Published 1999-02-18 · Federal Register document 99-3733
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 Series Airplanes
Publication summary
This document corrects information in an existing airworthiness directive (AD) that applies to certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes. That AD currently requires revising the Performance Section of the Airplane Flight Manual (AFM) to provide the flightcrew with procedures to adjust landing distances for landings performed with the anti-icing system active. That AD also requires revising the Limitations Section of the AFM to prohibit certain types of approaches with the anti-icing system active. This document corrects a typographical error that resulted in reference to a supplement of the AFM that does not exist. This correction is necessary to ensure that the appropriate supplement of the AFM is revised.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:22:57.343810+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_1999-e9a7378e7e7d30d5
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- results[76]
- Raw source SHA-256
- e9a7378e7e7d30d51578560dc0677c56bb1fef0a9323224e2a0afe1544919217
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 98-24-19
- Effective date printed in this edition
- Unknown
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Applicability wording · Applicability
Applicability: Model EMB-145 series airplanes, equipped with Allison Model AE3007A1/2 engines; certificated in any category.
Exact source excerpt. Text positions 5072–5202, end exclusive, in the original decoded publication. SHA-256: 0bfccd2482f09d9857ed2bd7fbdab0f8384885f9d96e3c7674f3a983c526db04
Compliance and requirements
Compliance: Required as indicated, unless accomplished
previously.
To ensure that the flightcrew is advised of appropriate landing
field lengths when operating with the anti-icing system active, and
that instrument approaches at certain flap settings are prohibited
with the anti-icing system active, accomplish the following:
(a) Within 10 days after the effective date of this AD,
accomplish the actions specified by paragraphs (a)(1) and (a)(2) of
this AD.
(1) Revise the Performance Section of the FAA-approved Airplane
Flight Manual (AFM) by inserting a copy of EMBRAER EMB-145 AFM 145/
1153, Revision 19, dated October 23, 1998, into the AFM.
Note 1: When landing in abnormal configurations per the
emergency and abnormal procedures of Section 3 of the AFM and
operating with the anti-icing system active, the landing field
length multiples specified in Section 3 should be applied to the
landing field lengths specified in Supplement 6 of Revision 19 of
the AFM.
(2) Revise the Limitations Section of Supplement 6 of the FAA-
approved AFM to include the following statement. This action may be
accomplished by inserting a copy of this AD into the AFM.
``Flaps 22 instrument approaches with anti-ice on are not
approved.''
(b) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, Atlanta Aircraft Certification
Office (ACO), FAA, Small Airplane Directorate. Operators shall
submit their requests through an appropriate FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, Atlanta ACO.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Atlanta ACO.
(c) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
(d) The AFM revision specified in paragraph (a)(1) of this AD
shall be done in accordance with EMBRAER EMB-145 Airplane Flight
Manual 145/1153, Revision 19, dated October 23, 1998, which contains
the following list of effective pages:
------------------------------------------------------------------------
Revision
Page No. level shown Date shown on page
on page
------------------------------------------------------------------------
List of Effective Pages, Pages 19 October 23, 1998.
A, S6-i, S6-ii.
List of Effective Pages, Page 18 August 6, 1998.
B.
------------------------------------------------------------------------
This incorporation by reference was approved previously by the
Director of the Federal Register in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51 as of December 10, 1998 (63 FR 65050, November 25,
1998). Copies may be obtained from Empresa Brasileira de Aeronautica
S.A. (EMBRAER), P.O. Box 343--CEP 12.225, Sao Jose dos Campos--SP,
Brazil. Copies may be inspected at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the
FAA, Small Airplane Directorate, Atlanta Aircraft Certification
Office, One Crown Center, 1895 Phoenix Boulevard, suite 450,
Atlanta, Georgia; or at the Office of the Federal Register, 800
North Capitol Street, NW., suite 700, Washington, DC.
(e) The effective date of this amendment remains December 10,
1998.
Exact source excerpt. Text positions 5202–8860, end exclusive, in the original decoded publication. SHA-256: dac2a56d4fd08f99e18415582b2cbd119f8fd18cf2188a3a73d9ca6f9d356126
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 98-24-19 · 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.
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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: 7765e89ded19ab494c32f84368d88ec5171fbd3350d062e92e4b6dc3d1d957d1. Source manifest: 47a9383cac188a59a1457bcf2cc2b3b0907ab6d54369dc083c5c6ab7fc04b009.
Official source · 1999-02-18
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 64, Number 32 (Thursday, February 18, 1999)]
[Rules and Regulations]
[Pages 7993-7994]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 99-3733]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 98-NM-317-AD; Amendment 39-10904; AD 98-24-19]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-145 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correcting amendment.
-----------------------------------------------------------------------
SUMMARY: This document corrects information in an existing
airworthiness directive (AD) that applies to certain Empresa Brasileira
de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes. That AD
currently requires revising the Performance Section of the Airplane
Flight Manual (AFM) to provide the flightcrew with procedures to adjust
landing distances for landings performed with the anti-icing system
active. That AD also requires revising the Limitations Section of the
AFM to prohibit certain types of approaches with the anti-icing system
active. This document corrects a typographical error that resulted in
reference to a supplement of the AFM that does not exist. This
correction is necessary to ensure that the appropriate supplement of
the AFM is revised.
DATES: Effective December 10, 1998.
The incorporation by reference of certain publications listed in
the regulations was approved previously by the Director of the Federal
Register as of December 10, 1998 (63 FR 65050, November 25, 1998).
FOR FURTHER INFORMATION CONTACT: Thomas Peters, Aerospace Engineer,
ACE-118A, FAA, Small Airplane Directorate, Atlanta Aircraft
Certification Office, One Crown Center, 1895 Phoenix Boulevard, suite
450, Atlanta, Georgia 30349; telephone (770) 703-6063; fax (770) 703-
6097.
SUPPLEMENTARY INFORMATION: On November 16, 1998, the Federal Aviation
Administration (FAA) issued AD 98-24-19, amendment 39-10904 (63 FR
65050, November 25, 1998), which applies to certain Empresa Brasileira
de Aeronautica S.A. (EMBRAER) Model EMB-145 series airplanes. That AD
requires revising the Performance Section of the Airplane Flight Manual
(AFM) to provide the flightcrew with procedures to adjust landing
distances for landings performed with the anti-icing system active.
That AD also requires revising the Limitations Sections of the AFM to
prohibit certain types of approaches with the anti-icing system active.
That AD was prompted by a report that increased (i.e., higher than
normal) flight idle thrust may occur when the anti-icing system is
active. The actions required by that AD are intended to ensure that the
flightcrew is advised of appropriate landing field lengths when
operating with the anti-icing system active, and that instrument
approaches at certain flap settings are prohibited with the anti-icing
system active. Increased flight idle thrust when the anti-icing system
is active, if not corrected, could result in landing overrun.
Need for the Correction
As published, AD 98-24-19 contains a typographical error in
paragraph (a)(2) of the AD. That paragraph specified a revision to the
Limitations Section of Supplement 12 of the FAA-approved AFM; however,
the correct supplement is Supplement 6. Supplement 12 of the AFM does
not exist.
The FAA has determined that a correction to AD 98-24-19 is
necessary. The correction will ensure that the appropriate supplement
of the AFM is revised.
Correction of Publication
This document corrects the error and revises the AD as an amendment
to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13).
The AD is reprinted in its entirety for the convenience of affected
operators. The effective date of the AD remains December 10, 1998.
Since this action only corrects a typographical error, it has no
adverse economic impact and imposes no additional burden on any person.
Therefore, the FAA has determined that notice and public procedures are
unnecessary.
[[Page 7994]]
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Correction
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) by making the
following correcting amendment:
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 [Corrected]
2. Section 39.13 is amended by revising the following airworthiness
directive (AD):
98-24-19 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-10904. Docket 98-NM-317-AD.
Applicability: Model EMB-145 series airplanes, equipped with
Allison Model AE3007A1/2 engines; certificated in any category.
Compliance: Required as indicated, unless accomplished
previously.
To ensure that the flightcrew is advised of appropriate landing
field lengths when operating with the anti-icing system active, and
that instrument approaches at certain flap settings are prohibited
with the anti-icing system active, accomplish the following:
(a) Within 10 days after the effective date of this AD,
accomplish the actions specified by paragraphs (a)(1) and (a)(2) of
this AD.
(1) Revise the Performance Section of the FAA-approved Airplane
Flight Manual (AFM) by inserting a copy of EMBRAER EMB-145 AFM 145/
1153, Revision 19, dated October 23, 1998, into the AFM.
Note 1: When landing in abnormal configurations per the
emergency and abnormal procedures of Section 3 of the AFM and
operating with the anti-icing system active, the landing field
length multiples specified in Section 3 should be applied to the
landing field lengths specified in Supplement 6 of Revision 19 of
the AFM.
(2) Revise the Limitations Section of Supplement 6 of the FAA-
approved AFM to include the following statement. This action may be
accomplished by inserting a copy of this AD into the AFM.
``Flaps 22 instrument approaches with anti-ice on are not
approved.''
(b) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, Atlanta Aircraft Certification
Office (ACO), FAA, Small Airplane Directorate. Operators shall
submit their requests through an appropriate FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, Atlanta ACO.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Atlanta ACO.
(c) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
(d) The AFM revision specified in paragraph (a)(1) of this AD
shall be done in accordance with EMBRAER EMB-145 Airplane Flight
Manual 145/1153, Revision 19, dated October 23, 1998, which contains
the following list of effective pages:
------------------------------------------------------------------------
Revision
Page No. level shown Date shown on page
on page
------------------------------------------------------------------------
List of Effective Pages, Pages 19 October 23, 1998.
A, S6-i, S6-ii.
List of Effective Pages, Page 18 August 6, 1998.
B.
------------------------------------------------------------------------
This incorporation by reference was approved previously by the
Director of the Federal Register in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51 as of December 10, 1998 (63 FR 65050, November 25,
1998). Copies may be obtained from Empresa Brasileira de Aeronautica
S.A. (EMBRAER), P.O. Box 343--CEP 12.225, Sao Jose dos Campos--SP,
Brazil. Copies may be inspected at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the
FAA, Small Airplane Directorate, Atlanta Aircraft Certification
Office, One Crown Center, 1895 Phoenix Boulevard, suite 450,
Atlanta, Georgia; or at the Office of the Federal Register, 800
North Capitol Street, NW., suite 700, Washington, DC.
(e) The effective date of this amendment remains December 10,
1998.
Issued in Renton, Washington, on February 9, 1999.
John J. Hickey,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 99-3733 Filed 2-17-99; 8:45 am]
BILLING CODE 4910-13-U
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