Understanding the Stall-Recovery Procedure for Turboprop
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Impacts of Aviation Emissions on Near-Airport Residential Air Quality Neelakshi Hudda,* Liam W
pubs.acs.org/est Article Impacts of Aviation Emissions on Near-Airport Residential Air Quality Neelakshi Hudda,* Liam W. Durant, Scott A. Fruin, and John L. Durant Cite This: https://dx.doi.org/10.1021/acs.est.0c01859 Read Online ACCESS Metrics & More Article Recommendations *sı Supporting Information ABSTRACT: Impacts of aviation emissions on air quality in and around residences near airports remain underexamined. We measured gases (CO, CO2, NO, and NO2) and particles (black carbon, particle-bound aromatic hydrocarbons, fine particulate matter fi (PM2.5), and ultra ne particles (reported using particle number concentrations (PNC) as a proxy)) continuously for 1 month at a residence near the Logan International Airport, Boston. The residence was located under a flight trajectory of the most utilized runway configuration. We found that when the residence was downwind of the airport, the concentrations of all gaseous and particulate pollutants (except PM2.5) were 1.1- to 4.8-fold higher than when the residence was not downwind of the airport. Controlling for runway usage and meteorology, the impacts were highest during overhead landing operations: average PNC was 7.5-fold higher from overhead landings versus takeoffs on the closest runway. Infiltration of aviation-origin emissions resulted in indoor PNC that were comparable to ambient concentrations measured locally on roadways and near highways. In addition, ambient NO2 concentrations at the residence exceeded those measured at regulatory monitoring sites in the area including near-road monitors. Our results highlight the need for further characterization of outdoor and indoor impacts of aviation emissions at the neighborhood scale to more accurately estimate residential exposures. -
CANARD.WING LIFT INTERFERENCE RELATED to MANEUVERING AIRCRAFT at SUBSONIC SPEEDS by Blair B
https://ntrs.nasa.gov/search.jsp?R=19740003706 2020-03-23T12:22:11+00:00Z NASA TECHNICAL NASA TM X-2897 MEMORANDUM CO CN| I X CANARD.WING LIFT INTERFERENCE RELATED TO MANEUVERING AIRCRAFT AT SUBSONIC SPEEDS by Blair B. Gloss and Linwood W. McKmney Langley Research Center Hampton, Va. 23665 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • DECEMBER 1973 1.. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA TM X-2897 4. Title and Subtitle 5. Report Date CANARD-WING LIFT INTERFERENCE RELATED TO December 1973 MANEUVERING AIRCRAFT AT SUBSONIC SPEEDS 6. Performing Organization Code 7. Author(s) 8. Performing Organization Report No. L-9096 Blair B. Gloss and Linwood W. McKinney 10. Work Unit No. 9. Performing Organization Name and Address • 760-67-01-01 NASA Langley Research Center 11. Contract or Grant No. Hampton, Va. 23665 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Technical Memorandum National Aeronautics and Space Administration 14. Sponsoring Agency Code Washington , D . C . 20546 15. Supplementary Notes 16. Abstract An investigation was conducted at Mach numbers of 0.7 and 0.9 to determine the lift interference effect of canard location on wing planforms typical of maneuvering fighter con- figurations. The canard had an exposed area of 16.0 percent of the wing reference area and was located in the plane of the wing or in a position 18.5 percent of the wing mean geometric chord above the wing plane. In addition, the canard could be located at two longitudinal stations. -
R&T Activities on Composite Structures
PUBLIC RELEASE R&T activities on composite structures for existing and future military A/C platforms at Airbus DS, Military Aircraft Mircea Calomfirescu, Rainer Neumaier, Thomas Körwien, Kay Dittrich Airbus Defence and Space GmbH Rechliner Str. 1 85077 Manching GERMANY [email protected] ABSTRACT This paper gives a short overview on the state of the art in composite aerostructures for civil and military aircraft. Major challenges are highlighted in this context and the requirements from military aircraft point of view are illustrated, derived from existing and future military aircraft perspectives. The main objective of the paper is to present the R&T activities in the aerostructure research program called FFS, advanced aerostructures. The activities range here from structural bonding, advanced radomes, new thermoplastic composite technologies and new materials and structures for low observability purposes. A brief insight is given to each of the topic highlighting the challenges and approaches, finishing with a summary of future trends and emerging technologies. 1.0 INTRODUCTION Composites offer several advantages over metallic aerostructures in civil as well as in military aircraft industry including reduced weight, less maintenance effort and costs due to “corrosion-free” composites and a superior fatigue behaviour compared to aluminium. The thermal expansion is much less and the material waste (“buy to fly ratio”) is more advantageous compared to aluminium structures. However, these advantages come along with higher material and manufacturing costs. For the prepreg technology for example the material has to be stored at -18°C, energy and investment intensive autoclaves are necessary and for quality assurance 100% non-destructive testing (NDT) is required in contrast to aluminium structures. -
Vertical Motion Simulator Experiment on Stall Recovery Guidance
NASA/TP{2017{219733 Vertical Motion Simulator Experiment on Stall Recovery Guidance Stefan Schuet National Aeronautics and Space Administration Thomas Lombaerts Stinger Ghaffarian Technologies, Inc. Vahram Stepanyan Universities Space Research Association John Kaneshige, Kimberlee Shish, Peter Robinson National Aeronautics and Space Administration Gordon Hardy Retired Research Test Pilot Science Applications International Corporation October 2017 NASA STI Program. in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part or other meetings sponsored or in helping NASA maintain this important co-sponsored by NASA. role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program operates under the technical, or historical information from auspices of the Agency Chief Information NASA programs, projects, and missions, Officer. It collects, organizes, provides for often concerned with subjects having archiving, and disseminates NASA's STI. substantial public interest. The NASA STI Program provides access to the NASA Aeronautics and Space Database • TECHNICAL TRANSLATION. English- and its public interface, the NASA Technical language translations of foreign scientific Report Server, thus providing one of the and technical material pertinent to largest collection of aeronautical and space NASA's mission. science STI in the world. Results are Specialized services also include organizing published in both non-NASA channels and and publishing research results, distributing by NASA in the NASA STI Report Series, specialized research announcements and which includes the following report types: feeds, providing information desk and • TECHNICAL PUBLICATION. Reports of personal search support, and enabling data completed research or a major significant exchange services. -
TAC Register Rev 6 22 Feb 2017
2/22/2017 Aircraft TAC TAC Register Rev 6 22 Feb 2017 THE REPOSITORY (SPREADSHEET): This data presented in this repository is a list of approved SACAA TACs as conferred to current foreign TC holders. Aircraft Type/Model File No. Conditions Category TAC Issue Issue Date Reissue Date Common Name 328 Support Services GmbH Dornier 328-100 & Dornier 328-300 J15/12/529 As per Type Certficate Data Sheet EASA.A.096 Standard Original 11 April 2007 - 328JET (328-300) Agusta S.p.A. (Now Leonardo Helicopter) A109E, A109K2, A109S, AW109SP and A109C J15/12/395 This certificate is issued as per EASA Type Certificate number EASA.R.005 Standard Reissue 15 September 1996 01 August 2013 AB139 J15/12/493 This certificate is issued as per EASA Type Certificate number EASA.R.006 Standard Original 21 April 2006 - AB139, AW139 AW189 J15/12/625 This certificate is issued as per EASA Type Certificate number EASA.R.510 Standard Original 24 November 2016 AW189 Air Tractor Inc. AT-402, AT-402B, AT-502, AT-502A, AT-502B & AT-504, AT-402A J15/12/327 This certificate is issued as per FAA Type Certificate number A17SW Restricted Original 15 October 2013 28 July 2016 AT-602, AT-802 and AT-802A J15/12/380 This certificate is issued as per FAA Type Certificate number A19SW Restricted Original 15 October 2013 - Airbus SAS A300B4-622R J15/12/565 This certificate is issued as per DGAC Type Certificate number 72. Standard Original 23 December 2009 - A320-232, A320-233 J15/12/593 This certificate is issued as per EASA Type Certificate number EASA.A.064 Standard Original 23 December 2011 - A330-301, A330-321, A330-322, A330- 341, A330-342, A330-202, A330-223, A330-243, A330-323, A330-343, A330- 203, A330-201, A330-302, A330-303, A330-223F and A330-243F J15/12/584 This certificate is issued as per EASA Type Certificate number EASA.A.004 Standard Original 08 December 2010 10 November 2016 A340-200, A340-300 and A340-600 series J15/12/382 As per DGAC Type Certficate number 183. -
Airplane Icing
Federal Aviation Administration Airplane Icing Accidents That Shaped Our Safety Regulations Presented to: AE598 UW Aerospace Engineering Colloquium By: Don Stimson, Federal Aviation Administration Topics Icing Basics Certification Requirements Ice Protection Systems Some Icing Generalizations Notable Accidents/Resulting Safety Actions Readings – For More Information AE598 UW Aerospace Engineering Colloquium Federal Aviation 2 March 10, 2014 Administration Icing Basics How does icing occur? Cold object (airplane surface) Supercooled water drops Water drops in a liquid state below the freezing point Most often in stratiform and cumuliform clouds The airplane surface provides a place for the supercooled water drops to crystalize and form ice AE598 UW Aerospace Engineering Colloquium Federal Aviation 3 March 10, 2014 Administration Icing Basics Important Parameters Atmosphere Liquid Water Content and Size of Cloud Drop Size and Distribution Temperature Airplane Collection Efficiency Speed/Configuration/Temperature AE598 UW Aerospace Engineering Colloquium Federal Aviation 4 March 10, 2014 Administration Icing Basics Cloud Characteristics Liquid water content is generally a function of temperature and drop size The colder the cloud, the more ice crystals predominate rather than supercooled water Highest water content near 0º C; below -40º C there is negligible water content Larger drops tend to precipitate out, so liquid water content tends to be greater at smaller drop sizes The average liquid water content decreases with horizontal -
CAP High Ground 18.03
The High Ground A Newsletter From Wyoming Wing Standards/Evaluation 15 March, 2018 Hot Topics Pilot Proficiency Profiles… The New Reality! With the implementation of CAPR 70-1 Flight Management, the Air Force came out with new requirements for documentation of training sorties. The AF now requires us to document what is planned, and what we actually accomplished during that sortie, per the Pilot Prof iciency Profile. We are required to accomplish all of the REQUIRED items listed in the PPP Checklist. We have to document each item and upload/note supporting documentation, or document why we did not accomplish the required item. Please review the preamble of the Pilot Proficiency Profiles (first page) and the specific Profile which you are planning on flying. Unfortunately, we can’t “just wing it” anymore. (Sigh) This ain’t my idea, this is from “On High”. Pilot Proficiency Profiles To review, the Pilot Proficiency Profiles, dated 01 January 2018, have changes. Best to print out a copy and keep it handy while operating under any one of these Profiles. And the Profiles are now to be documented in the “Profile Used” in WMIRS as P#, i.e. Profile number 1 would be entered as “P1”. Note that each Profile has a header which dictates the PIC qualifications to operate under that Profile. Read these before you attempt to fly the Profile. Now the BIG CHANGE is in the details of each Profile, what we are expected to do, and what we have to document for each Pilot Proficiency Profile sortie. Each PPP has in its description “Routine” and “Required” Items. -
Supplementary Materials
Experiment 1 Accidentally the young woman snubbed the acquaintance/*vinegar… Accidentally the young woman packed the vinegar/*acquaintance… After clearing the table at the diner the busboy thanked the cook/*pots… After clearing the table at the diner the busboy rinsed the pots/*cook… After feeding the infant the parent burped the tot/*cloth… After feeding the infant the parent unbuttoned the cloth/*tot… After getting his last card the high roller deceived the gambler/*money… After getting his last card the high roller hurled the money/*gambler… After heavy snowfalls in winter the old man thanked the groundskeeper/*stairs… After heavy snowfalls in winter the old man salted the stairs/*groundskeeper… After her son left for boarding school the mother praised the lad/*toys… After her son left for boarding school the mother stored his toys/*lad… After his daughter left the church the priest shunned the boyfriend/*tradition… After his daughter left the church the priest reiterated the tradition/*boyfriend… After much deliberation the university president appointed the director/*campus… After much deliberation the university president expanded the campus/*director… After school was out for the day the janitor insulted the superintendent/*cafeteria… After school was out for the day the janitor mopped the cafeteria/*superintendent… After she had been married for five years the woman divorced the deadbeat/*post… After she had been married for five years the woman resumed the post/*deadbeat… After soccer practice was over the player invited the teammate/*decision… -
Project Department of Automotive and Aeronautical
Project Department of Automotive and Aeronautical Engineering Aircraft Design Studies Based on the ATR 72 Author: Mihaela Florentina Niţă Examiner: Prof. Dr.-Ing. Dieter Scholz, MSME Delivered: 13.06.2008 Abstract This project gives a practical description of a preliminary aircraft design sequence. The sequence starts with a preliminary sizing method. The design sequence is illustrated with a redesign study of the ATR 72 turboprop aircraft. The requirements for the redesign aircraft are those of the ATR 72. The ATR 72 serves also as the reference during the redesign. The Preliminary sizing method was available (at the university) only for jet-powered aircraft. Therefore the method was adapted to work also with propeller driven aircrafts. The sizing method ensures that all requirements are met: take-off and landing field length, 2nd segment and missed approach gradients as well as cruise Mach number. The sizing method yields the best (low) power/weight ratio and the best wing loading. The redesign process covers all the aircraft components: fuselage, wing, empennage and landing gear. The aircraft design sequence defines the cabin layout, the wing parameters, the type of high lift system, the configuration and surface of the empennage. A mass distribution analysis is made, the position of the CG is calculated and the wing position determined. Finally the Direct Operating Costs (DOC) are calculated. DOCs are calculated applying the method from the Association of European Airlines (AEA). The DOCs serve for an aircraft evaluation. In order to meet requirements, the redesigned ATR 72 had to be slightly modified compared to the original ATR. -
Avation Increases to 35 Its Fleet of ATR 72S
Avation increases to 35 its fleet of ATR 72s ATR and the Singapore-based lessor announce 5 additional ATR 72-600s Singapore, February 16, 2016 – The world’s leading turboprop manufacturer ATR and the Singapore-based commercial aircraft lessor Avation PLC announced an agreement for the purchase of five new ATR 72-600 aircraft. At list prices the acquisition is valued at about US $130 million and brings to 35 the total number of firm ATR 72s ordered by Avation PLC since their first ATR purchase in 2011. As of today, Avation has already taken delivery of over 20 ATR 72s, mostly ATR 72-600s, which currently fly in the liveries of Virgin Australia, Flybe (for Scandinavian Airlines), UNI Air (Taiwan), Air India and Fiji Airways. Deliveries of the remaining ATR 72-600s on order extend out to 2018. ATR aircraft are the best-selling regional aircraft for below-90-seats size since 2010, representing 77% of global orders for turboprops. ATR is also experiencing an outstanding success among leasing firms in the same period, booking 87% of all their orders for below-90-seat regional aircraft. Avation is the second largest lessor by number of new ATRs ordered. According to Jeff Chatfield, Avation’s Executive Chairman, “We believe the ATR 72 is the most efficient aircraft type for regional routes. It provides the lowest fuel burn and the most reduced operating costs among all regional aircraft of its category. ATRs are superb assets for lessors, they offer great returns and also allow portfolio diversification. Avation raises equity and debt with the London and New York markets and we are proud to promote the ATR in these essential forums”. -
E N a C / Eetac Atr
E N A C / EETAC ATR FAA regulation analysis for ATR ETOPS validation Jordi CLARAMUNT SEGURA IENAC14 - Erasmus End of studies report / Treball Final de Grau 11/08/2017 FAA regulation analysis for ATR ETOPS validation 2 3 FAA regulation analysis for ATR ETOPS validation Acknowledgements With deepest gratitude and appreciation, I humbly give thanks to the people who helped me in making this end of studies project a possible one. First of all, I would like to offer my special thanks to Souhir Charfeddine, my internship tutor in ATR, for choosing me among the other candidates and giving me the possibility to perform this internship. Thanks for her valuable and constructive help during the planning and development of this internship. I really appreciate all the time she has dedicated to me with all the different meetings we have had inside the company. I have learnt a lot at her side, she has been an amazing tutor. Thank you. I am also grateful to all of those with whom I have had the pleasure to work with during this project. Each of the members I have worked with have provided me extensive and professional guidance and taught me a great deal about certification aspects, as well as other domains. Those include Antonio Paradies, Didier Cailhol, Eric Bédessem, Ciro Manco, Fabien Vançon, Jean-Paul Delpont, Nadège Gualina and Lucille Mitchell. Also, I would like to offer my gratitude to ENAC for first, giving me the possibility to join their Erasmus programme in its great university and then, for allowing me having the chance to do the internship, which has been the best election of my life so far. -
European Aviation Safety Agency
TCDS No.: EASA.A.084 ATR 42 - ATR 72 Page 1 of 35 Issue: 03 Date: 17 October 2012 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. EASA.A.084 for ATR 42 and ATR 72 Type Certificate Holder: ATR-GIE Avions de Transport Régional 1, Allée Pierre Nadot 31712 Blagnac Cedex FRANCE Transport Category: Large Aeroplanes For Models: ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500 ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, ATR 72-212A TCDS No.: EASA.A.084 ATR 42 - ATR 72 Page 2 of 35 Issue: 03 Date: 17 October 2012 Intentionally left blank TCDS No.: EASA.A.084 ATR 42 - ATR 72 Page 3 of 35 Issue: 03 Date: 17 October 2012 TABLE OF CONTENTS SECTION 1: ATR 42 Series ...................................................................................... 4 I. General .......................................................................................................................... 4 II. Certification Basis .......................................................................................................... 5 III. Technical Characteristics and Operational Limitations .................................................11 IV. Operating and Service Instructions ..............................................................................18 SECTION 2: ATR 72 Series .................................................................................... 19 I. General .........................................................................................................................19 II. Certification