Published 2005-04-07 · Federal Register document 05-6909
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Series Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 series airplanes. This AD requires revising the Limitations section of the airplane flight manual to advise the flightcrew to make sure the correct instrument landing system (ILS) identifier is included on the flight management system (FMS) flight plan before the flightcrew initiates an approach to landing with the autopilot engaged. This AD is prompted by reports that the airplane's autopilot may apply large- amplitude control inputs while following ILS guidance to a runway that is not included on the FMS flight plan. We are issuing this AD to prevent hazardous maneuvers close to the ground, which could result in an impact with an obstacle or terrain.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:17.300228+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2005-5d43d153038ee1c1
- Source row
- results[144]
- Raw source SHA-256
- 5d43d153038ee1c1c214f5c3688e38e25e37b832227fe65d52f7420a65ee20f2
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2005-07-22
- Effective date printed in this edition
- 2005-04-22
Read 9 complete recorded clauses
Effective Date
Effective Date
(a) This AD becomes effective April 22, 2005.
Exact source excerpt. Text positions 10311–10378, end exclusive, in the original decoded publication. SHA-256: a67e77190293599986aa9acee359dc6477c24761c478b57b627de0a0abfedd5a
Affected ADs
Affected ADs
(b) None.
Exact source excerpt. Text positions 10378–10407, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b
Applicability wording · Applicability
Applicability
(c) This AD applies to all Empresa Brasileira de Aeronautica
S.A. (EMBRAER) Model ERJ 170 series airplanes, certificated in any
category.
Exact source excerpt. Text positions 10407–10567, end exclusive, in the original decoded publication. SHA-256: a1336cb45810e03134565fe8c4cb841298b218fef6fc36706d2bb1d03f3b1f1f
Unsafe Condition
Unsafe Condition
(d) This AD was prompted by reports that the airplane's
autopilot may apply large-amplitude control inputs while following
instrument landing system (ILS) guidance to a runway that is not
included on the flight management system (FMS) flight plan. The FAA
is issuing this AD to prevent hazardous maneuvers close to the
ground, which could result in an impact with an obstacle or terrain.
Exact source excerpt. Text positions 10567–10983, end exclusive, in the original decoded publication. SHA-256: 9b7188bf8d84d5b023cd7ae3eca5f520b37921f9998ea0a4229cd780be23533d
Compliance
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Exact source excerpt. Text positions 10983–11161, end exclusive, in the original decoded publication. SHA-256: 64a7a1579f37f56eafecd0aeb3c528e7c89f6292ed0cb53091423917642d5847
Airplane Flight Manual Revision
Airplane Flight Manual Revision
(f) Within 15 days after the effective date of this AD, revise
the Limitations section of the EMBRAER Model ERJ 170 airplane flight
manual (AFM) to include the following statement in the ``Autopilot''
subsection. This may be done by inserting a copy of this AD in the
AFM.
``Before initiating an approach to landing with AUTOPILOT
engaged, make sure the correct ILS identifier has been inserted on
the FMS PROGRESS PAGE 1/3, Lines 5L and 5R.''
Note 1: When a statement identical to that in paragraph (f) of
this AD has been included in the general revisions of the AFM, the
general revisions may be inserted into the AFM, and the copy of this
AD may be removed from the AFM.
Exact source excerpt. Text positions 11161–11892, end exclusive, in the original decoded publication. SHA-256: fd4f70af711a9d2587753ffcd4ef5f517c303729514556dbc83c62578afe9383
Alternative Methods of Compliance (AMOCs)
Alternative Methods of Compliance (AMOCs)
(g) The Manager, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
Exact source excerpt. Text positions 11892–12123, end exclusive, in the original decoded publication. SHA-256: 42ad4b48fc8f1e1d3d0c919395397aac93707d7493c80c0d69538ca1b17256cf
Related Information
Related Information
(h) Brazilian airworthiness directive 2005-03-01, dated March
21, 2005, also addresses the subject of this AD.
Exact source excerpt. Text positions 12123–12261, end exclusive, in the original decoded publication. SHA-256: 410919d50df4b07afed5ec3668e6b67488317e296a449d137de4c480093440e9
Material Incorporated by Reference
Material Incorporated by Reference
(i) None.
[[Page 17608]]
Exact source excerpt. Text positions 12261–12328, end exclusive, in the original decoded publication. SHA-256: 81145457ac28f1b29c72986c4c41515af44b4a98e4d20bb1c370c733979ec862
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 2005-07-22 · 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: 5cf0a4ca0ffee41bd38ded73d923e032e604d45e1f5a8243457c09ea857dcbbe. Source manifest: 50f78a5647f2029af10f89d091f99bc926d5b9aeb80ee1c116402ea91f9900c7.
Official source · 2005-04-07
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 70, Number 66 (Thursday, April 7, 2005)]
[Rules and Regulations]
[Pages 17606-17608]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-6909]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20883; Directorate Identifier 2005-NM-064-AD;
Amendment 39-14047; AD 2005-07-22]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 series
airplanes. This AD requires revising the Limitations section of the
airplane flight manual to advise the flightcrew to make sure the
correct instrument landing system (ILS) identifier is included on the
flight management system (FMS) flight plan before the flightcrew
initiates an approach to landing with the autopilot engaged. This AD is
prompted by reports that the airplane's autopilot may apply large-
amplitude control inputs while following ILS guidance to a runway that
is not included on the FMS flight plan. We are issuing this AD to
prevent hazardous maneuvers close to the ground, which could result in
an impact with an obstacle or terrain.
DATES: Effective April 22, 2005. We must receive comments on this AD by
June 6, 2005.
ADDRESSES: Use one of the following addresses to submit comments on
this AD.
<bullet> DOT Docket Web site: Go to http://dms.dot.gov and follow
the instructions for sending your comments electronically.
<bullet> Government-wide rulemaking Web site: Go to http://www.regulations.gov and follow the instructions for sending your
comments electronically.
<bullet> Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street SW, Nassif Building, room PL-401,
Washington, DC 20590.
<bullet> Fax: (202) 493-2251.
<bullet> Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street SW., Washington, DC, between 9 a.m.
and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this AD, contact Empresa
Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343-CEP 12.225, Sao
Jose dos Campos--SP, Brazil.
You can examine the contents of this AD docket on the Internet at
http://dms.dot.gov, or in person at the Docket Management Facility,
U.S. Department of Transportation, 400 Seventh Street SW., room PL-401,
on the plaza level of the Nassif Building, Washington, DC. This docket
number is FAA-2005-20883; the directorate identifier for this docket is
2005-NM-064-AD.
Examining the Docket
You can examine the AD docket on the Internet at http://dms.dot.gov, or in person at the Docket Management Facility office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the DOT
street address stated in the ADDRESSES section. Comments will be
available in the AD docket shortly after the DMS receives them.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: The Departmento de Aviacao Civil (DAC),
which is the airworthiness authority for Brazil, notified the FAA that
an unsafe condition may exist on all Empresa Brasileira de Aeronautica
S.A. (EMBRAER) Model ERJ 170 series airplanes. The DAC advises that it
has received several reports that the airplane's autopilot applied
large-amplitude control inputs while following instrument landing
system (ILS) guidance to runways that were not included on the flight
management system (FMS) flight plan. This condition, if not corrected,
could cause hazardous maneuvers close to the ground, and result in an
impact with an obstacle or terrain.
Brazilian Airworthiness Directive
The DAC issued Brazilian airworthiness directive 2005-03-01, dated
March 21, 2005, which mandates modification of the autopilot-coupled
ILS approach procedures by revising the Limitations section of the
airplane flight manual to advise the flightcrew to make sure the
correct ILS identifier is included on the FMS flight plan before the
flightcrew initiates an approach to landing with the autopilot engaged.
The DAC issued airworthiness directive 2005-03-01 to ensure the
continued airworthiness of these airplanes in Brazil.
FAA's Determination and Requirements of This AD
This airplane model is manufactured in Brazil and is type
certificated for operation in the United States under the provisions of
section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and
the applicable bilateral airworthiness agreement. Pursuant to this
bilateral airworthiness agreement, the DAC has kept the FAA informed of
the situation described above. We have examined the DAC's findings,
evaluated all pertinent information, and determined that we need to
issue an AD
[[Page 17607]]
for products of this type design that are certificated for operation in
the United States.
Therefore, we are issuing this AD to prevent hazardous maneuvers
close to the ground, which could result in an impact with an obstacle
or terrain. This AD requires revising the Limitations section of the
airplane flight manual to advise the flightcrew to make sure the
correct ILS identifier is included on the FMS flight plan before the
flightcrew initiates an approach to landing with the autopilot engaged.
Interim Action
We consider this AD interim action. If final action is later
identified, we may consider further rulemaking then.
FAA's Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD; therefore, providing notice and opportunity for public comment
before the AD is issued is impracticable, and good cause exists to make
this AD effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements that affect
flight safety and was not preceded by notice and an opportunity for
public comment; however, we invite you to submit any relevant written
data, views, or arguments regarding this AD. Send your comments to an
address listed under ADDRESSES. Include ``Docket No. FAA-2005-20883;
Directorate Identifier 2005-NM-064-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the AD. We will consider
all comments received by the closing date and may amend the AD in light
of those comments.
We will post all comments we receive, without change, to http://dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact with FAA
personnel concerning this AD. Using the search function of our docket
Web site, anyone can find and read the comments in any of our dockets,
including the name of the individual who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
You can review the DOT's complete Privacy Act Statement in the Federal
Register published on April 11, 2000 (65 FR 19477-78), or you can visit
http://dms.dot.gov.
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 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
rulemaking action.
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 the regulation:
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 regulatory evaluation of the estimated costs to
comply with this AD. See the ADDRESSES section for a location to
examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the FAA amends 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. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2005-07-22 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-14047. Docket No. FAA-2005-20883; Directorate
Identifier 2005-NM-064-AD.
Effective Date
(a) This AD becomes effective April 22, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Empresa Brasileira de Aeronautica
S.A. (EMBRAER) Model ERJ 170 series airplanes, certificated in any
category.
Unsafe Condition
(d) This AD was prompted by reports that the airplane's
autopilot may apply large-amplitude control inputs while following
instrument landing system (ILS) guidance to a runway that is not
included on the flight management system (FMS) flight plan. The FAA
is issuing this AD to prevent hazardous maneuvers close to the
ground, which could result in an impact with an obstacle or terrain.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Airplane Flight Manual Revision
(f) Within 15 days after the effective date of this AD, revise
the Limitations section of the EMBRAER Model ERJ 170 airplane flight
manual (AFM) to include the following statement in the ``Autopilot''
subsection. This may be done by inserting a copy of this AD in the
AFM.
``Before initiating an approach to landing with AUTOPILOT
engaged, make sure the correct ILS identifier has been inserted on
the FMS PROGRESS PAGE 1/3, Lines 5L and 5R.''
Note 1: When a statement identical to that in paragraph (f) of
this AD has been included in the general revisions of the AFM, the
general revisions may be inserted into the AFM, and the copy of this
AD may be removed from the AFM.
Alternative Methods of Compliance (AMOCs)
(g) The Manager, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested in
accordance with the procedures found in 14 CFR 39.19.
Related Information
(h) Brazilian airworthiness directive 2005-03-01, dated March
21, 2005, also addresses the subject of this AD.
Material Incorporated by Reference
(i) None.
[[Page 17608]]
Issued in Renton, Washington, on March 31, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-6909 Filed 4-6-05; 8:45 am]
BILLING CODE 4910-13-P
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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.
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