Wichita State University Libraries Department of Special Collections UNIVERSITY ARCHIVES University of Wichita Engineering Reports (UWER)

Size: px
Start display at page:

Download "Wichita State University Libraries Department of Special Collections UNIVERSITY ARCHIVES University of Wichita Engineering Reports (UWER)"

Transcription

1 Wichita State University Libraries Department of Special Collections UNIVERSITY ARCHIVES University of Wichita Engineering Reports (UWER) Box 1 Index 0-3 List of Publications 005 Turning Radius Tests on Four Cars 007 Center of Gravity Measurements on Four Cars 022 The University of Wichita 7 x 10 Wind Tunnel 023 Two-Dimensional Wind Tunnel Investigation of Boundary Layer Control by Blowing on an NACA Airfoil 027 Full Scale Wind Tunnel Tests on Four 1950 and 1951 Automobiles 032 Wind Tunnel Investigation of a method of Boundary Layer Control as Applied to a Reflection Plane Model at Full Scale Reynolds Number 033 Ruberoid Shingle Test Series (Rep. No. 033, incorrectly assigned to Rep. No. 041) 034 Red Cedar Shingle Test Series (Rep No. 034, incorrectly assigned to Beech Pardel, see 042) 035 U.S. Gypsum Shingle Tests (No. 035 incorrectly assigned to H46 Wing (Beech), see 043) 036 Phillip Care Co. Shingle Tests (Rep. No. 036, incorrectly assigned to H46 Model, see 044) 037 Lloyd A. Fry Roofing Co. Shingle Test 038 CertainTeed Products Corp. Shingle Tests 039 An Analysis of the Effect of Boundary Layer Control on the Performance of an ASW Airplane 046 Wind Tunnel Tests on Asphalt Shingles for Certainteed Products Corporation 053 Calibration Tests on Blowers 071 Suction and Blowing Tests on the Cessna 309 Mockup 074 Development of High-Lift Airfoils by Boundary Layer Control 076 Endurance and Efficiency Test on the Generator and Drive Adaptor for the Cessna 309 Mockup 077 Progress Report on the Beech Sandwich Construction Project 078 Wind Tunnel Tests on Asphalt Shingles 085 A Progress Report on Jet Pump Research 086 Efficiency Test of a Bogue Electric Co. D.C. Motor Box 2

2 103 Wind Tunnel Tests on Asphalt Shingles 111 Wind Tunnel Tests of Asphalt Shingles 112 Wind Tunnel Tests of a Stock Tank Water Heater 113 Wind Tunnel Tests of an Asbestos Cement Chimney Housing 119 Wind Tunnel Tests of Two Asbestos Cement Chimney Housings 128 Performance Tests of an Allison J33A8 Turbojet 130 Wind Tunnel Tests of Two Asbestos-Cement Chimney Housings 131 Performance Test of a Side-Inlet, Steam-To-Air Jet Pump with an Inboard Nozzle 141 Progress Report on an Experimental Wind Tunnel Investigation of Boundary 143 Progress Report on an Experimental Wind Tunnel Investigation of Boundary 146 Summary of Performance Tests of Two Side Inlet, Steam to Air Jet Pumps 150 Progress Report on an Experimental Wind Tunnel Investigation of Boundary 158 Progress Report on an Experimental Wind Tunnel Investigation of Boundary 163A Engineering Research Facilities 165 Progress Report on an Experimental Wind Tunnel Investigation of Boundary 171 Wind Tunnel Tests of an Aluminum Window Awning and Door Hood 172 Wind Tunnel Tests on a Rubber and Wooden Road Barricade 173 Wind Tunnel Tests of Asphalt Shingles 176 Wind Tunnel Tests of Three Elementary Building Forms, Vol Wind Tunnel Tests of Three Elementary Building Forms, Vol 2 Box Wind Tunnel Tests of Three Elementary Building Forms, Vol 2, Section Wind Tunnel Tests of Three Elementary Building Forms, Vol 2, Section Wind Tunnel Tests of Three Elementary Building Forms, Vol 2, Section Tests of a Wind Duct Mockup for a Blowing, Circulation-Control Model 185 Wind Tunnel Tests of Asphalt Shingles Circulation Control Research Wind-Tunnel Tests of a Powered, Blowing-Type, Circulation Control Research Airplane Model Box Circulation Control Research Wind-Tunnel Tests of a Powered, Blowing-Type, Circulation Control Research Airplane Model Circulation Control Research Wind-Tunnel Tests of a Powered, Blowing-Type, Circulation Control Research Airplane Model 196 Qualification Test of a No. 475 Duct Assembly 199 Wind Tunnel Tests of Asphalt Shingles 200 Qualification Test of Three No. 482 Duct Assemblies

3 202 Qualification Test of a No Duct Assembly 203 Qualification Test of a No Duct Assembly 206 Qualification Test of a No Duct Assembly 207 Qualification Test of Three No. 470 Duct Assemblies 208 Qualification Test of Three No. 479 Duct Assemblies 210 Qualification Test of a No Duct Assembly 211 Qualification Test of a No Duct Assembly 212 Qualification Test of Three No. 483 Duct Assemblies Shrouded Propeller Investigations: Shroud and Centerbody Pressure Distributions of a Shrouded Propeller with a 17-Bladed Rotor, Inlet and Exit Stators and Long Chord Shroud Shrouded Propeller Investigations: Shroud and Centerbody Pressure Distributions of a Shrouded Propeller with a 10-Bladed Rotor, Inlet and Exit Stators and Long Chord Shroud Shrouded Propeller Investigations: Wind-Tunnel Tests of a 2-Bladed Shrouded Propeller Model Shrouded Propeller Investigations: Wind-Tunnel Tests of a 4-Bladed Shrouded Propeller Model Having a 0.30 Hub/Tip Diameter Ratio Centerbody Shrouded Propeller Investigations: Wind-Tunnel Tests of a 4-Bladed Shrouded Propeller Model Having a 0.4 Hub/Tip Diameter Ratio Centerbody Shrouded Propeller Investigations: Propeller Tip Clearance Effects Shrouded Propeller Investigations: Wind-Tunnel Tests of a Shrouded Propeller Model with an Elliptical Shroud Exit Shrouded Propeller Investigations: Total and Static Pressure Variations Across the Annulus of a Shrouded Propeller Model 215 Qualification Test of a No Duct Assembly 216 Qualification Test of a No. 489 Duct Assembly 217 Progress Report on Ducted Propeller Investigation 218 Progress Report for Powered Boundary Layer Control Airplane Model RM-9 Investigation 219 Progress Report on Static Slipstream Deflection Tests 224 Progress Report for June 1956 on Evaluation of the Performance, Stability and Control of the Helio Courier Airplane 225 Progress Report for June 1956 on Circulation Control Research 227 Qualification Test of a No. 498 Duct Assembly 228 Qualification Test of a No. 493 Duct Assembly 229 Qualification Test of a No. 486 Duct Assembly 230 Progress Report for June 1956 on Circulation Control Research Box Progress Report for July 1956 on Evaluation of Deflected Slipstream Configurations Utilizing Boundary Layer Control 232 Progress Report for July 1956 on Evaluation of the Performance, Stability and Control of the Helio Courier Airplane

4 Elementary Building Forms, Vol. 1 Elementary Building Forms, Vol. 2, Section 1 Elementary Building Forms, Vol. 2, Section 2 Elementary Building Forms, Vol. 2, Section 3 Elementary Building Forms, Vol. 2, Section 4 Elementary Building Forms, Vol. 2, Section 4 Box Flight Test Program for Evaluation of the Performance, Stability and Control of the Helio Courier Airplane 235 Progress Report for August 1956 on Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control 236 Qualification Test of Three No. 488 Duct Assemblies 237 Progress Report for August on Circulation Control Research 238 Progress Report for August 1956 on Evaluation of the Performance, Stability and Control of the Helio Courier Airplane 240 Structural Test of Two Air Conditioner Cabinets 241 Progress Report for September 1956 on Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control Progress Report for September 1956 on Evaluation of the Performance, Stability and Control of the Helio Courier Airplane 247 Qualification Test of Three No. 484 Duct Assemblies 248 Qualification Test of Three No. 487 Duct Assemblies Progress Report for October 1956 on Evaluation of the Performance, Stability and Control of the Helio Courier Airplane 251 Progress Report for September, October, 1956 on Circulation Control Research 252 Progress Report for November 1956 on Evaluation of the Performance, Stability and Control of the Helio Courier Airplane 253 Engineering Evaluation of Airframe Contractor Reports, Doak Model Qualification Test of a No Duct Assembly 255 Progress Report for November 1956 on Evaluation of Deflected Slipstream Configurations Utilizing Boundary-Layer Control 256 Progress Report for November 1956 on Circulation Control Research 257 Wind Tunnel Tests of a 15% Scale Model of the Vertol Model Wind Tunnel Tests of Asphalt Shingles 260 Progress Report for December 1956 on Evaluation of the Performance, Stability and Control of the Helio Courier Airplance 261 Progress Report for December 1956 on Evaluation of Deflected Slipstream

5 Configurations Utilizing Boundary-Layer Control 262 Wind Tunnel Tests of Model H21-D Inlet Duct 263 th Wind Tunnel Tests of a 1/7 Scale, Powered Model of the Grumman Design Evaluation of the Performance, Stability and Control of the Helio Courier Airplane 265 Qualification Test of Three No Duct Assemblies 266 Qualification Test of Three No Duct Assemblies 267 Qualification Test of Three No Duct Assemblies 268 Evaluation of Deflected Slipstream Configurations Utilizing Boundary Layer Control 269 Structural Test of a Steel Air Conditioner Cabinet 270 Progress Report for December 1956 and January 1957 on Circulation Control Research 273 Two-Dimensional Tests to Determine the Jet Momentum Loss Over the Flap of an NACA Airfoil Equipped with Circulation Control 274 Qualification Test of Three No Duct Assemblies 275 Qualification Test of Three No Duct Assemblies 276 Two-Dimensional Circulation-Control Tests on an NACA Airfoil Equipped with a Plain Flap and a Cusped Suction Slot Entry 277 Qualification Test of Three No Duct Assemblies 278 Qualification Test of Three No Duct Assemblies 281 Qualification Test of Three No Duct Assemblies 282 Progress Report for February and March 1957 on Wind-Tunnel Investigation of Shrouded Propellers Box Wind Tunnel Tests of a Nacelle Fitted with a 16% Scale YC-132 Inlet 286 Progress Report for April 1957 on Wind-Tunnel Investigation of Shrouded Propellers 287 Qualification Test of Three No. 499 Duct Assemblies 288 Progress Report for May 1957 on Wind-Tunnel Investigation of Shrouded Propellers 289 Qualification Test of Three No Duct Assemblies 290 Qualification Test of Three No Duct Assemblies 291 Progress Report for June 1957 Wind-Tunnel Investigation of Shrouded Propellers 292 Wind Tunnel Tests of a 5.5% Scale Reflection Plane Model of a Douglas YC-132 Wing 293 Qualification Test of One No Duct Assembly 294 Contributions to Jet Pump Theory 295 Qualification Test of a No Duct Assembly 296 Qualification Test of a No Duct Assembly 297 Qualification Test of a No Duct Assembly 298 Qualification Test of a No Duct Assembly 299 Revised Qualification Tests on Duct Assemblies, Nos. 499, Rev. A, and 470,

6 Rev. D 300 Progress Report for July 1954 through October 1957 on Wind-Tunnel Investigation of Shrouded Propellers 301 Qualification Test of Glass Fiber Panel Polyester Resin, Low Pressure Laminated Fiber No A Qualification Test of Glass Fiber Panel Polyester Resin, Low Pressure Laminated Fiber No Progress Report for November 1957 on Wind Tunnel Investigation of Shrouded Propellers 303 Wind Tunnel Tests of an NACA 63A216 Airfoil in the 4 x 7 Two-Dimensional Tunnel at the University of Wichita Flight Test Program for the Evaluation of the Performance, Stability and Control of the Dehavilland U-1A Otter Airplane 305 Progress Report for December 1957 on Wind-Tunnel Investigation of Shrouded Propellers 307 Note on Static Performance of Shrouded Propellers 308 Qualification Test of an Engine Fuel Supply Line Assembly Per Mac Specification Control Drawing 309 Qualification Test of an Engine Manifold Line Assembly Per Mac Specification Control Drawing 310 Wind Tunnel Tests of an NACA 64A007.5 Airfoil in the 4 x 7 Two- Dimensional Tunnel at the University of Wichita 311 Two Dimensional Circulation Control Tests of an NACA Airfoil Equipped with a Sealed and Slotted Flap to Determine Jet Momentum Loss Over the Flap Box Supplementary Report: Two Dimensional Circulation Control Tests of an NACA Airfoil Equipped with a Sealed and Slotted Flap to Determine Jet Momentum Loss Over the Flap 312 Qualification Test of Three No. 521 Duct Assemblies 313 Pressure Distribution Tests on Two Flap Configurations of an NACA 63A216 Airfoil Section 314 Power and Qualification Test of an Aeroproducts PGF-38 Air Driven Pump Generator in the 7 x7 Auxiliary Throat of the University of Wichita Wind Tunnel 316 Qualification Test of an Engine Manifold Line Assembly Per Mac Specification Control Drawing No Qualification Test of an Engine Fuel Supply Line Assembly Per Mac Specification Control Drawing No , Change H. 318 Fairchild Model 243 Acceptance Test Report 321 Wind Tunnel Tests of Armorweave Expanded Metal Panels 323 Wind Tunnel Tests of a Service Station canopy 325 Qualification Test of a No Duct Assembly 326 Full Scale Wind Tunnel Tests of Three Landing Gear Configurations 327 Wind Tunnel Tests of an NACA 63A216 Airfoil in the 4 x 7 Two-Dimensional

7 Tunnel at the University of Wichita 328 Qualification Test of a No. 520 Duct Assembly 329 Performance and Endurance Tests on a Variable Speed Hydraulic Drive Unit 331 Progress Report for January 1958 through November 1958 on Wind-Tunnel Investigation of Shrouded Propellers 332 Qualification Test of an Engine Manifold Line Assembly Per Mac Specification Control Drawing No , Change E 335 Wind Tunnel Tests of Aluminum Shingles 336 Qualification Test of a No Duct Assembly 337 Shrouded Propeller Investigations: Aerodynamic Characteristics of a Shroud with Centerbody 338 Wind Tunnel Tests of the 1/th Scale Yao-1 Airplane (Design 134) External Stores Powered Model 339 Wind Tunnel Tests of an NACA 63A216 Airfoil in the 4 x 7 Two-Dimensional Tunnel at the University of Wichita Series IV 344 th Wind Tunnel Tests of a 1/8 Scale Model of the YHC-1B Helicopter 348 Wind Tunnel Tests of the 1/5 Scale Cessna 332 Airplane Powered Model 349 Structural Test of a Heavy Duty Stand Assembly in Accordance with U.S.A.F. Specification MIL-S-26233A Dated 20 January Test on Conveyor Chain Linkage 351 Achieving Consistency in Maximum Performance STOL Landings Ground Effect Machine Investigations: Model Geometry & Mechanics of Testing Ground Effect Machine Investigations: Partial Report on Airflow Patterns on Shell, Base Plate and Ground Board for Two Circular, Annular Jet Models Ground Effect Machine Investigations at the University of Wichita: Final Report Summarizing the Test Program and Data Obtained 353 Qualification Test of a No Duct Assembly Box Wind Tunnel Tests of an Aerial Platform, Vol Wind Tunnel Tests of an Aerial Platform, Vol Wind Tunnel Tests of an Aerial Platform, Vol Qualification Test of a No Duct Assembly 357 Control of Ground Effect Machines by External, Supercirculation Control Surfaces: Basis and Preliminary Evaluation 358 Wind Tunnel Tests of Two-Dimensional and Reflection-Plane Three-Dimensional Model Equipped with Standard and Frise Ailerons 360 Vacuum Tests on Two Rubber Oil Return Hoses 361 A Wind Tunnel Test of a No Humphrey Tension-Sealed Aluminum Double Hung Insulating Window 362 Air Leakage Tests of a Storm Window Manufactured by Western Manufacturing Company Wichita, Kansas 364 Theory and State of the Art of Parametric Amplifiers Final Report on Digital Simulation of Radar

8 365 A Summary Analysis of an STOL Transport 366 Qualification Tests of Hanlon-Wilson Deflector Assembly No Sound Suppression Tests on Humphrey Storm Windows

AERODYNAMICS OF STOL AIRPLANES WITH POWERED HIGH-LIFT SYSTEMS A.V.Petrov

AERODYNAMICS OF STOL AIRPLANES WITH POWERED HIGH-LIFT SYSTEMS A.V.Petrov 28 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES AERODYNAMICS OF STOL AIRPLANES WITH POWERED HIGH-LIFT SYSTEMS A.V.Petrov Central Aerohydrodynamic Institute (TsAGI), Zhukovsky, Moscow Region,

More information

Lip wing Lift at zero speed

Lip wing Lift at zero speed Lip wing Lift at zero speed Dusan Stan, July 2014 http://hypertriangle.com/lipwing.php dusan.stan@hypertriangle.com HyperTriangle 2014 Lip_wing_Lift_at_zero_speed_R2.doc Page 1 of 7 1. Introduction There

More information

Type Acceptance Report

Type Acceptance Report TAR 13/21B/2 Revision 1 WILLIAMS INTERNATIONAL FJ44 Series Aircraft Certification Unit TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. ICAO TYPE CERTIFICATE DETAILS 1 3. TYPE ACCEPTANCE DETAILS

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Aeroplanes Cessna 120 26 November 2015 Notes 1. This AD schedule is applicable to Cessna 120 aircraft manufactured under Federal Aviation Administration (FAA) Type Certificate

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A16EA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A16EA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A16EA Revision 15 True Flight Holdings LLC AA-5, AA-5A, AA-5B AG-5B September 18, 2009 TYPE CERTIFICATE DATA SHEET NO. A16EA This data sheet,

More information

AERONAUTICAL ENGINEERING

AERONAUTICAL ENGINEERING AERONAUTICAL ENGINEERING SHIBIN MOHAMED Asst. Professor Dept. of Mechanical Engineering Al Ameen Engineering College Al- Ameen Engg. College 1 Aerodynamics-Basics These fundamental basics first must be

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 1A Piper Drive Vero Beach, Florida 32960 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1A6 Revision 33 PIPER PA-22 PA-22-108 PA-22-135 PA-22S-135 PA-22-150 PA-22S-150 PA-22-160 PA-22S-160 February 12, 1999 AIRCRAFT SPECIFICATION

More information

AE 452 Aeronautical Engineering Design II Installed Engine Performance. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering March 2016

AE 452 Aeronautical Engineering Design II Installed Engine Performance. Prof. Dr. Serkan Özgen Dept. Aerospace Engineering March 2016 AE 452 Aeronautical Engineering Design II Installed Engine Performance Prof. Dr. Serkan Özgen Dept. Aerospace Engineering March 2016 Propulsion 2 Propulsion F = ma = m V = ρv o S V V o ; thrust, P t =

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1A13 1A13 Revision 27 Revo, Inc. COLONIAL C-1 COLONIAL C-2 LAKE LA-4 LAKE LA-4A LAKE LA-4P LAKE LA-4-200 LAKE

More information

TYPE CERTIFICATE DATA SHEET NO. A8SO

TYPE CERTIFICATE DATA SHEET NO. A8SO DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A8SO Revision 21 (Pitts) S-1S S-1T S-2 S-2A S-2S S-2B S-2C February 15, 2005 TYPE CERTIFICATE DATA SHEET NO. A8SO This data sheet, which is

More information

Hawker Beechcraft Corporation on March 26, 2007

Hawker Beechcraft Corporation on March 26, 2007 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00010WI Revision 8 Hawker Beechcraft 390 March 26, 2007 TYPE CERTIFICATE DATA SHEET NO. A00010WI This data sheet, which is part of Type Certificate

More information

DESIGN OF ACTIVE FLOW CONTROL AT THE WING/PYLON/ENGINE JUNCTION

DESIGN OF ACTIVE FLOW CONTROL AT THE WING/PYLON/ENGINE JUNCTION DESIGN OF ACTIVE FLOW CONTROL AT THE WING/PYLON/ENGINE JUNCTION A. PRACHAŘ, P. VRCHOTA / VZLU A. GEBHARDT, J. WILD / DLR S. WALLIN / KTH D. HUE / ONERA M. MINERVINO / CIRA Coordinator : Martin Wahlich

More information

STRUCTURAL DESIGN AND ANALYSIS OF ELLIPTIC CYCLOCOPTER ROTOR BLADES

STRUCTURAL DESIGN AND ANALYSIS OF ELLIPTIC CYCLOCOPTER ROTOR BLADES 16 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS STRUCTURAL DESIGN AND ANALYSIS OF ELLIPTIC CYCLOCOPTER ROTOR BLADES In Seong Hwang 1, Seung Yong Min 1, Choong Hee Lee 1, Yun Han Lee 1 and Seung Jo

More information

13.3 List of Maintenance Documents for fitted Equipment

13.3 List of Maintenance Documents for fitted Equipment Maintenance Manual Maintenance Manual 13.3 List of Maintenance Documents for fitted Equipment - Engine Manual for the power-plant IAE 50R-AA in its currently valid edition. - Operating and Maintenance

More information

No. CONSUMER PRICE INDICES. Information bulletin. Moscow 2019

No. CONSUMER PRICE INDICES. Information bulletin. Moscow 2019 No. January 209 CONSUMER PRICE INDICES Information bulletin Moscow 209 No. (87) January 209 Consumer prices by group of goods and services (per cent change month-on-month) Table Inflation Core inflation

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A11EA Revision 9 American General Aircraft Holding Co. AA-1 AA-1A AA-1B AA-1C June 7, 1995 TYPE CERTIFICATE DATA SHEET NO. A11EA This data sheet,

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A18SW. San Antonio, Texas

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A18SW. San Antonio, Texas DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A18SW Revision 2 Fairchild Aircraft, Inc. SA227-CC SA227-DC (C-26B) November 14, 1996 TYPE CERTIFICATE DATA SHEET A18SW Type Certificate Holder:

More information

European Aviation Safety Agency

European Aviation Safety Agency European Aviation Safety Agency DECISION N o 2011/006/R OF THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY OF 19 AUGUST 2011 Amending Decision No. 2003/1/RM of the Executive Director of the

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1E8

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1E8 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 1E8 Revision 18 PRATT & WHITNEY AIRCRAFT TURBO WASP JT3D-1 JT3D-3 JT3D-1A JT3D-3B JT3D-1-MC6 JT3D-3C JT3D-1A-MC6 JT3D-7 JT3D-1-MC7 JT3D-7A JT3D-1A-MC7

More information

HCD-135. Industrial Control Damper. Application and Design. Ratings (see page 2 and 3 for specific limitations) Standard Construction.

HCD-135. Industrial Control Damper. Application and Design. Ratings (see page 2 and 3 for specific limitations) Standard Construction. Application and Design Model is a heavy duty industrial control damper with a flanged frame. It is designed to control airflow and provide shut off in HVAC or industrial process control systems. A variety

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET NO. EASA.A.607 for BS 115 Type Certificate Holder BLACKSHAPE S.P.A. Strada Statale 16 KM 841+900 70043 Monopoli (BA) ITALY For models: BS 115 TE.CERT.00048-001 European Aviation

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. T00009LA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. T00009LA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION T00009LA Revision 2 Marsh Aviation Company S-2F3AT November 18, 2002 TYPE CERTIFICATE DATA SHEET NO. T00009LA This data sheet, which is a part

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 5A5

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. 5A5 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 5A5 Revision 30 Cessna (USAF 0-1A) 305A (USAF 0-1E) 305C (USAF 0-1G) 305D 305F April 4, 1994 AIRCRAFT SPECIFICATION NO. 5A5 Type Certificate

More information

ENGINE STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE

ENGINE STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE 24 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES STARTING PERFORMANCE EVALUATION AT STATIC STATE CONDITIONS USING SUPERSONIC AIR INTAKE Author1* Takashi Nishikido Author2* Iwao Murata Author3**

More information

INDIAN INSTITUTE OF TECHNOLOGY KANPUR

INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR Removable, Low Noise, High Speed Tip Shape Tractor Configuration, Cant angle, Low Maintainence Hingelesss, Good Manoeuverability,

More information

TYPE CERTIFICATE DATA SHEET

TYPE CERTIFICATE DATA SHEET TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.512 for Bell 206/407 Series Type Certificate Holder Bell Helicopter Textron Canada Limited 12 800 rue de l Avenir Mirabel, Québec J7J 1R4, Canada For Models: 206A

More information

Active Flow Control A Tool to Improve System Efficiency

Active Flow Control A Tool to Improve System Efficiency Active Flow Control A Tool to Improve System Efficiency Prof. Miki Amitay Mechanical, Aerospace and Nuclear Engineering Rensselaer Polytechnic Institute Troy, NY Special Thanks to: Florine Cannelle, Marcus

More information

Charles H. Zimmerman promoted his Flying Pancake design from 1933 to 1937 while working for the

Charles H. Zimmerman promoted his Flying Pancake design from 1933 to 1937 while working for the Model Number : V-173 Model Name : Flying Pancake Model Type: Proof of Concept, Fighter Charles H. Zimmerman promoted his Flying Pancake design from 1933 to 1937 while working for the National Advisory

More information

European Aviation Safety Agency

European Aviation Safety Agency European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : IM.E.016 Issue : 07 Date : 21 May 2014 Type : Williams International Co. FJ44 Series Engines s FJ44-1A FJ44-1AP FJ44-2A FJ44-2C

More information

Design and Test of Transonic Compressor Rotor with Tandem Cascade

Design and Test of Transonic Compressor Rotor with Tandem Cascade Proceedings of the International Gas Turbine Congress 2003 Tokyo November 2-7, 2003 IGTC2003Tokyo TS-108 Design and Test of Transonic Compressor Rotor with Tandem Cascade Yusuke SAKAI, Akinori MATSUOKA,

More information

McQuay. Central Station Air Handler. LHD, LML, LSL, LWL, LYF, MMM, MSL, MWL Vintage C. Last Manufactured: 1984

McQuay. Central Station Air Handler. LHD, LML, LSL, LWL, LYF, MMM, MSL, MWL Vintage C. Last Manufactured: 1984 Replacement Parts List No. 055222700 Revision D 0/205 McQuay Central Station Air Handler LHD, LML, LSL, LWL, LYF, MMM, MSL, MWL 37-72 Vintage C Last Manufactured: 984 To find your Daikin Applied parts

More information

McQuay. Central Station Air Handlers Low Pressure. LHD, LYF, LSL, LML, LWL Vintage C. LML, LSB Vintage E. Last Manufactured: 1999

McQuay. Central Station Air Handlers Low Pressure. LHD, LYF, LSL, LML, LWL Vintage C. LML, LSB Vintage E. Last Manufactured: 1999 Replacement Parts List No. 055222600 Revision F 11/2011 McQuay Central Station Air Handlers Low Pressure LHD, LYF, LSL, LML, LWL 103-228 Vintage C LML, LSB 106-111 Vintage E Last Manufactured: 1999 To

More information

European Aviation Safety Agency

European Aviation Safety Agency European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : P.104 Issue : 03 Date : 21 December 2011 Type : MT-Propeller Entwicklung GmbH Models MTV-27-1 List of effective Pages: Page 1 2

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-684. Raytehon Aircraft Company on April 15, 1996

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-684. Raytehon Aircraft Company on April 15, 1996 Type Certificate Holder: Type Certicate Holder Record: DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-684 Hawker Beechcraft Corporation 9709 E. Central Wichita,

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A13CE

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A13CE DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A13CE Revision 28 CESSNA 177 177A 177B November 16, 2010 TYPE CERTIFICATE DATA SHEET NO. A13CE WARNING: Use of alcohol-based fuels can cause

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET APM 20 and APM 30 series Type Certificate Holder: BP 1 Manufacturer: BP 1 For variants: APM 20 APM 30 Issue 3 : 23 December

More information

NanoShine Group Corp.

NanoShine Group Corp. Test Report Page: 1 OF 2 NanoShine Group Corp. Product Description: Non-coating Cylinder and Coating Cylinder Product Submitted By: NanoShine Group Corp Date of Sample Received: February 16 th, 2016 Date

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E4WE Revision 34 HONEYWELL (AlliedSignal, Garrett, AiResearch) TPE331-3 TPE331-8 TPE331-10N TPE331-11U TPE331-3U TPE331-8A TPE331-10P TPE331-11UA

More information

DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-649

DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-649 DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION A-649 Revision 1 BEECH D17S (Army UC-43, UC-43B, Navy GB-1, GB-2) SD17S April 15, 1996 AIRCRAFT SPECIFICATION NO. A-649 Manufacturer Raytheon Aircraft

More information

Flow Visualization Tunnel. Owner s Manual. May 2009

Flow Visualization Tunnel. Owner s Manual. May 2009 Flow Visualization Tunnel May 2009 AEROLAB LLC 2009 Contents Introduction... 3 Description... 3 Warnings / Precautions... 4 Tunnel Overview... 5 Main Control Panel... 6 Basic Operation... 8 Auxiliary Blower

More information

NCAA Division I Championship Subdivision Football Recruiting Calendar August 1, 2017, through July 31, 2018

NCAA Division I Championship Subdivision Football Recruiting Calendar August 1, 2017, through July 31, 2018 NCAA Division I Championship Subdivision Football August 1, 2017, through July 31, 2018 (See NCAA Division I Bylaw 13.17.4.2 for Football Calendar Formula) (a) August 1-31, 2017: Dead Period (b) September

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET NO. EASA.IM.A.073 for Beechcraft 390 (PREMIER I and IA) Type Certificate Holder: Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 USA For Models: Model 390 1

More information

PET(S) FIRST & LAST NAME: January 2019

PET(S) FIRST & LAST NAME: January 2019 January 2019 1 2 3 4 5 New Year's Day 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 SPECIAL TE We will not have Doggie available during these dates: *3/29-4/7, 4/19-4/21, 5/24-5/27,

More information

Hoshizaki America, Inc.

Hoshizaki America, Inc. Hoshizaki America, Inc. Modular Flaker Models F-1001MAH(-C)(-22C) F-1001MWH(-C) F-1001MRH(-C) F-1001MLH(-C) A Superior Degree of Reliability PARTS LIST www.hoshizaki.com Number: 71196 Issued: 10-29-2001

More information

Aerodynamic Testing of the A400M at ARA. Ian Burns and Bryan Millard

Aerodynamic Testing of the A400M at ARA. Ian Burns and Bryan Millard Aerodynamic Testing of the A400M at ARA by Ian Burns and Bryan Millard Aircraft Research Association Bedford, England Independent non-profit distributing research and development organisation Set up in

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1E12

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1E12 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. 1E12 1E12 Revision 9 Lycoming Engines IO-320 -A1A-A2A-B1A, -B1B, B1C, -B1E, -B1D, -B2A, -C1A, -C1B, -D1A, -D1C,

More information

ENERCON GmbH ENERCON E-66. page 1 of 6. Design. Dreekamp 5 Tel.: / Aurich Fax: / Design

ENERCON GmbH ENERCON E-66. page 1 of 6. Design. Dreekamp 5 Tel.: / Aurich Fax: / Design 1 of 6 2 of 6 1 MAIN DATAS 1.1 / 18.70 technical data The E-66 / 18.70 is a wind energy converter with variable speed and active blade tilt via pitch drives. The generator is connected directly to the

More information

Civil Aviation Authority Czech Republic

Civil Aviation Authority Czech Republic TCDS 92-01 L 13 SL Vivat Page 1 of 12 Civil Aviation Authority Czech Republic CAA CZ TYPE-CERTIFICATE DATA SHEET L 13 SL Vivat Type Certificate Holder: EVEKTOR, spol. s r.o. Letecká 1008 CZECH REPUBLIC

More information

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET TYPE-CERTIFICATE DATA SHEET No. IM.E.016 issue 10 for FJ44/FJ33 Series Engines Certificate Holder Williams International Co. Walled Lake Michigan 48390-0200 USA For Models: FJ44-1A FJ44-1AP FJ44-2A FJ44-2C

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-804. Continental E165-2 (see Item 106 for optional engines)

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-804. Continental E165-2 (see Item 106 for optional engines) DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-804 Revision 14 LAND-AIR (TEMCO) (LUSCOMBE) 11A 11E April 6, 2005 AIRCRAFT SPECIFICATION NO. A-804 Type Certificate Holder Luscombe Aircraft

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A33EU

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A33EU DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A33EU Revision 2 DASSAULT-BREGUET Falcon 10 September 3, 1987 TYPE CERTIFICATE DATA SHEET NO. A33EU This data sheet which is a part of Type

More information

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC

CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC CIVIL AVIATION AUTHORITY OF THE CZECH REPUBLIC 92-03 Revision 4 MORAVAN AEROPLANES a.s. Model Z 242 L 15.07.2005 TYPE CERTIFICATE DATA SHEET No. 92-03 This data sheet which is a part of Type Certificate

More information

FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A8SW. San Antonio, Texas

FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET A8SW. San Antonio, Texas FEDERAL AVIATION ADMINISTRATION A8SW Revision 21 Fairchild Aircraft SA226-TC SA227-AC (C-26A) SA227-PC SA227-BC (C-26A) February 6, 1997 TYPE CERTIFICATE DATA SHEET A8SW This data sheet, which is part

More information

McQuay. Central Station Air Handler. LHD, LML, LSL, LWL, LYF, MMM, MSL, MWL Vintage D. LML, LSB, MMM, MSB Vintage E

McQuay. Central Station Air Handler. LHD, LML, LSL, LWL, LYF, MMM, MSL, MWL Vintage D. LML, LSB, MMM, MSB Vintage E Replacement Parts List No. 046902100 Revision D 01/2015 McQuay Central Station Air Handler LHD, LML, LSL, LWL, LYF, MMM, MSL, MWL 137-172 Vintage D LML, LSB, MMM, MSB 137-172 Vintage E Last Manufactured:

More information

AIRCRAFT DESIGN SUBSONIC JET TRANSPORT

AIRCRAFT DESIGN SUBSONIC JET TRANSPORT AIRCRAFT DESIGN SUBSONIC JET TRANSPORT Analyzed by: Jin Mok Professor: Dr. R.H. Liebeck Date: June 6, 2014 1 Abstract The purpose of this report is to design the results of a given specification and to

More information

European Aviation Safety Agency

European Aviation Safety Agency TCDS EASA.IM.A.162 Page 1/9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Tupolev TU 204-120CE Manufacturer: Tupolev PSC 17, Tupolev Embankment 111250 Moscow Russia For model: TU 204-120CE

More information

SECTION AXIAL HVAC FANS

SECTION AXIAL HVAC FANS SECTION 233413 - AXIAL HVAC FANS 1. PART 1 GENERAL 1.1. RELATED DOCUMENTS A. Drawings and general provisions of the Contract, including General and Supplementary Conditions and Division 01 Specification

More information

Inventory Levels - All Prices. Inventory Levels - By Price Range

Inventory Levels - All Prices. Inventory Levels - By Price Range Inventory Levels - All Prices Idaho Falls Bonneville Total 3-Mar-17 152 108 260 2-Mar-18 109 78 187-28% Inventory Levels - By Price Range 3-Mar-17 2-Mar-18 0-100,000 41 6 100,001-125,000 19 8 125,001-150,000

More information

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 11 Aircraft Weight Distribution Tables

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 11 Aircraft Weight Distribution Tables Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 01 Chapter 11 Aircraft Weight Distribution Tables No Component group Elements Weight X cg Y cg Z cg 1 Wing 1.1. Wing main structure 1..

More information

Inventory Levels - All Prices. Inventory Levels - By Price Range

Inventory Levels - All Prices. Inventory Levels - By Price Range Inventory Levels - All Prices Idaho Falls Bonneville Total 7-Apr-17 154 111 265 6-Apr-18 113 91 204-23% Inventory Levels - By Price Range 7-Apr-17 6-Apr-18 0-100,000 36 10 100,001-125,000 13 9 125,001-150,000

More information

HCD-230 Industrial Control Damper

HCD-230 Industrial Control Damper Application and Design Model is a heavy duty industrial control damper with a flanged frame. It is designed to control airflow and provide shut off in HVAC or industrial process control systems. A variety

More information

Engine Performance Analysis

Engine Performance Analysis Engine Performance Analysis Introduction The basics of engine performance analysis The parameters and tools used in engine performance analysis Introduction Parametric cycle analysis: Independently selected

More information

1.1 REMOTELY PILOTED AIRCRAFTS

1.1 REMOTELY PILOTED AIRCRAFTS CHAPTER 1 1.1 REMOTELY PILOTED AIRCRAFTS Remotely Piloted aircrafts or RC Aircrafts are small model radiocontrolled airplanes that fly using electric motor, gas powered IC engines or small model jet engines.

More information

CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION

CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION 26 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES CONCEPTUAL DESIGN OF ECOLOGICAL AIRCRAFT FOR COMMUTER AIR TRANSPORTATION Yasuhiro TANI, Tomoe YAYAMA, Jun-Ichiro HASHIMOTO and Shigeru ASO Department

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. TYPE CERTIFICATE DATA SHEET No. A50NM

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. TYPE CERTIFICATE DATA SHEET No. A50NM DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A50NM Dassault Aviation Falcon 2000 December 19, 1995 TYPE CERTIFICATE DATA SHEET No. A50NM This data sheet which is part of Type Certificate

More information

RESEARCH MEMORANDUM NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS. By John A. Ramen and George R. Gray w. WASHINGTON August 7, 1951

RESEARCH MEMORANDUM NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS. By John A. Ramen and George R. Gray w. WASHINGTON August 7, 1951 ! RESEARCH MEMORANDUM TANK NVESTGATON OF THE GRUMMAN JRF-5 ARPLANE WTH A SNGLE HYDRO-SK AND AN'EXTENDED AFTERBODY By John A. Ramen and George R. Gray w Of NATONAL ADVSORY COMMTTEE FOR AERONAUTCS WASHNGTON

More information

RESEARCH MEMORANDUM. fox the. U. S. Air Force

RESEARCH MEMORANDUM. fox the. U. S. Air Force RESEARCH MEMORANDUM fox the U. S. Air Force - NACA RM SL53L24 NATIONAL ADVISORY COMMITTEE FOR AERONAIJTICS RESEARCH "ORANDUM the for U. S. Air Force _.I SPEED-BRAKE INVESTIGATION AT LOW SPEEDOF A l/lo-scale

More information

Enhanced Heat Transfer Surface Development for Exterior Tube Surfaces

Enhanced Heat Transfer Surface Development for Exterior Tube Surfaces 511 A publication of CHEMICAL ENGINEERING TRANSACTIONS VOL. 32, 2013 Chief Editors: Sauro Pierucci, Jiří J. Klemeš Copyright 2013, AIDIC Servizi S.r.l., ISBN 978-88-95608-23-5; ISSN 1974-9791 The Italian

More information

In this lecture... Fixed and variable geometry nozzles Functions of nozzles Thrust vector control Thrust reversal Noise control

In this lecture... Fixed and variable geometry nozzles Functions of nozzles Thrust vector control Thrust reversal Noise control 1 In this lecture... Nozzle: Fixed and variable geometry nozzles Functions of nozzles Thrust vector control Thrust reversal Noise control 2 Exhaust nozzles Nozzles form the exhaust system of gas turbine

More information

Crane Inspection Log. Mailing Address: P.O. Box Tulsa, OK Phone: (918) Fax: (918)

Crane Inspection Log. Mailing Address: P.O. Box Tulsa, OK Phone: (918) Fax: (918) 999978000 Crane Inspection Log Mailing Address: P.O. Box 581510 Tulsa, OK 74158-1510 Physical Address: 4707 North Mingo Road Tulsa, OK 74117-5904 Phone: (918) 836-0463 Fax: (918) 834-5979 www.autocrane.com

More information

Type Acceptance Report

Type Acceptance Report TAR 18/21B/36 ROLLS-ROYCE TRENT 800 Series Aircraft Certification Unit TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. PRODUCT CERTIFICATION DETAILS 2 3. APPLICATION DETAILS AND BACKGROUND

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1 of 17 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET EASA.A.011 Extra Flugzeugproduktions- und Vertriebs GmbH Schwarze Heide 21 D-46569, Hünxe Germany For models: -500 Issue 24

More information

European Aviation Safety Agency

European Aviation Safety Agency TCDS A.075 GROB G 120 Page 1 of 9 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET G 120 Type Certificate Holder: GROB Aircraft AG Manufacturer: GROB Aircraft AG For Models: G 120A G 120A-I

More information

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles Stuart Boland Derek Keen 1 Justin Nelson Brian Taylor Nick Wagner Dr. Thomas Bradley 47 th AIAA/ASME/SAE/ASEE JPC Outline

More information

TYPE CERTIFICATE DATA SHEET 2A8

TYPE CERTIFICATE DATA SHEET 2A8 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET 2A8 2A8 Revision 20 LAVIA S.A. PA-25 PA-25-235 PA-25-260 November 30, 2000 This data sheet which is part of Type

More information

LOG OF REVISIONS. Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual

LOG OF REVISIONS. Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual LOG OF REVISIONS Model G58 Baron (Serials TH-2125 and After) Pilot s Operating Handbook and FAA Approved Airplane Flight Manual Revision A12 - May, 2015 Title Page LOEP LOR Section 1 All Reformatted to

More information

Global VPI Insulated Indirectly Hydrogen-Cooled Turbine Generator for Single-Shaft Type Combined Cycle Power Generation Facilities

Global VPI Insulated Indirectly Hydrogen-Cooled Turbine Generator for Single-Shaft Type Combined Cycle Power Generation Facilities Global VPI Insulated Indirectly Hydrogen-Cooled Turbine Generator for Single-Shaft Type Combined Cycle Power Generation Facilities YAMAZAKI Masaru NIIKURA Hitoshi TANIFUJI Satoshi ABSTRACT Fuji Electric

More information

Inventory Levels - All Prices. Inventory Levels - By Price Range

Inventory Levels - All Prices. Inventory Levels - By Price Range Inventory Levels - All Prices Idaho Falls Bonneville Total 3-Nov-17 198 128 326 2-Nov-18 155 134 289-11% Inventory Levels - By Price Range 3-Nov-17 2-Nov-18 0-100,000 17 11 100,001-125,000 15 9 125,001-150,000

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-725

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION AIRCRAFT SPECIFICATION NO. A-725 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-725 Revision 4 FS 2001 Corp. (Army L-4F) -80 J5B (Army L-4G) J5C March 30, 2001 AIRCRAFT SPECIFICATION NO. A-725 Type Certificate Holder FS

More information

Technological Achievements

Technological Achievements Open Rotor Technological Achievements François MIRVILLE SAFRAN/Snecma July 1, 2014 1/ SUMMARY Open Rotor Architectures and Aircraft Integration Main Technical Objectives Technologies involved Technology

More information

DEVELOPMENT OF A CARGO AIRCRAFT, AN OVERVIEW OF THE PRELIMINARY AERODYNAMIC DESIGN PHASE

DEVELOPMENT OF A CARGO AIRCRAFT, AN OVERVIEW OF THE PRELIMINARY AERODYNAMIC DESIGN PHASE ICAS 2000 CONGRESS DEVELOPMENT OF A CARGO AIRCRAFT, AN OVERVIEW OF THE PRELIMINARY AERODYNAMIC DESIGN PHASE S. Tsach, S. Bauminger, M. Levin, D. Penn and T. Rubin Engineering center Israel Aircraft Industries

More information

Technical Sheet: Beech Baron D55 & E55

Technical Sheet: Beech Baron D55 & E55 BRUCE'S CUSTOM COVERS 18850 Adams Ct Morgan Hill, CA 95037 www.aircraftcovers.com a div. of Aircraft Covers Inc. Phone: 408/738-3959 Toll Free (U.S.): 800/777-6405 Fax: 408/738-2729 Email: bruce@aircraftcovers.com

More information

REPUBLIC OF INDONESIA MINISTRY OF TRANSPORTATION DIRECTORATE GENERAL OF CIVIL AVIATION TYPE CERTIFICATE DATA SHEET NO. A094

REPUBLIC OF INDONESIA MINISTRY OF TRANSPORTATION DIRECTORATE GENERAL OF CIVIL AVIATION TYPE CERTIFICATE DATA SHEET NO. A094 REPUBLIC OF INDONESIA MINISTRY OF TRANSPORTATION DIRECTORATE GENERAL OF CIVIL AVIATION A094 Revision 0 Costruzioni Aeronautiche TECNAM S.r.L P2006T 7 June 2013 TYPE CERTIFICATE DATA SHEET NO. A094 This

More information

Artesis MCM Case Studies. March 2011

Artesis MCM Case Studies. March 2011 Artesis MCM Case Studies March 2011 Case 1 Automotive Company: Automobile Manufacturer A Equipment: Pump Stator Isolation Breakdown Decreasing current unbalance level Case 1 Automotive Company: Automobile

More information

UNITED STATES MILITARY AIRCRAFT by Jos Heyman

UNITED STATES MILITARY AIRCRAFT by Jos Heyman UNITED STATES MILITARY AIRCRAFT by Jos Heyman Air Force CG = Transport Glider (1941-1955) The G series was introduced on 11 June 1948 and continued the CG series. Last update: 1 February 2015 CG-1 Frankfort

More information

European Aviation Safety Agency

European Aviation Safety Agency Page 1/8 European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Cirrus Design SF50 Type Certificate Holder: Cirrus Design Corporation 4515 Taylor Circle Duluth, Minnesota 55811 United States

More information

I - Model CITATION (Transport Category), approved 09 October 1998.

I - Model CITATION (Transport Category), approved 09 October 1998. TYPE CERTIFICATE DATA SHEET Nº EA-9810 Type Certificate Holder: CESSNA AIRCRAFT CO. P. O. Box 7704 Wichita, Kansas, 67277 USA EA-9810-02 Sheet 01 CESSNA CITATION 750 X 10 October 2011 This data sheet,

More information

SR-71 PROPULSION SYSTEM P&W J58 ENGINE (JT11D-20) ONE OF THE BEST JET ENGINES EVER BUILT

SR-71 PROPULSION SYSTEM P&W J58 ENGINE (JT11D-20) ONE OF THE BEST JET ENGINES EVER BUILT SR-71 PROPULSION SYSTEM P&W J58 ENGINE (JT11D-20) PETER LAW ONE OF THE BEST JET ENGINES EVER BUILT Rolls-Royce Milestone Engines Merlin Conway W2B Welland Derwent Trent SR-71 GENERAL CHARACTERISTICS

More information

Introduction to Gas Turbine Engines

Introduction to Gas Turbine Engines Introduction to Gas Turbine Engines Introduction Gas Turbine Engine - Configurations Gas Turbine Engine Gas Generator Compressor is driven by the turbine through an interconnecting shaft Turbine is driven

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Gliders 22 February 2018 Notes: 1. This AD schedule is applicable to the following gliders manufactured by DG FLUGZEUGBAU GmbH (formerly Rolladen-Schneider Flugzeugbau

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Helicopters 25 January 2018 Notes: 1. This AD schedule is applicable to Bell 205A-1 helicopters manufactured under FAA Type Certificate No. H1SW. 2. The Type Certificate

More information

In this lecture... Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay

In this lecture... Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay 1 In this lecture... Intakes for powerplant Transport aircraft Military aircraft 2 Intakes Air intakes form the first component of all air breathing propulsion systems. The word Intake is normally used

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A19SO

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A19SO DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A19SO Revison 14 Piper Aircraft, Inc PA-44-180 PA-44-180T TYPE CERTIFICATE DATA SHEET NO. A19SO October 28, 2014 This data sheet, which is part

More information

Autonomous Mobile Robot Design

Autonomous Mobile Robot Design Autonomous Mobile Robot Design Topic: Propulsion Systems for Robotics Dr. Kostas Alexis (CSE) Propulsion Systems for Robotics How do I move? Understanding propulsion systems is about knowing how a mobile

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-761. P. O. Box 37 Rochester, Wisconsin 53167

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-761. P. O. Box 37 Rochester, Wisconsin 53167 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-761 A-761 Revision 17 American Champion (Bellanca) (Trytek) (Aeronca) 11AC S11AC 11BC S11BC August 1, 1991

More information

Helicopter Noise and Vibration (EU Project "HELINOVI")

Helicopter Noise and Vibration (EU Project HELINOVI) Helicopter Noise and Vibration (EU Project "HELINOVI") Hans-Jürgen Langer, DLR Aeronautics Days 19th/21st June 2006, Vienna Overview Motivation Acoustic Problem Vibration Problem Partners Tools - Configurations

More information

Progress. on the SKYLON Reusable Spaceplane. Alan Bond Managing Director. 7 th Appleton Space Conference. 8 December 2011

Progress. on the SKYLON Reusable Spaceplane. Alan Bond Managing Director. 7 th Appleton Space Conference. 8 December 2011 Progress on the SKYLON Reusable Spaceplane 7 th Appleton Space Conference 8 December 2011 Alan Bond Managing Director SKYLON C1 12 tonnes to LEO 10 tonnes to ISS 200m 3 payload bay 4.6m diameter payload

More information

Airworthiness Directive Schedule

Airworthiness Directive Schedule Airworthiness Directive Schedule Aeroplanes 27 July 2017 Notes 1. This AD schedule is applicable to Piper PA-32 series aircraft manufactured under the following Federal Aviation Administration (FAA) Type

More information

Hoshizaki America, Inc.

Hoshizaki America, Inc. Hoshizaki America, Inc. Modular Flaker Models F-1500MAH(-C) F-1500MWH(-C) F-1500MRH(-C) A Superior Degree of Reliability PARTS LIST www.hoshizaki.com Number: 71223 Issued: 11-11-2004 Revised: 10-8-2014

More information

Research in Internal and External Aerodynamics for the Next Generation of Effcient Aircraft

Research in Internal and External Aerodynamics for the Next Generation of Effcient Aircraft Research in Internal and External Aerodynamics for the Next Generation of Effcient Aircraft Huu Duc Vo Associate Professor Department of Mechanical Engineering École Polytechnique de Montréal 2017 National

More information