Recreational Aviation Risk Survey
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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. -
Taurus Manual ENG 250Special.Indd
Flight manual and Maintenance manual applies to Taurus 503 equipped with Rotax 503 engine REV. 0 (21 June, 2006) This is the original manual of Pipistrel d.o.o. Ajdovščina Should third-party translations to other languages contain any discreptancies, Pipistrel d.o.o. Ajdovščina denies all responsibility. WARNING! This booklet MUST be present inside the cockpit at all times! Should you be selling the aircraft make sure this manual is handed over to the new owner. 2 TAURUS motorglider www.pipistrel.si REV. 0 Taurus model: Factory serial number: Date of manufacture: Aircraft empty weight (kg): Available crew weight (no front ballast): Available crew weight (9 kg front ballast): Available luggage weight: List of equipment included in aircraft empty weight: Date and place of issue: Ajdovščina, www.pipistrel.si TAURUS motorglider 3 REV. 0 Pipistrel d.o.o. Ajdovščina, Goriška cesta 50a, SI-5270 Ajdovščina, Slovenija tel: +386 (0)5 3663 873, fax: +386 (0)5 3661 263, e-mail: [email protected] www.pipistrel.si Flight manual and Maintenance manual for Taurus motorglider Model: Taurus 503 (Rotax 503) Slovenian Data Sheet number: TC 02/001 - AT/ULN 04 Factory serial number: Registration number: Date of Issue: June, 2006 Pages signed under “Approval” in section Index of revisions and List of valid pages (pages 4 and 5 of this manual) are approved by: Authority: Signature: Stamp: Original date of Approval: This aircraft is to be operated in compliance with information and limitations contained herein. The original English Language edition of this manual has been approved as operating instruction according to “Pravilnik o ultralahkih letalnih napravah” of Republic of Slovenia. -
Aviation Annual Report
2018 Aviation Annual Report Aviation Aircraft Use Summary U.S. Forest Service 2018 Table of Contents Executive Summary ....................................................................................................................................... 1 Table 1 – 2018 Forest Service Total Aircraft Available ..................................................................... 2 Introduction: The Forest Service Aviation Program...................................................................................... 3 Aviation Utilization and Cost Information .................................................................................................... 4 2018 At-A-Glance ...................................................................................................................................... 4 Aviation Use .......................................................................................................................................... 4 Table 2 and Figure 1 – Aircraft Total Use CY 2014-2018................................................................... 4 Figure 2 – CY 2018 Flight Hours by Month........................................................................................ 5 Table 3 and Figure 3 – Percent of CY 2018 Flight Time by Aircraft Type .......................................... 5 Table 4 – CY 2018 Aircraft Use by Region/Agency ............................................................................ 6 Aviation Cost ........................................................................................................................................ -
Efficient Light Aircraft Design – Options from Gliding
Efficient Light Aircraft Design – Options from Gliding Howard Torode Member of General Aviation Group and Chairman BGA Technical Committee Presentation Aims • Recognise the convergence of interest between ultra-lights and sailplanes • Draw on experiences of sailplane designers in pursuit of higher aerodynamic performance. • Review several feature of current sailplanes that might be of wider use. • Review the future for the recreational aeroplane. Lift occurs in localised areas A glider needs efficiency and manoeuvrability Drag contributions for a glider Drag at low speed dominated by Induced drag (due to lift) Drag at high ASW-27 speeds Glider (total) drag polar dominated by profile drag & skin friction So what are the configuration parameters? - Low profile drag: Wing section design is key - Low skin friction: maximise laminar areas - Low induced drag – higher efficiencies demand greater spans, span efficiency and Aspect Ratio - Low parasitic drag – reduce excrescences such as: undercarriage, discontinuities of line and no leaks/gaps. - Low trim drag – small tails with efficient surface coupled with low stability for frequent speed changing. - Wide load carrying capacity in terms of pilot weight and water ballast Progress in aerodynamic efficiency 1933 - 2010 1957: Phoenix (16m) 1971: Nimbus 2 (20.3m) 2003: Eta (30.8m) 2010: Concordia (28m) 1937: Wiehe (18m) Wooden gliders Metal gliders Composite gliders In praise of Aspect Ratio • Basic drag equation in in non-dimensional, coefficient terms: • For an aircraft of a given scale, aspect ratio is the single overall configuration parameter that has direct leverage on performance. Induced drag - the primary contribution to drag at low speed, is inversely proportional to aspect ratio • An efficient wing is a key driver in optimising favourable design trades in other aspects of performance such as wing loading and cruise performance. -
Preventive Maintenance
Maintenance Aspects of Owning Your Own Aircraft Introduction According to 14 CFR Part 43, Maintenance, Preventive Maintenance, Rebuilding, and Alteration, the holder of a pilot certificate issued under 14 CFR Part 61 may perform specified preventive maintenance on any aircraft owned or operated by that pilot, as long as the aircraft is not used under 14 CFR Part 121, 127, 129, or 135. This pamphlet provides information on authorized preventive maintenance. How To Begin Here are several important points to understand before you attempt to perform your own preventive maintenance: First, you need to understand that authorized preventive maintenance cannot involve complex assembly operations. Second, you should carefully review 14 CFR Part 43, Appendix A, Subpart C (Preventive Maintenance), which provides a list of the authorized preventive maintenance work that an owner pilot may perform. Third, you should conduct a self-analysis as to whether you have the ability to perform the work satisfactorily and safely. Fourth, if you do any of the preventive maintenance authorized in 14 CFR Part 43, you will need to make an entry in the appropriate logbook or record system in order to document the work done. The entry must include the following information: • A description of the work performed, or references to data that are acceptable to the Administrator. • The date of completion. • The signature, certificate number, and kind of certificate held by the person performing the work. Note that the signature constitutes approval for return to service only for work performed. Examples of Preventive Maintenance Items The following is a partial list of what a certificated pilot who meets the conditions in 14 CFR Part 43 can do: • Remove, install, and repair landing gear tires. -
NASA Styrofoam Tray Glider.Pdf
RIGHT FLIGHT Objectives The students will: Construct a flying model glider. Determine weight and balance of a glider. Standards and Skills Science Science as Inquiry Physical Science Science and Technology Unifying Concepts and Processes Science Process Skills Observing Measuring Collecting Data Inferring Predicting Making Models Controlling Variables Mathematics Problem Solving Reasoning Prediction Measurement Background On December 17, 1903, two brothers, Wilbur and Orville Wright, became the first humans to fly a controllable, powered airplane. To unravel the mysteries of flight, the Wright brothers built and experimented extensively with model gliders. Gliders are airplanes without motors or a power source. 52 Aeronautics: An Educator’s Guide EG-2002-06-105-HQ Building and flying model gliders helped the Wright brothers learn and understand the importance of weight and balance in air- planes. If the weight of the airplane is not positioned properly, the airplane will not fly. For example, too much weight in the front (nose) will cause the airplane to dive toward the ground. The precise balance of a model glider can be determined by varying the location of small weights. Wilbur and Orville also learned that the design of an airplane was very important. Experimenting with models of different designs showed that airplanes fly best when the wings, fuselage, and tail are designed and balanced to interact with each other. The Wright Flyer was the first airplane to complete a controlled takeoff and landing. To manage flight direction, airplanes use control surfaces. Elevators are control surfaces that make the nose of the airplane pitch up and down. A rudder is used to move the nose left and right. -
Evolving Green Aviation Transport System: a Hoilistic Approah to Sustainable Green Market Development
American Journal of Climate Change, 2012, 1, 164-180 http://dx.doi.org/10.4236/ajcc.2012.13014 Published Online September 2012 (http://www.SciRP.org/journal/ajcc) Evolving Green Aviation Transport System: A Hoilistic Approah to Sustainable Green Market Development A. N. Sarkar International Business & Research, Asia-Pacific Institute of Management, New Delhi, India Email: [email protected] Received June 24, 2012; revised July 25, 2012; accepted August 10, 2012 ABSTRACT Aviation is one of the fastest growing industries as well as transportation modes in the world. Global aviation contrib- utes about 2% of global greenhouse gas emissions and supports 8% of the world economic activity in terms of GDP. With the phenomenal growth in air trafficking by the national and international airliners the total carbon space available for flying is getting progressively diminished and the consequential emission levels are also becoming alarming over passage of time. The paper describes the concept of evolution of Green Transport system with focus on manufacturing of green aircraft and sustainable green marketing involving green supply chain. This entails introduction of New and innovative technologies, including aircraft designing, improving operational efficiency, air traffic control & monitoring etc; combined with emission mitigation efforts towards sustainable growth of the industry, can make enormous im- provements in emission control and reduction in a planned and system-based manner. These integrated approaches are proposed to be used to harmonize the systems and processes that can essentially constitute the suggested framework of the Green Aviation Transport system. The paper, inter alia, discusses various conceptual, strategic, technological and economic and environmental dimensions of the Green Aviation transport system with focus on creating new Green Marketing opportunities for the aviation industry in future. -
Aviation Acronyms
Aviation Acronyms 5010 AIRPORT MASTER RECORD (FAA FORM 5010-1) 7460-1 NOTICE OF PROPOSED CONSTRUCTION OR ALTERATION 7480-1 NOTICE OF LANDING AREA PROPOSAL 99'S NINETY-NINES (WOMEN PILOTS' ASSOCIATION) A/C AIRCRAFT A/DACG ARRIVAL/DEPARTURE AIRFIELD CONTROL GROUP A/FD AIRPORT/FACILITY DIRECTORY A/G AIR - TO - GROUND A/G AIR/GROUND AAA AUTOMATED AIRLIFT ANALYSIS AAAE AMERICAN ASSOCIATION OF AIRPORT EXECUTIVES AAC MIKE MONRONEY AERONAUTICAL CENTER AAI ARRIVAL AIRCRAFT INTERVAL AAIA AIRPORT AND AIRWAY IMPROVEMENT ACT AALPS AUTOMATED AIR LOAD PLANNING SYSTEM AANI AIR AMBULANCE NETWORK AAPA ASSOCIATION OF ASIA-PACIFIC AIRLINES AAR AIRPORT ACCEPTANCE RATE AAS ADVANCED AUTOMATION SYSTEM AASHTO AMERICAN ASSOCIATION OF STATE HIGHWAY & TRANSPORTATION OFFICIALS AC AIRCRAFT COMMANDER AC AIRFRAME CHANGE AC AIRCRAFT AC AIR CONTROLLER AC ADVISORY CIRCULAR AC ASPHALT CONCRETE ACAA AIR CARRIER ACCESS ACT ACAA AIR CARRIER ASSOCIATION OF AMERICA ACAIS AIR CARRIER ACTIVITY INFORMATION SYSTEM ACC AREA CONTROL CENTER ACC AIRPORT CONSULTANTS COUNCIL ACC AIRCRAFT COMMANDER ACC AIR CENTER COMMANDER ACCC AREA CONTROL COMPUTER COMPLEX ACDA APPROACH CONTROL DESCENT AREA ACDO AIR CARRIER DISTRICT OFFICE ACE AVIATION CAREER EDUCATION ACE CENTRAL REGION OF FAA ACF AREA CONTROL FACILITY ACFT AIRCRAFT ACI-NA AIRPORTS COUNCIL INTERNATIONAL - NORTH AMERICA ACID AIRCRAFT IDENTIFICATION ACIP AIRPORT CAPITAL IMPROVEMENT PLANNING ACLS AUTOMATIC CARRIER LANDING SYSTEM ACLT ACTUAL CALCULATED LANDING TIME Page 2 ACMI AIRCRAFT, CREW, MAINTENANCE AND INSURANCE (cargo) ACOE U.S. ARMY -
Training Guide for Weight-Shift Ultralights
TTrraaiinniinngg GGuuiiddee ffoorr WWeeiigghhtt--SShhiifftt UUllttrraalliigghhttss Safety Information for Instructors and Students EAA Weight-Shift Ultralight Training Guide Version 1.3 ______________________________________________________________________________ Introduction Ultralight aviation in the United States is the most unencumbered opportunity for solo flight in the world. Tremendous freedoms are given to ultralight pilots. However, at the same time there are strict limitations that must be followed. With this freedom, however, come responsibilities to ensure the safety of other individuals in the airspace as well as on the ground. In 1982 the FAA issued Federal Aviation Regulation Part 103, Ultralight Vehicles. With this regulation, the FAA chose to identify ultralights as vehicles and not aircraft. Because they are vehicles and not aircraft, this regulation allows individuals to operate ultralight vehicles without requiring FAA pilot or vehicle certification. Upon publishing Part 103 the FAA said it did not wish to issue pilot certificates for ultralight operators. Instead, the FAA said individuals who want to fly ultralights should participate in industry-established self-regulation and training programs. Since 1983 EAA has maintained programs to support Part 103 and has held an exemption to Part 103 that allowed the operation of 2-place ultralight training vehicles by authorized ultralight flight instructors. In 2004, the FAA passed the sport pilot & light-sport aircraft regulations. One specific purpose of this new rule was to transition 2-place ultralight training vehicles to experimental light-sport aircraft. As a result, after the training exemption expires on 1/31/08 there will no longer be a way to fly a 2-place ultralight to train ultralight pilots. -
White Eng 17 1.Cdr
WHITE PAPER I’M AERO White paper - I’M AERO First and the only ultralight coaxial helicopter This document is not a securities oering or a scheme of collective investment, nor does it require the registration or approval of the Monetary Authority of Singapore. The participants are advised to carefully read this document and be cautious when investing funds. 1. Introduction 2. Company’s products and their description 2.1. Ultralight aviation and coaxial system in helicopter industry 2.2. Manufacturing facilities of I’M AERO 2.3. Application range of the helicopters of I’M AERO 2.4. Review of the models and technical peculiarities of the I’M AERO helicopters 2.4.1. Ultralight airplane Nestling 21 2.4.2. Ultralight coaxial helicopter Helicopter R-34 2.4.3. Unmanned aerial vehicle Aerobot A-34 2.5. Geography of product application 3. Implementation of the blockchain 4. I’M AERO meets market needs 5. Business model 6. Marketing research 7. Roadmap of the Project 8. Project team 9. Structure of the Token Sale 10. Jurisdiction 11. Contacts * The current version of White Paper is not final and can be adjusted. The final parameters will be presented a few days before the Token Sale starts. Introducon The aim of the I AM AERO Project is to create a series production of ultralight aircraft that meet the needs of the population at the level of everyday use, as well as to meet the challenges of private business and the demands of government agencies. I’M AERO is a specialized aviation enterprise engaged in the design, development and production of manned and unmanned aerial vehicles. -
Perpetual Flight in Flow Fields
Perpetual Flight in Flow Fields by Ricardo Ayres Gomes Bencatel A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy (Electrical and Computer Engineering) in the University of Porto, School of Engineering Faculdade de Engenharia da Universidade do Porto 2011 Doctoral Committee: Professor Fernando Lobo Pereira, Chair Professor Anouck Girard Associate Lu´ısaBastos Doctor Jos´eMorgado c Ricardo Ayres Gomes Bencatel 2012 All Rights Reserved To my family and my girlfriend, who supported my endeavors and endured the necessary absences. v ACKNOWLEDGEMENTS I thank with all my heart my family and my girlfriend for the support in the easy and the hard times, and for the encouragement to always do my best and surpass myself. Furthermore, I would like to thank the friendship of Nuno Costa with whom I developed and tested several model aircraft, which contributed to the knowledge required for this work. I would like to thank the support from AsasF group and the researchers from the Un- derwater Systems and Technology Laboratory, specially Jo~aoSousa and Gil Gon¸c´alves, and Pedro Almeida for their support, and in particular Jo~aoCorreia, Joel Gomes, Eduardo Oliveira, Rui Caldeira, Filipe Ferreira, Bruno Terra, Filipe Costa Ferreira, Joel Cardoso, and S´ergioFerreira for their friendship, support, and assistance. I gratefully acknowledge the support of the Portuguese Air Force Academy, specially Cap. El´oiPereira, Lt. Tiago Oliveira, Cap. Jos´eCosta, Sgt. Joaquim Gomes, Sgt. Paulo Teixeira, Lt. Gon¸caloCruz, Lt. Col. Morgado, Maj. Madruga, Lt. Jo~aoCaetano, and Sgt. Fernandes. I'm most grateful for the time I spend at the Aerospace Department from the University of Michigan. -
Space & Electronic Warfare Lexicon
1 Space & Electronic Warfare Lexicon Terms 2 Space & Electronic Warfare Lexicon Terms # - A 3 PLUS 3 - A National Missile Defense System using satellites and ground-based radars deployed close to the regions from which threats are likely. The space-based system would detect the exhaust plume from the burning rocket motor of an attacking missile. Forward-based radars and infrared-detecting satellites would resolve smaller objects to try to distinguish warheads from clutter and decoys. Based on that data, the ground-based interceptor - a hit-to-kill weapon - would fly toward an approximate intercept point, receiving course corrections along the way from the battle management system based on more up-to-date tracking data. As the interceptor neared the target its own sensors would guide it to the impact point. See also BALLISTIC MISSILE DEFENSE (BMD.) 3D-iD - A Local Positioning System (LPS) that is capable of determining the 3-D location of items (and persons) within a 3-dimensional indoor, or otherwise bounded, space. The system consists of inexpensive physical devices, called "tags" associated with people or assets to be tracked, and an infrastructure for tracking the location of each tag. NOTE: Related technology applications include EAS, EHAM, GPS, IRID, and RFID. 4GL - See FOURTH GENERATION LANGUAGE 5GL - See FIFTH GENERATION LANGUAGE A-POLE - The distance between a missile-firing platform and its target at the instant the missile becomes autonomous. Contrast with F-POLE. ABSORPTION - (RF propagation) The irreversible conversion of the energy of an electromagnetic WAVE into another form of energy as a result of its interaction with matter.