FAA Order JO 7110.65U, Air Traffic Control
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Garmin Reveals Autoland Feature Rotorcraft Industry Slams Possible by Matt Thurber NYC Helo Ban Page 45
PUBLICATIONS Vol.50 | No.12 $9.00 DECEMBER 2019 | ainonline.com Flying Short-field landings in the Falcon 8X page 24 Regulations UK Labour calls for bizjet ban page 14 Industry Forecast sees deliveries rise in 2020 page 36 Gratitude for Service Honor flight brings vets to D.C. page 41 Air Transport Lion Air report cites multiple failures page 51 Rotorcraft Garmin reveals Autoland feature Industry slams possible by Matt Thurber NYC helo ban page 45 For the past eight years, Garmin has secretly Mode. The Autoland system is designed to Autoland and how it works, I visited been working on a fascinating new capabil- safely fly an airplane from cruising altitude Garmin’s Olathe, Kansas, headquarters for ity, an autoland function that can rescue an to a suitable runway, then land the airplane, a briefing and demo flight in the M600 with airplane with an incapacitated pilot or save apply brakes, and stop the engine. Autoland flight test pilot and engineer Eric Sargent. a pilot when weather conditions present can even switch on anti-/deicing systems if The project began in 2011 with a Garmin no other safe option. Autoland should soon necessary. engineer testing some algorithms that could receive its first FAA approval, with certifi- Autoland is available for aircraft manu- make an autolanding possible, and in 2014 cation expected shortly in the Piper M600, facturers to incorporate in their airplanes Garmin accomplished a first autolanding in followed by the Cirrus Vision Jet. equipped with Garmin G3000 avionics and a Columbia 400 piston single. In September The Garmin Autoland system is part of autothrottle. -
Aircraft of Today. Aerospace Education I
DOCUMENT RESUME ED 068 287 SE 014 551 AUTHOR Sayler, D. S. TITLE Aircraft of Today. Aerospace EducationI. INSTITUTION Air Univ.,, Maxwell AFB, Ala. JuniorReserve Office Training Corps. SPONS AGENCY Department of Defense, Washington, D.C. PUB DATE 71 NOTE 179p. EDRS PRICE MF-$0.65 HC-$6.58 DESCRIPTORS *Aerospace Education; *Aerospace Technology; Instruction; National Defense; *PhysicalSciences; *Resource Materials; Supplementary Textbooks; *Textbooks ABSTRACT This textbook gives a brief idea aboutthe modern aircraft used in defense and forcommercial purposes. Aerospace technology in its present form has developedalong certain basic principles of aerodynamic forces. Differentparts in an airplane have different functions to balance theaircraft in air, provide a thrust, and control the general mechanisms.Profusely illustrated descriptions provide a picture of whatkinds of aircraft are used for cargo, passenger travel, bombing, and supersonicflights. Propulsion principles and descriptions of differentkinds of engines are quite helpful. At the end of each chapter,new terminology is listed. The book is not available on the market andis to be used only in the Air Force ROTC program. (PS) SC AEROSPACE EDUCATION I U S DEPARTMENT OF HEALTH. EDUCATION & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS BEEN REPRO OUCH) EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIG INATING IT POINTS OF VIEW OR OPIN 'IONS STATED 00 NOT NECESSARILY REPRESENT OFFICIAL OFFICE OF EOU CATION POSITION OR POLICY AIR FORCE JUNIOR ROTC MR,UNIVERS17/14AXWELL MR FORCEBASE, ALABAMA Aerospace Education I Aircraft of Today D. S. Sayler Academic Publications Division 3825th Support Group (Academic) AIR FORCE JUNIOR ROTC AIR UNIVERSITY MAXWELL AIR FORCE BASE, ALABAMA 2 1971 Thispublication has been reviewed and approvedby competent personnel of the preparing command in accordance with current directiveson doctrine, policy, essentiality, propriety, and quality. -
Aircraft Control After Engine Failure on Takeoff
General AviaƟon FAA Joint Steering CommiƩee Aviaon Safety Training Aid January 2016 Aircraft Control After Engine Failure on Takeoff Studies have shown that startle responses during unexpected situaons such as power‐plant failure during takeoff or inial climb have contributed to loss of control of aircra. By including an appropriate plan of acon in a departure briefing for a power‐plant failure during takeoff or inial climb, you can manage your startle response and maintain aircra control. Considerations for Takeoff Brief Best Practices The briefing given by the pilot‐in‐command As part of pre‐planning and preparaon, (PIC) should be specific for each flight. Avoid consider these in case of a power‐plant failure allowing the checklist to become roune and create during and aer take‐off. Addional training and complacency. pracce — in a safe environment with a flight instructor — can reduce the startle response to an Airport Info: Consider runway condions, traffic acvies, and airspace complexies. unexpected event, such as an actual power‐plant failure, and improve outcomes. Idenfy V Speeds: Airspeeds such as Vy, Vx, Vr and best glide should be considered for current Straight Ahead or Turn Back? Research condions prior to takeoff. indicates a higher probability of survival if you connue straight ahead following an engine Terrain/Obstrucons: Mountains, power‐lines, failure aer take‐off. Turning back actually trees or towers may become obstrucons requires a turn of greater than 180 degrees aer during emergencies; idenfy them prior to taking into account the turning radius. Making a departure. turn at low altudes and airspeeds could create Abort Point: Establish an abort point prior to a scenario for a stall/spin accident. -
Barnett, James Scott OH128
Wisconsin Veterans Museum Research Center Transcript of an Oral History Interview with JAMES S. BARNETT Navy, Airplane navigator and co-pilot, World War II 2000 OH 128 1 OH 128 Barnett, James Scott, (1918-). Oral History Interview, 2000. User Copy: 1 sound cassette (ca. 65 min.); analog, 1 7/8 ips, mono. Master Copy: 1 sound cassette (ca. 65 min.); analog, 1 7/8 ips, mono. Video Recording: 1 videorecording (ca. 65 min.); ½ inch, color. Transcript: 0.1 linear ft. (1 folder). Abstract: James Barnett, a Kenosha, Wisconsin native, discusses his World War II service as an aerial navigator and co-pilot with the Navy. Barnett mentions enlisting in 1942, attending preflight training in Iowa, and learning about navigation and gunnery at the Naval Air Station (Florida). He relates his duties as a crewmember of a PBY squadron in Hawaii. Barnett talks about bombing missions to the Gilbert Islands, Wake Island, and Ellice Island. He recalls how he and two other crew members were grounded with dysentery the day that their plane and the rest of the crew were shot down and killed. Barnett mentions his transfer to New Guinea and missions to the Philippines and Truk. He talks about getting hit in the leg during a bombing run and doing an emergency landing on Kwajalein due to engine damage. Barnett speaks of his return to the United States and being stationed at Kaneohe Bay (Hawaii). He describes losing a plane due to landing gear malfunction. He talks about flying from San Francisco to Hawaii in nine hours and judging whether to turn around using “how-goes-it” curves. -
(VL for Attrid
ECCAIRS Aviation 1.3.0.12 Data Definition Standard English Attribute Values ECCAIRS Aviation 1.3.0.12 VL for AttrID: 391 - Event Phases Powered Fixed-wing aircraft. (Powered Fixed-wing aircraft) 10000 This section covers flight phases specifically adopted for the operation of a powered fixed-wing aircraft. Standing. (Standing) 10100 The phase of flight prior to pushback or taxi, or after arrival, at the gate, ramp, or parking area, while the aircraft is stationary. Standing : Engine(s) Not Operating. (Standing : Engine(s) Not Operating) 10101 The phase of flight, while the aircraft is standing and during which no aircraft engine is running. Standing : Engine(s) Start-up. (Standing : Engine(s) Start-up) 10102 The phase of flight, while the aircraft is parked during which the first engine is started. Standing : Engine(s) Run-up. (Standing : Engine(s) Run-up) 990899 The phase of flight after start-up, during which power is applied to engines, for a pre-flight engine performance test. Standing : Engine(s) Operating. (Standing : Engine(s) Operating) 10103 The phase of flight following engine start-up, or after post-flight arrival at the destination. Standing : Engine(s) Shut Down. (Standing : Engine(s) Shut Down) 10104 Engine shutdown is from the start of the shutdown sequence until the engine(s) cease rotation. Standing : Other. (Standing : Other) 10198 An event involving any standing phase of flight other than one of the above. Taxi. (Taxi) 10200 The phase of flight in which movement of an aircraft on the surface of an aerodrome under its own power occurs, excluding take- off and landing. -
Table of Contents Next Page
, SERVICE PUBLICATION OF OCKHEED-GEORGIA COMPANY / DIVISION OF OCKHEED CORPORATION Editor: Don H. Hungate Associate Editors: Charles I. Gale, James A. Loftin, Arch McCleskey, Patricia Thomas Art Direction and Production: Anne G. Anderson This summer marks the 25th anniversary of the first flight of the Lockheed Hercules; a Volume 6, No. 3, July - September 1979 quarter century of service to nations throughout the world! Over 1,550 Hercules (C-130s Vol. 6, No. 3, July. September 1979 and L-100) have been delivered to 44 countries. We at Lockheed are very proud of this Contents: record and the reputation the Hercules has earned. It is a reputation built on depend- ability, versatility, and durability. 2 Focal Point The Hercules is a true workhorse. Many developing countries depend on it to carry all types of cargo, from lifesaving food to road-building equipment. They carry these cargoes to remote areas that are not easily accessible by any other mode of transporta- 3 tion. An additional advantage is its ability to land and take off in incredibly short 3 Crew Door Rigging distances, even on unpaved clearings. The tasks the Hercules is capable of accomplishing are almost limitless; from hunting hurricanes, to flying mercy relief missions. It is the universal airborne platform. And it is 14 Royal Norwegian Air Force energy-efficient, using only about half the fuel a comparable jet aircraft would require. 15 One of the more interesting aspects of these 25 years is that while the external design of 15 Hydraulic Pressure Drop the aircraft has changed very little, constant improvements in systems and avionics equip- ment have made the world’s outstanding cargo airplane also among the world’s most modern. -
China-US Aircraft Collision Incident of April 2001
Order Code RL30946 CRS Report for Congress Received through the CRS Web China-U.S. Aircraft Collision Incident of April 2001: Assessments and Policy Implications Updated October 10, 2001 Shirley A. Kan (Coordinator), Richard Best, Christopher Bolkcom, Robert Chapman, Richard Cronin, Kerry Dumbaugh, Stuart Goldman, Mark Manyin, Wayne Morrison, Ronald O’Rourke Foreign Affairs, Defense, and Trade Division David Ackerman American Law Division Congressional Research Service The Library of Congress China-U.S. Aircraft Collision Incident of April 2001: Assessments and Policy Implications Summary The serious incident of April 2001 between the United States and the People’s Republic of China (PRC) involved a collision over the South China Sea between a U.S. Navy EP-3 reconnaissance plane and a People’s Liberation Army (PLA) naval F-8 fighter that crashed. After surviving the near-fatal accident, the U.S. crew made an emergency landing of their damaged plane onto the PLA’s Lingshui airfield on Hainan Island, and the PRC detained the 24 crew members for 11 days. Washington and Beijing disagreed over the cause of the accident, the release of the crew and plane, whether Washington would “apologize,” and the PRC’s right to inspect the EP- 3. In the longer term, the incident has implications for the right of U.S. and other nations’ aircraft to fly in international airspace near China. (This CRS Report, first issued on April 20, 2001, includes an update on the later EP-3 recovery.) The incident prompted assessments about PRC leaders, their hardline position, and their claims. While some speculated about PLA dominance, President and Central Military Commission Chairman Jiang Zemin and his diplomats were in the lead, while PLA leaders followed in stance with no more inflammatory rhetoric. -
Emergency Evacuation of Commercial Passenger Aeroplanes Second Edition 2020
JUNE 2020 EMERGENCY EVACUATION OF COMMERCIAL PASSENGER AEROPLANES SECOND EDITION 2020 @aerosociety A specialist paper from the Royal Aeronautical Society www.aerosociety.com About the Royal Aeronautical Society (RAeS) The Royal Aeronautical Society (‘the Society’) is the world’s only professional body and learned society dedicated to the entire aerospace community. Established in 1866 to further the art, science and engineering of aeronautics, the Society has been at the forefront of developments in aerospace ever since. The Society seeks to; (i) promote the highest possible standards in aerospace disciplines; (ii) provide specialist information and act as a central forum for the exchange of ideas; and (iii) play a leading role in influencing opinion on aerospace matters. The Society has a range of specialist interest groups covering all aspects of the aerospace world, from airworthiness and maintenance, unmanned aircraft systems and aerodynamics to avionics and systems, general aviation and air traffic management, to name a few. These groups consider developments in their fields and are instrumental in providing industry-leading expert opinion and evidence from their respective fields. About the Honourable Company of Air Pilots (Incorporating Air Navigators) Who we are The Company was established as a Guild in 1929 in order to ensure that pilots and navigators of the (then) fledgling aviation industry were accepted and regarded as professionals. From the beginning, the Guild was modelled on the lines of the Livery Companies of the City of London, which were originally established to protect the interests and standards of those involved in their respective trades or professions. In 1956, the Guild was formally recognised as a Livery Company. -
Suborbital Reusable Launch Vehicles and Applicable Markets
SUBORBITAL REUSABLE LAUNCH VEHICLES AND APPLICABLE MARKETS Prepared by J. C. MARTIN and G. W. LAW Space Launch Support Division Space Launch Operations October 2002 Space Systems Group THE AEROSPACE CORPORATION El Segundo, CA 90245-4691 Prepared for U. S. DEPARTMENT OF COMMERCE OFFICE OF SPACE COMMERCIALIZATION Herbert C. Hoover Building 14th and Constitution Ave., NW Washington, DC 20230 (202) 482-6125, 482-5913 Contract No. SB1359-01-Z-0020 PUBLIC RELEASE IS AUTHORIZED Preface This report has been prepared by The Aerospace Corporation for the Department of Commerce, Office of Space Commercialization, under contract #SB1359-01-Z-0020. The objective of this report is to characterize suborbital reusable launch vehicle (RLV) concepts currently in development, and define the military, civil, and commercial missions and markets that could capitalize on their capabilities. The structure of the report includes a brief background on orbital vs. suborbital trajectories, as well as an overview of expendable and reusable launch vehicles. Current and emerging market opportunities for suborbital RLVs are identified and discussed. Finally, the report presents the technical aspects and program characteristics of selected U.S. and international suborbital RLVs in development. The appendix at the end of this report provides further detail on each of the suborbital vehicles, as well as the management biographies for each of the companies. The integration of suborbital RLVs with existing airports and/or spaceports, though an important factor that needs to be evaluated, was not the focus of this effort. However, it should be noted that the RLV concepts discussed in this report are being designed to minimize unique facility requirements. -
ASES Standardization Manual
ASES Standardization Manual Rainier Flight Service LLC, located at Renton Municipal Airport and is owned and operated as: Rainier Flight Service 800 W Perimeter Rd Renton, WA 98057 © 2013 Rainier Flight Service (v 2.0) Page 1 ASES Standardization Manual 1. Takeoffs And Landings ....................................................................................................... 3 1.1 MANEUVER: Normal Takeoff and Climb.................................................................................. 4 1.2 MANEUVER: Normal Approach and Landing ........................................................................... 5 1.3 MANEUVER: Crosswind Takeoff and Climb ............................................................................. 7 1.4 MANEUVER: Crosswind Approach and Landing ....................................................................... 9 1.5 MANEUVER: Glassy Water Takeoff and Climb ....................................................................... 11 1.6 MANEUVER: Glassy Water Approach and Landing ................................................................. 12 1.7 MANEUVER: Rough Water Takeoff and Climb ....................................................................... 14 1.8 MANEUVER: Rough Water Approach and Landing................................................................. 15 1.9 MANEUVER: Confined Area Takeoff and Climb (Straight and Turning) ................................... 17 1.10 MANEUVER: Confined Area Approach and Landing .............................................................. -
AOE 3104 Problem Sheet 10 (Ans) Our Class Business Jet Has the Following Characteristics
AOE 3104 Problem Sheet 10 (ans) Our class business jet has the following characteristics: Gross Weight = 10,000 lbs b = 40 ft CLmax = 1.8 (normal flight) 2 2 S = 200 ft CD = 0.02 + 0.05 (CL) CLmax = 2.4 (with flaps) 2 engines with 1000 lb / engine (up and away drag polar) During ground roll, the wing is 5 ft above the ground The coefficient of friction on the paved runway is : = 0.02 : The coefficient during braking is b = 0.3 51. Calculate the takeoff ground roll distance assuming no flaps are used for takeoff and that minimum takeoff distance conditions are used during the ground roll. Must calculate the conditions on the ground: However, units must be SI units so: and Then and The ground effect on the induced drag parameter K. Then the correction factor N is given by and Therefore This is the ground drag polar! For minimum distance takeoff, the proper ground lift coefficient is given by: The corresponding drag coefficient is determined from the ground drag polar” We can now calculate the constants in the takeoff equations: We need to calculate the reference speeds: Finally the takeoff distance can be calculated from: 52. Calculate the landing ground roll distance for this aircraft assuming a full flap landing and that zero lift occurs during the ground roll, and that brakes are applied at touch-down (short field landing in which you retract the flaps and hit the brakes as soon as possible after touch-down). Here we will assume that we land with flaps so we need to calculate new reference airspeeds: Ground run, no flaps. -
WEC Aircraft Use and Safety Handbook
AIRCRAFT USE AND SAFETY HANDBOOK FOR SCIENTISTS AND RESOURCE MANAGERS John C. Simon Peter C. Frederick Kenneth D. Meyer H. Percival Franklin DEVELOPED BY THE © University of Florida 2010 ABOUT THE AUTHORS John Charles Simon is a Research Coordinator for the University of Florida’s South Florida Wading Bird Project. He earned his private pilot’s certificate in 1986 and has flown over 750 hours as a passenger/observer in both fixed- winged and rotary aircraft conducting population and nesting surveys, habitat evaluations, following flights, and radio telemetry. Dr. Peter Frederick is a Research Professor in the University of Florida’s Department of Wildlife Ecology and Conservation. His research on wading birds in the Florida Everglades has used aerial survey techniques extensively and intensively, with over 1,500 hours flown in fixed-winged and rotary aircraft over 25 years. He survived one air crash in a Cessna 172 during the course of that work. Dr. Kenneth D. Meyer is Director of the Avian Research and Conservation Institute and an Associate Professor (Courtesy) in the University of Florida's Department of Wildlife Ecology and Conservation. Since 1981, Dr. Meyer's research on birds has involved fixed-wing and rotary aircraft for radio telemetry, population surveys, roost counts, nest finding, and following flights. Dr. H. Percival Franklin is Courtesy Associate Professor and Unit Leader of the Florida Cooperative Fish and Wildlife Research Unit. Its employees and cooperators, regardless of employment, are bound by strict aircraft training and use regulations of the Department of Interior. Dr Franklin has been a strong proponent of aircraft and other safety issues in the workplace.