Establishment of Class E Airspace; Oil City, PA, 11002 [08-875]

Download as PDF 11002 Federal Register / Vol. 73, No. 41 / Friday, February 29, 2008 / Rules and Regulations the calculated effects of altitude and temperature; * * * * * (8) Out-of-ground effect hover performance determined under § 29.49 and the maximum safe wind demonstrated under the ambient conditions for data presented. In addition, the maximum weight for each altitude and temperature condition at which the rotorcraft can safely hover out-of-ground-effect in winds of not less than 17 knots from all azimuths. These data must be clearly referenced to the appropriate hover charts; and * * * * * I 22. Amend Appendix B to Part 29 in paragraph V(b) by removing the word ‘‘cycle’’ and adding the word ‘‘cyclic’’ in its place; and by revising paragraphs V(a) and VII(a) to read as follows: must also be met throughout a practical flight envelope; and (iv) The static longitudinal and static directional stability requirements of Subpart B must be met throughout a practical flight envelope. * * * * * an adverse comment, were received within the comment period, the regulation would become effective on February 14, 2008. No adverse comments were received, and thus this notice confirms that effective date. Issued in Washington, DC, on February 20, 2008. Robert A. Sturgell, Acting Administrator. [FR Doc. E8–3817 Filed 2–28–08; 8:45 am] Issued in College Park, GA, on February 12, 2008. John D. Haley, Acting Manager, System Support Group, Eastern Service Center. [FR Doc. 08–875 Filed 2–28–08; 8:45 am] BILLING CODE 4910–13–P BILLING CODE 4910–13–M DEPARTMENT OF TRANSPORTATION DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Federal Aviation Administration 14 CFR Part 71 14 CFR Part 71 [Docket No. FAA–2007–0104; Airspace Docket No. 07–AEA–10] Appendix B to Part 29—Airworthiness Criteria for Helicopter Instrument Flight [Docket No. FAA–0165; Airspace Docket No. 07–AEA–11] Establishment of Class E Airspace; Oil City, PA Establishment of Class E Airspace; Montrose, PA * AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; confirmation of effective date. AGENCY: SUMMARY: This action confirms the effective date of a direct final rule that establishes a Class E airspace area to support Area Navigation (RNAV) Global Positioning System (GPS) Special Instrument Approach Procedures (IAPs) that serve the Northwest Medical Center in Oil City, PA. DATES: Effective 0901 UTC, February 14, 2008. The Director of the Federal Register approves this incorporation by reference action under Title 1, Code of Federal Regulations, part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments. SUMMARY: This action confirms the effective date of a direct final rule that establishes a Class E airspace area to support Area Navigation (RNAV) Global Positioning System (GPS) special Instrument Approach Procedures (IAPs) that serve the Montrose High School Heliport, Montrose, PA. DATES: Effective 0901 UTC, February 14, 2008. The Director of the Federal Register approves this incorporation by reference action under Title 1, Code of Federal Regulations, part 51, subject to the annual revision of FAA Order 7400.9 and publication of conforming amendments. FOR FURTHER INFORMATION CONTACT: Daryl Daniels, Airspace Specialist, System Support, AJO2–E2B.12, FAA Eastern Service Center, 1701 Columbia Ave., College Park, GA 30337; telephone (404) 305–5581; fax (404) 305–5572. SUPPLEMENTARY INFORMATION: FOR FURTHER INFORMATION CONTACT: Daryl Daniels, Airspace Specialist, System Support, AJO2–E2B.12, FAA Eastern Service Center, 1701 Columbia Ave., College Park, GA 30337; telephone (404) 305–5581; fax (404) 305–5572. SUPPLEMENTARY INFORMATION: Confirmation of Effective Date Confirmation of Effective Date The FAA published this direct final rule with a request for comments in the Federal Register on December 19, 2007 (72 FR 71762). The FAA uses the direct final rulemaking procedure for a non controversial rule where the FAA believes that there will be no adverse public comment. This direct final rule advised the public that no adverse comments were anticipated, and that unless a written adverse comment, or a written notice of intent to submit such The FAA published this direct final rule with a request for comments in the Federal Register on December 13, 2007 (72 FR 70768). The FAA uses the direct final rulemaking procedure for a non controversial rule where the FAA believes that there will be no adverse public comment. This direct final rule advised the public that no adverse comments were anticipated, and that unless a written adverse comment, or a written notice of intent to submit such * * * * V. Static Lateral Directional Stability (a) Static directional stability must be positive throughout the approved ranges of airspeed, power, and vertical speed. In straight and steady sideslips up to ±10° from trim, directional control position must increase without discontinuity with the angle of sideslip, except for a small range of sideslip angles around trim. At greater angles up to the maximum sideslip angle appropriate to the type, increased directional control position must produce an increased angle of sideslip. It must be possible to maintain balanced flight without exceptional pilot skill or alertness. rfrederick on PROD1PC67 with RULES * * * * * VII. Stability Augmentation System (SAS) (a) If a SAS is used, the reliability of the SAS must be related to the effects of its failure. Any SAS failure condition that would prevent continued safe flight and landing must be extremely improbable. It must be shown that, for any failure condition of the SAS that is not shown to be extremely improbable— (1) The helicopter is safely controllable when the failure or malfunction occurs at any speed or altitude within the approved IFR operating limitations; and (2) The overall flight characteristics of the helicopter allow for prolonged instrument flight without undue pilot effort. Additional unrelated probable failures affecting the control system must be considered. In addition— (i) The controllability and maneuverability requirements in Subpart B must be met throughout a practical flight envelope; (ii) The flight control, trim, and dynamic stability characteristics must not be impaired below a level needed to allow continued safe flight and landing; (iii) For Category A helicopters, the dynamic stability requirements of Subpart B VerDate Aug<31>2005 15:40 Feb 28, 2008 Jkt 214001 PO 00000 Frm 00032 Fmt 4700 Sfmt 4700 Federal Aviation Administration (FAA), DOT. ACTION: Final rule; confirmation of effective date. E:\FR\FM\29FER1.SGM 29FER1

Agencies

[Federal Register Volume 73, Number 41 (Friday, February 29, 2008)]
[Rules and Regulations]
[Page 11002]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 08-875]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 71

[Docket No. FAA-2007-0104; Airspace Docket No. 07-AEA-10]


Establishment of Class E Airspace; Oil City, PA

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION:  Final rule; confirmation of effective date.

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SUMMARY: This action confirms the effective date of a direct final rule 
that establishes a Class E airspace area to support Area Navigation 
(RNAV) Global Positioning System (GPS) Special Instrument Approach 
Procedures (IAPs) that serve the Northwest Medical Center in Oil City, 
PA.

DATES: Effective 0901 UTC, February 14, 2008. The Director of the 
Federal Register approves this incorporation by reference action under 
Title 1, Code of Federal Regulations, part 51, subject to the annual 
revision of FAA Order 7400.9 and publication of conforming amendments.

FOR FURTHER INFORMATION CONTACT: Daryl Daniels, Airspace Specialist, 
System Support, AJO2-E2B.12, FAA Eastern Service Center, 1701 Columbia 
Ave., College Park, GA 30337; telephone (404) 305-5581; fax (404) 305-
5572.

SUPPLEMENTARY INFORMATION:

Confirmation of Effective Date

    The FAA published this direct final rule with a request for 
comments in the Federal Register on December 19, 2007 (72 FR 71762). 
The FAA uses the direct final rulemaking procedure for a non 
controversial rule where the FAA believes that there will be no adverse 
public comment. This direct final rule advised the public that no 
adverse comments were anticipated, and that unless a written adverse 
comment, or a written notice of intent to submit such an adverse 
comment, were received within the comment period, the regulation would 
become effective on February 14, 2008. No adverse comments were 
received, and thus this notice confirms that effective date.

    Issued in College Park, GA, on February 12, 2008.
John D. Haley,
Acting Manager, System Support Group, Eastern Service Center.
[FR Doc. 08-875 Filed 2-28-08; 8:45 am]
BILLING CODE 4910-13-M
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