Takeoff Safety Training Aid
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Cessna 182P ©2010 Axenty Aviation LLC Cessna 182P ©2010 Axenty Aviation LLC V SPEEDS (KIAS) EXTERIOR INSPECTION FLOODED START EXTERIOR INSPECTION Vso
Cessna 182P ©2010 Axenty Aviation LLC Cessna 182P ©2010 Axenty Aviation LLC V SPEEDS (KIAS) EXTERIOR INSPECTION FLOODED START EXTERIOR INSPECTION Vso..........................................48 Aft Fuselage (CONT.) Master....................................ON Vs............................................53 Baggage Door..............LOCKED Throttle....................FULL OPEN Vr.......................................50-60 Fuselage.........................CHECK Stall Warning...................CLEAR Mixture................IDLE CUT OFF Vx (sea level)..........................59 Empennage Tie Down.....................REMOVE Ignition.........................ENGAGE Vx (10,000 ft.).........................63 Horiz. Stabilizer..............CHECK Leading Edge.................CHECK *When engine fires advance Vy (sea level)..........................80 Elevator..........................CHECK Left Aileron.....................CHECK mixture, retard throttle* Vy (10,000 ft.).........................73 Tail Tie-Down..............REMOVE Left Flap........................CHECK Vfe (10°)................................140 Trim Tab.........................CHECK COLD WEATHER START Vfe (10°-40°)...........................95 Rudder............................CHECK PRE-ENGINE START Vno........................................141 Antennas........................CHECK Prime.........................6-8 TIMES Vne........................................176 Horiz. Stabilizer..............CHECK Preflight...................COMPLETE Mixture......................FULL RICH -
Control and Performance During Asymmetrical Powered Flight
Control and Performance During Asymmetrical Powered Flight Detailed theoretical paper in accordance with the JAA Learning Objectives, US Federal Aviation Regulations and EASA Certification Specifications for Multi-engine Rated Pilots CPL & ATPL Based on Airplane Design Methods as taught by Aeronautical Universities and Flight Test Techniques as taught by Experimental Test Pilot Schools January 2012 Harry Horlings Lt-Col RNLAF, ret'd Graduate USAF Test Pilot School AvioConsult Independent Aircraft Expert and Consultant – Committed to Improve Aviation Safety – Copyright © 2012, AvioConsult. All rights reserved. AvioConsult Control and Performance During Asymmetrical Powered Flight The author is a retired Lt-Col of the Royal Netherlands Air Force, graduate Flight Test Engineer of the USAF Test Pilot School, Edwards Air Force Base, California, USA (Dec. 1985) and experienced private pilot. Following a career of 15 years in (experimental) flight-testing, of which the last 5 years as chief experimental flight-test, he founded AvioConsult and dedicated himself to improving the safety of aviation using his knowledge of experimental flight-testing. Copyright © 2012, AvioConsult. All rights reserved. The copyright of this paper belongs to and remains with AvioConsult unless specifically stated otherwise. By accepting this paper, the recipient agrees that neither this paper nor the information disclosed herein nor any part thereof shall be reproduced or transferred to other documents or used by or disclosed to others for any purpose except as specifically authorized in writing by AvioConsult. AvioConsult has written this paper in good faith, but no representation is made or guarantee given (either express or implied) as to the completeness of the information it contains. -
Guidance for the Implementation of Fdm Precursors
EUROPEAN OPERATORS FLIGHT DATA MONITORING WORKING GROUP B SAFETY PROMOTION Good Practice document GUIDANCE FOR THE IMPLEMENTATION OF FDM PRECURSORS June 2019 Rev 02 Guidance for the Implementation of FDM Precursors | Rev 02 Contents Table of Revisions .............................................................................................................................5 Introduction ......................................................................................................................................6 Occurrence Reporting and FDM interaction ............................................................................................ 6 Precursor Description ................................................................................................................................ 6 Methodology for Flight Data Monitoring ................................................................................................. 9 Runway Excursions (RE) ..................................................................................................................11 RE01 – Incorrect Performance Calculation ............................................................................................. 12 RE02 – Inappropriate Aircraft Configuration .......................................................................................... 14 RE03 – Monitor CG Position .................................................................................................................... 16 RE04 – Reduced Elevator Authority ....................................................................................................... -
PROPULSION SYSTEM/FLIGHT CONTROL INTEGRATION for SUPERSONIC AIRCRAFT Paul J
PROPULSION SYSTEM/FLIGHT CONTROL INTEGRATION FOR SUPERSONIC AIRCRAFT Paul J. Reukauf and Frank W. Burcham , Jr. NASA Dryden Flight Research Center SUMMARY The NASA Dryden Flight Research Center is engaged in several programs to study digital integrated control systems. Such systems allow minimization of undesirable interactions while maximizing performance at all flight conditions. One such program is the YF-12 cooperative control program. In this program, the existing analog air-data computer, autothrottle, autopilot, and inlet control systems are to be converted to digital systems by using a general purpose airborne computer and interface unit. First, the existing control laws are to be programed and tested in flight. Then, integrated control laws, derived using accurate mathematical models of the airplane and propulsion system in conjunction with modern control techniques, are to be tested in flight. Analysis indicates that an integrated autothrottle-autopilot gives good flight path control and that observers can be used to replace failed sensors. INTRODUCTION Supersonic airplanes, such as the XB-70, YF-12, F-111, and F-15 airplanes, exhibit strong interactions between the engine and the inlet or between the propul- sion system and the airframe (refs. 1 and 2) . Taking advantage of possible favor- able interactions and eliminating or minimizing unfavorable interactions is a chal- lenging control problem with the potential for significant improvements in fuel consumption, range, and performance. In the past, engine, inlet, and flight control systems were usually developed separately, with a minimum of integration. It has often been possible to optimize the controls for a single design point, but off-design control performance usually suffered. -
Constraints for STOL Operations in South Florida Conurbation Cedric Y
Constraints for STOL Operations in South Florida Conurbation Cedric Y. Justin June 2021 Based on research previously published: Development of a Methodology for Parametric Analysis of STOL Airpark Geo-Density, Robinson et al. AIAA AVIATION 2018 Door-to-Door Travel Time Comparative Assessment for Conventional Transportation Methods and Short Takeoff and Landing On Demand Mobility Concepts, Wei et al. AIAA AVIATION 2018 Wind and Obstacles Impact on Airpark Placement for STOL-based Sub-Urban Air Mobility, Somers et al., AIAA AVIATION 2019 Optimal Siting of Sub-Urban Air Mobility (sUAM) Ground Architectures using Network Flow Formulation, Venkatesh et al, AIAA AVIATION 2020 Comparative Assessment of STOL-based Sub-Urban Air Mobility Operations in Massachusetts and South Florida, Justin et al. AIAA AVIATION 2020 Current Market Segmentation ? VTOL CTOL CTOL CTOL CTOL Capacity ? 200-400+ pax Twin Aisle Are there 120-210 pax scenarios where Single Aisle an intermediate solution using 50-90 pax STOL vehicles and Regional Aircraft sitting in- Design range below 300 nm Commuters between UAM 9-50 pax Flight time below 1.5 hours Thin-Haul and thin-haul 9 to 50 seat capacity operations exists? 4-9 pax Sub-Urban Missions 50-150 nm Air Mobility 4 to 9 revenue-seats Missions below 50 nm Urban Air Mobility 1-4 pax 1 to 4 revenue-seats 50 nm 300 nm 500 nm 3000 nm 6000+ nm Artwork Credit Uber Design Range 2 Introduction • Population, urbanization, and congestion Atlanta, GA Miami, FL Dallas, TX Los Angeles, CA have increased steadily over the past several decades • Increasing delays damage the environment and substantially impact the economy Driving time: 8 min. -
GENERAL ENGINE BLEED Fokker 50
Fokker 50 - Bleed Air System GENERAL Bleed-air is used for airconditioning, pressurization, airframe and engine air intake de-icing, and for pressurizing the hydraulic tank. Bleed-air is supplied by the engines. For aircraft equipped with APU On the ground bleed-air can be supplied by the APU for air conditioning. ENGINE BLEED Tappings Bleed-air is obtained via tappings on each engine, referred to as Low-Pressure (LP) bleed and High-Pressure (HP) bleed. LP-bleed is normally in use during flight. HP-bleed will be used at idling and low engine speeds, when LP-bleed is insufficient. The HP-bleed valve will open automatically provided the BLEED push button, located at the AIR CONDITIONING panel, is blank. Bleed-air from the HP-Bleed is prevented from flowing into the LP-bleed by a check valve. Duct leak detection A duct leak between the engine tappings and the firewall, resulting in a significant leakage of bleed-air, is monitored by the engine fire detection and warning system. Distribution Bleed-air from both engines is used to supply the following services: • Airframe, and engine air intake de-icing, see ICE AND RAIN PROTECTION • Hydraulic tank pressurization, see HYDRAULIC SYSTEM. • Airconditioning and pressurization, see below. • If mentioned in aircraft system deviation table: Watertank pressurization, see AIRCRAFT GENERAL. Page 1 Fokker 50 - Bleed Air System BLEED AIR FOR AIRCONDITIONING Supply Controls and indicators are located at the AIRCONDITIONING panel. Bleed-air is available when the engines are running and the BLEED push buttons are blank. When a BLEED push button is depressed to OFF, the Pressure Regulating/Shut-Off valve (PR/SO) and the HP- bleed valve close. -
COM(79)311 Final Brussels / 6Th July 1979
ARCHIVES HISTORIQUES DE LA COMMISSION COLLECTION RELIEE DES DOCUMENTS "COM" COM (79) 311 Vol. 1979/0118 Disclaimer Conformément au règlement (CEE, Euratom) n° 354/83 du Conseil du 1er février 1983 concernant l'ouverture au public des archives historiques de la Communauté économique européenne et de la Communauté européenne de l'énergie atomique (JO L 43 du 15.2.1983, p. 1), tel que modifié par le règlement (CE, Euratom) n° 1700/2003 du 22 septembre 2003 (JO L 243 du 27.9.2003, p. 1), ce dossier est ouvert au public. Le cas échéant, les documents classifiés présents dans ce dossier ont été déclassifiés conformément à l'article 5 dudit règlement. In accordance with Council Regulation (EEC, Euratom) No 354/83 of 1 February 1983 concerning the opening to the public of the historical archives of the European Economic Community and the European Atomic Energy Community (OJ L 43, 15.2.1983, p. 1), as amended by Regulation (EC, Euratom) No 1700/2003 of 22 September 2003 (OJ L 243, 27.9.2003, p. 1), this file is open to the public. Where necessary, classified documents in this file have been declassified in conformity with Article 5 of the aforementioned regulation. In Übereinstimmung mit der Verordnung (EWG, Euratom) Nr. 354/83 des Rates vom 1. Februar 1983 über die Freigabe der historischen Archive der Europäischen Wirtschaftsgemeinschaft und der Europäischen Atomgemeinschaft (ABI. L 43 vom 15.2.1983, S. 1), geändert durch die Verordnung (EG, Euratom) Nr. 1700/2003 vom 22. September 2003 (ABI. L 243 vom 27.9.2003, S. -
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner Andrew S. Hahn 1 NASA Langley Research Center, Hampton, VA, 23681 Most jet airliner conceptual designs adhere to conventional takeoff and landing performance. Given this predominance, takeoff and landing performance has not been critical, since it has not been an active constraint in the design. Given that the demand for air travel is projected to increase dramatically, there is interest in operational concepts, such as Metroplex operations that seek to unload the major hub airports by using underutilized surrounding regional airports, as well as using underutilized runways at the major hub airports. Both of these operations require shorter takeoff and landing performance than is currently available for airliners of approximately 100-passenger capacity. This study examines the issues of modeling performance in this now critical flight regime as well as the impact of progressively reducing takeoff and landing field length requirements on the aircraft’s characteristics. Nomenclature CTOL = conventional takeoff and landing FAA = Federal Aviation Administration FAR = Federal Aviation Regulation RJ = regional jet STOL = short takeoff and landing UCD = three-dimensional Weissinger lifting line aerodynamics program I. Introduction EMAND for air travel over the next fifty to D seventy-five years has been projected to be as high as three times that of today. Given that the major airport hubs are already congested, and that the ability to increase capacity at these airports by building more full- size runways is limited, unconventional solutions are being considered to accommodate the projected increased demand. Two possible solutions being considered are: Metroplex operations, and using existing underutilized runways at the major hub airports. -
United States Rocket Research and Development During World War II
United States Rocket Research and Development During World War II Unidentified U.S. Navy LSM(R) (Landing Ship Medium (Rocket)) launching barrage rockets during a drill late in the Second World War. Image courtesy of the U.S. National Archives and Records Administration. and jet-assisted takeoff (JATO) units for piston-pow- Over the course of the Second World War, rockets ered attack fighters and bombers. Wartime American evolved from scientific and technical curiosities into rocket research evolved along a number of similar and practical weapons with specific battlefield applications. overlapping research trajectories. Both the U.S. Navy The Allied and Axis powers both pursued rocket re- and Army (which included the Army Air Forces) devel- search and development programs during the war. Brit- oped rockets for ground bombardment purposes. The ish and American rocket scientists and engineers (and services also fielded aerial rockets for use by attack their Japanese adversaries) mainly focused their efforts aircraft. The Navy worked on rocket-powered bombs on tactical applications using solid-propellant rockets, for antisubmarine warfare, while the Army developed while the Germans pursued a variety of strategic and the handheld bazooka antitank rocket system. Lastly, tactical development programs primarily centered on both the Army and Navy conducted research into JATO liquid-propellant rockets. German Army researchers units for use with bombers and seaplanes. Throughout led by Wernher von Braun spent much of the war de- the war, however, limited coordination between the veloping the A-4 (more popularly known as the V-2), armed services and federal wartime planning bodies a sophisticated long-range, liquid-fueled rocket that hampered American rocket development efforts and led was employed to bombard London and Rotterdam late to duplicated research and competition amongst pro- in the war. -
Gemini Series PFD
Gemini Series PFD Installation/User Manual 8300-083 Rev D Table of Contents Table of Contents ............................................................................................................................... 2 Document Revision Level & Notes ................................................................................................................ 4 Instrument Installation ................................................................................................................................... 5 Mounting Considerations................................................................................................................ 5 Wiring Considerations ..................................................................................................................... 5 Pitot and Static Connections .......................................................................................................... 5 RFI/EMI Considerations .................................................................................................................. 6 Getting Acquainted With Your Gemini PFD................................................................................................. 7 Gemini PFD Display........................................................................................................................... 7 Using the Touch Screen.................................................................................................................... 8 Info Page Display............................................................................................................................... -
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. -
Iv Jornadas Aeronáuticas De Gran Canaria
IV JORNADAS AERONÁUTICAS DE GRAN CANARIA _ ^ mM MAYO - 2008 IV JORNADAS AERONÁUTICAS DE GRAN CANARIA MAYO-2008 REAL SOCIEDAD ECONÓMICA DE AWOOS DEL PAÍS DE ORAK CANARIA OBRA FINANCIADA POR: DIRECCIÓN REGIONAL DE NAVEGACIÓN AÉREA DE CANARIAS Aena~Ji< Dirección Regional de Navegación Aérea INSTITUCIONES QUE HAN PARTICIPADO EN LA FINANCIACIÓN DE LAS ACTIVIDADES DE LA RSEAP DURANTE EL AÑO 2008: Secretaría de Estado de Universidades e Investigación. Ministerio de Educación y Ciencia. i Gobterno de Cuiulai Consejería de Educación, Cultura y Deportes del Gobierno ^ de Canarias. Gi.kk,* Excmo. Cabildo de Gran Canaria. Gran Canana Excmo. Ayuntamiento de Las Palmas de Gran Canaria. © Por los textos: los autores © Por esta edición: Dirección Regional de Navegación Aérea de Canarias Real Sociedad Económica de Amigos del País de Gran Canaria Documentación gráfica: Salvo las fotografías de carácter general que pertenecen a la Real Sociedad Económica de Amigos del País de Gran Canaria, el resto documental gráfico ha sido proporcionado por cada uno de los conferenciantes. Coordinación y maquetación: Manuel Ramos Almenara y Cristina Marín Sintes I.S.B.N.: 84 921673-1-9 Depósito Legal: G. C. 1377 - 2008. Imprime: TEGRARTE, S.L. TELDE (GRAN CANARIA) PORTADA: Sala de Operaciones del Centro de Control de Tránsito Aéreo de Canarias. Fotografía cedida por la Dirección Regional de Navegación Aérea (AENA). CONTRAPORTADA: Patrulla Águila del Ejército del Aire, sobre el cielo de Las Canteras. Fotografía cedida por el coronel de Aviación don Fabriciano Marián Pérez. f f y IV JORNADAS AERONÁUTICAS DE GRAN CANARIA MAYO - 2008 ÍNDICE IV Jomadas Aeronáuticas de Gran Canaria 9 Francisco Marín Lloris, marqués de la Frontera.