Phraseology Conflict – Sids/Stars Survey Report
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Aircraft Engine Performance Study Using Flight Data Recorder Archives
Aircraft Engine Performance Study Using Flight Data Recorder Archives Yashovardhan S. Chati∗ and Hamsa Balakrishnan y Massachusetts Institute of Technology, Cambridge, Massachusetts, 02139, USA Aircraft emissions are a significant source of pollution and are closely related to engine fuel burn. The onboard Flight Data Recorder (FDR) is an accurate source of information as it logs operational aircraft data in situ. The main objective of this paper is the visualization and exploration of data from the FDR. The Airbus A330 - 223 is used to study the variation of normalized engine performance parameters with the altitude profile in all the phases of flight. A turbofan performance analysis model is employed to calculate the theoretical thrust and it is shown to be a good qualitative match to the FDR reported thrust. The operational thrust settings and the times in mode are found to differ significantly from the ICAO standard values in the LTO cycle. This difference can lead to errors in the calculation of aircraft emission inventories. This paper is the first step towards the accurate estimation of engine performance and emissions for different aircraft and engine types, given the trajectory of an aircraft. I. Introduction Aircraft emissions depend on engine characteristics, particularly on the fuel flow rate and the thrust. It is therefore, important to accurately assess engine performance and operational fuel burn. Traditionally, the estimation of fuel burn and emissions has been done using the ICAO Aircraft Engine Emissions Databank1. However, this method is approximate and the results have been shown to deviate from the measured values of emissions from aircraft in operation2,3. -
E6bmanual2016.Pdf
® Electronic Flight Computer SPORTY’S E6B ELECTRONIC FLIGHT COMPUTER Sporty’s E6B Flight Computer is designed to perform 24 aviation functions and 20 standard conversions, and includes timer and clock functions. We hope that you enjoy your E6B Flight Computer. Its use has been made easy through direct path menu selection and calculation prompting. As you will soon learn, Sporty’s E6B is one of the most useful and versatile of all aviation computers. Copyright © 2016 by Sportsman’s Market, Inc. Version 13.16A page: 1 CONTENTS BEFORE USING YOUR E6B ...................................................... 3 DISPLAY SCREEN .................................................................... 4 PROMPTS AND LABELS ........................................................... 5 SPECIAL FUNCTION KEYS ....................................................... 7 FUNCTION MENU KEYS ........................................................... 8 ARITHMETIC FUNCTIONS ........................................................ 9 AVIATION FUNCTIONS ............................................................. 9 CONVERSIONS ....................................................................... 10 CLOCK FUNCTION .................................................................. 12 ADDING AND SUBTRACTING TIME ....................................... 13 TIMER FUNCTION ................................................................... 14 HEADING AND GROUND SPEED ........................................... 15 PRESSURE AND DENSITY ALTITUDE ................................... -
NORWAY LOCAL SINGLE SKY IMPLEMENTATION Level2020 1 - Implementation Overview
LSSIP 2020 - NORWAY LOCAL SINGLE SKY IMPLEMENTATION Level2020 1 - Implementation Overview Document Title LSSIP Year 2020 for Norway Info Centre Reference 20/12/22/79 Date of Edition 07/04/2021 LSSIP Focal Point Peder BJORNESET - [email protected] Luftfartstilsynet (CAA-Norway) LSSIP Contact Person Luca DELL’ORTO – [email protected] EUROCONTROL/NMD/INF/PAS LSSIP Support Team [email protected] Status Released Intended for EUROCONTROL Stakeholders Available in https://www.eurocontrol.int/service/local-single-sky-implementation- monitoring Reference Documents LSSIP Documents https://www.eurocontrol.int/service/local-single-sky-implementation- monitoring Master Plan Level 3 – Plan https://www.eurocontrol.int/publication/european-atm-master-plan- Edition 2020 implementation-plan-level-3 Master Plan Level 3 – Report https://www.eurocontrol.int/publication/european-atm-master-plan- Year 2020 implementation-report-level-3 European ATM Portal https://www.atmmasterplan.eu/ STATFOR Forecasts https://www.eurocontrol.int/statfor National AIP https://avinor.no/en/ais/aipnorway/ FAB Performance Plan https://www.nefab.eu/docs# LSSIP Year 2020 Norway Released Issue APPROVAL SHEET The following authorities have approved all parts of the LSSIP Year 2020 document and the signatures confirm the correctness of the reported information and reflect the commitment to implement the actions laid down in the European ATM Master Plan Level 3 (Implementation View) – Edition 2020. Stakeholder / Name Position Signature and date Organisation -
Design and Analysis of Advanced Flight: Planning Concepts
NASA Contractor Report 4063 Design and Analysis of Advanced Flight: Planning Concepts Johri A. Sorerisen CONrRACT NAS1- 17345 MARCH 1987 NASA Contractor Report 4063 Design and Analysis of Advanced Flight Planning Concepts John .A. Sorensen Analytical Mechanics Associates, Inc. Moantain View, California Prepared for Langley Research Center under Contract NAS 1- 17345 National Aeronautics and Space Administration Scientific and Technical Information Branch 1987 F'OREWORD This continuing effort for development of concepts for generating near-optimum flight profiles that minimize fuel or direct operating costs was supported under NASA Contract No. NAS1-17345, by Langley Research Center, Hampton VA. The project Technical Monitor at Langley Research Center was Dan D. Vicroy. Technical discussion with and suggestions from Mr. Vicroy, David H. Williams, and Charles E. Knox of Langley Research Center are gratefully acknowledged. The technical information concerning the Chicago-Phoenix flight plan used as an example throughout this study was provided by courtesy of United Airlines. The weather information used to exercise the experimental flight planning program EF'PLAN developed in this study was provided by courtesy of Pacific Southwest Airlines. At AMA, Inc., the project manager was John A. Sorensen. Engineering support was provided by Tsuyoshi Goka, Kioumars Najmabadi, and Mark H, Waters. Project programming support was provided by Susan Dorsky, Ann Blake, and Casimer Lesiak. iii DESIGN AND ANALYSIS OF ADVANCED FLIGHT PLANNING CONCEPTS John A. Sorensen Analytical Mechanics Associates, Inc. SUMMARY The Objectives of this continuing effort are to develop and evaluate new algorithms and advanced concepts for flight management and flight planning. This includes the minimization of fuel or direct operating costs, the integration of the airborne flight management and ground-based flight planning processes, and the enhancement of future traffic management systems design. -
The Difference Between Higher and Lower Flap Setting Configurations May Seem Small, but at Today's Fuel Prices the Savings Can Be Substantial
THE DIFFERENCE BETWEEN HIGHER AND LOWER FLAP SETTING CONFIGURATIONS MAY SEEM SMALL, BUT AT TODAY'S FUEL PRICES THE SAVINGS CAN BE SUBSTANTIAL. 24 AERO QUARTERLY QTR_04 | 08 Fuel Conservation Strategies: Takeoff and Climb By William Roberson, Senior Safety Pilot, Flight Operations; and James A. Johns, Flight Operations Engineer, Flight Operations Engineering This article is the third in a series exploring fuel conservation strategies. Every takeoff is an opportunity to save fuel. If each takeoff and climb is performed efficiently, an airline can realize significant savings over time. But what constitutes an efficient takeoff? How should a climb be executed for maximum fuel savings? The most efficient flights actually begin long before the airplane is cleared for takeoff. This article discusses strategies for fuel savings But times have clearly changed. Jet fuel prices fuel burn from brake release to a pressure altitude during the takeoff and climb phases of flight. have increased over five times from 1990 to 2008. of 10,000 feet (3,048 meters), assuming an accel Subse quent articles in this series will deal with At this time, fuel is about 40 percent of a typical eration altitude of 3,000 feet (914 meters) above the descent, approach, and landing phases of airline’s total operating cost. As a result, airlines ground level (AGL). In all cases, however, the flap flight, as well as auxiliarypowerunit usage are reviewing all phases of flight to determine how setting must be appropriate for the situation to strategies. The first article in this series, “Cost fuel burn savings can be gained in each phase ensure airplane safety. -
TCAS II) by Personnel Involved in the Implementation and Operation of TCAS II
Preface This booklet provides the background for a better understanding of the Traffic Alert and Collision Avoidance System (TCAS II) by personnel involved in the implementation and operation of TCAS II. This booklet is an update of the TCAS II Version 7.0 manual published in 2000 by the Federal Aviation Administration (FAA). It describes changes to the CAS logic introduced by Version 7.1 and updates the information on requirements for use of TCAS II and operational experience. Version 7.1 logic changes will improve TCAS Resolution Advisory (RA) sense reversal logic in vertical chase situations. In addition all “Adjust Vertical Speed, Adjust” RAs are converted to “Level-Off, Level-Off” RAs to make it more clear that a reduction in vertical rate is required. The Minimum Operational Performance Standards (MOPS) for TCAS II Version 7.1 were approved in June 2008 and Version 7.1 units are expected to be operating by 2010-2011. Version 6.04a and 7.0 units are also expected to continue operating for the foreseeable future where authorized. 2 Preface................................................................................................................................. 2 The TCAS Solution............................................................................................................. 5 Early Collision Avoidance Systems................................................................................ 5 TCAS II Development .................................................................................................... 6 Initial -
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. -
Advisory Circular (AC)
U.S. Department Advisory of Transportation Federal Aviation Administration Circular Subject: Parts 91, 121, 125, and 135 Date: 7/30/12 AC No: 120-74B Flightcrew Procedures During Taxi Initiated by: Change: Operations AFS-200/800 1. PURPOSE. This advisory circular (AC) provides guidelines for the development and implementation of standard operating procedures (SOP) for conducting safe aircraft operations during taxiing to avoid causing a runway incursion. In accordance with Federal Aviation Administration (FAA) Order 7050.1, Runway Safety Program, the definition of a runway incursion is any occurrence at an aerodrome involving the incorrect presence of an aircraft, vehicle, or person on the protected area of a surface designated for the landing and takeoff of aircraft. It is intended for use by persons operating aircraft with two or more pilots on the flight deck under Title 14 of the Code of Federal Regulations (14 CFR) parts 91, 121, 125, and 135. The FAA recommends that these guidelines become an integral part of all SOPs, flight operations manuals (FOM), and formal flightcrew member training programs. The use of flightcrew SOPs should be emphasized and employed during all phases of flight, including ground operations. Appendices 1 and 2 of this AC contain examples of SOPs that are identical or similar to some SOPs currently in use. These appendices are not directive or prescriptive in nature and do not represent a rigid FAA view of Best Practices. SOPs may vary among fleets and among certificate holders and may change over time. Operators may integrate the information contained in Appendices 1 and 2 into their fleet-specific, route-specific, and equipment-specific operations and checklists. -
CRUISE FLIGHT OPTIMIZATION of a COMMERCIAL AIRCRAFT with WINDS a Thesis Presented To
CRUISE FLIGHT OPTIMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS _______________________________________ A Thesis presented to the Faculty of the Graduate School at the University of Missouri-Columbia _______________________________________________________ In Partial Fulfillment of the Requirements for the Degree Master of Science _____________________________________________________ by STEPHEN ANSBERRY Dr. Craig Kluever, Thesis Supervisor MAY 2015 The undersigned, appointed by the dean of the Graduate School, have examined the thesis entitled CRUISE FLIGHT OPTMIZATION OF A COMMERCIAL AIRCRAFT WITH WINDS presented by Stephen Ansberry, a candidate for the degree of Master of Science, and hereby certify that, in their opinion, it is worthy of acceptance. Professor Craig Kluever Professor Roger Fales Professor Carmen Chicone ACKNOWLEDGEMENTS I would like to thank Dr. Kluever for his help and guidance through this thesis. I would like to thank my other panel professors, Dr. Chicone and Dr. Fales for their support. I would also like to thank Steve Nagel for his assistance with the engine theory and Tyler Shinn for his assistance with the computer program. ii TABLE OF CONTENTS ACKNOWLEDGEMENTS………………………………...………………………………………………ii LIST OF FIGURES………………………………………………………………………………………..iv LIST OF TABLES…………………………………………………………………………………….……v SYMBOLS....................................................................................................................................................vi ABSTRACT……………………………………………………………………………………………...viii 1. INTRODUCTION.....................................................................................................................................1 -
Estimation of Aircraft Taxi-Out Fuel Burn Using Flight Data Recorder Archives
Estimation of Aircraft Taxi-out Fuel Burn using Flight Data Recorder Archives Harshad Khadilkar∗ and Hamsa Balakrishnany Massachusetts Institute of Technology, Cambridge, MA 02139, USA The taxi-out phase of a flight accounts for a significant fraction of total fuel burn for aircraft. In addition, surface fuel burn is also a major contributor to CO2 emissions in the vicinity of airports. It is therefore desirable to have accurate estimates of fuel consumption on the ground. This paper builds a model for estimation of on-ground fuel consumption of an aircraft, given its surface trajectory. Flight Data Recorder archives are used for this purpose. The taxi-out fuel burn is modeled as a linear function of several factors including the taxi-out time, number of stops, number of turns, and number of acceleration events. The statistical significance of each potential factor is investigated. The parameters of the model are estimated using least-squares regression. Since these parameters are estimated using data from operational aircraft, they provide more accurate estimates of fuel burn than methods that use idealized physical models of fuel consumption based on aircraft velocity profiles, or the baseline fuel consumption estimates provided by the International Civil Aviation Organization. Our analysis shows that in addition to the total taxi time, the number of acceleration events is a significant factor in determining taxi fuel consumption. Nomenclature ICAO International Civil Aviation Organization FDR Flight Data Recorder MTOW Maximum TakeOff Weight Tamb Ambient absolute temperature f Total fuel consumed during taxi-out t Taxi-out time ns Number of stops nt Number of turns na Number of acceleration events I. -
May 31, 2004 5 - 1
Airports Authority of India Manual of Air Traffic Services – Part 1 CHAPTER 5 SEPARATION METHODS AND MINIMA 5.1 Provision for the separation of Whenever, as a result of failure or controlled traffic degradation of navigation, communications, altimetry, flight control or other systems, 5.1.1 Vertical or horizontal separation shall aircraft performance is degraded below the be provided: level required for the airspace in which it is a) between IFR flights in Class D and E operating, the flight crew shall advise the airspaces except when VMC climb or ATC unit concerned without delay. Where the descent is involved under the failure or degradation affects the separation conditions specified in para 5.5.6; minimum currently being employed, the b) between IFR flights and special VFR controller shall take action to establish flights; [and another appropriate type of separation or c) between special VFR flights separation minimum. 5.1.2 No clearance shall be given to execute any manoeuvre that would reduce 5.2 Reduction in separation minima the spacing between two aircraft to less than the separation minimum applicable in the 5.2.1 In the vicinity of aerodromes circumstances. In the vicinity of aerodromes, the separation 5.1.3 Larger separations than the specified minima may be reduced if: minima should be applied whenever a) adequate separation can be provided exceptional circumstances such as unlawful by the aerodrome controller when each interference or navigational difficulties call for aircraft is continuously visible to this extra precautions. This should be done with controller; or due regard to all relevant factors so as to b) each aircraft is continuously visible to avoid impeding the flow of air traffic by the flight crews of the other aircraft application of excessive separations. -
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.