Back to publication catalog

Published 2001-01-02 · Federal Register document 00-32935

Airworthiness Directives; Industrie Aeronautiche e Meccaniche Model Piaggio P-180 Airplanes

Publication summary

This amendment removes Airworthiness Directive (AD) 2000-03- 19, which currently applies to all Industrie Aeronautiche e Meccaniche (I.A.M.) Model Piaggio P-180 airplanes that are equipped with pneumatic deicing boots. AD 2000-03-19 requires revising the Airplane Flight Manual (AFM) to include requirements for activating the airframe pneumatic deicing boots. Since FAA issued AD 2000-03-19, I.A.M. has shown the language currently included in the AFM and the airplane configuration are satisfactory to address the conditions identified in AD 2000-03-19. Therefore, this action removes AD 2000-03-19.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:03.835669+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2001-8d66ddb74aa17366
Source row
results[0]
Raw source SHA-256
8d66ddb74aa17366596c5f6ccb4e6d04532df19ae027b6fa003379bdedb52c7e

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2000-03-19
Effective date printed in this edition
Unknown

No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.

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Find all recorded historical references to AD 2000-03-19 · 0 printed reference observations in this pinned collection.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: 6fca785cef220c8146ae94d8356d439b023e45704fff8f18343ac7beb0362d0d. Source manifest: 49abc6696392ede4d0014f5de1f14977e65d080d2311dee1f7c9393aca4f231c.

Official source · 2001-01-02

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 66, Number 1 (Tuesday, January 2, 2001)]
[Rules and Regulations]
[Pages 7-8]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 00-32935]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 99-CE-34-AD; Amendment 39-12053; AD 2000-03-19]
RIN 2120-AA64


Airworthiness Directives; Industrie Aeronautiche e Meccaniche 
Model Piaggio P-180 Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; Removal.

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

SUMMARY: This amendment removes Airworthiness Directive (AD) 2000-03-
19, which currently applies to all Industrie Aeronautiche e Meccaniche 
(I.A.M.) Model Piaggio P-180 airplanes that are equipped with pneumatic 
deicing boots. AD 2000-03-19 requires revising the Airplane Flight 
Manual (AFM) to include requirements for activating the airframe 
pneumatic deicing boots. Since FAA issued AD 2000-03-19, I.A.M. has 
shown the language currently included in the AFM and the airplane 
configuration are satisfactory to address the conditions identified in 
AD 2000-03-19. Therefore, this action removes AD 2000-03-19.

EFFECTIVE DATE: This removal is effective January 2, 2001.

FOR FURTHER INFORMATION CONTACT: Larry Werth, Airworthiness Directive 
Coordinator, FAA, Small Airplane Directorate, 901 Locust, Room 301, 
Kansas City, Missouri 64106; telephone: (816) 329-4147; facsimile: 
(816) 329-4090.

SUPPLEMENTARY INFORMATION:

Discussion

    Has FAA taken any action to this point? Reports of in-flight 
incidents and an accident (on airplanes other than I.A.M. Piaggio Model 
P-180 airplanes), that occurred in icing conditions where the airframe 
pneumatic deicing boots were not activated, caused FAA to issue AD 
2000-03-19, Amendment 39-11578 (65 FR 7717, February 16, 2000). This AD 
currently requires revising the Airplane Flight Manual (AFM) to include 
requirements for activating the airframe pneumatic deicing boots on all 
I.A.M. Model Piaggio P-180 airplanes that are equipped with pneumatic 
deicing boots.
    The actions of AD 2000-03-19 are intended to assure that 
flightcrews have the information necessary to activate the pneumatic 
wing and tail deicing boots at the first signs of ice build-up. Without 
this information, flightcrews could experience reduced control of the 
aircraft because of adverse aerodynamic effects of ice adhering to the 
airplane before the first deicing cycle.
    After issuing AD 2000-03-19, I.A.M. asserted that the wording 
within the AFM (without the revision) and the configuration of the 
airplane deice system provide for safe operation of the affected 
airplanes. Therefore, I.A.M. requests FAA remove the final rule because 
the AD requirements are redundant. The FAA has since evaluated all 
information related to the subject matter of AD 2000-03-19 and has 
determined the actions included in AD 2000-03-19 are redundant and not 
necessary.
    We issued a proposal to amend part 39 of the Federal Aviation 
Regulations (14 CFR part 39) to remove AD 2000-03-19. This proposal was 
published in the Federal Register as a Notice of proposed rulemaking 
(NPRM); removal of final rule on October 19, 2000 (65 FR 62650).
    Was the public invited to comment? Interested persons were afforded 
an opportunity to participate in the making of the action. No comments 
were received on the proposed rule.

FAA's Determination

    What is FAA's Final Determination on this Issue? Based on the above 
information, FAA has determined there is no need for AD 2000-03-19 and 
that it should be removed.

[[Page 8]]

    This action removes AD 2000-03-19. Removal of AD 2000-03-19 will 
not preclude FAA from issuing another action in the future, nor will it 
commit us to any course of action in the future.

Regulatory Impact

    Does this action involve a significant rule or regulatory action? 
Since this action only removes an AD, it is not an AD and, therefore, 
is not covered under Executive Order 12866, the Regulatory Flexibility 
Act, or DOT Regulatory Policies and Procedures (44 FR 11034, February 
26, 1979).

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

The Removal

    Accordingly, pursuant to 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 removing Airworthiness Directive (AD) 
2000-03-19, Amendment 39-11578 (65 FR 7717, February 16, 2000).

    Issued in Kansas City, Missouri, on December 19, 2000.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 00-32935 Filed 12-29-00; 8:45 am]
BILLING CODE 4910-13-U


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T04:33:26.856591+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
a4232cab386512007880aaf1837557d0b5e0bb6a1eec5d8edad97f34b0fc70c5
Text SHA-256
6fca785cef220c8146ae94d8356d439b023e45704fff8f18343ac7beb0362d0d

Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence

Coverage and limits

These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.

The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.