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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. -
ALT / VS Selector/Alerter
ALT / VS Selector / Alerter PN 01279-( ) Pilot’s Operating Handbook ENT ALT SEL ALR DH VS BARO S–TEC * Asterisk indicates pages changed, added, or deleted by List of Effective Pages current revision. Retain this record in front of handbook. Upon receipt of a Record of Revisions revision, insert changes and complete table below. Revision Number Revision Date Insertion Date/Initials 1st Ed. Oct 26, 00 2nd Ed. Jan 15, 08 3rd Ed. Jun 24, 16 3rd Ed. Jun 24, 16 i S–TEC Page Intentionally Blank ii 3rd Ed. Jun 24, 16 S–TEC Table of Contents Sec. Pg. 1 Overview...........................................................................................................1–1 1.1 Document Organization....................................................................1–3 1.2 Purpose..............................................................................................1–3 1.3 General Control Theory....................................................................1–3 1.4 Block Diagram....................................................................................1–4 2 Pre-Flight Procedures...................................................................................2–1 2.1 Pre-Flight Test....................................................................................2–3 3 In-Flight Procedures......................................................................................3–1 3.1 Selector / Alerter Operation..............................................................3–3 3.1.1 Data Entry.............................................................................3–3 -
How Doc Draper Became the Father of Inertial Guidance
(Preprint) AAS 18-121 HOW DOC DRAPER BECAME THE FATHER OF INERTIAL GUIDANCE Philip D. Hattis* With Missouri roots, a Stanford Psychology degree, and a variety of MIT de- grees, Charles Stark “Doc” Draper formulated the basis for reliable and accurate gyro-based sensing technology that enabled the first and many subsequent iner- tial navigation systems. Working with colleagues and students, he created an Instrumentation Laboratory that developed bombsights that changed the balance of World War II in the Pacific. His engineering teams then went on to develop ever smaller and more accurate inertial navigation for aircraft, submarines, stra- tegic missiles, and spaceflight. The resulting inertial navigation systems enable national security, took humans to the Moon, and continue to find new applica- tions. This paper discusses the history of Draper’s path to becoming known as the “Father of Inertial Guidance.” FROM DRAPER’S MISSOURI ROOTS TO MIT ENGINEERING Charles Stark Draper was born in 1901 in Windsor Missouri. His father was a dentist and his mother (nee Stark) was a school teacher. The Stark family developed the Stark apple that was popular in the Midwest and raised the family to prominence1 including a cousin, Lloyd Stark, who became governor of Missouri in 1937. Draper was known to his family and friends as Stark (Figure 1), and later in life was known by colleagues as Doc. During his teenage years, Draper enjoyed tinkering with automobiles. He also worked as an electric linesman (Figure 2), and at age 15 began a liberal arts education at the University of Mis- souri in Rolla. -
Air Force Airframe and Powerplant (A&P) Certification Program
Air Force Airframe and Powerplant (A&P) Certification Program Introduction: Most military aircraft maintenance technicians are eligible to pursue the Federal Aviation Administration (FAA) Airframe & Powerplant (A&P) certification based on documented evidence of 30 months practical aircraft maintenance experience in airframe and powerplant systems per Title 14, Code of Federal Regulations (CFR), Part 65- Certification: Airmen Other Than Flight Crew Members; Subpart D-Mechanics. Air Force education, training and experience and FAA eligibility requirements per Title 14, CFR Part 65.77. This FAA-approved program is a voluntary program which benefits the technician and the Air Force, with consideration to professional development, recruitment, retention, and transition. Completing this program, outlined in the program Qualification Training Package (QTP), will assist technicians in meeting FAA eligibility requirements and being better-prepared for the FAA exams. Three-Tier Program: The program is a three-tier training and experience program. These elements are required for program completion and are important for individual development, knowledge assessment, meeting FAA certification eligibility, and preparation for the FAA exams: Three Online Courses (02AF1-General, 02AF2-Airframe, & 02AF3-Powerplant). On the Job Training (OJT) Qualification Training Package(QTP). Documented evidence of 30 months practical experience in airframe and powerplant systems. Program Eligibility: Active duty, guard and reserve technicians who possess at least a 5-skill level in one of the following aircraft maintenance AFSCs are eligible to enroll: 2A0X1, 2A090, 2A2X1, 2A2X2, 2A2X3, 2A3X3, 2A3X4, 2A3X5, 2A3X7, 2A3X8, 2A390, 2A300, 2A5X1, 2A5X2, 2A5X3, 2A5X4, 2A590, 2A500, 2A6X1, 2A6X3, 2A6X4, 2A6X5, 2A6X6, 2A690, 2A691, 2A600 (except AGE), 2A7X1, 2A7X2, 2A7X3, 2A7X5, 2A790, 2A8X1, 2A8X2, 2A9X1, 2A9X2, and 2A9X3. -
Faa Ac 20-186
U.S. Department Advisory of Transportation Federal Aviation Administration Circular Subject: Airworthiness and Operational Date: 7/22/16 AC No: 20-186 Approval of Cockpit Voice Recorder Initiated by: AFS-300 Change: Systems 1 GENERAL INFORMATION. 1.1 Purpose. This advisory circular (AC) provides guidance for compliance with applicable regulations for the airworthiness and operational approval for required cockpit voice recorder (CVR) systems. Non-required installations may use this guidance when installing a CVR system as a voluntary safety enhancement. This AC is not mandatory and is not a regulation. This AC describes an acceptable means, but not the only means, to comply with Title 14 of the Code of Federal Regulations (14 CFR). However, if you use the means described in this AC, you must conform to it in totality for required installations. 1.2 Audience. We, the Federal Aviation Administration (FAA), wrote this AC for you, the aircraft manufacturers, CVR system manufacturers, aircraft operators, Maintenance Repair and Overhaul (MRO) Organizations and Supplemental Type Certificate (STC) applicants. 1.3 Cancellation. This AC cancels AC 25.1457-1A, Cockpit Voice Recorder Installations, dated November 3, 1969. 1.4 Related 14 CFR Parts. Sections of 14 CFR parts 23, 25, 27, 29, 91, 121, 125, 129, and 135 detail design substantiation and operational approval requirements directly applicable to the CVR system. See Appendix A, Flowcharts, to determine the applicable regulations for your aircraft and type of operation. Listed below are the specific 14 CFR sections applicable to this AC: • Part 23, § 23.1457, Cockpit Voice Recorders. • Part 23, § 23.1529, Instructions for Continued Airworthiness. -
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. -
Installation Manual, Document Number 200-800-0002 Or Later Approved Revision, Is Followed
9800 Martel Road Lenoir City, TN 37772 PPAAVV8800 High-fidelity Audio-Video In-Flight Entertainment System With DVD/MP3/CD Player and Radio Receiver STC-PMA Document P/N 200-800-0101 Revision 6 September 2005 Installation and Operation Manual Warranty is not valid unless this product is installed by an Authorized PS Engineering dealer or if a PS Engineering harness is purchased. PS Engineering, Inc. 2005 © Copyright Notice Any reproduction or retransmittal of this publication, or any portion thereof, without the expressed written permission of PS Engi- neering, Inc. is strictly prohibited. For further information contact the Publications Manager at PS Engineering, Inc., 9800 Martel Road, Lenoir City, TN 37772. Phone (865) 988-9800. Table of Contents SECTION I GENERAL INFORMATION........................................................................ 1-1 1.1 INTRODUCTION........................................................................................................... 1-1 1.2 SCOPE ............................................................................................................................. 1-1 1.3 EQUIPMENT DESCRIPTION ..................................................................................... 1-1 1.4 APPROVAL BASIS (PENDING) ..................................................................................... 1-1 1.5 SPECIFICATIONS......................................................................................................... 1-2 1.6 EQUIPMENT SUPPLIED ............................................................................................ -
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. -
Using an Autothrottle to Compare Techniques for Saving Fuel on A
Iowa State University Capstones, Theses and Graduate Theses and Dissertations Dissertations 2010 Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft Rebecca Marie Johnson Iowa State University Follow this and additional works at: https://lib.dr.iastate.edu/etd Part of the Electrical and Computer Engineering Commons Recommended Citation Johnson, Rebecca Marie, "Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft" (2010). Graduate Theses and Dissertations. 11358. https://lib.dr.iastate.edu/etd/11358 This Thesis is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Graduate Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. Using an autothrottle to compare techniques for saving fuel on A regional jet aircraft by Rebecca Marie Johnson A thesis submitted to the graduate faculty in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Major: Electrical Engineering Program of Study Committee: Umesh Vaidya, Major Professor Qingze Zou Baskar Ganapathayasubramanian Iowa State University Ames, Iowa 2010 Copyright c Rebecca Marie Johnson, 2010. All rights reserved. ii DEDICATION I gratefully acknowledge everyone who contributed to the successful completion of this research. Bill Piche, my supervisor at Rockwell Collins, was supportive from day one, as were many of my colleagues. I also appreciate the efforts of my thesis committee, Drs. Umesh Vaidya, Qingze Zou, and Baskar Ganapathayasubramanian. I would also like to thank Dr. -
P:\Dokumentation\Manual-O\DA 62\7.01.25-E
DA 62 AFM Ice Protection System Supplement S03 FIKI SUPPLEMENT S03 TO THE AIRPLANE FLIGHT MANUAL DA 62 ICE PROTECTION SYSTEM FOR FLIGHT INTO KNOWN ICING Doc. No. : 7.01.25-E Date of Issue of the Supplement : 01-Apr-2016 Design Change Advisory : OÄM 62-003 This Supplement to the Airplane Flight Manual is EASA approved under Approval Number EASA 10058874. This AFM - Supplement is approved in accordance with 14 CFR Section 21.29 for U.S. registered aircraft and is approved by the Federal Aviation Administration. DIAMOND AIRCRAFT INDUSTRIES GMBH N.A. OTTO-STR. 5 A-2700 WIENER NEUSTADT AUSTRIA Page 9-S03-1 Ice Protection System DA 62 AFM FIKI Supplement S03 Intentionally left blank. › Page 9-S03-2 05-May-2017 Rev. 2 Doc. # 7.01.25-E DA 62 AFM Ice Protection System Supplement S03 FIKI 0.1 RECORD OF REVISIONS Rev. Chap- Date of Approval Date of Date Signature Reason Page(s) No. ter Revision Note Approval Inserted Rev. 1 to AFM Supplement S03 to AFM 9-S03-1, Doc. No. FAA 7.01.25-E is 1 0 9-S03-3, 10 Oct 2016 14 Oct 2016 Approval approved by 9-S03-4 EASA with Approval No. EASA 10058874 › Rev. 2 to AFM › Supplement › S03 to AFM › Doc. No. › TR-MÄM › All, except 7.01.25-E is › 2 62-254, 05 May 2017 › All approved 13 Nov 2017 › Corrections Cover Page › under the › authority of › DOA › No.21J.052 › Doc. # 7.01.25-E Rev. 2 05-May-2017 Page 9-S03-3 Ice Protection System DA 62 AFM FIKI Supplement S03 0.3 LIST OF EFFECTIVE PAGES Chapter Page Date 9-S03-1 10-Oct-2016 › 9-S03-2 05-May-2017 › 9-S03-3 05-May-2017 › 9-S03-4 05-May-2017 0 › 9-S03-5 05-May-2017 › 9-S03-6 05-May-2017 › 9-S03-7 05-May-2017 › 9-S03-8 05-May-2017 › 9-S03-9 05-May-2017 › 9-S03-10 05-May-2017 1 › 9-S03-11 05-May-2017 › 9-S03-12 05-May-2017 › appr. -
Lockheed Martin F-35 Lightning II Incorporates Many Significant Technological Enhancements Derived from Predecessor Development Programs
AIAA AVIATION Forum 10.2514/6.2018-3368 June 25-29, 2018, Atlanta, Georgia 2018 Aviation Technology, Integration, and Operations Conference F-35 Air Vehicle Technology Overview Chris Wiegand,1 Bruce A. Bullick,2 Jeffrey A. Catt,3 Jeffrey W. Hamstra,4 Greg P. Walker,5 and Steve Wurth6 Lockheed Martin Aeronautics Company, Fort Worth, TX, 76109, United States of America The Lockheed Martin F-35 Lightning II incorporates many significant technological enhancements derived from predecessor development programs. The X-35 concept demonstrator program incorporated some that were deemed critical to establish the technical credibility and readiness to enter the System Development and Demonstration (SDD) program. Key among them were the elements of the F-35B short takeoff and vertical landing propulsion system using the revolutionary shaft-driven LiftFan® system. However, due to X- 35 schedule constraints and technical risks, the incorporation of some technologies was deferred to the SDD program. This paper provides insight into several of the key air vehicle and propulsion systems technologies selected for incorporation into the F-35. It describes the transition from several highly successful technology development projects to their incorporation into the production aircraft. I. Introduction HE F-35 Lightning II is a true 5th Generation trivariant, multiservice air system. It provides outstanding fighter T class aerodynamic performance, supersonic speed, all-aspect stealth with weapons, and highly integrated and networked avionics. The F-35 aircraft