Airworthiness Directives:

Federal Register Volume 76, Number 189 (Thursday, September 29, 2011)

Proposed Rules

Pages 60396-60398

From the Federal Register Online via the Government Printing Office [www.gpo.gov]

FR Doc No: 2011-25006

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 14 CFR Part 39

Docket No. FAA-2011-1040; Directorate Identifier 2011-CE-029-AD

RIN 2120-AA64

Airworthiness Directives; Piaggio Aero Industries S.p.A.

Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of

Transportation (DOT).

ACTION: Notice of proposed rulemaking (NPRM).

SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain Piaggio Aero Industries S.p.A. Model P-180 airplanes. This proposed AD results from mandatory continuing airworthiness information

(MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The

MCAI describes the unsafe condition as:

One event of in-flight baggage door opening occurred on an in- service aeroplane due to a defective locking mechanism or installation thereof; the BAG DOOR warning light went on properly before the event, but was ignored by the pilot, who misinterpreted it as a false warning.

NOTE: False in-service BAG DOOR warnings had occurred on other

P.180 aeroplanes, and Piaggio Aero Industries (PAI) had issued

Service Bulletin (SB) No. 80-0223 revision 1 to improve the installation of the baggage door warning microswitch and to modify the locking mechanism if necessary.

This condition, if not detected and corrected, could lead to in- flight detachment of the door, which could hit and damage the left propeller and/or the vertical or horizontal stabilizer, possibly resulting in loss of control of the aeroplane, or in injuries to persons or damage to property on the ground.

Instances of the baggage door open light illuminating have occurred when the baggage door was not open. This condition, if not corrected, could result in the pilot disregarding a valid warning. The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

DATES: We must receive comments on this proposed AD by November 14, 2011.

ADDRESSES: You may send comments 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: U.S. Department of Transportation, Docket

Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New

Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m.,

Monday through Friday, except Federal holidays.

For service information identified in this proposed AD, contact

Piaggio Aero Industries S.p.A.-Airworthiness Office, Via Luigi

Cibrario, 4-16154 Genova-Italy; phone: +39 010 6481353; fax: +39 010 6481881; e-mail: airworthiness@piaggioaero.it; Internet: http://www.piaggioaero.com/#/en/after-sales/service-support. 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.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov; 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 (telephone (800) 647-5527) is in the

ADDRESSES section. Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Mike Kiesov, Aerospace Engineer, FAA,

Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; e-mail: mike.kiesov@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2011-1040;

Directorate Identifier 2011-CE-029-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://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

The European Aviation Safety Agency (EASA), which is the Technical

Agent for the Member States of the European Community, has issued EASA

AD No.: 2011-0132, dated July 12, 2011 (referred to after this as ``the

MCAI''), to correct an unsafe condition for the specified products. The

MCAI states:

One event of in-flight baggage door opening occurred on an in- service aeroplane due to a defective locking mechanism or installation thereof; the BAG DOOR warning light went on properly before the event, but was ignored by the pilot, who misinterpreted it as a false warning.

NOTE: false in-service BAG DOOR warnings had occurred on other

P.180 aeroplanes, and Piaggio Aero Industries (PAI) had issued

Service Bulletin (SB) No. 80-0223 revision 1 to improve the installation of the baggage door warning microswitch and to modify the locking mechanism if necessary.

This condition, if not detected and corrected, could lead to in- flight detachment of the door, which could hit and damage the left propeller and/or the vertical or horizontal stabilizer, possibly resulting in loss of control of the aeroplane, or in injuries to persons or damage to property on the ground.

This AD requires an inspection of the locking mechanism of the baggage door and its proper adjustment, in accordance with PAI SB

No. 80-0289 revision 1; if baggage door lockpins do not reach the correct engagement, or false BAG DOOR warnings were reported by flight crew, this AD requires also a modification of the door mechanism in accordance with PAI SB No. 80-0223 revision 1.

Instances of the baggage door open light illuminating have occurred when the baggage door was not open. This condition, if not corrected, could result in the pilot disregarding a valid warning. You may obtain further information by examining the MCAI in the AD docket.

Relevant Service Information

Piaggio Aero Industries S.p.A. has issued Service Bulletin No. 80- 0223,

Page 60397

Revision 1, dated July 31, 2009; and Mandatory Service Bulletin No. 80- 0289, Revision 1, dated January 11, 2011. The actions described in this service information are intended to correct the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of the Proposed AD

This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with this State of Design Authority, they have notified us of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all information and determined the unsafe condition exists and is likely to exist or develop on other products of the same type design.

Differences Between This Proposed AD and the MCAI or Service

Information

We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the

AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information.

We might also have proposed different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a NOTE within the proposed AD.

Costs of Compliance

We estimate that this proposed AD will affect 102 products of U.S. registry. We also estimate that it would take about 29 work-hours per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Required parts would cost about $4,482 per product.

Based on these figures, we estimate the cost of the proposed AD on

U.S. operators to be $708,594, or $6,947 per product.

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); and 3. 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 a regulatory evaluation of the estimated costs to comply with this proposed 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.

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 AD:

Piaggio Aero Industries S.p.A.: Docket No. FAA-2011-1040;

Directorate Identifier 2011-CE-029-AD.

Comments Due Date

(a) We must receive comments by November 14, 2011.

Affected ADs

(b) None.

Applicability

(c) This AD applies to Piaggio Aero Industries S.p.A. P-180

Airplane Model P-180 airplanes, serial numbers affected 1002 and 1004 through 1189, certificated in any category.

Subject

(d) Air Transport Association of America (ATA) Code 52: Doors.

Reason

(e) The mandatory continuing airworthiness information (MCAI) states:

One event of in-flight baggage door opening occurred on an in- service aeroplane due to a defective locking mechanism or installation thereof; the BAG DOOR warning light went on properly before the event, but was ignored by the pilot, who misinterpreted it as a false warning.

NOTE: false in-service BAG DOOR warnings had occurred on other

P.180 aeroplanes, and Piaggio Aero Industries (PAI) had issued

Service Bulletin (SB) No. 80-0223 revision 1 to improve the installation of the baggage door warning microswitch and to modify the locking mechanism if necessary.

This condition, if not detected and corrected, could lead to in- flight detachment of the door, which could hit and damage the left propeller and/or the vertical or horizontal stabilizer, possibly resulting in loss of control of the aeroplane, or in injuries to persons or damage to property on the ground.

This AD requires an inspection of the locking mechanism of the baggage door and its proper adjustment, in accordance with PAI SB

No. 80-0289 revision 1; if baggage door lockpins do not reach the correct engagement, or false BAG DOOR warnings were reported by flight crew, this AD requires also a modification of the door mechanism in accordance with PAI SB No. 80-0223 revision 1.

Instances of the baggage door open light illuminating have occurred when the baggage door was not open. This condition, if not corrected, could result in the pilot disregarding a valid warning.

Actions and Compliance

(f) Unless already done, do the following actions:

(1) If false in-flight BAG DOOR indications have occurred, within 165 hours time-in-service (TIS) after the effective date of this AD or within the next 60 days after the effective date of this

AD, whichever occurs first, do the following actions:

(i) Modify the locking mechanism following the Accomplishment

Instructions in Piaggio Aero Industries S.p.A. Service Bulletin No. 80-0223, Revision 1, dated July 31, 2009.

(ii) Inspect the screws on the locking device installed on the door handle for proper tightness and correct as necessary after applying a thread locker following Part

Page 60398

D of the Accomplishment Instructions in Piaggio Aero Industries

S.p.A. Mandatory Service Bulletin No. 80-0289, Revision 1, dated

January 11, 2011.

(2) If false in-flight BAG DOOR indications have not occurred, within 165 hours TIS after the effective date of this AD or within the next 60 days after the effective date of this AD, whichever occurs first, do the following actions:

(i) Inspect the baggage door and the baggage door locking mechanism and do the necessary corrective actions following Parts A and B of the Accomplishment Instructions in Piaggio Aero Industries

S.p.A. Mandatory Service Bulletin No. 80-0289, Revision 1, dated

January 11, 2011.

(ii) If after the inspection required by paragraph (f)(2)(i) of this AD, the baggage door adjustment procedure was not required or was required and was done successfully, inspect the screws on the locking device on the door handle with the proper tightness. Take any necessary corrective actions after applying a thread locker following Part D of the Accomplishment Instructions in Piaggio Aero

Industries S.p.A. Mandatory Service Bulletin No. 80-0289, Revision 1, dated January 11, 2011.

(iii) If after the inspection required by paragraph (f)(2)(i) of this AD, the baggage door adjustment was required and was not done successfully, within the next 165 hours TIS after the effective date of this AD or within the next 60 days after the effective date of this AD, whichever occurs first, do the following actions:

(A) Modify the locking mechanism following the Accomplishment

Instructions in Piaggio Aero Industries S.p.A. Service Bulletin No. 80-0223, Revision 1, dated July 31, 2009.

(B) Inspect the screws on the locking device installed on the door handle for proper tightness and correct as necessary after applying a thread locker following Part D of the Accomplishment

Instructions in Piaggio Aero Industries S.p.A. Mandatory Service

Bulletin No. 80-0289, Revision 1, dated January 11, 2011.

(3) If the inspections specified in Piaggio Aero Industries

S.p.A. Mandatory Service Bulletin No. 80-0289, dated November 11, 2010, and the modification, if required, specified in Piaggio Aero

Industries S.p.A. Service Bulletin No. 80-0223, Revision 1, dated

July 31, 2009, were done before the effective date of this AD, we will allow ``unless already done'' credit to comply with the actions required in this AD. After the effective date of this AD, you must use Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80-0289, Revision 1, dated January 11, 2011, to comply with this AD.

FAA AD Differences

Note: This AD differs from the MCAI and/or service information as follows: No differences.

Other FAA AD Provisions

(g) The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager,

Standards Office, FAA, has the authority to approve AMOCs for this

AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Mike Kiesov, Aerospace Engineer, FAA, Small

Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4144; fax: (816) 329-4090; e-mail: mike.kiesov@faa.gov. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered

FAA-approved if they are approved by the State of Design Authority

(or their delegated agent). You are required to assure the product is airworthy before it is returned to service.

(3) Reporting Requirements: For any reporting requirement in this AD, a Federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control

Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn:

Information Collection Clearance Officer, AES-200.

Related Information

(h) Refer to MCAI European Aviation Safety Agency (EASA) AD No.: 2011-0132, dated July 12, 2011; Piaggio Aero Industries S.p.A.

Service Bulletin No. 80-0223, Revision 1, dated July 31, 2009;

Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80- 0289, dated November 11, 2010; and Piaggio Aero Industries S.p.A.

Mandatory Service Bulletin No. 80-0289, Revision 1, dated January 11, 2011, for related information. For service information related to this AD, contact Piaggio Aero Industries S.p.A-Airworthiness

Office, Via Luigi Cibrario, 4-16154 Genova-Italy; phone: +39 010 6481353; fax: +39 010 6481881; e-mail: airworthiness@piaggioaero.it;

Internet: http://www.piaggioaero.com/#/en/after-sales/service-support. 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.

Issued in Kansas City, Missouri on September 20, 2011.

Wes Ryan,

Acting Manager, Small Airplane Directorate, Aircraft Certification

Service.

FR Doc. 2011-25006 Filed 9-28-11; 8:45 am

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