Airworthiness Directives; Hawker Beechcraft Corporation Models B300 and B300C (C-12W) Airplanes, 23921-23923 [2011-10387]

Download as PDF Federal Register / Vol. 76, No. 83 / Friday, April 29, 2011 / Proposed Rules between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact Burl’s Aircraft, LLC, P.O. Box 671487, Chugiak, Alaska 99567–1487; phone: (907) 688–3715; fax (907) 688–5031; e-mail burl@biginalaska.com; Internet: https://www.burlac.com. You may review copies of the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (816) 329–4148. Examining the AD Docket You may examine the AD docket on the Internet at https:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket 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: Eric Wright, Aerospace Engineer, FAA, Anchorage Aircraft Certification Office, 222 W. 7th Ave., #14, Anchorage, Alaska 99513; telephone: (907) 271– 2648; fax: (907) 271–6365; e-mail: eric.wright@faa.gov. SUPPLEMENTARY INFORMATION: emcdonald on DSK2BSOYB1PROD with PROPOSALS Comments Invited We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2011–0318; Directorate Identifier 2010–CE–033–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD because of those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion FAA’s Determination We have considered the request and find it appropriate to extend the comment period to give all interested persons additional time to examine all data and the proposed requirements of the NPRM and submit comments. We determined that extending the comment period to 90 days will not compromise the safety of these airplanes. The comment period for Docket No. FAA–2011–0318; Directorate Identifier 2010–CE–033–AD is hereby extended to July 3, 2011. Since no portion of the NPRM or other regulatory information has been changed, the entire NPRM is not being republished. Issued in Kansas City, Missouri, on April 22, 2011. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2011–10383 Filed 4–28–11; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2011–0436; Directorate Identifier 2011–CE–009–AD] RIN 2120–AA64 Airworthiness Directives; Hawker Beechcraft Corporation Models B300 and B300C (C–12W) Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD would require inserting an update to SUMMARY: We issued an NPRM to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to all VerDate Mar<15>2010 Burl A. Rogers (type certificate previously held by William Brad Mitchell and Aeronca, Inc.) Models 15AC and S15AC airplanes. The NPRM published in the Federal Register on April 4, 2011 (76 FR 18454). The NPRM proposed to require repetitive inspections of the upper and lower main wing spar cap angles for cracks and/or corrosion and installing inspection access panels. The NPRM also proposed to require replacing the wing spar cap angles if moderate or severe corrosion is found and applying corrosion inhibitor. Since we issued the NPRM, we received a request to extend the comment period of the NPRM to 90 days. 17:59 Apr 28, 2011 Jkt 223001 PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 23921 the performance charts in the FAAapproved airplane flight manual and the pilot’s operating handbook, part number (P/N) 130–590031–245. This proposed AD was prompted by an error found in the take-off speeds and field lengths published in the FAA-approved airplane flight manual. We are proposing this AD to correct the published data in the airplane flight manual and the pilot’s operating handbook and ensure it corresponds with the published data in the pilot’s checklist. This condition, if not corrected, could result in a pilot taking off from shorter runways than required by the airplane if the airplane loses an engine after takeoff decision speed (V1). This could result in the airplane running out of runway before take-off can be accomplished. DATES: We must receive comments on this proposed AD by June 13, 2011. ADDRESSES: You may send comments by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: 202–493–2251. • 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. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, contact Hawker Beechcraft Corporation, 9709 East Central, Wichita, Kansas 67201; telephone: (316) 676–5034; fax: (316) 676–6614; Internet: https:// www.hawkerbeechcraft.com/ service_support/pubs/. You may review copies of the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (816) 329–4148. Examining the AD Docket You may examine the AD docket on the Internet at https:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (phone: 800–647–5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. E:\FR\FM\29APP1.SGM 29APP1 23922 Federal Register / Vol. 76, No. 83 / Friday, April 29, 2011 / Proposed Rules FOR FURTHER INFORMATION CONTACT: Jason Brys, Flight Test Engineer, FAA, Wichita Aircraft Certification Office (ACO), 1801 S. Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946–4100; fax: (316) 946–4107. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA– 2011–0436; Directorate Identifier 2011– CE–009–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD because of those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion We were notified by Hawker Beechcraft Corporation of an error found in the take-off speeds and field lengths published in the FAA-approved airplane flight manual. The required runway distances published in the current manual could be up to 320 feet shorter than what is necessary. Hawker Beechcraft Corporation determined data in the pilot’s checklist (P/N 130– 590031–273) was correct. This condition, if not corrected, could result in taking off from shorter runways than required by the airplane if the airplane loses an engine after takeoff decision speed (V1). This could result in the airplane running out of runway before take-off can be accomplished. Relevant Service Information We reviewed Hawker Beechcraft Corporation Temporary Change to the Pilot’s Operating Handbook and FAA– Approved Airplane Flight Manual, P/N 130–590031–245TC5, dated February 2011. The temporary change corrects the published data in the FAA-approved airplane flight manual and the pilot’s operating handbook. FAA’s Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. Proposed AD Requirements This proposed AD would require inserting an update to the performance charts in the FAA-approved airplane flight manual and the pilot’s operating handbook. Costs of Compliance We estimate that this proposed AD affects 46 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: ESTIMATED COSTS Cost per product Labor cost Parts cost AFM page replacement .................. emcdonald on DSK2BSOYB1PROD with PROPOSALS Action .5 work-hour × $85 per hour = $42.50. Not applicable ................................ 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 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 VerDate Mar<15>2010 16:52 Apr 28, 2011 Jkt 223001 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 this 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), (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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows: PO 00000 Frm 00009 Fmt 4702 Sfmt 4702 Cost on U.S. operators $42.50 $1,955 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 FAA amends § 39.13 by adding the following new airworthiness directive (AD): Hawker Beechcraft Corporation: Docket No. FAA–2011–0436; Directorate Identifier 2011–CE–009–AD. Comments Due Date (a) We must receive comments by June 13, 2011. Affected ADs (b) None. Applicability (c) This AD applies to Hawker Beechcraft Corporation Model B300 and B300C (C–12W) airplanes, all serial numbers, that: (1) Are certificated in any category; and (2) Are modified per Hawker Beechcraft Drawing 130M000030 or Kit Drawing 130– 4014 that incorporate Aircraft Flight Manual P/N 130–590031–245. E:\FR\FM\29APP1.SGM 29APP1 Federal Register / Vol. 76, No. 83 / Friday, April 29, 2011 / Proposed Rules Subject (d) Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 91, Charts. Unsafe Condition (e) This AD was prompted by an error that was discovered in the take-off speeds and field lengths published in the FAA-approved flight manual. We are proposing this AD to correct the published data in the airplane flight manual and the pilot’s operating handbook and ensure it corresponds with the published data in the pilot’s checklist. This condition, if not corrected, could result in taking off from shorter runways than required by the airplane if the airplane loses an engine after takeoff decision speed (V1). This could result in the airplane running out of runway before take-off can be accomplished. Compliance (f) Comply with this AD within the compliance times specified, unless already done. Action (g) Within 14 days after the effective date of this AD, insert Hawker Beechcraft Corporation Log of Temporary Changes, dated February 2011; and Hawker Beechcraft Corporation Temporary Change to the Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual, Part Number (P/N) 130–590031–245TC5, dated February 2011; into the airplanes Pilot’s Operating Handbook and FAA Approved Flight Manual, P/N 130–590031–245. The actions required by this paragraph may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9 (a)(1)–(4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417, 121.380, or 135.439. emcdonald on DSK2BSOYB1PROD with PROPOSALS Alternative Methods of Compliance (AMOCs) (h)(1) The Manager, Wichita Aircraft Certification Office (ACO), 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 ACO, send it to the attention of the person identified in the Related Information section of this AD. (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 (i) For more information about this AD, contact Jason Brys, Flight Test Engineer, FAA, Wichita ACO, 1801 S. Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946–4100; fax: (316) 946–4107. (j) For service information identified in this AD, contact Hawker Beechcraft Corporation, 9709 East Central, Wichita, Kansas 67201; telephone: (316) 676–5034; fax: (316) 676– VerDate Mar<15>2010 16:52 Apr 28, 2011 Jkt 223001 6614; Internet: https:// www.hawkerbeechcraft.com/service_support/ pubs/. You may review copies of the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (816) 329–4148. Issued in Kansas City, Missouri, on April 22, 2011. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2011–10387 Filed 4–28–11; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Pipeline and Hazardous Materials Safety Administration 49 CFR Part 177 [Docket No. PHMSA–2010–0227 (HM–256A)] RIN 2137–AE65 Hazardous Materials: Restricting the Use of Cellular Phones by Drivers of Commercial Motor Vehicles in Intrastate Commerce Pipeline and Hazardous Materials Safety Administration (PHMSA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The Pipeline and Hazardous Materials Safety Administration (PHMSA) proposes to restrict the use of hand-held mobile telephones, including hand-held cell phones, by drivers during the operation of a motor vehicle containing a quantity of hazardous materials requiring placarding under Part 172 of the 49 CFR or any quantity of a select agent or toxin listed in 42 CFR Part 73. Additionally, in accordance with requirements proposed by the Federal Motor Carrier Safety Administration (FMCSA), motor carriers are prohibited from requiring or allowing drivers of covered motor vehicles to engage in the use of handheld mobile telephones while driving. This rulemaking would improve health and safety on the Nation’s highways by reducing the prevalence of distracted driving-related crashes, fatalities, and injuries involving drivers of commercial motor vehicles. DATES: Comments must be received by June 28, 2011. ADDRESSES: You may submit comments identified by the docket number PHMSA–2010–0227 by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the SUMMARY: PO 00000 Frm 00010 Fmt 4702 Sfmt 4702 23923 online instructions for submitting comments. • Fax: (202) 493–2251. • Mail: Docket Operations, U.S. Department of Transportation, West Building, Ground Floor, Room W12– 140, Routing Symbol M–30, 1200 New Jersey Avenue, SE., Washington, DC 20590. • Hand Delivery: To Docket Operations; Room W12–140 on the ground floor of the West Building, 1200 New Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Instructions: All submissions must include the agency name and docket number for this rule. Note that all comments received will be posted without change, including any personal information provided. Please see the discussion of the Privacy Act below. Docket: For access to the docket to read background documents and comments received, go to https:// www.regulations.gov at any time or DOT’s Docket Operations Office (see ADDRESSES). FOR FURTHER INFORMATION CONTACT: Delmer Billings, Office of Hazardous Materials Safety, (202) 366–8553, Pipeline and Hazardous Materials Safety Administration, U.S. Department of Transportation, 1200 New Jersey Avenue, SE., Washington, DC 20590– 0001. SUPPLEMENTARY INFORMATION: I. Background A. US DOT Strategy The United States Department of Transportation (US DOT) is leading the effort to end the dangerous practice of distracted driving on our nation’s roadways and in other modes of transportation. Driver distraction can be defined as the voluntary or involuntary diversion of attention from the primary driving tasks due to an object, event, or person that shifts the attention away from the fundamental driving task. The US DOT has identified three main types of distraction that occur while operating a motor vehicle: 1. Visual—taking your eyes off of the road; 2. Manual—taking your hands off of the wheel; and 3. Cognitive—taking your mind off of driving. The US DOT is working across the spectrum with private and public entities to tackle distracted driving, and will lead by example. The individual agencies of the US DOT are working together to share knowledge, promote a E:\FR\FM\29APP1.SGM 29APP1

Agencies

[Federal Register Volume 76, Number 83 (Friday, April 29, 2011)]
[Proposed Rules]
[Pages 23921-23923]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-10387]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0436; Directorate Identifier 2011-CE-009-AD]
RIN 2120-AA64


Airworthiness Directives; Hawker Beechcraft Corporation Models 
B300 and B300C (C-12W) Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for the 
products listed above. This proposed AD would require inserting an 
update to the performance charts in the FAA-approved airplane flight 
manual and the pilot's operating handbook, part number (P/N) 130-
590031-245. This proposed AD was prompted by an error found in the 
take-off speeds and field lengths published in the FAA-approved 
airplane flight manual. We are proposing this AD to correct the 
published data in the airplane flight manual and the pilot's operating 
handbook and ensure it corresponds with the published data in the 
pilot's checklist. This condition, if not corrected, could result in a 
pilot taking off from shorter runways than required by the airplane if 
the airplane loses an engine after takeoff decision speed 
(V1). This could result in the airplane running out of 
runway before take-off can be accomplished.

DATES: We must receive comments on this proposed AD by June 13, 2011.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: 202-493-2251.
     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.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact 
Hawker Beechcraft Corporation, 9709 East Central, Wichita, Kansas 
67201; telephone: (316) 676-5034; fax: (316) 676-6614; Internet: 
https://www.hawkerbeechcraft.com/service_support/pubs/. You may review 
copies of the referenced service information at the FAA, Small Airplane 
Directorate, 901 Locust, Kansas City, MO 64106. For information on the 
availability of this material at the FAA, call (816) 329-4148.

Examining the AD Docket

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

[[Page 23922]]


FOR FURTHER INFORMATION CONTACT: Jason Brys, Flight Test Engineer, FAA, 
Wichita Aircraft Certification Office (ACO), 1801 S. Airport Road, Room 
100, Wichita, Kansas 67209; telephone: (316) 946-4100; fax: (316) 946-
4107.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under the ADDRESSES section. Include ``Docket No. FAA-2011-0436; 
Directorate Identifier 2011-CE-009-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD because of those comments.
    We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

Discussion

    We were notified by Hawker Beechcraft Corporation of an error found 
in the take-off speeds and field lengths published in the FAA-approved 
airplane flight manual. The required runway distances published in the 
current manual could be up to 320 feet shorter than what is necessary. 
Hawker Beechcraft Corporation determined data in the pilot's checklist 
(P/N 130-590031-273) was correct. This condition, if not corrected, 
could result in taking off from shorter runways than required by the 
airplane if the airplane loses an engine after takeoff decision speed 
(V1). This could result in the airplane running out of 
runway before take-off can be accomplished.

Relevant Service Information

    We reviewed Hawker Beechcraft Corporation Temporary Change to the 
Pilot's Operating Handbook and FAA-Approved Airplane Flight Manual, P/N 
130-590031-245TC5, dated February 2011. The temporary change corrects 
the published data in the FAA-approved airplane flight manual and the 
pilot's operating handbook.

FAA's Determination

    We are proposing this AD because we evaluated all the relevant 
information and determined the unsafe condition described previously is 
likely to exist or develop in other products of the same type design.

Proposed AD Requirements

    This proposed AD would require inserting an update to the 
performance charts in the FAA-approved airplane flight manual and the 
pilot's operating handbook.

Costs of Compliance

    We estimate that this proposed AD affects 46 airplanes of U.S. 
registry.
    We estimate the following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
              Action                      Labor cost             Parts cost           product        operators
----------------------------------------------------------------------------------------------------------------
AFM page replacement..............  .5 work-hour x $85     Not applicable.......          $42.50          $1,955
                                     per hour = $42.50.
----------------------------------------------------------------------------------------------------------------

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 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 this 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),
    (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.

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

Hawker Beechcraft Corporation: Docket No. FAA-2011-0436; Directorate 
Identifier 2011-CE-009-AD.

Comments Due Date

    (a) We must receive comments by June 13, 2011.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Hawker Beechcraft Corporation Model B300 
and B300C (C-12W) airplanes, all serial numbers, that:
    (1) Are certificated in any category; and
    (2) Are modified per Hawker Beechcraft Drawing 130M000030 or Kit 
Drawing 130-4014 that incorporate Aircraft Flight Manual P/N 130-
590031-245.

[[Page 23923]]

Subject

    (d) Joint Aircraft System Component (JASC)/Air Transport 
Association (ATA) of America Code 91, Charts.

Unsafe Condition

    (e) This AD was prompted by an error that was discovered in the 
take-off speeds and field lengths published in the FAA-approved 
flight manual. We are proposing this AD to correct the published 
data in the airplane flight manual and the pilot's operating 
handbook and ensure it corresponds with the published data in the 
pilot's checklist. This condition, if not corrected, could result in 
taking off from shorter runways than required by the airplane if the 
airplane loses an engine after takeoff decision speed 
(V1). This could result in the airplane running out of 
runway before take-off can be accomplished.

Compliance

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

Action

    (g) Within 14 days after the effective date of this AD, insert 
Hawker Beechcraft Corporation Log of Temporary Changes, dated 
February 2011; and Hawker Beechcraft Corporation Temporary Change to 
the Pilot's Operating Handbook and FAA Approved Airplane Flight 
Manual, Part Number (P/N) 130-590031-245TC5, dated February 2011; 
into the airplanes Pilot's Operating Handbook and FAA Approved 
Flight Manual, P/N 130-590031-245. The actions required by this 
paragraph may be performed by the owner/operator (pilot) holding at 
least a private pilot certificate and must be entered into the 
aircraft records showing compliance with this AD in accordance with 
14 CFR 43.9 (a)(1)-(4) and 14 CFR 91.417(a)(2)(v). The record must 
be maintained as required by 14 CFR 91.417, 121.380, or 135.439.

Alternative Methods of Compliance (AMOCs)

    (h)(1) The Manager, Wichita Aircraft Certification Office (ACO), 
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 ACO, send it to the 
attention of the person identified in the Related Information 
section of this AD.
    (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

    (i) For more information about this AD, contact Jason Brys, 
Flight Test Engineer, FAA, Wichita ACO, 1801 S. Airport Road, Room 
100, Wichita, Kansas 67209; telephone: (316) 946-4100; fax: (316) 
946-4107.
    (j) For service information identified in this AD, contact 
Hawker Beechcraft Corporation, 9709 East Central, Wichita, Kansas 
67201; telephone: (316) 676-5034; fax: (316) 676-6614; Internet: 
https://www.hawkerbeechcraft.com/service_support/pubs/. You may 
review copies of the referenced service information at the FAA, 
Small Airplane Directorate, 901 Locust, Kansas City, MO 64106. For 
information on the availability of this material at the FAA, call 
(816) 329-4148.

    Issued in Kansas City, Missouri, on April 22, 2011.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2011-10387 Filed 4-28-11; 8:45 am]
BILLING CODE 4910-13-P
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