Aerospace Facts and Figures 1980/1981
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CAAM 3 Report
3rd Technical Report On Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards A joint effort of The Federal Aviation Administration and The Aerospace Industries Association March 30, 2017 Questions concerning distribution of this report should be addressed to: Federal Aviation Administration Manager, Engine and Propeller Directorate. TABLE OF CONTENTS Page Table of Contents iii List of Figures v I. Foreword 1 II. Background 1 III. Scope 2 IV. Discussion 3 V. Relationship to Previous CAAM Data 7 VI. General Notes and Comments 8 VII. Fleet Utilization 11 VIII. CAAM3 Team Members 12 IX. Appendices List of Appendices 13 Appendix 1: Standardized Aircraft Event Hazard Levels and Definitions 14 • General Notes Applicable to All Event Hazard Levels 19 • Rationale for Changes in Severity Classifications 19 • Table 1. Historical Comparison of Severity Level Descriptions and Rationale for CAAM3 Changes 21 Appendix 2: Event Definitions 39 Appendix 3: Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards (2001 through 2012) 44 • Uncontained Blade 44 • Uncontained Disk 50 • Uncontained – Other 56 iii • Uncontained – All Parts 62 • High Bypass Comparison by Generation 63 • Relationship Among High Bypass Fleet 64 • Case Rupture 66 • Case Burnthrough 69 • Under-Cowl Fire 72 • Strut/Pylon Fire 76 • Fuel Leak 78 • Engine Separation 82 • Cowl Separation 85 • Propulsion System Malfunction Recognition and Response (PSMRR) 88 • Crew Error 92 • Reverser/Beta Malfunction – In-Flight Deploy 96 • Fuel Tank Rupture/Explosion 99 • Tailpipe Fire 102 • Multiple-Engine Powerloss – Non-Fuel 107 • Multiple-Engine Powerloss – Fuel-Related 115 • Fatal Human Ingestion / Propeller Contact 120 • IFSD Snapshot by Hazard Level – 2012 Data Only 122 • RTO Snapshot by Hazard Level – 2012 Data Only 123 • APU Events 123 • Turboprop Events 124 • Matrices of Event Counts, Hazard Ratios and Rates 127 • Data Comparison to Previous CAAM Data 135 [ The following datasets which were collected in CAAM2 were not collected in CAAM3. -
Runway Analysis
CHAPTER 5 RUNWAY ANALYSIS 5 5 RUNWAY ANALYSIS INTRODUCTION The primary issue to be addressed in the William R. Fairchild International Airport (CLM) Master Plan involves the ultimate length and configuration of the runway system. At present there are two runways; primary Runway 8/26 and crosswind Runway 13/31. Runway 8/26 is 6,347 feet long and 150-feet wide with a displaced threshold of 1,354 feet on the approach end to Runway 26. The threshold was displaced to provide for an unobstructed visual approach slope of 20:1. Runway 13/31 is designated as the crosswind runway and is 3,250-feet long by 50-feet wide. In the 1997 ALP Update, the FAA determined that this runway was not required to provide adequate wind coverage and would not be eligible for FAA funding of any improvements in the future. The Port of Port Angeles has committed to keeping this runway functional without FAA support for as long as it is feasible. Subsequent sections of this analysis will reexamine the need for the runway. Both runways are supported by parallel taxiway systems with Taxiway A serving Runway 8/26 and Taxiway J for Runway 13/31. Taxiway A is 40 feet wide and Taxiway J is 50 feet wide. AIRFIELD REQUIREMENTS In determining airfield requirements, FAA Advisory Circular (AC) 150/5300-13, Airport Design (Change 14), has been consulted. This circular requires that future classification of the airport be defined as the basis for airfield planning criteria. As shown in the forecast chapter, the critical aircraft at CLM is expected to be the small business jet represented by the Cessna Citation within 5-years. -
Aerospace Engine Data
AEROSPACE ENGINE DATA Data for some concrete aerospace engines and their craft ................................................................................. 1 Data on rocket-engine types and comparison with large turbofans ................................................................... 1 Data on some large airliner engines ................................................................................................................... 2 Data on other aircraft engines and manufacturers .......................................................................................... 3 In this Appendix common to Aircraft propulsion and Space propulsion, data for thrust, weight, and specific fuel consumption, are presented for some different types of engines (Table 1), with some values of specific impulse and exit speed (Table 2), a plot of Mach number and specific impulse characteristic of different engine types (Fig. 1), and detailed characteristics of some modern turbofan engines, used in large airplanes (Table 3). DATA FOR SOME CONCRETE AEROSPACE ENGINES AND THEIR CRAFT Table 1. Thrust to weight ratio (F/W), for engines and their crafts, at take-off*, specific fuel consumption (TSFC), and initial and final mass of craft (intermediate values appear in [kN] when forces, and in tonnes [t] when masses). Engine Engine TSFC Whole craft Whole craft Whole craft mass, type thrust/weight (g/s)/kN type thrust/weight mini/mfin Trent 900 350/63=5.5 15.5 A380 4×350/5600=0.25 560/330=1.8 cruise 90/63=1.4 cruise 4×90/5000=0.1 CFM56-5A 110/23=4.8 16 -
Spacecraft American Aerospace Controls
Spacecraft For More Than 50 Years, Our Experience Is Your Assurance™ AAC Manufactures high-reliability voltage and current sensors for: Satellites UAVs Commercial Aircraft Missiles Underwater Vehicles Military Aircraft Launch Systems Armored Vehicles Ships Helicopters Industrial Equipment Rail AAC is a Woman-Owned Business and all parts are manufactured at AAC’s Farmingdale, NY location. American Aerospace Controls 570 Smith Street, Farmingdale NY 11735 Phone: +1 (631) 694-5100 – Fax: +1 (631) 694-6739 http://a-a-c.com ©American Aerospace Controls 10-2016 Aircraft-UAVs Rail AAC Quality and Engineering Industrial Defense For More Than 50 Years, Our Experience is Your Assurance™ AAC Engineering and Quality Depart- Since 1965, American Aerospace Controls has been manufacturing high reliability ments are here to work with you on the AC & DC current, voltage and frequency sensors, transducers and detectors. With design and qualification of your parts. an emphasis on engineering solutions and customer support, AAC has developed Our vast experience in space flight app- long-term relationships with some of the largest aerospace, defense, transit and industrial companies around the globe. lications allows us to offer insight into the design and requirements of each unique Space Application. AAC main- AAC in Space tains the highest standards in Quality and Production. AAC sensors have been used on numerous manned and unmanned spacecraft, satellite, rocket and Unmanned Aerial Vehicle (UAV) programs. AAC has been involved with space flight applications since the mid-1960s. AAC’s extensive From the Mercury Program in the 1960’s to today’s international commercial and knowledge and decades of experience in designing and manufacturing defense satellite systems, AAC engineers have helped design current and voltage transducers and detectors capable of providing high reliability in harsh remote detectors and transducers that are the best available. -
1.1 Goals and Objectives
Chapter One INVENTORY Rock Hill/York County Airport (Bryant Field – UZA) (the Airport) is a publicly owned general aviation facility located approximately four miles north of the central business district of the City of Rock Hill, South Carolina (the City, refer to Figures 1-1 and 1-2, pages 1-2 and 1-3). The Airport is owned and operated by the City of Rock Hill. In order to establish a planning guideline for future airport development, the owner has contracted this Airport Master Plan (Master Plan), which will satisfy future aviation demand in a financially feasible manner. 1.1 GOALS AND OBJECTIVES The Airport Master Plan presents both short- and long-term development for the Airport and graphically displays and reports the data and logic upon which the Master Plan is based. The goal of the Master Plan is to provide guidelines for future airport development, which will satisfy aviation demand in a cost-effective, feasible manner, while resolving aviation, environmental, and socioeconomic issues of the community. Objectives are attainable targets that are action-oriented and designed to address specific elements consistent with attainment of the goal. The objectives for Rock Hill/York County Airport (Bryant Field) are based on an initial evaluation of the Airport and its surrounding environs and meetings with Airport staff, City staff, South Carolina Department of Commerce Division of Aeronautics (SCDOA), and Federal Aviation Administration (FAA). As information is developed during data gathering efforts, objectives for the Airport Master -
Aviation Industry Agreed in 2008 to the World’S First Set of Sector-Specific Climate Change Targets
CONTENTS Introduction 2 Executive summary 3 Key facts and figures from the world of air transport A global industry, driving sustainable development 11 Aviation’s global economic, social and environmental profile in 2016 Regional and group analysis 39 Africa 40 Asia-Pacific 42 Europe 44 Latin America and the Caribbean 46 Middle East 48 North America 50 APEC economies 52 European Union 53 Small island states 54 Developing countries 55 OECD countries 56 Least-developed countries 57 Landlocked developing countries 58 National analysis 59 A country-by-country look at aviation’s benefits A growth industry 75 An assessment of the next 20 years of aviation References 80 Methodology 84 1 AVIATION BENEFITS BEYOND BORDERS INTRODUCTION Open skies, open minds The preamble to the Chicago Convention – in many ways aviation’s constitution – says that the “future development of international civil aviation can greatly help to create and preserve friendship and understanding among the nations and peoples of the world”. Drafted in December 1944, the Convention also illustrates a sentiment that underpins the construction of the post-World War Two multilateral economic system: that by trading with one another, we are far less likely to fight one another. This pursuit of peace helped create the United Nations and other elements of our multilateral system and, although these institutions are never perfect, they have for the most part achieved that most basic aim: peace. Air travel, too, played its own important role. If trading with others helps to break down barriers, then meeting and learning from each other surely goes even further. -
Soviet Steps Toward Permanent Human Presence in Space
SALYUT: Soviet Steps Toward Permanent Human Presence in Space December 1983 NTIS order #PB84-181437 Recommended Citation: SALYUT: Soviet Steps Toward Permanent Human Presence in Space–A Technical Mere- orandum (Washington, D. C.: U.S. Congress, Office of Technology Assessment, OTA- TM-STI-14, December 1983). Library of Congress Catalog Card Number 83-600624 For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 Foreword As the other major spacefaring nation, the Soviet Union is a subject of interest to the American people and Congress in their deliberations concerning the future of U.S. space activities. In the course of an assessment of Civilian Space Stations, the Office of Technology Assessment (OTA) has undertaken a study of the presence of Soviets in space and their Salyut space stations, in order to provide Congress with an informed view of Soviet capabilities and intentions. The major element in this technical memorandum was a workshop held at OTA in December 1982: it was the first occasion when a significant number of experts in this area of Soviet space activities had met for extended unclassified discussion. As a result of the workshop, OTA prepared this technical memorandum, “Salyut: Soviet Steps Toward Permanent Human Presence in Space. ” It has been reviewed extensively by workshop participants and others familiar with Soviet space activities. Also in December 1982, OTA wrote to the U. S. S. R.’s Ambassador to the United States Anatoliy Dobrynin, requesting any information concerning present and future Soviet space activities that the Soviet Union judged could be of value to the OTA assess- ment of civilian space stations. -
A Decade of Economic Change and Population Shifts in U.S. Regions
Regional Economic Changes A decade of economic change and population shifts in U.S. regions Regional ‘fortunes,’ as measured by employment and population growth, shifted during the 1983–95 period, as the economy restructured, workers migrated, and persons immigrated to the United States etween 1983 and 1990, the United States The national share component shows the pro- William G. Deming experienced one of its longest periods of portion of total employment change that is Beconomic expansion since the Second due simply to overall employment growth in World War. After a brief recession during 1990– the U.S. economy. That is, it answers the ques- 91, the economy resumed its expansion, and has tion: “What would employment growth in continued to improve. The entire 1983–95 pe- State ‘X’ have been if it had grown at the same riod also has been a time of fundamental eco- rate as the Nation as a whole?” The industry nomic change in the Nation. Factory jobs have mix component indicates the amount of em- declined in number, while service-based employ- ployment change attributable to a State’s ment has continued to increase. As we move from unique mix of industries. For example, a State an industrial to a service economy, States and re- with a relatively high proportion of employ- gions are affected in different ways. ment in a fast-growing industry, such as ser- While commonalties exist among the States, vices, would be expected to have faster em- the economic events that affect Mississippi, for ployment growth than a State with a relatively example, are often very different from the factors high proportion of employment in a slow- which influence California. -
The Return of the 1950S Nuclear Family in Films of the 1980S
University of South Florida Scholar Commons Graduate Theses and Dissertations Graduate School 2011 The Return of the 1950s Nuclear Family in Films of the 1980s Chris Steve Maltezos University of South Florida, [email protected] Follow this and additional works at: https://scholarcommons.usf.edu/etd Part of the American Studies Commons, and the Film and Media Studies Commons Scholar Commons Citation Maltezos, Chris Steve, "The Return of the 1950s Nuclear Family in Films of the 1980s" (2011). Graduate Theses and Dissertations. https://scholarcommons.usf.edu/etd/3230 This Thesis is brought to you for free and open access by the Graduate School at Scholar Commons. It has been accepted for inclusion in Graduate Theses and Dissertations by an authorized administrator of Scholar Commons. For more information, please contact [email protected]. The Return of the 1950s Nuclear Family in Films of the 1980s by Chris Maltezos A thesis submitted in partial fulfillment of the requirements for the degree of Master of Liberal Arts Department of Humanities College Arts and Sciences University of South Florida Major Professor: Daniel Belgrad, Ph.D. Elizabeth Bell, Ph.D. Margit Grieb, Ph.D. Date of Approval: March 4, 2011 Keywords: Intergenerational Relationships, Father Figure, insular sphere, mother, single-parent household Copyright © 2011, Chris Maltezos Dedication Much thanks to all my family and friends who supported me through the creative process. I appreciate your good wishes and continued love. I couldn’t have done this without any of you! Acknowledgements I’d like to first and foremost would like to thank my thesis advisor Dr. -
CHAMPION AEROSPACE LLC AVIATION CATALOG AV-14 Spark
® CHAMPION AEROSPACE LLC AVIATION CATALOG AV-14 REVISED AUGUST 2014 Spark Plugs Oil Filters Slick by Champion Exciters Leads Igniters ® Table of Contents SECTION PAGE Spark Plugs ........................................................................................................................................... 1 Product Features ....................................................................................................................................... 1 Spark Plug Type Designation System ............................................................................................................. 2 Spark Plug Types and Specifications ............................................................................................................. 3 Spark Plug by Popular Aircraft and Engines ................................................................................................ 4-12 Spark Plug Application by Engine Manufacturer .........................................................................................13-16 Other U. S. Aircraft and Piston Engines ....................................................................................................17-18 U. S. Helicopter and Piston Engines ........................................................................................................18-19 International Aircraft Using U. S. Piston Engines ........................................................................................ 19-22 Slick by Champion ............................................................................................................................. -
The Atmospheric Remote-Sensing Infrared Exoplanet Large-Survey
ariel The Atmospheric Remote-Sensing Infrared Exoplanet Large-survey Towards an H-R Diagram for Planets A Candidate for the ESA M4 Mission TABLE OF CONTENTS 1 Executive Summary ....................................................................................................... 1 2 Science Case ................................................................................................................ 3 2.1 The ARIEL Mission as Part of Cosmic Vision .................................................................... 3 2.1.1 Background: highlights & limits of current knowledge of planets ....................................... 3 2.1.2 The way forward: the chemical composition of a large sample of planets .............................. 4 2.1.3 Current observations of exo-atmospheres: strengths & pitfalls .......................................... 4 2.1.4 The way forward: ARIEL ....................................................................................... 5 2.2 Key Science Questions Addressed by Ariel ....................................................................... 6 2.3 Key Q&A about Ariel ................................................................................................. 6 2.4 Assumptions Needed to Achieve the Science Objectives ..................................................... 10 2.4.1 How do we observe exo-atmospheres? ..................................................................... 10 2.4.2 Targets available for ARIEL .................................................................................. -
Part 2 — Aircraft Type Designators (Decode) Partie 2 — Indicatifs De Types D'aéronef (Décodage) Parte 2 — Designadores De Tipos De Aeronave (Descifrado) Часть 2
2-1 PART 2 — AIRCRAFT TYPE DESIGNATORS (DECODE) PARTIE 2 — INDICATIFS DE TYPES D'AÉRONEF (DÉCODAGE) PARTE 2 — DESIGNADORES DE TIPOS DE AERONAVE (DESCIFRADO) ЧАСТЬ 2. УСЛОВНЫЕ ОБОЗНАЧЕНИЯ ТИПОВ ВОЗДУШНЫХ СУДОВ ( ДЕКОДИРОВАНИЕ ) DESIGNATOR MANUFACTURER, MODEL DESCRIPTION WTC DESIGNATOR MANUFACTURER, MODEL DESCRIPTION WTC INDICATIF CONSTRUCTEUR, MODÈLE DESCRIPTION WTC INDICATIF CONSTRUCTEUR, MODÈLE DESCRIPTION WTC DESIGNADOR FABRICANTE, MODELO DESCRIPCIÓN WTC DESIGNADOR FABRICANTE, MODELO DESCRIPCIÓN WTC УСЛ . ИЗГОТОВИТЕЛЬ , МОДЕЛЬ ВОЗДУШНОГО WTC УСЛ . ИЗГОТОВИТЕЛЬ , МОДЕЛЬ ВОЗДУШНОГО WTC ОБОЗНАЧЕНИЕ ОБОЗНАЧЕНИЕ A1 DOUGLAS, Skyraider L1P M NORTH AMERICAN ROCKWELL, Quail CommanderL1P L DOUGLAS, AD Skyraider L1P M NORTH AMERICAN ROCKWELL, A-9 Sparrow L1P L DOUGLAS, EA-1 Skyraider L1P M Commander NORTH AMERICAN ROCKWELL, A-9 Quail CommanderL1P L A2RT KAZAN, Ansat 2RT H2T L NORTH AMERICAN ROCKWELL, Sparrow CommanderL1P L A3 DOUGLAS, TA-3 Skywarrior L2J M DOUGLAS, NRA-3 SkywarriorL2J M A10 FAIRCHILD (1), OA-10 Thunderbolt 2 L2J M DOUGLAS, A-3 Skywarrior L2J M FAIRCHILD (1), A-10 Thunderbolt 2L2J M FAIRCHILD (1), Thunderbolt 2L2J M DOUGLAS, ERA-3 SkywarriorL2J M AVIADESIGN, A-16 Sport Falcon L1P L DOUGLAS, Skywarrior L2J M A16 AEROPRACT, A-19 L1P L A3ST AIRBUS, Super Transporter L2J H A19 AIRBUS, Beluga L2J H A20 DOUGLAS, Havoc L2P M DOUGLAS, A-20 Havoc L2P M AIRBUS, A-300ST Super TransporterL2J H AEROPRACT, Solo L1P L AIRBUS, A-300ST Beluga L2J H A21 SATIC, Beluga L2J H AEROPRACT, A-21 Solo L1P L SATIC, Super Transporter L2J H A22 SADLER, Piranha