Noise Certification of Supersonic Airplanes
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Minimum Standard Requirements for Airport Aeronautical Services
BBUUCCKKEEYYEE MMUUNNIICCIIPPAALL AAIIRRPPOORRTT MMINIMUM SSTANDARD RREQUIREMENTS FFOR AAIRPORT AAERONAUTICAL SSERVICES AAPPRRIILL 99,, 22001144 Buckeye Municipal Airport Minimum Standards April 9, 2014 TABLE OF CONTENTS Section 1 GENERAL INFORMATION Section 1-1. Purpose. 4 Section 1-2. Introduction. 4 Section 1-3. Application of minimum operating standards. 4 Section 1-4. Activities not covered by minimum operating standards. 4 Section 1-5. Multiple activities by one commercial airport operator. 4 Section 1-6. Right to amend standards. 5 Section 1-7. Waiver or modification of standards. 5 Section 1-8. Categories of aeronautical service operator. 5 Section 1-9. Effective date. 5 Section 2 DEFINITIONS Section 2-1. Aircraft definitions. 6 Section 2-2. General definitions. 6 Section 2-3. Governmental definitions. 7 Section 2-4. Fueling definitions. 8 Section 2-5. Lease and agreements definitions. 8 Section 2-6. Service definitions. 8 Section 2-7. Infrastructure definitions. 9 Section 3 APPLICATION PROCESS Section 3-1. Application and qualifications. 10 Section 3-2. Action on application. 10 Section 3-3. Appeal process. 11 Section 4 GENERAL CONTRACTUAL PROVISIONS Section 4-1. General contractual provisions. 12 Section 5 GENERAL OPERATIONAL REQUIREMENTS Section 5-1. Airport rules and regulations. 13 Section 5-2. Taxiway access. 13 Section 5-3. Right-of-entry reserved. 13 Section 5-4. Rates and charges. 13 Section 5-5. Personnel, subtenants and invitees; control and demeanor. 13 Section 5-6. Interference with utilities and systems. 13 Section 5-7. Fire equipment. 13 Section 5-8. Vehicle identification. 13 Section 5-9. Indemnification. 14 Section 5-10. Environmental. 14 Section 6 INSURANCE Section 6-1. -
A Design Study Me T Rop"Ol Itan Air Transit System
NASA CR 73362 A DESIGN STUDY OF A MET R OP"OL ITAN AIR TRANSIT SYSTEM MAT ir 0 ± 0 49 PREPARED UNDER, NASA-ASEE SUMMER FACULTY FELLOWSHIP PROGRAM ,IN Cq ENGINEERING SYSTEMS DESIGN NASA CONTRACT NSR 05-020-151 p STANFORD UNIVERSITY STANFORD CALIFORNIA CL ceoroducedEAR'C-by thEGHOU AUGUST 1969 for Federal Scientific &Va Tec1nical 2 Information Springfied NASA CR 73362 A DESIGN STUDY OF A METROPOLITAN AIR TRANSIT SYSTEM MAT Prepared under NASA Contract NSR 05-020-151 under the NASA-ASEE Summer Faculty Fellowship Program in Engineering Systems Design, 16 June 29 August, 1969. Faculty Fellows Richard X. Andres ........... ......... ..Parks College Roger R. Bate ....... ...... .."... Air Force Academy Clarence A. Bell ....... ......"Kansas State University Paul D. Cribbins .. .... "North Carolina State University William J. Crochetiere .... .. ........ .Tufts University Charles P. Davis . ... California State Polytechnic College J. Gordon Davis . .... Georgia Institute of Technology Curtis W. Dodd ..... ....... .Southern Illinois University Floyd W. Harris .... ....... .... Kansas State University George G. Hespelt ........ ......... .University of Idaho Ronald P. Jetton ...... ............ .Bradley University Kenneth L. Johnson... .. Milwaukee School of Engineering Marshall H. Kaplan ..... .... Pennsylvania State University Roger A. Keech . .... California State Polytechnic College Richard D. Klafter... .. .. Drexel Institute of Technology Richard S. Marleau ....... ..... .University of Wisconsin Robert W. McLaren ..... ....... University'of Missouri James C. Wambold..... .. Pefinsylvania State University Robert E. Wilson..... ..... Oregon State University •Co-Directors Willi'am Bollay ...... .......... Stanford University John V. Foster ...... ........... .Ames Research Center Program Advisors Alfred E. Andreoli . California State Polytechnic College Dean F. Babcock .... ........ Stanford Research Institute SUDAAR NO. 387 September, 1969 i NOT FILMED. ppECEDING PAGE BLANK CONTENTS Page CHAPTER 1--INTRODUCTION ... -
FAA Order 8130.2H, February 4, 2015
U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADM INISTRATION ORDER 8130.2H 02/04/2015 National Policy SUBJ: Airworthiness Certification of Products and Articles This order establishes procedures for accomplishing original and recurrent airworthiness certification ofaircraft and related products and articles. The procedures contained in this order apply to Federal Aviation Administration (FAA) manufacturing aviation safety inspectors (ASI), to FAA airworthiness AS Is, and to private persons or organizations delegated authority to issue airworthiness certificates and related approvals. Suggestions for improvement of this order may be submitted using the FAA Office of Aviation Safety (AVS) directive feedback system at http://avsdfs.avs.faa.gov/default.aspx, or FAA Form 1320-19, Directive Feedback Information, found in appendix I to this order. D G!JD Cf1 · ~ David Hempe Manager, Design, Manufacturing, & Airworthiness Division Aircraft Certification Service Distribution: Electronic Initiated By: AIR-1 00 02/04/2015 8130.2H Table of Contents Paragraph Page Chapter 1. Introduction 100. Purpose of This Order .............................................................................. 1-1 101. Audience .................................................................................................. 1-1 102. Where Can I Find This Order .................................................................. 1-1 103. Explanation of Policy Changes ................................................................ 1-1 104. Cancellation ............................................................................................ -
CHAPTER 11 Subsonic and Supersonic Aircraft Emissions
CHAPTER 11 Subsonic and Supersonic Aircraft Emissions Lead Authors: A. Wahner M.A. Geller Co-authors: F. Arnold W.H. Brune D.A. Cariolle A.R. Douglass C. Johnson D.H. Lister J.A. Pyle R. Ramaroson D. Rind F. Rohrer U. Schumann A.M. Thompson CHAPTER 11 SUBSONIC AND SUPERSONIC AIRCRAFT EMISSIONS Contents SCIENTIFIC SUMMARY ......................................................................................................................................... 11.1 11.1 INTRODUCTION ............................................................................................................................................ 11.3 11.2 AIRCRAFT EMISSIONS ................................................................................................................................. 11.4 11.2.1 Subsonic Aircraft .................................................................................................................................. 11.5 11.2.2 Supersonic Aircraft ............................................................................................................................... 11.6 11.2.3 Military Aircraft .................................................................................................................................... 11.6 11.2.4 Emissions at Altitude ............................................................................................................................ 11.6 11.2.5 Scenarios and Emissions Data Bases ................................................................................................... -
E. Runway Length Analysis
JOSLIN FIELD, MAGIC VALLEY REGIONAL AIRPORT DECEMBER 2012 E. Runway Length Analysis This appendix describes the runway length analysis conducted for the Airport. Runway 7-25, the Airport’s primary runway, has a length of 8,700 feet and the existing crosswind runway (Runway 12-30) has a length of 3,207 feet. A runway length analysis was conducted to determine if additional runway length is required to meet the needs of aircraft forecasted to operate at the Airport through the planning period. The analysis was conducted according to Federal Aviation Administration (FAA) guidance contained in Advisory Circular (AC) 150/5325-4B, Runway Length Requirements for Airport Design. The runway length analysis set forth in AC 150/5325-4B relates to both arrivals and departures, although departures typically require more runway length. Runway length requirements were determined separately for Runway 7-25 and Runway 12-30. E.1 Primary Runway Length Requirements According to AC 150/5325-4B, the design objective for the primary runway is to provide a runway length for all aircraft without causing operational weight restrictions. The methodology used to determine required runway lengths is based on the MTOW of the aircraft types to be evaluated, which are grouped into the following categories: Small aircraft (MTOW of 12,500 pounds or less) – Aircraft in this category range in size from ultralight aircraft to small turboprop aircraft. Within this category, aircraft are broken out by approach speeds (less than 30 knots, at least 30 knots but less than 50 knots, and more than 50 knots). Aircraft with approach speeds of more than 50 knots are further broken out by passenger seat capacity (less than 10 passenger seats and 10 or more passenger seats). -
RASG-PA ESC/29 — WP/04 14/11/17 Twenty
RASG‐PA ESC/29 — WP/04 14/11/17 Twenty ‐ Ninth Regional Aviation Safety Group — Pan America Executive Steering Committee Meeting (RASG‐PA ESC/29) ICAO NACC Regional Office, Mexico City, Mexico, 29‐30 November 2017 Agenda Item 3: Items/Briefings of interest to the RASG‐PA ESC PROPOSAL TO AMEND ICAO FLIGHT DATA ANALYSIS PROGRAMME (FDAP) RECOMMENDATION AND STANDARD TO EXPAND AEROPLANES´ WEIGHT THRESHOLD (Presented by Flight Safety Foundation and supported by Airbus, ATR, Embraer, IATA, Brazil ANAC, ICAO SAM Office, and SRVSOP) EXECUTIVE SUMMARY The Flight Data Analysis Program (FDAP) working group comprised by representatives of Airbus, ATR, Embraer, IATA, Brazil ANAC, ICAO SAM Office, and SRVSOP, is in the process of preparing a proposal to expand the number of functional flight data analysis programs. It is anticipated that a greater number of Flight Data Analysis Programs will lead to significantly greater safety levels through analysis of critical event sets and incidents. Action: The FDAP working group is requesting support for greater implementation of FDAP/FDMP throughout the Pan American Regions and consideration of new ICAO standards through the actions outlined in Section 4 of this working paper. Strategic Safety Objectives: References: Annex 6 ‐ Operation of Aircraft, Part 1 sections as mentioned in this working paper RASG‐PA ESC/28 ‐ WP/09 presented at the ICAO SAM Regional Office, 4 to 5 May 2017. 1. Introduction 1.1 Flight Data Recorders have long been used as one of the most important tools for accident investigations such that the term “black box” and its recovery is well known beyond the aviation industry. -
Subsonic Aircraft Wing Conceptual Design Synthesis and Analysis
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by GSSRR.ORG: International Journals: Publishing Research Papers in all Fields International Journal of Sciences: Basic and Applied Research (IJSBAR) ISSN 2307-4531 (Print & Online) http://gssrr.org/index.php?journal=JournalOfBasicAndApplied --------------------------------------------------------------------------------------------------------------------------- Subsonic Aircraft Wing Conceptual Design Synthesis and Analysis Abderrahmane BADIS Electrical and Electronic Communication Engineer from UMBB (Ex.INELEC) Independent Electronics, Aeronautics, Propulsion, Well Logging and Software Design Research Engineer Takerboust, Aghbalou, Bouira 10007, Algeria [email protected] Abstract This paper exposes a simplified preliminary conceptual integrated method to design an aircraft wing in subsonic speeds up to Mach 0.85. The proposed approach is integrated, as it allows an early estimation of main aircraft aerodynamic features, namely the maximum lift-to-drag ratio and the total parasitic drag. First, the influence of the Lift and Load scatterings on the overall performance characteristics of the wing are discussed. It is established that the optimization is achieved by designing a wing geometry that yields elliptical lift and load distributions. Second, the reference trapezoidal wing is considered the base line geometry used to outline the wing shape layout. As such, the main geometrical parameters and governing relations for a trapezoidal wing are -
Explanatory Note to ED Decision
European Aviation Safety Agency Explanatory Note to Decision 2017/016/R Appendix I — Aircraft type ratings for Part-66 aircraft maintenance licence RELATED NPA/CRD 2016-20 — RMT.0541 EXECUTIVE SUMMARY This Decision addresses a regulatory coordination issue related to aircraft type ratings for Part-66 aircraft maintenance licences. According to the acceptable means of compliance (AMC) to Part-66, type ratings should be endorsed on a licence in accordance with Appendix I to AMC to Part-66 ‘Aircraft type ratings for Part-66 aircraft maintenance licence’. The specific objective of this rulemaking task is to ensure a common standard throughout the Member States. Executive Director Decisions are issued regularly to amend this list following the changes coming from industry, to add new aircraft types, or remove aircraft types that became obsolete. Action area: Regular updates Affected rules: AMC to Part-66 Affected stakeholders: Member States NAA, industry, individual license holders. Driver: Level playing field Rulemaking group: No Impact assessment: None Rulemaking Procedure: Standard 12.05.2009 22.12.2016 1.6.2017 TE.RPRO.00058-005 © European Aviation Safety Agency. All rights reserved. ISO 9001 certified. Proprietary document. Copies are not controlled. Confirm revision status through the EASA intranet/internet. Page 1 of 16 An agency of the European Union European Aviation Safety Agency Explanatory Note to Decision 2017/016/R Table of contents Table of contents 1. About this Decision .............................................................................................................................. 3 2. In summary — why and what ............................................................................................................... 4 2.1. Why we need to change the AMC. ........................................................................................................... 4 2.2. What we want to achieve ......................................................................................................................... 4 2.3. -
Designating and Naming Defense Military Aerospace Vehicles
BY ORDER OF THE SECRETARIES AIR FORCE INSTRUCTION 16-401 OF THE AIR FORCE, ARMY, AND NAVY ARMY REGULATION 70-50 NAVAIRINST 13100.16 16 MAY 2014 Operations DESIGNATING AND NAMING DEFENSE MILITARY AEROSPACE VEHICLES COMPLIANCE WITH THIS PUBLICATION IS MANDATORY ACCESSIBILITY: Publications and forms are available for downloading or ordering on the e- Publishing website at www.e-Publishing.af.mil RELEASABILITY: There are no releasability restrictions on this publication. OPR: HQ USAF/A8PE Certified by: HQ USAF/A8P (Maj Gen Boera) Supersedes: AFI 16-401_IP; Pages: 42 AR 70-50; NAVAIRINST 13100.16; 14 April 2005 This Air Force publication implements DoD Directive 4120.15E, Designating and Naming Military Aerospace Vehicles. It provides guidance and procedures for designating and naming defense military aerospace vehicles across the DoD. This AFI defines the roles and responsibilities of required organizations, the processes for requesting new or retiring old designators and popular names, and the relationship between and military aerospace vehicle designators and names. Additionally, descriptions of standardized Mission Design Series (MDS) designation symbols, military department contacts, and sample MDS and Popular Name request letters are provided. This instruction applies to all military services and departments, including Reserve and National Guard components, which require official designators or names for defense aerospace vehicles. Ensure that all records created as a result of processes prescribed in this publication are maintained in accordance with AFMAN 33-363, Management of Records, and disposed of in accordance with the Air Force Records Disposition Schedule (RDS) located at https://www.my.af.mil/afrims/afrims/afrims/rims.cfm. -
Aircraft of Today. Aerospace Education I
DOCUMENT RESUME ED 068 287 SE 014 551 AUTHOR Sayler, D. S. TITLE Aircraft of Today. Aerospace EducationI. INSTITUTION Air Univ.,, Maxwell AFB, Ala. JuniorReserve Office Training Corps. SPONS AGENCY Department of Defense, Washington, D.C. PUB DATE 71 NOTE 179p. EDRS PRICE MF-$0.65 HC-$6.58 DESCRIPTORS *Aerospace Education; *Aerospace Technology; Instruction; National Defense; *PhysicalSciences; *Resource Materials; Supplementary Textbooks; *Textbooks ABSTRACT This textbook gives a brief idea aboutthe modern aircraft used in defense and forcommercial purposes. Aerospace technology in its present form has developedalong certain basic principles of aerodynamic forces. Differentparts in an airplane have different functions to balance theaircraft in air, provide a thrust, and control the general mechanisms.Profusely illustrated descriptions provide a picture of whatkinds of aircraft are used for cargo, passenger travel, bombing, and supersonicflights. Propulsion principles and descriptions of differentkinds of engines are quite helpful. At the end of each chapter,new terminology is listed. The book is not available on the market andis to be used only in the Air Force ROTC program. (PS) SC AEROSPACE EDUCATION I U S DEPARTMENT OF HEALTH. EDUCATION & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS BEEN REPRO OUCH) EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIG INATING IT POINTS OF VIEW OR OPIN 'IONS STATED 00 NOT NECESSARILY REPRESENT OFFICIAL OFFICE OF EOU CATION POSITION OR POLICY AIR FORCE JUNIOR ROTC MR,UNIVERS17/14AXWELL MR FORCEBASE, ALABAMA Aerospace Education I Aircraft of Today D. S. Sayler Academic Publications Division 3825th Support Group (Academic) AIR FORCE JUNIOR ROTC AIR UNIVERSITY MAXWELL AIR FORCE BASE, ALABAMA 2 1971 Thispublication has been reviewed and approvedby competent personnel of the preparing command in accordance with current directiveson doctrine, policy, essentiality, propriety, and quality. -
Scheduled Civil Aircraft Emission Inventories for 1992: Database Development and Analysis
NASA Contractor Report 4700 Scheduled Civil Aircraft Emission Inventories for 1992: Database Development and Analysis Steven L. Baughcum, Terrance G. Tritz, Stephen C. Henderson, and David C. Pickett Contract NAS1-19360 Prepared for Langley Research Center April 1996 NASA Contractor Report 4700 Scheduled Civil Aircraft Emission Inventories for 1992: Database Development and Analysis Steven L. Baughcum, Terrance G. Tritz, Stephen C. Henderson, and David C. Pickett Boeing Commercial Airplane Group • Seattle Washington National Aeronautics and Space Administration Prepared for Langley Research Center Langley Research Center • Hampton, Virginia 23681-0001 under Contract NAS1-19360 April 1996 Printed copies available from the following: NASA Center for AeroSpace Information National Technical Information Service (NTIS) 800 Elkridge Landing Road 5285 Port Royal Road Linthicum Heights, MD 21090-2934 Springfield, VA 22161-2171 (301) 621-0390 (703) 487-4650 Executive Summary This report describes the development of a database of aircraft fuel burned and emissions from scheduled air traffic for each month of 1992. In addition, the earlier results (NASA CR-4592) for May 1990 scheduled air traffic have been updated using improved algorithms. These emissions inventories were developed under the NASA High Speed Research Systems Studies (HSRSS) contract NAS1-19360, Task Assignment 53. They will be available for use by atmospheric scientists conducting the Atmospheric Effects of Aviation Project (AEAP) modeling studies. A detailed database of fuel burned and emissions [NOx, carbon monoxide(CO), and hydrocarbons (HC)] for scheduled air traffic has been calculated for each month of 1992. In addition, the emissions for May 1990 have been recalculated using the same methodology. The data are on a 1° latitude x 1° longitude x 1 km altitude grid. -
Guide to Aircraft-Based Observations
Guide to Aircraft-based Observations 2017 edition WEATHER CLIMATE WATER CLIMATE WEATHER WMO-No. 1200 Guide to Aircraft-based Observations 2017 edition WMO-No. 1200 EDITORIAL NOTE METEOTERM, the WMO terminology database, may be consulted at http://public.wmo.int/en/ resources/meteoterm. Readers who copy hyperlinks by selecting them in the text should be aware that additional spaces may appear immediately following http://, https://, ftp://, mailto:, and after slashes (/), dashes (-), periods (.) and unbroken sequences of characters (letters and numbers). These spaces should be removed from the pasted URL. The correct URL is displayed when hovering over the link or when clicking on the link and then copying it from the browser. WMO-No. 1200 © World Meteorological Organization, 2017 The right of publication in print, electronic and any other form and in any language is reserved by WMO. Short extracts from WMO publications may be reproduced without authorization, provided that the complete source is clearly indicated. Editorial correspondence and requests to publish, reproduce or translate this publication in part or in whole should be addressed to: Chairperson, Publications Board World Meteorological Organization (WMO) 7 bis, avenue de la Paix Tel.: +41 (0) 22 730 84 03 P.O. Box 2300 Fax: +41 (0) 22 730 81 17 CH-1211 Geneva 2, Switzerland Email: [email protected] ISBN 978-92-63-11200-2 NOTE The designations employed in WMO publications and the presentation of material in this publication do not imply the expression of any opinion whatsoever on the part of WMO concerning the legal status of any country, territory, city or area, or of its authorities, or concerning the delimitation of its frontiers or boundaries.