Unmanned Aircraft Systems (UAS) Operational Approval
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Off Airport Ops Guide
Off Airport Ops Guide TECHNIQUES FOR OFF AIRPORT OPERATIONS weight and balance limitations for your aircraft. Always file a flight plan detailing the specific locations you intend Note: This document suggests techniques and proce- to explore. Make at least 3 recon passes at different levels dures to improve the safety of off-airport operations. before attempting a landing and don’t land unless you’re It assumes that pilots have received training on those sure you have enough room to take off. techniques and procedures and is not meant to replace instruction from a qualified and experienced flight instruc- High Level: Circle the area from different directions to de- tor. termine the best possible landing site in the vicinity. Check the wind direction and speed using pools of water, drift General Considerations: Off-airport operations can be of the plane, branches, grass, dust, etc. Observe the land- extremely rewarding; transporting people and gear to lo- ing approach and departure zone for obstructions such as cations that would be difficult or impossible to reach in trees or high terrain. any other way. Operating off-airport requires high perfor- mance from pilot and aircraft and acquiring the knowledge Intermediate: Level: Make a pass in both directions along and experience to conduct these operations safely takes either side of the runway to check for obstructions and time. Learning and practicing off-airport techniques under runway length. Check for rock size. Note the location of the supervision of an experienced flight instructor will not the touchdown area and roll-out area. Associate land- only make you safer, but also save you time and expense. -
4. Lunar Architecture
4. Lunar Architecture 4.1 Summary and Recommendations As defined by the Exploration Systems Architecture Study (ESAS), the lunar architecture is a combination of the lunar “mission mode,” the assignment of functionality to flight elements, and the definition of the activities to be performed on the lunar surface. The trade space for the lunar “mission mode,” or approach to performing the crewed lunar missions, was limited to the cislunar space and Earth-orbital staging locations, the lunar surface activities duration and location, and the lunar abort/return strategies. The lunar mission mode analysis is detailed in Section 4.2, Lunar Mission Mode. Surface activities, including those performed on sortie- and outpost-duration missions, are detailed in Section 4.3, Lunar Surface Activities, along with a discussion of the deployment of the outpost itself. The mission mode analysis was built around a matrix of lunar- and Earth-staging nodes. Lunar-staging locations initially considered included the Earth-Moon L1 libration point, Low Lunar Orbit (LLO), and the lunar surface. Earth-orbital staging locations considered included due-east Low Earth Orbits (LEOs), higher-inclination International Space Station (ISS) orbits, and raised apogee High Earth Orbits (HEOs). Cases that lack staging nodes (i.e., “direct” missions) in space and at Earth were also considered. This study addressed lunar surface duration and location variables (including latitude, longi- tude, and surface stay-time) and made an effort to preserve the option for full global landing site access. Abort strategies were also considered from the lunar vicinity. “Anytime return” from the lunar surface is a desirable option that was analyzed along with options for orbital and surface loiter. -
(VL for Attrid
ECCAIRS Aviation 1.3.0.12 Data Definition Standard English Attribute Values ECCAIRS Aviation 1.3.0.12 VL for AttrID: 391 - Event Phases Powered Fixed-wing aircraft. (Powered Fixed-wing aircraft) 10000 This section covers flight phases specifically adopted for the operation of a powered fixed-wing aircraft. Standing. (Standing) 10100 The phase of flight prior to pushback or taxi, or after arrival, at the gate, ramp, or parking area, while the aircraft is stationary. Standing : Engine(s) Not Operating. (Standing : Engine(s) Not Operating) 10101 The phase of flight, while the aircraft is standing and during which no aircraft engine is running. Standing : Engine(s) Start-up. (Standing : Engine(s) Start-up) 10102 The phase of flight, while the aircraft is parked during which the first engine is started. Standing : Engine(s) Run-up. (Standing : Engine(s) Run-up) 990899 The phase of flight after start-up, during which power is applied to engines, for a pre-flight engine performance test. Standing : Engine(s) Operating. (Standing : Engine(s) Operating) 10103 The phase of flight following engine start-up, or after post-flight arrival at the destination. Standing : Engine(s) Shut Down. (Standing : Engine(s) Shut Down) 10104 Engine shutdown is from the start of the shutdown sequence until the engine(s) cease rotation. Standing : Other. (Standing : Other) 10198 An event involving any standing phase of flight other than one of the above. Taxi. (Taxi) 10200 The phase of flight in which movement of an aircraft on the surface of an aerodrome under its own power occurs, excluding take- off and landing. -
Royal Institute of Technology
Royal Institute of Technology bachelor thesis aeronautics Transport Aircraft Conceptual Design Albin Karlsson & Anton Lomaeus Supervisor: Christer Fuglesang & Fredrik Edelbrink Stockholm, Sweden June 15, 2017 This page is intentionally left blank. Abstract A conceptual design for a transport aircraft has been created, tailored for human- itarian missions along the equator with its home base in the European Union while optimizing for fuel efficiency and speed. An initial estimate of the empty weight was made using historical data and Breguet equations, based on a required payload of 60 tonnes and range of 5 500 nautical miles. A constraint diagram consisting of require- ments for stall speed, takeoff distance, climb rate and landing distance was used to determine wing loading and thrust to weight ratio, resulting in a main wing area of 387 m2 and thrust to weight ratio of 0:224, for which two Rolls Royce Trent 1000-H engines were selected. A high aspect ratio wing was designed with blended winglets to optimize against lift induced drag. Wing placement and tail volume were decided by iterative calculations, resulting in a centre of lift located aft of the centre of gravity during all stages of the mission. The resulting aircraft model has a high wing with a span of 62 m, length of 49 m with a takeoff gross weight of 221 tonnes, of which 83 tonnes are fuel. Contents 1 Background 1 2 Specification 1 2.1 Payload . .1 2.2 Flight requirements . .1 2.3 Mission profile . .2 3 Initial weight estimation 3 3.1 Total takeoff weight . .3 3.2 Empty weight . -
Airworthiness Requirements for the Type Certification of Airships in the Categories Normal and Commuter
Section 1 LFLS Airworthiness Requirements Lufttüchtigkeitsforderungen for the type certification of für die Prüfung und Zulassung von airships in the categories Luftschiffen der Kategorien Normal and Commuter Normal und Zubringer (LFLS) References: Referenzen: - Announcement: NfL II - 94/93 - Bekanntmachung: NfL II - 103/99 - Publication in Bundesanzeiger: - Veröffentlichung im Bundesanzeiger: BAnz. Volume 53, page 9286, Nr. 185 BAnz. Jahrgang 53, Seite 6813, Nr. 72 - Effective date: 13. April 2001 - inkraftgetreten: 13. April 2001 - Amendments: - Änderungen: NfL II - 25/01 (correction § 341) NfL II - 25/01 (Korrektur § 341) - This Implemenation Order has been notified under - Diese Durchführungsverordnung wurde unter der the No. 1996/420/D with the directives 83/189/EEC, Nr. 1996/420/D entsprechend den Richtlinien 88/182/EEC and 94/10/EC concerning an 83/189/EWG, 88/182/EWG und 94/10/EG betreffend information procedure in the field of standards and eines Informationsverfahrens auf dem Gebiet der technical negotiations Normen und technischen Vorschriften notifiziert. In Hinblick auf die zu erwartenden Zulassungen im Ausland erfolgte die Bekanntmachung der LFLS in englischer Sprache. Eine deutsche Übersetzung wird angefertigt, sobald hierfür ein Bedarf erkennbar wird. FOREWORD These Airworthiness Requirements for Airships have been based on the report "Airship Design Criteria" of the US Department of Transportation, Paper No. FAA P-8110-2, change 1, dated July 24, 1992. The purpose of the FAA report was to provide acceptable airworthiness requirements for the type certification of conventional, near- equilibrium, non-rigid airships. The report contained the design requirements necessary to provide an equivalent level of safety to that prescribed in 14 CFR 21.17(b) for special classes of aircraft. -
Aircraft Fuel Consumption – Estimation and Visualization
1 Project Aircraft Fuel Consumption – Estimation and Visualization Author: Marcus Burzlaff Supervisor: Prof. Dr.-Ing. Dieter Scholz, MSME Delivery Date: 13.12.2017 Faculty of Engineering and Computer Science Department of Automotive and Aeronautical Engineering URN: http://nbn-resolving.org/urn:nbn:de:gbv:18302-aero2017-12-13.019 Associated URLs: http://nbn-resolving.org/html/urn:nbn:de:gbv:18302-aero2017-12-13.019 © This work is protected by copyright The work is licensed under a Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International License: CC BY-NC-SA http://creativecommons.org/licenses/by-nc-sa/4.0 Any further request may be directed to: Prof. Dr.-Ing. Dieter Scholz, MSME E-Mail see: http://www.ProfScholz.de This work is part of: Digital Library - Projects & Theses - Prof. Dr. Scholz http://library.ProfScholz.de Published by Aircraft Design and Systems Group (AERO) Department of Automotive and Aeronautical Engineering Hamburg University of Applied Science This report is deposited and archived: Deutsche Nationalbiliothek (http://www.dnb.de) Repositorium der Leibniz Universität Hannover (http://www.repo.uni-hannover.de) This report has associated published data in Harvard Dataverse: http://doi.org/10.7910/DVN/2HMEHB Abstract In order to uncover the best kept secret in today’s commercial aviation, this project deals with the calculation of fuel consumption of aircraft. With only the reference of the aircraft manu- facturer’s information, given within the airport planning documents, a method is established that allows computing values for the fuel consumption of every aircraft in question. The air- craft's fuel consumption per passenger and 100 flown kilometers decreases rapidly with range, until a near constant level is reached around the aircraft’s average range. -
Design of an Unmanned Aerial Vehicle for Long-Endurance Communication Support
AIAA 2017-4148 AIAA AVIATION Forum 5-9 June 2017, Denver, Colorado 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference Design of an Unmanned Aerial Vehicle for Long-Endurance Communication Support Berk Ozturk,∗ Michael Burton,∗ Ostin Zarse,y Warren Hoburg,z Mark Drela,x John Hansmanx A long-endurance, medium-altitude unmanned aerial vehicle (UAV) was designed to provide communication support to areas lacking communication infrastructure. Current solutions involve larger, more costly aircraft that carry heavier payloads and have maximum flight durations of less than 36 hours. The presented design would enable a 5.6 day mission with a 10 lb, 100 W communications payload, providing coverage over an area 100 km in diameter. A geometric program was used to size the aircraft, which is a piston-engine unmanned aircraft with a 24 ft wingspan, and a takeoff weight of 147 lbs. The airframe is designed to be modular, which allows for fast and easy transportation and assembly for an operating crew of four to six. The aircraft can station-keep in 90% of global wind conditions at an altitude of 15,000 ft. Nomenclature ADS-B Automatic Dependent LOS line-of-sight Surveillance-Broadcast MSL mean sea level BLOS beyond line-of-slight MTOW maximum takeoff weight BSFC brake specific fuel consumption PMU power management unit CG center of gravity RC remote control GP geometric program RPM revolutions per minute ECU engine control unit STP standard temperature and pressure FAA Federal Aviation Administration UAV unmanned aerial vehicle FAR Federal Aviation Regulations UHF ultra-high frequency GPS Global Positioning System IC internal combustion I. -
Business & Commercial Aviation
JUNE/JULY 2020 $10.00 AviationWeek.com/BCA Business & Commercial Aviation 2020 PURCHASE PLANNING HANDBOOK Production Aircraft Comparison A Look at the Trends and New AND Performance Tables Developments in Avionics ALSO IN THIS ISSUE Bombardier Global 7500 Smoke Signals Under Pressure Mountain Wave Monsters One Too Many Digital Edition Copyright Notice The content contained in this digital edition (“Digital Material”), as well as its selection and arrangement, is owned by Informa. and its affiliated companies, licensors, and suppliers, and is protected by their respective copyright, trademark and other proprietary rights. Upon payment of the subscription price, if applicable, you are hereby authorized to view, download, copy, and print Digital Material solely for your own personal, non-commercial use, provided that by doing any of the foregoing, you acknowledge that (i) you do not and will not acquire any ownership rights of any kind in the Digital Material or any portion thereof, (ii) you must preserve all copyright and other proprietary notices included in any downloaded Digital Material, and (iii) you must comply in all respects with the use restrictions set forth below and in the Informa Privacy Policy and the Informa Terms of Use (the “Use Restrictions”), each of which is hereby incorporated by reference. Any use not in accordance with, and any failure to comply fully with, the Use Restrictions is expressly prohibited by law, and may result in severe civil and criminal penalties. Violators will be prosecuted to the maximum possible extent. You may not modify, publish, license, transmit (including by way of email, facsimile or other electronic means), transfer, sell, reproduce (including by copying or posting on any network computer), create derivative works from, display, store, or in any way exploit, broadcast, disseminate or distribute, in any format or media of any kind, any of the Digital Material, in whole or in part, without the express prior written consent of Informa. -
Fighter Aircraft
- https://ntrs.nasa.gov/search.jsp?R=19810011498 2020-03-21T13:44:30+00:00Z NASA TP 1837 NASA TechnicalPaper 1837 c. 1 . A Computer Technique for Detailed Analysis of MissionRadius and ManeuverabilityCharacteristics of Fighter Aircraft Willard E. FOSS, Jr. MARCH 198 1 TECH LIBRARY KAFB, NM 00b788Z NASA Technical Paper 1837 A ComputerTechnique for Detailed Analysis of Mission Radiusand ManeuverabilityCharacteristics of FighterAircraft Willard E. FOSS, Jr. La ugley Resea rcb Ceu ter Harnpton, Virginia National Aeronautics and Space Administration Scientific and Technical Information Branch 1981 SUMMARY A computer technique to determine the mission radius and maneuverability characteristics ofcombat aircraft has been developed. The technique has been used at the Langley ResearchCenter to determine critical operational require- ments and the areas in which research programs would be expected to yield the most beneficialresults. In turn,the results of researchefforts havebeen evaluated in terms of aircraft performance on selected mission segments and for complete mission profiles. The aircraftcharacteristics and flight constraints are represented in sufficient detail to permit realistic sensitivity studies in terms of either configuration modifications or changes in operational proce- dures. Sample calculationsare provided to illustrate the wide variety of mili- tary mission profiles that maybe represented.Extensive use of thetechnique in evaluationstudies indicates that the calculated performance is essentially the same as that obtained by the proprietary programs in use throughout the air- craft industry. INTRODUCTION A computer technique to determinethe mission radius and maneuverability characteristics ofcombat aircraft for a variety of military profiles hasbeen developed. The technique has beenused at the Langley Research Center todeter- mine critical operational requirements and the areas in which research programs wouldbe expected toyield the most beneficialresults. -
Getting to Grips with Fuel Economy
Flight Operations Support & Line Assistance Issue III - July 2004 Issue III - July fuel economy getting to grips with getting to grips with AIRBUS AIRBUS S.A.S. 31707 BLAGNAC CEDEX - FRANCE CUSTOMER SERVICES COMMUNICATION REFERENCE GDCOS-A179 JULY 2004 PRINTED IN FRANCE fuel economy © AIRBUS S.A.S. 2004 ALL RIGHTS RESERVED AN EADS JOINT COMPANY Issue 4 - October 2004 WITH BAE SYSTEMS Flight Operations Support & Line Assistance The statements made herein do not constitute an offer. They are based on the assumptions shown and are expressed in good faith. Where the supporting grounds for these statements are not shown, the Company will be pleased to explain the basis thereof. This document is the property of Airbus and is supplied on the express condition that it is to be treated as confidential. No use of reproduction may be made thereof other than that expressely authorised. Flight Operations Support & Line Assistance Customer Services 1, rond-point Maurice Bellonte, BP 33 31707 BLAGNAC Cedex FRANCE Telephone (+33) 5 61 93 33 33 Telefax (+33) 5 61 93 29 68 Telex AIRBU 530526F SITA TLSBI7X getting to grips with fuel economy Issue 4 - October 2004 Getting to grips with Fuel Economy Table of contents TABLE OF CONTENTS TABLE OF CONTENTS 1 1. SUMMARY 4 2. PREAMBLE 5 3. INTRODUCTION 6 4. PRE-FLIGHT PROCEDURES 7 4.1 CENTER OF GRAVITY POSITION 8 4.1.1 INTRODUCTION 8 4.1.2 AUTOMATIC CENTER OF GRAVITY MANAGEMENT 8 4.1.3 INFLUENCE ON FUEL CONSUMPTION 9 4.2 TAKEOFF WEIGHT 11 4.2.1 INTRODUCTION 11 4.2.2 OVERLOAD EFFECT 11 4.2.3 AIRCRAFT OPERATING WEIGHT 12 4.2.4 PAYLOAD 13 4.2.5 EMBARKED FUEL 13 4.3 FLIGHT PLANNING 14 4.4 TAXIING 17 4.5 FUEL FOR TRANSPORTATION 19 4.6 AUXILIARY POWER UNIT 21 4.7 AERODYNAMIC DETERIORATION 23 5. -
Final Transcript Runway Safety Landing Scenario
Final Transcript Runway Safety Landing Scenario Narrator - Safety relies not only on the training and skillset of a pilot, but also on their ability to maintain a proactive mindset, when preparing for landing or taxiing. A proactive mindset is key in maintaining situational awareness in the air and on the ground. There are a number of elements to consider as you prepare to land, such as conducting a robust checklist and using effective communication with air traffic control. And don’t forget - a thorough understanding of phraseology, hot spots, markings, signage, and lighting - all lead to surface safety. In the following scenario, you are returning from a cross-country flight. Get ready to land! Narrator: You are on a visual approach to Runway Two Eight Left. Pilot: Tower, November One Two Three is with you on a visual approach to Runway Two Eight Left. Tower: November One Two Three, Runway Two Eight Left cleared to land, wind 2-7-0 at 8. Pilot: November One Two Three cleared to land Runway Two Eight Left, copy the wind. Narrator: As you approach the airport ensure you are lined up with the correct surface. Tower: November One Two Three, go-around, you appear to be aligned with the wrong runway. Pilot: November One Two Three, go-round. Tower: November One Two Three, go-around, you appear to be aligned with the taxiway. Pilot: November One Two Three, go-round. Narrator: You picked the correct surface. Remember, when identifying your landing surface, use all available resources to ensure the correct runway. These resources can include visual cues, such as terminals, hangars and taxiways. -
Phraseology Conflict – Sids/Stars Survey Report
Phraseology Conflict SID/STAR – Report on Potential Misunderstanding 2nd Edition Phraseology Conflict SID/STAR—Report on Potential Misunderstanding International Air Transport Association Montreal—Geneva 2nd Edition NOTICE DISCLAIMER. The information contained in this Report is subject to constant review in the light of changing government requirements and regulations. No subscriber or other reader should act on the basis of any such information without referring to applicable laws and regulations and without taking appropriate professional advice. Although every effort has been made to ensure accuracy, the International Air Transport Association (IATA), the International Federation of Air Line Pilots’ Associations (IFALPA), and any other contributors to this publication shall not be held responsible for any loss or damage caused by errors, omissions, misprints or misinterpretation of the contents hereof. Furthermore, IATA, IFALPA, and any other contributors to this publication expressly disclaim any and all liability to any person or entity, whether a purchaser of this publication or not, in respect of anything done or omitted, and the consequences of anything done or omitted, by any such person or entity in reliance on the contents of this publication. Other contributors’ opinions expressed in this publication do not necessarily reflect the opinion of the International Air Transport Association. The mention of specific companies, products in this publication does not imply that they are endorsed or recommended by the International Air Transport Association in preference to others of a similar nature which are not mentioned. © International Air Transport Association 2015. All Rights Reserved. No part of this publication may be reproduced, recast, reformatted or transmitted in any form by any means, electronic or mechanical, including photocopying, recording or any information storage and retrieval system, without the prior written permission from: Senior Vice President Safety & Flight Operations International Air Transport Association 800 Place Victoria, P.O.