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Bell 429 Product Specifications
BELL 429 SPECIFICATIONS BELL 429 SPECIFICATIONS Publisher’s Notice The information herein is general in nature and may vary with conditions. Individuals using this information must exercise their independent judgment in evaluating product selection and determining product appropriateness for their particular purpose and requirements. For performance data and operating limitations for any specific mission, reference must be made to the approved flight manual. Bell Helicopter Textron Inc. makes no representations or warranties, either expressed or implied, including without limitation any warranties of merchantability or fitness for a particular purpose with respect to the information set forth herein or the product(s) and service(s) to which the information refers. Accordingly, Bell Helicopter Textron Inc. will not be responsible for damages (of any kind or nature, including incidental, direct, indirect, or consequential damages) resulting from the use of or reliance on this information. Bell Helicopter Textron Inc. reserves the right to change product designs and specifications without notice. © 2019 Bell Helicopter Textron Inc. All registered trademarks are the property of their respective owners. FEBRUARY 2019 © 2019 Bell Helicopter Textron Inc. Specifications subject to change without notice. i BELL 429 SPECIFICATIONS Table of Contents Bell 429 ..................................................................................................................................1 Bell 429 Specification Summary (U.S. Units) ........................................................................4 -
Remote ID NPRM Maps out UAS Airspace Integration Plans by Charles Alcock
PUBLICATIONS Vol.49 | No.2 $9.00 FEBRUARY 2020 | ainonline.com « Joby Aviation’s S4 eVTOL aircraft took a leap forward in the race to launch commercial service with a January 15 announcement of $590 million in new investment from a group led by Japanese car maker Toyota. Joby says it will have the piloted S4 flying as part of the Uber Air air taxi network in early adopter cities before the end of 2023, but it will surely take far longer to get clearance for autonomous eVTOL operations. (Full story on page 8) People HAI’s new president takes the reins page 14 Safety 2019 was a bad year for Part 91 page 12 Part 135 FAA has stern words for BlackBird page 22 Remote ID NPRM maps out UAS airspace integration plans by Charles Alcock Stakeholders have until March 2 to com- in planned urban air mobility applications. Read Our SPECIAL REPORT ment on proposed rules intended to provide The final rule resulting from NPRM FAA- a framework for integrating unmanned air- 2019-100 is expected to require remote craft systems (UAS) into the U.S. National identification for the majority of UAS, with Airspace System. On New Year’s Eve, the exceptions to be made for some amateur- EFB Hardware Federal Aviation Administration (FAA) pub- built UAS, aircraft operated by the U.S. gov- When it comes to electronic flight lished its long-awaited notice of proposed ernment, and UAS weighing less than 0.55 bags, (EFBs), most attention focuses on rulemaking (NPRM) for remote identifica- pounds. -
1 Einleitung
User Manual ATOS C Version: 29.01.2002 English translation: 9 August 2002 by Heiner Biesel Please read before flying! Congratulations on your purchase, and welcome to the ATOS world! Your ATOS C is a high performance glider. To fully exploit its capabilities while remaining well within safe limits, you should become thoroughly familiar with the contents of this manual. If you have any questions or need support, do not hesitate to contact the A.I.R. Team. Your A.I.R. Team Version: 01/02 1 1. Transport • By car The carbon fiber D-tube can be damaged by point loading. For safe transport the glider should always be supported by a large padded area. A ladder with several padded steps is one possibility. If the D- tube is supported at only two places, these supports need to be padded at least 4 inches in length, and wide enough to support the full width of the glider. Anything less is likely to result in transport damage, which can seriously reduce the strength of the main spar and the entire D-tube. Do not tie down the glider too tightly, and use wide tubular of flat webbing to minimize point loading. If the glider is likely to get exposed to rain, and especially to salt water, a watertight cover bag is strongly recommended. If the ATOS C gets wet, dry it as quickly as possible to avoid staining the sail, or causing corrosion of the metal parts. Exposure to salt water should always be followed by a thorough rinse in sweet water. -
1/3-Scale Unlimited Aerobatic ARF
TM® WE GET PEOPLE FLYING 1/3-Scale Unlimited Aerobatic ARF INSTRUCTION MANUAL • Superior controllability and aerobatic flight characteristics • Lightweight construction • Designed by veteran TOC competitor Mike McConville • 90% built 1/3-scale ARF • Plug-in wings for easy transport and field assembly Specifications Wingspan: . 97 in (2463.8 mm) Length: . 88.7 in (2253 mm) Wing Area: . 1810 sq in (116.7 sq dm) Weight: . 22.5–25.5 lb (10.2–11.6 kg) Recommended Engines: . 60–80cc Table of Contents Introduction . 4 Warning . 4 Additional Required Equipment . 5 Other Items Needed (not included in the kit) . 6 Tools and Adhesives Needed (not included in the kit) . 6 Additional Items Needed . 6 Contents of Kit . 7 Section 1. Installing the Wing to the Fuselage . 8 Section 2. Installing the Aileron Servos . 9 Section 3. Installing the Aileron Control Horns . 11 Section 4. Hinging and Sealing the Aileron Control Surfaces . 13 Section 5. Installing the Aileron Linkages . 16 Section 6. Installing the Rudder and Elevator Servos . 18 Section 7. Installing the Elevator, Control Horns, and Linkages . 19 Section 8. Installing the Rudder, Control Horns, and Linkages . 22 Section 9. Attaching the Tail Wheel . 24 Section 10. Installing the Landing Gear and Wheelpants . 25 Section 11. Installing the Receiver, Battery, and Fuel Tank . 28 Section 12. Mounting the Engine and Cowl . 30 Section 13. Hatch Assembly . 33 Section 14. Balancing the Model . 34 Section 15. Radio Setup . 34 Section 16. Control Throws . 35 Section 17. Preflight at the Field . 35 Section 18. Setup and Flight Information by Mike McConville . 36 AMA Safety Code . -
Nflight Report: Canadair's Corporate RJ
PILOT REPORT nflight Report: Canadair’s Corporate RJ I A business aircraft designed to make the “corporate commuter” a practical reality. By FRED GEORGE December 1992, Document No. 2404 (9 pages) Stand by for a startling change in the way a business trips are representative of the air travel patterns of large aircraft is justified. Canadair claims its new Corporate U.S. companies that could take advantage of a 24- to- Regional Jet (RJ for short) can challenge the airlines 30-seat corporate shuttle aircraft. head-to-head in a seat-mile cost showdown and win. The seat-mile costs of a 30-seat RJ assume a utiliza- Whatever happened to all those subjective intangi- tion of 1,000 hours per year. While such annual bles we’ve heard for decades? Time-honored terms usage may be modest by airline standards, it repre- such as “value of executive time” “lost opportunity sents a lot of flight hours to a company accustomed to cost,” and “productivity index” are missing from on-demand business aircraft operations. A shuttle Canadair’s RJ marketing materials. That’s because the operation, though, typically might fly two, two-hour company cuts straight to bottom line operating eco- legs per weekday that would add up to 1,000 hours nomics. Canadair salespeople claim a company oper- in a 50 week period. ating a 24- to 30-seat, business-class configured Canadair didn’t cut corners on estimating the costs Corporate RJ will spend less for air transportation on involved with operating the Corporate RJ. The projec- most trips than if it bought coach fare seats on sched- tions cover capital costs in the form of lease payments; uled airlines. -
The «Active Aeroelasticity» Concept – the Main Stages and Prospects of Development
THE «ACTIVE AEROELASTICITY» CONCEPT – THE MAIN STAGES AND PROSPECTS OF DEVELOPMENT 1 G.A. Amiryants, 2 A.V. Grigorev, 3 Y.A. Nayko, 4 S.E. Paryshev, 1 Main scientific researcher, 2 Junior Scientific researcher, 3 Scientific researcher, 4 Head of department Central Aero-hydrodynamic Institute – TsAGI, Russia Keywords: active aeroelasticity, multidisciplinary investigations, elastically scaled model From the very beginning of static aeroelasticity supervision by A.Z. Rekstin and research it’s important part was searching for V.G. Mikeladze. However, the common rational ways of providing airplanes’ safety drawback of these control surfaces too was from aileron reversal and divergence as well as negative influence of structural elasticity on providing weight efficiency and high these surfaces’ effectiveness. aerodynamic performance of airplanes. The studies by Ja.M.. Parchomovsky, G.A. Amiryants, D.D. Evseev, S.Ja. Sirota, One of the most promising directions of aircraft V.A. Tranovich, L.A. Tshai, Ju.F. Jaremchuk design worldwide today is related to the term of performed in 1950-1960 in TsAGI “exploitation of structural elasticity” or the systematically demonstrated the possibilities to “active aerolasticity” concept. The early 1960s increase control surfaces effectiveness (and faced the urgent need to increase stiffness of solving other static aeroelasticity problems) thin low-aspect-ratio wings of supersonic M-50 using “traditional” approaches: rational increase and R-020 airplanes to diminish negative of wing stiffness (by changing wing skin influence of structural elastic deformations on thickness distribution, airfoil thickness, roll control. As it turned out, even with the choosing the position of stiffness axis, wing optimal increase of structural stiffness to solve spar stiffness), variation of position and shape severe aileron reversal problem the increase of of conventional ailerons and rudders, the airframe weight was unacceptable. -
10CAG/10CHG/10CG-2.4Ghz 10-CHANNEL RADIO CONTROL SYSTEM
10CAG/10CHG/10CG-2.4GHz 10-CHANNEL RADIO CONTROL SYSTEM INSTRUCTION MANUAL Technical updates and additional programming examples available at: http://www.futaba-rc.com/faq Entire Contents ©Copyright 2009 1M23N21007 TABLE OF CONTENTS INTRODUCTION ........................................................... 3 Curve, Prog. mixes 5-8 ............................................. 71 Additional Technical Help, Support and Service ........ 3 GYA gyro mixing (GYRO SENSE) ............................... 73 $SSOLFDWLRQ([SRUWDQG0RGL¿FDWLRQ ........................ 4 Other Equipment ....................................................... 74 Meaning of Special Markings ..................................... 5 Safety Precautions (do not operate without reading) .. 5 Introduction to the 10CG ............................................ 7 GLIDER (GLID(1A+1F)(2A+1F)(2A+2F)) FUNCTIONS . 75 &RQWHQWVDQG7HFKQLFDO6SHFL¿FDWLRQV........................ 9 Table of contents........................................................ 75 Accessories ............................................................... 10 Getting Started with a Basic 4-CH Glider ................ 76 Transmitter Controls & GLIDER-SPECIFIC BASIC MENU FUNCTIONS ........ 78 6ZLWFK,GHQWL¿FDWLRQ$VVLJQPHQWV ............................. 11 Model type (PARAMETER submenu) ........................... 78 Charging the Ni-Cd Batteries ................................... 15 MOTOR CUT ................................................................ 79 Stick Adjustments .................................................... -
Wing Construction
68 INCH YAK-54 Instruction Manual Thank you for your purchase of the Extreme Flight RC 68 inch Yak-54. Please take a few moments to read this instruction manual before beginning assembly. We have outlined a fast, clear and easy method to assemble this aircraft and familiarizing yourself with this process will aid in a quick, easy build. Please read the following paragraph before beginning assembly of your aircraft! THIS IS NOT A TOY! Serious injury, destruction of property, or even death may result from the misuse of this product. Extreme Flight RC is providing you, the buyer with a very high quality model aircraft component kit, from which you, the buyer, will assemble a flying model. However it is beyond our control to monitor the finished aircraft you produce. Extreme Flight RC will in no way accept or assume responsibility or liability for damages resulting from the use of this user assembled product. This aircraft should be flown in accordance to the AMA safety code. It is highly recommended that you join the Academy of Model Aeronautics in order to be properly insured, and to operate your model at AMA sanctioned flying fields only. If you are not willing to accept ALL liability for the use of this product, please return it to the place of purchase immediately. Extreme Flight RC, Ltd. guarantees this kit to be free of defects in materials and workmanship for a period of 90 days from the date of purchase. All warranty claims must be accompanied by the original dated receipt. This warranty is extended to the original purchaser of the aircraft kit only. -
R66 Police Brochure
The R66 POLICE HELICOPTER offers law enforcement a reliable, high-performance TURBINE POLICE turbine helicopter that is economical and easy to maintain. R66 HELICOPTER The four-place R66 Police Helicopter meets the latest FAA crashworthiness regula- tions. Its aerodynamic fuselage optimizes airspeed and fuel economy, allowing the helicopter to remain on station for up to three hours. The R66 Police Helicopter comes turn-key equipped with the latest in navigation and surveillance technology. • Wescam MX-10 Infrared Camera • Garmin G500H 1060 TXi PFD/MFD (compatible with optional autopilot) • Garmin GTN 635 Touchscreen GPS/COM • SX-7 Starsun Searchlight System, 25-30 Million Candlepower Searchlight • Two 6-Channel Audio Controllers • Lithium-ion Battery • Fold-Away Color Monitor • Garmin GTX 335 Transponder A wide variety of upgrades and options are available including: searchlight-to-cam- era slaving system, 5-point shoulder harness system (front seats), P/A speaker and siren, LoJack provisions, moving map systems, Garmin Synthetic Vision Technol- ogy, a selection of UHF, VHF, and 800 MHz police radios, SAS/Autopilot, radar altime- ter, air conditioning, and auxiliary fuel tank. Wescam MX-10 Infrared Camera TURBINE POLICE R66 HELICOPTER SPECIFICATIONS Engine Rolls Royce RR300 turbine Horsepower 300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous Maximum Gross Weight 2700 lb (1225 kg) Approximate Empty Weight 1421 lb (644 kg) (including oil, avionics and standard police package) Fuel Capacity (73.6 gal) 493 lb (224 kg) Pilot, Passengers and Cargo 786 lb (357 kg) with Standard Fuel Cruise Speed at Maximum up to 110 kts (127 mph) Gross Weight Maximum Range approx 325 nm (602 km) STANDARD EQUIPMENT (no reserve) • Hydraulic power controls Hover Ceiling IGE over 10,000 ft • Bladder fuel tank at Max. -
Phoenix Supplement
CONSUMER AEROSPACE Phoenix Rocket Launched R/C Aerobatic Glider Assembly and Operation Manual Supplement HIS sheet contains some recent additions to the Phoenix instructions. Please read them before you Tbegin construction of your Phoenix rocket glider. The following three items are very important, and must be done before you fly your Phoenix. Mandatory Additions Trim Rudder Horn Screws OU must trim the screws that Ymount the rudder horn flush with the outside of the nylon plate. If the screws are not trimmed, it is possible for them to hit the L-7 guides on the launcher during lift off. The rudder may be damaged if this happens. The screws may be cut after assembly with a razor saw or a cut off disc in a Moto-Tool. If you use a cut off disc, be very careful to keep the heat generated by the cut off disc from melting the nylon plate. Trim these screws flush with nylon plate Elevator Pushrod Stiffness HERE are 8 pieces of 3/16” square balsa strip provided in the kit. Before you start assembly, examine all T8 pieces. Due to the high speeds encountered during a Phoenix launch, the pushrods need to be both straight and stiff. The stiffest one should be used for the elevator pushrod, and the next stiffest one for rud- der. The remaining pieces are used for the fuselage corner stock. We use the stiffest balsa that we can obtain for the pushrods, but if you feel the pushrods provided in your kit are not stiff enough, please contact us and we will provide substitutes. -
Aviation Week & Space Technology Student Edition
Chinese Aviation Revealed Fly by Wire How Quick a Recovery? U.S./UK Hypersonic Thresher for All $14.95 APRIL 6-19, 2020 REMAKING THE U.S. MARINES Aviation Week Workforce Initiative Supported by: The Wings Club 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. -
Lift-The-Flap How Your Body Works Pdf, Epub, Ebook
LIFT-THE-FLAP HOW YOUR BODY WORKS PDF, EPUB, EBOOK Rosie Dickins | 16 pages | 26 Jun 2019 | Usborne Publishing Ltd | 9781474950732 | English | London, United Kingdom Lift-the-Flap How Your Body Works PDF Book My belly had a new name. Upon completion of checkout, you will receive an email with a link for you to download the file and save to your local device. The health and safety of our patients, visitors and staff remains our top priority. I too think of the flap as my pouch a reminder of when my now 24 and 16 year old where part of my body. I hear everything you are saying. Continue Shopping Proceed to Wish List. Welcome to The Points Guy! Learn More - opens in a new window or tab. Discover what really happens inside you, from breathing and eating to thinking and growing. Good luck Cheers Angie xx. You May Also Like. Ailerons: The Little Wing Ailerons — a commercial aircraft has two — control the movement of the aircraft on its longitudinal axis, causing it to roll left to right. Thank goodness for a true and honest post. Mike Arnot. How am I to get used to this? Oh Dear Mom, I am the mother of 4 babies in 5 years. Breast lift: Also known as mastopexy; surgery to lift the breasts. They are deployed in degrees, as the aircraft descends for landing. PAP Flap The profunda artery perforator PAP flap transfers blood vessels, fat, and skin from your upper inner thigh to restore your breast mound. The donor site for the superior gluteal artery perforator SGAP flap is your upper buttocks.