Norwegian Boeing 787-8/9 Dreamliner
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The Boeing Company 2012 Annual Report at Boeing, We Aspire to Be the Strongest, Best and Best-Integrated Aerospace- Based Company in the World— for Today and Tomorrow
The Boeing Company 2012 Annual Report At Boeing, we aspire to be the strongest, best and best-integrated aerospace- based company in the world— for today and tomorrow. The Boeing Company Contents Boeing is the world’s largest aerospace Operational Summary 1 company and leading manufacturer Message From Our Chairman 2 of commercial airplanes and defense, space and security systems. The top The Executive Council 7 U.S. exporter, Boeing supports airlines and U.S. and allied government cus- Financial Results 8 tomers in more than 150 countries. Our Form 10-K 9 products and tailored services include commercial and military aircraft, satel- Selected Programs, lites, weapons, electronic and defense Products and Services 122 systems, launch systems, advanced Shareholder Information 129 information and communication sys- Cover photo: The liquid tems, and performance-based logistics Board of Directors 130 hydrogen–powered high- and training. With corporate offices in Company Officers 130 altitude long-endurance Chicago, Boeing employs more than Phantom Eye unmanned 174,000 people across the United aircraft system States and in 70 countries. In addition, Photo above: The new our enterprise leverages the talents of 737 MAX—designed for hundreds of thousands of skilled people maximum efficiency, reliabil- working for Boeing suppliers worldwide. ity and customer appeal Financial Highlights U.S. dollars in millions except per share data 2012 2011 2010 2009 2008 Revenues 81,698 68,735 64,306 68,281 60,909 Net earnings 3,900 4,018 3,307 1,312 2,672 Earnings per share* 5.11 5.33 4.46 1.87 3.65 Operating margins 7.7% 8.5% 7.7% 3.1% 6.5% Operating cash flow 7,508 4,023 2,952 5,603 (401) Contractual backlog 372,355 339,657 303,955 296,500 323,860 Total backlog† 390,228 355,432 320,826 315,558 351,926 * Represents diluted earnings per share from continuing operations. -
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. -
Touring Rudder Sit-On Top Kit Kit to Fit Rudder Enabled Sit-On Tops with a 10Mm Rudder Fixing Point
touring rudder sit-on top kit Kit to fit rudder enabled sit-on tops with a 10mm rudder fixing point. Note: It is easier to fit the Touring Rudder System if you have a screw hatch fitted to the rear stowage area of the kayak. If your kayak does not have this screw hatch and you wish to fit one, please contact a Perception dealer for advice. These instructions explain how to fit the rudder kit to a kayak with or without a rear screw hatch in place. Please make sure you follow the correct steps for your version of sit-on top kayak. This kit should contain the following: 1x rudder assembly with up-haul rope & split ring 4x deck fittings 4x length of rudder hose 5x self tapping screws 2x Dyneema control line - with cord end assembly 2x oval toggle 1x pair of Tip-Toes control footrests with foam washers 1x length of 4mm shock cord 6x footrest screws, washers and nuts - pre-fitted 1x rudder park - inc. hook, shock cord & fixing block You will also require some tools to fit this kit: Drill with 3mm, 5mm and 6mm drill bits Marker pen Short phillips screwdriver Wire cutters Small adjustable spanner or pair of pliers Lighter Tape measure Small amount of sticky tape Please read these instructions carefully before fitting! Step 1 - Control line entry points The rudder will need to have two control lines attached, each one running through hose sections inside the kayak from the rudder to the Tip-Toes footrests. This kit has four hose sections (two pairs) as two sections are needed per control line. -
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. -
Boeing's Commercial Jetliners Make an Ideal Platform for a Variety Of
s Boeing commercial jetliners crisscross the globe every Aircraft sees huge potential in modifying the Next-Generation 737 Development. “We must continue to show compelling value day, military and government aircraft based on those platform for a host of other military missions. Boeing also is com- to our customers.” The development of the new 737-based A planes are transporting state leaders, patrolling the skies peting to have its 767-based NewGen Tanker replace hundreds P-8A for the U.S. Navy offers an ideal model for how that can and assisting warfighters. of aging KC-135 tankers operated by the U.S. Air Force. be accomplished, he added. For more than a half-century, Boeing and its heritage companies Meanwhile, the U.S. president and congressional leaders fly The Poseidon team is using an in-line production process— have designed and built more than 1,000 specialized aircraft based on specially outfitted 747s, 757s and 737s. the industry’s first for derivative aircraft—based on the Boeing on commercial airplanes. With growing international demand for Modifying commercial aircraft for military and government uses Next-Generation 737 production system to build P-8 aircraft. military derivatives, and the recent success of the P-8A Poseidon, is not novel. Boeing heritage company Douglas Aircraft produced “It is the most affordable and efficient way to build military deriva- these programs are garnering significant attention. the first airplane used regularly by a president in 1944, when tive airplanes, and no one else in the world has this capability,” “We have a historic window, both domestically and internation- Franklin D. -
Reno – Stead Airport
Reno-Tahoe Airport Authority FY 2017-18 ANNUAL BUDGET Table of Contents SECTION 1 – Introduction and Summary Airport System Overview. ......................................................................................... 1-2 National and Regional Economic Outlook. ............................................................. 2-13 Air Service Market Update. ................................................................................... 13-17 Air Cargo Update. .................................................................................................. 17-19 Operating Environment. ........................................................................................ 19-29 Budget Process. ..................................................................................................... 29-30 Revenue Bond Resolution .......................................................................................... 30 Planning for the Future .......................................................................................... 30-32 Budget Document Structure ....................................................................................... 32 Conclusion ............................................................................................................. 32-33 Acknowledgments ...................................................................................................... 33 Distinguished Budget Presentation Award ................................................................. 34 SECTION 2 – Executive Summary -
Rules and Regulations Commissioners
Airport Commission City and County of San Francisco Edwin M. Lee Mayor Rules and Regulations Commissioners: Larry Mazzola President San Francisco International Airport Linda S. Crayton Vice President Adopted: March 15, 2016 Eleanor Johns Issued by: The Airport Commission Richard J. City and County of San Francisco Guggenhime Peter A. Stern John L. Martin Director CityandCountyofSanFrancisco AirportCommissionRulesandRegulations AIRPORT COMMISSION CITY AND COUNTY OF SAN FRANCISCO EDWIN M. LEE MAYOR COMMISSIONERS LARRY MAZZOLA PRESIDENT LINDA S. CRAYTON VICE PRESIDENT ELEANOR JOHNS RICHARD J. GUGGENHIME PETER A. STERN CityandCountyofSanFrancisco AirportCommissionRulesandRegulations FOREWORD The statements contained herein express the policy of the San Francisco Airport Commission, duly adopted as the Rules and Regulations, and are intended to ensure the safe and efficient operations of San Francisco International Airport. These Rules and Regulations govern the general conduct of the public, tenants, employees, and commercial users of San Francisco International Airport as their activities relate to the possession, management, supervision, operation and control of San Francisco International Airport by the City through its Airport Commission. JOHN L. MARTIN AIRPORT DIRECTOR City and County of San Francisco Airport Commission Rules and Regulations TABLE OF CONTENTS Rule .....................................................................................................................Page RULE 1.0 DEFINITIONS.................................................................................................................... -
Boeing 787 Dreamliner Video System Advanced, Integrated Security and Surveillance Solutions for Modern Airplanes Photo Courtesy Boeing
Boeing 787 Dreamliner Video System Advanced, integrated security and surveillance solutions for modern airplanes Photo courtesy Boeing ™ Cabin Video Monitoring UTC Aerospace Systems provides one of the most advanced airplane security and surveillance systems in commercial transport. The Cabin Video Monitoring System (CVMS) provides video and audio surveillance capability through the deployment of up to 16 covertly mounted digital cameras that also contain an integrated microphone. The cabin video can be viewed real-time and/or recorded. Flight Deck Entry Video Surveillance System cameras can also be integrated into the CVMS to provide the flight crew with comprehensive, situational awareness of all on-airplane systems. Equipment CVMS Benefits & Features • Up to 12 8410P1 Series Internet Protocol (IP) cameras provide • Enables real-time audio and video cabin monitoring color or monochromatic images and digital audio and video • IP cameras allow transition from analog to all-digital system, customizable to meet installation requirements • 8930A1 series Digital Video Recorder (DVR) • System accessed by Class 3 EFB system or via Ground Access • 256GB removable solid state memory Panel • Digital Video Recorder (DVR) capability CVMS P/N Table • Flight deck notified of CVMS activation via Engine Indicating and Crew-Alerting System (EICAS) “Cabin Alert” message IP Camera 8410P1 series Digital Video Recorder (DVR) 8930A1 series Digital Video Recorder Storage Memory 8732C1 series Security Camera Interface Unit (SCIU) 8730B2 series CVMS Client Application 8410P1 Series Camera Specifications Video Signal Dual Stream MPEG-4 (H.264) and MJPEG over Ethernet (RTP/RTSP) Video Format Color or Monochromatic Resolution 640 x 480 pixels Field of View 50º horizontal / 37.5º vertical Frame Rate 1 - 30 FPS configurable Power Consumption 2.5W max. -
Aircraft: Boeing 727, 737, 747, 757; Douglas DC-8, DC-9
No.: 2009-20080703001 Date: September 4, 2009 http://www.faa.gov/aircraft/safety/programs/sups/upn AFFECTED PRODUCTS: Aircraft: Boeing 727, 737, 747, 757; Douglas DC-8, DC-9 and MD-11 aircraft Part Number: Half Hinge Assembly, P/N 3953095U504 Notes: Additional parts may be affected (see parts list below). PURPOSE: The notification advises all aircraft owners, operators, manufacturers, maintenance organizations, parts suppliers and distributors regarding the unapproved parts produced by Watson’s Profiling Corporation, located in Ontario, CA 91761. BACKGROUND: Information received during a Federal Aviation Administration (FAA) Suspected Unapproved Parts (SUP) investigation revealed that between August 2005 and November 2007, Watson’s Profiling Corp., 1460 Balboa Avenue, Ontario, CA 91761, produced and sold parts (SEE ATTACHED PARTS LIST) without Direct Ship or Drop Ship authority from The Boeing Company. Furthermore, Watson’s Profiling Corp. is not an FAA Production Approval Holder. The parts produced by Watson’s Profiling Corporation have the following characteristics. • Their accompanying documentation indicates that the parts were manufactured by Watson’s, Profiling; however, they did not have FAA approval to manufacture and sell the parts as FAA-approved replacement parts. In addition, the investigation determined that some parts passed through various distributors. The majority, which were sold by Fossco Inc., 1211 Rainbow Avenue, Suite A, Pensacola, FL 32505. Documentation with the parts incorrectly indicated Watson’s Profiling, had -
Know About Boating Before You Go Floating
Know About Boating Before You Go Floating KEY TERMS All-around white light: Navigation light that Gunwale: Upper edge of a boat’s side. is visible in all directions around the boat from Hull: The main body of a boat. 2 miles away. Port: The left side of a boat. Bow: The front part of a boat. Propeller: A device with two or more blades Buoy: An object that floats on the water in that turn quickly and cause a boat to move. a bay, river, lake or other body of water and Sidelights: Red (port side) and green provides information to boats. (starboard side) navigation lights on a boat, Capsize: To turn a craft upside down in visible from 1 mile away. the water. Skipper: The person who commands a boat. Cleat: A wooden or metal fitting on the deck Starboard: The right side of a boat. of a boat. It has two projecting horns around which a rope or line may be tied. Stern: The back part of a boat. OBJECTIVES After completing this lesson, students will be able to: zz Name the main parts of a boat. zz Explain some boating terms. zz Describe some important safety equipment that should be on a boat. zz Demonstrate putting on a life jacket. zz Explain how to board a boat. zz Understand how to balance a boat. zz Explain what to do if a boat capsizes (turns over). MATERIALS, EQUIPMENT AND SUPPLIES zz Poster: Know About Boating Before You Go Floating zz Several Type II and/or Type III life jackets (in the various sizes that would fit the students) zz Mat or tape to create outline of boat zz Chairs (6) zz Watch or clock with a second hand zz Crayons, markers -
A Study of Vehicle Structural Layouts in Post-WWII Aircraft
A Study of Vehicle Structural Layouts in Post-WWII Aircraft Mark D. Sensmeier* Embry-Riddle Aeronautical University, Prescott, Arizona, 86301 Jamshid A. Samareh† NASA Langley Research Center, Hampton, Virginia, 23681 In this paper, results of a study of structural layouts of post-WWII aircraft are presented. This study was undertaken to provide the background information necessary to determine typical layouts, design practices, and industry trends in aircraft structural design. Design decisions are often predicated not on performance-related criteria, but rather on such factors as manufacturability, maintenance access, and of course cost. For this reason, a thorough understanding of current “best practices” in the industry is required as an input for the design optimization process. To determine these best practices and industry trends, a large number of aircraft structural “cutaway” illustrations were analyzed for five different aircraft categories (commercial transport jets, business jets, combat jet aircraft, single- engine propeller aircraft, and twin-engine propeller aircraft). Several aspects of wing design and fuselage design characteristics are presented here for the commercial transport and combat aircraft categories. A great deal of commonality was observed for transport structure designs over a range of eras and manufacturers. A much higher degree of variability in structural designs was observed for the combat aircraft, though some discernable trends were observed as well. Nomenclature Frames = Circumferential fuselage structures which help maintain fuselage shape and prevent skin buckling Longerons = Lengthwise fuselage structures which carry bending loads Ribs = Chordwise wing structures which maintain wing shape, carry shear, and prevent skin buckling Spars = Spanwise wing structures which provide primary wing resistance to aerodynamic bending loads I.