Safety First Safety First Safety First, #23 January, 2017
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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 ................................... -
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. -
Services of the A350 XWB | August 2015
More mobility for the world th ing e f in u Services for the A350 XWB a t t u r n e i a Extra-wide support M NEW 0 A 5 irbus A3 The new shape of maintenance With the entry into service of the A350 XWB (extra-wide body), Airbus is ushering in a new era in commercial aviation – ultra-efficient long-range travel in a new aircraft class. Yet support by an experienced MRO provider is essential in order to make the most of the excellent qualities this new twin-jet aircraft promises. Turning a vision into a profitable reality Preparation on the ground means success in the air Lufthansa Technik has always played an important role in the The Airbus A350 XWB is another quantum leap in technology, from unprecedented success story of Airbus: our engineers have the large share of carbon fiber composites and titanium alloys contributed valuable technical and commercial expertise to the used in its structure to its highly advanced turbofan engines. Since development of new Airbus aircraft. No other MRO provider a number of its system technologies are derivatives of its larger can can be proud of such a strong history of supporting aircraft sister, the A380 – such as the solid state power control, variable development. With the newest Airbus twin jet, Lufthansa Technik frequency generators and high-pressure hydraulics – Lufthansa once again helped to turn the vision of a new aircraft into a Technik has already gained substantial experience with these new working reality. Lufthansa Technik’s engineers participated in systems and their specific features. -
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. -
Type-Certificate Data Sheet
TCDS EASA.A.151 AIRBUS A350 Issue 24 Date: 26 June 2020 TYPE-CERTIFICATE DATA SHEET No. EASA.A.151 AIRBUS A350 Type Certificate Holder: AIRBUS S.A.S. 2 Rond-point Emile Dewoitine 31700 BLAGNAC FRANCE Airworthiness Category: Large Aeroplanes For Model(s): A350-941 A350-1041 Page 1 / 31 TCDS EASA.A.151 AIRBUS A350 Issue 24 Date: 26 June 2020 Table of Contents SECTION 1: A350-900 SERIES 4 I. GENERAL 4 1. Type/Model 4 2. Performance Class 4 3. Certifying Authority 4 4. Manufacturer 4 5. EASA Certification Application Date 4 6. EASA Type Certification Date 4 II. CERTIFICATION BASIS 5 1. EASA Certification Basis 5 2. Special Conditions 5 3. Exemptions / Deviations 6 4. Equivalent safety findings (21A.21(c)(2)) 7 5. Environmental requirements 7 6. Operational Suitability Data 8 III. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS 9 1. A350-900 powered by RR engines 9 2. Data pertinent to all A350-900 series 11 IV. OPERATING AND SERVICE INSTRUCTIONS 15 1. Aircraft Flight Manual 15 2. Maintenance Instructions and Airworthiness Limitations 15 3. ETOPS 15 V. OPERATIONAL SUITABILITY DATA (OSD) 16 1. Master Minimum Equipment List 16 2. Flight Crew Data 16 3. Cabin Crew Data 16 SECTION 2: A350-1000 SERIES 17 I. GENERAL 17 1. Type/Model 17 2. Performance Class 17 3. Certifying Authority 17 4. Manufacturer 17 5. EASA Certification Application Date 17 6. EASA Type Certification Date 17 II. CERTIFICATION BASIS 18 1. EASA Certification Basis 18 2. Special Conditions 18 3. Exemptions / Deviations 19 4. Equivalent safety findings (21A.21(c)(2)) 19 5. -
Aircraft Performance (R18a2110)
AERONAUTICAL ENGINEERING – MRCET (UGC Autonomous) AIRCRAFT PERFORMANCE (R18A2110) COURSE FILE II B. Tech II Semester (2019-2020) Prepared By Ms. D.SMITHA, Assoc. Prof Department of Aeronautical Engineering MALLA REDDY COLLEGE OF ENGINEERING & TECHNOLOGY (Autonomous Institution – UGC, Govt. of India) Affiliated to JNTU, Hyderabad, Approved by AICTE - Accredited by NBA & NAAC – ‘A’ Grade - ISO 9001:2015 Certified) Maisammaguda, Dhulapally (Post Via. Kompally), Secunderabad – 500100, Telangana State, India. AERONAUTICAL ENGINEERING – MRCET (UGC Autonomous) MRCET VISION • To become a model institution in the fields of Engineering, Technology and Management. • To have a perfect synchronization of the ideologies of MRCET with challenging demands of International Pioneering Organizations. MRCET MISSION To establish a pedestal for the integral innovation, team spirit, originality and competence in the students, expose them to face the global challenges and become pioneers of Indian vision of modern society . MRCET QUALITY POLICY. • To pursue continual improvement of teaching learning process of Undergraduate and Post Graduate programs in Engineering & Management vigorously. • To provide state of art infrastructure and expertise to impart the quality education. [II year – II sem ] Page 2 AERONAUTICAL ENGINEERING – MRCET (UGC Autonomous) PROGRAM OUTCOMES (PO’s) Engineering Graduates will be able to: 1. Engineering knowledge: Apply the knowledge of mathematics, science, engineering fundamentals, and an engineering specialization to the solution -
Airbus A350 Aftermarket Services Global Sales
Airbus A350 Aftermarket Services Global Sales Our regional business development managers are focused on working with you to understand the specific needs of your organization. Our managers work closely with our customer support team to convey your needs and develop tailored support programs to best address your objectives. General Manager Director, Global Aftermarket Commercial Aircraft Sales & Business Development Mark Brooks Andrea Davis Tel: +1 716 361 9704 Tel: +1 716 517 0085 [email protected] [email protected] Moog Inc. is a worldwide designer, manufacturer, and integrator of precision motion control products and systems. Over the past 60 years, we have developed a reputation for delivering innovative solutions for the most challenging motion control applications. As a result, we have Sales Manager, Account Manager, Sales Manager, Sales Manager, become a key supplier to the world’s leading aircraft manufacturers and are positioned on Americas Europe Northern Europe China virtually every platform in the marketplace – supplying reliable actuation systems that are Tim Leach Judith Bindert Phill Parsons Bruce Zhang highly supportable and add significant value for our customers. Tel: +1 716 864 7194 Tel: +49 171 261 0372 Tel: +44 7764 894719 Tel: +86 135 0126 0296 [email protected] [email protected] [email protected] [email protected] A key element of our success has been our customer focus. With Moog, you will find a team Technical Sales Manager, Technical Sales Manager, Technical Sales Manager, Technical Sales Manager, of people ready to deliver quality products and support services, all while being flexible and Global Europe Middle East, Africa Asia Pacific responsive to your needs. -
Chapter: 4. Approaches
Chapter 4 Approaches Introduction This chapter discusses general planning and conduct of instrument approaches by pilots operating under Title 14 of the Code of Federal Regulations (14 CFR) Parts 91,121, 125, and 135. The operations specifications (OpSpecs), standard operating procedures (SOPs), and any other FAA- approved documents for each commercial operator are the final authorities for individual authorizations and limitations as they relate to instrument approaches. While coverage of the various authorizations and approach limitations for all operators is beyond the scope of this chapter, an attempt is made to give examples from generic manuals where it is appropriate. 4-1 Approach Planning within the framework of each specific air carrier’s OpSpecs, or Part 91. Depending on speed of the aircraft, availability of weather information, and the complexity of the approach procedure Weather Considerations or special terrain avoidance procedures for the airport of intended landing, the in-flight planning phase of an Weather conditions at the field of intended landing dictate instrument approach can begin as far as 100-200 NM from whether flight crews need to plan for an instrument the destination. Some of the approach planning should approach and, in many cases, determine which approaches be accomplished during preflight. In general, there are can be used, or if an approach can even be attempted. The five steps that most operators incorporate into their flight gathering of weather information should be one of the first standards manuals for the in-flight planning phase of an steps taken during the approach-planning phase. Although instrument approach: there are many possible types of weather information, the primary concerns for approach decision-making are • Gathering weather information, field conditions, windspeed, wind direction, ceiling, visibility, altimeter and Notices to Airmen (NOTAMs) for the airport of setting, temperature, and field conditions. -
Transatlantic Airline Fuel Efficiency Ranking, 2017
WHITE PAPER SEPTEMBER 2018 TRANSATLANTIC AIRLINE FUEL EFFICIENCY RANKING, 2017 Brandon Graver, Ph.D., and Daniel Rutherford, Ph.D. www.theicct.org [email protected] BEIJING | BERLIN | BRUSSELS | SAN FRANCISCO | WASHINGTON ACKNOWLEDGMENTS The authors thank Tim Johnson, Andrew Murphy, Anastasia Kharina, and Amy Smorodin for their review and support. We also acknowledge Airline Data Inc. for providing processed BTS data, and FlightGlobal for Ascend Fleet data. International Council on Clean Transportation 1225 I Street NW Suite 900 Washington, DC 20005 USA [email protected] | www.theicct.org | @TheICCT © 2018 International Council on Clean Transportation TRANSATLANTIC AIRLINE FUEL EFFICIENCY RANKING, 2017 TABLE OF CONTENTS EXECUTIVE SUMMARY ............................................................................................................ iii 1. INTRODUCTION .................................................................................................................... 2 2. METHODOLOGY ................................................................................................................... 3 2.1 Airline selection .................................................................................................................................3 2.2 Fuel burn modeling..........................................................................................................................5 2.3 Fuel efficiency calculation ............................................................................................................6 -
Practical Application of Pressurization Systems
Practical Application of Pressurization Systems Pressurization Instruments A B 1 2 A. Cabin Rate of Climb Indicator – Similar to VSI, shows rate at which cabin altitude is climbing or descending (in this example the cabin is descending at 700 feet per minute). B. Cabin Altitude and Pressure Differential Indicator 1. Outside ring (long needle) shows cabin altitude in thousands of feet (in this example cabin altitude is a little over 3,000 feet. 2. Inside ring (short needle) shows the pressure differential in inches of mercury between the air in the cabin and the outside atmosphere (in this example, pressure differential is 4.8 inches) Pressurization Controller Setting Prior To Takeoff C A B A. Cabin Altitude Control – Prior to takeoff, set to 1,000 feet above cruise altitude on the inner ring.* The outer ring indicates what the cabin altitude will be when reaching cruise altitude. In this example the aircraft is climbing to 16,000 feet, so the altitude is set at 17,000 feet. The cabin altitude at cruise will be 4,100 feet. B. Cabin Rate of Climb/Descent Control: Usually set in the “12 O’clock” position which causes the cabin to climb at about ½ the rate at which the aircraft climbs. C. Cabin Pressure Dump Valve – Dumps cabin pressure * Setting altitude 1,000 feet above cruise altitude will prevent the cabin from climbing or descending if the aircraft climbs or descends a few hundred feet when at max pressure differential. This prevents cabin pressure changes and discomfort the crew and passengers. Pressurization Controller Setting Prior to Descent C B A A. -
EGNOS BULLETIN Issue 34, Autumn’20 Edition
EGNOS BULLETIN Issue 34, Autumn’20 Edition Credits: Finnair https://egnos-user-support.essp-sas.eu/ https://www.essp-sas.eu/ 2 EGNOS BULLETIN | ISSUE 34 | AUTUMN’20 EDITION EGNOS implementation EGNOS BULLETIN | ISSUE 34 | AUTUMN’20 EDITION 3 EGNOS Success Stories FINNAIR’S A350 TRANSCONTINENTAL ROUNDTRIP USING SBAS LPV (WAAS & EGNOS) AT BOTH ORIGIN AND DESTINATION AIRPORTS Finnair’s A350 transcontinental roundtrip using SBAS LPV (WAAS & EGNOS) at both origin and destination airports Credits: Finnair Landing at HEL airport Finnair’s strategic vision of the future includes Moreover, they also confirmed the ADS-B out fundamental fleet management decisions that option, which is now an almost-basic requirement have borne fruit years later. to comply with EASA’s implementing rule and FAA As a launch customer of the Airbus A350 XWB, one. Both decisions made Finnair’s A350 future- Finnair received its first A350-900 in October 2015. proof from the manufacturing line. Five years later, Captain Marko Valtonen, Finnair’s Operational approval Fleet Chief Pilot for the A330/350, has performed Apart from airworthiness, the flight operation the first known transcontinental roundtrip between elements that allowed Finnair to perform those Europe and the USA using SBAS LPV approaches RNP APCH down to LPV minima comprised at both origin and destination airports with the two main activities: the training A350 (tail OH-LWI). of pilots and the modification of This singular flight used the latest SBAS technology the operational manual described Establishing approval to approach both airports using the United States generically in the PBN Manual (ICAO procedures that are efficient SBAS (WAAS) at John F. -
Airbus and Rockwell Collins: Innovating Together for the A350 XWB
AIRBUS A350 XWB TESTIMONIAL Airbus and Rockwell Collins: Innovating together for the A350 XWB In response to demand for a series of highly efficient, medium- For the A350 XWB, we’re providing significantly more capacity, long-range, wide-body aircraft, Airbus is launching its content than on any other Airbus aircraft. This includes A350 XWB (“Extra-Wide Body”) family. navigation and data-network capabilities, landing guidance systems, flight control equipment, information management With the widest fuselage in its category, the A350 XWB and communications. offers unprecedented levels of comfort as well as the lowest operating and seat-mile costs of any aircraft in the 270- to Airbus is also relying on us to lead new complex integration 350-seat market segment. Key design elements address the activities, introducing a new level of trust. challenges of volatile fuel prices, rising passenger expectations and environmental concerns. Rockwell Collins has been an Airbus avionics supplier since “We appreciate the constant drive the 1970s. Our equipment is on board all in-production Airbus aircraft, and our consistently high level of service has earned of Rockwell Collins to deliver high- us a number of Airbus customer performance awards. quality packages and the solutions that best fit our needs in a positive collaborative environment”. – Regis Delpierre, A350 XWB Systems & Testing Vice-President, Airbus Rockwell Collins systems aboard the A350 XWB Communication global work package Landing systems This package ensures the management of voice and data Airbus selected the Rockwell Collins Multi-Mode Receiver and communications of the aircraft, between pilots, flight crew, Digital Low Range Altimeter, confirming Rockwell Collins’ controllers and the airline company.