Airlines Must Work with Their Fuel Suppliers to Ensure That Local Fuel Handling Procedures Are Being Followed. Engine Fuel Filter Contamination
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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. -
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. -
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 -
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. -
Re-Engining a Boeing 727-200 (Advanced) Versus Buying a New Boeing 757-200
Journal of Aviation/Aerospace Education & Research Volume 4 Number 1 JAAER Fall 1993 Article 1 Fall 1993 A Cost Analysis: Re-Engining a Boeing 727-200 (Advanced) Versus Buying a New Boeing 757-200 Peter B. Coddington Follow this and additional works at: https://commons.erau.edu/jaaer Scholarly Commons Citation Coddington, P. B. (1993). A Cost Analysis: Re-Engining a Boeing 727-200 (Advanced) Versus Buying a New Boeing 757-200. Journal of Aviation/Aerospace Education & Research, 4(1). https://doi.org/10.15394/ jaaer.1993.1110 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in Journal of Aviation/Aerospace Education & Research by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Coddington: A Cost Analysis: Re-Engining a Boeing 727-200 (Advanced) Versus B A COSTANALYSIS: RE-ENGINlNG A BOEING 727-200 (ADVANCED) VERSUS BUYING A NEWBOEING 757-200 Peter B. Coddington The Boeing 727-200 and 757-200 are both narrowbody aircraft designed for short- to medium-range flights carrying 164 to 214 passengers. Until recently, when overtaken by the Boeing 737, the 727-200 program was the most successful aircraft program in history. The 727 airplane has carried 2.3 billion passengers, equivalent to half the world's population (Sterling, 1992). More than half of all 727s sold were advanced 200s and as late as 1990 an incredible 50% of all U.S. passenger traffic had flown on 727-200s since the advanced model was launched in 1971. -
Transatlantic Airline Fuel Efficiency Ranking, 2017
WHITE PAPER SEPTEMBER 2018 TRANSATLANTIC AIRLINE FUEL EFFICIENCY RANKING, 2017 Brandon Graver, Ph.D., and Daniel Rutherford, Ph.D. www.theicct.org [email protected] BEIJING | BERLIN | BRUSSELS | SAN FRANCISCO | WASHINGTON ACKNOWLEDGMENTS The authors thank Tim Johnson, Andrew Murphy, Anastasia Kharina, and Amy Smorodin for their review and support. We also acknowledge Airline Data Inc. for providing processed BTS data, and FlightGlobal for Ascend Fleet data. International Council on Clean Transportation 1225 I Street NW Suite 900 Washington, DC 20005 USA [email protected] | www.theicct.org | @TheICCT © 2018 International Council on Clean Transportation TRANSATLANTIC AIRLINE FUEL EFFICIENCY RANKING, 2017 TABLE OF CONTENTS EXECUTIVE SUMMARY ............................................................................................................ iii 1. INTRODUCTION .................................................................................................................... 2 2. METHODOLOGY ................................................................................................................... 3 2.1 Airline selection .................................................................................................................................3 2.2 Fuel burn modeling..........................................................................................................................5 2.3 Fuel efficiency calculation ............................................................................................................6 -
Download This Issue (PDF)
03 Jeppesen Expands Products and Markets 05 Preparing Ramp Operations for the 787-8 15 Fuel Filter Contamination 21 Preventing Engine Ingestion Injuries QTR_03 08 A QUARTERLY PUBLICATION BOEING.COM/COMMERCIAL/ AEROMAGAZINE Cover photo: Next-Generation 737 wing spar. contents 03 Jeppesen Expands Products and Markets Boeing subsidiary Jeppesen is transforming its support to customers with a broad array of technology-driven solutions that go beyond the paper navigational charts for which Jeppesen 03 is so well known. 05 Preparing Ramp Operations for the 787-8 Airlines can ensure a smooth transition to the Boeing 787 Dreamliner by understanding what it has in common with existing airplanes in their fleets, as well as what is unique. 15 Fuel Filter Contamination 05 Dirty fuel is the main cause of engine fuel filter contamination. Although it’s a difficult problem to isolate, airlines can take steps to deal with it. 21 Preventing Engine Ingestion Injuries 15 Observing proper safety precautions, such as good communication and awareness of the hazard areas in the vicinity of an operating jet engine, can prevent serious injury or death. 21 01 WWW.BOEING.COM/COMMERCIAL/AEROMAGAZINE Issue 31_Quarter 03 | 2008 Publisher Design Cover photography Shannon Frew Methodologie Jeff Corwin Editorial director Writer Printer Jill Langer Jeff Fraga ColorGraphics Editor-in-chief Distribution manager Web site design Jim Lombardo Nanci Moultrie Methodologie Editorial Board Gary Bartz, Frank Billand, Richard Breuhaus, Darrell Hokuf, Al John, Doug Lane, Jill Langer, -
U.S. Command and Control and Intelligence, Surveillance, and Reconnaissance Aircraft
U.S. Command and Control and Intelligence, Surveillance, and Reconnaissance Aircraft Jeffrey Nelson US Air Force Fellow July 15, 2015 Congressional Research Service 7-5700 www.crs.gov R44108 c11173008 . U.S. Command and Control and Intelligence, Surveillance, and Reconnaissance Aircraft Summary The fleet of manned aircraft accomplishing the Department of Defense’s (DOD’s) Command and Control (C2) and Intelligence, Surveillance, and Reconnaissance (ISR) missions for the joint military community (E-8, E-3, RC-135, WC-135, OC-135, and E-6) is primarily based on Boeing 707 aircraft procured from the 1960s to the early 1990s. As the age of these legacy C2ISR aircraft increases, understanding the Air Force and Navy modernization and recapitalization plans is likely important for Congress. This report examines the Air Force’s and Navy’s current sustainment, modernization, and recapitalization efforts for these Boeing 707-based aircraft, and issues Congress may take into account when considering appropriating funds for continued sustainment and modernization of these aircraft versus funding for recapitalization of these missions to new aircraft. This report addresses potential congressional oversight and appropriations concerns for the sustainment, modernization, and recapitalization of the DOD’s Boeing 707-based legacy C2ISR aircraft fleet. It does not address options for recapitalization currently being offered by industry to other countries. Congress has the authority to approve, reject, or modify Air Force and Navy funding requests for C2ISR aircraft sustainment, modernization, and recapitalization, as well as oversight of the nation’s C2ISR requirements and capabilities. Congress’s decisions on appropriations for the C2ISR force could impact the nation’s C2ISR capabilities and have additional consequences for the U.S. -
Charter Report - 2019 Prospectuses
CHARTER REPORT - 2019 PROSPECTUSES Beginning Number of Type of Aircraft Charter Operator Carrier Origin Destination Date Ending Date Remarks/Indirect Carrier Flights & No. of Seats Embraer 135 19-001 Resort Air Services RVR Aviation (air taxi) DAL-89TE LAJ-DAL-89TE 2/22/2019 12/15/2019 94 w/30 sts New England Air Transport Inc. PILATUS PC-12 19-002 JetSmarter Inc. (air taxi) FLL MYN 2/8/2019 2/8/2019 1 w/6 guests Hawker 800 w/8 19-003 JetSmarter Inc. Jet-Air, LLC (air taxi) FLL HPN 3/3/2019 3/3/2019 1 guests Gulfstream G200 w/10 19-004 JetSmarter Inc. Chartright Air Inc. (air taxi) FLL YYZ 3/7/2019 3/7/2019 1 guests Domier 328 Jet Ultimate Jetcharters, LLC dba w/30sts/ Ultimate Jet Shuttle Public Ultimate JETCHARTERS, LLC Embraer 135 Jet 19-005 Charters Inc.(co-charterer) dba Ultimate Air Shuttle CLT PDK 2/25/2019 2/24/2020 401 w/30 sts Citation C J2 19-006 JetSmarter Inc. Flyexclusive, Inc. (air taxi) ORL TEB 3/30/2019 3/30/2019 1 w/6 guests Phenom 300 19-007 JetSmarter Inc. GrandView Aviation (air taxi) JAX MTN 3/24/2019 3/24/2019 1 w/7 guests Aviation Advantage/E-Vacations Corp Boeing 737-400 19-008 (co-charterer) Swift Air SJU-PUJ-POP-etc PUJ-SJU-CUN-etc 6/3/2019 8/3/2019 50 w/150 sts Boeing 737-400 19-009 PrimeSport Southwest Airlines BOS ATL 2/1/2019 2/4/2019 50 w/150 sts CHARTER REPORT - 2019 PROSPECTUSES Delux Public Charter, LLC EMB-135 w/30 19-010 JetBlue Airways Corporation dba JetSuite X (commuter) KBUR-KLAS-KCCR-etc KLAS-KBUR-KCCR-etc 4/1/2019 7/1/2019 34,220 sts Glulfstream IV- 19-011 MemberJets, LLC Prine Jet, LLC (air taxi) OPF-TEB-MDW--etc TEB-OPF-PBI-etc 2/14/2019 12/7/2019 62.5 SP w/10 sts Phenom 300 19-012 JetSmarter Inc. -
Summary of the FAA's Review of the Boeing 737
Summary of the FAA’s Review of the Boeing 737 MAX Summary of the FAA’s Review of the Boeing 737 MAX Return to Service of the Boeing 737 MAX Aircraft Date: November 18, 2020 Summary of the FAA’s Review of the Boeing 737 MAX This page intentionally left blank. 1 Summary of the FAA’s Review of the Boeing 737 MAX Table of Contents Executive Summary ............................................................................................ 5 Introduction .................................................................................................... 5 Post-Accident Actions ....................................................................................... 6 Summary of Changes to Aircraft Design and Operation ........................................ 9 Additional Changes Related to the Flight Control Software Update. ...................... 10 Training Enhancements .................................................................................. 11 Compliance Activity ....................................................................................... 12 System Safety Analysis .................................................................................. 13 Return to Service .......................................................................................... 13 Conclusion .................................................................................................... 14 1. Purpose of Final Summary ........................................................................... 15 2. Introduction ..............................................................................................