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Published 2008-12-24 · Federal Register document E8-30406

Airworthiness Directives; Piper Aircraft, Inc. Models PA-46-350P, PA-46R-350T, and PA-46-500TP Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Models PA-46-350P, PA-46R-350T, and PA-46- 500TP airplanes. This AD requires you to install a stall warning heat control modification kit. This AD results from ice forming on the stall vane heater during flights into icing conditions with the landing gear down. We are issuing this AD to prevent ice from forming on the stall vane, which may result in failure of the stall warning system. This failure could result in the pilot being unaware of an approaching stall situation.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:26.953736+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2008-e9cf118935fdae82
Source row
results[474]
Raw source SHA-256
e9cf118935fdae82a000e2c01764c770bd79679c1dd4c2b00fdcd3b030f92fe5

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2008-26-11
Effective date printed in this edition
2009-01-28
Read 7 complete recorded clauses
Effective Date
Effective Date

    (a) This AD becomes effective on January 28, 2009.

Exact source excerpt. Text positions 7141–7213, end exclusive, in the original decoded publication. SHA-256: 002dcc4ca821a8897c7f1dabf6196ffc44d44ee7be4bf1aa4e81d71eb2de58c9

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 7213–7242, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to the following airplane models and serial 
numbers that are certificated in any category:

------------------------------------------------------------------------
                 Models                            Serial Nos.
------------------------------------------------------------------------
PA-46-350P.............................  4622001 through 4622200 and
                                          4636001 through 4636445.
PA-46R-350T............................  4692001 through 4692054.
PA-46-500TP............................  4697001 through 4697365.
------------------------------------------------------------------------

Exact source excerpt. Text positions 7242–7925, end exclusive, in the original decoded publication. SHA-256: 2e2bbc19c770604e05d46f2c67eda97ab29c78510fa333c0402974c9ea98fd6a

Unsafe Condition
Unsafe Condition

    (d) This AD results from ice forming on the stall vane heater 
during flights into icing conditions with the landing gear down. We 
are issuing this AD to prevent ice from forming on the stall vane, 
which may result in failure of the stall warning system. This 
failure could result in the pilot being unaware of an approaching 
stall situation.

Exact source excerpt. Text positions 7925–8295, end exclusive, in the original decoded publication. SHA-256: b9441be06c94bbf2b0aa15f2a3f868e5b6533ba840c95ee982e68fc0ac4f33d3

Compliance
Compliance

    (e) To address this problem, you must do the following, unless 
already done:

------------------------------------------------------------------------
           Actions                 Compliance            Procedures
------------------------------------------------------------------------
Install Stall Warning Heat    Within the next 100   As specified in
 Control Modification Kit,     hours time-in-        Piper Mandatory
 Piper part number 88452-002.  service after         Service Bulletin
                               January 28, 2009      No. 1192, dated
                               (the effective date   September 15, 2008,
                               of this AD).          following Drawing
                                                     No. 88452, dated
                                                     June 19, 2008.
------------------------------------------------------------------------

Exact source excerpt. Text positions 8295–9236, end exclusive, in the original decoded publication. SHA-256: 83fd8e5a4246b875ec5ca096ba2aaa6ab02ceb6e98cd61e9f45b4a0f205c3818

Alternative Methods of Compliance (AMOCs)
Alternative Methods of Compliance (AMOCs)

    (f) The Manager, Atlanta Aircraft Certification Office (ACO), 
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: John Lee, Aerospace Engineer, Federal Aviation Administration, 
Atlanta ACO, One Crown Center, 1895 Phoenix Blvd., Suite 450, 
Atlanta, Georgia 30349; telephone: (770) 994-6736; fax: (770) 703-
6097. 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.

Exact source excerpt. Text positions 9236–9897, end exclusive, in the original decoded publication. SHA-256: ab59ff909cf02d789a43043524738e9949c1bd99a8eb5218f223b9d4c3b539bd

Material Incorporated by Reference
Material Incorporated by Reference

    (g) You must use Piper Mandatory Service Bulletin No. 1192, 
dated September 15, 2008, and Drawing No. 88452, dated June 19, 
2008, to do the actions required by this AD, unless the AD specifies 
otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact Piper 
Aircraft, Inc., 2926 Piper Drive, Vero Beach, Florida 32960; 
telephone: (772) 567-4361; fax: (772) 978-6573; Internet: http://www.newpiper.com/.
    (3) You may review copies of the service information 
incorporated by reference for this AD at the FAA, Central Region, 
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the 
Central Region, call (816) 329-3768.
    (4) You may also review copies of the service information 
incorporated by reference for this AD 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/code_of_federal_regulations/ibr_locations.html.

Exact source excerpt. Text positions 9897–11158, end exclusive, in the original decoded publication. SHA-256: fa3f8211e54bd3c7d318afc30b0e06d44e2b8e55fa79f10ecff6112936d73afc

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 2008-26-11 · 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: 2b70668d458b2ed1db92c576ebfe80842fa6eeb8025483a4d8481944fdd2aae4. Source manifest: 5535025d3da49d23ca2d86c72ba2fdc12fedd0fa80d334cb9dabc764cba74665.

Official source · 2008-12-24

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 73, Number 248 (Wednesday, December 24, 2008)]
[Rules and Regulations]
[Pages 78934-78935]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E8-30406]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-1085; Directorate Identifier 2008-CE-057-AD; 
Amendment 39-15777; AD 2008-26-11]
RIN 2120-AA64


Airworthiness Directives; Piper Aircraft, Inc. Models PA-46-350P, 
PA-46R-350T, and PA-46-500TP Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain 
Piper Aircraft, Inc. (Piper) Models PA-46-350P, PA-46R-350T, and PA-46-
500TP airplanes. This AD requires you to install a stall warning heat 
control modification kit. This AD results from ice forming on the stall 
vane heater during flights into icing conditions with the landing gear 
down. We are issuing this AD to prevent ice from forming on the stall 
vane, which may result in failure of the stall warning system. This 
failure could result in the pilot being unaware of an approaching stall 
situation.

DATES: This AD becomes effective on January 28, 2009.
    On January 28, 2009, the Director of the Federal Register approved 
the incorporation by reference of certain publications listed in this 
AD.

ADDRESSES: For service information identified in this AD, contact Piper 
Aircraft, Inc., 2926 Piper Drive, Vero Beach, Florida 32960; telephone: 
(772) 567-4361; fax: (772) 978-6573; Internet: http://www.newpiper.com/
.
    To view the AD docket, go to U.S. Department of Transportation, 
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 
New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at 
http://www.regulations.gov. The docket number is FAA-2008-1085; 
Directorate Identifier 2008-CE-057-AD.

FOR FURTHER INFORMATION CONTACT: John Lee, Aerospace Engineer, Federal 
Aviation Administration, Aircraft Certification Office, One Crown 
Center, 1895 Phoenix Blvd., Suite 450, Atlanta, Georgia 30349; 
telephone: (770) 994-6736; fax: (770) 703-6097.

SUPPLEMENTARY INFORMATION:

Discussion

    On October 3, 2008, 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 Piper Models PA-46-350P, PA-46R-350T, and PA-46-
500TP airplanes. This proposal was published in the Federal Register as 
a notice of proposed rulemaking (NPRM) on October 10, 2008 (73 FR 
60201). The NPRM proposed to require you to install a stall warning 
heat control modification kit.

Comments

    We provided the public the opportunity to participate in developing 
this AD. We received no comments on the proposal or on the 
determination of the cost to the public.

Conclusion

    We have carefully reviewed the available data and determined that 
air safety and the public interest require adopting the AD as proposed 
except for minor editorial corrections. We have determined that these 
minor corrections:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for correcting the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Costs of Compliance

    We estimate that this AD affects 803 airplanes in the U.S. 
registry.
    We estimate the following costs to do the modification:

----------------------------------------------------------------------------------------------------------------
                                                                                 Total cost per   Total cost on
                          Labor cost                              Parts cost        airplane     U.S.  operators
----------------------------------------------------------------------------------------------------------------
1.5 work-hours x $80 per hour = $120.........................             $95             $215         $172,645
----------------------------------------------------------------------------------------------------------------

    Warranty credit may be given to the extent noted in the service 
bulletin.

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

[[Page 78935]]

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 AD.

Regulatory Findings

    We have determined that 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 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 summary of the costs to comply with this AD (and 
other information as included in the Regulatory Evaluation) and placed 
it in the AD Docket. You may get a copy of this summary by sending a 
request to us at the address listed under ADDRESSES. Include ``Docket 
No. FAA-2008-1085; Directorate Identifier 2008-CE-057-AD'' in your 
request.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
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

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. FAA amends Sec.  39.13 by adding the following new AD:

2008-26-11 Piper Aircraft, Inc.: Amendment 39-15777; Docket No. FAA-
2008-1085; Directorate Identifier 2008-CE-057-AD.

Effective Date

    (a) This AD becomes effective on January 28, 2009.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to the following airplane models and serial 
numbers that are certificated in any category:

------------------------------------------------------------------------
                 Models                            Serial Nos.
------------------------------------------------------------------------
PA-46-350P.............................  4622001 through 4622200 and
                                          4636001 through 4636445.
PA-46R-350T............................  4692001 through 4692054.
PA-46-500TP............................  4697001 through 4697365.
------------------------------------------------------------------------

Unsafe Condition

    (d) This AD results from ice forming on the stall vane heater 
during flights into icing conditions with the landing gear down. We 
are issuing this AD to prevent ice from forming on the stall vane, 
which may result in failure of the stall warning system. This 
failure could result in the pilot being unaware of an approaching 
stall situation.

Compliance

    (e) To address this problem, you must do the following, unless 
already done:

------------------------------------------------------------------------
           Actions                 Compliance            Procedures
------------------------------------------------------------------------
Install Stall Warning Heat    Within the next 100   As specified in
 Control Modification Kit,     hours time-in-        Piper Mandatory
 Piper part number 88452-002.  service after         Service Bulletin
                               January 28, 2009      No. 1192, dated
                               (the effective date   September 15, 2008,
                               of this AD).          following Drawing
                                                     No. 88452, dated
                                                     June 19, 2008.
------------------------------------------------------------------------

Alternative Methods of Compliance (AMOCs)

    (f) The Manager, Atlanta Aircraft Certification Office (ACO), 
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: John Lee, Aerospace Engineer, Federal Aviation Administration, 
Atlanta ACO, One Crown Center, 1895 Phoenix Blvd., Suite 450, 
Atlanta, Georgia 30349; telephone: (770) 994-6736; fax: (770) 703-
6097. 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.

Material Incorporated by Reference

    (g) You must use Piper Mandatory Service Bulletin No. 1192, 
dated September 15, 2008, and Drawing No. 88452, dated June 19, 
2008, to do the actions required by this AD, unless the AD specifies 
otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact Piper 
Aircraft, Inc., 2926 Piper Drive, Vero Beach, Florida 32960; 
telephone: (772) 567-4361; fax: (772) 978-6573; Internet: http://www.newpiper.com/.
    (3) You may review copies of the service information 
incorporated by reference for this AD at the FAA, Central Region, 
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the 
Central Region, call (816) 329-3768.
    (4) You may also review copies of the service information 
incorporated by reference for this AD 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/code_of_federal_regulations/ibr_locations.html.

    Issued in Kansas City, Missouri, on December 16, 2008.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E8-30406 Filed 12-23-08; 8:45 am]
BILLING CODE 4910-13-P


Why this text is shown

The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:26:08.031775+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
159473370e70c5a6de36e5a0cf4e8b4272f6a15e4ba44ed039172ff6cb4a0d02
Text SHA-256
2b70668d458b2ed1db92c576ebfe80842fa6eeb8025483a4d8481944fdd2aae4

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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.