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Published 2011-06-27 · Federal Register document 2011-15989

Airworthiness Directives; Dassault Aviation Model FALCON 7X Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for the products listed above. This emergency AD was sent previously to all known U.S. owners and operators of these airplanes. This AD requires that, as of the effective date of the AD, operation of Model FALCON 7X airplanes is prohibited. This AD was prompted by a report of an uncontrolled pitch trim runaway during descent. We are issuing this AD to prevent loss of control of the airplane.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:36.067984+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2011-e3661fa6ab35b428
Source row
results[186]
Raw source SHA-256
e3661fa6ab35b428e6e5ee3716d50c22e985c092328ad8ce2f0f440b962ae0cd

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2011-12-51
Effective date printed in this edition
Unknown
Read 9 complete recorded clauses
Effective Date
Effective Date

    (a) This AD is effective July 12, 2011 to all persons except 
those persons to whom it was made immediately effective by Emergency 
AD 2011-12-51, issued on May 27, 2011, which contained the 
requirements of this amendment.

Exact source excerpt. Text positions 8712–8957, end exclusive, in the original decoded publication. SHA-256: b9e952573a5617a5954d0328cd0b6c4dc10afbfceb76e05c0b85d8a6bf5f5189

Affected ADs
Affected ADs

    (b) None.

Exact source excerpt. Text positions 8957–8986, end exclusive, in the original decoded publication. SHA-256: 027fbc44617399472b6ac4741da3aee18448654374228bcf4fe3f01df6b1539b

Applicability wording · Applicability
Applicability

    (c) This AD applies to Dassault Aviation Model FALCON 7X 
airplanes, certificated in any category, all serial numbers.

Exact source excerpt. Text positions 8986–9125, end exclusive, in the original decoded publication. SHA-256: 482b05b9b05d76a365b5b274688d6ca7c33fa95b2faf998e14ea947408ad01c4

Subject
Subject

    (d) Joint Aircraft System Component (JASC)/Air Transport 
Association (ATA) of America Code 27: Flight controls.

Exact source excerpt. Text positions 9125–9252, end exclusive, in the original decoded publication. SHA-256: d8c55bd240f495118852700e2f2587e5932255258a3c9173a6e10a7b3bb96d54

Unsafe Condition
Unsafe Condition

    (e) This AD was prompted by a report of an uncontrolled pitch 
trim runaway during descent. We are issuing this AD to prevent loss 
of control of the airplane.

Exact source excerpt. Text positions 9252–9435, end exclusive, in the original decoded publication. SHA-256: bc4400c6a41e1471be29d7de9e74f5ebd6ea862fc1e94fadff4674fd149d3394

Compliance
Compliance

    (f) Comply with this AD within the compliance times specified, 
unless already done.

Exact source excerpt. Text positions 9435–9537, end exclusive, in the original decoded publication. SHA-256: 76a8ec0548389ac4eaa60ddcc67a7a3de5aedefd320c767b7cf621baa6140ea8

Flight Prohibited
Flight Prohibited

    (g) As of the effective date of this AD, operation of the 
airplane is prohibited.

Exact source excerpt. Text positions 9537–9644, end exclusive, in the original decoded publication. SHA-256: a9a1d6c67447493334b3b0770a156b53b7937672aa36d522af0f97f79908eeee

Special Flight Permit
Special Flight Permit

    (h) Special flight permits, as described in Section 21.197 and 
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197 
and 21.199), are not allowed.

Alternative Methods of Compliance (AMOCs)

    (i)(1) The Manager, International Branch, Transport Airplane 
Directorate, FAA, has the authority to approve AMOCs for this AD, if 
requested using the procedures found in 14 CFR 39.19. In accordance 
with 14 CFR 39.19, send your request to your principal inspector or 
local Flight Standards District Office, as appropriate. If sending 
information directly to the manager of the International Branch, 
send it to the attention of the person identified in the Related 
Information section of this AD. Information may be e-mailed to: [email protected].
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.

Related Information

    (j)(1) For further information about this AD, contact Tom 
Rodriguez, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; phone: 425-227-1137; fax: 425-227-1149.
    (2) Refer to MCAI European Aviation Safety Agency (EASA) 
Emergency Airworthiness Directive 2011-0102-E, dated May 26, 2011, 
for related information.

Exact source excerpt. Text positions 9644–11086, end exclusive, in the original decoded publication. SHA-256: 2cc7d759855be34987c5620a24a90c6cd3913b0506d98a5a5eb1b822e5c9e2ce

Material Incorporated by Reference
Material Incorporated by Reference

    (k) None.

Exact source excerpt. Text positions 11086–11136, end exclusive, in the original decoded publication. SHA-256: 5f9f4186bdc284fd4d5116111d055a69aa0e98a7110e30c8860fcf9b7c7d31bc

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 2011-12-51 · 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: f33e75dfd28adf62a5e760184048801427601c79688d397da93da632e3ffc263. Source manifest: 05bb640f95f5da8dc23b09fa46f70eed25dd88bdac9d04ed0a600d30978fc0fe.

Official source · 2011-06-27

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 76, Number 123 (Monday, June 27, 2011)]
[Rules and Regulations]
[Pages 37251-37253]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-15989]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0477; Directorate Identifier 2011-NM-108-AD; 
Amendment 39-16735; AD 2011-12-51]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Model FALCON 7X 
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for the 
products listed above. This emergency AD was sent previously to all 
known U.S. owners and operators of these airplanes. This AD requires 
that, as of the effective date of the AD, operation of Model FALCON 7X 
airplanes is prohibited. This AD was prompted by a report of an 
uncontrolled pitch trim runaway during descent. We are issuing this AD 
to prevent loss of control of the airplane.

DATES: This AD is effective July 12, 2011 to all persons except those 
persons to whom it was made immediately effective by Emergency AD 2011-
12-51, issued on May 27, 2011, which contained the requirements of this 
amendment.
    We must receive comments on this AD by August 11, 2011.

ADDRESSES: You may send comments by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue, SE., Washington, DC 20590.

[[Page 37252]]

    <bullet> Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations Office 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this AD, the regulatory evaluation, 
any comments received, and other information. The street address for 
the Docket Operations Office (phone: 800-647-5527) is in the ADDRESSES 
section. Comments will be available in the AD docket shortly after 
receipt.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; phone: 425-227-
1137; fax: 425-227-1149.

SUPPLEMENTARY INFORMATION:

Discussion

    On May 27, 2011, we issued Emergency AD 2011-12-51, which requires 
that, as of receipt of the AD, operation of Model FALCON 7X airplanes 
is prohibited.
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Community, has issued 
Emergency Airworthiness Directive 2011-0102-E, dated May 26, 2011 
(referred to after this as ``the MCAI''), to correct an unsafe 
condition for the specified products.
    EASA has advised that a Model FALCON 7X airplane experienced an 
uncontrolled pitch trim runaway during descent. The crew succeeded in 
recovering a stable situation and performed an uneventful landing. 
Analysis of the Digital Flight Data Recorder (DFDR) and Fault History 
Database (FHDB) confirmed the event, but did not identify the cause of 
the pitch trim runaway. This condition, if not corrected, could result 
in loss of control of the airplane.
    To address this unsafe condition, the EASA AD prohibits, from the 
effective date of the EASA AD, any flight operations of FALCON 7X 
airplanes.

FAA's Determination

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI referenced 
above. We are issuing this AD because we evaluated all pertinent 
information and determined the unsafe condition exists and is likely to 
exist or develop on other products of the same type design.

AD Requirements

    This AD requires that, as of effective date of the AD, operation of 
Model FALCON 7X airplanes is prohibited.

Interim Action

    We consider this AD interim action pending the outcome of the 
investigation currently being carried out by the manufacturer. We may 
consider further rulemaking when additional information is available.

FAA's Determination of the Effective Date

    An unsafe condition exists that requires the immediate adoption of 
this AD. The FAA has found that the risk to the flying public justifies 
waiving notice and comment prior to adoption of this rule because an 
uncontrolled pitch trim runaway during descent could result in loss of 
control of the airplane. Therefore, we find that notice and opportunity 
for prior public comment are impracticable and that good cause exists 
for making this amendment effective in less than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety and was not preceded by notice and an opportunity for public 
comment. However, we invite you to send any written data, views, or 
arguments about this AD. Send your comments to an address listed under 
the ADDRESSES section. Include the docket number FAA-2011-0477 and 
Directorate Identifier 2011-NM-108-AD at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this AD. We will 
consider all comments received by the closing date and may amend this 
AD because of those comments.
    We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this AD.

Costs of Compliance

    We estimate that this AD affects 26 airplanes of U.S. registry. 
There are no costs associated with complying with this AD.

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

    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 DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) 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.

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 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.

[[Page 37253]]

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2011-12-51 Dassault Aviation: Amendment 39-16735; Docket No. FAA-
2011-0477; Directorate Identifier 2011-NM-108-AD.

Effective Date

    (a) This AD is effective July 12, 2011 to all persons except 
those persons to whom it was made immediately effective by Emergency 
AD 2011-12-51, issued on May 27, 2011, which contained the 
requirements of this amendment.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Dassault Aviation Model FALCON 7X 
airplanes, certificated in any category, all serial numbers.

Subject

    (d) Joint Aircraft System Component (JASC)/Air Transport 
Association (ATA) of America Code 27: Flight controls.

Unsafe Condition

    (e) This AD was prompted by a report of an uncontrolled pitch 
trim runaway during descent. We are issuing this AD to prevent loss 
of control of the airplane.

Compliance

    (f) Comply with this AD within the compliance times specified, 
unless already done.

Flight Prohibited

    (g) As of the effective date of this AD, operation of the 
airplane is prohibited.

Special Flight Permit

    (h) Special flight permits, as described in Section 21.197 and 
Section 21.199 of the Federal Aviation Regulations (14 CFR 21.197 
and 21.199), are not allowed.

Alternative Methods of Compliance (AMOCs)

    (i)(1) The Manager, International Branch, Transport Airplane 
Directorate, FAA, has the authority to approve AMOCs for this AD, if 
requested using the procedures found in 14 CFR 39.19. In accordance 
with 14 CFR 39.19, send your request to your principal inspector or 
local Flight Standards District Office, as appropriate. If sending 
information directly to the manager of the International Branch, 
send it to the attention of the person identified in the Related 
Information section of this AD. Information may be e-mailed to: [email protected].
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.

Related Information

    (j)(1) For further information about this AD, contact Tom 
Rodriguez, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; phone: 425-227-1137; fax: 425-227-1149.
    (2) Refer to MCAI European Aviation Safety Agency (EASA) 
Emergency Airworthiness Directive 2011-0102-E, dated May 26, 2011, 
for related information.

Material Incorporated by Reference

    (k) None.

    Issued in Renton, Washington, on June 16, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2011-15989 Filed 6-24-11; 8:45 am]
BILLING CODE 4910-13-P


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The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T03:08:21.364801+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
d29609fb186006b4c3a7b061628c34a08e8476f4f3d854783a6f30ae58e9da04
Text SHA-256
f33e75dfd28adf62a5e760184048801427601c79688d397da93da632e3ffc263

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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.