Published 2002-04-23 · Federal Register document 02-9389
Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A. Model P-180 Airplanes
Publication summary
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 replace the four defective horizontal stabilizer hinge bushings with replacement bushings. 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 replace defective bushings before they cause failure of the horizontal stabilizer. Such failure could lead to reduced or loss of control of the aircraft.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:07.262592+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2002-c8c2ee537a56d16c
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- results[146]
- Raw source SHA-256
- c8c2ee537a56d16c3d3246bbaa55e183792a136494260623f45827707b4e2a64
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2002-08-04
- Effective date printed in this edition
- Unknown
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Read 7 complete recorded clauses
Applicability wording · What airplanes are affected by this AD?
(a) What airplanes are affected by this AD? This AD affects Model P-180 airplanes, serial numbers 1034, 1035, 1039, and 1045, that are certificated in any category.
Exact source excerpt. Text positions 6951–7122, end exclusive, in the original decoded publication. SHA-256: d3cbc5988c5c5fcaa7025e2839e4cffbb9922fad66068bdc387e8dd4a62fa45e
Who must comply with this AD?
(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.
Exact source excerpt. Text positions 7122–7277, end exclusive, in the original decoded publication. SHA-256: f2b11b7b60b538412202242294037660d7e4e44ceb713e9daf36640867a0121c
What problem does this AD address?
(c) What problem does this AD address? The actions specified by this AD are intended to replace defective bushings before they cause failure of the horizontal stabilizer. Such failure could lead to reduced or loss of control of the aircraft.
Exact source excerpt. Text positions 7277–7526, end exclusive, in the original decoded publication. SHA-256: 2f140aab0dab99e1b33b86c6fe8c380f568baf3993d85568c8c45993a051e120
What actions must I accomplish to address this problem?
(d) What actions must I accomplish to address this problem? To
address this problem, you must accomplish the following:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Replace the horizontal Within the next 150 Follow the
stabilizer hinge bushings hours time-in- ACCOMPLISHMENT
with replacement bushings service (TIS) after INSTRUCTIONS
(part number RDC. 19-09-167- June 10, 2002 (the section of PIAGGIO
1/300) (or FAA-approved effective date of AERO INDUSTRIES
equivalent part number). this AD). S.p.A Service
Bulletin (Mandatory
) No. SB-80-0140,
dated October 15,
2001, and the
applicable service
manual.
------------------------------------------------------------------------
[[Page 19659]]
(2) Send the removed Within 10 days after Send the removed
bushings to PIAGGIO AERO removing the bushings to PIAGGIO
INDUSTRIES S.p.A. so the bushings or within AERO INDUSTRIES
bushings cannot be reused 10 days after June S.p.A, Via Cibrario
and report the return to 10, 2002 (the 4, 16154 Genoa,
FAA. The Office of effective date of Italy, and report
Management and Budget (OMB) this AD), whichever the return to Doug
approved the information occurs later. Rudolph, FAA, at
collection requirements the address in
contained in this paragraph (f) of
regulation under the this AD.
provisions of the Paperwork
Reduction Act of 1980 (44
U.S.C. 3501 et seq.) and
assigned OMB Control Number
2120-0056.
------------------------------------------------------------------------
(e) Can I 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, Standards Office, Small Airplane Directorate.
Note 1: 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.
Exact source excerpt. Text positions 7526–11224, end exclusive, in the original decoded publication. SHA-256: 8b4ca0e4964d1f8ab9b9e2b17e56fdfe058eb081bc912d1133060df33275a379
What if I need to fly the airplane to another location to comply with this AD?
(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 sections 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.
Exact source excerpt. Text positions 11224–11546, end exclusive, in the original decoded publication. SHA-256: 6fa51fb7fc066a4f0a66dc494f9d716f95779f49fd67a3358066bda9eb4e1aec
Are any service bulletins incorporated into this AD by reference?
(h) Are any service bulletins incorporated into this AD by
reference? Actions required by this AD must be done in accordance
with PIAGGIO AERO INDUSTRIES S.p.A Service Bulletin (Mandatory ) No.
SB-80-0140, dated October 15, 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. 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 2: The subject of this AD is addressed in Italian AD Number
2001-512, dated November 30, 2001.
Exact source excerpt. Text positions 11546–12331, end exclusive, in the original decoded publication. SHA-256: 9e3166ee509fae0502c0110f79f1df624a9e66a5a2c94b90813b7bab78467190
When does this amendment become effective?
(i) When does this amendment become effective? This amendment becomes effective on June 10, 2002.
Exact source excerpt. Text positions 12331–12434, end exclusive, in the original decoded publication. SHA-256: 2701bd3ae0ac18fd8f230500774ca1aa36477440f071866d77369446b8ef9056
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2002-08-04 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 31e7146afd677bb45eac5a4242ccf3487731fe690f8cf718faa9b4cc82923dcd. Source manifest: 7d60a1a5533d02796fbc879bcf0a5c26340332bb7e2ce60a8f0dfa6146f05a84.
Official source · 2002-04-23
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 67, Number 78 (Tuesday, April 23, 2002)]
[Rules and Regulations]
[Pages 19657-19659]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-9389]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002-CE-02-AD; Amendment 39-12712; AD 2002-08-04]
RIN 2120-AA64
Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A. Model P-
180 Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: 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 replace the four defective
horizontal stabilizer hinge bushings with replacement bushings. 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 replace defective bushings before they cause
failure of the horizontal stabilizer. Such failure could lead to
reduced or loss of control of the aircraft.
DATES: This AD becomes effective on June 10, 2002.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the regulations as of June
10, 2002.
ADDRESSES: You may get the service information referenced in this AD
from PIAGGIO AERO INDUSTRIES S.p.A, Via Cibrario 4, 16154 Genoa, Italy;
telephone: +39 010 6481 856; facsimile: +39 010 6481 374. You may view
this information at the Federal Aviation Administration (FAA), Central
Region, Office of the Regional Counsel, Attention: Rules Docket No.
2002-CE-02-AD, 901 Locust, Room 506, Kansas City, Missouri 64106; or at
the Office of the Federal Register, 800 North Capitol Street, NW, suite
700, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
[[Page 19658]]
Missouri 64106; telephone: (816) 329-4059; facsimile: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
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 that an unsafe
condition may exist on certain PIAGGIO Model P-180 airplanes. The ENAC
reports that PIAGGIO has discovered four incidents of defective
horizontal stabilizer hinge bushings being installed on 4 PIAGGIO Model
P-180 airplanes. The defect is a missing thermal process during bushing
manufacturing.
What Is the Potential Impact if FAA Took No Action?
Continued operation with defective bushings could result in failure
of the horizontal stabilizer. Such failure could lead to reduced or
loss of control of the aircraft.
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
February 11, 2002 (67 FR 6205). The NPRM proposed to require you to
replace the defective bushings, return the bushings to PIAGGIO, and
report the return to FAA.
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 2 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 replacement:
----------------------------------------------------------------------------------------------------------------
Total cost per
Labor cost Parts cost airplane Total cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
50 workhours x $60 per hour=$3,000 $400 per aircraft.... $3,400 $3,400 x 2=$6,800
----------------------------------------------------------------------------------------------------------------
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.
Sec. 39.13 [Amended]
2. FAA amends Sec. 39.13 by adding a new AD to read as follows:
2002-08-04 PIAGGIO AERO INDUSTRIES S.p.A.: Amendment 39-12712;
Docket No. 2002-CE-02-AD.
(a) What airplanes are affected by this AD? This AD affects
Model P-180 airplanes, serial numbers 1034, 1035, 1039, and 1045,
that 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 replace defective bushings before they cause
failure of the horizontal stabilizer. Such failure could lead to
reduced or loss of control of the aircraft.
(d) What actions must I accomplish to address this problem? To
address this problem, you must accomplish the following:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Replace the horizontal Within the next 150 Follow the
stabilizer hinge bushings hours time-in- ACCOMPLISHMENT
with replacement bushings service (TIS) after INSTRUCTIONS
(part number RDC. 19-09-167- June 10, 2002 (the section of PIAGGIO
1/300) (or FAA-approved effective date of AERO INDUSTRIES
equivalent part number). this AD). S.p.A Service
Bulletin (Mandatory
) No. SB-80-0140,
dated October 15,
2001, and the
applicable service
manual.
------------------------------------------------------------------------
[[Page 19659]]
(2) Send the removed Within 10 days after Send the removed
bushings to PIAGGIO AERO removing the bushings to PIAGGIO
INDUSTRIES S.p.A. so the bushings or within AERO INDUSTRIES
bushings cannot be reused 10 days after June S.p.A, Via Cibrario
and report the return to 10, 2002 (the 4, 16154 Genoa,
FAA. The Office of effective date of Italy, and report
Management and Budget (OMB) this AD), whichever the return to Doug
approved the information occurs later. Rudolph, FAA, at
collection requirements the address in
contained in this paragraph (f) of
regulation under the this AD.
provisions of the Paperwork
Reduction Act of 1980 (44
U.S.C. 3501 et seq.) and
assigned OMB Control Number
2120-0056.
------------------------------------------------------------------------
(e) Can I 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, Standards Office, Small Airplane Directorate.
Note 1: 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
sections 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? Actions required by this AD must be done in accordance
with PIAGGIO AERO INDUSTRIES S.p.A Service Bulletin (Mandatory ) No.
SB-80-0140, dated October 15, 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. 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 2: The subject of this AD is addressed in Italian AD Number
2001-512, dated November 30, 2001.
(i) When does this amendment become effective? This amendment
becomes effective on June 10, 2002.
Issued in Kansas City, Missouri, on April 10, 2002.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 02-9389 Filed 4-22-02; 8:45 am]
BILLING CODE 4910-13-P
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