AD 2018-02-05

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Models PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-181,

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PA-28-236, PA-28-201T, PA-28R-180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, and PA-28RT-201T airplanes. This AD requires inspecting the fuel tank selector cover to verify the left and right fuel tank selector placards are located at the proper positions and replacing those that are improperly located with new placards. This AD was prompted by a quality control issue at the manufacturer that resulted in the installation of the fuel tank selector covers with the left and right fuel tank selector placards improperly located. We are issuing this AD to address the unsafe condition on these products.

Final rule; request for comments.

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):

2018-02-05 Piper Aircraft, Inc.: Amendment 39-19158; Docket No. FAA- 2018-0015; Product Identifier 2017-CE-045-AD.

(a) Effective Date

This AD is effective February 7, 2018.

(b) Affected ADs

None.

(c) Applicability

This AD applies to the following Piper Aircraft, Inc. airplane models and serial numbers (S/Ns) that are certificated in any category:

Table 1 to Paragraph (c) of This AD--Applicable Airplane Models and S/Ns ------------------------------------------------------------------------
ModelSerial No. ------------------------------------------------------------------------ PA-28-140................... 28-20001 through 28-26946; 28-7125001
through 28-7725290. PA-28-150................... 28-03, 28-1 through 28-4377, and 28-1760A. PA-28-151................... 28-741500l through 28-7715314. PA-28-160................... 28-03, 28-1 through 28-4377, and 28-1760A. PA-28-161................... 2841001 through 2841365, 28-7716001
through 28-8216300, 28-8316001 through 28-
8616057, 2816001 through 2816109, 2816110
through 2816119, and 2842001 through
2842420. PA-28-180................... 28-03, 28-671 through 28-5859, 28-7105001
through 28-7205318, 28-E13, and 28-
7305001 through 28-7505261.

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PA-28-181................... 28-769000l through 28-8690056, 28-8690061,
28-8690062, 289000l through 2890205,
2890206 through 2890231, and 2843001
through 2843879. PA-28-236................... 28-7911001 through 28-8611008and 2811001
through 2811050. PA-28-201T.................. 28-7921001 through 28-7921095. PA-28R-180.................. 28R-30002 through 28R-31270 and 28R-
7130001 through 28R-7130019. PA-28R-200.................. 28R-30482, 28R-35001 through 28R-35820,
28R-7135001 through 28R-7135238, and 28R-
7235001 through 28R-7635545. PA-28R-201.................. 28R-7737002 through 28R-7837317, 2837001
through 2837061, and 2844001 through
2844171. PA-28R-201T................. 28R-7703001 through 28R-7803374 and
2803001 through 2803015. PA-28RT-201................. 28R-7918001 through 28R-8218026. PA-28RT-201T................ 28R-7931001 through 28R-8631005, and
2831001 through 2831038. ------------------------------------------------------------------------

(d) Subject

Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 11, Placard and Markings.

(e) Unsafe Condition

This AD was prompted by a quality control issue at the manufacturer that resulted in the installation of fuel tank selector covers with the left and right fuel tank selector placards improperly located. We are issuing this AD to prevent fuel management error. The unsafe condition, if not addressed, could result in fuel starvation and loss of engine power in flight.

(f) Compliance

Comply with this AD within the compliance times specified, unless already done.

(g) Inspect Fuel Selector Cover

Before further flight after February 7, 2018 (the effective date of this AD), inspect the left and right fuel selector cover placards for proper installation using Part I of Piper Aircraft, Inc. (Piper) Service Bulletin (SB) No. 1309, dated October 10, 2017. If the fuel selectors placards are properly installed, no further action is required.

(h) Install Temporary Fuel Selector Placards

If improper (reversed clock positions) installation of the left and right fuel selector placards is found during the inspectionrequired in paragraph (g) of this AD, before further flight, fabricate and install temporary left and right fuel selector placards using Part II of Piper SB No. 1309, dated October 10, 2017. In lieu of installing the temporary placards required by this paragraph, you may install the permanent placards specified in paragraph (i) of this AD.

(i) Install Permanent Fuel Selector Placards

Within the next 100 hours time-in-service (TIS) after February 7, 2018 (the effective date of this AD), replace the temporary placard installed in paragraph (h) of this AD with permanent left and right fuel selector placards using Part III of Piper SB No. 1309, dated October 10, 2017, unless already done in lieu of installing the temporary placards specified in paragraph (h) of this AD.

(j) Special Flight Permit

A special flight permit is allowed for this AD per 14 CFR 39.23 with the following limitations: Flights are not to exceed a total of 100 hours TIS with temporary placards installed.

(k) Alternative Methods of Compliance (AMOCs)

(1) The Manager, Atlanta ACO Branch, 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 certification office, send it to the attention of the person identified in Related Information, paragraph (l), 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.

(l) Related Information

For more information about this AD, contact Ronald Segall, Aerospace Engineer, Atlanta ACO Branch, FAA, 1701 Columbia Avenue, College Park, Georgia 30337; phone: (404) 474-5541; fax: (404) 474- 5506; email: ronald.segall@faa.gov.

(m) 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) Piper Aircraft, Inc. Service Bulletin No. 1309, dated October 10, 2017.
(ii) Reserved.
(3) For Piper Aircraft, Inc. service information identified in this AD, contact Piper Aircraft, Inc., 2926 Piper Drive, Vero Beach, FL 32960; telephone: (772) 567-4361; internet: www.piper.com/technical-publications-documents/.
(4) You may view this service information at FAA, Policy and Innovation Division, 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Discussion

We received a report from Piper Aircraft, Inc., that they had a quality control issue that resulted in the installation of fuel tank selector covers with the placement of the left and right fuel tank selector placards installed in reverse on certain Piper Aircraft, Inc. Models PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28- 180, PA-28-181, PA-28-236, PA-28-201T, PA-28R-180, PA-28R-200, PA-28R- 201, PA-28R-201T, PA-28RT-201, and PA-28RT-201T airplanes. This condition, if not addressed, could result in fuel management errors resulting in fuel starvation and loss of engine power in flight. We are issuing this AD to address the unsafe condition on these products.

Related Service Information Under 1 CFR Part 51

We reviewed Piper Aircraft, Inc. Service Bulletin No. 1309, dated October 10, 2017. The service bulletin describes procedures for inspecting the fuel tank selector cover to verify the left and right fuel tank selector placards are located at the 12:00 and 3:00 clock positions, respectively, and replacing those that are improperly located with new placards. 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.

FAA's Determination

We are issuing 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.

AD Requirements

This AD requires accomplishing the actions specified in the service information described previously.

FAA's Justification and Determination of the Effective Date

An unsafe condition exists that requires the immediate adoption of this AD without providing an opportunity for public comments prior to adoption. The FAA has found that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule because improper fuel selection could result in fuel starvation and loss of engine power in flight. Therefore, we find good cause that notice and opportunity for prior public comment are impracticable. In addition, for the reason stated above, we find that good cause exists for making this amendment effective in less than 30 days.

Comments Invited

This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment. However, we invite you to send any written data, views, or arguments about this final rule. Send your comments to an address listed under the ADDRESSES section. Include the docket number FAA-2018- 0015 and Product Identifier 2017-CE-045-AD at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this final rule. We will consider all comments received by the closingdate and may amend this final rule 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 final rule.

Costs of Compliance

We estimate that this AD affects 17,957 airplanes, of U.S. registry.
We estimate the following costs to comply with this AD:

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Estimated Costs ----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Inspect the left and right fuel .5 work-hour x $85 Not applicable............. $42.50 $763,172.50
tank selector placards for per hour = $42.50.
proper installation. ----------------------------------------------------------------------------------------------------------------

We estimate the following costs to do any necessary replacements that would be required based on the results of the inspection. We have no way of determining the number of aircraft that might need this replacements:

On-Condition Costs ----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Install new fuel selector placards on the fuel .5 work-hour x $85 per hour = $9.26 $51.76
selector cover. $42.50. ----------------------------------------------------------------------------------------------------------------

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.
This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to small airplanes, gliders, and domestic business jet transport airplanes and associated appliances to the Director of the Policy and Innovation Division.

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.