2005 HQ Lear 45 Flightcheck 8 02 Lyt.Qxp
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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. -
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. -
Raisbeck Performance Systems for Your King
20142014 RAISBECK PERFORMANCE SYSTEMSRAISBECK FOR PERFORMANCE YOURSYSTEMS KING FOR AIR YOUR LEARJET 31, 35, 36 & 60 Raisbeck’s new Aft Fuselage Locker for the Learjet 60 takes flight. A Message from the CEO Overview of Raisbeck Performance Systems We at Raisbeck Engineering are completing de- velopment and certification of our Lear 60 Aft Fuselage Locker…28 cubic feet of additional baggage space, AND reduced drag at the same time. Certification is scheduled for May 2014, and first production deliveries begin shortly thereafter. We have been working hand-in- hand with Learjet on this program. Over the decades, you and your predeces- James D. Raisbeck, CEO sors have been benefactors of a long line of [email protected] Raisbeck Performance Systems for various ZR LITE Performance System for 30-Series Learjets models of Learjets. The Raisbeck Aft Fuselage Locker for the aisbeck’s ZR LITE Performance Systems provide significantly enhanced performance benefits for In fact, Raisbeck engineers have been de- Learjet 31/35/36 was developed in the mid- RLearjet 31/35/36 models, while providing the highest return on investment available for the veloping systems for the Learjet family since ’90s. More baggage space and less airplane owner and operator. More than 100 Learjet 30 series have now been equipped with Raisbeck’s ZR 1971, and continue drag were the LITE, and the list grows every day. Please contact us if you would like to speak to a satisfied ZR LITE to do so today. This is Raisbeck’s Performance Systems for the results. Learjet Learjet family represents the longest operator and we will provide you with our extensive list of owners. -
BRIZE ASSET RAF Readies for Tactical Transformation As It Welcomes First Airbus Airlifter to New Home
BIG BUSINESS CUTTING KJOS IN RETREAT WHY SIZE STILL Norwegian boss calls on Significant restructuring REALLY MATTERS US critics to cease their under way for US Army IN MIDDLE EAST “slanderous campaigns” aviation after $12 billion MEBA SPECIAL P24 against Irish venture 14 reduction in budget 18 FLIGHT INTERNATIONAL 2-8 DECEMBER 2014 A400M HANDOVER BRIZE ASSET RAF readies for tactical transformation as it welcomes first Airbus airlifter to new home £3.40 49 9 770015 371266 FLIGHT INTERNATIONAL VOLUME 186 NUMBER 5467 2-8 DECEMBER 2014 NEWS BIG BUSINESS CUTTING KJOS IN RETREAT WHY SIZE STILL Norwegian boss calls on Significant restructuring REALLY MATTERS US critics to cease their under way for US Army IN MIDDLE EAST “slanderous campaigns” aviation after $12 billion MEBA SPECIAL P24 against Irish venture 14 reduction in budget 18 THIS WEEK FLIGHT 8 Lion takes largest share of ATR sales INTERNATIONAL 10 UAV sense-and-avoid one step closer. 2-8 DECEMBER 2014 Rolls-Royce maintains interest in US Ospreys A400M HANDOVER BRIZE ASSET 11 Mi-171A2 makes first flight as home market RAF readies for tactical transformation as it welcomes first Airbus airlifter to new home beckons. UTC names new chief following Chenevert retirement. New Zealand to review UAV rules AIR TRANSPORT £3.40 12 GE seeks material benefits. 49 9 770015 371266 Sukhoi secures VNAV clearance for Superjet 100. Airbus Defence & Space EASA orders checks on A380 doors US Army COVER IMAGE 13 ICAO plea for practice drills in case of another US Army set to retire its Kiowa Warrior scouts P18 Airbus Defence & Space MH370. -
SSK 0980 Rev 1.Fm
2b LEARJET 23/24/25, 28/29, 35/36 APPROVEDWHITEIN RT 0980 Revision Transmittal Sheet This page transmits Revision 1 to SSK 0980, “Replacement of Air Conditioning Evaporator Assembly”. Rework: No rework is required for aircraft which have complied with previous issues of this document. Summary: This revision adds clamp part number MS21919WDG20 as an alternate to MS21919DG20, removes the 7600122-3 evaporator assembly from the 2499002-2, -3, -4, and -010 kits, and adds the AN919-15D reducer to the 2499002-2 and -010 kits. The kit prices are updated. NOTE: Change bars are placed in the left margin of pages where significant changes are located. This revision incorporates the latest document format for Learjet service instructions. The general arrangement of this document may change from the previous issue. Description of Changes In the Planning Information section: Changed the Material Required information section as follows: Updated the 2499002-1 thru -010 kit pricing. In the Material Information section: Changed the 2499002-1 and -009 kit information as follows: Removed Model 25 aircraft serials that were never built, and removed reference to Model 25F. Changed the 2499002-1, -2, -3, -4, -009, and -010 kit information as follows: Added alternate part number clamp. Changed the 2499002-2, -3, -4, and -010 kit information as follows: Moved the 7600122-3 evaporator assembly to the “Other materials/parts necessary” table. Changed the 2499002-2 and -010 kit information as follows: Added the AN919-15D reducer. Filing Instructions: This is a COMPLETE revision. Remove and discard all pages of the prior issue and replace them with pages of Revision 1. -
Annex to ED Decision 2011/003/R 10/05/2011
Annex to ED Decision 2011/003/R 10/05/2011 APPENDIX I AIRCRAFT TYPE RATINGS FOR PART-66 AIRCRAFT MAINTENANCE LICENCE Amendment 10 (Corrigendum) 10 May 2011 The following aircraft type ratings should be used to ensure a common standard throughout the Member States. The inclusion of an aircraft type in the licence does not indicate that the aircraft type has been granted a type certificate under the Basic Regulation and its Implementing Rules Regulation 1702/2003, this list is only intended for the maintenance purposes. In order to keep this list current and type ratings consistent, such information should be first passed on to the Agency at [email protected] in case a Member State needs to issue a type rating that is not included in this list. Notes: Note 1. For aeroplanes in lists 1 and 2, and helicopters in lists 11, 12 and 13, the table of Appendix I include 3 columns: o column 1: TC holder designation o column 2: aircraft model and, when available, the aircraft commercial designation, o column 3: aircraft designation for endorsement on the Part-66 licence. Only the designations in column 3 should be used for endorsing ratings on Part-66 licences. In the tables of the remaining lists 3 to 10 the TC holder designation is added. Note 2. When a modification is introduced by this Decision to an aircraft type rating or to an engine designation in the rating which affect licences already issued, the ratings on the AML licences may be modified at next renewal or when the licence is re-issued. -
Making the Rounds in a King Air Saos–Maximum Slickness
FOR THE PILOTS OF OWNER-FLOWN, CABIN-CLASS AIRCRAFT APRIL 2016 $3.95 US VOLUME 20 NUMBER 4 Making The Rounds In A King Air SaOS–Maximum Slickness Push And Hold–To Live NBAA Focus APRIL 2016 TWIN & TURBINE • 1 The Worldwide General Aviation & Business Aviation Markets owner/operators and chief pilots of these aircraft ALL RECEIVE Twin &Turbine every month TOTAL MARKET COVERAGE JETS 1 DIAMOND I 40 HAWKER 1000A 34 LEARJET 36A 53 DIAMOND IA 9 HAWKER 125-1A 24 LEARJET 40 CHIEF PILOTS & OWNERS 3 DORNIER ENVOY 3 2 HAWKER 125-1AS 219 LEARJET 45 Aircraft Count 282 ECLIPSE EA500 1 HAWKER 125-3A/RA 193 LEARJET 45XR 47 EMBRAER LEGACY 600 2 HAWKER 125-400A 115 LEARJET 55 4 AIRBUS ACJ319 8 EMBRAER LEGACY 650 29 HAWKER 125-400AS 5 LEARJET 55B 32 ASTRA 1125 158 EMBRAER PHENOM 100 1 HAWKER 125-400B 12 LEARJET 55C 31 ASTRA 1125SP House Ad 82 EMBRAER PHENOM 300 4 HAWKER 125-600A 293 LEARJET 60 63 ASTRA 1125SPX 123 FALCON 10 11 HAWKER 125-600AS 130 PREMIER I 51 BEECHJET 400 28 FALCON 100 113 HAWKER 125-700A 16 SABRELINER 40 Full Page 275 BEECHJET 400A 25 FALCON 200 50 HAWKER 4000 13 SABRELINER 40A 58 BOEING BBJ 4/C Ad 176 FALCON 2000 187 HAWKER 400XP 7 SABRELINER 40EL 391 CHALLENGER 300 21 FALCON 2000EX 21 HAWKER 750 3 SABRELINER 40R 65 CHALLENGER 600 81 FALCON 20C 223 HAWKER 800A 24 SABRELINER 60 58 CHALLENGER 601-1A 17 FALCON 20C-5 2 HAWKER 800B 1 SABRELINER 60A 133 CHALLENGER 601-3A 26 FALCON 20D 335 HAWKER 800XP 2 SABRELINER 60AELXM 56 CHALLENGER 601-3R 3 FALCON 20D-5 14 HAWKER 800XPI 12 SABRELINER 60ELXM 279 CHALLENGER 604 7 FALCON 20E 67 HAWKER 850XP