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Remote Pilot – Small Unmanned Aircraft Systems Study Guide
F FAA-G-8082-22 U.S. Department of Transportation Federal Aviation Administration Remote Pilot – Small Unmanned Aircraft Systems Study Guide August 2016 Flight Standards Service Washington, DC 20591 This page intentionally left blank. Preface The Federal Aviation Administration (FAA) has published the Remote Pilot – Small Unmanned Aircraft Systems (sUAS) Study Guide to communicate the knowledge areas you need to study to prepare to take the Remote Pilot Certificate with an sUAS rating airman knowledge test. This Remote Pilot – Small Unmanned Aircraft Systems Study Guide is available for download from faa.gov. Please send comments regarding this document to [email protected]. Remote Pilot – Small Unmanned Aircraft Systems Study Guide i This page intentionally left blank. Remote Pilot – Small Unmanned Aircraft Systems Study Guide ii Table of Contents Introduction ........................................................................................................................... 1 Obtaining Assistance from the Federal Aviation Administration (FAA) .............................................. 1 FAA Reference Material ...................................................................................................................... 1 Chapter 1: Applicable Regulations .......................................................................................... 3 Chapter 2: Airspace Classification, Operating Requirements, and Flight Restrictions .............. 5 Introduction ........................................................................................................................................ -
Easy Access Rules for Auxiliary Power Units (CS-APU)
APU - CS Easy Access Rules for Auxiliary Power Units (CS-APU) EASA eRules: aviation rules for the 21st century Rules and regulations are the core of the European Union civil aviation system. The aim of the EASA eRules project is to make them accessible in an efficient and reliable way to stakeholders. EASA eRules will be a comprehensive, single system for the drafting, sharing and storing of rules. It will be the single source for all aviation safety rules applicable to European airspace users. It will offer easy (online) access to all rules and regulations as well as new and innovative applications such as rulemaking process automation, stakeholder consultation, cross-referencing, and comparison with ICAO and third countries’ standards. To achieve these ambitious objectives, the EASA eRules project is structured in ten modules to cover all aviation rules and innovative functionalities. The EASA eRules system is developed and implemented in close cooperation with Member States and aviation industry to ensure that all its capabilities are relevant and effective. Published February 20181 1 The published date represents the date when the consolidated version of the document was generated. Powered by EASA eRules Page 2 of 37| Feb 2018 Easy Access Rules for Auxiliary Power Units Disclaimer (CS-APU) DISCLAIMER This version is issued by the European Aviation Safety Agency (EASA) in order to provide its stakeholders with an updated and easy-to-read publication. It has been prepared by putting together the certification specifications with the related acceptable means of compliance. However, this is not an official publication and EASA accepts no liability for damage of any kind resulting from the risks inherent in the use of this document. -
Cranfield University Xue Longxian Actuation
CRANFIELD UNIVERSITY XUE LONGXIAN ACTUATION TECHNOLOGY FOR FLIGHT CONTROL SYSTEM ON CIVIL AIRCRAFT SCHOOL OF ENGINEERING MSc by Research THESIS CRANFIELD UNIVERSITY SCHOOL OF ENGINEERING MSc by Research THESIS Academic Year 2008-2009 XUE LONGXIAN Actuation Technology for Flight Control System on Civil Aircraft Supervisor: Dr. C. P. Lawson Prof. J. P. Fielding January 2009 This thesis is submitted in fulfilment of the requirements for the degree of Master of Science © Cranfield University 2009. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner. ABSTRACT This report addresses the author’s Group Design Project (GDP) and Individual Research Project (IRP). The IRP is discussed primarily herein, presenting the actuation technology for the Flight Control System (FCS) on civil aircraft. Actuation technology is one of the key technologies for next generation More Electric Aircraft (MEA) and All Electric Aircraft (AEA); it is also an important input for the preliminary design of the Flying Crane, the aircraft designed in the author’s GDP. Information regarding actuation technologies is investigated firstly. After initial comparison and engineering consideration, Electrohydrostatic Actuation (EHA) and variable area actuation are selected for further research. The tail unit of the Flying Crane is selected as the case study flight control surfaces and is analysed for the requirements. Based on these requirements, an EHA system and a variable area actuation system powered by localised hydraulic systems are designed and sized in terms of power, mass and Thermal Management System (TMS), and thereafter the reliability of each system is estimated and the safety is analysed. -
Electrical Power Codde 1 Page 1 / 6 General Dgt97831 Issue 2
FALCON 7X 02-24-05 ATA 24 – ELECTRICAL POWER CODDE 1 PAGE 1 / 6 GENERAL DGT97831 ISSUE 2 ACRONYMS AC Alternative Current APU Auxiliary Power Unit BC Battery Contactor BIT Built In Test BTC Bus Tie Contactor CAS Crew Alerting System CB Circuit Breaker CLSC Cabin Load Shed Contactor CMC Central Maintenance Computer DC Direct Current ECU Electronic Control Unit EEC Engine Electronic Controller FADEC Full Authority Digital Electronic Control FBW Fly By Wire GCU Generator Control Unit GLC Generator Line Contactor GLSC Galley Load Shed Contactor GPC Ground Power Contactor GPU Ground Power Unit GSB Ground Service Bus LFSPDB Left Front Secondary Power Distribution Box LH Left Hand LPPDB Left Primary Power Distribution Box LRSPDB Left Rear Secondary Power Distribution Box LS Load shed MAU Modular Avionic Unit MDU Multi function Display Unit MMEL Master Minimum Equipment List O/C OverCurrent OP Overhead Panel OVHT OVerHeaT PDCU Power Distribution Control Unit PFCS Primary Flight Control System PMA Permanent Magnet Alternator PPDB Primary Power Distribution Box RAT Ram Air Turbine RATC Ram Air Turbine Contactor DASSAULT AVIATION Proprietary Data 02-24-05 FALCON 7X ATA 24 – ELECTRICAL POWER PAGE 2 / 6 CODDE 1 GENERAL ISSUE 2 DGT97831 RFSPDB Right Front Secondary Power Distribution Box RH Right Hand RPPDB Right Primary Power Distribution Box RRSPDB Right Rear Secondary Power Distribution Box S/G Starter Generator SOV Shut Off Valve SPDB Secondary Power Distribution Box SSPC Solid State Power Controller TRU Transformer Rectifier Unit VDC Volt Direct Courant DASSAULT AVIATION Proprietary Data FALCON 7X 02-24-05 ATA 24 – ELECTRICAL POWER CODDE 1 PAGE 3 / 6 GENERAL DGT97831 ISSUE 2 INTRODUCTION The Falcon 7X uses 28 Volts DC power for operation of the various systems installed in the airplane. -
Integrating Air Systems in Aircraft Multidisciplinary Design Optimization Ali Tfaily Department of Mechanical Engineering Mcgil
Integrating Air Systems in Aircraft Multidisciplinary Design Optimization Ali Tfaily Department of Mechanical Engineering McGill University, Montreal August 2018 A thesis submitted to McGill University in partial fulfillment of the requirements of the degree of Master of Engineering ACKNOWLEDGEMENTS I would like to thank my supervisor, Prof. Michael Kokkolaras, for his support and guidance throughout my time as his student. I am honored to have worked along a supervisor that always helped me in my work and even my personal life. I am grateful to members of Bombardier’s Advanced Product Development department for their insights on aircraft design and optimization. Special acknowledgment is given to the Thermodynamics department at Bombardier Product Development Engineering, namely Sebastien Beaulac, Hongzhi Wang, Jean-Francois Reis, and Emmanuel Germaine, who provided expertise that greatly assisted this research. I would also like to thank Jean Brousseau for sharing his knowledge on air systems design. I am very grateful to John Ferneley, Susan Liscouët-Hanke, Pat Piperni, and Fassi Kafyeke who were supportive of my career goals and provided me the means to pursue these goals. Finally, I am grateful to my friends and family for their constant support and encouragement throughout the ups and downs of my studies. ABSTRACT The strong interactions between aircraft and air systems necessitate the integration of the latter to multidisciplinary design optimization (MDO) considerations of the former. This research presents such a methodology considering environmental control and ice protection systems. These systems consume pressurized bleed air from the aircraft’s engines to perform their respective functions. We first describe the models used to predict the behavior of these systems and then propose different approaches to their integration into an existing aircraft MDO environment. -
PRELIMINARY KNKT.17.10.31.04 Aircraft
KOMITE NASIONAL KESELAMATAN TRANSPORTASI REPUBLIC OF INDONESIA PRELIMINARY KNKT.17.10.31.04 Aircraft Accident Investigation Report PT. Batik Air Boeing 737-800; PK-LBY Inflight from Jakarta to Medan Republic of Indonesia 24 October 2017 JETPHOTOS.NET Image copyright : Dimas Satrio Baringgo 2017 This Preliminary Report was produced by the Komite Nasional Keselamatan Transportasi (KNKT), Transportation Building, 3rd Floor, Jalan Medan Merdeka Timur No. 5 Jakarta 10110, Indonesia. The report is based upon the initial investigation carried out by the KNKT in accordance with Annex 13 to the Convention on International Civil Aviation Organization, the Indonesian Aviation Act (UU No. 1/2009) and Government Regulation (PP No. 62/2013). The preliminary report consists of factual information collected until the preliminary report published. This report will not include analysis and conclusion. Readers are advised that the KNKT investigates for the sole purpose of enhancing aviation safety. Consequently, the KNKT reports are confined to matters of safety significance and may be misleading if used for any other purpose. As the KNKT believes that safety information is of greatest value if it is passed on for the use of others, readers are encouraged to copy or reprint for further distribution, acknowledging the KNKT as the source. When the KNKT makes recommendations as a result of its investigations or research, safety is its primary consideration. However, the KNKT fully recognizes that the implementation of recommendations arising from its investigations will in some cases incur a cost to the industry. Readers should note that the information in KNKT reports and recommendations is provided to promote aviation safety. -
Systems Engineering Approach in Aircraft Design Education; Techniques and Challenges
Paper ID #11232 Systems Engineering Approach in Aircraft Design Education; Techniques and Challenges Prof. Mohammad Sadraey, Daniel Webster College Mohammad H. Sadraey is an Associate Professor in the Engineering School at the Daniel Webster Col- lege, Nashua, New Hampshire, USA. Dr. Sadraey’s main research interests are in aircraft design tech- niques, and design and automatic control of unmanned aircraft. He received his MSc. in Aerospace Engineering in 1995 from RMIT, Melbourne, Australia, and his Ph.D. in Aerospace Engineering from the University of Kansas, Kansas, USA. Dr. Sadraey is a senior member of the American Institute of Aeronautics and Astronautics (AIAA), and a member of American Society for Engineering Education (ASEE). Prof. Nicholas Bertozzi, Daniel Webster College Nick Bertozzi is a Professor of Engineering at Daniel Webster College (DWC) and Dean of the School of Engineering and Computer Science (SECS). His major interest over the past 18 years has been the concurrent engineering design process, an interest that was fanned into flame by attending an NSF faculty development workshop in 1996 led by Ron Barr and Davor Juricic. Nick has a particular interest in help- ing engineering students develop good communications skills and has made this a SECS priority. Over the past ten years he and other engineering and humanities faculty colleagues have mentored a number of undergraduate student teams who have co-authored and presented papers and posters at Engineering Design Graphics Division (EDGD) and other ASEE, CDIO (www.cdio.org), and American Institute of Aeronautics and Astronautics (AIAA) meetings as well. Nick was delighted to serve as the EDGD pro- gram chair for the 2008 ASEE Summer Conference and as program co-chair with Kathy Holliday-Darr for the 68th EDGD Midyear meeting at WPI in October 2013. -
Aircraft Collection
A, AIR & SPA ID SE CE MU REP SEU INT M AIRCRAFT COLLECTION From the Avenger torpedo bomber, a stalwart from Intrepid’s World War II service, to the A-12, the spy plane from the Cold War, this collection reflects some of the GREATEST ACHIEVEMENTS IN MILITARY AVIATION. Photo: Liam Marshall TABLE OF CONTENTS Bombers / Attack Fighters Multirole Helicopters Reconnaissance / Surveillance Trainers OV-101 Enterprise Concorde Aircraft Restoration Hangar Photo: Liam Marshall BOMBERS/ATTACK The basic mission of the aircraft carrier is to project the U.S. Navy’s military strength far beyond our shores. These warships are primarily deployed to deter aggression and protect American strategic interests. Should deterrence fail, the carrier’s bombers and attack aircraft engage in vital operations to support other forces. The collection includes the 1940-designed Grumman TBM Avenger of World War II. Also on display is the Douglas A-1 Skyraider, a true workhorse of the 1950s and ‘60s, as well as the Douglas A-4 Skyhawk and Grumman A-6 Intruder, stalwarts of the Vietnam War. Photo: Collection of the Intrepid Sea, Air & Space Museum GRUMMAN / EASTERNGRUMMAN AIRCRAFT AVENGER TBM-3E GRUMMAN/EASTERN AIRCRAFT TBM-3E AVENGER TORPEDO BOMBER First flown in 1941 and introduced operationally in June 1942, the Avenger became the U.S. Navy’s standard torpedo bomber throughout World War II, with more than 9,836 constructed. Originally built as the TBF by Grumman Aircraft Engineering Corporation, they were affectionately nicknamed “Turkeys” for their somewhat ungainly appearance. Bomber Torpedo In 1943 Grumman was tasked to build the F6F Hellcat fighter for the Navy. -
Press Release
PRESS RELEASE East Meadow, March 19, 2018 Lufthansa begins biometric boarding at LAX, paving the way for nationwide usage at airports − Biometric technologies simplify, de-stress and significantly speed up airplane boarding − During the initial trial, Lufthansa boarded an A380 in about 20 minutes − Following Lufthansa’s successful LAX trial, the Airline will introduce biometrics boarding at other U.S. airports nationwide Lufthansa Group, as part of its ongoing efforts to digitalize the travel world, has launched hassle- free, one-step biometric boarding utilizing facial recognition. This innovative pilot, enabled through a collaboration with Lufthansa Group’s longstanding IT partner, Amadeus, as well as U.S. Customs and Border Protection (CBP), Los Angeles World Airports Authority (LAWA), and Vision Box, is now available at Los Angeles International Airport (LAX). During initial trials, Lufthansa received very positive feedback from guests and boarded approximately 350 passengers onto an A380 in about 20 minutes. Here is how it works: • Self-boarding gates with sophisticated facial recognition cameras capture passengers’ facial images as they approach the device • This image is securely sent to the CBP database for real-time matching and verification • After a successful, instantaneous match within a few seconds, the system recognizes the passenger as “boarded” • The passenger no longer needs to show a boarding pass or passport at the gate “The increasing need for airlines, airports and authorities to offer faster and more convenient processes for guests to move through the airport creates a unique opportunity for the use of biometrics,” said Bjoern Becker, Senior Director, Product Management Ground and Digital Services for Lufthansa. -
AP3456 the Central Flying School (CFS) Manual of Flying: Volume 4 Aircraft Systems
AP3456 – 4-1- Hydraulic Systems CHAPTER 1 - HYDRAULIC SYSTEMS Introduction 1. Hydraulic power has unique characteristics which influence its selection to power aircraft systems instead of electrics and pneumatics, the other available secondary power systems. The advantages of hydraulic power are that: a. It is capable of transmitting very high forces. b. It has rapid and precise response to input signals. c. It has good power to weight ratio. d. It is simple and reliable. e. It is not affected by electro-magnetic interference. Although it is less versatile than present generation electric/electronic systems, hydraulic power is the normal secondary power source used in aircraft for operation of those aircraft systems which require large power inputs and precise and rapid movement. These include flying controls, flaps, retractable undercarriages and wheel brakes. Principles 2. Basic Power Transmission. A simple practical application of hydraulic power is shown in Fig 1 which depicts a closed system typical of that used to operate light aircraft wheel brakes. When the force on the master cylinder piston is increased slightly by light operation of the brake pedals, the slave piston will extend until the brake shoe contacts the brake drum. This restriction will prevent further movement of the slave and the master cylinder. However, any increase in force on the master cylinder will increase pressure in the fluid, and it will therefore increase the braking force acting on the shoes. When braking is complete, removal of the load from the master cylinder will reduce hydraulic pressure, and the brake shoe will retract under spring tension. -
AFRAA Annual Report 2019
IRLINES ASS A PAGNIES O OM AERI C 20N S C EN 19 E N I A D ES A N A T C IO F I T R I I O R IA C C A I N F O N S E S A S A ANNUAL AFRAA REPORT Amadeus Airline Platform Bringing SIMPLICITY to airlines You can follow us on: AmadeusITGroup amadeus.com/airlineplatform AFRAA Executive Committee (EXC) Members 2019 AIR MAURITIUS (MK) RWANDAIR (WB) PRESIDENT OF AFRAA CHAIRPERSON OF THE EXECUTIVE COMMITTEE Mr. Somas Appavou Ms. Yvonne Makolo Chief Executive Officer Chief Executive Officer CONGO AIRWAYS (8Z) KENYA AIRWAYS (KQ) CAMAIR-CO (QC) Mr. Desire Balazire Esono Mr. Sebastian Mikosz Mr. Louis Roger Njipendi Kouotou 1st Vice Chairman of the EXC 2nd Vice Chairman of the EXC Chief Executive Officer Chief Executive Officer Chief Executive Officer ROYAL AIR MAROC (AT) EGYPTAIR (MS) TUNISAIR (TU) Mr. Abdelhamid Addou Capt. Ahmed Adel Mr. Ilyes Mnakbi Chief Executive Officer Chairman & Chief Executive Officer Chief Executive Officer ETHIOPIAN AIRLINES (ET) AIR ZIMBABWE (UM) AIR NAMIBIA (SW) MAURITANIA AIRLINES (L6) Mr. Tewolde GebreMariam Mr. Joseph Makonise Mr. Xavier Masule Mrs. Amal Mint Maoulod Chief Executive Officer Chief Executive Officer Chief Executive Officer Chief Executive Officer ANNUAL REPORT 2019 I Foreword raffic growth in Africa has been consistently increasing since 2011. The demand for air passenger services remained strong in 2018 with a 6.9% year Ton year growth. Those good results were supported by the good global economic environment particularly in the first half of the year. Unlike passenger traffic, air freight demand recorded a very weak performance in 2018 compared to 2017. -
Issues Statement
ANTICIPATED ACQUISITION BY SABRE CORPORATION OF FARELOGIX INC Issues statement 17 October 2019 The reference 1. On 2 September 2019, the Competition and Markets Authority (CMA), in exercise of its duty under section 33 of the Enterprise Act 2002 (the Act), referred the anticipated acquisition by Sabre Corporation (Sabre) of Farelogix Inc (Farelogix) (the Merger) for further investigation and report by a group of CMA panel members (the Group). 2. In exercise of its duty under section 36(1) of the Act, the CMA must decide: (a) whether arrangements are in progress or in contemplation which, if carried into effect, will result in the creation of a relevant merger situation; and (b) if so, whether the creation of that situation may be expected to result in a substantial lessening of competition (SLC) within any market or markets in the UK for goods or services. 3. In answering these two questions we are required to apply a ‘balance of probabilities’ threshold to our analysis.1 4. In this statement, we set out the main issues we are likely to consider in reaching our decision on the SLC question (paragraph 2(b) above), having had regard to the evidence available to us to date, including the evidence referred to in the CMA’s Phase 1 decision on SLC (the Phase 1 Decision).2 5. We are publishing this issues statement to assist parties submitting evidence to our investigation. The issues statement sets out the issues we currently envisage being relevant to our investigation and we invite parties to notify us if 1 Merger Assessment Guidelines (CC2/OFT1254), paragraph 2.12.