How Can You Become a Pilot? What Is Ground School?
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Weather and Aviation: How Does Weather Affect the Safety and Operations of Airports and Aviation, and How Does FAA Work to Manage Weather-Related Effects?
Kulesa 1 Weather and Aviation: How Does Weather Affect the Safety and Operations of Airports and Aviation, and How Does FAA Work to Manage Weather-related Effects? By Gloria Kulesa Weather Impacts On Aviation In addition, weather continues to play a significant role in a number of aviation Introduction accidents and incidents. While National Transportation Safety Board (NTSB) reports ccording to FAA statistics, weather is most commonly find human error to be the the cause of approximately 70 percent direct accident cause, weather is a primary of the delays in the National Airspace contributing factor in 23 percent of all System (NAS). Figure 1 illustrates aviation accidents. The total weather impact that while weather delays declined with overall is an estimated national cost of $3 billion for NAS delays after September 11th, 2001, delays accident damage and injuries, delays, and have since returned to near-record levels. unexpected operating costs. 60000 50000 40000 30000 20000 10000 0 1 01 01 0 01 02 02 ul an 01 J ep an 02 J Mar May S Nov 01 J Mar May Weather Delays Other Delays Figure 1. Delay hours in the National Airspace System for January 2001 to July 2002. Delay hours peaked at 50,000 hours per month in August 2001, declined to less than 15,000 per month for the months following September 11, but exceeded 30,000 per month in the summer of 2002. Weather delays comprise the majority of delays in all seasons. The Potential Impacts of Climate Change on Transportation 2 Weather and Aviation: How Does Weather Affect the Safety and Operations of Airports and Aviation, and How Does FAA Work to Manage Weather-related Effects? Thunderstorms and Other Convective In-Flight Icing. -
Water Rocket Booklet
A guide to building and understanding the physics of Water Rockets Version 1.02 June 2007 Warning: Water Rocketeering is a potentially dangerous activity and individuals following the instructions herein do so at their own risk. Exclusion of liability: NPL Management Limited cannot exclude the risk of accident and, for this reason, hereby exclude, to the maximum extent permissible by law, any and all liability for loss, damage, or harm, howsoever arising. Contents WATER ROCKETS SECTION 1: WHAT IS A WATER ROCKET? 1 SECTION 3: LAUNCHERS 9 SECTION 4: OPTIMISING ROCKET DESIGN 15 SECTION 5: TESTING YOUR ROCKET 24 SECTION 6: PHYSICS OF A WATER ROCKET 29 SECTION 7: COMPUTER SIMULATION 32 SECTION 8: SAFETY 37 SECTION 9: USEFUL INFORMATION 38 SECTION 10: SOME INTERESTING DETAILS 40 Copyright and Reproduction Michael de Podesta hereby asserts his right to be identified as author of this booklet. The copyright of this booklet is owned by NPL. Michael de Podesta and NPL grant permission to reproduce the booklet in part or in whole for any not-for-profit educational activity, but you must acknowledge both the author and the copyright owner. Acknowledgements I began writing this guide to support people entering the NPL Water Rocket Competition. So the first acknowledgement has to be to Dr. Nick McCormick, who founded the competition many years ago and who is still the driving force behind the activity at NPL. Nick’s instinct for physics and fun has brought pleasure to thousands. The inspiration to actually begin writing this document instead of just saying that someone ought to do it, was provided by Andrew Hanson. -
APPLICATION for FLIGHT SCHOOL LICENSE Page 1 of 2 of 4Transportation9 Informationrequired by Act 327, P.A
Michigan Department APPLICATION FOR FLIGHT SCHOOL LICENSE Page 1 of 2 of 4Transportation9 Informationrequired by Act 327, P.A. of 1945 to apply for license. AERONAUTICS 00 (01/21) USE ONLY RETURN TO: DATE Michigan Department of Transportation Finance Cashier AMOUNT P. 0. Box 30648 Lansing, Ml 48909 LIC.NO. (517) 242-7771 or (517) 335-9283 EXP.DATE FEES: Initial - $25.00, Annual Renewal - $10.00, Late Renewal - $25.00. SCHOOL NAME PHONE NO. DATE I OWNER(S) SCHOOL MANAGER MAILLING ADDRESS CITY I ZIP CODE NAME OF THE AIRPORT WHERE FLIGHT SCHOOL WILL BE BASED FAX I E-MAIL Courses Offered: □ Private □ Part 141 School □ Type Ratings D Flight Instructor D Ground School □ Recreation □ Commercial D Sea Plane D Instrument □ Glider □ Sport □ Multi Engine D Airline Transport D Helicopter MAINTENANCE PERSONNEL Name Address FAA Certificate Number Chief Mechanic INSTRUCTOR FLIGHT Name Address FAA Certificate Number Chief Flight Instructor □ Instrument □ Multi Enoine □ Instrument □ Multi Enqine □ Instrument □ Multi Engine □ Instrument □ Multi Enoine □ Instrument □ Multi Engine □ Instrument □ Multi Enoine □ Instrument □ Multi Enqine Flight School Aircraft Michigan To be completed by State Registrar Aircraft Make Model N Number AERO USE ONLY Registration 1. □ Yes □ No 2. □ Yes □ No 3. □ Yes □ No 4. □ Yes □ No 5. □ Yes □ No 6. □ Yes □ No 7. □ Yes □ No MDOT4009 (01/21) Page 2 of 2 Flight School Manager Compliance Checklist and Certification Please answer the questions below. Refer to the enclosed Michigan Aeronautics Code, section 259.85 (Flight Schools) requirements. Yes No Do You: □ □ Operate from an airport licensed by the State of Michigan? □ □ Have a written commercial operating agreement with the airport at which the school is based? (Submit a copy with this application or submit airport manager signature). -
A “Short Course” on Ice and the TBM
A “Short Course” on Ice and the TBM. Icing is topical at the present time as a result of a recent accident in a TBM. I have had a number of conversations with pilots who I would consider knowledgeable and it is apparent that there is a lot of confusion surrounding this subject. Also noting on line posts this confusion is not limited to owner pilots. I have had occasion to be a victim of my own stupidity in a serious icing condition years ago and I can vouch that icing is a deadly serious situation in more ways than one. Before going on with the subject we want to stipulate that the data we are about to provide is a summary of information that is to be found on line, along with narrative and data provided from knowledgeable instructors, if any of the data provided conflicts with anything you have been taught we urge you to satisfy yourself as to which data is correct. TBM operators fly in the same airspace where we find Part 25 aircraft (Commercial Category) aircraft. There is a big difference in how these two categories of aircraft are affected by icing conditions. A 767 will often be climbing at over 300 kts and 4000+ ft/min at typical icing altitudes. This creates two very distinct advantages for the 767: first, their icing exposure time may be less than 1/3 of ours. Second, icing conditions are a function of TAT (Total Air Temperature), not SAT (static air temp). TAT is warmer than SAT because of the effects of compressibility as the airplane operates at faster and faster speeds. -
Cessna Owner Magazine Article, October 2017
The following article appeared in the October 2017 edition of CESSNA OWNER magazine, the official publication of the Cessna Owner Organization. Whether for business or pleasure, the Official Publication of the Cessna Owner Organization Since 1975 Cessna Owner Organization is dedicated to assisting CESSNA>> October 2017 aircraft owners in OWNER MAGAZINE their continual pursuit to become better, TKS smarter and safer ROTECTION owners and pilots. ICE P Since 1975, the Liquid Armor for the collective knowledge War on Icing and experience of its members has saved owners countless hours of downtime and thousands of dollars in operational expenses. www.cessnaowner.org www.facebook.com/ CessnaOwnerOrganization Est. 1975 Not a member? Learn more at www.CessnaOwner.org TKS Ice Protection Liquid Armor for the War on Icing By Scott Sherer here are many people out accumulation before launching. I wind is strong and the wind chill there who really like snow also have a heavy-duty tug for get- is very low. The winter cloud in Tsports; things like skiing, ting my bird in and out of the han- Wisconsin is dark and grey. (I say snowboarding, ice skating, hockey, gar quickly, and the Janitrol fur- “cloud” and not “clouds” because we snowmobiling and all of those other nace, along with an assortment of seem to have only one cloud here sports that you typically see during other engine and interior warming and it covers the entire state from the winter Olympics. I’m sure that contraptions, helps to get my plane November well into January!) many aviators enjoy some of these warm and ready fast. -
Leading the Charge We Put TBM 940 Speedster Through Its Paces for NBAA
15-21 October 2019 I flightglobal.com FLIGHT TEST Leading the charge We put TBM 940 speedster through its paces for NBAA £3.90 Wow, how? ACES high 42 Questions remain over defunct US Air Force boosts Collins Icelandic carrier’s comeback 13 with ejection seat deal 20 9 770015 371310 FLIGHT TEST Power of one Turboprop-single family has been a market success since launch in 1988, amassing sales of more than 900 units across three variants Daher has delivered a compelling offer for owner-flyers, with a range of enhancements on the TBM 940 providing an edge over the piston-twin segment. We put it through its paces MICHAEL GERZANICS POMPANO BEACH have allowed single-engined designs to make to be efficient. Airspace congestion, however, inroads into the twin-turbine segment. can make reaching optimum altitudes for jets he single-engined turboprop market The growth of the single-engined turbo- problematic, so their real-world range can be is populated by numerous aircraft of prop segment is based on the near-bulletproof shorter. Jets also have higher direct operating varying configurations. In broad reliability and scalability of the PT6 family. costs, however. T strokes, it can be broken down into This paradigm shift from piston-twins to tur- Runway performance and training require- two segments: fast, low-winged aircraft and bine-singles is conceptually on par with ex- ments are also two factors that fuel the single- slower, more spacious high-winged designs. tended twin-engine operations authorisations engined turboprop segment, because runway In the West, these diverse offerings share a all but killing off three- and four-engined civil length for turboprops is shorter than that single critical component – their engine. -
Integrated Diagnostics of Rocket Flight Control
IEEE AEROSPACE CONFERENCE ¢ MARCH 2005, BIG SKY, MT Integrated Diagnostics of Rocket Flight Control Dimitry Gorinevsky¤, Sikandar Samary; Honeywell Labs, Fremont, CA 94539 John Bain, Honeywell Space Systems, Houston, TX 77058 and Gordon Aaseng, Honeywell Space Systems, Glendale, AZ 85308 Abstract— This paper describes an integrated approach to the approach by using simulated telemetry data for a launch parametric diagnostics demonstrated in a flight control sim- vehicle of Space Shuttle class. Faults seeded in the simula- ulation of a space launch vehicle. The proposed diagnostic tion are subsequently estimated by the VHM algorithms to approach is able to detect incipient faults despite the natural validate their performance. The estimated fault parameters masking properties of feedback in the guidance and control include air drag change from aerodynamic surface damage. loops. Estimation of time varying fault parameters uses para- This could model leading edge damage like that sustained metric vehicle-level data and detailed dynamical models. The in the Columbia Accident STS-107 mission. We also con- algorithms explicitly utilize the knowledge of fault mono- sider estimation and trending of such parameters as propul- tonicity (damage can only increase, never improve with time) sion performance, thrust vectoring actuator/gimbal wear, and where available. The developed algorithms can be applied a drift in one of GN&C sensors (pitch angle). These faults to health management of next generation space systems. We are choosen as plausible representative faults that demon- present a simulation case study of rocket ascent application strate the detection algorithm effectiveness. Development of to illustrate and validate the proposed approach. a practical VHM system would require an additional careful analysis and engineering of the fault models in the VHM al- TABLE OF CONTENTS gorithms. -
LORD Flight Control Equipment
LORD Flight Control Equipment ELECTROMECHANICAL SOLUTIONS LORD provides customers innovative offerings globally with best-in-class cockpit controls • Inceptors to convert pilot inputs into flight control system commands • Force feedback optimized for pilot effectiveness • Electromechanical actuators for deployment of doors, landing gear, vents and control surfaces • Worldwide distribution, repair and overhaul network with AOG stock, servicing OEMs and end users Typical Applications: Benefits: • Cockpit Controls/ • Enable safer flights Inceptors Flight Controls for Business and Commercial Aircraft • Reduce pilot workload • Actuators • Reduce aircraft weight • Sensors • Optimize drag of wings • Dampers Side Stick • Enhance pilot comfort Throttle Control Flaps and Spoiler Levers Electric Pedals Actuator Systems for Aircraft and Helicopters • Door Systems • Flight Control Systems • Force Feel Systems • Locking Systems Our extensive experience in commercial fixed wing flight control systems and our innovative active vibration control systems in helicopters combine to make us a great partner for providing advanced flight control interfaces for aerospace applications. Cockpit Control Solutions LORD inceptors provide functional and ergonomic interfaces between pilots and various aircraft systems. Our Cockpit Control solutions are compact and lightweight and can be seamlessly integrated into cockpit designs. LORD flight control inceptors can be tailored to sidestick or yoke based cockpit layouts. Pilot Interface with: Modular Inceptor Components: • Flight Control Systems • Force Feel Dampers • Engine Control Systems • RVDT Transducer Units • Landing Gear Systems • Force Transducer Units Integrated Inceptors: • Auto Throttle Control Unit • Speed Brake Control Unit • Flap and Slat Control Unit • Nose Wheel Steering Hand Wheel • Side Stick (or Yoke) • Rudder and Brake Pedals Electromechanical Actuators Current aircraft primarily use hydraulic actuators to move surfaces and manage the landing gear operations. -
09 Stability and Control
Aircraft Design Lecture 9: Stability and Control G. Dimitriadis Introduction to Aircraft Design Stability and Control H Aircraft stability deals with the ability to keep an aircraft in the air in the chosen flight attitude. H Aircraft control deals with the ability to change the flight direction and attitude of an aircraft. H Both these issues must be investigated during the preliminary design process. Introduction to Aircraft Design Design criteria? H Stability and control are not design criteria H In other words, civil aircraft are not designed specifically for stability and control H They are designed for performance. H Once a preliminary design that meets the performance criteria is created, then its stability is assessed and its control is designed. Introduction to Aircraft Design Flight Mechanics H Stability and control are collectively referred to as flight mechanics H The study of the mechanics and dynamics of flight is the means by which : – We can design an airplane to accomplish efficiently a specific task – We can make the task of the pilot easier by ensuring good handling qualities – We can avoid unwanted or unexpected phenomena that can be encountered in flight Introduction to Aircraft Design Aircraft description Flight Control Pilot System Airplane Response Task The pilot has direct control only of the Flight Control System. However, he can tailor his inputs to the FCS by observing the airplane’s response while always keeping an eye on the task at hand. Introduction to Aircraft Design Control Surfaces H Aircraft control -
F-117A Accident During Air Show Flyover Caused by Omission of Fasteners in Wing-Support Structure
FLIGHT SAFETY FOUNDATION Aviation Mechanics Bulletin SEPTEMBER–OCTOBER 1998 F-117A Accident during Air Show Flyover Caused by Omission of Fasteners in Wing-support Structure FLIGHT SAFETY FOUNDATION Aviation Mechanics Bulletin Dedicated to the aviation mechanic whose knowledge, craftsmanship and integrity form the core of air safety. Robert A. Feeler, editorial coordinator September–October 1998 Vol. 46 No. 5 F-117A Accident during Air Show Flyover Caused by Omission of Fasteners in Wing-support Structure.......................................................... 1 Maintenance Alert ...................................................................................... 9 News & Tips ............................................................................................... 13 AVIATION MECHANICS BULLETIN Copyright © 1998 FLIGHT SAFETY FOUNDATION INC. ISSN 0005-2140 Suggestions and opinions expressed in FSF publications belong to the author(s) and are not necessarily endorsed by Flight Safety Foundation. Content is not intended to take the place of information in company policy handbooks and equipment manuals, or to supersede government regulations. Staff: Roger Rozelle, director of publications; Wayne Rosenkrans, senior editor; Mark Lacagnina, senior editor; John D. Green, copyeditor; Rick Darby, editorial consultant; Karen K. Ehrlich, production coordinator; Ann L. Mullikin, assistant production coordinator; and David Grzelecki, librarian, Jerry Lederer Aviation Safety Library. Subscriptions: US$35 (U.S.-Canada-Mexico), US$40 Air Mail (all other countries), six issues yearly. • Include old and new addresses when requesting address change. • Flight Safety Foundation, Suite 300, 601 Madison Street, Alexandria, VA 22314 U.S. • Telephone: (703) 739-6700 • Fax: (703) 739-6708 We Encourage Reprints Articles in this publication, in the interest of aviation safety, may be reprinted, in whole or in part, in all media, but may not be offered for sale or used commercially without the express written permission of Flight Safety Foundation’s director of publications. -
Evaluation of Two Unique Side Stick Controllers in a Fixed-Base Flight Simulator
NASA/TM-2003-212042 Evaluation of Two Unique Side Stick Controllers in a Fixed-Base Flight Simulator Jann Mayer and Timothy H. Cox NASA Dryden Flight Research Center Edwards, California December 2003 The NASA STI Program Office…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 Office plays a key or other meetings sponsored or cosponsored part in helping NASA maintain this by NASA. important role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program Office is operated by technical, or historical information from Langley Research Center, the lead center for NASA programs, projects, and mission, NASA’s scientific and technical information. often concerned with subjects having The NASA STI Program Office provides access substantial public interest. to the NASA STI Database, the largest collection of aeronautical and space science STI in the • TECHNICAL TRANSLATION. English- world. The Program Office is also NASA’s language translations of foreign scientific institutional mechanism for disseminating the and technical material pertinent to results of its research and development activities. NASA’s mission. These results are published by NASA in the NASA STI Report Series, which includes the Specialized services that complement the STI following report types: Program Office’s diverse offerings include creating custom thesauri, building customized databases, organizing and publishing research • TECHNICAL PUBLICATION. Reports of results…even providing videos. completed research or a major significant phase of research that present the results of For more information about the NASA STI NASA programs and include extensive data Program Office, see the following: or theoretical analysis. -
DESIGN and ANALYSIS of PERFORMANCE PARAMETERS of WING with FLAPERONS Debanjali Dey, R.Aasha #Department of Aeronautical Engineering , KCG College of Technology
International Journal of Scientific Research and Review ISSN NO: 2279-543X DESIGN AND ANALYSIS OF PERFORMANCE PARAMETERS OF WING WITH FLAPERONS Debanjali Dey, R.Aasha #Department of Aeronautical Engineering , KCG College Of Technology. 1. [email protected] 2. [email protected] ABSTRACT- The main objective of this project is to design a flaperon for a wing and compare the performance characteristic of this flaperon-wing combination with that of conventional wing design that makes use of separate flap and aileron. Theoretical analysis and comparison is performed following which the computational analysis is carried out to validate the results. Further aim is to give a clarity on the fact that the use of this high lift device aids in improvising the aerodynamic characteristics of a wing by experimental testing of the wing design incorporated with flaperon, which is designed using a special methodology. Then, modification of wing design can be done to overcome the drawbacks of flaperons if any. INTRODUCTION - When looking at an aircraft, it is easy to observe that they have a number of common features: wings, a tail with vertical and horizontal wing sections, engines to propel them through the air, and a fuselage to carry passengers or cargo. If, however, you take a more critical look beyond the gross features, you also can see subtle, and sometimes not so subtle, differences. The reasons for these differences, why the designers configured them this way, is quite an intriguing study. Today, 100,000 flights will safely crisscross the planet. At no time in history have our lives been so global and full of possibility.