Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 Airplanes, 295-297 [E5-8241]

Download as PDF Federal Register / Vol. 71, No. 2 / Wednesday, January 4, 2006 / Proposed Rules products identified in this rulemaking action. Regulatory Findings We have determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 proposed 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 proposed 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, Safety. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows: 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. § 39.13 [Amended] 2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD): Fokker Services B.V.: Docket No. FAA– 2005–23476; Directorate Identifier 2005– NM–204–AD. wwhite on PROD1PC65 with PROPOSAL Comments Due Date (a) The FAA must receive comments on this AD action by February 3, 2006. Affected ADs (b) None. Applicability (c) This AD applies to Fokker Model F.28 Mark 0070 and 0100 airplanes, certificated in any category; equipped with Messier-Dowty Main Landing Gears (MLGs). VerDate Aug<31>2005 16:23 Jan 03, 2006 Jkt 208001 Unsafe Condition (d) This AD results from a report that an MLG main fitting failed on an airplane that was braking while moving backward. We are issuing this AD to detect and correct cracks in the MLG main fitting, which could result in reduced structural integrity of the MLG main fitting. 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 and Placard Installation (f) Within 14 days after the effective date of this AD, amend the Limitations Section of the AFM to prohibit application of brakes during backward movement of the airplane. This may be done by inserting a copy of this AD in the AFM. Note 1: When a statement to prohibit application of brakes during backward movement of the airplane 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. (g) Within 14 days after the effective date of this AD, affix a placard on the pedestal, next to the parking brake handle, having the following wording: ‘‘Applicaction of Brakes During Backward Movement Is Prohibited.’’ Inspection and Corrective Action (h) At the applicable time specified in paragraph (h)(1) or (h)(2) of this AD: Do an eddy current inspection of the MLG main fittings and repair before further flight as applicable, in accordance with the Accomplishment Instructions of MessierDowty Service Bulletin F100–32–106, dated February 18, 2005, including Appendices A through D, except as provided by paragraphs (i) and (j) of this AD. (1) For airplanes on which an inspection has not been done in accordance with Messier-Dowty Service Bulletin F100–32– 104, Revision 2, dated October 30, 2003: Within 3 months after the effective date of this AD. (2) For airplanes on which an inspection has been done in accordance with MessierDowty Service Bulletin F100–32–104, Revision 2, dated October 30, 2003: Within 2,000 flight cycles since the last inspection done in accordance with the service bulletin or within 3 months after the effective date of this AD, whichever occurs later. Exceptions to the Service Bulletin (i) Where Fokker Service Bulletin F100– 32–106, dated February 18, 2005, including Appendices A through D, specifies contacting the manufacturer for repair: Before further flight, repair using a method approved by either the Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA; or the Civil Aviation Authority—The Netherlands (CAA– NL) (or its delegated agent). (j) Although Fokker Service Bulletin F100– 32–106, dated February 18, 2005, including Appendices A through D, specifies to submit PO 00000 Frm 00021 Fmt 4702 Sfmt 4702 295 certain information to the manufacturer, this AD does not include that requirement. Parts Installation (k) As of the effective date of this AD, no person may install, on any airplane, a Messier-Dowty MLG, unless it has been inspected/repaired according to paragraph (h) of this AD. Alternative Methods of Compliance (AMOCs) (l)(1) The Manager, International Branch, ANM–116, 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 § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (m) Dutch airworthiness directives 2002– 115/2, dated October 8, 2004; and NL–2005– 002, dated April 14, 2005, also address the subject of this AD. Issued in Renton, Washington, on December 27, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E5–8240 Filed 1–3–06; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2005–23478; Directorate Identifier 2005–NM–175–AD] RIN 2120–AA64 Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Notice of proposed rulemaking (NPRM). AGENCY: SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) for all Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 airplanes. This proposed AD would require revising the Limitations section of the airplane flight manual (AFM) by incorporating revised takeoff performance tables. This proposed AD results from a correction of the power setting logic and table limits in the performance model by the engine manufacturer. We are proposing this AD to ensure that the flightcrew is provided E:\FR\FM\04JAP1.SGM 04JAP1 296 Federal Register / Vol. 71, No. 2 / Wednesday, January 4, 2006 / Proposed Rules with correct information to ensure a safe takeoff at certain altitudes. DATES: We must receive comments on this proposed AD by February 3, 2006. ADDRESSES: Use one of the following addresses to submit comments on this proposed AD. • DOT Docket Web site: Go to https://dms.dot.gov and follow the instructions for sending your comments electronically. • Government-wide rulemaking Web site: Go to https://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, P.O. Box 2206, Mail Station D–25, Savannah, Georgia 31402– 2206, for service information identified in this proposed AD. FOR FURTHER INFORMATION CONTACT: Mike Borfitz, Aerospace Engineer, International Branch, ANM–116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 227–2677; fax (425) 227–1149. SUPPLEMENTARY INFORMATION: wwhite on PROD1PC65 with PROPOSAL Comments Invited We invite you to submit any relevant written data, views, or arguments regarding this proposed AD. Send your comments to an address listed in the ADDRESSES section. Include the docket number ‘‘FAA–2005–23478; Directorate Identifier 2005–NM–175–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the proposed AD. We will consider all comments received by the closing date and may amend the proposed AD in light of those comments. We will post all comments we receive, without change, to https:// 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 proposed 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, VerDate Aug<31>2005 16:23 Jan 03, 2006 Jkt 208001 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 https:// dms.dot.gov. Examining the Docket You may examine the AD docket on the Internet at https://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. Discussion The Civil Aviation Administration of Israel (CAAI), which is the airworthiness authority for Israel, notified us that an unsafe condition may exist on Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 airplanes. The CAAI advises that the engine manufacturer has corrected the power setting logic and table limits in the performance model. This correction was necessary to bring the model in line with the control software currently installed in the Full Authority Digital Engine Control (FADEC). The new power setting logic sets lower takeoff and automatic performance reserve (APR) N1 values. This applies to elevations of 6,000 feet and higher when outside air temperature (OAT) is below standard day conditions, as defined by the Instrumentation, Systems, and Automations Society (ISA). This correction is intended to ensure that the flightcrew is provided with correct information to ensure a safe takeoff at certain altitudes. Relevant Service Information Gulfstream Aerospace LP has issued Temporary Revision (TR) 7, dated August 18, 2003, to the Gulfstream 200 Airplane Flight Manual. The TR describes procedures for incorporating revised takeoff performance tables to prevent reduced balanced field length and single engine climb performance. Accomplishing the actions specified in the TR is intended to adequately address the unsafe condition. The CAAI mandated the service information and issued Israeli airworthiness directive 72–03–05–09, dated September 22, 2003, to ensure the continued airworthiness of these airplanes in Israel. PO 00000 Frm 00022 Fmt 4702 Sfmt 4702 FAA’s Determination and Requirements of the Proposed AD These airplane models are manufactured in Israel and are type certificated for operation in the United States under the provisions of § 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the applicable bilateral airworthiness agreement. Pursuant to this bilateral airworthiness agreement, the CAAI has kept the FAA informed of the situation described above. We have examined the CAAI’s findings, evaluated all pertinent information, and determined that we need to issue an AD for airplanes of this type design that are certificated for operation in the United States. Therefore, we are proposing this AD, which would require accomplishing the actions specified in the service information described previously. Costs of Compliance This proposed AD would affect about 82 airplanes of U.S. registry. The proposed AFM revision would take about 1 work hour per airplane, at an average labor rate of $65 per work hour. Based on these figures, the estimated cost of the proposed AD for U.S. operators is $5,330, or $65 per airplane. 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 proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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. E:\FR\FM\04JAP1.SGM 04JAP1 Federal Register / Vol. 71, No. 2 / Wednesday, January 4, 2006 / Proposed Rules For the reasons discussed above, I certify that the proposed 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 proposed 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, Safety. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES Authority: 49 U.S.C. 106(g), 40113, 44701. [Amended] 2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD): Gulfstream Aerospace LP (Formerly Israel Aircraft Industries, Ltd.): Docket No. FAA–2005–23478; Directorate Identifier 2005–NM–175–AD. BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION 14 CFR Part 39 [Docket No. FAA–2005–23477; Directorate Identifier 2005–NM–181–AD] Affected ADs (b) None. RIN 2120–AA64 Applicability (c) This AD applies to all Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 airplanes, certificated in any category. wwhite on PROD1PC65 with PROPOSAL Issued in Renton, Washington, on December 20, 2005. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E5–8241 Filed 1–3–06; 8:45 am] Federal Aviation Administration Comments Due Date (a) The FAA must receive comments on this AD action by February 3, 2006. Unsafe Condition (d) This AD results from an engine performance modification done by the engine manufacturer. We are issuing this AD to ensure that the flightcrew is provided with correct information to ensure a safe takeoff at certain altitudes. 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. VerDate Aug<31>2005 Alternative Methods of Compliance (AMOCs) (g)(1) The Manager, International Branch, 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. (2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (h) Israeli airworthiness directive 72–03– 05–09, dated September 22, 2003, also addresses the subject of this AD. 1. The authority citation for part 39 continues to read as follows: § 39.13 Airplane Flight Manual (AFM) Revision (f) Within 50 flight hours after the effective date of this AD: Revise the Limitations section of the Gulfstream 200 AFM, to include the information in Gulfstream Temporary Revision (TR) 7, dated August 18, 2003, as specified in the TR. The TR includes procedures for incorporating revised takeoff performance tables. Thereafter, operate the airplane according to the limitations and procedures in the TR. This may be done by inserting a copy of Gulfstream TR 7 in the AFM. When the TR has been included in the general revisions of the AFM, the general revisions may be inserted in the AFM, provided the relevant information in the general revision is identical to that in Gulfstream TR 7. 16:23 Jan 03, 2006 Jkt 208001 Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146–RJ Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Notice of proposed rulemaking (NPRM). AGENCY: SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) for certain BAE Systems (Operations) Limited Model BAe 146 and Model Avro 146–RJ airplanes. This proposed AD would require a one-time detailed PO 00000 Frm 00023 Fmt 4702 Sfmt 4702 297 inspection for corrosion of the hinge bracket assembly of the left and right main landing gear (MLG) doors, and corrective action if necessary. This proposed AD results from in-service reports of hinge bracket failures on the MLG doors. We are proposing this AD to prevent failure of the hinge bracket on the MLG door, which could result in separation of the door, consequent structural damage to the airplane, and possible injury to people on the ground. DATES: We must receive comments on this proposed AD by February 3, 2006. ADDRESSES: Use one of the following addresses to submit comments on this proposed AD. • DOT Docket Web site: Go to https://dms.dot.gov and follow the instructions for sending your comments electronically. • Government-wide rulemaking Web site: Go to https://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 British Aerospace Regional Aircraft American Support, 13850 Mclearen Road, Herndon, Virginia 20171, for service information identified in this proposed AD. FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, International Branch, ANM–116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 227–2125; fax (425) 227–1149. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to submit any relevant written data, views, or arguments regarding this proposed AD. Send your comments to an address listed in the ADDRESSES section. Include the docket number ‘‘FAA–2005–23477; Directorate Identifier 2005–NM–181–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the proposed AD. We will consider all comments received by the closing date and may amend the proposed AD in light of those comments. We will post all comments we receive, without change, to https:// dms.dot.gov, including any personal E:\FR\FM\04JAP1.SGM 04JAP1

Agencies

[Federal Register Volume 71, Number 2 (Wednesday, January 4, 2006)]
[Proposed Rules]
[Pages 295-297]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E5-8241]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-23478; Directorate Identifier 2005-NM-175-AD]
RIN 2120-AA64


Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy 
and Model Gulfstream 200 Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for all Gulfstream Aerospace LP Model Galaxy and Model Gulfstream 200 
airplanes. This proposed AD would require revising the Limitations 
section of the airplane flight manual (AFM) by incorporating revised 
takeoff performance tables. This proposed AD results from a correction 
of the power setting logic and table limits in the performance model by 
the engine manufacturer. We are proposing this AD to ensure that the 
flightcrew is provided

[[Page 296]]

with correct information to ensure a safe takeoff at certain altitudes.

DATES: We must receive comments on this proposed AD by February 3, 
2006.

ADDRESSES: Use one of the following addresses to submit comments on 
this proposed AD.
     DOT Docket Web site: Go to https://dms.dot.gov and follow 
the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to https://
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, P.O. Box 2206, Mail 
Station D-25, Savannah, Georgia 31402-2206, for service information 
identified in this proposed AD.

FOR FURTHER INFORMATION CONTACT: Mike Borfitz, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2677; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to submit any relevant written data, views, or 
arguments regarding this proposed AD. Send your comments to an address 
listed in the ADDRESSES section. Include the docket number ``FAA-2005-
23478; Directorate Identifier 2005-NM-175-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of the proposed AD. We will 
consider all comments received by the closing date and may amend the 
proposed AD in light of those comments.
    We will post all comments we receive, without change, to https://
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 proposed 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 https://dms.dot.gov.

Examining the Docket

    You may examine the AD docket on the Internet at https://
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.

Discussion

    The Civil Aviation Administration of Israel (CAAI), which is the 
airworthiness authority for Israel, notified us that an unsafe 
condition may exist on Gulfstream Aerospace LP Model Galaxy and Model 
Gulfstream 200 airplanes. The CAAI advises that the engine manufacturer 
has corrected the power setting logic and table limits in the 
performance model. This correction was necessary to bring the model in 
line with the control software currently installed in the Full 
Authority Digital Engine Control (FADEC). The new power setting logic 
sets lower takeoff and automatic performance reserve (APR) N1 values. 
This applies to elevations of 6,000 feet and higher when outside air 
temperature (OAT) is below standard day conditions, as defined by the 
Instrumentation, Systems, and Automations Society (ISA). This 
correction is intended to ensure that the flightcrew is provided with 
correct information to ensure a safe takeoff at certain altitudes.

Relevant Service Information

    Gulfstream Aerospace LP has issued Temporary Revision (TR) 7, dated 
August 18, 2003, to the Gulfstream 200 Airplane Flight Manual. The TR 
describes procedures for incorporating revised takeoff performance 
tables to prevent reduced balanced field length and single engine climb 
performance. Accomplishing the actions specified in the TR is intended 
to adequately address the unsafe condition. The CAAI mandated the 
service information and issued Israeli airworthiness directive 72-03-
05-09, dated September 22, 2003, to ensure the continued airworthiness 
of these airplanes in Israel.

FAA's Determination and Requirements of the Proposed AD

    These airplane models are manufactured in Israel and are type 
certificated for operation in the United States under the provisions of 
Sec.  21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the 
applicable bilateral airworthiness agreement. Pursuant to this 
bilateral airworthiness agreement, the CAAI has kept the FAA informed 
of the situation described above. We have examined the CAAI's findings, 
evaluated all pertinent information, and determined that we need to 
issue an AD for airplanes of this type design that are certificated for 
operation in the United States.
    Therefore, we are proposing this AD, which would require 
accomplishing the actions specified in the service information 
described previously.

Costs of Compliance

    This proposed AD would affect about 82 airplanes of U.S. registry. 
The proposed AFM revision would take about 1 work hour per airplane, at 
an average labor rate of $65 per work hour. Based on these figures, the 
estimated cost of the proposed AD for U.S. operators is $5,330, or $65 
per airplane.

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 proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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.

[[Page 297]]

    For the reasons discussed above, I certify that the proposed 
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 proposed 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, Safety.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

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  [Amended]

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

Gulfstream Aerospace LP (Formerly Israel Aircraft Industries, Ltd.): 
Docket No. FAA-2005-23478; Directorate Identifier 2005-NM-175-AD.

Comments Due Date

    (a) The FAA must receive comments on this AD action by February 
3, 2006.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all Gulfstream Aerospace LP Model Galaxy 
and Model Gulfstream 200 airplanes, certificated in any category.

Unsafe Condition

    (d) This AD results from an engine performance modification done 
by the engine manufacturer. We are issuing this AD to ensure that 
the flightcrew is provided with correct information to ensure a safe 
takeoff at certain altitudes.

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) Within 50 flight hours after the effective date of this AD: 
Revise the Limitations section of the Gulfstream 200 AFM, to include 
the information in Gulfstream Temporary Revision (TR) 7, dated 
August 18, 2003, as specified in the TR. The TR includes procedures 
for incorporating revised takeoff performance tables. Thereafter, 
operate the airplane according to the limitations and procedures in 
the TR. This may be done by inserting a copy of Gulfstream TR 7 in 
the AFM. When the TR has been included in the general revisions of 
the AFM, the general revisions may be inserted in the AFM, provided 
the relevant information in the general revision is identical to 
that in Gulfstream TR 7.

Alternative Methods of Compliance (AMOCs)

    (g)(1) The Manager, International Branch, 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.
    (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.

Related Information

    (h) Israeli airworthiness directive 72-03-05-09, dated September 
22, 2003, also addresses the subject of this AD.

    Issued in Renton, Washington, on December 20, 2005.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E5-8241 Filed 1-3-06; 8:45 am]
BILLING CODE 4910-13-P

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