[Federal Register Volume 71, Number 71 (Thursday, April 13, 2006)]
[Rules and Regulations]
[Pages 19114-19117]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 06-3540]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-24438; Directorate Identifier 2006-NM-061-AD; 
Amendment 39-14560; AD 2006-04-13 R1]
RIN 2120-AA64


Airworthiness Directives; Gulfstream Model GIV-X and GV-SP Series 
Airplanes

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

ACTION: Final rule; request for comments.

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SUMMARY: The FAA is revising an existing airworthiness directive (AD), 
which applies to certain Gulfstream Model GIV-X and GV-SP series 
airplanes. That AD currently requires revising the Limitations section 
of the airplane flight manual (AFM) by incorporating new procedures to 
follow in the event that the cockpit displays go blank or malfunction. 
This AD allows for the use of alternative AFM revisions for a certain 
subset of the existing applicability. This AD results from a report 
that all four of the cockpit flight panel display units simultaneously 
went blank during flight. We are issuing this AD to ensure that the 
flightcrew is advised of the appropriate procedures to follow in the 
event that the cockpit displays go blank or malfunction, which could 
result in a reduction of the flightcrew's situational awareness and 
possible loss of control of the airplane.

DATES: The effective date of this AD is March 13, 2006.
    On March 13, 2006 (71 FR 9436, February 24, 2006), the Director of 
the Federal Register approved the incorporation by reference of certain 
other publications.
    We must receive any comments on this AD by June 12, 2006.

ADDRESSES: Use one of the following addresses to submit comments on 
this AD:
     DOT Docket Web site: Go to http://dms.dot.gov and follow 
the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to http://www.regulations.gov and follow the instructions for sending your 
comments electronically.
     Mail: Docket Management Facility; U.S. Department of 
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, 
Washington, DC 20590.
     Fax: (202) 493-2251.
     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.
    Contact Gulfstream Aerospace Corporation, Technical Publications 
Dept., P.O. Box 2206, Savannah, Georgia 31402-2206, for service 
information identified in this AD.

FOR FURTHER INFORMATION CONTACT: Robert Chupka, Aerospace Engineer, 
Systems and Equipment Branch, ACE-119A, Atlanta Aircraft Certification 
Office, FAA, One Crown Center, 1895 Phoenix Boulevard, Suite 450, 
Atlanta, Georgia 30349; telephone (770) 703-6070; fax (770) 703-6097.

SUPPLEMENTARY INFORMATION:

Discussion

    On February 14, 2006, we issued AD 2006-04-13, amendment 39-14495 
(71 FR 9436, February 24, 2006). That AD applies to certain Gulfstream 
Model GIV-X and GV-SP series airplanes. That AD requires revising the 
Limitations section of the airplane flight manual (AFM) by 
incorporating new procedures to follow in the event that the cockpit 
displays go blank or malfunction. That AD resulted from a report that 
all four of the cockpit flight panel display units simultaneously went 
blank during flight. The actions specified in that AD are intended to 
ensure that the flightcrew is advised of the appropriate procedures to 
follow in the event that the cockpit displays go blank or malfunction, 
which could result in a reduction of the flightcrew's situational 
awareness and possible loss of control of the airplane.

Actions Since AD Was Issued

    Since we issued AD 2006-04-13, the European Aviation Safety Agency 
(EASA) informed us that the information contained in the Joint Aviation 
Authority (JAA) Gulfstream AFM revisions is considered acceptable for 
airplanes operated under and in accordance with the JAA and EASA 
regulations, supervision, and oversight, and should be added to the AD. 
We inadvertently omitted that information from AD 2006-04-13; 
therefore, we have added a new Note 2 to this AD to give credit for 
those revisions.

Relevant Service Information

    We have reviewed the revisions to the Limitations section of 
Gulfstream G350, G450, G500, and G550 AFMs, as listed in the table 
below:

                                            Gulfstream AFM Revisions
----------------------------------------------------------------------------------------------------------------
                                                                    Revision
       Affected airplane models                    AFM                level              Revision date
----------------------------------------------------------------------------------------------------------------
Model GIV-X...........................  Gulfstream G350..........           3  January 25, 2006.
                                        GAC-AC-JAA-G350-OPS-0001.
Model GIV-X...........................  Gulfstream G450..........           3  January 25, 2006.
                                        GAC-AC-JAA-G450-OPS-0001.
Model GV-SP...........................  Gulfstream G500..........           3  January 25, 2006.
                                        GAC-AC-JAA-G500-OPS-0001.

[[Page 19115]]

 
Model GV-SP...........................  Gulfstream G550..........           5  January 25, 2006.
                                        GAC-AC-JAA-G550-OPS-0001.
----------------------------------------------------------------------------------------------------------------

    The revisions describe procedures to follow in the event that all 
four cockpit flight panel display units simultaneously go blank or 
malfunction. The procedures include identifying the malfunctioning 
components and taking appropriate corrective action to return certain 
displays to a functional condition. The procedures also include weather 
minimums designed to mitigate the effects of display blanking events 
during takeoff or landing.

FAA's Determination and Requirements of This AD

    The unsafe condition described previously is likely to exist or 
develop on other airplanes of the same type design. For this reason, we 
are issuing this AD to revise AD 2006-04-13. This new AD retains the 
requirements of the existing AD. This AD also provides for 
accomplishing the actions specified in the AFM revisions described 
previously for a certain subset of the existing applicability.

Interim Action

    We consider this AD interim action. The manufacturer is currently 
developing a software modification that will address the unsafe 
condition identified in this AD, which will constitute terminating 
action for the AFM revisions required by this AD action. Once this 
modification is developed, approved, and available, we may consider 
additional rulemaking. However, the planned compliance time for the 
modification will allow enough time to provide notice and opportunity 
for prior public comment on the merits of the modification.

FAA's Determination of the Effective Date

    No airplane affected by this AD is currently on the U.S. Register. 
Therefore, providing notice and opportunity for public comment is 
unnecessary before this AD is issued, and this AD may be made effective 
in less than 30 days after it is published in the Federal Register.

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 in the ADDRESSES section. Include ``Docket No. FAA-2006-
24438; Directorate Identifier 2006-NM-061-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of the AD that might 
suggest a need to modify it.
    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 that 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 may review the DOT's complete Privacy Act Statement in the Federal 
Register published on April 11, 2000 (65 FR 19477-78), or you may visit 
http://dms.dot.gov.

Examining the Dockets

    You may 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 Docket Management System 
receives them.

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 and placed it in the AD docket. 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, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the FAA 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. The Federal Aviation Administration (FAA) amends Sec.  39.13

[[Page 19116]]

by removing amendment 39-14495 (71 FR 9436, February 24, 2006) and 
adding the following new airworthiness directive (AD):

2006-04-13 R1 Gulfstream Aerospace Corporation: Amendment 39-14560. 
Docket No. FAA-2006-24438; Directorate Identifier 2006-NM-061-AD.

Effective Date

    (a) The effective date of this AD is March 13, 2006.

Affected ADs

    (b) This AD revises AD 2006-04-13.

Applicability

    (c) This AD applies to Gulfstream Model GIV-X series airplanes, 
certificated in any category, serial numbers 4001 and subsequent; 
and Gulfstream Model GV-SP series airplanes, certificated in any 
category, serial numbers 5001 and subsequent; on which Gulfstream 
Modification ASC-904 or production equivalent has been incorporated.

Unsafe Condition

    (d) This AD results from a report that all four of the cockpit 
flight panel display units simultaneously went blank during flight. 
We are issuing this AD to ensure that the flightcrew is advised of 
the appropriate procedures to follow in the event that the cockpit 
displays go blank or malfunction, which could result in a reduction 
of the flightcrew's situational awareness and possible loss of 
control of the airplane.

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 (AFM) Revision

    (f) Except as provided by paragraph (g) of this AD: Within 10 
days after March 13, 2006 (the effective date of AD 2006-04-13), 
revise the Limitations section of the Gulfstream G350, G450, G500, 
and G550 AFMs to include the information in the applicable revision 
listed in Table 1 of this AD. Thereafter, operate the airplane 
according to the limitations and procedures in the applicable 
revision. Any further revisions to the AFM must contain the 
identical procedures in the Limitations section of the AFM revisions 
as required by this AD.

                   Table 1.--Gulfstream AFM Revisions
------------------------------------------------------------------------
       Affected airplane models            Applicable Gulfstream AFM
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Model GIV-X..........................  GAC-AC-G350-OPS-0001, as
                                        specified in Revision 6, dated
                                        January 24, 2006.
Model GIV-X..........................  GAC-AC-G450-OPS-0001, as
                                        specified in Revision 7, dated
                                        January 24, 2006.
Model GV-SP..........................  GAC-AC-G500-OPS-0001, as
                                        specified in Revision 13, dated
                                        January 24, 2006.
Model GV-SP..........................  GAC-AC-G550-OPS-0001, as
                                        specified in Revision 15, dated
                                        January 24, 2006.
------------------------------------------------------------------------


    Note 1: The actions required by paragraph (f) of this AD may be 
done by inserting a copy of the applicable Gulfstream revisions 
listed in Table 1 of this AD into the applicable AFM.


    Note 2: For airplanes that are operated under and in accordance 
with the Joint Aviation Authority (JAA)/European Aviation Safety 
Agency regulations, supervision, and oversight: Revising the 
Limitations section of the Gulfstream G350, G450, G500, and G550 
AFMs to include the information in the applicable revision listed in 
Table 2 of this AD is acceptable for compliance with the 
requirements of paragraph (f) of this AD.


                 Table 2.--JAA Gulfstream AFM Revisions
------------------------------------------------------------------------
       Affected airplane models            Applicable Gulfstream AFM
------------------------------------------------------------------------
Model GIV-X..........................  GAC-AC-JAA-G350-OPS-0001, as
                                        specified in Revision 3, dated
                                        January 25, 2006.
Model GIV-X..........................  GAC-AC-JAA-G450-OPS-0001, as
                                        specified in Revision 3, dated
                                        January 25, 2006.
Model GV-SP..........................  GAC-AC-JAA-G500-OPS-0001, as
                                        specified in Revision 3, dated
                                        January 25, 2006.
Model GV-SP..........................  GAC-AC-JAA-G550-OPS-0001, as
                                        specified in Revision 5, dated
                                        January 25, 2006.
------------------------------------------------------------------------

Alternative Methods of Compliance (AMOCs)

    (g)(1) The Manager, Atlanta Aircraft Certification Office, FAA, 
has the authority to approve AMOCs for this AD, if requested in 
accordance with the procedures found in 14 CFR 39.19.
    (2) Before using any AMOC approved in accordance with Sec.  
39.19 on any airplane to which the AMOC applies, notify the 
appropriate principal inspector in the FAA Flight Standards 
Certificate Holding District Office.

Material Incorporated by Reference

    (h) You must use the documents listed in Table 3 of this AD, as 
applicable, to perform the actions that are required by this AD, 
unless the AD specifies otherwise.
    (1) On March 13, 2006 (71 FR 9436, February 24, 2006), the 
Director of the Federal Register approved the incorporation by 
reference of the documents listed in Table 3 of this AD.
    (2) Contact Gulfstream Aerospace Corporation, Technical 
Publications Dept., P.O. Box 2206, Savannah, Georgia 31402-2206, for 
a copy of this service information. You may review copies at the 
Docket Management Facility, U.S. Department of Transportation, 400 
Seventh Street SW., Room PL-401, Nassif Building, Washington, DC; on 
the Internet at http://dms.dot.gov; or at the National Archives and 
Records Administration (NARA). For information on the availability 
of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

         Table 3.--Material Previously Incorporated by Reference
------------------------------------------------------------------------
                                  Revision
Gulfstream service information     level            Revision date
------------------------------------------------------------------------
Gulfstream G350 Airplane                  6  January 24, 2006.
 Flight Manual.
GAC-AC-G350-OPS-0001..........
Gulfstream G450...............            7  January 24, 2006.
GAC-AC-G450-OPS-0001..........
Gulfstream G500...............           13  January 24, 2006.
GAC-AC-G500-OPS-0001..........

[[Page 19117]]

 
Gulfstream G550...............           15  January 24, 2006.
GAC-AC-G550-OPS-0001..........
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    Issued in Renton, Washington, on April 5, 2006.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 06-3540 Filed 4-12-06; 8:45 am]
BILLING CODE 4910-13-P