AD 2003-04-08

This amendment adopts a new airworthiness directive (AD) that applies to certain Piaggio Aero Industries S.p.A. (Piaggio) Model P-180 airplanes. This AD requires you to install a placard on the inside of the lavatory door that prohibits occupying the lavatory seat during takeoff and landing. This AD also requires you to incorporate a temporary revision into the Limitations Section of the pilot operating handbook/airplane flight manual (POH/AFM). This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent passengers from occupying the lavatory seat during takeoff and landing. The lavatory/cabin partition could fail and lead to passenger injury in an emergency situation.

Final rule.

2003-04-08 Piaggio Aero Industries S.p.A.: Amendment 39-13056; Docket No. 2002-CE-47-AD.

(a) What airplanes are affected by this AD? This AD affects Model P-180 airplanes, serial numbers 1002, 1004, 1006 through 1037, 1039, 1040, 1042, 1043, and 1045, that are:

(1) Equipped with a toilet seat; and

(2) Are certificated in any category.

(b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD.

(c) What problem does this AD address? The actions specified by this AD are intended to prevent passengers from occupying the lavatory seat during takeoff and landing. The lavatory/cabin partition could fail and lead to passenger injury in an emergency situation.

(d) What actions must I accomplish to address this problem? To address this problem, you must accomplish the following:

Actions
Compliance
Procedures

(1) Fabricate a placard that incorporates the following words (using at least 1/4-inch black letters on a
white background) and install this placard on the inside of the lavatory door in front of the lavatory seat: LAVATORY SEAT CANNOT BE OCCUPIED DURING TAKEOFF AND LANDING .
Within the next 30 days after April 11, 2003 (the effective date of this AD), unless already accomplished.
The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may fabricate and install the placard. Make an entry into the aircraft records showing compliance with these portions of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).

(2) Incorporate into the Limitations Section of the pilot operating handbook/airplane flight manual (POH/
AFM), page 4 of Piaggio Alert Service Bulletin No. ASB-80-0164, Original Issue: September 10, 2001.
Within the next 30 days after April 11, 2003 (the effective date of this AD), unless already accomplished.
The owner/operator holding at least a private pilot certificate as authorized by 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may accom-
plish the POH/AFM manual insertion of this AD. Make an entry into the aircraft records showing compliance with these portions of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).

(3) As an alternative method of compliance to this AD, you may modify the lavatory/cabin partition.
At any time as terminating action
for the placard and POH/AFM
requirements of this AD.
In accordance with Piaggio Service Bulletin (Recommended) No. SB-80-0165, Original Issue:
September 10, 2001.

Note 1: Information about fabricating and installing the placard and the POH/AFM manual insertion is referenced in Piaggio Alert Service Bulletin No. ASB-80-0164, Original Issued: September 10, 2001.

(e) CanI comply with this AD in any other way? You may use an alternative method of compliance or adjust the compliance time if:

(1) Your alternative method of compliance provides an equivalent level of safety; and

(2) The Manager, Standards Office, Small Airplane Directorate, approves your alternative. Submit your request through an FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Manager, Standards Office.

Note 2: This AD applies to each airplane identified in paragraph (a) of this AD, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/ operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if you have not eliminated the unsafe condition, specific actions you propose to address it.

(f) Where can I get information about any already-approved alternative methods of compliance? Contact Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329-4059; facsimile: (816) 329-4090.

(g) What if I need to fly the airplane to another location to comply with this AD? The FAA can issue a special flight permit under 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate your airplane to a location where you can accomplish the requirements of this AD.

(h) Are any service bulletins incorporated into this AD by reference? The POH/AM requirements of this AD must be done in accordance with Piaggio Alert Service Bulletin No. ASB-80-0164, Original Issue: September 10, 2001. The procedures for accomplishing the optional modification of this AD are contained in Piaggio Service Bulletin (Recommended) No. SB-80-0165, Original Issue: September 10, 2001. The Director of the Federal Register approved this incorporation by reference under 5 U.S.C. 552(a) and 1 CFR part 51. You may get copies from Piaggio Aero Industries S.p.A, Via Cibrario 4, 16154 Genoa, Italy; telephone: +39 010 6481 856; facsimile: +39 010 6481. You may view copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW., Suite 700, Washington, DC.

Note 3: The subject of this AD is addressed in Italian AD Number 2001-513, dated November 30, 2001.

(i) When does this amendment become effective ? This amendment becomes effective on April 11, 2003.

Discussion

What events have caused this AD? The Ente Nazionale per l' Aviazione Civile (ENAC), which is the airworthiness authority for Italy, recently notified FAA of a manufacturing/installation defect on the lavatory/cabin partitions on certain Piaggio Model P-180 airplanes. The lavatory/cabin partitions were installed improperly and are not of sufficient strength. This condition was found during a quality control inspection.

What is the potential impact if FAA took no action? Occupying the lavatory seat during takeoff or landing could result in failure of the lavatory/cabin partition. Such failure could result in passenger injury in an emergency situation.

Has FAA taken any action to this point? We issued a proposal to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) to include an AD that would apply to certain Piaggio Model P-180 airplanes. This proposal was published in the Federal Register as a notice of proposed rulemaking (NPRM) on November 21, 2002 (67 FR 70187). The NPRM proposed to require you to install a placard on the inside of the lavatory door that prohibits occupying the lavatory seat during takeoff and landing; and incorporate a temporary revision into the Limitations Section of the pilot operating handbook/airplane flight manual (POH/AFM).

Was the public invited to comment? The FAA encouraged interested persons to participate in the making of this amendment. We did not receive any comments on the proposed rule or on our determination of the cost to the public.

FAA's Determination

What is FAA's final determination on this issue? After careful review of all available information related to the subject presented above, we have determined that air safety and the public interest require the adoption of the rule as proposed except for minor editorial corrections. We have determined that these minor corrections:

Provide 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.

Cost Impact

How many airplanes does this AD impact? We estimate that this AD affects 12 airplanes in the U.S. registry.

What is the cost impact of this AD on owners/operators of the affected airplanes? We estimate the following costs to accomplish the placard installation:

Labor cost
Parts cost
Total cost per airplane
Total cost on U.S. operators
1 workhour x $60 = $60
$20
$80
12 x $80 = $960

Compliance Time of This AD

What is the compliance time of this AD? The compliance time of this AD is ``within the next 30 days after the effective date of this AD, unless already accomplished.''

Why is the compliance time presented in calendar time instead of hours time-in-service (TIS)? The compliance of this AD is presented in calendar time instead of hours TIS because the lavatory/cabin partitions are unsafe as a result of an improper installation. The unsafe condition has the same chance of occurring on an airplane with 50 hours TIS as it does for an airplane with 1,000 hours TIS. Therefore, we believe that a compliance time of 30 days will:

Ensure that the unsafe condition does not go undetected for a long period of time on the affected airplanes; and

Not inadvertently ground any of the affected airplanes.

Regulatory Impact

Does this AD impact various entities? The regulations adopted herein 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. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132.

Does this AD involve a significant rule or regulatory action? For the reasons discussed above, I certify that this action (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); 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. A copy of the final evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting the Rules Docket at the location provided under the caption ADDRESSES.

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 Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (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.

39.13 [Amended]

2. FAA amends 39.13 by adding a new AD to read as follows: