Installation Instructions
Engineering Order EO-2006-020-1, Revision F, dated August 18, 2011.
(i) Special Flight Permit
The compressor drive belt must be cut and removed before the
airplane may be moved for one ferry flight to an approved repair
facility to comply with the remainder of this AD.
(j) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Atlanta 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
[[Page 63169]]
attention of the person identified in the Related Information
section of this AD.
(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.
(k) Related Information
For more information about this AD, contact Hal Horsburgh,
Aerospace Engineer, FAA, Atlanta ACO, 1701 Columbia Avenue, College
Park, Georgia 30337; telephone: (404) 474-5553; fax: (404) 474-5606;
e-mail: <a href="/cdn-cgi/l/email-protection#197178753771766b6a7b6c6b7e71597f7878377e766f"><span class="__cf_email__" data-cfemail="99f1f8f5b7f1f6ebeafbecebfef1d9fff8f8b7fef6ef">[email protected]</span></a>.
(l) Material Incorporated by Reference
(1) You must use the following service information to do the
actions required by this AD, unless the AD specifies otherwise. The
Director of the Federal Register approved the incorporation by
reference (IBR) under 5 U.S.C. 552(a) and 1 CFR part 51 of the
following service information on November 16, 2011:
(i) Premier Aircraft Service Work Instruction PAS-WI-MSB-40-
2011-001, dated March 4, 2011; and
(ii) Premier Aircraft Service Mandatory Service Bulletin No.
PAS-MSB-40-2011-001, dated March 4, 2011.
(2) If you accomplish the optional actions specified by this AD,
you must use the following service information to perform those
actions. The Director of the Federal Register approved the
incorporation by reference (IBR) of the following service
information on November 16, 2011:
(i) Premier Aircraft Service Service Bulletin No. PAS-SB-40-
2011-002, dated August 18, 2011;
(ii) Seamech International Inc. Vapor Cycle Air Conditioning
with Automatic Climate Control Instructions for Continued
Airworthiness, ASI-772216A, Revision G, dated August 9, 2011;
(iii) Seamech International Inc. Kit Compressor Mounting,
Drawing SII 2216155, Revision D, dated July 21, 2011;
(iv) DER Services Installation Instructions Engineering Order
EO-2006-020-1, Revision F, dated August 18, 2011.
(3) For service information identified in this AD, contact
Premier Aircraft Service, 5540 NW 23 Avenue Hangar 14, Ft.
Lauderdale, FL 33309, telephone: (954) 771-0411; fax: (954) 334-
1489; Internet: <a href="http://www.flypas.com">http://www.flypas.com</a>.
(4) You may review copies of the 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 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
material at an NARA facility, call 202-741-6030, or go to <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.
Issued in Kansas City, Missouri, on October 3, 2011.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2011-26001 Filed 10-11-11; 8:45 am]
BILLING CODE 4910-13-P
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