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2017-04-06 UNITED INSTRUMENTS, INC.:
Amendment 39-18801; Docket No. FAA-2016-9345; Directorate Identifier 2016-CE-028-AD.

(a) EFFECTIVE DATE

    This AD is effective April 7, 2017.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD  applies  to  United Instruments, Inc. 5934  series altimeters
    that were manufactured between January 2015 and  February 2016 and in-
    stalled in airplanes and helicopters.

(1) The specific affected serial number altimeters can be found  in United
    Instruments, Inc. Service Bulletin No. 13, dated March 25, 2016. Para-
    graph (j)(3) of this AD contains addresses  for obtaining  the service
    bulletin.

(2) Altimeters  that  have  been  corrected  by  United Instruments,  Inc.
    following  Service Bulletin  No. 13,  dated  March 25, 2016,  are  not
    affected by this AD and no further action is necessary.

(3) Altimeters that have been corrected by United Instruments, Inc. can be
    identified by a yellow dot, approximately 1/4 inch (6 mm) in diameter,
    located  approximately 1 inch (25 mm)  to  the  left side of the name-
    plate.  The corrected altimeters will also have a letter "M," approxi-
    mately 1/8 inch (3mm) high,  metal stamped on the nameplate  after the
    name "ALTIMETER."

(d) SUBJECT

    Joint Aircraft System Component (JASC)/Air Transport Association (ATA)
    of America Code 44, Cabin Systems.

(e) UNSAFE CONDITION

    This  AD  was prompted  by  reports of  certain  altimeters displaying
    higher  than actual  altitude due  to a  slow diaphragm  leak. We  are
    issuing this AD to prevent display of misleading altitude data,  which
    could result in inadvertent flight into terrain.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REPLACEMENT

    Within the next 12 months after  April 7, 2017 (the effective date  of
    this  AD),  replace any  affected  altimeter with  a  serviceable part
    following  United Instruments,  Inc.  Service  Bulletin No. 13,  dated
    March 25, 2016.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, Wichita Aircraft Certification Office (ACO), FAA, has the
    authority  to  approve  AMOCs  for this  AD,  if  requested  using the
    procedures found  in 14  CFR 39.19.  In accordance  with 14 CFR 39.19,
    send  your  request  to  your  principal  inspector  or  local  Flight
    Standards  District  Office, as  appropriate.  If sending  information
    directly to the manager  of the ACO, send  it to the attention  of the
    person identified in paragraph (i) of this AD.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking  a principal inspector,  the manager of  the local
    flight standards district office/certificate holding district office.

(i) RELATED INFORMATION

    For more information about this AD,  contact Les Lyne, Aerospace Engi-
    neer,  FAA,  Wichita ACO, 1801 Airport Road, Room 100, Wichita, Kansas
    67209; telephone: (316) 946-4190; fax: (316) 946-4107;  email: leslie.
    lyne@faa.gov.

(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 this AD specifies otherwise.

(i) United Instruments, Inc. Service Bulletin No. 13 dated March 25, 2016.

(ii) Reserved.

(3) For United Instruments, Inc. service information identified in this AD
    contact  United Instruments, Inc.,  3625 Comotara Avenue,  Wichita, KS
    67226; telephone (316) 636-9203;  fax: (316) 636-9243; email: customer
    service@unitedinst.com;  Internet: www.unitedinst.com  or  http://www.
    unitedinst.com/Products/SpecificationsSheets/d132811.aspx.

(4) You  may  view  this  service  information  at  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.
    It is also available on the internet at http://www.regulations.gov  by
    searching for and locating Docket No. FAA-2016-9345.

(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 Kansas City, Missouri,  on  February 6, 2017. Kelly A. Broadway,
Acting  Manager,  Small   Airplane  Directorate,  Aircraft   Certification
Service.

FOR FURTHER INFORMATION CONTACT: Les Lyne, Aerospace Engineer, FAA Wichita
Aircraft Certification Office, 1801 Airport Road, Rm. 100, Wichita, Kansas
67209; telephone: (316) 946-4190; fax: (316) 946-4107; email: leslie.lyne@
faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39


[Docket No. FAA-2016-9345; Directorate Identifier 2016-CE-028-AD;
Amendment 39-18801; AD 2017-04-06]
RIN 2120-AA64

Airworthiness Directives; United Instruments, Inc. Series
Altimeters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
United Instruments, Inc. 5934 series altimeters that were manufactured
between January 2015 and February 2016 and installed in airplanes and
helicopters. This AD was prompted by reports of certain altimeters
displaying higher than actual altitude due to a slow diaphragm leak,
which would affect the accuracy of the altimeters. This AD requires
replacing the affected altimeters. We are issuing this AD to correct
the unsafe condition on these products.

DATES: This AD is effective April 7, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 7,
2017.

ADDRESSES: For service information identified in this final rule,
contact United Instruments, Inc., 3625 Comotara Avenue, Wichita, KS
67226; telephone (316) 636-9203; fax: (316) 636-9243; email:
customerservice@unitedinst.com; Internet: www.unitedinst.com or http://www.unitedinst.com/Products/SpecificationsSheets/d132811.aspx. 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.
It is also available on the internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2016-9345.

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-2016-
9345; 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: Les Lyne, Aerospace Engineer, FAA,
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100,
Wichita, Kansas 67209; telephone: (316) 946-4190; fax: (316) 946-4107;
email: leslie.lyne@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain United Instruments,
Inc. 5934 series altimeters that were manufactured between January 2015
and February 2016 and installed in airplanes and helicopters. The NPRM
published in the Federal Register on November 7, 2016 (81 FR 78083).
The NPRM was prompted by a report that certain 5934 series altimeters
that were manufactured between January 2015 and February 2016 may
display higher than actual altitude. These altimeters are susceptible
to developing a slow diaphragm leak, which would affect the accuracy of
the altimeters. It has been determined that insufficient removal of
chemical substance on the diaphragm assembly during the production
process of the altimeter caused the misleading display of altitude
data. The NPRM proposed to require replacing the affected altimeters.
We are issuing this AD to prevent display of misleading altitude data,
which could result in inadvertent flight into terrain.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM 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 this 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
NPRM for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

We reviewed United Instruments, Inc. Service Bulletin No. 13, dated
March 25, 2016. The service bulletin describes procedures for replacing
the nonconforming altimeters. 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.

Costs of Compliance

We estimate that this AD affects 1,351 altimeters as installed in
airplanes and helicopters of U.S. registry.
We estimate the following costs to comply with this AD:

Estimated Costs

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Replace altimeter 1 work-hour x $85 per hour = $85 $1,600 $1,685 $2,276,435

According to the manufacturer, 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 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

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]


2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):