Chapter: 4. Approaches
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Call out Miutia in Pennsy Strike Pledges Continue To
VOL. U L, NO. 256. Philaddphia Strikere Picket Hosiery Mills PLEDGES CONTINUE CALL OUT MIUTIA n m F A T A L IN PENNSY STRIKE TO COME IN FROM TO H0]D DRIVER ALL OVER NATION Martial Law to Be Pro- ARREST THIRD MAN Yondi ffit by (^r Dmeu by daoM d ia Fayette Connty IN SYLLA MURDER RockriDe Wonian Tester- M EHCAN BEATEN Officials Busy Explaining ?A ere 15,000 Miners day Passes Away at Hos BY SrA M SB COPS Various Pbases ef die Have Defied Authorities. Stanley Kenefic Also Comes pital This Momiug. Program— Coal and Ante* from Stamford — Police Raymond Judd Stoutnar, 17, son Pl^debpbia Man (Sves Ifis mobiles Next to Be Taken lUrrlsburf, Pa., July 29—(AP)— of Mr. and Mrs. John Stoatnar of Governor Plnchot told early today Seek Fourth Suspect. 851 Tolland Turnpike died at 7:30 m Up— Monday Sled h r jna-tlal law will be proclaimed in Side of His Arrest this morning at the Manchester Me Fayette county, heart of the turbu strike there. morial hospital from injuries re dnstry WiD Disenss Code. lent coal strike area, with the ar New York, July 29.—(AP)— A Barcelona. ceived early yesterday afternoon rival of National Guard troops now third man from Stamford, Conn., enroute. when thrown from his bicycle when Three hundred state soldiers, was booked on a homicide charge to MAY REQUEST LOAN hit by an automobile driven by Mrs. New York, July 29—(AP) — The Washington, July 29.—(AP)— eoulpped with automatic rifles, day In the slaying of Dr. -
FAA) Privacy Impact Assessment Service Availability Prediction Tool (SAPT)
U.S. Department of Transportation Federal Aviation Administraiton (FAA) Privacy Impact Assessment Service Availability Prediction Tool (SAPT) Responsible Official David E. Gray Program Manager [email protected] Approving Official Claire W. Barrett Chief Privacy & Information Asset Officer Office of the Chief Information Officer [email protected] 0 U.S. Department of Transportation Executive Summary On May 28, 2010, the Federal Aviation Administration (FAA) published the Automatic Dependent Surveillance – Broadcast (ADS-B) final rule mandating that aircraft flying in certain controlled airspace be equipped with ADS-B Out capability not later than January 1, 2020.1 In turn, the FAA developed the Service Availability Prediction Tool (SAPT) to assist pilots, dispatchers, and commercial operators in checking their predicted navigation and surveillance availability before a flight as well as handle requests for Air Traffic Control (ATC) authorization pursuant to 14 CFR § 91.225(g). The SAPT has three main components: Receiver Autonomous Integrity Monitoring (RAIM) SAPT, Automatic Dependent Surveillance-Broadcast (ADS-B) SAPT, and ADS-B Deviation Authorization Pre-Flight Tool (ADAPT). This Privacy Impact Assessment (PIA) was developed pursuant to Section 208 of the E-Government Act of 2002 because the SAPT includes a web-based capability to collect and manage Personally Identifiable Information (PII) captured from aircraft operators to facilitate the automated handling of ATC authorization requests and FAA’s responses. What is a Privacy Impact Assessment? The Privacy Act of 1974 articulates concepts for how the federal government should treat individuals and their information and imposes duties upon federal agencies regarding the collection, use, dissemination, and maintenance of personally identifiable information (PII). -
Federal Communications Commission Before the Federal
Federal Communications Commission Before the Federal Communications Commission Washington, D.C. 20554 In the Matter of ) ) Existing Shareholders of Clear Channel ) BTCCT-20061212AVR Communications, Inc. ) BTCH-20061212CCF, et al. (Transferors) ) BTCH-20061212BYE, et al. and ) BTCH-20061212BZT, et al. Shareholders of Thomas H. Lee ) BTC-20061212BXW, et al. Equity Fund VI, L.P., ) BTCTVL-20061212CDD Bain Capital (CC) IX, L.P., ) BTCH-20061212AET, et al. and BT Triple Crown Capital ) BTC-20061212BNM, et al. Holdings III, Inc. ) BTCH-20061212CDE, et al. (Transferees) ) BTCCT-20061212CEI, et al. ) BTCCT-20061212CEO For Consent to Transfers of Control of ) BTCH-20061212AVS, et al. ) BTCCT-20061212BFW, et al. Ackerley Broadcasting – Fresno, LLC ) BTC-20061212CEP, et al. Ackerley Broadcasting Operations, LLC; ) BTCH-20061212CFF, et al. AMFM Broadcasting Licenses, LLC; ) BTCH-20070619AKF AMFM Radio Licenses, LLC; ) AMFM Texas Licenses Limited Partnership; ) Bel Meade Broadcasting Company, Inc. ) Capstar TX Limited Partnership; ) CC Licenses, LLC; CCB Texas Licenses, L.P.; ) Central NY News, Inc.; Citicasters Co.; ) Citicasters Licenses, L.P.; Clear Channel ) Broadcasting Licenses, Inc.; ) Jacor Broadcasting Corporation; and Jacor ) Broadcasting of Colorado, Inc. ) ) and ) ) Existing Shareholders of Clear Channel ) BAL-20070619ABU, et al. Communications, Inc. (Assignors) ) BALH-20070619AKA, et al. and ) BALH-20070619AEY, et al. Aloha Station Trust, LLC, as Trustee ) BAL-20070619AHH, et al. (Assignee) ) BALH-20070619ACB, et al. ) BALH-20070619AIT, et al. For Consent to Assignment of Licenses of ) BALH-20070627ACN ) BALH-20070627ACO, et al. Jacor Broadcasting Corporation; ) BAL-20070906ADP CC Licenses, LLC; AMFM Radio ) BALH-20070906ADQ Licenses, LLC; Citicasters Licenses, LP; ) Capstar TX Limited Partnership; and ) Clear Channel Broadcasting Licenses, Inc. ) Federal Communications Commission ERRATUM Released: January 30, 2008 By the Media Bureau: On January 24, 2008, the Commission released a Memorandum Opinion and Order(MO&O),FCC 08-3, in the above-captioned proceeding. -
E6bmanual2016.Pdf
® Electronic Flight Computer SPORTY’S E6B ELECTRONIC FLIGHT COMPUTER Sporty’s E6B Flight Computer is designed to perform 24 aviation functions and 20 standard conversions, and includes timer and clock functions. We hope that you enjoy your E6B Flight Computer. Its use has been made easy through direct path menu selection and calculation prompting. As you will soon learn, Sporty’s E6B is one of the most useful and versatile of all aviation computers. Copyright © 2016 by Sportsman’s Market, Inc. Version 13.16A page: 1 CONTENTS BEFORE USING YOUR E6B ...................................................... 3 DISPLAY SCREEN .................................................................... 4 PROMPTS AND LABELS ........................................................... 5 SPECIAL FUNCTION KEYS ....................................................... 7 FUNCTION MENU KEYS ........................................................... 8 ARITHMETIC FUNCTIONS ........................................................ 9 AVIATION FUNCTIONS ............................................................. 9 CONVERSIONS ....................................................................... 10 CLOCK FUNCTION .................................................................. 12 ADDING AND SUBTRACTING TIME ....................................... 13 TIMER FUNCTION ................................................................... 14 HEADING AND GROUND SPEED ........................................... 15 PRESSURE AND DENSITY ALTITUDE ................................... -
Aviation Definitions
Aviation Definitions: A Air Carrier - A commercial airline with published schedules operating at least five round trips per week. Airport Layout Plan (ALP) - The official, FAA approved map of an airport's facilities Air Route Traffic Control Center (ARTCC)- A facility providing air traffic control to aircraft on an IFR flight plan within controlled airspace and principally during the enroute phase of flight. Air Taxi - An aircraft certificated for commercial service available for hire on demand. Air Traffic Control (ATC)- The control of aircraft traffic, in the vicinity of airports from control towers, and in the airways between airports from control centers Air Traffic Control Tower (ATCT)- A central operations tower in the terminal air traffic control system with an associated IFR room if radar equipped, using air/ground communications and/or radar, visual signaling and other devices to provide safe, expeditious movement of air traffic. Altitude MSL - Aircraft altitude measured in feet above mean sea level. Approach Lighting System (ALS) - Radiating light beams guiding pilots to the extended centerline of the runway on final approach and landing. Approach Lights - High intensity lights located along the approach path at the end of an instrument runway. Approach lights aid the pilot in the transition from instrument flight conditions to visual conditions at the end of an instrument approach. Arrival - The act of landing at an airport. Arrival Procedure - A series of directions from air traffic control, using fixes and procedures, to guide an aircraft from the enroute environment to an airport for landing. Arrival Stream - A flow of aircraft following similar arrival procedures. -
Instrument Standard Operating Procedures
INSTRUMENT STANDARD OPERATING PROCEDURES INTRODUCTION PRE-FLIGHT ACTIONS BASIC INSTRUMENT MANEUVERS UNUSUAL ATTITUDE RECOVERY HOLDING PROCEDURES INSTRUMENT APPROACH PROCEDURES APPENDIX TABLE OF CONTENTS INTRODUCTION AND THEORY .......................................................................................................... 1 PRE-FLIGHT ACTIONS ........................................................................................................................ 3 IMC WEATHER ................................................................................................................................... 3 PRE-FLIGHT INSTRUMENT CHECKS ......................................................................................... 3 BASIC INSTRUMENT MANEUVERS ................................................................................................... 6 STRAIGHT AND LEVEL FLIGHT (SLF) ......................................................................................... 6 CHANGES OF AIRSPEEDS .......................................................................................................... 8 CONSTANT AIRSPEED CLIMBS AND DESCENTS ..................................................................... 9 CONSTANT RATE CLIMBS AND DESCENTS ............................................................................ 10 TIMED TURNS TO MAGNETIC COMPASS HEADINGS ............................................................ 12 MAGNETIC COMPASS TURNS ................................................................................................. -
RNAV Instrument Approach Procedures (IAP's) and the New Charting Format
Effective: Until Further Notice Area Navigation Systems Area Navigation (RNAV)/Wide Area Augmentation System (WAAS) Instrument Approach Procedures (IAP’s) and the New Charting Format. [REVISED 1/5/00] PURPOSE. Instrument procedures in the first half of the 21st century will be based on satellite navigation, also known as Global Navigation Satellite System (GNSS). Within the United States, the Global Positioning System (GPS), the Wide Area Augmentation system (WAAS), and the Local Area Augmentation System (LAAS) will comprise the primary components of the GNSS. Air navigation is increasingly dependent upon RNAV systems - as exemplified by Flight Management System (FMS) and Global Positioning System (GPS) avionics. These systems navigate with reference to geographic positions called “waypoints” (WP) specified in latitude/longitude rather than to/from a specific ground-based navigation aid. Reliance on RNAV systems for approach and departure operations will increase as new systems such as WAAS are developed and deployed. To foster and support full and optimal integration of RNAV into the National Airspace System (NAS), the FAA has developed a new procedure type for RNAV IAP’s. This Notice serves to inform the flying public of the new concepts being implemented with the RNAV IAP’s. OPERATIONS. In order to avoid unnecessary duplication and proliferation of instrument approach charts, Jeppesen will publish approach minimums for unaugmented GPS and WAAS (when operational) on the same chart. In addition, approach minimums will be established and published for LNAV/ VNAV - a new type of RNAV instrument approach with lateral and vertical navigation. The approach chart will be titled "RNAV RWY XX." The chart may contain as many as four columns of approach minimums: GLS; LNAV/VNAV; LNAV; and CIRCLING. -
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. -
Aviation Glossary
AVIATION GLOSSARY 100-hour inspection – A complete inspection of an aircraft operated for hire required after every 100 hours of operation. It is identical to an annual inspection but may be performed by any certified Airframe and Powerplant mechanic. Absolute altitude – The vertical distance of an aircraft above the terrain. AD - See Airworthiness Directive. ADC – See Air Data Computer. ADF - See Automatic Direction Finder. Adverse yaw - A flight condition in which the nose of an aircraft tends to turn away from the intended direction of turn. Aeronautical Information Manual (AIM) – A primary FAA publication whose purpose is to instruct airmen about operating in the National Airspace System of the U.S. A/FD – See Airport/Facility Directory. AHRS – See Attitude Heading Reference System. Ailerons – A primary flight control surface mounted on the trailing edge of an airplane wing, near the tip. AIM – See Aeronautical Information Manual. Air data computer (ADC) – The system that receives and processes pitot pressure, static pressure, and temperature to present precise information in the cockpit such as altitude, indicated airspeed, true airspeed, vertical speed, wind direction and velocity, and air temperature. Airfoil – Any surface designed to obtain a useful reaction, or lift, from air passing over it. Airmen’s Meteorological Information (AIRMET) - Issued to advise pilots of significant weather, but describes conditions with lower intensities than SIGMETs. AIRMET – See Airmen’s Meteorological Information. Airport/Facility Directory (A/FD) – An FAA publication containing information on all airports, seaplane bases and heliports open to the public as well as communications data, navigational facilities and some procedures and special notices. -
Module-7 Lecture-29 Flight Experiment
Module-7 Lecture-29 Flight Experiment: Instruments used in flight experiment, pre and post flight measurement of aircraft c.g. Module Agenda • Instruments used in flight experiments. • Pre and post flight measurement of center of gravity. • Experimental procedure for the following experiments. (a) Cruise Performance: Estimation of profile Drag coefficient (CDo ) and Os- walds efficiency (e) of an aircraft from experimental data obtained during steady and level flight. (b) Climb Performance: Estimation of Rate of Climb RC and Absolute and Service Ceiling from experimental data obtained during steady climb flight (c) Estimation of stick free and fixed neutral and maneuvering point using flight data. (d) Static lateral-directional stability tests. (e) Phugoid demonstration (f) Dutch roll demonstration 1 Instruments used for experiments1 1. Airspeed Indicator: The airspeed indicator shows the aircraft's speed (usually in knots ) relative to the surrounding air. It works by measuring the ram-air pressure in the aircraft's Pitot tube. The indicated airspeed must be corrected for air density (which varies with altitude, temperature and humidity) in order to obtain the true airspeed, and for wind conditions in order to obtain the speed over the ground. 2. Attitude Indicator: The attitude indicator (also known as an artificial horizon) shows the aircraft's relation to the horizon. From this the pilot can tell whether the wings are level and if the aircraft nose is pointing above or below the horizon. This is a primary instrument for instrument flight and is also useful in conditions of poor visibility. Pilots are trained to use other instruments in combination should this instrument or its power fail. -
Performance Improvement Methods for Terrain Database Integrity
PERFORMANCE IMPROVEMENT METHODS FOR TERRAIN DATABASE INTEGRITY MONITORS AND TERRAIN REFERENCED NAVIGATION A thesis presented to the Faculty of the Fritz J. and Dolores H. Russ College of Engineering and Technology of Ohio University In partial fulfillment of the requirements for the degree Master of Science Ananth Kalyan Vadlamani March 2004 This thesis entitled PERFORMANCE IMPROVEMENT METHODS FOR TERRAIN DATABASE INTEGRITY MONITORS AND TERRAIN REFERENCED NAVIGATION BY ANANTH KALYAN VADLAMANI has been approved for the School of Electrical Engineering and Computer Science and the Russ College of Engineering and Technology by Maarten Uijt de Haag Assistant Professor of Electrical Engineering and Computer Science R. Dennis Irwin Dean, Russ College of Engineering and Technology VADLAMANI, ANANTH K. M.S. March 2004. Electrical Engineering and Computer Science Performance Improvement Methods for Terrain Database Integrity Monitors and Terrain Referenced Navigation (115pp.) Director of Thesis: Maarten Uijt de Haag Terrain database integrity monitors and terrain-referenced navigation systems are based on performing a comparison between stored terrain elevations with data from airborne sensors like radar altimeters, inertial measurement units, GPS receivers etc. This thesis introduces the concept of a spatial terrain database integrity monitor and discusses methods to improve its performance. Furthermore, this thesis discusses an improvement of the terrain-referenced aircraft position estimation for aircraft navigation using only the information from downward-looking sensors and terrain databases, and not the information from the inertial measurement unit. Vertical and horizontal failures of the terrain database are characterized. Time and frequency domain techniques such as the Kalman filter, the autocorrelation function and spectral estimation are designed to evaluate the performance of the proposed integrity monitor and position estimator performance using flight test data from Eagle/Vail, CO, Juneau, AK, Asheville, NC and Albany, OH. -
N87- 19393 CE Bith Ab AUTCEETIC TESMINAL EM (BASA) 21 P CSCL 17Ti Unclas H1/06 43501 NASA Tech Ni Ca I Paper 2669
) A SIPSCLATICL EVALUATION GP A N87- 19393 CE bITH Ab AUTCEETIC TESMINAL EM (BASA) 21 p CSCL 17ti Unclas H1/06 43501 NASA Tech ni ca I Paper 2669 1987 A Simulation Evaluation of a Pilot Interface With an Automatic Terminal Approach System David A. Hinton Langley Research Center Hampt o n, Virginia National Aeronautics and Space Administration Scientific and Technical Information Branch Summary with a high potential for mistakes and has limited time to detect and correct any errors. A successful A piloted-simulation study was performed to arrival depends on the correct interpretation of ap- evaluate the pilot interface with an automatic termi- proach chart details, the correct setting of numerous nal approach system (ATAS). The ATAS was con- cockpit controls, and precise aircraft guidance near ceived as a concept for improving the pilot inter- the ground. face with high levels of automation. It consists of Automation in the form of an autopilot has been instrument approach data storage, automatic radio used to reduce pilot work load and improve pilot tuning, autopilot, autothrottle, and annunciation of performance in the terminal area. Research studies These components allow the ATAS flight status. (ref. 2) and airplane accident and incident reports to automatically execute instrument approaches, in- suggest, however, that the probability of pilot error cluding procedure turns, altitude changes, missed actually increases with an increase in automation, approaches, and holding patterns, without requir- partially because of design limitations of the pilot- ing the pilot to set up navigation radios or change machine interface. Conventional autopilot interfaces autopilot modes. provide the pilot with many opportunities to make The results show that fewer pilot blunders were errors because of the requirements to change radio made during approaches when using the ATAS than frequencies and autopilot modes as the approach when using a baseline, heading-select autopilot.