List of Avionics Design and Modification
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Serialization List Year Produced MODEL 18 D18S A-1 Thru A-37 1945 37
Commercial Genealogy Travel Air 1926 Beech Aircraft 1932 Beechcraft (A Raytheon Company) 1980 Raytheon Corporate Jets 1993 Raytheon Aircraft 1994 Hawker Beechcraft 2007 Beechcraft 2013 Textron Aviation 2014 Serialization 1945 thru 2020 21 May 2021 HAWKER 4000 BRITISH AEROSPACE AIRCRAFT HAWKER 1000 HAWKER 900XP HAWKER SIDDELEY 125-400 BEECHCRAFT HAWKER 125-400 U125A HAWKER 800 • HAWKER SIDDELEY 125 HAWKER 800XP HAWKER 800XPi HAWKER 850 HAWKER 800XPR SERIES 1 HAWKER 125-700 HAWKER 750 HAWKER 125-600 MODEL 400 BEECHJET • HAWKER SIDDELEY 125 400A BEECHJET 400A HAWKER 400XP HAWKER 400XPR SERIES 3 S18A T1A XA-38 GRIZZLY MODEL 2000 STARSHIP PREMIER I PREMIER IA S18 AT-10 KING AIR 350ER F2 KING AIR 350 • • • UC-45 U-21J SUPER KING AIR 300 KING AIR 350i KING AIR 350i D18S C45H SUPER E18 • • KING AIR B200 MODEL 18 SUPER H18 • • TWIN BEECH SUPER KING AIR 200 KING AIR B200GT KING AIR 250 KING AIR 250 C-12 AIR FORCE C-12 NAVY JRB-1 C-12 ARMY 1300 AIRLINER • • • • RC-12K C-12K JRB-2 • JRB-6 C-12 AIR FORCE U21F AT-11 • C-12 NAVY/MARINES KING AIR 100 • • • AT-7 KING AIR A100 B100 C-12 ARMY VC-6A B90 KING AIR B100 Legendary Innovation— • • • C90 SNB-1 MODEL 90 KING AIR T-44A E90 F90 KING AIR C90A Yesterday, Today and Tomorrow. SNB-2 • SNB-5P • • KING AIR C90B KING AIR C90GT KING AIR C90GTx KING AIR C90GTx U-21 RU-21 KING AIR F90-1 With a rich history dating back more than 80 years, Beechcraft Corporation continues to design, build NU-8F MODEL 99 AIRLINER B99 • and support a versatile and globally renowned fl eet of aircraft. -
Runway Analysis
CHAPTER 5 RUNWAY ANALYSIS 5 5 RUNWAY ANALYSIS INTRODUCTION The primary issue to be addressed in the William R. Fairchild International Airport (CLM) Master Plan involves the ultimate length and configuration of the runway system. At present there are two runways; primary Runway 8/26 and crosswind Runway 13/31. Runway 8/26 is 6,347 feet long and 150-feet wide with a displaced threshold of 1,354 feet on the approach end to Runway 26. The threshold was displaced to provide for an unobstructed visual approach slope of 20:1. Runway 13/31 is designated as the crosswind runway and is 3,250-feet long by 50-feet wide. In the 1997 ALP Update, the FAA determined that this runway was not required to provide adequate wind coverage and would not be eligible for FAA funding of any improvements in the future. The Port of Port Angeles has committed to keeping this runway functional without FAA support for as long as it is feasible. Subsequent sections of this analysis will reexamine the need for the runway. Both runways are supported by parallel taxiway systems with Taxiway A serving Runway 8/26 and Taxiway J for Runway 13/31. Taxiway A is 40 feet wide and Taxiway J is 50 feet wide. AIRFIELD REQUIREMENTS In determining airfield requirements, FAA Advisory Circular (AC) 150/5300-13, Airport Design (Change 14), has been consulted. This circular requires that future classification of the airport be defined as the basis for airfield planning criteria. As shown in the forecast chapter, the critical aircraft at CLM is expected to be the small business jet represented by the Cessna Citation within 5-years. -
Aviation Activity Forecasts
SOUTHWEST WASHINGTON REGIONAL AIRPORT AIRPORT MASTER PLAN Chapter 3 – Aviation Activity Forecasts The overall goal of aviation activity forecasting is to provide reasonable projections of future activity that can be translated into specific airport facility needs anticipated during the next twenty years and beyond. The first draft of this chapter was prepared in January 2018. Following FAA review, several revisions have been made, including updated based aircraft and aircraft operations forecasts. The original forecasts are maintained as originally presented for reference. Overview and Purpose This chapter provides updated aviation activity forecasts for Southwest Washington Regional Airport (KLS) for the twenty-year master plan horizon (2017-2037). The most recent Federal Aviation Administration (FAA) approved aviation activity forecasts for KLS were developed for the 2007-2027 planning period in the 2011 Airport Master Plan update. The forecasts presented in this chapter are consistent with the current and historic role of KLS as a regional general aviation airport, capable of accommodating a wide range of activity, including business class turboprops and jets. The well-documented shortage of public use airports in Southwest Washington with comparable capabilities, highlights the importance of recognizing the regional role of KLS in its current and long term planning. CHAPTER 3 - AVIATION ACTIVITY FORECASTS | DECEMBER 2020 | PAGE 3-1 SOUTHWEST WASHINGTON REGIONAL AIRPORT AIRPORT MASTER PLAN The forecasts of activity are unconstrained and assume the City of Kelso will be able to make the facility improvements necessary to accommodate the anticipated demand, unless specifically noted. The City of Kelso will consider if any unconstrained demand will not or cannot be reasonably met through the evaluation of airport development alternatives later in the master plan. -
Decision 2005/07/R
DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to Regulation (EC) No 1592/2002 of 15 July 2002 on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency1 (hereinafter referred to as the “Agency”), and in particular Articles 13 and 14 thereof. Having regard to the Commission Regulation (EC) No 2042/2003 of 28 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.2 Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. -
Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft
Air s.Pace ELectric Innovative Commuter Aircraft D2.1 Economic Feasibility Study for a 19 PAX Hybrid-Electric Commuter Aircraft Name Function Date Author: Maximilian Spangenberg (ASP) WP2 Co-Lead 31.03.2020 Approved by: Markus Wellensiek (ASP) WP2 Lead 31.03.2020 Approved by: Dr. Qinyin Zhang (RRD) Project Lead 31.03.2020 D2.1 Economic Feasibility Study page 1 of 81 Clean Sky 2 Grant Agreement No. 864551 © ELICA Consortium No export-controlled data Non-Confidential Air s.Pace Table of contents 1 Executive summary .........................................................................................................................3 2 References ........................................................................................................................................4 2.1 Abbreviations ...............................................................................................................................4 2.2 List of figures ................................................................................................................................5 2.3 List of tables .................................................................................................................................6 3 Introduction ......................................................................................................................................8 4 ELICA market study ...................................................................................................................... 12 4.1 Turboprop and piston engine -
Arctic Discovery Seasoned Pilot Shares Tips on Flying the Canadian North
A MAGAZINE FOR THE OWNER/PILOT OF KING AIR AIRCRAFT SEPTEMBER 2019 • VOLUME 13, NUMBER 9 • $6.50 Arctic Discovery Seasoned pilot shares tips on flying the Canadian North A MAGAZINE FOR THE OWNER/PILOT OF KING AIR AIRCRAFT King September 2019 VolumeAir 13 / Number 9 2 12 30 36 EDITOR Kim Blonigen EDITORIAL OFFICE 2779 Aero Park Dr., Contents Traverse City MI 49686 Phone: (316) 652-9495 2 30 E-mail: [email protected] PUBLISHERS Pilot Notes – Wichita’s Greatest Dave Moore Flying in the Gamble – Part Two Village Publications Canadian Arctic by Edward H. Phillips GRAPHIC DESIGN Rachel Wood by Robert S. Grant PRODUCTION MANAGER Mike Revard 36 PUBLICATIONS DIRECTOR Jason Smith 12 Value Added ADVERTISING DIRECTOR Bucket Lists, Part 1 – John Shoemaker King Air Magazine Be a Box Checker! 2779 Aero Park Drive by Matthew McDaniel Traverse City, MI 49686 37 Phone: 1-800-773-7798 Fax: (231) 946-9588 Technically ... E-mail: [email protected] ADVERTISING ADMINISTRATIVE COORDINATOR AND REPRINT SALES 22 Betsy Beaudoin Aviation Issues – 40 Phone: 1-800-773-7798 E-mail: [email protected] New FAA Admin, Advertiser Index ADVERTISING ADMINISTRATIVE ASSISTANT PLANE Act Support and Erika Shenk International Flight Plan Phone: 1-800-773-7798 E-mail: [email protected] Format Adopted SUBSCRIBER SERVICES by Kim Blonigen Rhonda Kelly, Mgr. Kelly Adamson Jessica Meek Jamie Wilson P.O. Box 1810 24 Traverse City, MI 49685 1-800-447-7367 Ask The Expert – ONLINE ADDRESS Flap Stories www.kingairmagazine.com by Tom Clements SUBSCRIPTIONS King Air is distributed at no charge to all registered owners of King Air aircraft. -
Boeing 737-300, 9H-ABT
Boeing 737-300, 9H-ABT AAIB Bulletin No: 5/98 Ref: EW/C97/8/3Category: 1.1 Aircraft Type and Registration: Boeing 737-300, 9H-ABT No & Type of Engines: 2 CFM56 turbofan engines Year of Manufacture: 1993 Date & Time (UTC): 1 August 1997 at 0943 hrs Location: On approach to Manchester Airport Type of Flight: Public Transport Persons on Board: Crew - 7 - Passengers - 93 Injuries: Crew - None - Passengers - None Nature of Damage: Nil Commander's Licence: Airline Transport Pilot's Licence Commander's Age: 49 years Commander's Flying Experience: 11,765 hours (of which 7,500 hours were on type) Last 90 days - 255 hours Last 28 days - 96 hours Information Source: AAIB Field Investigation History of flight The crew were operating a scheduled flight, as AMC 202, from Maltato Manchester. For the first part of the flight, the first officerwas the handling pilot. However, the forecast weather at Manchesterindicated that Low Visibility Procedures (LVP) would be requiredand, in accordance with company procedures, this would requirethe commander in the left seat to be the handling pilot. Therefore,towards the end of the cruise, the commander took over the handlingduties and the first officer assumed the normal non-handling dutiesincluding the radio monitoring and response. Prior to flight,the commander had confirmed the serviceability of the aircraftand noted that there were no 'Carried Forward Defects' in theTechnical Log; additionally, he had also confirmed that both thefirst officer and himself were qualified to carry out the expectedLVP approach. Throughout the flight, the aircraft was fully serviceable. Before descent, the crew obtained the airport weather informationand the commander briefed for the expected approach to Runway24 at Manchester. -
ICCT Aircraft Efficiency Design Public Draft
TRENDS IN AIRCRAFT EFFICIENCY AND DESIGN PARAMETERS Mazyar Zeinali, Ph.D. Daniel Rutherford, Ph.D. International Council on Clean Transportation (ICCT) ABSTRACT Developing an aircraft CO2 candidate metric and subsequent compliance assessment requires an understanding of practices and trends in aircraft design. Historically, fuel burn has been an important consideration for airlines, and manufacturers have responded by developing technologies to improve the efficiency of new aircraft designs. However, market forces also demand improvements in aircraft performance beyond reduced fuel burn. As a consequence, some portion of efficiency gained through improved technology has been devoted to increasing other aircraft design parameters such as range, maximum payload, and speed rather than to reducing emissions on a constant mission. In this paper, we discuss some initial ICCT work on sales‐weighted historical trends in new aircraft design attributes and their influence on aircraft efficiency, using design range as a first area of inquiry. We show that aircraft design parameters that influence fuel efficiency have changed over time, both in aggregate and for specific replacement designs, and therefore need to be taken into account when developing a CO2 certification requirement and stringency scenarios for further consideration. We also present evidence that commercial aircraft are not typically operated near their maximum performance points (i.e. design range and max payload), and therefore setting a CO2 certification requirement and standard at those points may overestimate improvements in future designs. 1. INTRODUCTION Developing an aircraft CO2 candidate metric and stringency scenarios will require knowledge and understanding of a complex system. Proper design choices will not only result in a policy that underscores environmental performance accurately, but also one that minimizes costs, undesirable impacts on competitiveness, and potential standard gaming. -
Aircraft Design Was Modeled More Closely After It
Aircraft Final Project GD3-200 Prepared by: Group 3 Tian Chen. Quoc Tran . Oge Onuoha. Tony Haughton. Jean-Etienne Dongmo. Introduction The GD3-200 is a twin engine, new technology jet airplane designed for low fuel burn and short-to-medium range operations. This airplane uses new aerodynamics, advanced composite materials, structures, and systems to fill market requirement that cannot be efficiently provided by existing equipment or derivatives. The GD3-200 will provide airlines with unmatched fuel efficiency. The airplane will use 20 percent less fuel for comparable missions than any other airplane in its class. The key to this exceptional performance lies in the use of advanced composite materials for the majority of the airplane’s fuselage and wing structure. GD3 has also enlisted General Electric to develop engines for the new airplane. The GD3-200 is a highly fuel efficient low-noise airplane powered by General Electric new GEnx CF6-6 engines. These 9.5 to 1 high-bypass-ratio engines are reliable and easy to maintain. Using GEnx derived technology means these engines bring an average 15 percent improvement in specific fuel consumption over all other engines in its class. In the passenger configuration, the GD3-200 can typically carry 186 passengers (200 including crew) in a six-abreast, mixed class configuration over a 3000 mile range with full load. The GD3-200 can be equipped for Extended Range Operations (EROPS) to allow extended over-water operations. Changes include a backup hydraulic motor-generator set and an auxiliary fan for equipment cooling. Mission Requirement Payload: -200 passengers/crew at 200 lb each (includes baggage) 40000lb -5000 lb Cruise: 0.8 Mach at 33000 ft Cruise Range: 3000 miles Cruise Altitude: 33,000 ft Loiter: 30 minutes at 0.8 m Mach at 33000 ft Climb: Initial climb to cruise altitude starting at maximum takeoff weight Take-off distance: 5000 to 6000 ft with 50 ft clearance at sea level and standard conditions at maximum takeoff weight Power plant: more than 1; high-by-pass turbofan; choose from existing ones. -
Bombardier Learjet 35A
Contact Pilot Maintenance Us Fact Sheet Fact Sheet Share Next Bombardier Learjet 35A Professional Pilot and Technician Training Programs Updated 10/16 Contact Pilot Maintenance Us Fact Sheet Fact Sheet Share Prev Next FlightSafety offers comprehensive, professional training on Bombardier’s full line of business aircraft, including the Learjet 35A. Our highly qualified and experienced instructors, advanced-technology flight simulators and integrated training systems help ensure proficiency and safety. Pilot training for the Learjet 35A is available at FlightSafety’s Learning Centers in Atlanta, Georgia and Tucson, Arizona. Maintenance technicians train for the Learjet 35A at our Tucson Learning Center. Innovation With One Purpose: Training Corporate Aviation Professionals for Safety and Proficiency FlightSafety International is the world’s leading aviation training organization. The leader in experience. The leader in technological innovation. The leader in global reach. FlightSafety serves the world’s aviation community providing total aviation training for pilots, maintenance technicians and other aviation professionals. We serve business, commercial, general and military aviation with training for virtually Experienced all fixed-wing aircraft and helicopters. We live, breathe and ThinkSafety. Instructors, FlightSafety provides training for the Bombardier Global series, Bombardier Challenger and Bombardier Learjet. Superior We offer business aviation pilots and maintenance technicians of Bombardier aircraft the resources to achieve proficiency -
The Indonesia Dassault Falcon 7X Wu Zhendong Metrics & Mood Jets & Helicopters
FOURTH QUARTER 2015 THE INDONESIA PERSPECTIVE THE CHECKUP : DASSAULT FALCON 7X INDUSTRY INSIDER: WU ZHENDONG ASIA-PACIFIC OUTLOOK: METRICS & MOOD CURRENT MARKET SUMMARIES: JETS & HELICOPTERS THE WORLD STANDARD Intercontinental range, record-setting speed, advanced technology, unrivaled utility and top-rated worldwide product support. The World Standard™ isn’t just a company tagline, it’s a benchmark by which all others must be measured. BEIJING (北京): +86 10 8535 1866 HONG KONG (香港): +852 2918 1600 SINGAPORE (新加坡): +65 6572 7777 GULFSTREAM.COM G650ER, G650, G600, G500, G550, G450, G280 and G150 are trademarks or registered trademarks of Gulfstream Aerospace Corporation in the U.S. and other countries. THE WORLD STANDARD Intercontinental range, record-setting speed, advanced technology, unrivaled utility and top-rated worldwide product support. The World Standard™ isn’t just a company tagline, it’s a benchmark by which all others must be measured. BEIJING (北京): +86 10 8535 1866 HONG KONG (香港): +852 2918 1600 SINGAPORE (新加坡): +65 6572 7777 GULFSTREAM.COM G650ER, G650, G600, G500, G550, G450, G280 and G150 are trademarks or registered trademarks of Gulfstream Aerospace Corporation in the U.S. and other countries. TWO WAYS TWO WAYS TO CONQUER THE WORLD. TO CONQUER THE WORLD. 广告 two ways to conquer the world. Now you have two choices for superior, ultra-long-range capability. The 5,950 nm Falcon 7X—the fastest selling Falcon ever (and with Now you have two choices for superior, ultra-long-range capability. The 5,950 nm Falcon 7X—the fastest selling Falcon ever (and with good reason). Or the new, 6,450 nm Now you have two choices for superior, ultra-long-range capability.good Thereason). -
Investigating Optimal Replacement of Aging Air Force Systems
R Investigating Optimal Replacement of Aging Air Force Systems Edward G. Keating, Matthew Dixon Prepared for the United States Air Force Project AIR FORCE Approved for public release; distribution unlimited The research reported here was sponsored by the United States Air Force under Contract F49642-01-C-0003. Further information may be obtained from the Strategic Planning Division, Directorate of Plans, Hq USAF. Library of Congress Cataloging-in-Publication Data Keating, Edward G. (Edward Geoffrey), 1965- Investigating optimal replacement of aging Air Force systems / Edward G. Keating, Matthew C. Dixon. p. cm. Includes bibliographical references. “MR-1763.” ISBN 0-8330-3483-9 (pbk. : alk. paper) 1. United States. Air Force—Procurement—Mathematical models. 2. KC–135 (Tanker aircraft) 3. Lear jet aircraft. 4. Jet transports—United States—Maintenance and repair— Mathematical models. I. Dixon, Matthew C. II. Title. UG1123.K43223 2003 358.4'1621—dc22 2003020469 RAND is a nonprofit institution that helps improve policy and decisionmaking through research and analysis. RAND® is a registered trademark. RAND’s publications do not necessarily reflect the opinions or policies of its research sponsors. © Copyright 2003 RAND All rights reserved. No part of this book may be reproduced in any form by any electronic or mechanical means (including photocopying, recording, or information storage and retrieval) without permission in writing from RAND. Published 2003 by RAND 1700 Main Street, P.O. Box 2138, Santa Monica, CA 90407-2138 1200 South Hayes Street, Arlington, VA 22202-5050 201 North Craig Street, Suite 202, Pittsburgh, PA 15213-1516 RAND URL: http://www.rand.org/ To order RAND documents or to obtain additional information, contact Distribution Services: Telephone: (310) 451-7002; Fax: (310) 451-6915; Email: [email protected] iii Preface Whether to maintain or replace an aging system is a common decision.