Twins in an Ever-Changing Business Aviation World, Turboprops
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Cessna Denali Has Been Realigned to Beechcraft Turboprop Family
50SKYSHADESImage not found or type unknown- aviation news CESSNA DENALI HAS BEEN REALIGNED TO BEECHCRAFT TURBOPROP FAMILY News / Business aviation, Manufacturer Image not found or type unknown © 2015-2021 50SKYSHADES.COM — Reproduction, copying, or redistribution for commercial purposes is prohibited. 1 Textron Aviation is realigning its turboprop aircraft lineup as the single-engine Beechcraft Denali (previously branded the Cessna Denali) joins the legendary twin-engine Beechcraft King Air 260 and King Air 360/360ER as part of the company’s high-performance turboprop product lineup. The aircraft development program continues to progress toward a first flight anticipated later this year. “The Beechcraft Denali represents our continued strategy to invest in clean-sheet and current products in both our Beechcraft and Cessna iconic brands. Beechcraft turboprops are renowned for their versatility and reliability, and the single-engine Denali is a perfect complement to this legendary family of products,” said Ron Draper, Textron Aviation, president and CEO. “Pilots and passengers will appreciate the aircraft for its enhanced capabilities, innovative technology and all-around passenger comfort.” The Beechcraft Denali is designed to outperform its competition with projected lower operating costs, Garmin G3000 avionics, and the largest cabin in its class. Engineered to achieve cruise speeds of 285 knots with a full fuel payload of 1,100 pounds, the Denali will have a range of 1,600 nautical miles at high speed cruise with one pilot and four passengers. “We continue to receive interest around the world from turboprop and piston owners of competing aircraft, who are looking to move into an aircraft with greater performance and enhanced passenger experience,” said Lannie O’Bannion, senior vice president, Global Sales and Flight Operations. -
FAA Advisory Circular AC 91-74B
U.S. Department Advisory of Transportation Federal Aviation Administration Circular Subject: Pilot Guide: Flight in Icing Conditions Date:10/8/15 AC No: 91-74B Initiated by: AFS-800 Change: This advisory circular (AC) contains updated and additional information for the pilots of airplanes under Title 14 of the Code of Federal Regulations (14 CFR) parts 91, 121, 125, and 135. The purpose of this AC is to provide pilots with a convenient reference guide on the principal factors related to flight in icing conditions and the location of additional information in related publications. As a result of these updates and consolidating of information, AC 91-74A, Pilot Guide: Flight in Icing Conditions, dated December 31, 2007, and AC 91-51A, Effect of Icing on Aircraft Control and Airplane Deice and Anti-Ice Systems, dated July 19, 1996, are cancelled. This AC does not authorize deviations from established company procedures or regulatory requirements. John Barbagallo Deputy Director, Flight Standards Service 10/8/15 AC 91-74B CONTENTS Paragraph Page CHAPTER 1. INTRODUCTION 1-1. Purpose ..............................................................................................................................1 1-2. Cancellation ......................................................................................................................1 1-3. Definitions.........................................................................................................................1 1-4. Discussion .........................................................................................................................6 -
Top Turboprop Series: We Compare Popular Pre-Owned Models
FOR THE PILOTS OF OWNER-FLOWN, CABIN-CLASS AIRCRAFT SEPTEMBER 2019 $3.95 US VOLUME 23 NUMBER 9 Top Turboprop Series: We Compare Popular Pre-Owned Models Five Questions The Latest on One Pilot’s with Corporate the Cessna Denali Introduction Angel Network & SkyCourier to Aerobatics Jet It US One year $15.00, two years $29.00 Canadian One year $24.00, two years $46.00 Overseas One Year $52.00, Two Years $99.00 Single copies $6.50 PRIVATE. FAST. SMART. EDITOR Rebecca Groom Jacobs SEPTEMBER2019 • VOL. 23, NO. 9 (316) 641-9463 Contents [email protected] EDITORIAL OFFICE 2779 Aero Park Drive 4 Traverse City, MI 49686 Editor’s Briefing Phone: (316) 641-9463 E-mail: [email protected] 2 A Career Shaped by Turboprops PUBLISHER by Rebecca Groom Jacobs Dave Moore PRESIDENT Position Report Dave Moore 4 What Makes a Turboprop CFO Safer? Answer: You Rebecca Mead PRODUCTION MANAGER by Dianne White Mike Revard PUBLICATIONS DIRECTOR Jake Smith GRAPHIC DESIGNER Marci Moon 6 TWIN & TURBINE WEBSITE 6 Top Turboprop Series: www.twinandturbine.com Pre-Owned Piper Meridian ADVERTISING DIRECTOR and Daher TBM 700C2 John Shoemaker Twin & Turbine by Joe Casey 2779 Aero Park Drive Traverse City, MI 49686 12 Five on the Fly with Phone: 1-800-773-7798 Corporate Angel Network Fax: (231) 946-9588 [email protected] by Rebecca Groom Jacobs ADVERTISING ADMINISTRATIVE COORDINATOR & REPRINT SALES 14 The Latest on the Betsy Beaudoin Cessna Denali and Phone: 1-800-773-7798 [email protected] SkyCourier ADVERTISING ADMINISTRATIVE by Rich Pickett ASSISTANT Jet It Erika Shenk 22 Intro to Aerobatics Phone: 1-800-773-7798 by Jared Jacobs [email protected] SUBSCRIBER SERVICES Rhonda Kelly Diane Smith Jamie Wilson Molly Costilow 22 Kelly Adamson P.O. -
PROPULSION SYSTEM/FLIGHT CONTROL INTEGRATION for SUPERSONIC AIRCRAFT Paul J
PROPULSION SYSTEM/FLIGHT CONTROL INTEGRATION FOR SUPERSONIC AIRCRAFT Paul J. Reukauf and Frank W. Burcham , Jr. NASA Dryden Flight Research Center SUMMARY The NASA Dryden Flight Research Center is engaged in several programs to study digital integrated control systems. Such systems allow minimization of undesirable interactions while maximizing performance at all flight conditions. One such program is the YF-12 cooperative control program. In this program, the existing analog air-data computer, autothrottle, autopilot, and inlet control systems are to be converted to digital systems by using a general purpose airborne computer and interface unit. First, the existing control laws are to be programed and tested in flight. Then, integrated control laws, derived using accurate mathematical models of the airplane and propulsion system in conjunction with modern control techniques, are to be tested in flight. Analysis indicates that an integrated autothrottle-autopilot gives good flight path control and that observers can be used to replace failed sensors. INTRODUCTION Supersonic airplanes, such as the XB-70, YF-12, F-111, and F-15 airplanes, exhibit strong interactions between the engine and the inlet or between the propul- sion system and the airframe (refs. 1 and 2) . Taking advantage of possible favor- able interactions and eliminating or minimizing unfavorable interactions is a chal- lenging control problem with the potential for significant improvements in fuel consumption, range, and performance. In the past, engine, inlet, and flight control systems were usually developed separately, with a minimum of integration. It has often been possible to optimize the controls for a single design point, but off-design control performance usually suffered. -
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. -
Boeing Submission for Asiana Airlines (AAR) 777-200ER HL7742 Landing Accident at San Francisco – 6 July 2013
Michelle E. Bernson The Boeing Company Chief Engineer P.O. Box 3707 MC 07-32 Air Safety Investigation Seattle, WA 98124-2207 Commercial Airplanes 17 March 2014 66-ZB-H200-ASI-18750 Mr. Bill English Investigator In Charge National Transportation Safety Board 490 L’Enfant Plaza, SW Washington DC 20594 via e-mail: [email protected] Subject: Boeing Submission for Asiana Airlines (AAR) 777-200ER HL7742 Landing Accident at San Francisco – 6 July 2013 Reference: NTSB Tech Review Meeting on 13 February 2014 Dear Mr. English: As requested during the reference technical review, please find the attached Boeing submission on the subject accident. Per your request we are sending this electronic version to your attention for distribution within the NTSB. We would like to thank the NTSB for giving us the opportunity to make this submission. If you have any questions, please don’t hesitate to contact us. Best regardsregards,, Michelle E. E Bernson Chief Engineer Air Safety Investigation Enclosure: Boeing Submission to the NTSB for the subject accident Submission to the National Transportation Safety Board for the Asiana 777-200ER – HL7742 Landing Accident at San Francisco 6 July 2013 The Boeing Company 17 March 2014 INTRODUCTION On 6 July 2013, at approximately 11:28 a.m. Pacific Standard Time, a Boeing 777-200ER airplane, registration HL7742, operating as Asiana Airlines Flight 214 on a flight from Seoul, South Korea, impacted the seawall just short of Runway 28L at San Francisco International Airport. Visual meteorological conditions prevailed at the time of the accident with clear visibility and sunny skies. -
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. -
2017 Fact Book Textron Inc
2017 FACT BOOK TEXTRON INC. is a $14.2 billion multi-industry company with approximately 37,000 employees. The Company leverages its global network of aircraft, defense, industrial, and finance businesses to provide customers with innovative products and services. Textron is known around the world for its powerful brands such as Bell, Cessna, Beechcraft, Hawker, Jacobsen, Kautex, Lycoming, E-Z-GO, Greenlee, Textron Off Road, Arctic Cat, Textron Systems, and TRU Simulation + Training. Textron Revenue by Segment FINANCIAL HIGHLIGHTS Dollars in millions, except per share data 2017 2016 Change TEXTRON AVIATION 33% Revenues $14,198 $13,788 3% INDUSTRIAL 30% International revenues % 38% 38% BELL 23% Segment profit1 $ 1,169 $ 1,309 (11)% TEXTRON AVIATIONSYSTEMS 33%13% INDUSTRIALFINANCE 1% 30% Income from continuing operations—GAAP $ 306 $ 843 (64)% BELL 23% Adjusted income from continuing TEXTRON AVIATIONSYSTEMS 33%13% operations—Non-GAAP2 $ 658 $ 715 (8)% FINANCEINDUSTRIAL 1% 30% Manufacturing group debt3 $ 3,088 $ 2,777 11% BELL 23% TEXTRON SYSTEMS 13% Shareholders’ equity $ 5,647 $ 5,574 1% Textron Revenue by Type 3 FINANCE 1% Manufacturing group debt-to-capital (net of cash) 26% 23% COMMERCIAL 70% U.S. GOVERNMENT 22% OTHER MILITARY 7% Common Share Data COMMERCIALFINANCE 1% 70% Diluted EPS from continuing operations—GAAP $ 1.14 $ 3.09 (63)% U.S. GOVERNMENT 22% Adjusted diluted EPS from continuing OTHER MILITARY 7% operations—Non-GAAP2 $ 2.45 $ 2.62 (6)% FINANCECOMMERCIAL 1% 70% Dividends per share $ 0.08 $ 0.08 — U.S. GOVERNMENT 22% OTHER MILITARY 7% Diluted average shares outstanding (in thousands) 268,750 272,365 (1)% U.S. -
Access Aerospace Industry Competitiveness, 2012
W. Frank Barton School of Business Center for Economic Development and Business Research Aerospace Industry Competitiveness, 2012 For The Governor’s Council of Economic Advisors 1845 Fairmount St. Wichita KS 67260-0121 316-978-3225 www.CEDBR.org [email protected] Contents Introduction .................................................................................................................................................. 6 Industry Definition ........................................................................................................................................ 7 336411 Aircraft Manufacturing ............................................................................................................ 7 336412 Aircraft Engine and Engine Parts Manufacturing ..................................................................... 7 336413 Other Aircraft Parts and Auxiliary Equipment Manufacturing ................................................ 7 336414 Guided Missile and Space Vehicle Manufacturing ................................................................... 7 336415 Guided Missile and Space Vehicle Propulsion Unit and Propulsion Unit Parts Manufacturing .............................................................................................................................................................. 7 336419 Other Guided Missile and Space Vehicle Parts and Auxiliary Equipment Manufacturing ....... 8 Community Economic Indicators ................................................................................................................. -
Vpa Report 2002-12-05
UNCLASSIFIED NAVAL AIR WARFARE CENTER AIRCRAFT DIVISION PATUXENT RIVER, MARYLAND TECHNICAL REPORT REPORT NO: NAWCADPAX/TR-2002/71 REVIEW OF THE CARRIER APPROACH CRITERIA FOR CARRIER-BASED AIRCRAFT PHASE I; FINAL REPORT by Thomas Rudowsky Stephen Cook Marshall Hynes Robert Heffley Melvin Luter Thomas Lawrence CAPT Robert Niewoehner Douglas Bollman Page Senn Dr. Wayne Durham Henry Beaufrere Michael Yokell Albert Sonntag Approved for public release; distribution is unlimited. UNCLASSIFIED DEPARTMENT OF THE NAVY NAVAL AIR WARFARE CENTER AIRCRAFT DIVISION PATUXENT RIVER, MARYLAND NAWCADPAX/TR-2002/71 REVIEW OF THE CARRIER APPROACH CRITERIA FOR CARRIER-BASED AIRCRAFT - PHASE I; FINAL REPORT by Thomas Rudowsky Stephen Cook Marshall Hynes Robert Heffley Melvin Luter Thomas Lawrence CAPT Robert Niewoehner Douglas Bollman Page Senn Dr. Wayne Durham Henry Beaufrere Michael Yokell Albert Sonntag NAWCADPAX/TR-2002/71 REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing this collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. -
Flight Deck Solutions, Technologies and Services Moving the Industry Forward Garmin Innovation Brings Full Integration to Business Flight Operations and Support
FLIGHT DECK SOLUTIONS, TECHNOLOGIES AND SERVICES MOVING THE INDUSTRY FORWARD GARMIN INNOVATION BRINGS FULL INTEGRATION TO BUSINESS FLIGHT OPERATIONS AND SUPPORT From web-based flight planning, fleet scheduling and tracking services to integrated flight display technology, head-up displays, advanced RNP navigation, onboard weather radar, Data Comm datalinks and much more — Garmin offers an unrivaled range of options to help make flying as smooth, safe, seamless and reliable as it can possibly be. Whether you operate a business jet, turboprop or hard-working helicopter, you can look to Garmin for industry-leading solutions scaled to fit your needs and your cockpit. The fact is, no other leading avionics manufacturer offers such breadth of capability — or such versatile configurability — in its lineup of flight deck solutions for aircraft manufacturers and aftermarket upgrades. When it comes to bringing out the best in your aircraft, Garmin innovation makes all the difference. CREATING A VIRTUAL REVOLUTION IN GLASS FLIGHT DECK SOLUTIONS By presenting key aircraft performance, navigation, weather, terrain routings and so on. The map function is designed to interface with a and traffic information, in context, on large high-resolution color variety of sensor inputs, so it’s easy to overlay weather, lightning, traffic, displays, today’s Garmin glass systems bring a whole new level of terrain, towers, powerlines and other avoidance system advisories, as clarity and simplicity to flight. The screens offer wide viewing angles, desired. These display inputs are selectable, allowing the pilot to add advanced backlighting and crystal-sharp readability, even in bright or deselect overlays to “build at will” the map view he or she prefers for sunlight. -
Systems Study for an Integrated Digital/Electric Aircraft (IDEA)
NASA-CR-3840 19850007405 NASA Contractor Report 3840 t i Systems Study for an Integrated Digital/Electric Aircraft (IDEA) G. E. Tagge, L. A. Irish, and A. R.Bailey CONTRACT NAS1-17528 JANUARY 1985 R [_.._ _ _ _'l _ €__!7 . ','7:2! ' ;: ;; 11) LANGLEY RESEJtRCHCEI",I_ER LIBRARY, NASA H;_4MPTO_JVIRG_N!A, NASA Contractor Report 3840 Systems Study for an Integrated Digital/Electric Aircraft (IDEA) G. E. Tagge, L. A. Irish, and A. R. Bailey Boeing Commercial Airplane Company Seattle, Washington Prepared for Langley Research Center under Contract NAS1-17528 N/ A NationalAeronautics and SpaceAdministration Scientific and Technical IntormatlonBranch 1985 FOREWORD This document constitutes the final report of the Integrated Digital/Electric Aircraft (IDEA)Program,ContractNASI-17528. The major studyobjectiveweres to definethe configurationof an IDEA aircraftd,efine technicalrisksassociatedwith the IDEA systemsconcepts,and identifytheresearchand developmentrequiredto reducetheserisksforpotentialapplicationto transporatircraft intheearly1990s. The NASA TechnicalRepresentativeforthistaskwas Cary R. SF1tzer;the Contracting Officerwas James Y. Taylor,of theLangleyResearchCenter. The work was accompUshed withinthe PreUmlnaryDesign Department of the Boeing Commercial AirplaneCompany. Key personnelwho contrlbutewdere: G. E.Tagge ProgramManager L.A. Irish StudyManager J.D.Vachal AerodynamicsTechnology L.A. Ostrom AerodynamicsTechnology R. H. Johnson PropulslonTeclmology G. G. Redfield PropulsionTechnology A. R. Bailey WeightsTechnology K. E. Siedentopf We_,_htsTechnology D. L.Grande StructuresTechnology C. B. Crumb Electronic FlightControlDesign F.Byford Mechanical FlightControlDesign W. F. Shivttz Flight Systems Technology C. W. Lee Flight Systems Technology P.J.Campbell FUght Systems Technology J. W. Harper Airframe Systems Technology-Electrlcal K. T. Tanemura AirframeSystemsTechnology-ECS E. C. Lim AirframeSystemsTechnology-ECS R. A. Johnson AirframeSystemsTechnology-ECS D. E. Cozby AirframeSystemsTechnology-lcing J.R.