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CAAM 3 Report
3rd Technical Report On Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards A joint effort of The Federal Aviation Administration and The Aerospace Industries Association March 30, 2017 Questions concerning distribution of this report should be addressed to: Federal Aviation Administration Manager, Engine and Propeller Directorate. TABLE OF CONTENTS Page Table of Contents iii List of Figures v I. Foreword 1 II. Background 1 III. Scope 2 IV. Discussion 3 V. Relationship to Previous CAAM Data 7 VI. General Notes and Comments 8 VII. Fleet Utilization 11 VIII. CAAM3 Team Members 12 IX. Appendices List of Appendices 13 Appendix 1: Standardized Aircraft Event Hazard Levels and Definitions 14 • General Notes Applicable to All Event Hazard Levels 19 • Rationale for Changes in Severity Classifications 19 • Table 1. Historical Comparison of Severity Level Descriptions and Rationale for CAAM3 Changes 21 Appendix 2: Event Definitions 39 Appendix 3: Propulsion System and Auxiliary Power Unit (APU) Related Aircraft Safety Hazards (2001 through 2012) 44 • Uncontained Blade 44 • Uncontained Disk 50 • Uncontained – Other 56 iii • Uncontained – All Parts 62 • High Bypass Comparison by Generation 63 • Relationship Among High Bypass Fleet 64 • Case Rupture 66 • Case Burnthrough 69 • Under-Cowl Fire 72 • Strut/Pylon Fire 76 • Fuel Leak 78 • Engine Separation 82 • Cowl Separation 85 • Propulsion System Malfunction Recognition and Response (PSMRR) 88 • Crew Error 92 • Reverser/Beta Malfunction – In-Flight Deploy 96 • Fuel Tank Rupture/Explosion 99 • Tailpipe Fire 102 • Multiple-Engine Powerloss – Non-Fuel 107 • Multiple-Engine Powerloss – Fuel-Related 115 • Fatal Human Ingestion / Propeller Contact 120 • IFSD Snapshot by Hazard Level – 2012 Data Only 122 • RTO Snapshot by Hazard Level – 2012 Data Only 123 • APU Events 123 • Turboprop Events 124 • Matrices of Event Counts, Hazard Ratios and Rates 127 • Data Comparison to Previous CAAM Data 135 [ The following datasets which were collected in CAAM2 were not collected in CAAM3. -
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A múlt, a jelen és a jövő fegyverei HHADITECHNIKAADITECHNIKA 2017/3 LI. évfolyam 3. szám Ára 520 Ft A német-holland Boxer harcjármű Éves előfizetési díj 3120 Ft 9 770230 6891081 7 0 0 3 Tartalom A HONVÉDELMI MINISZTÉRIUM FÓKUSZBAN TANULMÁNYOK MŰSZAKI-TUDOMÁNYOS ÉS ISMERETTERJESZTŐ Arany László: A Kínai Népköz- Dr. Mujzer Péter: A Magyar Királyi FOLYÓIRATA társaság űrtevékenysége Honvédség páncélos I. rész 28 szervezeteinek részvétele 2017/3. szám. LI. évfolyam a Szovjetunió elleni hadműveletben, 1941-ben 2 A szerkesztőbizottság elnöke: Dr. Hegedűs Ernő: A Bell/Boeing Varga János altábornagy Honvéd Vezérkar főnök koordinációs helyettes (HVK) V–22 Osprey konvertiplán és a jövő billenőrotoros Elnökhelyettes: Baráth István ddtbk repülőgép-fejlesztései 9 c. egyetemi docens (MH LK pk.) A szerkesztőbizottság tagjai: NEMZETKÖZI Amaczi Viktor ny. mk. alez. (HT) HADITECHNIKAI SZEMLE Dr. Balajti István (NATO) Benkó Imre (HM Currus Zrt.) Ocskay István: A német – Dr. Both Előd nyá. csillagász Amaczi Viktor: Repülőmúzeum Ferenczi Ferenc (HM ArmCom KT Zrt.) holland Boxer kerekes Dr. Gáspár Tibor nyá. mk. vörgy. (MKLE) Virginiában 39 harcjármű I. rész 16 Gecse János ezds. (MH LK) Kelecsényi István: Az A–10-es Dr. Germuska Pál (HM HIM) Dr. habil. Gyarmati József mk. alez. (NKE) csatarepülőgép története Dr. Gyulai Gábor nyá mk. ezds. (NKE KMDI) II. rész 22 Prof. Dr. Ványa László mk. ezds. (NKE) Prof. Dr. Haig Zsolt mk. ezds. (NKE) Prof. Dr. Halász László mk. ezds. (NKE) ŰRTECHNIKA Kaposvári László Zoltán ddtbk. (HVK LCsF csf.) Prof. Dr. Kende György mk. ezds. (NKE) Schuminszky Nándor – Arany Prof. Dr. Kiss Péter (SzIE) László: Kína újabb hordozó- Dr. Koller József ezds. -
A Design Study Me T Rop"Ol Itan Air Transit System
NASA CR 73362 A DESIGN STUDY OF A MET R OP"OL ITAN AIR TRANSIT SYSTEM MAT ir 0 ± 0 49 PREPARED UNDER, NASA-ASEE SUMMER FACULTY FELLOWSHIP PROGRAM ,IN Cq ENGINEERING SYSTEMS DESIGN NASA CONTRACT NSR 05-020-151 p STANFORD UNIVERSITY STANFORD CALIFORNIA CL ceoroducedEAR'C-by thEGHOU AUGUST 1969 for Federal Scientific &Va Tec1nical 2 Information Springfied NASA CR 73362 A DESIGN STUDY OF A METROPOLITAN AIR TRANSIT SYSTEM MAT Prepared under NASA Contract NSR 05-020-151 under the NASA-ASEE Summer Faculty Fellowship Program in Engineering Systems Design, 16 June 29 August, 1969. Faculty Fellows Richard X. Andres ........... ......... ..Parks College Roger R. Bate ....... ...... .."... Air Force Academy Clarence A. Bell ....... ......"Kansas State University Paul D. Cribbins .. .... "North Carolina State University William J. Crochetiere .... .. ........ .Tufts University Charles P. Davis . ... California State Polytechnic College J. Gordon Davis . .... Georgia Institute of Technology Curtis W. Dodd ..... ....... .Southern Illinois University Floyd W. Harris .... ....... .... Kansas State University George G. Hespelt ........ ......... .University of Idaho Ronald P. Jetton ...... ............ .Bradley University Kenneth L. Johnson... .. Milwaukee School of Engineering Marshall H. Kaplan ..... .... Pennsylvania State University Roger A. Keech . .... California State Polytechnic College Richard D. Klafter... .. .. Drexel Institute of Technology Richard S. Marleau ....... ..... .University of Wisconsin Robert W. McLaren ..... ....... University'of Missouri James C. Wambold..... .. Pefinsylvania State University Robert E. Wilson..... ..... Oregon State University •Co-Directors Willi'am Bollay ...... .......... Stanford University John V. Foster ...... ........... .Ames Research Center Program Advisors Alfred E. Andreoli . California State Polytechnic College Dean F. Babcock .... ........ Stanford Research Institute SUDAAR NO. 387 September, 1969 i NOT FILMED. ppECEDING PAGE BLANK CONTENTS Page CHAPTER 1--INTRODUCTION ... -
Thrust Reversal for Turbofan Gas Turbine Engine
(19) TZZ¥Z___T (11) EP 3 091 198 A1 (12) EUROPEAN PATENT APPLICATION (43) Date of publication: (51) Int Cl.: 09.11.2016 Bulletin 2016/45 F01D 21/14 (2006.01) F02K 1/76 (2006.01) F02K 1/72 (2006.01) F02C 9/26 (2006.01) (21) Application number: 16168699.3 (22) Date of filing: 09.05.2016 (84) Designated Contracting States: (71) Applicant: United Technologies Corporation AL AT BE BG CH CY CZ DE DK EE ES FI FR GB Farmington, CT 06032 (US) GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR (72) Inventor: MARCOS, Juan A. Designated Extension States: Middletown, CT Connecticut 06457 (US) BA ME Designated Validation States: (74) Representative: Hull, James Edward MA MD Dehns St. Bride’s House (30) Priority: 08.05.2015 US 201514707500 10 Salisbury Square London EC4Y 8JD (GB) (54) THRUST REVERSAL FOR TURBOFAN GAS TURBINE ENGINE (57) A method of thrust reversal operation according is deployed, and denying the increase in engine power to an example of the present disclosure includes, among when the at least one criterion is met. A system for thrust other things, permitting an increase in engine power reversal is also disclosed. when at least one criterion is not met and a thrust reverser EP 3 091 198 A1 Printed by Jouve, 75001 PARIS (FR) 1 EP 3 091 198 A1 2 Description of a predefined limit when the at least one predetermined criterion is met. BACKGROUND [0010] A gas turbine engine according to an example of the present disclosure includes a fan section including [0001] The present disclosure relates to a thrust re- 5 a fan nacelle arranged at least partially about a fan, an verser, and more particular to thrust reversal operation. -
They Hate US for Our War Crimes: an Argument for US Ratification of the Rome Statute in Light of the Post-Human Rights
UIC Law Review Volume 52 Issue 4 Article 4 2019 They Hate U.S. for Our War Crimes: An Argument for U.S. Ratification of the Rome Statute in Light of the ost-HumanP Rights Era, 53 UIC J. MARSHALL. L. REV. 1011 (2019) Michael Drake Follow this and additional works at: https://repository.law.uic.edu/lawreview Part of the Human Rights Law Commons, International Humanitarian Law Commons, and the Military, War, and Peace Commons Recommended Citation Michael Drake, They Hate U.S. for Our War Crimes: An Argument for U.S. Ratification of the Rome Statute in Light of the Post-Human Rights Era, 53 UIC J. MARSHALL. L. REV. 1011 (2019) https://repository.law.uic.edu/lawreview/vol52/iss4/4 This Comments is brought to you for free and open access by UIC Law Open Access Repository. It has been accepted for inclusion in UIC Law Review by an authorized administrator of UIC Law Open Access Repository. For more information, please contact [email protected]. THEY HATE U.S. FOR OUR WAR CRIMES: AN ARGUMENT FOR U.S. RATIFICATION OF THE ROME STATUTE IN LIGHT OF THE POST-HUMAN RIGHTS ERA MICHAEL DRAKE* I. INTRODUCTION ......................................................... 1012 II. BACKGROUND ............................................................ 1014 A. Continental Disparities ......................................... 1014 1. The International Process in Africa ............... 1014 2. The National Process in the United States of America ............................................................ 1016 B. The Rome Statute, the ICC, and the United States ................................................................................. 1020 1. An International Court to Hold National Leaders Accountable ...................................................... 1020 2. The Aims and Objectives of the Rome Statute .......................................................................... 1021 3. African Bias and U.S. -
79952 Federal Register / Vol
79952 Federal Register / Vol. 75, No. 244 / Tuesday, December 21, 2010 / Rules and Regulations Unsafe Condition DEPARTMENT OF TRANSPORTATION 1601 Lind Avenue, SW., Renton, (d) This AD was prompted by an accident Washington 98057–3356; telephone and the subsequent discovery of cracks in the Federal Aviation Administration (425) 227–1137; fax (425) 227–1149. main rotor blade (blade) spars. We are issuing SUPPLEMENTARY INFORMATION: 14 CFR Part 39 this AD to prevent blade failure and Discussion subsequent loss of control of the helicopter. [Docket No. FAA–2009–0864; Directorate We issued a supplemental notice of Compliance Identifier 2008–NM–202–AD; Amendment 39–16544; AD 2010–26–05] proposed rulemaking (NPRM) to amend (e) Before further flight, unless already 14 CFR part 39 to include an AD that done: RIN 2120–AA64 would apply to the specified products. (1) Revise the Limitations section of the That supplemental NPRM was Airworthiness Directives; DASSAULT Instructions for Continued Airworthiness by published in the Federal Register on AVIATION Model Falcon 10 Airplanes; establishing a life limit of 8,000 hours time- July 27, 2010 (75 FR 43878). That Model FAN JET FALCON, FAN JET in-service (TIS) for each blade set Remove supplemental NPRM proposed to FALCON SERIES C, D, E, F, and G each blade set with 8,000 or more hours TIS. correct an unsafe condition for the Airplanes; Model MYSTERE-FALCON (2) Replace each specified serial-numbered specified products. The MCAI states: 200 Airplanes; Model MYSTERE- blade set with an airworthy blade set in During maintenance on one aircraft, it was accordance with the following table: FALCON 20–C5, 20–D5, 20–E5, and 20– F5 Airplanes; Model FALCON 2000 and discovered that the overpressure capsules were broken on both pressurization valves. -
(12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz Et Al
USOO88695 04B1 (12) United States Patent (10) Patent No.: US 8,869,504 B1 Schwarz et al. (45) Date of Patent: Oct. 28, 2014 (54) GEAREDTURBOFAN ENGINE GEARBOX 5.431,539 A 7/1995 Carvalho ARRANGEMENT 5,443,365 A * 8/1995 Ingling et al. ............. 416, 193A 5,778,659 A 7/1998 Duesler et al. 6,464,401 B1 10/2002 Allard (71) Applicant: United Technologies Corporation, 7,144.221 B2 * 12/2006 Giffin ............................ 416,189 Hartford, CT (US) 8,137,070 B2 * 3/2012 Van Houten ... 416,189 2006.0024162 A1* 2, 2006 Giffin .......... ... 415,208.3 (72) Inventors: Frederick M. Schwarz, Glastonbury, 2007/015.1258 A1* 7/2007 Gaines et al. ................... 60,792 CT (US); William G. Sheridan, 2008/00987.17 A1* 5, 2008 Orlando et al. .... ... 60,226.1 Southington, CT (US) 2010/0218478 A1* 9/2010 Merry et al. .................... 60,205 glon, 2011/0056208 A1 3/2011 Norris et al. .................... 6Of772 2011/O123326 A1 5/2011 DiBenedetto et al. (73) Assignee: United Technologies Corporation, 2012/0110979 A1* 5, 2012 Rosenkrans et al. ......... 60,226.1 Hartford, CT (US) 2012fO251306 A1* 10/2012 Reinhardt et al. ......... 415, 1821 2012fO263579 A1* 10, 2012 Otto et al. .......... ... 415,124.2 (*) Notice: Subject to any disclaimer, the term of this 2012/0291449 A1* 11/2012 Adams et al. ................... 60,793 2012/03 15130 A1 12/2012 Hasel et al. patent is extended or adjusted under 35 2013, OO25257 A1 1/2013 Suciu et all U.S.C. 154(b) by 0 days. 2013/0025258 A1* 1/2013 Merry et al. -
Electrical Generation for More-Electric Aircraft Using Solid Oxide Fuel Cells
PNNL-XXXXX Prepared for the U.S. Department of Energy under Contract DE-AC05-76RL01830 Electrical Generation for More-Electric Aircraft using Solid Oxide Fuel Cells GA Whyatt LA Chick April 2012 PNNL-XXXXX Electrical Generation for More- Electric Aircraft using Solid Oxide Fuel Cells GA Whyatt LA Chick April 2012 Prepared for the U.S. Department of Energy under Contract DE-AC05-76RL01830 Pacific Northwest National Laboratory Richland, Washington 99352 Summary This report examines the potential for Solid-Oxide Fuel Cells (SOFC) to provide electrical generation on-board commercial aircraft. Unlike a turbine-based auxiliary power unit (APU) a solid oxide fuel cell power unit (SOFCPU) would be more efficient than using the main engine generators to generate electricity and would operate continuously during flight. The focus of this study is on more-electric aircraft which minimize bleed air extraction from the engines and instead use electrical power obtained from generators driven by the main engines to satisfy all major loads. The increased electrical generation increases the potential fuel savings obtainable through more efficient electrical generation using a SOFCPU. However, the weight added to the aircraft by the SOFCPU impacts the main engine fuel consumption which reduces the potential fuel savings. To investigate these relationships the Boeing 787-8 was used as a case study. The potential performance of the SOFCPU was determined by coupling flowsheet modeling using ChemCAD software with a stack performance algorithm. For a given stack operating condition (cell voltage, anode utilization, stack pressure, target cell exit temperature), ChemCAD software was used to determine the cathode air rate to provide stack thermal balance, the heat exchanger duties, the gross power output for a given fuel rate, the parasitic power for the anode recycle blower and net power obtained from (or required by) the compressor/expander. -
Department of Transportation
Vol. 81 Friday, No. 98 May 20, 2016 Part II Department of Transportation Federal Aviation Administration 14 CFR Part 60 Flight Simulation Training Device Qualification Standards for Extended Envelope and Adverse Weather Event Training Tasks (Correction); Final Rule VerDate Sep<11>2014 18:26 May 19, 2016 Jkt 238001 PO 00000 Frm 00001 Fmt 4717 Sfmt 4717 E:\FR\FM\20MYR2.SGM 20MYR2 mstockstill on DSK3G9T082PROD with RULES2 32016 Federal Register / Vol. 81, No. 98 / Friday, May 20, 2016 / Rules and Regulations DEPARTMENT OF TRANSPORTATION March 30, 2016, make the following corrections: Federal Aviation Administration ■ 1. Correct the table appearing on page 14 CFR Part 60 18240 to read as follows: [Docket No.: FAA–2014–0391; Amdt. No. 60—4] RIN 2120–AK08 Flight Simulation Training Device Qualification Standards for Extended Envelope and Adverse Weather Event Training Tasks Correction 14 CFR PART 60 [CORRECTED] In FR Rule Doc. No. 2016–05860 beginning on page 18178 in the issue of TABLE A1B—TABLE OF TASKS VS. SIMULATOR LEVEL QPS Requirements Information Subjective requirements Simulator Entry No. In order to be qualified at the simulator qualification level indi- levels cated, the simulator must be able to perform at least the Notes tasks associated with that level of qualification A B C D ******* 3. Inflight Maneuvers. ******* 3.b. High Angle of Attack Maneuvers 3.b.1 .......................... Approaches to Stall ................................................................... X X X X 3.b.2 .......................... Full Stall .................................................................................... X X Stall maneuvers at angles of attack above the activation of the stall warn- ing system. Required only for FSTDs qualified to conduct full stall training tasks as indi- cated on the Statement of Qualifica- tion. -
DASSAULT AVIATION Model Falcon 10 Airplanes
43878 Federal Register / Vol. 75, No. 143 / Tuesday, July 27, 2010 / Proposed Rules Applicability New Requirements of This AD: Actions Bulletin SBF100–27–092, dated April 27, (c) This AD applies to Fokker Services B.V. (h) Within 30 months after the effective 2009; and Goodrich Service Bulletin 23100– Model F.28 Mark 0100 airplanes, certificated date of this AD, do the actions specified in 27–29, dated November 14, 2008; for related in any category, all serial numbers. paragraphs (h)(1) and (h)(2) of this AD information. concurrently. Accomplishing the actions of Issued in Renton, Washington, on July 21, Subject both paragraphs (h)(1) and (h)(2) of this AD 2010. (d) Air Transport Association (ATA) of terminates the actions required by paragraph Jeffrey E. Duven, America Code 27: Flight Controls. (g) of this AD. (1) Remove the tie-wrap, P/N MS3367–2– Acting Manager, Transport Airplane Reason 9, from the lower bolts of the horizontal Directorate, Aircraft Certification Service. (e) The mandatory continuing stabilizer control unit, in accordance with the [FR Doc. 2010–18399 Filed 7–26–10; 8:45 am] airworthiness information (MCAI) states: Accomplishment Instructions of Fokker BILLING CODE 4910–13–P Two reports have been received where, Service Bulletin SBF100–27–092, dated April during inspection of the vertical stabilizer of 27, 2009. F28 Mark 0100 aeroplanes, one of the bolts (2) Remove the lower bolts, P/N 23233–1, DEPARTMENT OF TRANSPORTATION that connect the horizontal stabilizer control of the horizontal stabilizer control unit and unit actuator with the dog-links was found install bolts, P/N 23233–3, in accordance Federal Aviation Administration broken (one on the nut side & one on the with the Accomplishment Instructions of Goodrich Service Bulletin 23100–27–29, head side). -
Vol. 86 Friday, No. 42 March 5, 2021 Pages 12799–13148
Vol. 86 Friday, No. 42 March 5, 2021 Pages 12799–13148 OFFICE OF THE FEDERAL REGISTER VerDate Sep 11 2014 22:07 Mar 04, 2021 Jkt 253001 PO 00000 Frm 00001 Fmt 4710 Sfmt 4710 E:\FR\FM\05MRWS.LOC 05MRWS jbell on DSKJLSW7X2PROD with FR_WS II Federal Register / Vol. 86, No. 42 / Friday, March 5, 2021 The FEDERAL REGISTER (ISSN 0097–6326) is published daily, SUBSCRIPTIONS AND COPIES Monday through Friday, except official holidays, by the Office PUBLIC of the Federal Register, National Archives and Records Administration, under the Federal Register Act (44 U.S.C. Ch. 15) Subscriptions: and the regulations of the Administrative Committee of the Federal Paper or fiche 202–512–1800 Register (1 CFR Ch. I). The Superintendent of Documents, U.S. Assistance with public subscriptions 202–512–1806 Government Publishing Office, is the exclusive distributor of the official edition. Periodicals postage is paid at Washington, DC. General online information 202–512–1530; 1–888–293–6498 Single copies/back copies: The FEDERAL REGISTER provides a uniform system for making available to the public regulations and legal notices issued by Paper or fiche 202–512–1800 Federal agencies. These include Presidential proclamations and Assistance with public single copies 1–866–512–1800 Executive Orders, Federal agency documents having general (Toll-Free) applicability and legal effect, documents required to be published FEDERAL AGENCIES by act of Congress, and other Federal agency documents of public Subscriptions: interest. Assistance with Federal agency subscriptions: Documents are on file for public inspection in the Office of the Federal Register the day before they are published, unless the Email [email protected] issuing agency requests earlier filing. -
Avions Civils
SOMMAIRE DU VOLUME I LA CONDUITE DES PROGRAMMES CIVILS AVANT-PROPOS ET REMERCIEMENTS........................................................................... 3 PREFACE.............................................................................................................................. 5 PRESENTATION GENERALE ............................................................................................. 9 CHAPITRE 1 PRESENTATION DE L’ACTIVITE...................................................................................... 11 LE MARCHE DU TRANSPORT AERIEN .................................................................................. 11 Le passager et l’évolution du trafic.......................................................................................... 11 Les compagnies et la flotte d’avions ....................................................................................... 13 LA CONSTRUCTION DES AVIONS CIVILS .............................................................................. 14 Les caractéristiques de l’activité.............................................................................................. 14 La compétition et son évolution............................................................................................... 18 La dimension économique et monétaire ................................................................................. 20 L’ ADMINISTRATION ET SES MISSIONS ................................................................................. 22 La tutelle militaire de