DOCSLIB.ORG

Version 1.4C

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Version 1.4C Nynja Build manual Version 1.4c 1 Nynja Build Manual 1.4b Figure 1 tube numbering scheme. 2 Nynja Build Manual 1.4b Figure 2 Basic frame (Skyranger). 3 Nynja Build Manual 1.4b Figure 3 uncovered Skyranger frame. 4 Nynja Build Manual 1.4b Figure 4 Uncovered Nynja frame Figure 5 Nynja fuselage with rear fairings removed 5 Nynja Build Manual 1.4b Figure 6 Nynja fuselage with rear fairings removed – rear view Figure 7 simply assemble thus! 6 Nynja Build Manual 1.4b Contents Introduction ............................................................................................................. 10 1.1 How to Build Your Aircraft .................................................................................................... 10 1.2 The BMAA Homebuilt Aircraft System ....................................................................................... 12 1.3 General Assembly Notes ........................................................................................................... 14 1.4 Finish .......................................................................................................................................... 18 1.5 Weight ........................................................................................................................................ 20 2. Forward Fuselage ............................................................................................ 21 2.1 Tube Numbering .................................................................................................................. 21 2.2 Fuselage frame assembly overview ........................................................................................... 23 2.3 Lower Cabin Triangle .................................................................................................................. 25 2.4 Upper Cabin Triangle ................................................................................................................. 30 2.5 Rear Cabin Frame ................................................................................................................ 33 2.6 Rear cabin frame bracing. .................................................................................................... 34 2.7 Engine Supports ................................................................................................................... 37 2.8 Floor ..................................................................................................................................... 46 2.9 Rudder Pedals ..................................................................................................................... 48 2.10 Control Stick Assembly ........................................................................................................ 49 2.11 Finishing the Forward Fuselage ........................................................................................... 52 3 Rear Fuselage .................................................................................................. 54 3.1 Tail End ................................................................................................................................ 54 3.2 Bracing Frame ............................................................................................................................. 56 3.3 Front End.............................................................................................................................. 57 3.4 Fuselage bracing cables ............................................................................................................. 58 3.5 Tailplane Front Mounting ..................................................................................................... 63 3.6 Fuel Tank Support and Flap Handle ........................................................................................... 64 Not Tightening the Bolts and cables! ................................................................................................ 66 4 Undercarriage .................................................................................................. 67 4.1 Wheels ................................................................................................................................. 67 4.2 Main Undercarriage .............................................................................................................. 69 4.3 Nose Gear ................................................................................................................................... 73 4.4 Brakes .................................................................................................................................. 77 5. Tail Surfaces ....................................................................................................... 80 5.1 Tensioning the Rear Fuselage ............................................................................................. 80 5.2 Elevator Trim Tab ................................................................................................................. 81 5.3 Tailplane ...................................................................................................................................... 83 5.4 Rudder .................................................................................................................................. 87 5.5 Control Cables ..................................................................................................................... 90 6 Fitting the Rear Fuselage Fairings ............................................................... 100 6.1 Preparing the rear fuselage fairings ................................................................................... 100 6.2 Fitting the rear fuselage fairings ......................................................................................... 101 7. Engine Installation Rotax 912UL/912ULS .................................................... 105 8. Wings .............................................................................................................. 110 8.1 Wing Frame ........................................................................................................................ 110 8.2 Aileron Horn Assembly ....................................................................................................... 119 8.3 Attaching the Wings to the Fuselage ................................................................................. 121 8.4 Aileron Control Cables ....................................................................................................... 122 8.5 Flaps ................................................................................................................................... 126 8.6 Covering the Wings ............................................................................................................ 128 8.7 Inserting the Battens .......................................................................................................... 135 9. Windscreen Frame and Throttles ................................................................. 138 9.1 Windscreen Frame ............................................................................................................. 138 9.2 Throttles ............................................................................................................................. 143 7 Nynja Build Manual 1.4b 10. Floor pan, firewall and cowlings .................................................................. 147 10.1 Floor pan ............................................................................................................................ 147 10.2 Firewall and scuttle moulding ............................................................................................. 150 10.3 Engine cowlings ................................................................................................................. 153 11. Engine Ancillaries ......................................................................................... 158 11.1 CKT twin outlet exhaust fitting ........................................................................................... 158 11.2 Oil cooling ................................................................................................................................ 160 11.3 Water cooling ..................................................................................................................... 164 12 Fuel System ................................................................................................... 167 12.1 Fuel lines and connections ...................................................................................................... 167 12.2 Engine compartment ............................................................................................................... 168 12.3 Fuel Tanks............................................................................................................................... 169 12.4 Fitting instructions for HADS Optional Mod 33 – Large diameter balance pipe between fuel tanks ................................................................................................................................................ 170 Overview ......................................................................................................................................... 170 Parts: ..............................................................................................................................................
Load more

Recommended publications
  • Garmin Reveals Autoland Feature Rotorcraft Industry Slams Possible by Matt Thurber NYC Helo Ban Page 45
    PUBLICATIONS Vol.50 | No.12 $9.00 DECEMBER 2019 | ainonline.com Flying Short-field landings in the Falcon 8X page 24 Regulations UK Labour calls for bizjet ban page 14 Industry Forecast sees deliveries rise in 2020 page 36 Gratitude for Service Honor flight brings vets to D.C. page 41 Air Transport Lion Air report cites multiple failures page 51 Rotorcraft Garmin reveals Autoland feature Industry slams possible by Matt Thurber NYC helo ban page 45 For the past eight years, Garmin has secretly Mode. The Autoland system is designed to Autoland and how it works, I visited been working on a fascinating new capabil- safely fly an airplane from cruising altitude Garmin’s Olathe, Kansas, headquarters for ity, an autoland function that can rescue an to a suitable runway, then land the airplane, a briefing and demo flight in the M600 with airplane with an incapacitated pilot or save apply brakes, and stop the engine. Autoland flight test pilot and engineer Eric Sargent. a pilot when weather conditions present can even switch on anti-/deicing systems if The project began in 2011 with a Garmin no other safe option. Autoland should soon necessary. engineer testing some algorithms that could receive its first FAA approval, with certifi- Autoland is available for aircraft manu- make an autolanding possible, and in 2014 cation expected shortly in the Piper M600, facturers to incorporate in their airplanes Garmin accomplished a first autolanding in followed by the Cirrus Vision Jet. equipped with Garmin G3000 avionics and a Columbia 400 piston single. In September The Garmin Autoland system is part of autothrottle.
    [Show full text]
  • Recreational Flyer January - February 2010 Elevated: Angus Watt’S Ch-750
    January - February 2010 Recreational Aircraft Association Canada www.raa.ca The Voice of Canadian Amateur Aircraft Builders $6.95 Elevated: Angus Watt's CH-750 Elevated: The original Zenith 701 was designed as an Angus Watt’s Ch-750 ultralight go-anywhere all metal bush plane that could be plans built by anyone with a 4 ft tabletop bending brake and a pair of snips. It was rarely described as a thing of beauty but so well does it fulfill its mission that these planes are found all over the world. They are inexpensive to construct, and because of their leading edge slats they can get in and out of extremely short patches of clear ground. 22 Recreational Flyer January - February 2010 Elevated: Angus Watt’s Ch-750 WITH THE ADVENT of the Light Sport category in and the only part interchangeable with the 701 is the US, Chris Heintz saw the need for an updated the signature Zenith all-flying rudder. Formerly the version, something with a larger cabin, greater skins were all .016” and they are now .020 to handle payload, and the ability to use an array of four the greater mass of the range of possible four stroke stroke engines. The CH 750 was the result and its engines and the 1320 pound gross weight on wheels, lineage is visually apparent but while the new plane 1430 on floats. resembles the 701 it is almost completely different in Chris Heintz correctly surmised that the US construction. CNC fabrication methods have made Light Sport category would be attractive to aging it possible to simplify the design, speed up the con- American pilots who wanted to bargain down to struction, and end up with a larger and faster plane their Sport Pilot category that allows a valid driver’s at only a slight weight penalty.
    [Show full text]
  • DART Brochure
    DART SERIES THE NEXT LEVEL OF VERSATILITY FROM CONCEPT TO PRESENT general information The all-carbon-fiber DART Series, envisioned as an aerobatic (+7/- MAIDEN FLIGHT DART-450 4G) tandem trainer, features centre stick control, ejection seats, a 17 MAY 2016 five-blade MT propeller and a Garmin avionics system. ENGINE VARIANTS ▪ Turboprop engine AI-450 CP (450 SHP) manufactured by Motor Sich for DART-450 ▪ Turboprop engine GE H75-A (550 SHP) manufactured by General Electric for DART-550 KINDS OF OPERATION ▪ VFR (day and night) and IFR ▪ Take-off and landing on paved surfaces or grass surfaces APPLICATIONS Basic to advanced flight training, Aerobatic, Formation, Multi Role STRUCTURE All composite aircraft CFRP (Carbon Fiber Reinforced Polymer). MOCK UP DART-450 From the very beginning, DEC 2015 CERTIFICATION STANDARD Diamond Aircraft knew that the DART series will be something CS/FAR23 1) unmatched on the market and will eliminate old generation CATEGORY trainer from the market for a Aerobatic / Utility (Multi Role) very long period of time. KICK OFF DART-450 ROLL OUT DART-450 MAIDEN FLIGHT DART-550 MAY 2015 APRIL 2016 03 MAY 2018 1) Certification ongoing Page 3 DART FEATURES TANDEM SEAT, CENTRE STICK CONTROL, EJECTION SEATS, TOUCH SCREEN AVIONICS dart FEATURES HOTAS, NVIS CANOPY WITH SUPERIOR LARGEST SURROUND VIEW INTERNAL FUEL TANK CAPACITY IN TRAINER CLASS ENDURANCE: >5.5 HOURS 15’’ CAMERA HATCH FOR MULTI ROLE OPERATION DOUBLE SLOTTED FLAPS FOR MAXIMUM LIFT LOW STALL SPEED SHORT LANDING DISTANCES LEADING EDGE DE - ICE SYSTEM FULL COMPOSITE AIRFRAME ALLOWS FOR SUPERB HARD POINTS AERODYNAMIC DESIGN ROBUST LANDING GEAR FOR UNPAVED SURFACE OPERATION TWO STATIONS PER WING SIDE COMPOSITE 5 BLADE PROPELLER PROVEN HIGH SPEED WING POWERED BY FUEL & COST EFFICIENT TURBINE (WIND TUNNEL TESTED UP TO M0.65) Page 5 DART VARIANTS DART-450 DART-550 Turboprop engine AI-450 CP (450 SHP) manufactured by Motor Turboprop aerobatic engine GE H75-A (550 SHP) manufactured by Sich.
    [Show full text]
  • J-10A Vigorous Dragon - 2008, PLAAF
    J-10A Vigorous Dragon - 2008, PLAAF China Type: Fighter Min Speed: 350 kt Max Speed: 920 kt Commissioned: 2008 Length: 15.5 m Wingspan: 9.7 m Height: 4.8 m Crew: 1 Empty Weight: 9750 kg Max Weight: 19277 kg Max Payload: 4500 kg Propulsion: 1x AL-31F Sensors / EW: - Generic DECM [Average] - (1980s) ECM, DECM, Defensive ECM, Max range: 0 km - China KLJ-3 [Zhemchoug] - (J-10A, Zhuk-M Mod) Radar, Radar, FCR, Air-to-Air, Medium-Range, Max range: 111.1 km - SPO-15LM Beryoza - (J-10A, Zhuk-M Mod) ESM, RWR, Radar Warning Receiver, Max range: 222.2 km Weapons / Loadouts: - PL-8B [Python 3] - (AAM) Guided Weapon. Air Max: 14.8 km. - PL-12 - (2004) Guided Weapon. Air Max: 92.6 km. - 800 liter Drop Tank - Drop Tank. - 1700 liter Drop Tank - Drop Tank. - 57mm Rocket - (Generic) Rocket. Surface Max: 1.9 km. Land Max: 1.9 km. - 90mm Rocket - (Generic) Rocket. Surface Max: 3.7 km. Land Max: 3.7 km. - 250kg GPB - (Generic) Bomb. Surface Max: 1.9 km. Land Max: 1.9 km. - 500kg GPB - (Generic) Bomb. Surface Max: 1.9 km. Land Max: 1.9 km. - LT-2 LGB [LS-500J, 500kg HE] - (China) Guided Weapon. Surface Max: 7.4 km. Land Max: 7.4 km. - K/JDC-01A Blue Sky Pod [FLIR + LRMTS, 12k ft] - (China) Sensor Pod. - PL-8C [Python 3] - (AAM) Guided Weapon. Air Max: 14.8 km. - China Type 200-4 [Durandal Copy] - (1997) Bomb. Land Max: 1.9 km. OVERVIEW: The Chengdu J-10, Nato reporting name Firebird, export designation F-10 Vanguard is a multirole fighter aircraft designed and produced by the People's Republic of China's Chengdu Aircraft Corporation (CAC) for the People's Liberation Army Air Force (PLAAF).
    [Show full text]
  • Aircraft Accident Final Report a 07/18
    AIRCRAFT ACCIDENT FINAL REPORT A 07/18 Air Accident Investigation Bureau (AAIB) Ministry of Transport, Malaysia ________________________________________________________________ Accident involving Rotorcraft Helicopter Robinson R66 Registration 9M-RML at Sultan Abdul Aziz Shah Airport, Subang, Kuala Lumpur on the 15th August 2018 AIR ACCIDENT INVESTIGATION BUREAU (AAIB) MALAYSIA ACCIDENT REPORT NO. : A 07/18 OPERATOR : PRIVATE AIRCRAFT TYPE : ROBINSON R66 NATIONALITY : MALAYSIA REGISTRATION : 9M-RML PLACE OF OCCURRENCE : SULTAN ABDUL AZIZ SHAH AIRPORT, SUBANG, KUALA LUMPUR DATE AND TIME : 15th AUGUST 2018 AT 0758LT This report contains a statement of facts which have been determined up to the time of issue. It must be regarded as tentative, and is subjected to alteration or correction if additional evidence becomes available. This investigation is carried out to determine the circumstances and causes of the accident with a view to the preservation of life and the avoidance of accident in the future: It is not the purpose to apportion blame or liability (Annex 13 to the Chicago Convention and Civil Aviation Regulations 2016). INTRODUCTION The Air Accident Investigation Bureau of Malaysia The Air Accident Investigation Bureau (AAIB) is the air accident and serious incident investigation authority in Malaysia and is responsible to the Minister of Transport. Its mission is to promote aviation safety through the conduct of independent and objective investigations into air accidents and serious incidents. The AAIB conducts the investigations in accordance with Annex 13 to the Chicago Convention and Civil Aviation Regulations of Malaysia 2016. In carrying out the investigations, the AAIB will adhere to ICAO’s stated objective, which is as follows: “The sole objective of the investigation of an accident or incident shall be the prevention of accidents and incidents.
    [Show full text]
  • Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft
    Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft B. van Lierop Technische Universiteit Delft HANDLING QUALITIES CRITERIAFOR TRAINING EFFECTIVENESS ASSESSMENT OFTHE BS115 AIRCRAFT by B. van Lierop in partial fulfillment of the requirements for the degree of Master of Science in Aerospace Engineering at the Delft University of Technology, to be defended publicly on Wednesday August 23, 2017 at 9:30 AM. Supervisor: Ir. J. A. Melkert TU Delft Thesis committee: Dr. Ir. M. F.M. Hoogreef TU Delft Ir. T. J. Mulder TU Delft An electronic version of this thesis is available at http://repository.tudelft.nl/. Thesis Registration Number: 147#17#MT#FPP PREFACE "Man’s flight through life is sustained by the power of his knowledge" Austin Dusty Miller I am proud to present this master thesis, which marks the end of my time as an aerospace engineer- ing student at Delft University of Technology. It would not have been possible to complete this thesis without the support of all the people around me, for which I would like to express my gratitude. First of all I would like to thank Blackshape SpA, and in particular Giuseppe Verde, for providing me with the opportunity to do my thesis work at this wonderful company. Secondly I would like to thank my supervisor Joris Melkert for his guidance, support, and feedback throughout this project. I would also like to thank Maurice Hoogreef and Hans Mulder for being a part of my thesis committee. Special thanks to Paolo Mezzanotte for his never-ending enthusiasm and support throughout both my master thesis and internship.
    [Show full text]
  • PRINCIPLES of FLIGHT SIMULATION Aerospace Series List
    PRINCIPLES OF FLIGHT SIMULATION Aerospace Series List Handbook of Space Technology Ley, Wittmann April 2009 & Hallmann Surrogate Modelling in Engineering Forrester, Sobester August 2008 Design: A Practical Guide & Keane Aircraft Performance Theory and Swatton August 2008 Practice for Pilots Aircraft Systems, 3rd Edition Moir & Seabridge Introduction to Aircraft Aeroelasticity Wright & Cooper December 2007 and Loads Stability and Control of Aircraft Systems Langton September 2006 Military Avionics Systems Moir & Seabridge February 2006 Design and Development of Aircraft Moir & Seabridge June 2004 Systems Aircraft Loading and Structural Layout Howe May 2004 Aircraft Display Systems Jukes December 2003 Civil Avionics Systems Moir & Seabridge December 2002 PRINCIPLES OF FLIGHT SIMULATION David Allerton Department of Automatic Control and Systems Engineering The University of Sheffield A John Wiley and Sons, Ltd., Publication This edition first published 2009 2009, John Wiley & Sons, Ltd Registered office John Wiley & Sons Ltd, The Atrium, Southern Gate, Chichester, West Sussex, PO19 8SQ, United Kingdom For details of our global editorial offices, for customer services and for information about how to apply for permission to reuse the copyright material in this book please see our website at www.wiley.com. The right of the author to be identified as the author of this work has been asserted in accordance with the Copyright, Designs and Patents Act 1988. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, except as permitted by the UK Copyright, Designs and Patents Act 1988, without the prior permission of the publisher.
    [Show full text]
  • CRANFIELD UNIVERSITY Brian P. Lee Pilot and Control System
    CRANFIELD UNIVERSITY Brian P. Lee Pilot and Control System Modelling for Handling Qualities Analysis of Large Transport Aircraft School of Engineering Department of Aerospace Sciences Dynamics, Simulation, and Control Group PhD Thesis Academic Year: 2011 - 2012 Supervisor: M. V. Cook August, 2012 School of Engineering Department of Aerospace Sciences Dynamics, Simulation, and Control Group PhD Thesis Academic Year 2011 - 2012 Brian P. Lee Pilot and Control System Modelling for Handling Qualities Analysis of Large Transport Aircraft Supervisor: M. V. Cook August, 2012 © Cranfield University 2012. All rights reserved. No part of this publication may be reproduced without the written permission of the copyright owner. ABSTRACT The notion of airplane stability and control being a balancing act between stability and control has been around as long as aeronautics. The Wright brothers’ first successful flights were born of the debate, and were successful at least in part because they spent considerable time teaching themselves how to control their otherwise unstable airplane. This thesis covers four aspects of handling for large transport aircraft: large size and the accompanying low frequency dynamics, the way in which lifting surfaces and control system elements are modelled in flight dynamics analyses, the cockpit feel characteristics and details of how pilots interact with them, and the dynamic instability associated with Pilot Induced Oscillations. The dynamics associated with large transport aircraft are reviewed from the perspective of pilot-in-the-loop handling qualities, including the effects of relaxing static stability in pursuit of performance. Areas in which current design requirements are incomplete are highlighted. Issues with modelling of dynamic elements which are between the pilot’s fingers and the airplane response are illuminated and recommendations are made.
    [Show full text]
  • Aviation Week & Space Technology
    STARTS AFTER PAGE 36 20 Twenties Aerospace’s Has Aircraft Leasing Class of 2020 Perfect Storm Gone Too Far? ™ $14.95 MARCH 9-22, 2020 BOEING’S ATTACK CONTENDER Digital Edition Copyright Notice The content contained in this digital edition (“Digital Material”), as well as its selection and arrangement, is owned by Informa. and its affiliated companies, licensors, and suppliers, and is protected by their respective copyright, trademark and other proprietary rights. Upon payment of the subscription price, if applicable, you are hereby authorized to view, download, copy, and print Digital Material solely for your own personal, non-commercial use, provided that by doing any of the foregoing, you acknowledge that (i) you do not and will not acquire any ownership rights of any kind in the Digital Material or any portion thereof, (ii) you must preserve all copyright and other proprietary notices included in any downloaded Digital Material, and (iii) you must comply in all respects with the use restrictions set forth below and in the Informa Privacy Policy and the Informa Terms of Use (the “Use Restrictions”), each of which is hereby incorporated by reference. Any use not in accordance with, and any failure to comply fully with, the Use Restrictions is expressly prohibited by law, and may result in severe civil and criminal penalties. Violators will be prosecuted to the maximum possible extent. You may not modify, publish, license, transmit (including by way of email, facsimile or other electronic means), transfer, sell, reproduce (including by copying or posting on any network computer), create derivative works from, display, store, or in any way exploit, broadcast, disseminate or distribute, in any format or media of any kind, any of the Digital Material, in whole or in part, without the express prior written consent of Informa.
    [Show full text]
  • Publishable Summary
    ARISTOTEL ACPO-GA-2010-266073 2nd Project Periodic Report Publishable summary Project acronym: ARISTOTEL Project full title: Aircraft and Rotorcraft Pilot Couplings – Tools and Techniques for Alleviation and Detection Grant Agreement no.: 266073 Project web site: http://www.aristotel-project.eu/ Project logo: Project coordinator: Prof. Dr. Marilena Pavel Telephone: +31 15 2785374 Fax: +31 15 2789564 E-mail: [email protected] Beneficiaries: Short N. Name Team leader Contact name 1 Technische Universiteit Delft TU Delft Marilena Pavel [email protected] 2 Wytwornia Sprzetu Komunikacy PZL- Jacek Malecki [email protected] Jnego PZL-Swidnik Spolka Akcyjna Swidnik 3 Office National d'Etudes et de ONERA Binh Dang Vu [email protected] Recherches Aerospatiales 4 Politecnico di Milano POLIMI Pierangelo Masarati [email protected] 5 Universita Degli Studi Roma Tre UROMA3 Massimo Gennaretti [email protected] 6 The University of Liverpool UoL Mike Jump [email protected] 7 Stichting Nationaal Lucht- en NLR Verbeek, Marcel [email protected] Ruimtevaartlaboratorium 8 SC Straero SA STRAERO Achim Ionita [email protected] 9 Federal State Unitary Enterprise The TsAGI Larisa Zaichik [email protected] Central Aerohydrodynamic Institute named after Prof. N.E. Zhukovsky 11 European Research and Project Eurice Corinna Hahn [email protected] Office GmbH Page 1 of 5 Project context and objectives Fixed and rotary wing pilots alike are familiar with potential instabilities or with annoying limit cycle oscillations that arise from the effort of controlling aircraft with high response actuation systems. Understanding, predicting and supressing these inadvertent and sustained aircraft oscillations, known as Aircraft (Rotorcraft)-Pilot Couplings (A/RPCs) is a challenging problem for all aerospace community.
    [Show full text]
  • NPA) No 18/2006
    NOTICE OF PROPOSED AMENDMENT (NPA) No 18/2006 DRAFT DECISION OF THE EXECUTIVE DIRECTOR OF THE AGENCY AMENDING DECISION NO. 2005/06/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 12 December 2005 on certification specifications, including airworthiness code and acceptable means of compliance, for large aeroplanes (CS-25) Flight Guidance Systems Page 1 of 125 NPA No 18-2006 TABLE OF CONTENTS. Page A EXPLANATORY NOTE 3 I General 3 II Consultation 3 III Comment Response Document 4 IV Content of the draft decision 4 B DRAFT DECISION CS-25 8 I Proposal 1: amendments to CS.25.1329 8 II Proposal 2: amendments to CS.25.1335 9 III Proposal 3: amendments to AMC 25.1329 10 AMC No.1 to CS 25.1329 10 AMC No.2 to CS 25.1329 82 C APPENDICIES 92 I Original JAA NPA 25F-344 proposals justification 92 II Original JAA NPA 25F-344 Regulatory Impact Assessment 95 III Original JAA NPA 25F-344 Comment Response Document 99 Page 2 of 125 NPA No 18-2006 A EXPLANATORY NOTE I. General 1. The purpose of this Notice of Proposed Amendment (NPA) is to envisage amending Decision 2005/06/R of the Executive Director of 12 December 2005 on Certification Specifications, including airworthiness codes and acceptable means of compliance, for Large Aeroplanes (CS- 25). The scope of this rulemaking activity is outlined in ToR 25.004 and is described in more detail below. 2. The Agency is directly involved in the rule-shaping process. It assists the Commission in its executive tasks by preparing draft regulations, and amendments thereof, for the implementation of the Basic Regulation1 which are adopted as “Opinions” (Article 14(1)).
    [Show full text]
  • English Nlr Tr 83150 L Design Guidelines For
    ORIGINAL: ENGLISH NLR TR 83150 L DESIGN GUIDELINES FOR HANDLIITG QUALITIES OF FUTURE TRANSPORT AIRCRAFT WITH ACTIVE CONTROL TECHNOLOGY by W.P. de Boer, M.F.C. van Gool, C. La Burthe, O.P. Nicholas and D. Schafranek This report contains the provisional findings of an Action Group created by the GARTEUR Flight Mechanics Group of Responsables to study the handling qualities of future actively controlled transport aircraft. The responses of Industry to a questionnaire drawn up by the Action Group are presented. Based on these, present and future manual control piloting tasks are defined. Handling qualities criteria, currently used in the design of transport aircraft are presented. A flight simulator experiment is proposed to establish their applicability to ACT transport aircraft. It is anticipated that useful handling qualities guidelines for the design of those aircraft will be generated.' Prepared under the auspices of the Responsables for Flight Mechanics of the Group for Aeronautical Research and Technology in Europe (GARTEUR). Division: Flight Completed : 840401 Prepared: WCVG/& Ordernumber : 533.002 Approved : "dB/& '&P. : PTP -2- CONTENTS PREFACE LIST OF SYMBOLS AND ACRONYMS 1 INTRODUCTION 2 SUMMARY AND INTERPRETATION OF RESPONSES TO THE QUESTIONNAIRE 2.1 General 2.2 Questions and responses 3 DEFINITION OF PRESENT AND FUTURE MANLJAL CONTROL TASKS 4 EVALUATION OF AVAILABLE ANALYTICAL METHODS DESCRIBING THE PILOT-AIRCRAFT SYSTEM 4.1 General 4.2 Methods available at NLR 4.3 Methods available at RAE 4.4 Methods available at DFVLR 4.5
    [Show full text]