Airplane Flying Handbook (FAA-H-8083-3B) Chapter 17
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The Canadian Rule Book for Flag Football
The Canadian Rule Book for Flag Football Football Canada — Flag Football Rules Committee Members John Turner, Football PEI Shannon Noel, Football Nova Scotia Francois Bougie, Flagbec Arliss Wilson, Football New Brunswick Mike Thomas, Football Saskatchewan Editor and Rules’ Interpreter Robert St-Pierre, Football PEI Football Canada Consultant Shannon Donovan All Rights Reserved 2013. Canadian Amateur Football Association e 2015 Également disponible en Français sous Ie titre —Manuel des règlements canadiens de Flag Football. Flag Football Rule Book Provincial Associations Football British Columbia Football New Brunswick 222- 6939 Hastings Street 215 Carriage Hill Dr. Burnaby, B.C. V5B 1S9 Fredericton, NB E3E 1A4 Tel: 604-583-9363 Tel: 506-260-2993 Fax: 604-583-9939 www.footballnewbrunswick.nb.ca www.playfootball.bc.ca Football Nova Scotia Football Alberta 1076 Highway 2 11759 Groat Road Lantz, NS B2S 1M8 Edmonton, Alberta T5M 3K6 Tel: (902) 425-5450 extension 371 Tel: 780-427-8108 Fax: (902) 477-3535 Fax: 780-427-0524 www.footballnovascotia.ca www.footballalberta.ab.ca Football P.E.I. Football Saskatchewan 40 Enman Crescent 1860 Lorne Street Charlottetown, PE C1E 1E6 Regina, Saskatchewan S4P 2L7 Tel: 902-368-4262 Tel: 306-780-9239 Fax: 902-368-4548 Fax: 306-525-4009 www.footballpei.com www.footballsaskatchewan.ca Ontario Football Alliance Football Manitoba 30-7384 Wellington Road 506-145 Pacific Avenue Guelph, ON N1H 6J2 Winnipeg, MB R3B 2Z6 Tel: 519-780-0200 Tel: 204-925-5769 Fax: 519-780-0705 Fax: 204-925-5772 www.ontariofootballalliance.ca www.footballmanitoba.com Football Quebec 4545 Ave. Pierre de Coubertin CP 1000, Station M Montreal, QC H1V 3R2 Tel: 514-252-3059 Fax: 514-252-5216 www.footballquebec.com For additional copies of this book, please contact your Provincial Association. -
Lighting up to 7 Times Brighter Than Other LED Landing Lights!
Lighting FAA-PMA Approved AeroLEDs Lighting Increase safety and reduce operating cost! See the Difference... Lighting Know the Difference... • Increased safety • Direct replacement • Up to 80% reduced power consumption • Long life - over 50,000 hours! • Lighter weight - no heavy power supply - save up to 3 lbs • Reduced drag • Zero maintenance • 10x more efficient than incandescent! Increased Safety AeroLED lights allow you to comply with the latest FAA recommendations (Operation Lights On) regarding extended use of taxi, landing, and anti-collision lights without fear of reduced light performance or life. They all feature optimized light color (6500k sunlight equivalent) for proven superior air-to-air recognition. The landing and taxi lights also feature an optional pulsed recognition light mode. Reduced Power Consumption High efficiency LED lights use less than 1/3 the power of halogen bulbs. They significantly reduce the load on the electrical system and they won't dim due to low voltage, typical of low RPM final approaches when you need them most! Postition lights aerodynamic design results in less drag than original equipment! Longer Life - Zero Maintenance All AeroLED products are designed to be a "lifetime buy". They last over 50,000 hours when properly installed and do not degrade with on/off cycles. They are extremely rugged and hardened against all kinds of electrical damage, shock, and vibration. Up to 7 times brighter than other LED landing lights! PAR36 Landing Light Comparison Measured Brightness at 50 Ft. Manufacturer Intensity -
Into the Woods Is Presented Through Special Arrangement with Music Theatre International (MTI)
PREMIER SPONSOR ASSOCIATE SPONSOR MEDIA SPONSOR Music and Lyrics by Book by Stephen Sondheim James Lapine June 28-July 13, 2019 Originally Directed on Broadway by James Lapine Orchestrations by Jonathan Tunick Original Broadyway production by Heidi Landesman Rocco Landesman Rick Steiner M. Anthony Fisher Frederic H. Mayerson Jujamcyn Theatres Originally produced by the Old Globe Theater, San Diego, CA. Scenic Design Costume Design Shoko Kambara† Megan Rutherford Lighting Design Puppetry Consultant Miriam Nilofa Crowe† Peter Fekete Sound Design Casting Director INTO The Jacqueline Herter Michael Cassara, CSA Woods Musical Director Choreographer/Associate Director Daniel Lincoln^ Andrea Leigh-Smith Production Stage Manager Production Manager Myles C. Hatch* Adam Zonder Director Michael Barakiva+ Into the Woods is presented through special arrangement with Music Theatre International (MTI). All authorized performance materials are also supplied by MTI. www.MTIShows.com Music and Lyrics by Book by STEPHEN JAMES Directed by SONDHEIM LAPINE MICHAEL * Member of Actor’s Equity Association, † USA - Member of Originally directed on Broadway by James LapineBARAKIVA the Union of Professional Actors and United Scenic Artists Orchestrations by Jonathan Tunick Stage Managers in the United States. Local 829. ^ Member of American Federation of Musicians, + Local 802 or 380. CAST NARRATOR ............................................................................................................................................HERNDON LACKEY* CINDERELLA -
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. -
NASA's Real World: Mathematics
National Aeronautics and Space Administration NASA’s Real World: Mathematics Educator Guide “Preparing for a Soft Landing” Educational Product Educators & Students Grades 6-8 www.nasa.gov NP-2008-09-106-LaRC Preparing For A Soft Landing Grade Level: 6-8 Lesson Overview: Students are introduced to the Orion Subjects: Crew Exploration Vehicle (CEV) and NASA’s plans Middle School Mathematics to return to the Moon in this lesson. Thinking and acting like Physical Science engineers, they design and build models representing Orion, calculating the speed and acceleration of the models. Teacher Preparation Time: 1 hour This lesson is developed using a 5E model of learning. This model is based upon constructivism, a philosophical framework or theory of learning that helps students con- Lesson Duration: nect new knowledge to prior experience. In the ENGAGE section of the lesson, students Five 55-minute class meetings learn about the Orion space capsule through the use of a NASA eClips video segment. Teams of students design their own model of Orion to be used as a flight test model in the Time Management: EXPLORE section. Students record the distance and time the models fall and make sug- gestions to redesign and improve the models. Class time can be reduced to three 55-minute time blocks During the EXPLAIN section, students answer questions about speed, velocity and if some work is completed at acceleration after calculating the flight test model’s speed and acceleration. home. Working in teams, students redesign the flight test models to slow the models by National Standards increasing air resistance in the EXTEND section of this lesson. -
How to Line the Fields
HOW TO LINE THE FIELDS The Playing Area FIELD DIMENSIONS Section 1. The playing area shall be rectangular and marked with a solid lined boundary. The field should be between 110 to 140 yards from end line to end line; and between 60 to 70 yards from sideline to sideline. The goals shall be placed no more than 100 yards and no less than 90 yards apart, measured from goal line to goal line. There must be a minimum of 10 yards and a maximum of 20 yards of space behind each goal line, extending to the end line and running the width of the field. There must be a minimum of 4m of space between the sideline boundary and the scorer’s table. There should be at least 4m of space between the other sideline and any spectator area. There should be 2m of space beyond each end line. Section 2. It shall be the host institution’s responsibility to see that the field is in proper condition for safe play, and that the field is consistent with the Rules. Where these field dimension requirements are not or cannot be met due to field space limitations, play may take place if the visiting team has been notified in writing prior to the day of the game and personnel from both participating teams agree. However, the minimum distance of 10 yards of space from goal line to end line must be maintained. Soft/flexible cones, pylons or flags must be used to mark the corners of the field. The playing area must be flat and free of glass, stones, and any protruding objects. -
Bell 429 Product Specifications
BELL 429 SPECIFICATIONS BELL 429 SPECIFICATIONS Publisher’s Notice The information herein is general in nature and may vary with conditions. Individuals using this information must exercise their independent judgment in evaluating product selection and determining product appropriateness for their particular purpose and requirements. For performance data and operating limitations for any specific mission, reference must be made to the approved flight manual. Bell Helicopter Textron Inc. makes no representations or warranties, either expressed or implied, including without limitation any warranties of merchantability or fitness for a particular purpose with respect to the information set forth herein or the product(s) and service(s) to which the information refers. Accordingly, Bell Helicopter Textron Inc. will not be responsible for damages (of any kind or nature, including incidental, direct, indirect, or consequential damages) resulting from the use of or reliance on this information. Bell Helicopter Textron Inc. reserves the right to change product designs and specifications without notice. © 2019 Bell Helicopter Textron Inc. All registered trademarks are the property of their respective owners. FEBRUARY 2019 © 2019 Bell Helicopter Textron Inc. Specifications subject to change without notice. i BELL 429 SPECIFICATIONS Table of Contents Bell 429 ..................................................................................................................................1 Bell 429 Specification Summary (U.S. Units) ........................................................................4 -
Milton's Use of the Epic Simile in Paradise Lost
Loyola University Chicago Loyola eCommons Master's Theses Theses and Dissertations 1941 Milton's Use of the Epic Simile in Paradise Lost Francis Louis Martinsek Loyola University Chicago Follow this and additional works at: https://ecommons.luc.edu/luc_theses Part of the English Language and Literature Commons Recommended Citation Martinsek, Francis Louis, "Milton's Use of the Epic Simile in Paradise Lost" (1941). Master's Theses. 289. https://ecommons.luc.edu/luc_theses/289 This Thesis is brought to you for free and open access by the Theses and Dissertations at Loyola eCommons. It has been accepted for inclusion in Master's Theses by an authorized administrator of Loyola eCommons. For more information, please contact [email protected]. This work is licensed under a Creative Commons Attribution-Noncommercial-No Derivative Works 3.0 License. Copyright © 1941 Francis Louis Martinsek J3 MILTON'S USE OF THE EPIC SIMILE IN PARADISE -LOST by Francis Louis Martinsek, S.J. JUNE 1941 A THESIS SUBMITTED IN PARTIAL FULFILL~ffiNT OF THE REQUIREMENTS FOR THE DEGREE OF W~STER OF ARTS IN LOYOLA UNIVERSITY VITA AUCTORIS Francis L. ~~rtinsek, S.J., was born at Export, Pennsylvania, on November 12, 1912. He received his elementary training at Export Public Schools, and his high-school training at Export Junior High School and Trafford City High School. He entered Xavier University, Cincinnati, in 1932 and transferred to West Baden College of Loyola University in 1935, where he received his Bachelor of Arts degree in 1936. TABLE OF CONTENTS INTRODUCTION PAGE Purpose of Thesis; Method~ Procedure •••••••••••1 CHAPTER I The Familz ~~~Epic Simile •••••••••••••••~ CHAPTER II The Function£!~ Simile••••••••••••••••••••••!! CHAPTER III ~Epic Simile in Paradise Lost ••••••••••••••••~ CHAPTER IV The Epic Simile~ Milton's Style ••••••••••••••~ COl\fCLUSION •••••••••••••••••••••••••••••••••••••••••• •~ BIBLIOGRAPIIT • ••••••••••••••••••••••••••••••••••••••••§1_ L.D.S. -
EWIS Practices Job Aid 2.0
Aircraft EWIS Practices Job Aid 2.0 Federal Aviation Administration Aircraft Electrical Wiring Interconnect System (EWIS) Best Practices Job Aid Revision: 2.0 This job aid covers applicable 14 CFR part 25 aircraft (although it is also widely acceptable for use with other types of aircraft such as military, small airplanes, and rotorcraft). This job aid addresses policy; industry EWIS practices; primary factors associated with EWIS degradation; information on TC/STC data package requirements; EWIS selection and protection; routing, splicing and termination practices; and EWIS maintenance concepts (including how to perform a EWIS general visual inspection). The job aid also includes numerous actual aircraft EWIS photos and examples. UNCONTROLLED COPY WHEN DOWNLOADED 1 Aircraft EWIS Practices Job Aid 2.0 Additional Notes • This presentation contains additional speaker notes for most slides • It’s advisable to read these notes while viewing the slide presentation Aircraft EWIS Best Practices Job Aid 2.0 Federal Aviation 2 Administration UNCONTROLLED COPY WHEN DOWNLOADED 2 Aircraft EWIS Practices Job Aid 2.0 Printing the Additional Notes To print the slides and accompanying speaker notes: – Navigate back to the FAA Aircraft Certification job aids web page – Open and print Printable Slides and Notes Aircraft EWIS Best Practices Job Aid 2.0 Federal Aviation 3 Administration UNCONTROLLED COPY WHEN DOWNLOADED 3 Aircraft EWIS Practices Job Aid 2.0 Background • Why the need for EWIS best practices Job Aid? – Accident/Incident Service History – Aging Transport Systems Rulemaking Advisory Committee (ATSRAC) – Enhanced Airworthiness Program for Airplane System (EAPAS) – EAPAS Rule Making Aircraft EWIS Best Practices Job Aid 2.0 Federal Aviation 4 Administration Historically, wiring and associated components were installed without much thought given to the aging aspects: • Fit and forget. -
EVALUATION of a COLLISION AVOIDANCE and MITIGATION SYSTEM (CAMS) on WINTER MAINTENANCE TRUCKS Research Administration Reference Number: OR17-103
EVALUATION OF A COLLISION AVOIDANCE AND MITIGATION SYSTEM (CAMS) ON WINTER MAINTENANCE TRUCKS Research Administration Reference Number: OR17-103 Prepared for Michigan Department of Transportation Division of Research 8885 Ricks Road Lansing, MI 48917 Prepared by Michigan State University Department of Civil and Environmental Engineering 428 South Shaw Lane East Lansing, MI 48824 Institute for Transportation Iowa State University 2711 South Loop Drive, Suite 4700 Ames, IA 50010 FreezePoint Consulting 179 University Circle Akron, OH SEPTEMBER 21, 2018 Technical Report Documentation Page 1. Report No. 2. Government Accession No. 3. MDOT Project Manager OR 17-103 N/A Steven J. Cook, P.E. 4. Title and Subtitle 5. Report Date EVALUATION OF A COLLISION AVOIDANCE AND MITIGATION September 21, 2018 SYSTEM (CAMS) ON WINTER MAINTENANCE TRUCKS 6. Performing Organization Code N/A 7. Author(s) 8. Performing Organization Report No. Ali Zockaie, Ramin Saedi, Timothy Gates, Peter Savolainen, Bill Schneider, N/A Mehrnaz Ghamami, Rajat Verma, Fatemeh Fakhrmoosavi, Mohammad Kavianipour, MohammadHossein (Sam) Shojaei, Harprinderjot Singh, Jacob Warner, and Chao Zhou 9. Performing Organization Name and Address 10. Work Unit No. (TRAIS) Michigan State University N/A 428 S. Shaw Lane 11. Contract or Grant No. East Lansing, Michigan 48824 2018-0060 11 (a). Authorization No. 12. Sponsoring Organization Name and Address 13. Type of Report and Period Covered Michigan Department of Transportation Final Report Research Administration 10/01/2017 to 09/30/2018 8885 Ricks Rd. P.O. Box 30049 14. Sponsoring Agency Code Lansing, Michigan 48909 N/A 15. Supplementary Notes Conducted in cooperation with the U.S. Department of Transportation, Federal Highway Administration. -
Emergency Procedures C172
EMERGENCY PROCEDURES NON CRITICAL ACTION June 2015 1. Maintain aircraft control. Table of Contents 2. Analyze the situation and take proper action. C 172 3.Land as soon as conditions permit NON CRITICAL ACTION PROCEDURES E-2 GROUND OPERATION EMERGENCIES GROUND OPERATION EMERGENCIES E-2 Emergency Engine Shutdown on the Ground Emergency Engine Shutdown on the Ground E-2 1. FUEL SELECTOR -------------------------------- OFF Engine Fire During Start E-2 2. MIXTURE ---------------------------- IDLE CUTOFF TAKEOFF EMERGENCIES E-2 3. IGNITION ------------------------------------------ OFF Abort E-2 4. MASTER SWITCH ------------------------------- OFF IN-FLIGHT EMERGENCIES E-3 Engine Failure Immediately After T/O E-3 Engine Fire during Start Engine Failure In Flt - Forced Landing E-3 If Engine starts Engine Fire During Flight E-4 1. POWER ------------------------------------- 1700 RPM Emergency Descent E-4 2. ENGINE -------------------------------- SHUTDOWN Electrical Fire/High Ammeter E-4 If Engine fails to start Negative Ammeter Reading E-4 1. CRANKING ----------------------------- CONTINUE Smoke and Fume Elimination E-5 2. MIXTURE --------------------------- IDLE CUT-OFF Oil System Malfunction E-4 3 THROTTLE ----------------------------- FULL OPEN Structural Damage or Controllability Check E-5 4. ENGINE -------------------------------- SHUTDOWN Recall E-6 FUEL SELECTOR ------ OFF Lost Procedures E-6 IGNITION SWITCH --- OFF Radio Failure E-7 MASTER SWITCH ----- OFF Diversions E-8 LANDING EMERGENCIES E-9 TAKEOFF EMERGENCIES Landing with flat tire E-9 ABORT E-9 LIGHT SIGNALS 1. THROTTLE -------------------------------------- IDLE 2. BRAKES ----------------------------- AS REQUIRED E-2 E-1 IN-FLIGHT EMERGENCIES Engine Fire During Flight Engine Failure Immediately After Takeoff 1. FUEL SELECTOR --------------------------------------- OFF 1. BEST GLIDE ------------------------------------ ESTABLISH 2. MIXTURE------------------------------------ IDLE CUTOFF 2. FUEL SELECTOR ----------------------------------------- OFF 3. -
Comment Response Document
EASA SC-VTOL-01 Comment Response Document Note: The comments have been grouped by theme or objective and renumbered sequentially. Bookmarks are available to navigate the document. General type of vehicle Explanatory Note 1: type of vehicle The Special Condition (SC) has been developed to cover a new category of person-carrying vertical take-off and landing (VTOL) heavier-than-air aircraft with lift/thrust units used to generate powered lift and control. The vertical take-off and landing capability distinguishes this type of aircraft from aeroplanes. The Special Condition does not intend to cover traditional rotorcraft either but rather aircraft with distributed lift/thrust and it will be clarified that, for the SC to be applicable, more than 2 lift/thrust units should be used to provide lift during vertical take-off or landing. The Special Condition background mentioned “the aircraft may not be able to perform an autorotation or a controlled glide in the event of a loss of lift/thrust” as it is the case for some VTOL aircraft being proposed, however this is not a requirement. Comment Comment summary Suggested resolution Comment is an Comment is EASA EASA response observation or substantive or comment is a is an NR Author Paragraph Page disposition suggestion* objection** 1 1David Loebl, Background/Sc 1 “Although hover flight may be possible, the aircraft Clarify the condition where no glide is possible: Yes No Noted See Explanatory Note 1 AutoFlightX ope may not be able to perform an autorotation or a “…not be able to perform an autorotation or a controlled glide in the event of a loss of lift/thrust.” controlled glide in the event of a loss of lift/thrust implies that the given SC are not applicable for during hover.” transition vehicles that can fly also with aerodynamic lift.