Published 2018-12-17 · Federal Register document 2018-27134
Airworthiness Directives; Air Comm Corporation Air Conditioning Systems
Publication summary
We are adopting a new airworthiness directive (AD) for Air Comm Corporation (Air Comm) air conditioning systems installed on various model helicopters. This AD requires replacing electrical connectors and prohibits the installation of other parts. This AD was prompted by reports of overheated connectors. The actions of this AD are intended to address an unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:58.123663+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2018-258c65fa72d503e0
- Source row
- results[391]
- Raw source SHA-256
- 258c65fa72d503e0b0dfb928a28beb1793ddc7dd9218bce0413e53dfe11d78fb
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2018-25-17
- Effective date printed in this edition
- 2019-01-22
Some source clauses remain unstructured. Read the complete publication for conditions that have not been interpreted here.
Read 10 complete recorded clauses
Applicability wording · Applicability
(a) Applicability
This AD applies to the following helicopters, certificated in
any category:
(1) Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3,
AS350BA, AS350C, AS350D, and AS350D1 helicopters with an Air Comm
air conditioning system part number (P/N) AS350-202-1, AS350-202-2,
AS350-202-3, AS350-202-4, AS350-202-5, AS350-204-1, AS350-204-2,
AS350-204-3, AS350-204-4, AS350-204-5, AS350-204-6, AS350-204-7,
AS350-204-8, AS350-204-9, AS350-204-10, AS350-204-11, or AS350-204-
12 installed.
(2) Airbus Helicopters Model EC130B4 helicopters with an Air
Comm air conditioning system P/N EC130-202-1, EC130-202-2, EC130-
202-3, EC130-202-4, EC130-202-5, EC130-202-6, EC130-202-7, or EC130-
202-8 installed.
(3) Bell Helicopter Textron Canada Limited (Bell) Model 206A,
206B, 206L, 206L-1, 206L-3, and 206L-4 helicopters with an Air Comm
air conditioning system P/N 206EC-200, 206EC-201, 206EC-202, 206EC-
203, 206EC-204, 206EC-205, 206EC-206, 206EC-207, 206EC-208, 206EC-
209, 206EC-210, 206EC-211, or 206EC-212 installed.
(4) Bell Model 407 helicopters with an Air Comm air conditioning
system P/N 407 EC-201, 407 EC-202, or 407 EC-203 installed.
Exact source excerpt. Text positions 11634–12824, end exclusive, in the original decoded publication. SHA-256: ca5e96c9dc9383e50553f5302db21ad109e03b84a7c1d02e8a19588fa9505765
Unsafe Condition
(b) Unsafe Condition
This AD defines the unsafe condition as an overheated connector.
This condition could result in a fire and subsequent loss of control
of the helicopter.
Exact source excerpt. Text positions 12824–13006, end exclusive, in the original decoded publication. SHA-256: a1dceb4d5f76b6cdcadbc984ed117e5c8e8d62ba0ddcf6b20fe5cd0408cc0126
Effective Date
(c) Effective Date
This AD becomes effective January 22, 2019.
Exact source excerpt. Text positions 13006–13075, end exclusive, in the original decoded publication. SHA-256: 83e0a56aabfb055d0fed9e8cf5503da760079cab6bca33eb8707861311ffcb55
Compliance
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
Exact source excerpt. Text positions 13075–13262, end exclusive, in the original decoded publication. SHA-256: 56042b53a75a0db2af067b711f9b82d8091413842e43863752e31aeffdd54a72
Required Actions
(e) Required Actions
(1) Within 90 hours time-in-service:
(i) For Airbus Helicopters Model AS350B, AS350B1, AS350B2,
AS350B3, AS350BA, AS350C, AS350D, and AS350D1 helicopters, replace
each aft evaporator blower motor connector with an Air Comm
connector as depicted in Figures 2, 3, and 4 of Air Comm Service
Bulletin (SB) SB AS350-1110014, Revision B, dated January 10, 2017,
by using a Deutsch HDT-48-00 or an equivalent MIL-DTL22520 Type 1
crimping tool.
(ii) For Airbus Helicopters Model EC130B4 helicopters, replace
each aft evaporator blower motor connector with an Air Comm
connector as depicted in Figures 2, 3, and 4 of Air Comm SB EC130-
6204, Revision B, dated January 10, 2017, by using a Deutsch HDT-48-
00 or an equivalent MIL-DTL22520 Type 1 crimping tool.
(iii) For Bell Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-
4 helicopters, replace each aft evaporator blower motor connector
with an Air Comm connector as depicted in Figures 4, 5, and 6 of Air
Comm SB 206-110414, Revision C, dated January 13, 2017, by using a
Deutsch HDT-48-00 or an equivalent MIL-DTL22520 Type 1 crimping
tool.
(iv) For Bell Model 407 helicopters, replace each aft evaporator
blower motor connector with an Air Comm connector as depicted in
Figures 4, 5, and 6 of Air Comm SB 407-110414, Revision D, dated
January 13, 2017, by using a Deutsch HDT-48-00 or an equivalent MIL-
DTL22520 Type 1 crimping tool.
(2) After the effective date of this AD, do not install the
following in any aft evaporator assembly P/Ns AS350-6202-1, EC130-
6204-1, or EC130-6204-2; aft evaporator blower assembly P/Ns S-
6078EC-15, S-6102EC-3, or S-6102EC-4; or aft condenser blower P/Ns
S-7060EC-1, S-7060EC-2, S-7062EC-1 or S-7062EC-2:
(i) Plug P/N 03-09-1022 and 03-09-1032;
(ii) Socket P/N 02-09-1103 and 02-09-1104;
(iii) Receptacle P/N 03-09-2022 and 03-09-2032; and
(iv) Pin P/N 02-09-2103.
Exact source excerpt. Text positions 13262–15193, end exclusive, in the original decoded publication. SHA-256: f504cf8485719a5ed7255ab524a740f60725d9fb694863095480ccd03efa0deb
Credit for Previous Actions
(f) Credit for Previous Actions
Replacing the connectors before the effective date of this AD in
accordance with Air Comm SB 206-110414, Revision A, dated June 3,
2016; SB AS350-111014 or SB EC130-6204, both Revision A and both
dated July 6, 2016; SB 407-110414, Revision B, dated July 6, 2016;
SB 206-110414, Revision B, dated January 10, 2017; or SB 407-110414,
Revision C, dated January 10, 2017, is considered acceptable for
compliance with the corresponding required actions specified in
paragraph (e)(1) of this AD.
Exact source excerpt. Text positions 15193–15728, end exclusive, in the original decoded publication. SHA-256: 4ef689c49590d1dbb9b69cf4f0667575215352620480f6b1881429d239a0d235
Alternative Methods of Compliance (AMOCs)
(g) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Denver ACO Branch, FAA, may approve AMOCs for
this AD. Send your proposal to: Matthew Bryant, Aerospace Engineer,
Denver ACO Branch, Compliance & Airworthiness Division, FAA, 26805
East 68th Ave., Room 214, Denver, CO 80249; telephone (303) 342-
1092; email [email protected] and [email protected].
(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.
Exact source excerpt. Text positions 15728–16473, end exclusive, in the original decoded publication. SHA-256: 769f803f51a9339979c0f97c576531608632d125a48ad4ad99d3a9b8d31556ff
Additional Information
(h) Additional Information
Air Comm SB 206-110414, Revision A, dated June 3, 2016; SB
AS350-111014 or SB EC130-6204, both Revision A and both dated July
6, 2016; SB 407-110414, Revision B, dated July 6, 2016; SB 206-
110414, Revision B, dated January 10, 2017; and SB 407-110414,
Revision C, dated January 10, 2017, which are not incorporated by
reference, contain additional information about the subject of this
AD. For service information identified in this AD, contact Air Comm
Corporation, 1575 West 124th Ave., Westminster, CO 80234; telephone
(303) 440-4075; email [email protected]; website
www.aircommcorp.com. You may review a copy of this service
information at the FAA, Office of the Regional Counsel, Southwest
Region, 10101 Hillwood Pkwy, Room 6N-321, Fort Worth, TX 76177.
Exact source excerpt. Text positions 16473–17277, end exclusive, in the original decoded publication. SHA-256: 5d086c05251936b0e450256660cf35834485817275bf7e23267d78cf9417bd0f
Subject
(i) Subject
Joint Aircraft Service Component (JASC) Code: 2197, Air
Conditioning System Wiring.
Exact source excerpt. Text positions 17277–17380, end exclusive, in the original decoded publication. SHA-256: 382a87d88f3f289c67f815fb66de6bb5ec7b3641d9a4672137c2cc60cab79341
Material Incorporated by Reference
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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.
(i) Air Comm Corporation Service Bulletin (SB) SB AS350-111014,
Revision B, dated January 10, 2017.
(ii) Air Comm Corporation SB EC130-6204, Revision B, dated
January 10, 2017.
(iii) Air Comm Corporation SB 206-110414, Revision C, dated
January 13, 2017.
(iv) Air Comm Corporation SB 407-110414, Revision D, dated
January 13, 2017.
(3) For Air Comm service information identified in this AD,
contact Air Comm Corporation, 1575 West 124th Ave., Westminster, CO
80234; telephone (303) 440-4075; email [email protected];
website www.aircommcorp.com.
(4) You may view this service information at FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-
321, Fort Worth, TX 76177. For information on the availability of
this material at the FAA, call (817) 222-5110.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 17380–18861, end exclusive, in the original decoded publication. SHA-256: d2e86e98bb84b89739c8e0be97798f98d0266a5d0bd6550bf3a9c6edbedf7929
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2018-25-17 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: aff66e3ddf85537a957ce2d61c214f9047751a9f4e399c5aa67a82706685d33b. Source manifest: e21bd1dbe67dfaa5c5c43778d3ff065ac2112c83ada2ae1aa82e1322582e32e2.
Official source · 2018-12-17
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 83, Number 241 (Monday, December 17, 2018)]
[Rules and Regulations]
[Pages 64435-64437]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-27134]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-1217; Product Identifier 2016-SW-080-AD; Amendment
39-19528; AD 2018-25-17]
RIN 2120-AA64
Airworthiness Directives; Air Comm Corporation Air Conditioning
Systems
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for Air
Comm Corporation (Air Comm) air conditioning systems installed on
various model helicopters. This AD requires replacing electrical
connectors and prohibits the installation of other parts. This AD was
prompted by reports of overheated connectors. The actions of this AD
are intended to address an unsafe condition on these products.
DATES: This AD is effective January 22, 2019.
The Director of the Federal Register approved the incorporation by
reference of certain documents listed in this AD as of January 22,
2019.
ADDRESSES: For service information identified in this final rule,
contact Air Comm Corporation, 1575 West 124th Ave., Westminster, CO
80234; telephone (303) 440-4075; email [email protected]; website
www.aircommcorp.com. You may review a copy of the referenced service
information at the FAA, Office of the Regional Counsel, Southwest
Region, 10101 Hillwood Pkwy, Room 6N-321, Fort Worth, TX 76177. It is
also available on the internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2017-1217.
Examining the AD Docket
You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1217; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this AD, any incorporated-by-reference service information, the
economic evaluation, the Special Airworthiness Information Bulletin
(SAIB), any comments received, and other information. The street
address for Docket Operations (phone: 800-647-5527) is 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: Matthew Bryant, Aerospace Engineer,
Denver ACO Branch, Compliance & Airworthiness Division, FAA, 26805 East
68th Ave., Room 214, Denver, CO 80249; telephone (303) 342-1092; email
[email protected].
SUPPLEMENTARY INFORMATION:
Discussion
On January 11, 2018, at 83 FR 1313, the Federal Register published
our notice of proposed rulemaking (NPRM), which proposed to amend 14
CFR part 39 by adding an AD that would apply to Airbus Helicopters
Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350C, AS350D,
AS350D1, and EC130B4, and Bell Model 206A, 206B, 206L, 206L-1, 206L-3,
and 206L-4, and 407 helicopters with certain part-numbered Air Comm air
conditioning systems installed. The NPRM proposed to require replacing
certain connectors with Air Comm connectors and to prohibit installing
certain part-numbered plugs, sockets, receptacles, and pin in some aft
evaporator assemblies, aft evaporator blower assemblies, and aft
condenser blowers. The proposed requirements were intended to address
the unsafe condition of an overheated connector, which could result in
a fire and subsequent loss of control of the helicopter.
Ex Parte Contact
On April 17, 2018, after the comment period closed, we had a
teleconference with Air Comm about some of the Air Comm parts
identified in the NPRM. We subsequently continued this discussion by
email. Air Comm's comment during these discussions is addressed below.
A copy of each email contact and a summary of each telephone contact
can be found in the rulemaking docket at http://www.regulations.gov in
Docket No. FAA-2017-1217.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comment we received and the FAA's
response.
Request
Air Comm requested that we review paragraph (e)(2) of the NPRM,
which lists aft evaporator assembly part number (P/N) AS350-6202. Air
Comm stated that this P/N is not part of the type design for the air
conditioning system. According to Air Comm, the
[[Page 64436]]
correct P/N is AS350-6202-1. In support of this request, Air Comm
provided the type design data for our review.
We agree. Although Figure 1 of Air Comm Corporation Service
Bulletin (SB) AS350-111014, Revision B, dated January 10, 2017,
identifies the aft evaporator assembly as P/N AS350-6202, the correct
P/N is AS350-6202-1. We have corrected this error in this Final Rule.
Further, because of Air Comm's comments, we conducted additional
review of the blower and wire harness drawings for the affected
components. As a result, we determined that plug P/N 03-09-1042 and
receptacle P/N 03-09-2042 were listed in error in the NPRM. These two
P/Ns are also not part of the type design for the air conditioning
system. Accordingly, we have removed these P/Ns from paragraph (e)(2)
of this Final Rule.
FAA's Determination
We have reviewed the relevant information and determined that an
unsafe condition exists and is likely to exist or develop on other
products of these same type designs and that air safety and the public
interest require adopting the AD requirements as proposed with the
changes described previously. These changes are consistent with the
intent of the proposals in the NPRM and will not increase the economic
burden on any operator nor increase the scope of the AD.
Related Service Information Under 1 CFR Part 51
Air Comm Corporation has issued SB AS350-111014, Revision B, dated
January 10, 2017, for Airbus Helicopters AS350 series helicopters and
SB EC130-6204, Revision B, dated January 10, 2017, for Airbus
Helicopters EC130 series helicopters. Air Comm Corporation has also
issued SB 206-110414 for Bell 206 series helicopters, Revision C, and
SB 407-110414 for Bell Model 407 helicopters, Revision D, both dated
January 13, 2017. This service information specifies inspecting certain
aft evaporator blower motor and certain condenser blower electrical
connectors for indications of overheating, discoloration, and plastic
deformation and performing a pull test. This service information also
specifies replacing connector housings and contacts that fail the
inspection or the pull test.
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Other Related Service Information
Air Comm Corporation has also issued the following:
<bullet> SB AS350-111014 and SB EC130-6204, both Revision A and
both dated July 6, 2016;
<bullet> SB 206-110414, Revision B, dated January 10, 2017, and
Revision A dated June 3, 2016; and
<bullet> SB 407-110414, Revision C, dated January 10, 2017, and
Revision B, dated July 6, 2016.
This service information contains the same procedures described
above. However, SB AS350-111014 and SB EC130-6204, both Revision B and
dated January 10, 2017, contain additional instructions and figures for
the connectors. SB 206-110414, Revision C, and SB 407-110414, Revision
D, both dated January 13, 2017, contain minor corrections.
Differences Between This AD and the Service Information
The Air Comm service information specifies a compliance time of 20
flight hours. This AD requires compliance within 90 hours time-in-
service. The Air Comm service information specifies inspecting each
connector and replacing the connector housings and contacts that have
any signs of overheating or that fail a pull test. This AD requires
replacing each connector without an inspection. This AD also prohibits
installing certain parts in certain part-numbered aft evaporator
assemblies, aft evaporator blower assemblies, and aft condenser
blowers.
Costs of Compliance
We estimate that this AD affects 914 units installed on helicopters
of U.S. Registry. We estimate that operators may incur the following
costs in order to comply with this AD. Labor costs are estimated at $85
per work-hour.
Replacing the connectors takes about 1 work-hour and parts cost
about $60 for a total estimated cost of $145 per helicopter and
$132,530 for the U.S. fleet.
According to Air Comm's service information, some 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 by Air
Comm. Accordingly, 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 to the extent
that it justifies making a regulatory distinction; 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.
We prepared an economic evaluation of the estimated costs to comply
with this AD and placed it in the AD docket.
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):
[[Page 64437]]
2018-25-17 Air Comm Corporation (Air Comm) Air Conditioning Systems:
Amendment 39-19528; Docket No. FAA-2017-1217; Product Identifier
2016-SW-080-AD.
(a) Applicability
This AD applies to the following helicopters, certificated in
any category:
(1) Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3,
AS350BA, AS350C, AS350D, and AS350D1 helicopters with an Air Comm
air conditioning system part number (P/N) AS350-202-1, AS350-202-2,
AS350-202-3, AS350-202-4, AS350-202-5, AS350-204-1, AS350-204-2,
AS350-204-3, AS350-204-4, AS350-204-5, AS350-204-6, AS350-204-7,
AS350-204-8, AS350-204-9, AS350-204-10, AS350-204-11, or AS350-204-
12 installed.
(2) Airbus Helicopters Model EC130B4 helicopters with an Air
Comm air conditioning system P/N EC130-202-1, EC130-202-2, EC130-
202-3, EC130-202-4, EC130-202-5, EC130-202-6, EC130-202-7, or EC130-
202-8 installed.
(3) Bell Helicopter Textron Canada Limited (Bell) Model 206A,
206B, 206L, 206L-1, 206L-3, and 206L-4 helicopters with an Air Comm
air conditioning system P/N 206EC-200, 206EC-201, 206EC-202, 206EC-
203, 206EC-204, 206EC-205, 206EC-206, 206EC-207, 206EC-208, 206EC-
209, 206EC-210, 206EC-211, or 206EC-212 installed.
(4) Bell Model 407 helicopters with an Air Comm air conditioning
system P/N 407 EC-201, 407 EC-202, or 407 EC-203 installed.
(b) Unsafe Condition
This AD defines the unsafe condition as an overheated connector.
This condition could result in a fire and subsequent loss of control
of the helicopter.
(c) Effective Date
This AD becomes effective January 22, 2019.
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
(e) Required Actions
(1) Within 90 hours time-in-service:
(i) For Airbus Helicopters Model AS350B, AS350B1, AS350B2,
AS350B3, AS350BA, AS350C, AS350D, and AS350D1 helicopters, replace
each aft evaporator blower motor connector with an Air Comm
connector as depicted in Figures 2, 3, and 4 of Air Comm Service
Bulletin (SB) SB AS350-1110014, Revision B, dated January 10, 2017,
by using a Deutsch HDT-48-00 or an equivalent MIL-DTL22520 Type 1
crimping tool.
(ii) For Airbus Helicopters Model EC130B4 helicopters, replace
each aft evaporator blower motor connector with an Air Comm
connector as depicted in Figures 2, 3, and 4 of Air Comm SB EC130-
6204, Revision B, dated January 10, 2017, by using a Deutsch HDT-48-
00 or an equivalent MIL-DTL22520 Type 1 crimping tool.
(iii) For Bell Model 206A, 206B, 206L, 206L-1, 206L-3, and 206L-
4 helicopters, replace each aft evaporator blower motor connector
with an Air Comm connector as depicted in Figures 4, 5, and 6 of Air
Comm SB 206-110414, Revision C, dated January 13, 2017, by using a
Deutsch HDT-48-00 or an equivalent MIL-DTL22520 Type 1 crimping
tool.
(iv) For Bell Model 407 helicopters, replace each aft evaporator
blower motor connector with an Air Comm connector as depicted in
Figures 4, 5, and 6 of Air Comm SB 407-110414, Revision D, dated
January 13, 2017, by using a Deutsch HDT-48-00 or an equivalent MIL-
DTL22520 Type 1 crimping tool.
(2) After the effective date of this AD, do not install the
following in any aft evaporator assembly P/Ns AS350-6202-1, EC130-
6204-1, or EC130-6204-2; aft evaporator blower assembly P/Ns S-
6078EC-15, S-6102EC-3, or S-6102EC-4; or aft condenser blower P/Ns
S-7060EC-1, S-7060EC-2, S-7062EC-1 or S-7062EC-2:
(i) Plug P/N 03-09-1022 and 03-09-1032;
(ii) Socket P/N 02-09-1103 and 02-09-1104;
(iii) Receptacle P/N 03-09-2022 and 03-09-2032; and
(iv) Pin P/N 02-09-2103.
(f) Credit for Previous Actions
Replacing the connectors before the effective date of this AD in
accordance with Air Comm SB 206-110414, Revision A, dated June 3,
2016; SB AS350-111014 or SB EC130-6204, both Revision A and both
dated July 6, 2016; SB 407-110414, Revision B, dated July 6, 2016;
SB 206-110414, Revision B, dated January 10, 2017; or SB 407-110414,
Revision C, dated January 10, 2017, is considered acceptable for
compliance with the corresponding required actions specified in
paragraph (e)(1) of this AD.
(g) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Denver ACO Branch, FAA, may approve AMOCs for
this AD. Send your proposal to: Matthew Bryant, Aerospace Engineer,
Denver ACO Branch, Compliance & Airworthiness Division, FAA, 26805
East 68th Ave., Room 214, Denver, CO 80249; telephone (303) 342-
1092; email [email protected] and [email protected].
(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
Air Comm SB 206-110414, Revision A, dated June 3, 2016; SB
AS350-111014 or SB EC130-6204, both Revision A and both dated July
6, 2016; SB 407-110414, Revision B, dated July 6, 2016; SB 206-
110414, Revision B, dated January 10, 2017; and SB 407-110414,
Revision C, dated January 10, 2017, which are not incorporated by
reference, contain additional information about the subject of this
AD. For service information identified in this AD, contact Air Comm
Corporation, 1575 West 124th Ave., Westminster, CO 80234; telephone
(303) 440-4075; email [email protected]; website
www.aircommcorp.com. You may review a copy of this service
information at the FAA, Office of the Regional Counsel, Southwest
Region, 10101 Hillwood Pkwy, Room 6N-321, Fort Worth, TX 76177.
(i) Subject
Joint Aircraft Service Component (JASC) Code: 2197, Air
Conditioning System Wiring.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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.
(i) Air Comm Corporation Service Bulletin (SB) SB AS350-111014,
Revision B, dated January 10, 2017.
(ii) Air Comm Corporation SB EC130-6204, Revision B, dated
January 10, 2017.
(iii) Air Comm Corporation SB 206-110414, Revision C, dated
January 13, 2017.
(iv) Air Comm Corporation SB 407-110414, Revision D, dated
January 13, 2017.
(3) For Air Comm service information identified in this AD,
contact Air Comm Corporation, 1575 West 124th Ave., Westminster, CO
80234; telephone (303) 440-4075; email [email protected];
website www.aircommcorp.com.
(4) You may view this service information at FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-
321, Fort Worth, TX 76177. For information on the availability of
this material at the FAA, call (817) 222-5110.
(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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Fort Worth, Texas, on December 7, 2018.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2018-27134 Filed 12-14-18; 8:45 am]
BILLING CODE 4910-13-P
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