Federal Aviation Administration July 2005 – Federal Register Recent Federal Regulation Documents

Results 101 - 137 of 137
Establishment of Class E Airspace; Mifflintown, PA; Correction
Document Number: 05-13366
Type: Rule
Date: 2005-07-07
Agency: Federal Aviation Administration, Department of Transportation
This action corrects a final rule published in the Federal Register on March 14, 2005 (70 FR 12414). In that rule, the effective date was inadvertently published as September 29, 2005. The correct effective date is September 1, 2005. This action corrects that error.
Establishment of Class E Surface Area, South Lake Tahoe, CA
Document Number: 05-13365
Type: Rule
Date: 2005-07-07
Agency: Federal Aviation Administration, Department of Transportation
This action establishes a Class E Surface Area to replace existing Class D airspace at South Lake Tahoe, CA.
Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Model TBM 700 Airplanes
Document Number: 05-13333
Type: Proposed Rule
Date: 2005-07-07
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain SOCATAGroupe AEROSPATIALE (SOCATA) Model TBM 700 airplanes. This proposed AD would require you to inspect the fuselage skin in the VHF1 antenna mounting area for cracks and loose rivets. This proposed AD would also require you to modify the area if you find cracks or loose rivets. This proposed AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. We are issuing this proposed AD to detect and correct cracks in the fuselage skin, which could result in loss of aircraft pressurization. Loss of aircraft pressurization could lead to flight crew incapacitation.
Petitions for Exemption; Dispositions of Petitions Issued
Document Number: 05-13271
Type: Notice
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption, part 11 of title 14, Code of Federal Regulations (14 CFR), this notice contains the disposition of certain petitions previously received. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Petitions for Exemption; Summary of Petitions Received
Document Number: 05-13270
Type: Notice
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Petitions for Exemption; Summary of Petitions Received
Document Number: 05-13269
Type: Notice
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
Pursuant to FAA's rulemaking provisions governing the application, processing, and disposition of petitions for exemption part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice contains a summary of certain petitions seeking relief from specified requirements of 14 CFR. The purpose of this notice is to improve the public's awareness of, and participation in, this aspect of FAA's regulatory activities. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of any petition or its final disposition.
Notice of Intent To Request Approval From the Office of Management and Budget (OMB) of One New Public Collection of Information
Document Number: 05-13267
Type: Notice
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
In compliance with the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the FAA invites public comment on one public information collection which will be submitted to OMB for review and approval.
Proposed Establishment of Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR); Cincinnati, OH
Document Number: 05-13266
Type: Proposed Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish four Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR) in the Cincinnati, OH, terminal area. RITTRs are low altitude Air Traffic Service routes, based on area navigation (RNAV), for use by aircraft having instrument flight rules (IFR)-approved Global Positioning (GPS)/ Global Navigation Satellite System (GNSS) equipment. The purpose of RITTR is to expedite the handling of IFR overflight aircraft through busy terminal airspace areas. The FAA is proposing this action to enhance the safe and efficient use of the navigable airspace in the Cincinnati, OH, terminal area.
Airworthiness Directives; Bell Helicopter Textron Model 47D1, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A and Coastal Helicopters, Inc. Model OH-13H (Tomcat Mark 5A, 6B, 6C) Helicopters
Document Number: 05-13237
Type: Proposed Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
This document proposes adopting a new airworthiness directive (AD) for Bell Helicopter Textron (Bell) Model 47D1, 47G, 47G-2, 47G-2A, 47G-2A-1, 47G-3, 47G-3B, 47G-3B-1, 47G-3B-2, 47G-3B-2A, 47G-4, 47G-4A, 47G-5, 47G-5A and Coastal Helicopters, Inc. Model OH-13H (Tomcat Mark 5A, 6B, 6C) helicopters that have a certain scissors assembly or weld assembly scissors bracket installed. The AD would require, within 60 days, determining and recording the total hours time-in-service (TIS) for each Parts Manufacturer Approval (PMA)-produced scissors assembly and weld assembly scissors bracket and would establish a life limit for each affected part. This proposal is prompted by the need to establish a life limit on scissors assemblies and weld assembly scissors brackets produced under PMA No. PQ808SW or installed per Supplemental Type Certificate (STC) No. SH2772SW. The actions specified by the proposed AD are intended to establish a life limit to prevent using a scissors assembly or weld assembly scissors bracket past its life limit, which could result in failure of the part and subsequent loss of control of the helicopter.
Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
Document Number: 05-13225
Type: Proposed Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 767-200, -300, and -300F series airplanes. This proposed AD would require replacing the aileron control override quadrant with a modified unit. This proposed AD is prompted by a report of the seizing of the input override mechanism bearings of the lateral central control actuator on affected airplanes. We are proposing this AD to prevent corrosion of the input override mechanism bearings of the lateral central control actuator, which, in the event of a subsequent jam in the pilot's aileron control system, could result in failure of the aileron override system and consequent reduced lateral controllability of the airplane.
Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes
Document Number: 05-13224
Type: Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 777-200 and -300 series airplanes. This AD requires applying an anti-static conductive coating to the fuel access and thermal anti-icing blowout doors at the location of the bonding fasteners on the leading edge of the wings, and performing a resistance test on the new coating to ensure correct ground path resistance. This AD is prompted by a report that an anti-static coating was not applied correctly on doors located within a flammable fluid leakage zone. We are issuing this AD to prevent an uncontrollable fire in the leading edge of the wing, which could damage critical wing structures and cause a fuel tank explosion.
Airworthiness Directives; Boeing Model 767-200 and -300 Series Airplanes
Document Number: 05-13222
Type: Proposed Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 767-200 and -300 series airplanes. This proposed AD would require measuring the turnbuckle gap of the inflation cylinder of the off-wing emergency escape slide; corrective action if necessary; and installing a safety device on the inflation cylinder of the off-wing emergency escape slide. This proposed AD is prompted by a report indicating that the inflation trigger cable may inadvertently disconnect from the inflation turnbuckle of the inflation cylinder of the off-wing emergency escape slide, due to incorrect spacing of the cable insertion gap; and additional reports indicating that the pull force increase mechanism on the off-wing charged cylinder assemblies of the escape slide may be inadvertently disengaged. We are proposing this AD to prevent failed deployment of the emergency escape slide during an emergency, which could impede an evacuation and result in injury to passengers or airplane crewmembers, or inadvertent inflation and loss of an emergency escape slide during flight, which could result in possible structural damage to the airplane.
Airworthiness Directives; Boeing Model 757 Airplanes
Document Number: 05-13221
Type: Proposed Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA is revising an earlier proposed airworthiness directive (AD) for certain Boeing Model 757 airplanes. The original NPRM would have required inspections of certain wire bundles in the left and right engine-to-wing aft fairings for discrepancies, and related investigative and corrective actions if necessary. The original NPRM was prompted by a report indicating that a circuit breaker for the fuel shutoff valve tripped due to a wire that chafed against the structure in the flammable leakage zone of the aft fairing, causing a short circuit. This action revises the original NPRM by adding a new requirement for installing back-to-back p-clamps between the wire and hydraulic supply tube at the aft end of the right-hand strut only; and associated re-routing of the wire bundles, if necessary; and adding airplanes to the applicability. This action also clarifies the applicability specified in the original NPRM. We are proposing this supplemental NPRM to prevent chafing between the wire bundle and the structure of the aft fairing, which could result in electrical arcing and subsequent ignition of flammable vapors and possible uncontrollable fire.
Airworthiness Directives; Airbus Model A300 B2-203 and B4-203 Airplanes; Model A310-200 and -300 Series Airplanes; and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model A300 C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes)
Document Number: 05-13143
Type: Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Airbus transport category airplanes. This AD requires an inspection to determine if suspect part numbers (P/Ns) and serial numbers of certain Thales Avionics equipment are installed, and replacement of any suspect part with a modified part having a new P/N. This AD is prompted by reports of loss of the digital distance radio magnetic indicator and subsequent loss of both very high frequency omnidirectional range indicators, both distance measuring equipment, and one centralized maintenance computer. We are issuing this AD to prevent loss of navigation indications on the primary flight display requiring continuation of the flight on emergency instruments, which could lead to reduced ability to control the airplane in adverse conditions.
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-145 and EMB-135 Series Airplanes
Document Number: 05-13142
Type: Rule
Date: 2005-07-06
Agency: Federal Aviation Administration, Department of Transportation
This amendment adopts a new airworthiness directive (AD), applicable to certain EMBRAER Model EMB-145 and EMB-135 series airplanes, that requires replacement of the engine-driven hydraulic pump. This action is necessary to prevent engine oil leakage at the coupling seal between the hydraulic pump and the engine gearbox from causing low engine oil levels, which could lead to in-flight engine shutdown and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
Establishment of Class E2 Airspace; and Modification of Class E5 Airspace; Valentine, NE
Document Number: C5-9435
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
Modification of Class E Airspace; Parsons, KS
Document Number: C5-9434
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
Proposed Establishment of Class E2 Airspace; and Modification of Class E5 Airspace; Storm Lake, IA
Document Number: C5-12378
Type: Proposed Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
Amendment to Restricted Area 2211 Blair Lakes; AK
Document Number: C5-11761
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
Airworthiness Directives; Boeing Model 737-600, -700, -700C, -800, and -900 Series Airplanes
Document Number: 05-13141
Type: Proposed Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. This proposed AD would require modification of certain wire bundles located above the center fuel tank. This proposed AD is prompted by the results of fuel system reviews conducted by the manufacturer. We are proposing this AD to prevent chafed wire bundles near the center fuel tank, which could cause electrical arcing through the tank wall and ignition of fuel vapor in the fuel tank, and result in a fuel tank explosion.
Airworthiness Directives; Boeing Model 767-400ER Series Airplanes; and Model 777-200 and -300 Series Airplanes
Document Number: 05-13139
Type: Proposed Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Model 767-400ER series airplanes; and Model 777-200 and - 300 series airplanes. This proposed AD would require, for certain airplanes, repetitive testing of the fill and safety fittings of the fire extinguishing bottles in the forward cargo compartment for leaks; and repetitive application of a corrosion inhibiting compound (CIC) or replacement of the fire extinguishing bottles with reworked fire extinguishing bottles, as necessary. For all airplanes, this proposed AD would require replacement of the fire extinguishing bottles with reworked fire extinguishing bottles, which would end the repetitive tests and CIC applications if applicable. This proposed AD is prompted by failure of the safety fittings for the fire extinguishing bottles. We are proposing this AD to prevent failure of the safety fittings for the fire extinguishing bottles due to corrosion, which could result in leakage of extinguishing agent. If a fire occurs in the cargo bay, the fire extinguishing bottles could have less than enough extinguishing agent to control a fire.
Airworthiness Directives; Boeing Model 737 Airplanes
Document Number: 05-13136
Type: Proposed Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD) for certain Boeing Model 737 airplanes. This proposed AD would require modifying the elevator input torque tube assembly. This proposed AD is prompted by a report of a restriction in the pilots' elevator input control system. We are proposing this AD to prevent loss of elevator control and consequent reduced controllability of the airplane.
Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG (Formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH) Models BR700-710A1-10 and BR700-710A2-20 Turbofan Engines
Document Number: 05-13135
Type: Proposed Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to supersede an existing airworthiness directive (AD) for Rolls-Royce Deutschland Ltd & Co KG (RRD) (formerly Rolls-Royce Deutschland GmbH, formerly BMW Rolls-Royce GmbH) models BR700-710A1-10 and BR700-710A2-20 turbofan engines. That AD currently requires initial and repetitive visual and ultrasonic inspections of fan discs, part numbers (P/Ns) BRR18803, BRR19248, and BRR20791 for cracks, and if necessary, replacement with serviceable parts. This proposed AD would require the same inspections of these fan discs, with certain old design P/N fan blades installed. This proposed AD would extend the inspection interval for certain fan discs having new design P/N fan blades installed. Also, this proposed AD would add as optional terminating action to the repetitive inspections, installation of certain P/N new fan discs, certain P/N new fan blades, and engine fan speed (N1) Keep Out Zone software. This proposed AD results from a revised RRD service bulletin (SB) that introduces relaxed inspection intervals for certain P/N combinations of fan discs and fan blades, and introduces improved design fan discs and fan blades. We are proposing this AD to detect and prevent cracks in the fan disc that could result in an uncontained engine failure and damage to the airplane.
Airworthiness Directives; Hamilton Sundstrand Power Systems (formerly Sundstrand Power Systems) Auxiliary Power Units Models T-62T-46C2, T-62T-46C2A, T-62T-46C3, T-62T-46C7, and T-62T-46C7A
Document Number: 05-13134
Type: Proposed Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA proposes to adopt a new airworthiness directive (AD). The new AD is for Hamilton Sundstrand Power Systems (formerly Sundstrand Power Systems) auxiliary power units (APUs) models T-62T- 46C2, T-62T-46C2A, T-62T-46C3, T-62T-46C7, and T-62T-46C7A, with compressor impeller assembly, part number (P/N) 4502020 or 4502020A, installed. This proposed AD would require removal from service of those compressor impeller assemblies at reduced service life limits. This proposed AD results from two reports of uncontained failures of compressor impeller assemblies. We are proposing this AD to prevent an uncontained APU failure and damage to the airplane.
Stage 4 Aircraft Noise Standards
Document Number: 05-13076
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new noise standard for subsonic jet airplanes and subsonic transport category large airplanes. This noise standard ensures that the latest available noise reduction technology is incorporated into new aircraft designs. This noise standard, Stage 4, applies to any person submitting an application for a new airplane type design on and after January 1, 2006. The standard may be chosen voluntarily prior to that date. This noise standard is intended to provide uniform noise certification standards for Stage 4 airplanes certificated in the United States and those airplanes that meet the new International Civil Aviation Organization Annex 16 Chapter 4 noise standard.
Airworthiness Directives; Airbus Model A321-100 and -200 Series Airplanes
Document Number: 05-12843
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA is superseding an existing airworthiness directive (AD), which applies to Airbus Model A321 series airplanes. That AD currently requires revising the Limitations section of the airplane flight manual to include an instruction to use Flap 3 for landing when performing an approach in conditions of moderate to severe icing, significant crosswind (i.e., crosswinds greater than 20 knots, gust included), or moderate to severe turbulence. This new AD requires replacing existing elevator and aileron computers (ELACs) with ELACs having either L83 or L91 software, as applicable, which terminates the requirements of the existing AD. This AD also requires a related concurrent action. In addition, this AD revises the applicability by removing airplanes with these ELAC software standards incorporated in production. This AD is prompted by issuance of mandatory continuing airworthiness information by a civil airworthiness authority. We are issuing this AD to prevent roll oscillations during approach and landing in certain icing, crosswind, and turbulent conditions, which could result in reduced controllability of the airplane.
Airworthiness Directives; Learjet Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A (C-21A), and 36 Airplanes
Document Number: 05-12842
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Learjet Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A (C- 21A), and 36 airplanes. This AD requires a one-time inspection of the center ball of the aileron control cable or cables for a defective swage, and corrective actions if necessary. This AD is prompted by a report indicating that an aileron cable failed on one affected airplane when the cable underwent a tension check. We are issuing this AD to prevent severe weakening of the aileron cable, and consequent reduced controllability of the airplane.
Airworthiness Directives; Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 Series Airplanes
Document Number: 05-12837
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes. This AD requires revising the airworthiness limitations section of the Instructions for Continued Airworthiness by incorporating new and revised structural inspection procedures and new and revised inspection intervals for the longitudinal skin joints in the fuselage pressure shell. This proposed AD also requires phase-in inspections and repair of any crack found during any phase-in inspection. This AD is prompted by a report indicating that visual inspections were not adequate for detecting fatigue cracking in portions of the longitudinal skin joints in the fuselage pressure shell. We are issuing this AD to detect and correct fatigue cracking of the longitudinal skin joints in the fuselage pressure shell, which could affect the structural integrity of the airplane, and result in loss of cabin pressurization during flight.
Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes
Document Number: 05-12836
Type: Rule
Date: 2005-07-05
Agency: Federal Aviation Administration, Department of Transportation
The FAA is adopting a new airworthiness directive (AD) for all Fokker Model F.28 Mark 0070 and 0100 airplanes. This AD requires repetitive inspections for damage of the drive rod assembly of the aileron tab on each aileron actuator; repetitive measurements of the clearance between the aileron hydraulic lines and the drive rod; and related investigative and corrective actions if necessary. This AD is prompted by a report of an aileron 2 fault caused by severe wear of the polyamide washer that is part of an anti-rotation bush assembly in the aileron attachment lug. We are issuing this AD to prevent excessive wear of the polyamide washer of the aileron actuator bush assembly, which could result in aileron flutter and loss of control of the airplane.
Special Conditions: AMSAFE, Incorporated; Cirrus Design Corporation SR20 and SR22; Inflatable Four-Point Restraint Safety Belt with an Integrated Airbag Device
Document Number: 05-13093
Type: Rule
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
These special conditions are issued for the installation of an AMSAFE, Inc., Inflatable Four-Point Restraint Safety Belt with an Integrated Airbag Device on Cirrus Models SR20 and SR22. These airplanes, as modified by the installation of this Inflatable Safety Belt, will have novel and unusual design features associated with the upper-torso restraint portions of the four-point safety belt, which contains an integrated airbag device. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
Proposed Establishment of Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR); Jacksonville, FL
Document Number: 05-13085
Type: Proposed Rule
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
This action proposes to establish seven Area Navigation Instrument Flight Rules Terminal Transition Routes (RITTR) in the Jacksonville, FL, terminal area. RITTRs are low altitude Air Traffic Service routes, based on Area Navigation (RNAV), for use by aircraft having instrument flight rules (IFR)-approved Global Positioning System (GPS)/Global Navigation Satellite System (GNSS) equipment. The purpose of RITTR is to expedite the handling of IFR overflight aircraft through busy terminal airspace areas. The FAA is proposing this action to enhance the safe and efficient use of the navigable airspace in the Jacksonville, FL, terminal area.
Revision of Federal Airways V-2, V-257 and V-343; MT
Document Number: 05-13084
Type: Rule
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
This action corrects an error in the airspace description of a final rule that was published in the Federal Register on May 18, 2005 (70 FR 28423), Airspace Docket No. 04-ANM-09.
Proposed Modification of Class E Airspace; Akron, OH
Document Number: 05-13083
Type: Proposed Rule
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
This document proposes to modify Class E airspace at Akron, OH. An Airship RNAV Global Positioning System 263[deg] Standard Instrument Approach Procedure has been developed for Wingfoot Lake Airship Operations Airport, Akron Suffield, OH. Controlled airspace extending upward from 700 feet or more above the surface of the earth is needed to contain aircraft executing this approach. This action would increase the area of the existing controlled airspace for Akron, OH.
Modification of Class E Airspace; Muskegon, MI
Document Number: 05-13082
Type: Rule
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
This action modifies Class E airspace at Muskegon, MI. Standard Instrument Approach Procedures have been developed for Grand Haven Memorial Airpark. Controlled airspace extending upward from 700 feet or more above the surface of the earth is needed to contain aircraft executing these approaches. This action increases the area of existing controlled airspace for Grand Haven Memorial Airpark.
Proposed Modification of Class E Airspace; Madison, IN
Document Number: 05-13081
Type: Proposed Rule
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
This document proposes to modify Class E airspace at Madison, IN. Standard Instrument Approach Procedures have been developed for Madison Municipal Airport, Madison, IN. Controlled airspace extending upward from 700 feet or more above the surface of the earth is needed to contain aircraft executing these approach procedures. This action would increase the area of existing controlled airspace for Madison, IN.
Proposed Federal Aviation Administration (FAA) Policy for Provisional Type Certificates
Document Number: 05-13080
Type: Notice
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
This notice announces the availability of and request comments on the proposed policy for the issuance of provisional type certificates (TCs) as prescribed by Title 14 of the Code of Federal Regulations(14 CFR) 21.81.
Agency Information Collection Activity Under OMB Review
Document Number: 05-13079
Type: Notice
Date: 2005-07-01
Agency: Federal Aviation Administration, Department of Transportation
In compliance with the Paperwork Reduction Act of 1995 (44 U.S.C. 3501 et seq.), this notice announces that the Information Collection Request (ICR) abstracted below has been forwarded to the Office of Management and Budget (OMB) for extension of the currently approved collection. The ICR describes the nature of the information collection and the expected burden. The Federal Register Notice within a 60-day comment period soliciting comments on the following collection of information was published on March 9, 2005 on page 11725-11726.