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2017-SR20-Domestic-Pricelist.Pdf
2017 $389,900 Base weight 2120 lbs | Useful Load 1030 lbs Cabin payload with 3 hr. trip fuel and 45 min. reserve 776 lbs. SR20 STANDARD FEATURES AIRFRAME & POWERPLANT AVIONICS Lycoming IO-390-C3B6 215 HP Engine Cirrus Perspective+™ by Garmin® Cockpit Cirrus Airframe Parachute System® (CAPS®) 10” Screens 3-Blade Propeller GMA 350c All-Digital Bluetooth® Audio Panel Airbag Seatbelts (Front Seats) QWERTY Keyboard Controller Single Movement Power Lever Dual WAAS GPS/Comm/Nav Radios Dual Side Yoke Engine & Fuel Monitoring 60/40 Flex Seating™ Seats up to 5 Garmin Pilot – 1 year subscription included Four USB Power Ports Dual Alternators Advanced Wheel Fairings 406 MHz ELT High Performance Brakes ADS-B In Weather & Traffic Tubeless Tires ADS-B Out Transponder Surface Illumination Lights FliteCharts® & SafeTaxi® *US only. Subscription required. Spectra™ Wingtip Lighting GFC 700 Autopilot including Standard Leather Interior Electronic Stability & Protection (ESP) Tinted Windows Dual ADAHRS 2 Year Spinner-to-Tail Warranty Hypoxia Check/Automated Descent Mode Blue Level Button Autopilot Stall Protection TRAINING 3 Day Transition Training Package SR20 PACKAGES CIRRUS SELECT $39,900 Cirrus Select adds the Enhanced Vision System (EVS) displayed on big 12” screens and eTAWS2. EVS creates an image of what is outside the aircraft by using infrared technology to turn night into day. eTAWS is a TAWS-B terrain warning system with greater predictive precision information based on your flight path, and if terrain is ahead, gives you early warning aural alerts. Weight Δ: 5 lbs. ALERTS, AWARENESS & ASSISTANCE $28,900 Fly with increased precision and awareness with Synthetic Vision Technology (SVT™). -
MSP 2019 Annual Noise Contour Report Metropolitan Airports Commission
Minneapolis St. Paul International Airport (MSP) 2019 Annual Noise Contour Report Comparison of the 2019 Actual and the 2007 Forecast Noise Contours February 2020 MAC Community Relations Office and HNTB Corporation MSP 2019 Annual Noise Contour Report Metropolitan Airports Commission Table of Contents ES EXECUTIVE SUMMARY .................................................................................................. 1 ES.1 BACKGROUND ...................................................................................................................... 1 ES.2 AIRPORT NOISE LITIGATION AND CONSENT DECREE .............................................................. 1 ES.3 MSP 2020 IMPROVEMENTS EA/EAW ..................................................................................... 2 ES.4 THE AMENDED CONSENT DECREE ......................................................................................... 2 ES.5 2019 NOISE CONTOURS ......................................................................................................... 3 ES.6 AMENDED CONSENT DECREE PROGRAM ELIGIBILITY ............................................................. 3 ES.7 AMENDED CONSENT DECREE PROGRAM MITIGATION STATUS ............................................. 5 1. INTRODUCTION AND BACKGROUND ................................................................................. 9 1.1 CORRECTIVE LAND USE EFFORTS TO ADDRESS AIRCRAFT NOISE ............................................ 9 1.2 2007 FORECAST CONTOUR ................................................................................................. -
Using an Autothrottle to Compare Techniques for Saving Fuel on A
Iowa State University Capstones, Theses and Graduate Theses and Dissertations Dissertations 2010 Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft Rebecca Marie Johnson Iowa State University Follow this and additional works at: https://lib.dr.iastate.edu/etd Part of the Electrical and Computer Engineering Commons Recommended Citation Johnson, Rebecca Marie, "Using an autothrottle ot compare techniques for saving fuel on a regional jet aircraft" (2010). Graduate Theses and Dissertations. 11358. https://lib.dr.iastate.edu/etd/11358 This Thesis is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Graduate Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. Using an autothrottle to compare techniques for saving fuel on A regional jet aircraft by Rebecca Marie Johnson A thesis submitted to the graduate faculty in partial fulfillment of the requirements for the degree of MASTER OF SCIENCE Major: Electrical Engineering Program of Study Committee: Umesh Vaidya, Major Professor Qingze Zou Baskar Ganapathayasubramanian Iowa State University Ames, Iowa 2010 Copyright c Rebecca Marie Johnson, 2010. All rights reserved. ii DEDICATION I gratefully acknowledge everyone who contributed to the successful completion of this research. Bill Piche, my supervisor at Rockwell Collins, was supportive from day one, as were many of my colleagues. I also appreciate the efforts of my thesis committee, Drs. Umesh Vaidya, Qingze Zou, and Baskar Ganapathayasubramanian. I would also like to thank Dr. -
Warbirds Over Wanaka the Pearse Project Cirrus Adventure: the Long Way to Brisbane
KiwiFlyer TM Magazine of the New Zealand Aviation Community Issue 45 2016 #2 $ 6.90 inc GST ISSN 1170-8018 Warbirds Over Wanaka The Pearse Project Cirrus Adventure: The long way to Brisbane Products, Services, News, Events, Warbirds, Recreation, Training and more. KiwiFlyer Issue 45 2016 #2 From the Editor In this issue Welcome to KiwiFlyer #45. We hope you’ll find 7. The Pearse Project plenty of good reading within. Ivan Mudrovich has spent more than a decade creating a faithful interpretation of Richard There’s more than a few owners of GA and Pearse’s 1903 aircraft. Chris Gee attended the recreational aircraft who will have thought at some attempts to get it airborne. time “I could fly to Australia”. And then added “if I wanted to” and then left it at that. Satisfying 10. Cirrus Adventure: The long way to Brisbane to think that you could, but in reality all a bit too Lance Weller wanted to relocate his Cirrus from risky and difficult, and for that matter, hardly cost NZ to Brisbane and chose a route through efficient. Albeit that Lance Weller had the additional Noumea and PNG. He tells the adventure here. motive of relocating his Cirrus to Brisbane, Lance is indeed someone who headed off on an international 16. EAA AirVenture Oshkosh with Gaye Pardy flight(s) ‘because he could’. Far from taking the This years Gaye Pardy Travel tour to Oshkosh traditional route via Norfolk and Lord Howe Islands, will be their 30th. All aviation enthusiasts should Lance and co-pilot Garth Jensen made the journey go at least once. -
Boeing 737 Postmaintenance Test Flight Encounters Uncommanded Roll-And-Yaw Oscillations
FLIGHT SAFETY FOUNDATION Accident Prevention Vol. 55 No. 5 For Everyone Concerned with the Safety of Flight May 1998 Boeing 737 Postmaintenance Test Flight Encounters Uncommanded Roll-and-yaw Oscillations Fluid leaking from the cabin onto the yaw-damper coupler in the electronic-and-equipment bay affected electronic signals transmitted to the yaw-damper actuator and caused a dutch-roll oscillation. FSF Editorial Staff On Oct. 22, 1995, a Boeing 737-236 Advanced was • “Sufficiently conductive contaminant paths in straight-and-level flight at Flight Level (FL) 200 between certain adjacent pins had affected the (20,000 feet), at an indicated airspeed of 290 knots phase and magnitude of the signals transmitted when roll-and-yaw oscillations began. The flight crew to the yaw-damper actuator, thereby stimulating disengaged the autopilot, autothrottles and yaw a forced dutch-roll mode of the aircraft; damper, but the uncommanded roll-and-yaw oscillations continued. • “The location of the E&E bay — beneath the cabin floor in the area of the aircraft doors, galleys The crew declared an emergency and descended to and toilets — made it vulnerable to fluid ingress 7,000 feet. The oscillations stopped when airspeed was from a variety of sources; [and,] reduced to about 250 knots. After a satisfactory check of the aircraft’s low-speed handling characteristics, the • “The crew actions immediately following the crew returned to London (England) Gatwick Airport onset of the dutch-roll oscillations did not result and landed without further incident. in the disengagement of the malfunctioning yaw- damper system.” The U.K. Air Accidents Investigation Branch (AAIB), in its final report on the incident, identified four causal factors: The B-737, operated by British Airways, was built in 1980 and had accumulated 37,871 hours in service. -
Cirrus SR20/SR22/SR22T Integrated Avionics System Cockpit Reference Guide
Cirrus SR20/SR22/SR22T Integrated Avionics System Cockpit Reference Guide FLIGHT INSTRUMENTS EIS NAV/COM/TRANSPONDER/AUDIO PANEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES ABNORMAL OPERATION ANNUNCIATIONS & ALERTS APPENDIX INDEX Copyright © 2008-2010 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0764.08 or later for the Cirrus SR20, SR22, and SR22T. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138 Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. Tel: 44/0870.8501241 Fax: 44/0870.8501251 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099 For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836. Web Site Address: www.garmin.com Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. -
2019 Domestic SR22 20181115.Indd
2019 $629,900 Base weight 2269 lbs. | Useful Load 1331 lbs. Cabin payload with 3 hr. trip fuel and 45 min. reserve 966 lbs. SR22 STANDARD FEATURES AIRFRAME & POWERPLANT AVIONICS Continental IO-550-N 310 HP Engine Cirrus Perspective+™ by Garmin® Cockpit Cirrus Airframe Parachute System® (CAPS®) Synthetic Vision Technology (SVT™) Airbag Seatbelts (Front Seats) 10” Screens Dual Side Yoke GMA 350c All-Digital Bluetooth® Audio Panel 3-Blade Propeller QWERTY Keyboard Controller Four USB Power Ports Dual WAAS GPS/Comm/Nav Radios High Performance Brakes Engine & Fuel Monitoring Advanced Wheel Fairings Garmin Pilot1 – 1 year subscription included Tubeless Tires ADS-B Out Transponder Remote Keyless Entry ADS-B In Weather & Traffic Surface Illumination Lights 406 MHz ELT Interior/Exterior Ambient Convenience Lighting FliteCharts® & SafeTaxi® *US only. Subscription required. Spectra™ Wingtip Lighting Digital 4-in-1 Standby Instrument Single Movement Power Lever SiriusXM Weather & Audio2 60/40 Flex Seating™ Seats up to 5 Garmin Flight Stream 5101 Standard Leather Interior GFC 700 Autopilot including UV Protected Windows Electronic Stability & Protection (ESP) 3 Year / 1000 Hour Spinner-to-Tail Warranty Dual ADAHRS Hypoxia Check/Automated Descent Mode TRAINING Blue Level Button Autopilot Stall Protection 3 Day Transition Training Package SR22 PACKAGES CIRRUS EXECUTIVE $31,900 Bring must-have jet features to your Cirrus SR Series aircraft. Yaw Damper provides cruising comfort for pilot and passengers, reduces pilot workload and enables true three-axis autopilot functionality. The Enhanced Vision System (EVS) leverages infrared imaging technology to display what the human eye cannot see. Gain peace of mind in night and low-visibility conditions knowing cloud tops & build-ups, surrounding terrain, runway obstacles, taxiways and surface markings are clearly visible on the MFD. -
New FBO Manager Named at Juneau
Fall 2008 Newsletter of the Watertown, Madison, & Dodge County FBOs Fall 2011 Volume 28, No. 4 New FBO Manager A View Named at Juneau from Our Wisconsin Aviation has named Mary Gasper as FBO manager of Wisconsin President Aviation’s Juneau facility at the Dodge County Airport, one of the finest, state-of- the-art airports in Wisconsin. Mary, a native of Milwaukee, has worked for Wisconsin Aviation as a customer service representative since 2002, when she moved to Juneau. In her Winning new role as FBO manager, she will oversee fueling operations, buildings and Charlie Sheen has certainly added a new dimension to the facilities, customer service, flight school activities, and tenant relations. word winning. There was a time when it had but one meaning, “Mary displays an exemplary performance in customer service,” Wisconsin and now you hear it tossed around like a bean bag. Here in Aviation President Jeff Baum said. “She repeatedly goes above and beyond Wisconsin, we’re defining winning in terms of our beloved our customers’ expectations and has always demonstrated friendliness and Packers, Badgers, and Brewers having quite a year. Our hats professionalism to our aviation enthusiasts as well as to her fellow employees. off to them! She brings energy, experience, and a customer-first attitude.” Personally, we each have our own criteria for winning. It Mary is also a private pilot, obtaining her license in July of 2002, two may be as simple as getting through the day or as complicated days before starting her employment with Wisconsin Aviation. In March as getting a new degree, a new job, or the affection of someone 2008 she obtained her instrument rating and has aspirations for acquiring a special. -
Cirrus-Perspective-Touch-Brochure Low-Res.Pdf
1 2 3 THE POWER OF TOUCH To touch...is to sense the world around you, to gather information. Now use touch to effortlessly access and control information. This is more than just modern avionics - this is Cirrus Perspective Touch™ by Garmin®. For nearly a decade, Cirrus Perspective® by Garmin® has been the industry standard in technically-advanced, general aviation avionics. Cirrus Perspective Touch follows suit as an innovative, user-friendly aircraft interface. More integrated and capable than traditional off-the-shelf products, Perspective Touch is designed around the pilot experience, providing a seamless connection to the airframe and environment. 4 5 FLIGHT DECK SUPERIORITY The Vision Jet® defines the Personal Jet category. Rightfully so, it has the most advanced flight deck in the world. The Vision Jet is outfitted with high resolution flight displays and is designed with three landscape touchscreen controllers to truly optimize turbine aircraft operations. The controllers present a familiar, intuitive interface, providing pilots quick access to detailed flight and systems information across a bright, panoramic display. The three-touchscreen layout allows for advanced interaction with aircraft systems, enhanced real-time weather, integrated weight and balance, radio tuning, cabin communication and much more. Additionally, with a single command, each touchscreen is interchangeable with the ability to function as either a PFD, MFD or NAV/COM controller. No other flight deck offers this level of integration and capability, delivered in such a clean and ergonomic cockpit layout. 6 7 UNRIVALED INTEGRATION Aircraft systems and subsystems come to life on the Perspective Touch flight displays as digital diagrams, tailored specifically to the design of your Vision Jet. -
11ADOBL04 December 2010
11ADOBL04 December 2010 Use of rudder on Airbus A300-600/A310 (extracted from former FCOM Bulletin N°15/1 – Subject N°40) Reason for issue On February 8th, 2002, the National Transportation Safety Board (NTSB), in cooperation with the French Bureau d'Enquêtes et d'Analyses (BEA), issued recommendations that aircraft manufacturers re-emphasize the structural certification requirements for the rudder and vertical stabilizer, showing how some maneuvers can result in exceeding design lim- its and even lead to structural failure. The purpose of this Bulletin is to re-emphasize proper operational use of the rudder, highlight certification requirements and rud- der control design characteristics. Yaw control General In flight, yaw control is provided by the rudder, and directional stability is provided by the vertical stabilizer. The rudder and vertical stabilizer are sized to meet the two following objectives: Provide sufficient lateral control of the aircraft during crosswind takeoffs and landings, within the published crosswind limits (refer to FCOM Operating Limitations chapter). Provide positive aircraft control under conditions of engine failure and maximum asymmetric thrust, at any speed above Vmcg (minimum control speed - on ground). The vertical stabilizer and the rudder must be capable of generating sufficient yawing moments to maintain directional control of the aircraft. The rudder deflection, necessary to achieve these yawing moments, and the resulting sideslip angles place significant aerodynamic loads on the rudder and on the vertical stabilizer. Both are designed to sustain loads as prescribed in the JAR/FAR 25 certification requirements which define several lateral loading conditions (maneuver, gust loads and asymmetric loads due to engine failure) leading to the required level of structural strength. -
Social Responsibility Report 2017
STAY TRUE TO ORIGINAL INTENTIONS, AND KEEP THE MISSION IN MIND – Building an Air Power in the New Era Modern enterprises are the cells of a society, while society is the matrix within which enterprises grow. Therefore, while developing, an enterprise should act as a good “corporate citizen”, be grateful for favors received, and repay society, which is the social responsibility of an enterprise, and also an important factor in building a harmonious society. The majority of enterprises need to maintain self-discipline and self-respect, establish a scientific operation philosophy, rationalize internal and external relations, and strive to become responsible “corporate citizens” to guide the enterprise to develop and grow stronger and put it on the track of harmony and health. —— Quotations from President Xi CONTENTS 04 About Us 06 Address from the Chairman PROMOTE RESPONSIBLE MANAGEMENT 10 The Concept and Model of Responsibility 11 Corporate Governance Optimization 12 Communication Methods of Stakeholders 16 Practice of Responsible Management Serving the Country • Aviation 22 Serving the Country through Industry 26 Making the Armed Forces Powerful and Serving the Country Responsibility • Aviation [•••] Managing Enterprises According to Law, Legislating Responsibility [•••] Green Aviation, Environmental Responsibility [•••] Health Quality, Safety Responsibility Innovation • Aviation 48 Independent Efforts, Technological Innovation 50 Deepening Reform, Management Innovation Finesse • Aviation 56 Aviation Glory, Employee Finesse 62 Help Those in Need and Distress, Finesse in Public Welfare 68 Global Citizen, Finesse Overseas About Us Aviation Industry Corporation of China,Ltd (hereinafter referred to as “Aviation Industry”) is a large state-owned enterprise managed by the central government as well as a state authorized investment institution, and was established through restructuring integration of the original AVIC I and AVIC II on November 6, 2008. -
B737-800 FTD System Failures
IOS B737 FTD System Failures 0 Welcome The information contained within this document is believed to be accurate at the time of publication. However, it is subject to change without notice and does not represent a commitment on the part of Multi Pilot Simulations (MPS). Multi Pilot Simulations assumes no responsibility or liability for any errors or inaccuracies that may appear in this document. Boeing, Boeing 737 and Boeing 737NG are registered trademarks of Boeing Company. Airbus, Airbus A320 are registered trademarks of Airbus. All other trademarks mentioned herein are the property of their respective owners. All rights reserved. No rights or claims can be derived from data in this document. WELCOME-1 FSTD: B737 FTD 1 Index Applicability: - Failures marked with a @-sign in the failure title are available on FNPT II/MCC and FTD1/FTD2 FSTDs - Failures without a @-sign are available on FTD1/FTD2 FSTDs only 0 WELCOME .................................................................................................................................. 1 CONTACT INFORMATION ................................................................................................................................ 1 DOCUMENT OWNER ....................................................................................................................................... 1 REVISION HISTORY ......................................................................................................................................... 1 1 INDEX ...................................................................................................................................