Unknown. Final rule; request for comments

5,198 words·~24 min read·/register/2001/12/06/01-30083·

A research copy — for the controlling text, always check the official state or federal source. Not legal advice.

--- schema: federal-register doc_type: fedreg source_file: FR-2001-12-06.xml --- 66 235 Thursday, December 6, 2001 Contents Agriculture Agriculture Department See Animal and Plant Health Inspection Service See Commodity Credit Corporation See Forest Service Amtrak Amtrak Reform Council NOTICES Meetings, 63359 01-30265 Animal Animal and Plant Health Inspection Service NOTICES Environmental statements; availability, etc.: North Dakota and South Dakota; sunflowers protection from red-winged blackbird damage; scoping document availability, 63356-63358 01-30258 Arts Arts and Humanities, National Foundation See National Foundation on the Arts and the Humanities Broadcasting Broadcasting Board of Governors NOTICES Meetings;

Sunshine Act, 63359 01-30346 Census Census Bureau NOTICES Surveys, determinations, etc. Manufacturing area; annual, 63360-63361 01-30256 Centers Centers for Medicare & Medicaid Services NOTICES Privacy Act: Systems of records, 63392-63400 01-30005 Commerce Commerce Department See Census Bureau See Export Administration Bureau See Foreign-Trade Zones Board See International Trade Administration See National Institute of Standards and Technology See National Oceanic and Atmospheric Administration See National Telecommunications and Information Administration See Patent and Trademark Office See Technology Administration NOTICES Agency information collection activities:

Submission for OMB review; comment request, 63359-63360 01-30294 01-30295 Commodity Commodity Credit Corporation PROPOSED RULES Conservation Reserve Program: Cropland eligibility and private sector technical assistance, 63339-63341 01-30213 Consumer Consumer Product Safety Commission NOTICES Settlement agreements: MTS Products, Inc., 63379-63381 01-30307 Defense Defense Department RULES Acquisition regulations: Multiyear contracting, 63336-63338 01-30264 Performance-based contracting, 63335-63336 01-30262 Technical amendments, 63334-63335 01-30263 PROPOSED RULES Acquisition regulations:

Research and development streamlined contracting procedures, 63348-63349 01-30261 Employment Employment and Training Administration NOTICES Grants and cooperative agreements, etc.: Workforce Investment Act— Disability Employment Program, 63415 01-30186 Energy Energy Department See Federal Energy Regulatory Commission NOTICES Grants and cooperative agreements; availability, etc.: Petroleum technologies applications on Native American and Alaskan Native Corporation properties for benefit of entire Tribe/Native Corporation, 63381-63382 01-30243 EPA Environmental Protection Agency RULES Air pollutants, hazardous; national emission standards:

Hazardous waste combustors, 63313-63318 01-30267 Air pollution control: State operating permits programs— Texas, 63318-63331 01-30270 Air quality implementation plans; approval and promulgation; various States: Connecticut, 63311-63313 01-30098 Antarctica; nongovernmental activities; environmental impact assessment; assessment and coordination requirements, 63453-63472 01-30268 Hazardous waste program authorizations: Indiana, 63331-63334 01-30269 PROPOSED RULES Air quality implementation plans; approval and promulgation; various States:

Maine, 63343-63348 01-30271 NOTICES Pesticide programs: Restricted use pesticides; applicators certification; State plans— Nebraska, 63389-63390 01-30273 MISSING FOR: Export Administration Bureau Export Administration Bureau NOTICES Agency information collection activities: Proposed collection; comment request, 63361-63362 01-30296 FAA Federal Aviation Administration RULES Air traffic operating and flight rules, etc.: Criminal history records checks, 63473-63486 01-30282 Airworthiness directives:

Raytheon, 63307-63310 01-30083 Restricted areas; correction, 63433 C1-27159 PROPOSED RULES Airworthiness directives: Rolls-Royce plc, 63341-63343 01-30266 NOTICES Airport noise compatibility program: Hilo International Airport, HI, 63424-63425 01-30281 FCC Federal Communications Commission NOTICES Agency information collection activities: Proposed collection; comment request, 63390 01-30245 FDIC Federal Deposit Insurance Corporation NOTICES Meetings; Sunshine Act, 63390-63391 01-30345 Federal Election Federal Election Commission NOTICES Meetings;

Sunshine Act, 63391 01-30347 Federal Energy Federal Energy Regulatory Commission NOTICES Electric rate and corporate regulation filings: Bluegrass Generation Co., L.L.C., et al., 63383-63385 01-30217 Hydroelectric applications, 63385-63389 01-30249 01-30250 01-30251 01-30252 *Applications, hearings, determinations, etc.:* Dominion Transmission, Inc., 01-30253 63382-63383 01-30254 Sithe/Independence Power Partners, L.P., 63383 01-30255 Federal Highway Federal Highway Administration NOTICES Agency information collection activities:

Submission for OMB review; comment request, 63426 01-30280 FMC Federal Maritime Commission NOTICES Agreements filed, etc., 63391 01-30180 Ocean transportation intermediary licenses: George J. Young & Co., 63391 01-30179 International Services Corp., 63391-63392 01-30181 Federal Reserve Federal Reserve System NOTICES Meetings; Sunshine Act, 63392 01-30321 Fish Fish and Wildlife Service PROPOSED RULES Migratory bird permits: Rehabilitation activities and permit exceptions, 63349-63355 01-30297 NOTICES Marine mammal permit applications, 63402 01-30257 MISSING FOR:

Foreign-Trade Zones Board Foreign-Trade Zones Board NOTICES *Applications, hearings, determinations, etc.:* California Ultramar Diamond Shamrock Corp.; oil refinery complex, 63362 01-30289 Forest Forest Service NOTICES Environmental statements; notice of intent: Florida National Forests, 63358 01-30237 Winema National Forest, OR; cancellation, 63358 01-30235 Health Health and Human Services Department See Centers for Medicare & Medicaid Services See Health Resources and Services Administration See Substance Abuse and Mental Health Services Administration Health Health Resources and Services Administration NOTICES Organization, functions, and authority delegations:

Telehealth Advancement Office et al., 63400-63401 01-30233 Housing Housing and Urban Development Department RULES Multifamily properties; civil money penalties, 63435-63443 01-30033 Interior Interior Department See Fish and Wildlife Service See Land Management Bureau See National Park Service International International Trade Administration NOTICES Antidumping: Brake rotors from— China, 63362-63363 01-30284 Iron construction castings from— Canada, 63363 01-30283 Stainless steel sheet and strip in coils from— Japan, 63364 01-30287 Steel concrete reinforcing bars from— Turkey, 63364-63365 01-30285 Structural steel beams from— Japan, 63365-63368 01-30286 Welded large diameter line pipe from— Japan, 63368-63369 01-30288 International International Trade Commission NOTICES Import investigations:

Integrated circuits, processes for making same, and products containing same, 63409-63410 01-30275 Network interface cards and access points for use in direct sequence spread spectrum wireless local area networks and products containing same, 63410 01-30276 Labor Labor Department See Employment and Training Administration NOTICES Agency information collection activities: Submission for OMB review; comment request, 63410-63414 01-30187 01-30218 01-30219 Land Land Management Bureau RULES Minerals management:

Mineral materials disposal; sales; free use Correction, 63334 01-30231 NOTICES Environmental statements; availability, etc.: Andrews Resource Area and Steens Mountain Cooperative Management and Protection Area, OR, 63402-63404 01-30222 Environmental statements; notice of intent: Jack Morrow Hills Area, WY, 63404-63405 01-30277 Oil and gas leases: Wyoming, 63405 01-30224 01-30225 01-30226 Organization, functions, and authority delegations: Oregon and Washington State Office move, 63405 01-30229 Realty actions; sales, leases, etc.:

Nevada, 63405-63406 01-30227 Resource management plans, etc.: Black Rock Desert-High Rock Canyon Emigrant Trails National Conservation Area et al., NV, 63406-63407 01-30223 Survey plat filings: Missouri, 63407-63408 01-30228 Withdrawal and reservation of lands: New Mexico, 63408 01-30230 Legal Legal Services Corporation NOTICES Grants and cooperative agreements; availability, etc.: Civil legal services to poor— Louisiana, 63415 01-30248 National National Council on Disability NOTICES Meetings;

Sunshine Act, 63415-63416 01-30340 National Foundation National Foundation on the Arts and the Humanities NOTICES Meetings: International Exhibitions Federal Advisory Committee, 63416 01-30214 National Institute National Institute of Standards and Technology NOTICES Information processing standards, Federal: Advanced Encryption Standard, 63369-63371 01-30232 National Labor National Labor Relations Board NOTICES Organization, functions, and authority delegations: Deputy General Counsel, 63416-63417 01-30305 NOAA National Oceanic and Atmospheric Administration NOTICES Agency information collection activities:

Proposed collection; comment request, 01-30291 63371-63373 01-30292 01-30293 National Park National Park Service NOTICES Environmental statements; availability, etc.: Cane River Creole National Historic Park, LA; general management plan, 63408-63409 01-30240 National Science National Science Foundation NOTICES Antarctic Conservation Act of 1978; permit applications, etc., 63417 01-30220 National Telecommunications National Telecommunications and Information Administration NOTICES Grants and cooperative agreements; availability, etc.:

Technology Opportunities Program, 63373-63378 01-30172 Nuclear Nuclear Regulatory Commission NOTICES Environmental statements; availability, etc.: Exelon Generation Co., LLC, 63417-63418 01-30238 University of Virginia Research Reactor, 63418-63419 01-30239 Patent Patent and Trademark Office NOTICES Agency information collection activities: Proposed collection; comment request, 63378-63379 01-30212 Personnel Personnel Management Office NOTICES Agency information collection activities:

Submission for OMB review; comment request, 63419-63420 01-30246 01-30247 Public Public Health Service See Health Resources and Services Administration See Substance Abuse and Mental Health Services Administration SEC Securities and Exchange Commission NOTICES Agency information collection activities: Proposed collection; comment request, 63420-63421 01-30215 Investment Company Act of 1940: Deregistration applications— Vanguard Preferred Stock Fund et al., 63421-63422 01-30216 Meetings;

Sunshine Act, 63422-63423 01-30326 Self-regulatory organizations; proposed rule changes: International Securities Exchange LLC, 63423-63424 01-30274 Substance Substance Abuse and Mental Health Services Administration NOTICES Agency information collection activities: Proposed collection; comment request, 63401-63402 01-30234 Technology Technology Administration NOTICES Meetings: Digital entertainment and rights management; workshop, 63379 01-30221 Transportation Transportation Department See Federal Aviation Administration See Federal Highway Administration Treasury Treasury Department NOTICES Agency information collection activities:

Proposed collection; comment request; correction, 63433 C1-27268 Veterans Veterans Affairs Department RULES Medical benefits: Copayments for medications, 63448-63451 01-30183 Inpatient hospital care and outpatient medical care; copayments, 63445-63449 01-30182 NOTICES Privacy Act: Systems of records, 63426-63432 01-30241 Separate Parts In This Issue Part II Housing and Urban Development Department, 63435-63443 01-30033 Part III Veterans Affairs Department, 63445-63451 01-30182 01-30183 Part IV Environmental Protection Agency, 63453-63472 01-30268 Part V Transportation Department, Federal Aviation Administration, 63473-63486 01-30282 Reader Aids Consult the Reader Aids section at the end of this issue for phone numbers, online resources, finding aids, reminders, and notice of recently enacted public laws.

To subscribe to the Federal Register Table of Contents LISTSERV electronic mailing list, go to http://listserv.access.gpo.gov and select Online mailing list archives, FEDREGTOC-L, Join or leave the list (or change settings); then follow the instructions. 66 235 Thursday, December 6, 2001 Rules and Regulations DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-347-AD; Amendment 39-12528; AD 2001-24-11] RIN 2120-AA64 Airworthiness Directives;

Raytheon Model Beech 400, 400A, and 400T Series Airplanes, Model Mitsubishi MU-300 Airplanes, and Model Beech MU-300-10 Airplanes AGENCY: Federal Aviation Administration, DOT. ACTION: Final rule; request for comments. SUMMARY: This amendment adopts a new airworthiness directive

(AD)that is applicable to all Raytheon Model Beech 400, 400A, and 400T series airplanes, Model Mitsubishi MU-300 airplanes, and Model Beech MU-300-10 airplanes. This action requires revising the Emergency Procedures Section of the Airplane Flight Manual to ensure the flightcrew is advised of in-flight procedures in the event of loss of airspeed indication. Such loss of airspeed indication and the resulting adverse effects on certain connecting systems could result in reduced controllability of the airplane. DATES: Effective December 11, 2001. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of December 11, 2001. Comments for inclusion in the Rules Docket must be received on or before February 4, 2002. ADDRESSES: Submit comments in triplicate to the Federal Aviation Administration (FAA), Transport Airplane Directorate, ANM-114, Attention: Rules Docket No. 2001-NM-347-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056. Comments may be inspected at this location between 9 a.m. and 3 p.m., Monday through Friday, except Federal holidays. Comments may be submitted via fax to

(425)227-1232. Comments may also be sent via the Internet using the following address: *9-anm-iarcomment@faa.gov.* Comments sent via fax or the Internet must contain “Docket No. 2001-NM-347-AD” in the subject line and need not be submitted in triplicate. Comments sent via the Internet as attached electronic files must be formatted in Microsoft Word 97 for Windows or ASCII text. The service information referenced in this AD may be obtained from Raytheon Aircraft Company, Department 62, P.O. Box 85, Wichita, Kansas 67201-0085. This information may be examined at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. FOR FURTHER INFORMATION CONTACT: Bennett Sorensen, Aerospace Engineer, Flight Test Branch, ACE-117W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone

(316)946-4165; fax

(316)946-4407. SUPPLEMENTARY INFORMATION: The FAA has received several reports of loss of the pilot's and/or the co-pilot's Indicated Airspeed

(IAS)display on certain Raytheon Model Beech 400A series airplanes. Such loss of IAS display may lead to loss of the altitude displays and up to 10 degrees of pitch error in the pilot's and/or co-pilot's attitude display. Loss of the Indicated Airspeed

(IAS)display can also adversely affect the display for altitude and attitude (Attitude/Heading/Reference System (AHRS)), and can result in uncommanded autopilot or yaw damper disengagement. The reported incidents occurred between 38,000 and 41,000 feet of altitude while the airplanes were in cruise or during initial descent. In the reported incidents, the altitude indication returned to normal at an undetermined point in the descent, and the airplanes landed without further incident. Investigation of those reports indicates that the cause of the loss of airspeed indication display may be due to water freezing in the pitot systems. Loss of airspeed indication and the resulting adverse effects on certain connecting systems could result in reduced controllability of the airplane. Similar Models The pitot systems installation on Raytheon Model Beech 400, and 400T series airplanes, Model Mitsubishi MU-300 airplanes, and Model Beech MU-300-10 airplanes are identical to those installed on the affected Model Beech 400A series airplanes. Therefore, all of these models may be subject to the same unsafe condition. Explanation of Relevant Service Information The FAA has reviewed and approved the following Raytheon Temporary Changes to the FAA-approved Airplane Flight Manual: • Beechjet 400T Temporary Change, P/N 132-590002-5TC3, dated November 12, 2001; • Beechjet 400T Temporary Change, P/N 134-590002-1TC3, dated November 12, 2001; • Beechjet 400A Temporary Change, P/N 128-590001-91TC5, dated November 12, 2001; • Beechjet 400A Temporary Change, P/N 128-590001-95TC5, dated November 12, 2001; • Beechjet 400A Temporary Change, P/N 128-590001-107TC5, dated November 12, 2001; • Beechjet 400A Temporary Change, P/N 128-590001-109TC5, dated November 12, 2001; • Beechjet 400A Temporary Change, P/N 128-590001-167TC7, dated November 12, 2001; • Beechjet 400A Temporary Change, P/N 128-590001-169TC3, dated November 12, 2001; • Beechjet 400 Temporary Change, P/N 128-590001-13BTC1, dated November 12, 2001; • Beechjet 400 Temporary Change P/N 128-590001-13BTC2, dated November 12, 2001; • MU-300 Diamond I Temporary Change, P/N MR-0460TC1, dated November 12, 2001; • MU-300 Diamond IA Temporary Change, P/N MR-0873TC1, dated November 12, 2001. The documents specified above describe certain in-flight procedures in the event of loss of airspeed indication for the various models specified. Explanation of the Requirements of the Rule Since an unsafe condition has been identified that is likely to exist or develop on other airplanes of the same type design, this AD is being issued to ensure the flightcrew is advised of in-flight procedures in the event of loss of airspeed indication. Such loss of airspeed indication and the resulting adverse effects of certain connecting systems could result in reduced controllability of the airplane. This AD requires accomplishment of the actions specified in the Temporary AFM's described previously, or insertion of this AD into the Airplane Flight Manual (AFM). Interim Action This is considered to be interim action until final action is identified, at which time the FAA may consider further rulemaking. Determination of Rule's Effective Date Since a situation exists that requires the immediate adoption of this regulation, it is found that notice and opportunity for prior public comment hereon are impracticable, and that good cause exists for making this amendment effective in less than 30 days. Comments Invited Although this action is in the form of a final rule that involves requirements affecting flight safety and, thus, was not preceded by notice and an opportunity for public comment, comments are invited on this rule. Interested persons are invited to comment on this rule by submitting such written data, views, or arguments as they may desire. Communications shall identify the Rules Docket number and be submitted in triplicate to the address specified under the caption ADDRESSES. All communications received on or before the closing date for comments will be considered, and this rule may be amended in light of the comments received. Factual information that supports the commenter's ideas and suggestions is extremely helpful in evaluating the effectiveness of the AD action and determining whether additional rulemaking action would be needed. Submit comments using the following format: • Organize comments issue-by-issue. For example, discuss a request to change the compliance time and a request to change the service bulletin reference as two separate issues. • For each issue, state what specific change to the AD is being requested. • Include justification ( *e.g.,* reasons or data) for each request. Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify the rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report that summarizes each FAA-public contact concerned with the substance of this AD will be filed in the Rules Docket. Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this rule must submit a self-addressed, stamped postcard on which the following statement is made: “Comments to Docket Number 2001-NM-347-AD.” The postcard will be date stamped and returned to the commenter. Regulatory Impact The regulations adopted herein 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. Therefore, it is determined that this final rule does not have federalism implications under Executive Order 13132. The FAA has determined that this regulation is an emergency regulation that must be issued immediately to correct an unsafe condition in aircraft, and that it is not a “significant regulatory action” under Executive Order 12866. It has been determined further that this action involves an emergency regulation under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). If it is determined that this emergency regulation otherwise would be significant under DOT Regulatory Policies and Procedures, a final regulatory evaluation will be prepared and placed in the Rules Docket. A copy of it, if filed, may be obtained from the Rules Docket at the location provided under the caption ADDRESSES. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (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. Section 39.13 is amended by adding the following new airworthiness directive: **2001-24-11 Raytheon Aircraft Company** (Formerly Beech): Amendment 39-12528. Docket 2001-NM-347-AD. *Applicability:* All Model Beech 400, 400A, and 400T series airplanes, Model Mitsubishi MU-300 airplanes, and Model Beech MU-300-10 airplanes; certificated in any category. *Compliance:* Required as indicated, unless accomplished previously. To prevent reduced controllability of the airplane due to loss of airspeed indication by ensuring that the flightcrew is advised of in-flight procedures in the event of loss of airspeed indication, accomplish the following:

(a)Within five days after the effective date of this AD, revise the Emergency Procedures Section of the FAA-approved Airplane Flight Manual (AFM), as applicable, by inserting a copy of Raytheon Beechjet 400T Temporary Change, P/N 132-590002-5TC3, dated November 12, 2001; Beechjet 400T Temporary Change, P/N 134-590002-1TC3, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-91TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-95TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-107TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-109TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-167TC7, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-169TC3, dated November 12, 2001; Beechjet 400 Temporary Change, P/N 128-590001-13BTC1, dated November 12, 2001; Beechjet 400 Temporary Change P/N 128-590001-13BTC2, dated November 12, 2001; MU-300 Diamond I Temporary Change, P/N MR-0460TC1, dated November 12, 2001; or MU-300 Diamond IA Temporary Change, P/N MR-0873TC1, dated November 12, 2001; as applicable, into the AFM or by inserting a copy of this AD into the AFM to include the following procedures: “Emergency Procedures (400 & MU-300) Loss of Airspeed Note: If the pilot's and/or copilot's airspeed(s) are noted to be decreasing toward zero, refer to the AOA indicator for airspeed control and land at the nearest suitable airport. 1. Autopilot—Disconnect 2. Airspeed—Slow to and Maintain 0.2 AOA 3. Thrust—As Required 4. Speed Brakes—As Required (Slow to 0.25 AOA with speed brakes extended) Note: An AOA of 0.2 (0.25 with speed brakes extended) will yield an airspeed of about 210 knots. Use pitch attitude as the primary reference. Make small changes in pitch and wait for the AOA to stabilize. When Ready for Descent 5. Seat Belts/Shoulder Harnesses—Fastened 6. Cabin Sign—As Required 7. Recognition Light—As Required 8. Anti/De-Ice Systems—As Required Caution If icing conditions are anticipated during the descent and approach, turn ice protection systems ON as early as possible prior to penetrating clouds. Maintain wing anti/deice operation light ON (approximately 70% N2) during descent to assure proper wing anti-ice operation. 9. Cabin Pressure Control—Set Field Elevation + 500 Feet 10. Windshield Defog—As Required 11. Altimeters—Set When Ready for Approach 12. Airspeed—Slow to and Maintain 0.3 AOA Note: Maintain 0.3 AOA throughout the configuration change to Flaps 10° Gear Down. This will yield an airspeed of about 180 knots. 13. Fuel Management—Check 14. N1, Landing Distance—Confirm 15. Cabin Sign—Safety 16. Windshield Anti-Ice—Low 17. Hydraulic/Nitrogen Pressure—Check 18. Engine Sync—Off 19. Flaps 10° Before Landing 20. AOA Index—Preset 1.3 V/Vs 21. Landing Gear—Down 22. Airspeed—Slow to 0.4 AOA 23. Recognition Light—Off 24. Landing Lights—As Required 25. Ignitions—On 26. Flaps—30° 27. Approach Airspeed (VREF)—Slow to and Maintain 0.57 AOA Note: This will yield a normal approach speed of VREF (0.57 AOA) and normal landing distances. Balked Landing 28. Thrust—Takeoff N1 29. Pitch Attitude—10° When Positive Climb Has Been Established 30. Flaps—10° 31. Landing Gear—Up 32. Airspeed—Accelerate to 0.3 AOA 33. Flaps—Up 34. Airspeed—Accelerate and Maintain 0.2 AOA 35. Landing Lights—Ret/off Emergency Procedures (400A & RJ-61) Loss of Airspeed Note: If the pilot's, or copilot's and standby, or all three airspeed(s) are noted to be decreasing toward zero, refer to the standby attitude indicator, standby altimeter, standby heading and the AOA indicator for aircraft control and land at the nearest suitable airport. On PFD equipped airplanes, the pilot's and copilots altimeters, attitude displays and heading displays may be unreliable and the autopilot may disconnect. This may be accompanied by amber boxed A/S, ALT, ATT and/or HDG comparator flags. The comparator flags may be followed by red FAIL flags and removal of airspeed and altitude tapes and attitude/heading displays. 1. Autopilot—Disconnect 2. Airspeed—Slow to and Maintain 0.2 AOA 3. Thrust—As Required 4. Speed Brakes—As Required (Slow to 0.25 AOA with speed brakes extended) Note: An AOA of 0.2 (0.25 speed brakes extended) will yield an airspeed of about 210 knots. Use pitch attitude as primary reference. Make small changes in pitch attitude and wait for AOA to stabilize. When Ready for Descent 5. Seat Belts/Shoulder Harnesses—Fastened 6. Cabin Sign—As Required 7. Recognition Light—As Required 8. Anti/De-Ice Systems—As Required Caution If icing conditions are anticipated during the descent and approach, turn ice protection systems ON as early as possible prior to penetrating clouds. Maintain wing anti/deice operation light ON (approximately 70% N2) during descent to assure proper wing anti-ice operation. 9. Cabin Pressure Control—Set Field Elevation + 500 Feet 10. Windshield Defog—As Required 11. Altimeters—Set When Ready for Approach 12. Airspeed—Slow to and Maintain 0.3 AOA Note: Maintain 0.3 AOA throughout the configuration change to Flaps 10°, Gear Down. This will yield an airspeed of about 180 knots. 13. Fuel Management—Check 14. N1, Landing Distance—Confirm 15. Cabin Sign—Safety 16. Windshield Anti-Ice—Low 17. Hydraulic/Nitrogen Pressure—Check 18. Engine Sync—Off 19. Flaps—10° Before Landing 20. AOA Index—Preset 1.3 V/Vs 21. Landing Gear—Down 22. Airspeed—Slow to 0.4 AOA 23. Recognition Light—Off 24. Landing Lights—As Required 25. Ignitions—On 26. Flaps—30° 27. Approach Airspeed

(VREF)Slow to and Maintain 0.57 AOA Note: This will yield a normal approach speed of VREF (0.57 AOA) and normal landing distances. 28. Yaw Damp—Off Balked Landing 29. Thrust—Takeoff N1 30. Pitch Attitude 10° When Positive Climb Has Been Established 31. Flaps—10° 32. Landing Gear—Up 33. Yaw Damp—On 34. Airspeed—Accelerate to 0.3 AOA 35. Flaps—Up 36. Airspeed—Accelerate and Maintain 0.2 AOA 37. Landing Lights—Ret/off Emergency Procedures 400T(T-1A) Loss of Airspeed Note: If the pilot's, or copilot's and standby, or all three airspeed(s) are noted to be decreasing toward zero, refer to the standby attitude indicator, standby altimeter, standby heading and the AOA indicator for aircraft control and land at the nearest suitable airport. The pilot's and copilots altimeter's, attitude displays and heading displays may be unreliable and the autopilot may disconnect. This may be accompanied by amber boxed A/S, ALT, ATT and/or HDG comparator flags. The comparator flags may be followed by red FAIL flags on the airspeed, altitude, attitude and heading displays. 1. Autopilot—Disconnect 2. Airspeed—Slow to and Maintain 0.2 AOA 3. Thrust—As Required 4. Speed Brakes—As Required (Slow to 0.25 AOA with speed brakes extended) Note: An AOA of 0.2 (0.25 speed brakes extended) will yield an airspeed of about 210 knots. Use pitch attitude as primary reference. Make small changes in pitch attitude and wait for AOA to stabilize. When Ready for Descent 5. Seat Belts/Shoulder Harnesses—Fastened 6. Cabin Sign—AS Required 7. Anti/De-Ice Systems—As Required Caution If icing conditions are anticipated during the descent and approach, turn ice protection systems ON as early as possible prior to penetrating clouds. Maintain wing anti/deice operation light ON (approximately 70% N2) during descent to assure proper wing anti-ice operation. 8. Cabin Pressure Control—Set Field Elevation + 500 Feet 9. Windshield Defog—As Required 10. Altimeters—Set When Ready for Approach 11. Airspeed—Slow to and Maintain 0.3 AOA Note: Maintain 0.3 AOA throughout the configuration change to Flaps 10°, Gear Down. This will yield an airspeed of about 180 knots. 12. Fuel Management—Check 13. N1, Landing Distance—Confirm 14. Cabin Sign—Safety 15. Windshield Anti-Ice—Low 16. Hydraulic/Nitrogen Pressure—Check 17. Engine Sync—Off 18. Flaps—10° 19. GPWS TAC and FLP ORIDE—Off Before Landing 20. AOA Index—Preset 1.3 V/Vs 21. Landing Gear—Down 22. Airspeed—Slow to 0.4 AOA 23. Landing Lights—As Required 24. Ignitions—On 25. Flaps—Set for Landing 26. Approach Airspeed (VREF)—Slow to and Maintain 0.57 AOA Note: This will yield an approach speed of VREF (0.57 AOA) and normal landing distances. 27. Yaw Damp—Off Caution If icing conditions are encountered during flight, the maximum landing flap is 10° unless one of the following are met. The icing conditions are encountered for less than 10 minutes, and the RAM Air Temperature

(RAT)during the encounter was warmer than −8°C. A RAT of +10°C, or warmer, is observed during the descent, approach or landing. If either of the above two conditions are met, Flaps 30° may be used for landing. Balked Landing 28. Thrust—Takeoff N1 29. Pitch Attitude—10° When Positive Climb Has Been Established 30. Flaps—10° 31. Landing Gear—Up 32. Yaw Damp—On 33. Airspeed—Accelerate to 0.3 AOA 34. Flaps—Up 35. Airspeed—Accelerate and Maintain 0.2 AOA 36. Landing Lights—Ret/off Emergency Procedures 400T(TX) Loss of Airspeed Note: If the pilot's, or copilot's and standby, or all three airspeed(s) are noted to be decreasing toward zero, refer to the standby attitude indicator, standby altimeter, standby heading and the AOA indicator for aircraft control and land at the nearest suitable airport. The pilot's and copilots altimeter's, attitude displays and heading displays may be unreliable and the autopilot may disconnect. This may be accompanied by amber boxed A/S, ALT, ATT and/or HDG comparator flags. The comparator flags may be followed by red FAIL flags on the airspeed, altitude, attitude and heading displays. 1. Autopilot—Disconnect 2. Airspeed—Slow to and Maintain 0.2 AOA 3. Thrust—As Required 4. Speed Brakes—As Required (Slow to 0.25 AOA with speed brakes extended) Note: An AOA of 0.2 (0.25 speed brakes extended) will yield an airspeed of about 210 knots. Use pitch attitude as primary reference. Make small changes in pitch attitude and wait for AOA to stabilize. When Ready for Descent 5. Seat Belts/Shoulder Harnesses—Fastened 6. Cabin Sign—As Required 7. Anti/DeIce Systems—As Required Caution If icing conditions are anticipated during the descent and approach, turn ice protection systems ON as early as possible prior to penetrating clouds. Maintain wing anti/deice operation light ON (approximately 70% N2) during descent to assure proper wing anti-ice operation. 8. Cabin Pressure Control—Set Field Elevation + 500 Feet 9. Windshield Defog—As Required 10. Altimeters—Set When Ready for Approach 11. Airspeed—Slow to and Maintain 0.3 AOA Note: Maintain 0.3 AOA throughout the configuration change to Flaps—10°, Gear Down. This will yield an airspeed of about 180 knots. 12. Fuel Management—Check 13. N1, Landing Distance—Confirm 14. Cabin Sign—Safety 15. Windshield Anti-Ice—Low 16. Hydraulic/Nitrogen Pressure—Check 17. Engine Sync—Off 18. Flaps—10° Before Landing 19. AOA Index—Preset 1.3 V/Vs 20. Landing Gear—Down 21. Airspeed—Slow to 0.4 AOA 22. Landing Lights—As Required 23. Ignitions—On 24. Flaps—30° 25. Approach Airspeed (VREF)—Slow to and Maintain 0.57 AOA Note: This will yield a normal approach speed of VREF (0.57 AOA) and normal landing distances. 26. Yaw Damp—Off Balked Landing 26. Thrust—Takeoff N1 27. Pitch Attitude 10° When Positive Climb Has Been Established 29. Flaps 10° 30. Landing Gear—Up 31. Yaw Damp—On 32. Airspeed—Accelerate to 0.3 AOA 33. Flaps— 0° 34. Airspeed—Accelerate and Maintain 0.2 AOA 35. Landing Lights—Ret/off” Note 1: When a previously specified Temporary AFM revision has been incorporated into the general revisions of the AFM, the general revision may be inserted in the AFM, provided the information contained in the general revision is identical to that specified in the specified Temporary AFM revision. Alternative Methods of Compliance

(b)An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Wichita Aircraft Certification Office (ACO), FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Wichita ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. Special Flight Permits

(c)Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. Incorporation by Reference

(d)Except as provided by paragraph

(a)of this AD, the AFM revision shall be done in accordance with Raytheon Beechjet 400T Temporary Change, P/N 132-590002-5TC3, dated November 12, 2001; Beechjet 400T Temporary Change, P/N 134-590002-1TC3, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-91TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-95TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-107TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-109TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-167TC7, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128-590001-169TC3, dated November 12, 2001; Beechjet 400 Temporary Change, P/N 128-590001-13BTC1, dated November 12, 2001; Beechjet 400 Temporary Change P/N 128-590001-13BTC2, dated November 12, 2001; MU-300 Diamond I Temporary Change, P/N MR-0460TC1, dated November 12, 2001; or MU-300 Diamond IA Temporary Change, P/N MR-0873TC1, dated November 12, 2001; as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Raytheon Aircraft Company, Department 62, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Effective Date

(e)This amendment becomes effective on December 11, 2001. Issued in Renton, Washington, on November 26, 2001. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01-30083 Filed 12-5-01; 8:45 am]

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