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767, Awl, D622t001-9-01
767-200/300/300F/400ER AIRWORTHINESS LIMITATIONS 767-200/300/300F/400ER AIRWORTHINESS LIMITATIONS (AWLs) D622T001-9-01 JUNE 2019 This document has EAR data with an Export Control Classification Number (ECCN) of 9E991. Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws. Boeing claims copyright in each page of this document on to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work. This document includes proprietary information owned by the Boeing Company and/or one or more third parties. Treatment of the document and the information it contains is governed by contract with Boeing. For more information, contact the Boeing Company, P.O. Box 3707, Seattle WA 98124. Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, BBJ, DC-8, DC-9, DC-10, MD-10, MD-11, MD-80, MD-88, MD-90, and the red-white-blue Boeing livery are all trademarks owned by The Boeing Company; no trademark license is granted in connection with this document unless provided in writing by Boeing. COMPILED AND PUBLISHED BY: MAINTENANCE PROGRAMS ENGINEERING BOEING COMMERCIAL AIRPLANE GROUP SEATTLE, WASHINGTON D622T001-9-01 JUN 2019 BOEING PROPRIETARY - Copyright -
Issue No. 4, Oct-Dec
Focal Product Support: Commitment, Cooperation, Communication A SERVICE PUBLICATION OF The Lockheed Aeronautical Systems Company LOCKHEED AERONAUTICAL Product Support organization is determined to provide SYSTEMS COMPANY the highest level of service to each of our customers and every one of our airplanes. This level of support Editor is focused toward our personal commitment to our Charles I. Gale customers, quick and open lines of communication to provide information and receive feedback from our Art Director customers, and full cooperation with our customers Cathy E. Howard to develop a team approach to support. Vol. 20, No. 4, October-December 1993 The support arena has undergone vast change in John Gaffney recent years and LASC Product Support has had to CONTENTS evolve to keep pace and meet our customers’ needs. This evolution has resulted in the customer becoming 2 Focal Point more and more prominent in the market place, competition intensifying, and change John L. Gaffney, Director itself becoming constant. LASC Product Support Product Support has made changes and continues to make changes to respond 3 Ramp Hook Retainer to market conditions. Our customers indicated they wanted: Mislocation Playing mix and match with the A “one-stop shop” for all support services. We have become that “one- hook retainers makes cargo ramp stop shop.” Any element of support needed by a customer can be rigging an exercise in frustration. obtained from a single source within LASC Product Support. 10 Making a Ramp Hook Retainer Competitive prices. We are finalizing teaming arrangements which will Identification Tool allow us to offer customers a full spectrum of parts-new, used, and This locally manufactured shop aid overhauled-at competitive prices, all under the auspices of the original can correctly identify the retainers equipment manufacturer. -
Germans .Britain Boosts Income Tax to New Peak^ Harbors, Airports
\ UeilDAr.}T)LTII.tM« ..im r i M L v s '■’Vi flatirftfstnr Etiratno 3SrndIk Average Dally Cirealetlea Far tha Moath at Jama. l$ i . The regular meatlng af Mlaato- Mra Herbert Sargent and tv-f 4 The Weather While working on the new town Dr. Edward F. Krtksclun of Chi Pr. and Mrs. A. A. Friahalt o f M Edward Harris, ■7ST Maary Mrs. Joi^^hina Ptow4k Hills, Elwood street are taking a vaca street, was sersiiaded ftmdey. by noraoh TTlbe No. BB, I. O. ft. M., children, Alice Jeen and Herbert roraeaat af O. S. WaaUur Bmi who U oondudUng a summer art dump several men of the Love cago, ni., one of the successful wUl ha held In the Sports Center Kilby, have left for Weymouth HitTawn Lane W. P. A. project have been tion until August 2, and enjoying tha siOvatlon Army Band. X f. 6,429 course in Rodm 10 of ManehooUr candidates In the state dental sViaon WellsTT vgam ,^ streetv tonight at el^ t Nova Scotia, where they will epenf / affected by^tHrlUtlon of the skin short trips to nsarby places of in HarriA wbo is a member o f thr High school, has changsd the in exams Is a nephew of Peter Staum terest band'haa been confined to bed adth shiu’p. the remainder of the summer. Maatbar af tha Aadit / struction hours, by request, frops from polpcmlng. None of the cases of 89 W. Middle Turnpike. He 1s a heart aliment for the past six BnieM o f Otienlotlono ^ srsji BMtriM AnoM. -
The Wing Is the Principal Structural Unit of the Airplane. It Has Several Functions Beyond That of Providing Lift. for a Wing To
1 WING The wing is the principal structural unit of the airplane. It has several functions beyond that of providing lift. For a wing to produce "lift", it must be oriented at a suitable angle of attack relative to the flow of air past the wing. In aerodynamics, angle of attack (AOA) specifies the angle between the chord line of the wing of a fixed-wing aircraft and the vector representing the relative motion between the aircraft and the atmosphere. On larger airplanes the engines are mounted in nacelles either attached to the wing or mounted in the wing. The nacelles also provide a housing for the landing gear when it is retracted. The space within the wing is usually used for fuel storage. The main geometrical features of a wing are its span; the area of the wing; its dihedral angle; its sweepback angle; and the wing section. Dihedral angle is the upward angle of an aircraft's wing, from the wing root to the wing tip. The amount of dihedral determines the amount of inherent stability along the roll axis. Although an increase of dihedral will increase inherent stability, it will also decrease lift, and increase drag. The design of the wing depends on the size, weight, and use of the airplane. Generally, there are two kinds of wing design: cantilever and semi-cantilever. The semi-cantilever usually has one, or perhaps two, supporting wires or struts attached to each wing and the fuselage. As far as the internal structure is concerned, there are three general types of conventional wings: monospar, two-spar, and multispar. -
Unusual Attitudes and the Aerodynamics of Maneuvering Flight Author’S Note to Flightlab Students
Unusual Attitudes and the Aerodynamics of Maneuvering Flight Author’s Note to Flightlab Students The collection of documents assembled here, under the general title “Unusual Attitudes and the Aerodynamics of Maneuvering Flight,” covers a lot of ground. That’s because unusual-attitude training is the perfect occasion for aerodynamics training, and in turn depends on aerodynamics training for success. I don’t expect a pilot new to the subject to absorb everything here in one gulp. That’s not necessary; in fact, it would be beyond the call of duty for most—aspiring test pilots aside. But do give the contents a quick initial pass, if only to get the measure of what’s available and how it’s organized. Your flights will be more productive if you know where to go in the texts for additional background. Before we fly together, I suggest that you read the section called “Axes and Derivatives.” This will introduce you to the concept of the velocity vector and to the basic aircraft response modes. If you pick up a head of steam, go on to read “Two-Dimensional Aerodynamics.” This is mostly about how pressure patterns form over the surface of a wing during the generation of lift, and begins to suggest how changes in those patterns, visible to us through our wing tufts, affect control. If you catch any typos, or statements that you think are either unclear or simply preposterous, please let me know. Thanks. Bill Crawford ii Bill Crawford: WWW.FLIGHTLAB.NET Unusual Attitudes and the Aerodynamics of Maneuvering Flight © Flight Emergency & Advanced Maneuvers Training, Inc. -
Fined for Sunday Work. Red Bank to New Mexico
RED BANE REGISTER. litngd Waikhr, Estatad M Sioond-Olsli Mattar at tha Post. VOLUME LII, NO. 9. oOoa >t Bad Dank, N. J» andgr th« Aot of Maroh 8, 1871). RED BANK, N. J., WEDNESDAY, AUGUST 28, 1929. $1.50 PER YEAR PAGES 1 TO 16. used in tho construction of these hog TINTON FALLS IS DRY. FINED FOR SUNDAY WORK. sheltors. AGAINST NOISY BOATS. RED BANK TO NEW MEXICO We havo seen another uso for thes BABIES AWARDED PRIZES. Water Supply In Many Wells Falls as VISIT ICE CREAM PUNT. PROFITS IN IRRIGATION. A tents. A good many new house! Ilcsult of Drought. THE "BLUE LAWS" AIIE INVOKED SOME OF THE INTERESTING havo llttlo trees, two or three feel MIDDLETOWN RESIDENTS COM- HIGHLANDS BABY PARADE BIG CHILDREN INSPECT CASTLE'S So far as well water is concerned, GEORGE H. IIOBEBT8 18 HOT AT rOilT MONMOUTH. THINGS SEEN ON THE WAY. high, set out around them, and simi- PLAIN OF NOISE ON IUVEB. GEIl THAN EVER. FACTORY AT PERTH AMBOY. lar trees are set out In new parks, probably no place in this part of wonnnsD BY THE DROUGHT. These A tents, mado of cement bags They Took Their Grievances to War Monmouth county has been harder Bnlvntoro Scagllone Was Fined $10.25 A Waterspout and Flying Fish in tho Thero Were 114 Children In Line and hit by the drought than Tinton Falls. About Thirty Boys ami GLrls From Now Monmouth Farmer Una Flvo Last VVcoU—Other Sunday Busi- Atlantic—Trolley Italia Laid in or other old and wornout bags, with Department nnd Wero Informed It Fifty Cups Wero Awarded as tho Red Bank Playground Made their sides spilt up, are put over Was Local Mutter—Association A dozen or more wells at that place Acres of Ills Fiirm Irrigated With nesses Rcniuln Open and This Gruss l'lots—Hunches Raising Prizes — Virginia Reuter Was have gone dry. -
Airframe & Aircraft Components By
Airframe & Aircraft Components (According to the Syllabus Prescribed by Director General of Civil Aviation, Govt. of India) FIRST EDITION AIRFRAME & AIRCRAFT COMPONENTS Prepared by L.N.V.M. Society Group of Institutes * School of Aeronautics ( Approved by Director General of Civil Aviation, Govt. of India) * School of Engineering & Technology ( Approved by Director General of Civil Aviation, Govt. of India) Compiled by Sheo Singh Published By L.N.V.M. Society Group of Institutes H-974, Palam Extn., Part-1, Sec-7, Dwarka, New Delhi-77 Published By L.N.V.M. Society Group of Institutes, Palam Extn., Part-1, Sec.-7, Dwarka, New Delhi - 77 First Edition 2007 All rights reserved; no part of this publication may be reproduced, stored in a retrieval system or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, without the prior written permission of the publishers. Type Setting Sushma Cover Designed by Abdul Aziz Printed at Graphic Syndicate, Naraina, New Delhi. Dedicated To Shri Laxmi Narain Verma [ Who Lived An Honest Life ] Preface This book is intended as an introductory text on “Airframe and Aircraft Components” which is an essential part of General Engineering and Maintenance Practices of DGCA license examination, BAMEL, Paper-II. It is intended that this book will provide basic information on principle, fundamentals and technical procedures in the subject matter areas relating to the “Airframe and Aircraft Components”. The written text is supplemented with large number of suitable diagrams for reinforcing the key aspects. I acknowledge with thanks the contribution of the faculty and staff of L.N.V.M. -
Structural Certification of the F-16 Block 52+ Aircraft 29 November 2005 2005 USAF Aircraft Structural Integrity Program Conference
Structural Certification of the F-16 Block 52+ Aircraft 29 November 2005 2005 USAF Aircraft Structural Integrity Program Conference Robert J. Burt Director and Deputy F-35 Structural Development and Integrity Lockheed Martin Aeronautics Company Fort Worth © 2005 LOCKHEED MARTIN CORPORATION Lockheed Martin Aeronautics Company Structural Certification of the F-16 Block 52+ Aircraft Abstract This presentation will describe in some detail the process followed by Lockheed Martin Aeronautics – Fort Worth for the structural certification of the new production F-16 Block 52+ aircraft for foreign military sales (FMS). The F-16 Block 52+ aircraft are structurally upgraded from the USAF Block 50/52 aircraft due to carriage of the fuselage shoulder mounted conformal fuel tanks and due to the addition of numerous advanced systems. The structural requirements and their methods of verification are set forth in the program contract and subsequent program documents such as the weapon system specification and air vehicle specification. Every USAF and FMS F-16 has an Aircraft Structural Integrity Program (ASIP) based upon program contractual requirement and tailored to MIL-STD-1530B Aircraft Structural Integrity Program. An ASIP Master Plan has been written for the Block 52+ aircraft which has been coordinated with and approved by the USAF F-16 System Group. This ASIP Master Plan states in specific terms how all the tasking outlined in the “five pillars” is accomplished. An overall design process will be discussed in depth pointing out how all historical structural analysis, structural test and field information has been used in the structural design of the Block 52+ aircraft. -
Technical Order 00-105E-9, 1 February 2006, Revision 11
WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, REVISION 11. THIS IS SEGMENT 11 COVERING CHAPTER 8 FROM THE QF-4 TO F-16. TO NAVIGATE CLICK ON THE CONTINUE BOOKMARKS AND CLICK ON THE (+) SYMBOLS, THEN NOTICE CLICK ON SUBJECT LINKS TO GO TO SPECIFIC VIEWS CONTACT IN THIS SEGMENT. TO GO DIRECTLY TO THE TECHNICAL ORDER, CLICK ON THE CONTINUE BUTTON. TO SEE THE SEGMENT INFORMATION CHANGE NOTICE, CLICK ON THE NOTICE BUTTON. TO CONTACT THE TECHNICAL CONTENT MANAGER , CLICK ON THE CONTACT BUTTON. TECHNICAL ORDER 00-105E-9 TECHNICAL CONTENT MANAGER WRITTEN CORRESPONDENCE: HQ AFCESA/CEXF ATTN: Fire and Emergency Services Egress Manager 139 Barnes Drive Suite 1 Tyndall AFB, Florida 32403-5319 E-MAIL: [email protected] INTERNET: HQ AFCESA Fire and Emergency Services PUBLIC WEB PAGE: http://www.afcesa.af.mil/CEX/cexf/index.asp Safety Supplements: http://www.afcesa.af.mil/CEX/cexf/_firemgt.asp PHONE: (850) 283-6150 DSN 523-6150 FAX: (850) 283-6383 DSN 523-6383 For technical order improvements, correcting procedures, and other inquiries, please use the above media most convenient. SEGMENT 11 INFORMATION CHANGE NOTICE This page is provided to notifiy the user of any informational changes made to Technical Order 00-105E-9 in this Segment and the current Revision. Informational changes will be referenced in the Adobe Reader’s Bookmark tool as a designator symbol illustrated as a <[C]> for quick reference to the right of the affected aircraft. The user shall insure the most current information contained in this TO is used for his operation. -
"FINAL DESTINATION" Originally Called "FLIGHT 180"
"FINAL DESTINATION" Originally Called "FLIGHT 180" By James Wong and Glen Morgan January 15, 1999 Awaiting......each of us; a cold...dark...lonely place. Deny its finality. Deride its totality. Dread the inescapable inevitability......it will arrive. The BLACK SILENT SCREEN senses this moment before a distant blues harp introduces a contemporary band's cover of Blood, Sweat, and Tears' campy, yet haunting, gospel, "And When I Die." As the Introduction closes, RESONATES... A FLASH OF LIGHTING! A CRACK OF THUNDER! CUT TO: INT. ALEX'S BEDROOM - NIGHT - CLOSE - BED An airline ticket is tossed INTO FRAME beside a suitcase; "EURO-AIR. FLIGHT #180. New York City (JFK) - Paris, Charles de Gaulle (CDG.) Departure: Thursday 13May. 16H25 - Arrival: Friday 14May. 05H40." "And When I Die" Continues throughout the MAIN TITLES: AN OLD TABLE FAN swivels beside and open window. Outside, a humid spring THUNDER STORM drops warm, ominous rain. The figure of a seventeen year old boy, ALEX BROWNING, packing for a trip, passing the fan... THE BED A Paris guidebook is tossed atop the plane ticket. CAMERA PUSHES IN ON THE BOOK as the fan's breezes flip through the pages. THE TABLE FAN turns, head swiveling away from the bed. TIGHTER - THE GUIDEBOOK PAGES stop flipping, REVEALING A GULLOTINE from the Reign of Terror. As an American passport is dropped beside the guidebook... THE TABLE FAN swivels, returning towards the guidebook on the bed. THE GUIDEBOOK PAGES FLIP. FLIP. FLIP. Alex's faint shadow continues moving about the room. The fan head swivels away, allowing the pages to settle.. -
Federal Register/Vol. 84, No. 127/Tuesday, July 2, 2019
31522 Federal Register / Vol. 84, No. 127 / Tuesday, July 2, 2019 / Proposed Rules special nuclear material waste as compatible with the program of the ARTICLE IX defined in regulations or orders of the Commission for the regulation of This Agreement shall become Commission; materials covered by this Agreement. effective on [date], and shall remain in G. The regulation of the disposal of The State and the Commission agree effect unless and until such time as it is such other byproduct, source, or special to keep each other informed of proposed terminated pursuant to Article VIII. nuclear material as the Commission changes in their respective rules and determines by regulation or order Done at [location] this [date] day of regulations and to provide each other should, because of the hazards or [month], 2019. the opportunity for early and potential hazards thereof, not be so For the Nuclear Regulatory Commission. substantive contribution to the proposed disposed without a license from the Kristine L. Svinicki, changes. Commission; and Chairman. H. The regulation of activities not The State and the Commission agree Done at [location] this [date] day of exempt from Commission regulation as to keep each other informed of events, [month], 2019. stated in 10 CFR part 150. accidents, and licensee performance For the State of Vermont. that may have generic implication or Philip B. Scott, ARTICLE III otherwise be of regulatory interest. Governor. With the exception of those activities [FR Doc. 2019–13453 Filed 7–1–19; 8:45 am] ARTICLE VII identified in Article II, paragraphs D. BILLING CODE 7590–01–P through H., this Agreement may be The Commission and the State agree amended, upon application by the State that it is desirable to provide reciprocal and approval by the Commission to recognition of licenses for the materials DEPARTMENT OF TRANSPORTATION include one or more of the additional listed in Article I licensed by the other activities specified in Article II, Federal Aviation Administration party or by any other Agreement State. -
Maintenance Manual Volume 1 General Information
BHT-205A1-MM-1 MAINTENANCE MANUAL VOLUME 1 GENERAL INFORMATION NOTICE The instructions set forth in this manual, as supplemented or modified by Alert Service Bulletins (ASB) or other directions issued by Bell Helicopter Textron Inc. and Airworthiness Directives (AD) issued by the applicable regulatory agencies, shall be strictly followed. COPYRIGHT NOTICE COPYRIGHT 201 BELL ® HELICOPTER TEXTRON INC. AND BELL HELICOPTER TEXTRON CANADA LTD. ALL RIGHTS RESERVED REISSUE — 7 AUGUST 1990 Export Classification C, ECCN EAR99 REVISION 9 — 5 JULY 2016 BHT-205A1-MM-1 PROPRIETARY RIGHTS NOTICE These data are proprietary to Bell Helicopter Textron Inc. Disclosure, reproduction, or use of these data for any purpose other than helicopter operation or maintenance is forbidden without prior written authorization from Bell Helicopter Textron Inc. DESTINATION CONTROL STATEMENT WARNING — This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25. Additional copies of this publication may be obtained by contacting: Commercial Publication Distribution Center Bell Helicopter Textron Inc. P. O. Box 482 Fort Worth, Texas 76101-0482 PN Rev. 9 5 JUL 2016 Export Classification C, ECCN EAR99 BHT-205A1-MM-1 WARNING THIS MANUAL APPLIES ONLY TO HELICOPTERS AND COMPONENTS MAINTAINED IN ACCORDANCE WITH BELL HELICOPTER TEXTRON (BELL) APPROVED PROCEDURES USING BELL APPROVED PARTS. ALL INSPECTION, REPAIR AND OVERHAUL PROCEDURES PUBLISHED BY BELL, INCLUDING PART RETIREMENT LIFE, ARE BASED SOLELY ON THE USE OF BELL PARTS THAT HAVE BEEN MAINTAINED USING BELL APPROVED DATA.