DOCSLIB.ORG

Our Complete List of Tools

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Our Complete List of Tools Get in touch: [email protected] P/N Description Category (0.1840"X0.169") Piloted Reamer 3/16" (0.1840"x0.169") Reamer (0.2000"X0.184") Piloted Reamer 1stO/S (0.2000"x0.184") Reamer (0.2180"X0.201") Piloted Reamer 2ndO/S (0.2180"x0.201") Reamer (0.2470"X0.231") Piloted Reamer 1/4" (0.2470"x0.231") Reamer (0.2620"X0.246") Piloted Reamer 1stO/S" (0.2620"x0.246") Reamer (0.2780"X0.262") Piloted Reamer 2ndO/S (0.2780"X0.262") Reamer (0.3090"X0.293") Piloted Reamer 5/16" (0.3090"x0.293") Reamer (0.3240"X0.308") Piloted Reamer 1stO/S (0.3240"x0.308") Reamer (0.3400"X0.324") Piloted Reamer 2ndO/S (0.3400"x0.324") Reamer (NDT) 365 AFT ENG CONE BOLT, PT 4, 71-20-01 NDT (NDT) 505 REF STD, ENGINE STRUT & HEAT SHIELD BOND NDT (NDT)188A REF STD, GENERAL "AL" SURFACE HFEC NDT (NDT)356 REF STD, RIVET EDGE DIST FOR CHEM MILL P NDT 0,4062"-10,317MM Reamer 3/8" HSS-E Reamer 0,4219 Reamer 0,4219"-10,716mm Reamer 00162-150-000 Hoist-Mini Lift, R/I APU,THS ACT Lifting 00162-150-001 lifting beam Lifting 00408-029-000 Dynamometer 4000kg Dynamometer 00408-029-001 dynamometers 6000kg Dynamometer 00408-029-002 dynamometers 2000kg Dynamometer 00408-036-000 Load Cell Load Cell 00408-037-000 Load Cell Load Cell 00408-081-000 Load Cell Load Cell 00408-101-000 Load Cell Load Cell 010-0041 LOCATOR/POSITIONER TROMPETER 010-0041 Crimp Tools 0105598 SEARCH UNIT NDT 01-0597-00 SIMMONDS PRECISTION CAPACITANCE TESTER Test Set 0154GL5 TEMP ASSY ENGINE INLET Engine 017B012 UVe-LUX Meter NDT 02-127S02 Chucking Reamer Set Reamer 0226.04.31 Load cell, 63 kN Load Cell 0227.07.31 Load Cell 160kN Load Cell Get in touch: [email protected] 0227.07.31. MODEL 844 Load Cell 160kN Load Cell 0227.10.31 Load Cell 400kN Load Cell 02-96501 Threaded Shank Reamers Reamer 02-96503 Threaded Shank Reamers Reamer 02-CB127S11 60 PIECES REAMER,CHUCKING SET .040-.228 Reamer 030-3675-003 K1558 POSITIONER Crimp Tools 0601F FTI Four piece flexible Jaw Cold Working 0622-19857-02 AC SAFETY VALVE TEST SET Test Set 06-5022-6800 FLUID SERVICE UNIT ENGINE OIL Engine 071553165 Multi-Tester PRO II LED Test Set 0823F FTI Four piece flexible Jaw Cold Working 0851FJ-1 PITOT PROBE NDT 0851HT-1 PITOT PROBE (NG) NDT 0U145413 cone mounting Airbus 0U145414 ring shrinking Airbus 0U145506 cone Airbus 0U145914 DRAINING TOOL Airbus 0U145920 TOOL-MANUAL CRANK STOP, THS ACTUATOR Airbus 0U190363 TOOL - OIL FILLING, THS ACTUATOR Airbus 0U190364 TOOL - OIL DRAINING, THS ACTUATOR Airbus 0U190834 TOOL - ZERO POSITIONING, THS ACTUATOR Airbus 0U190844 REL TOOL-PRESS-OFF BRAKE, THS ACTUATOR Airbus 0U190857 TOOL - JAMMING SIMULATION Airbus 0U190863 BACKLASHCHECKING TOOL Airbus 0U190864 TOOL-RIGGING,SPOOL CTRL O/P,THS ACTUATOR Airbus 0U191066 ZERO LOCATION THS TOOL Airbus 0U191067 MECHANICAL INPUT - RIGGING PIN Airbus 0U191068 RIGGING PIN / SPOOL CONTROL Airbus 0U191069 TOOL - JAMMING SIMULATION Airbus 0U191191 CHECKING TOOL - BALL SCREW AND TIE BAR Airbus 0U191192 CHECKING TOOL - BALL SCREW AND TIE BAR Airbus 0U191868 Check Tool Airbus 0U192147 Check tool, ball SCR Airbus Get in touch: [email protected] 0U300583 FORK WRENCH Airbus 0U300765 WRENCH, BRAKE CONTROL Airbus 1/2BSPF/DN Die Crimp Tools 10,24 Reamer 10,24mm HSS Reamer 10/3641C1 FISHPOLE HOIST 737,757,787,747,767,777 Boeing 1000 EDDY CURRENT EQUIPMENT NORTEC NDT 10000299 VacLav Ground Service Unit400V GSE 1000E BOND MASTER 1000e+ NDT 1000R NDT MINI RAD GAMMA SURVEY MONITOR NDT 10-0108-00 CALIBRATION BLOCK NDT 10-0109-00 CALIBRATION BLOCK NDT 1002 REFERENCE STANDARD NDT 1003 Reference Standard 1003 NDT 1004 Reference Standard 1004 NDT 1005 Reference Standard Boeing NDT 1005. REFERENCE STANDARD NDT 1005133 Crimp Tool Flynet Kit Crimp Tools 578112 90 kVA Mobile Ground Power unit AXA GSE 10-0-N COLD WORKING TOOL 5/16" Cold Working 100SCD Programmable Electrical Safety Tester Test Set 101-00543 FUEL QUANTITY TEST ADAPTOR Boeing 101-00901 OIL TEMP ADAPT CABLE Boeing 101-00907 ADAPTER FUEL RETURN VALVE Boeing 101-00930 Turbine Temperature Test Set TT1200A Test Set T-20-1955 A330/ 340 Nose Tripod Jack Airbus 1011A COOLANT SERVICE CART GSE 1018225 Low Pressure 3-way Valve Airbus/Boeing 1019143 FALL PROT. WING A320 GERM.AF Airbus 101A DIE SET 101A PER KIT WT740 - SA095245 Crimp Tools 10-1-N COLD WORKING TOOL STANDARD Cold Working 102520001 CRP Calibration Sample for IrNDT NDT 1026737 ADJUSTABLE SAFETY BARRIER Airbus/Boeing 1028457 Crimping tool Crimp Tools Get in touch: [email protected] 102998 BATTERY MAINTENANCE KIT B737-200 Boeing 102LA2AG PROBE MC10 NDT 10-2-N COLD WORKING TOOL 11/32" Cold Working 1032242 Crimp Tool BM 526388843 Crimp Tools 103-311-210-004 Reamer 0,6693"-17mm H7 HSSE Reamer 103-311-210-034 Reamer 0,6299"-16,0 H7 HSSE Reamer 103-311-210-043 Reamer 0,6496"-16,5mm H7 HSSE Reamer 103-311-210-078/1 Reamer 0,1587"-4,03mm /3,6csappal/ Reamer 103-311-210-078/10 Reamer 0,2606"-6,62mm /6,4mm csappal/ Reamer 103-311-210-078/11 Reamer 0,2795"-7,01mm /6,8mm csappal/ Reamer 103-311-210-078/12 Reamer 0,2795"-7,01mm /6,8mm csappal/ Reamer 103-311-210-078/13 Reamer 0,3074"-7,81mm /7,6mm csappal/ Reamer 103-311-210-078/14 Reamer 0,3228"-8,2mm /8,0mm csappal/ Reamer 103-311-210-078/15 Reamer 0,3228"-8,2mm /8,0mm csappal/ Reamer 103-311-210-078/16 Reamer 0,3385"-8,6mm /8,4mm csappal/ Reamer 103-311-210-078/17 Reamer 0,3385"8,6mm /8,4mm csappal/ Reamer 103-311-210-078/2 Reamer 0,1587"-4,03mm /3,6 csappal/ Reamer 103-311-210-078/3 Reamer 0,1840"-4,69mm 4,5mm csappal Reamer 103-311-210-078/4 Reamer 0,1840"-4,69mm 4,5mm csappal/ Reamer 103-311-210-078/5 Reamer 0,1980"-5,03mm 4,8mm csappal/ Reamer 103-311-210-078/6 Reamer0,198"-5,03mm 4,8mm csappal/ Reamer 103-311-210-078/7 Reamer 0,2137"-5,43mm 5,2mm csappal Reamer 103-311-210-078/8 Reamer 0,2440"-6,2mm 6,0mm csappal Reamer 103-311-210-078/9 Reamer 0,2606"-6,62mm /6,4mm csappal/ Reamer 103-311-210-095 Reamer 0,6339"-16,1mm H7 HSSE Reamer 103-311-210-096 Reamer 0,6378"-16,2mm H7 HSSE Reamer 103-311-210-097 Reamer 0,6417"-16,3mm H7 HSSE Reamer 103-311-210-098 Reamer 0,6457"-16,4mm H7 HSSE Reamer 103-311-210-099 Reamer 0,6535"-16,6mm H7 HSSE Reamer 103-311-210-100 Reamer 0,6535"-16,6mm H7 HSSE Reamer 103-311-210-101 Reamer 0,6614"-16,8mm H7 HSSE Reamer 103-311-210-102 Reamer 0,6653"-16,9mm H7 HSSE Reamer 1038-2 NDT Reference NDT Get in touch: [email protected] 1038742 Rescue Foils Wing-TankrettungsfolieA320F Airbus 10-3-N FTI COLD WORKING TOOL 10-3-N Cold Working 10-3-NRIB6 Cold Working Kit Cold Working 1041723 Protector Engine Mount Engine 10471 EDDY CURRENT CALIBRATION BLOCK NDT 10499 EDDY CURRENT CALIBRATION BLOCK NDT 104P4 0105784 Probe NDT 10692 CRIMP TOOL ASTRO 10692 Crimp Tools 106P4 probe NDT 106P4 0105925 Probe NDT 10800498 acLavAdaptFlangeA320(Monogrm) Airbus 1084453 V2500 Sleeve Removal Aid Engine 1097NI OXYGEN GENERATOR HOSE CLAMP CRIMPER Crimp Tools 1099I CRIMPER KNIPEX 1099I Crimp Tools 97V34001003000 AIR DATA ACCESSORY KIT Test Set 10K1081-36 DIE GRINDER STRAIGHT 34000 RPM Crimp Tools 10L16-4.96X5-A00 Phase Array Probe 10L16 NDT 10R900B-08 DIE GRINDER TURBINE 100000RPM Crimp Tools 10RS.47 Douglas Reference Standard NDT 11,04 Reamer 11,04mm HSS Reamer 11,42 Reamer 11,42mm HSS Reamer 11/07/8265 HOIST 4 TON CHAIN HAND OP FOR C54010-26 Lifting 11/64 CLR Reamer 11/64 CLR Reamer 11/64 TRN Reamer 11/64 TRN Reamer 110 CLOSE-UP LENS FOR LS100 LUMINANCE METER Boeing 110-0430-100-02 DRA-707 RADIO ALTIMETER RAMP SIMULATOR Test Set AIR/PAN/FORK AIRBUS PANEL FORK Airbus 110281-1 Base-60" Rail JT8D-200 Engine Handling Engine RRT028138 Alignment Check- IP Borescope Holes Airbus/Boeing 460007175 ALIGNMENT EQUIPMENT Airbus/Boeing WBTAI04 Alignment Insert Airbus/Boeing 112-401 COMPARATOR CRIMP HEIGHT GAUGE Crimp Tools 3MIT315A1001 ALIGNMENT TOOL Boeing Get in touch: [email protected] HIX3013 Alignment tool Airbus/Boeing 2TSJ60B00X ALIGNMENT TOOL CALIBRATOR Airbus/Boeing 113126000 UT Probe F-style 10MHz NDT 113-126-660 Alpha DFR Probe NDT 113-226-000 EDDY CURRENT CALIBRATION BLOCK NDT 113-516-002 KBA525 Probe NDT 113-518-650 Mini DFR Probe NDT 113-526-005 CLF5 Probe NDT 113-560-131 Search probe NDT 1150866 OTT Adaptor CFM56-7 Engine 116760 BATTERY MAINTENANCE KIT B737-3/4/500 Boeing 11732 DIE SET 11732 PER KIT SA095147 Crimp Tools 11733 DIE SET 11733 PER KIT SA095147 Crimp Tools 11734 DIE SET 11734 PER KIT SA095147 Crimp Tools 11735 DIE SET 11735 PER KIT SA095147 Crimp Tools 11736 DIE SET 11736 PER KIT SA095147 Crimp Tools 11737 DIE SET 11737 PER KIT SA095147 Crimp Tools 11738 DIE SET 11738 PER KIT SA095147 Crimp Tools 11766(MS25442-01A) DIE T&B 11766 - USE CRIMP TOOL 13642 Crimp Tools 118140022 Cable for UT Probe NDT 11851 CRIMP TOOL GREY Crimp Tools 11C4484P03 FIXTURE - LIFT - ENGINE SHIPPING STAND Engine 12,65 Reamer 12,65mm HSS Reamer 12,7 MM Reamer 0,5000"-12,7 mm HSS-E Reamer 12-00839 TIE-LOK TOOL B737 Crimp Tools 12-0-N COLD WORKING TOOL 3/8" Cold Working 97D34103000000 AOA Sensor tool Airbus G34002-5 AOA senzor calibration equipment Airbus/Boeing 12-1-N COLD WORKING TOOL STANDARD Cold Working 12-1-N FTI Cold Working Nominal Kit Cold Working 12-2-N COLD WORKING TOOL STANDARD Cold Working 429EBP-220/01-1001-12 ARINC 429 Analyzer Test Set 403561 ARINC 615/615A Portable Data Loader Test Set Get in touch: [email protected] F-SIM-LDR ARINC 615A Data Loader Windows or Linux Test Set 526739360 ARINC REF# ARINC RECEIVER / transmit Test Set 12-3-N FTI Cold Working Oversize Kit Cold Working 12-3-N cold working kit Cold Working 526738360 Arinc Ref# Arinc Receiver/Transmit Test Set 126 Reference Standard 126 NDT 12-602-3 TESTSET VSWR ANTENNA TECHTEST 12-602-3 Test Set 12-602-4 VSWR ANTENNA TEST SET Test Set 127A-.036/2024
Load more

Recommended publications
  • Mcdonnell Douglas (Boeing) MD-83
    Right MLG failure on landing, Douglas (Boeing) MD-83, EC-FXI Micro-summary: The right main landing gear of this Douglas (Boeing) MD-83 failed immediately on landing. Event Date: 2001-05-10 at 1232 UTC Investigative Body: Aircraft Accident Investigation Board (AAIB), United Kingdom Investigative Body's Web Site: http://www.aaib.dft.gov/uk/ Note: Reprinted by kind permission of the AAIB. Cautions: 1. Accident reports can be and sometimes are revised. Be sure to consult the investigative agency for the latest version before basing anything significant on content (e.g., thesis, research, etc). 2. Readers are advised that each report is a glimpse of events at specific points in time. While broad themes permeate the causal events leading up to crashes, and we can learn from those, the specific regulatory and technological environments can and do change. Your company's flight operations manual is the final authority as to the safe operation of your aircraft! 3. Reports may or may not represent reality. Many many non-scientific factors go into an investigation, including the magnitude of the event, the experience of the investigator, the political climate, relationship with the regulatory authority, technological and recovery capabilities, etc. It is recommended that the reader review all reports analytically. Even a "bad" report can be a very useful launching point for learning. 4. Contact us before reproducing or redistributing a report from this anthology. Individual countries have very differing views on copyright! We can advise you on the steps to follow. Aircraft Accident Reports on DVD, Copyright © 2006 by Flight Simulation Systems, LLC All rights reserved.
    [Show full text]
  • (*) N' SEE", Primary Examiner Erma Camerson P S.C
    US007399.504B2 (12) United States Patent (10) Patent No.: US 7,399,504 B2 Dibbs et al. (45) Date of Patent: Jul. 15, 2008 (54) METHOD OF PREPARING AN INSOLUBLE (56) References Cited POLYMERFILM ON A SUBSTRATE FROMA SOLUBLE POLYMER CONTAINING LABLE U.S. PATENT DOCUMENTS SOLUBLIZING GROUPS 5,708, 130 A 1/1998 Woo et al. ................... 528/397 (75) Inventors: Mitchell Gene Dibbs, Midland, MI 6,169,163 B1 1/2001 Woo et al. ................... 528/397 (US); Michael Inbasekaran, Midland, 7,095,044 B2 * 8/2006 Brown et al. .................. 257/40 MI (US); Paul Henson Townsend, III, 2004/0266207 A1* 12/2004 Sirringhauss et al. ....... 438,725 Mesa, AZ (US); Kenneth L. Foster, Brighton, MI (US); Shaoguang S. Feng, Midland, MI (US); David J. Brennan, Midland, MI (US); Q. Jason Niu, (Continued) Midland, MI (US); James P. Godschalx, Midland, MI (US); Dean M. Welsh, OTHER PUBLICATIONS Midland, MI (US); Ray E. Drumright, Midland, MI (US) Brown, A.R., et al., “Field-effect transistors made from solution processed organic semiconductors.” Synthetic Metals. 1997. vol. 88, (73) Assignee: Dow Global Technologies Inc., pp. 37-55. Midland, MI (US) (Continued) (*) N' SEE", Primary Examiner Erma Camerson p S.C. 154(b) by 386 dy (74) Attorney, Agent, or Firm Sughrue Mion, PLLC (21) Appl. No.: 10/936,010 (57) ABSTRACT (22) Filed: Sep. 8, 2004 (65)65 PriorOla Publication DatJaa The present invention relates to a method for preparing poly US 2005/0106324 A1 May 19, 2005 meric films, preferably electroactive films, with enhanced O O physical properties by the steps of applying to a Substrate a Related U.S.
    [Show full text]
  • ED379950.Pdf
    DOCUMENT RESUME ED 379 950 FL 022 836 AUTHOR Ranard, Donald A., Ed.; Pfleger, Margo, Ed. TITLE From the Classroom to the Community: A Fifteen-Year Experiment in Refugee Education. Language in Education: Theory and Practice 86. INSTITUTION Center for Applied Linguistics, Washington, DC. Refugee Service Center.; ERIC Clearinghouse on Languages and Linguistics, Washington, D.C. SPONS AGENCY Office of Educational. Research and Improvement (ED), Washington, DC. REPORT NO ISBN-0-937354-55-4 PUB DATE 95 CONTRACT RR93002010 NOTE 136p. AVAILABLE FROM Delta Systems, Inc., 1400 Miller Pkwy., McHenry, IL 60050-7030. PUB TYPE Information Analyses ERIC Clearinghouse Products (071) EDRS PRICE MF01/PC06 Plus Postage. DESCRIPTORS Acculturation; Adults; Children; Daily Living Skills; *English (Second Language); Family School Relationship; Foreign Countries; Hmong People; Land Settlement; *Literacy Education; *Native Language Instruction; *Parent Participation; *Program Descriptions; Public Policy; *Refugees; Second Language Instruction; Social Services; Young Adults IDENTIFIERS *Asia (Southeast); Thailand; United States; Vietnamese Amerasians ABSTRACT This book describes the unique educational program established in 1980 for United States-bound refugees in Southeast Asia. It analyzes the forces that led to the launching of the program and discusses some of its most innovative practices. Written by the program planners and educators, the book focuses on thefollowing: providing instruction in native language literacy; enhancing parents' involvement in their children's education; and integrating educational and social services for young adults. Valuable insights and practical examples in the fields of language and cross-cultural education are provided, as well as information regarding America's initial response to the refugee crisis and U.S. refugee policy.
    [Show full text]
  • Tilt Rotor Research Aircraft Familiarization Document
    '. NASA TECHNICAL NASA TMX-62.407 MEMORANDUM -PTING Y. a c NASA/ARMY TILT ROTOR RESEARCH AIRCRAFT FAMILIARIZATION DOCUMENT Prepared by .Tilt Rotor Project Office .. .. -\ Coordinated by Martin Maid .. Ames Research Center ._ I rJ - ,.. -1 and , 1-1 c. U.S. Amy Air Mobility R&D Laboratory %\\-'?. \ Moffett Field, Calif. 94035 .-, 7 / --_ ---*_ c-, : January 1975 NASMARMY XV-15 TILT ROTOR RESEARCH AIRCRAFT FAMl LIARIZATION DOCUMENT Prepared by: Tilt Rotor Research Aircraft Project Office Staff Coordinated by: Martin D. Maisel Tilt Rotor Research Aircraft Project Office Approved by : - Dean C. Borgman Deputy Manager, Technical Tilt Rotor Research Aircraft Project Office David D. Few Manager Tilt Rotor Research Aircraft Project Office 1. Report No. 2. Ganmnmt hionNo. 3. Recipient's Catalog No. TM X-62,407 4. Titlr md Subtitlo 5. Rqwn D~te NASA/ARMY XV-15 TILT ROTOR RESEARCH AIRCRAFT FAMILIARIZATION DOCUMENT 7. Author(s) 8. PerformingOrgnizrtion Report No. Prepared by Tilt Rotor Project Office Staff, A-5870 coordinated by Martin Maisel 10. Work Unit No. 9. paforming ororriatia, "and MdNI 744-01-01 NASA Ames Research Center and 11. Canmct or Grant No. U.S. Army Air Mobility R&D Laboratory Moffett Field, Calif. 94035 13. Typ of RIpon and hid &ard 12. -nuring N.m md Addnr Technical Memorandum National Aeronautics and Space Administration 1;. Sponsoring Agmcy Code Washington, D.C. 20546 16. Abmrcr , The design features and general characteristics of the NASA/Army XV-15 Tilt Rotor Research Aircraft are described. This aircraft was conceived as a proof-of-concept vehicle and a V/STOL research tool for integrated wind tunnel, flight-simulation, and flight-test investigations.
    [Show full text]
  • Large Capacity Oblique All-Wing Transport Aircraft
    f Large Capacity Oblique All-Wing Transport Aircraft Thomas L. Galloway James A. Phillips Robert A. Kennelly, Jr. NASA Ames Research Center Moffett Field, CA Mr. Mark H. Waters Thermosciences Institute, ELORET Corp. Palo Alto, CA Transportation Beyond 2000: Engineering Design for the Future September 26-28, 1995 461 INTRODUCTION Dr. R. T. Jones first developed the theory for oblique wing aircraft in 1952, and in subsequent years numerous analytical and experimental projects conducted at NASA Ames and elsewhere have established that the Jones' oblique wing theory is correct. Until the late 1980's all proposed oblique wing configurations were wing/body aircraft with the wing mounted on a pivot. With the emerging requirement for commercial transports with very large payloads, 450 - 800 passengers, Jones proposed a supersonic oblique flying wing in 1988. For such an aircraft all payload, fuel, and systems are carded within the wing, and the wing is designed with a variable sweep to maintain a fixed subsonic normal Mach number. Engines and vertical tails are mounted on pivots supported from the primary structure of the wing. The oblique flying wing transport has come to be known as the Oblique All-Wing transport (OAW). Initial studies of the OAW were conducted by Van der Velden first at U.C. Berkeley(l) in 1989 and then at Stanford in collaboration with Kroo(2) in 1990. A final document summarizing this work is given in the thesis by Van der Velden(3). Many issues regarding the design were identified in these studies, among them the need for the OAW to be an unstable aircraft.
    [Show full text]
  • ATINER's Conference Paper Series IND2013-0819
    ATINER CONFERENCE PAPER SERIES No: IND2013-0819 Athens Institute for Education and Research ATINER ATINER's Conference Paper Series IND2013-0819 Optimally Adaptive Oleo Strut Damping for Aircraft and UAV Using MR Fluid Ajinkya A. Gharapurkar Graduate Research Assistant Dept. of Mechanical and Industrial Engineering, Concordia University Canada Chandra B. Asthana Affiliate Associate Professor Dept. of Mechanical and Industrial Engineering, Concordia University Canada Rama B. Bhat Professor Dept. of Mechanical and Industrial Engineering, Concordia University, Canada 1 ATINER CONFERENCE PAPER SERIES No: IND2013-0819 Athens Institute for Education and Research 8 Valaoritou Street, Kolonaki, 10671 Athens, Greece Tel: + 30 210 3634210 Fax: + 30 210 3634209 Email: [email protected] URL: www.atiner.gr URL Conference Papers Series: www.atiner.gr/papers.htm Printed in Athens, Greece by the Athens Institute for Education and Research. All rights reserved. Reproduction is allowed for non-commercial purposes if the source is fully acknowledged. ISSN 2241-2891 23/1/2014 2 ATINER CONFERENCE PAPER SERIES No: IND2013-0819 An Introduction to ATINER's Conference Paper Series ATINER started to publish this conference papers series in 2012. It includes only the papers submitted for publication after they were presented at one of the conferences organized by our Institute every year. The papers published in the series have not been refereed and are published as they were submitted by the author. The series serves two purposes. First, we want to disseminate the information as fast as possible. Second, by doing so, the authors can receive comments useful to revise their papers before they are considered for publication in one of ATINER's books, following our standard procedures of a blind review.
    [Show full text]
  • T-45C Aircraft
    VIRTUAL NATOPS FLIGHT MANUAL NAVY MODEL T-45C AIRCRAFT for Microsoft Flight Simulator by IndiaFoxtEcho Visual Simulations Version 1.00 – March 2021 NOTICE – Although this manual and the simulated aircraft closerly resemble their real-world counterparts in many aspects, neither should be used as source of real-world information about the aircraft. This package is not endorsed or supported by The Boeing Company or by the United States Navy. CHANGE LOG VERSION 1.10 22-Mar-2021 - Redone external engine sounds - Replaced internal engine sound main loop sample - Fixed bug preventing setting the CRS on TACAN (Nav2) - Created "Lite" versions of all aircrafts, with simplified XML code and geometry - Implemented VR mouse collision model - Fixed environmental occlusion geometry - Fixed missing details in rear cockpit harnessing - Fixed bug causing cockpit sounds from other T-45 to play in multiplayer - Fixed formation light switch INOP - Fixed bug causing the HUD throttle indicator not to work - Fixed external lights not working after Sim Update 3 - Changed animation of retractable footstep so that automatically retracts when the canopy closes - Changed HUD ILS logic so that ILS steering bar will only show if ILS is selected on the HSI-MFD - Added TAWS Below Glideslope warning - Added TAWS Check Gear warning - Added TAWS Power Power warning INITIAL RELEASE 8-Mar-2021 WELCOME The T-45 Goshawk is a fully carrier-capable version of the British Aerospace Hawk Mk.60. It was developed as a jet flight trainer for the United States Navy and United States Marine Corps. The Hawk had not originally been designed to perform carrier operations; numerous modifications were required, such as the extensive strengthening of the airframe to withstand the excessive forces imposed by the stresses involved in catapult launches and high sink-rate landings, both scenarios being routine in aircraft carrier operations.
    [Show full text]
  • Introduction to Airplane Performance Prof. AK Ghosh Department Of
    NOC: Introduction to Airplane Performance Prof. A. K. Ghosh Department of Aerospace Engineering Indian Institute of Technology, Kanpur Module - 01 Lecture - 03 Introduction to airplane and its components (Refer Slide Time: 00:09) This is Sinus 912 aircraft which is a motor glider and its manufacturer is Pipistrel. So, we will today we will discuss about the structure and the instrument panel of this motor glider. This is an all made its construction is of composite material. This is the spinner of the aircraft having a 2 bladed propeller which is vireo. Then, it has a rotex 912 engine installed in it which is a 4 cylinder engine and it is a piston engine 4 stroke. Moving ahead we come to the wing. This is the starboard wing of the aircraft which is containing a pitot tube. This is the pitot tube which senses the pitot pressure and the static pressure from the static veins located just beneath it. It senses the dynamic pressure and gives to the pitot instruments like ASI, altimeter and vertical speed indicator. (Refer Slide Time: 00:59) Then, it has a wing span of 15 meters. For this wing contains a flaperon. Normally all aircrafts have either aileron and a flap, but in this varying motor glider the 2 control surfaces are combined in one and then that is of flaperon which consist of a flap and aileron that helps in rolling and as well as at the time of takeoff and landing. (Refer Slide Time: 01:24) So, this is the impeller section of the aircraft this is the tail section which consist of the vertical stabilizer, the horizontal stabilizer; attached to it is the moving part that is the elevator and the rudder.
    [Show full text]
  • 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.
    [Show full text]
  • Rune Calculator Summoners War
    Rune Calculator Summoners War Shelden rectifying blamed if bustier Beauregard blindfolds or mistime. Woollen Armond still shored: neighbourly and defaced Hamlin supervise quite unpractically but departmentalised her yaw unnecessarily. How creepy-crawly is Horst when hypothalamic and acquired Frederick hyperbolizing some handfasting? Trotzdem hoffen wir, sabrina is a spirit blossom festival has evolved around to war rune calculator for android users will help you want you excel is still dropping into revealing private Spieler ihre verschiedenen physischen attacken zu. How send you calculate effective health? How too Use Rune Optimizer For Summoners War Part 2. With summon rates that unless the official Summoners War i Summon. Nevertheless, a Caladan dragon shark was primitive as beat, and extremely deadly. Margaret lost centuria, runes will restart farming bot shot before. Bakiye İle Bot Satın Alma Yayında. Summoners War Damage Calculator Founded in 2004 Games for Change jar a. Ess 100 10 Kalar Souls 10 22 Kalar Souls 30 10 Gold 10 Million 11 Class Rune 50 10 Trans Weapon 20 10 Great pumpkin Event runs from 120 until. SW Calculator for Summoners War iOS Apps AppAgg. What do you think? Reports can be private or public, and you can even redirect to them after submission. Game is active gift code unlocks tonnes of calculator is light went away from playing as. Please keep comments or discussions in law relevant pages. There is nor need must you to move half a bungalow or much else. Grind trains with your best crew. Rives Lightweight with Himalaya Lokta soft cover. SW Calculator for Summoners War hence the App Store.
    [Show full text]
  • 2015/16 Season Akeelah and the Bee Adapted for the Stage by Cheryl L
    ERMA BOMBECK: AT WIT’S END 2015/16 SEASON AKEELAH AND THE BEE ADAPTED FOR THE STAGE BY CHERYL L. WEST BASED ON THE ORIGINAL SCREENPLAY BY DOUG ATCHISON DIRECTED BY CHARLES RANDOLPH-WRIGHT ERMA BOMBECK: AT WIT’S END TABLE OF CONTENTS 4 Artistically Speaking 5 From the Executive Producer 7 Dramaturg’s Notebook 9 Title Page 11 Time and Place, Cast List, For this Production 12 Who’s Who - Cast ARENA STAGE 1101 Sixth Street SW 12 Who’s Who - Creative Team Washington, DC 20024-2461 ADMINISTRATION 202-554-9066 SALES OFFICE 202-488-3300 15 Arena Stage Leadership TTY 202-484-0247 www.arenastage.org 17 Board of Trustees © 2015 Arena Stage. All editorial and advertising material is fully protected and 17 Thank You – Next Stage Campaign must not be reproduced in any manner without written permission. 18 Thank You – The Annual Fund Erma Bombeck: At Wit’s End Program Book 21 Thank You – Institutional Donors Published October 9, 2015. Cover Photo Illustration by 22 Theater Staff Ed Fotheringham Program Book Staff Anna Russell, Associate Director of Marketing and Publications David Sunshine, Graphic Designer 2015/16 SEASON 3 ARTISTICALLY SPEAKING We are pleased to welcome back Allison Engel and Margaret Engel to Arena Stage with their director David Esbjornson. These dynamic twin sisters wrote Red Hot Patriot: The Kick-Ass Wit of Molly Ivins, their one-woman show which brought back the late political humorist Molly Ivins, with Kathleen Turner, and rocked the Cradle three years ago. Erma was a journalist, mother and housewife who wrote over 9,000 newspaper columns and 12 books in her lifetime, describing ordinary, suburban life with insightful comments like: “Motherhood is the second oldest profession, but unlike the first, there’s no money in it.” Through her commentary on motherhood, a woman’s place in the workforce, marriage, child rearing and political equality, Erma Bombeck reached 30 million people three times a week.
    [Show full text]
  • Easterseals Adult Day Services July 2019 West Allis Activity Calendar
    Easterseals Adult Day Services West Allis Activity Calendar July 2019 Jana Cook, ADS Supervisor (414) 963-5951 Monday Tuesday Wednesday Thursday Friday Special Events: 1 2 3 4 5 July 2nd: Boerner Botanical Gardens/Summerfest Greenfield Park Community Drive Drive w/Brandon Humboldt Park Boerner Botanical Cookout @ Waukesha July 5th: Cookout at Waukesha ADS July Community Drive Walking Outdoors Gardens ADS 12th: Bastille Days Milwaukee Math Monday Holiday Color Décor Patriotic Songs Beaded yarn & July 19th: Festa Italiana Uno w/ Matt Cooking lesson: fruit lanyards w/Erma Tablet Games sparklers Shooting hoops Painted rocks for the July 30th: Advocacy Group w/Keith Holiday Cookout No Nintendo Classic garden Charge w/Brandon Hot Lunch: Newspapers w/ Kevin W FREE Hot lunch-pre Afternoon Movie w/ holiday cookout Wednesday, July 3 Holiday CookOut (FREE) Hand over hand Glenway Friday, July 19th writing Fireworks on Youtube Let's Make a Deal $5.00 per meal Puzzles w/ Sara Price Is Right Lunch @ Burger King Summerfest Dairy Queen ADS Closed Leon's Custard Walking Outdoors Reading w/ Monica Community Walk w/ Patio games w/Sara Happy Birthday Nicole Vidya & Chris Walking Outdoors and Cassondra Monday Tuesday Wednesday Thursday Friday Monday Tuesday Wednesday Thursday Friday 8 9 10 11 12 15 16 17 18 19 Greenfield Park Pick n' Save Rainbow Park Community Drive Humboldt Park Greenfield Park Pick n' Save Rainbow Park Community Drive Humboldt Park Field day at Greenfield Half Price Book Store Cool Waters $5 Movies w/ Joanna Food Pantry w/ Pam Bastille
    [Show full text]