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PROPOSED AD AEROSPACE WELDING MINNEAPOLIS, INC.: Docket No. FAA-2017-0324; Directorate Identifier 2017-CE-004-AD.
(a) COMMENTS DUE DATE

    We must receive comments by June 2, 2017.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Aerospace Welding Minneapolis, Inc. (AWI)  mufflers
    listed in figure 1 of paragraph  (c) of this AD that are  installed on
    but limited to the  airplanes listed in figure  2 of paragraph (c)  of
    this AD.

Note 1 to  paragraph (c) of  this AD:  You  may use AWI  Mandatory Service
Bulletin No. 16063001,  dated  June 30, 2015,  to  identify if an affected
muffler is installed on the airplane.

           FIGURE 1 OF PARAGRAPH (C) OF THIS AD - AFFECTED MUFFLERS       
    ______________________________________________________________________
    MUFFLER PART NO.                         MUFFLER SERIAL NO.
    ______________________________________________________________________
    A1754001-23                  33553 through 33557; 34721 through 34728;
                                 35322 through 35329; 35670; 38481 through
                                 38485; 38584 through 38586; and 38723
                                 through 38727.

    A1754001-25                  32795 through 32800; 33558 through 33569;
                                 33779 through 33790; 34636 through 34653;
                                 34968 through 34984; 35159 through 35176;
                                 37903 through 37906; 38174 through 38193;
                                 38502 through 38506; 38566 through 38575;
                                 and 38817 through 38836.
    ______________________________________________________________________


           FIGURE 2 OF PARAGRAPH (C) OF THIS AD - AFFECTED AIRPLANES      
    ______________________________________________________________________
                                 TEXTRON AVIATION INC. (TYPE CERTIFICATE
    MUFFLER PART NO.               PREVIOUSLY HELD BY CESSNA AIRCRAFT
                                           COMPANY) AIRPLANES
    ______________________________________________________________________
    A1754001-23                 Model 172 Serial numbers (S/Ns) 17259224
                                and up; Model 172R S/Ns 80001 and up; and
                                Model 172S S/Ns 8001 and up.

    A1754001-25                 Model 172 S/Ns 17256513 and up; Model 172R
                                S/Ns 80001 and up; 172S S/N 8001 and up;
                                and Model 177 S/N 1770001 and up.
    ______________________________________________________________________

(d) SUBJECT

    Joint Aircraft System Component (JASC)/Air Transport Association (ATA)
    of America Code 7820, Exhaust Noise Suppressor.

(e) UNSAFE CONDITION

    This AD was prompted by occurrences  of cracks or broken welds in  the
    connecting weld  of the  muffler body  to muffler  cuff that may allow
    carbon monoxide (CO) exhaust fumes into the cockpit heating system. We
    are issuing this AD  to prevent cracks in  the connecting weld of  the
    muffler body  to muffler  cuff that  may allow  CO fumes  to enter the
    cockpit heating  system and  possibly inhibit  the pilot's  ability to
    maintain control of the airplane.

(f) COMPLIANCE

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

(g) INSPECTION OF THE MUFFLER

    Within 5 hours  time-in-service after the  effective date of  this AD,
    inspect  the  affected  muffler following  the instructions  listed in
    paragraphs (g)(1) through (3).

(1) Using  a  vacuum cleaner with the hose attached to the blowing side of
    the vacuum (with the filter installed),  attach the vacuum to the air-
    plane tailpipe and seal securely.

(2) The vacuum will pressurize the system sufficiently for a soap solution
    to be brushed or applied from a spray bottle to the surface of the ex-
    haust system.

(3) Inspect for evidence of breaches (leakage) in the system from cracks.

(4) In lieu of doing this inspection  and at the same within 5 hours after
    the effective date of this AD compliance time,  you  may  replace  the
    affected muffler  with  an FAA-approved part that  is  not  a  muffler
    listed in figure 1 of paragraph (c) of this AD.

(i) This  replacement  must  be  done  following AWI Cessna 172 (Lycoming)
    Muffler Removal and Installation, Revision 01, January 17, 2017.

(ii) If replacement is done instead of the inspection,  then paragraph (h)
     (3) of this AD is the only additional requirement of this AD.

(h) REPLACEMENT OF THE MUFFLER

(1) If evidence of breaches (leakage) is found  during  the inspection re-
    quired in paragraph (g) of this AD, before further flight, replace the
    affected muffler  with  an  FAA-approved part following AWI Cessna 172
    (Lycoming) Muffler Removal and Installation,  Revision 01, January 17,
    2017.

(2) If no evidence of breaches (leakage) is found  during  the  inspection
    required in paragraph (g)  of this AD, within  the next 100 hours  TIS
    after the effective date of this  AD or at the next annual  inspection
    after the effective date of  this AD, whichever occurs later,  replace
    the affected muffler with an  FAA-approved part that is not  a muffler
    listed in figure 1  of paragraph (c) of  this AD following AWI  Cessna
    172 (Lycoming) Muffler Removal and Installation, Revision 01,  January
    17, 2017.

(3) After the effective date of this AD, do not install on any airplane an
    affected muffler listed in figure 1 of paragraph (c) of this AD.

(i) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

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

(j) RELATED INFORMATION

(1) For  more information  about this AD,  contact  Mark Grace,  Aerospace
    Engineer,  FAA, Chicago Aircraft Certification Office, 2300 East Devon
    Avenue, Des Plaines, IL 60018-4696;  telephone:  (847) 294-7377;  fax:
    (847) 294-7834; email: mark.grace@faa.gov.

(2) For  service information identified  in  this  AD,  contact  Aerospace
    Welding Minneapolis, Inc.  1045 Gemini Road,  Eagan,  Minnesota 55121;
    telephone: 651-379-9888; fax: 651-379-9889; Internet: www.awi-ami.com.
    You may view this referenced service information  at  the  FAA,  Small
    Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For in-
    formation on the availability of this material at the FAA,  call (816)
    329-4148.

Issued in  Kansas City,  Missouri, on  April 11, 2017.  Pat Mullen, Acting
Manager, Small Airplane Directorate, Aircraft Certification Service.

DATES: We must receive comments on this proposed AD by June 2, 2017.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2017-0324; Directorate Identifier 2017-CE-004-AD]
RIN 2120-AA64

Airworthiness Directives; Aerospace Welding Minneapolis, Inc. Mufflers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain Aerospace Welding Minneapolis, Inc. mufflers, part numbers
A1754001-23 and A1754001-25, installed on Textron Aviation Inc. (type
certificate previously held by Cessna Aircraft Company) Models 172,
172R, 172S, and 177 airplanes. This proposed AD was prompted by
occurrences of cracks or broken welds in the connecting weld of the
muffler body to muffler cuff that may allow carbon monoxide exhaust
fumes into the cockpit heating system. This proposed AD would require
an inspection of the muffler for leaking to identify cracks and
replacement of the muffler. We are proposing this AD to correct the
unsafe condition on these products.

DATES: We must receive comments on this proposed AD by June 2, 2017.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:

Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the
instructions for submitting comments.

Fax: 202-493-2251.

Mail: U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.

Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.

For service information identified in this NPRM, contact Aerospace
Welding Minneapolis, Inc. (AWI) 1045 Gemini Road, Eagan, Minnesota
55121; telephone: 651-379-9888; fax: 651-379-9889; Internet: www.awi-
ami.com. 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.

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-2017-0324;
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 proposed AD, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT
: Mark Grace, Aerospace Engineer, FAA,
Chicago Aircraft Certification Office, 2300 East Devon Avenue, Des
Plaines, IL 60018-4696; telephone: (847) 294-7377; fax: (847) 294-7834;
email: mark.grace@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

We invite you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include "Docket No. FAA-2017-0324;
Directorate Identifier 2017-CE-004-AD" at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We will
consider all comments received by the closing date and may amend this
proposed AD because of those comments.

We will post all comments we receive, without change, to http://www.
regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.

Discussion

We were notified of broken or cracked welds in the connecting weld
of the muffler body to muffler cuff on certain Aerospace Welding
Minneapolis, Inc. (AWI) mufflers, part numbers (P/Ns) A1754001-23 and
A1754001-25 that were installed on Textron Aviation Inc. (type
certificate previously held by Cessna Aircraft Company) Models 172,
172R, 172S, and 177 airplanes. There have been 54 occurrences
identified by maintenance and 2 occurrences identified by the carbon
monoxide (CO) gas monitor warning system. This condition, if not
corrected, could lead to CO exhaust fumes entering the cockpit heating
system and result in inhibiting the pilot's ability to maintain control
of the airplane.

Related Service Information Under 1 CFR Part 51

We reviewed AWI Cessna 172 (Lycoming) Muffler Removal and
Installation, Revision 01, January 17, 2017. The service information
describes procedures for removing and replacing the affected mufflers.
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

We reviewed AWI Mandatory Service Bulletin No. 16063001, dated June
30, 2015. The service bulletin describes how to identify the
installation of an affected muffler.

FAA's Determination

We are proposing this AD because we evaluated all the relevant
information and determined the unsafe condition described previously is
likely to exist or develop in other products of the same type design.

Proposed AD Requirements

This proposed AD would require inspecting the muffler for leaking
to identify cracks and replacement of the muffler with an FAA-approved
part.

Differences Between This Proposed AD and the Service Information

The AWI service bulletin requires replacement of the muffler before
further flight. This proposed AD would require an inspection of the
muffler for leaking to identify cracks within 5 hours time-in-service
(TIS) after the effective date of the AD with replacement of leaking
mufflers before further flight. This proposed AD would allow 100 hours
TIS or at the next annual inspection for replacement of non-leaking
mufflers. The service bulletin also requires returning the affected
mufflers back to AWI, and this proposed AD does not require return of
the muffler. The actions of the proposed AD would take precedence over
the service information.

Costs of Compliance

We estimate that this proposed AD affects 171 mufflers installed on
airplanes of U.S. registry.

We estimate the following costs to comply with this proposed AD:

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Inspection of muffler 1 work-hour x $85 per hour = $85
Not applicable
$85
$14,535
Replacement of the muffler 4 work-hours x $85 per hour = $340
$350
690
117,990

The proposed AD would affect 171 mufflers with parts manufacturer
approval; however, only 9 mufflers remain in service.

According to the manufacturer, some of the costs of this proposed
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

We determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 proposed
regulation:

(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.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

The Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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):