Principles of Flight for Pilots (Aerospace Series (PEP))
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Kaman Corporation · Annual Report 2016 Powering the Future Corporate and Shareholder Information Kaman Corporation and Subsidiaries
PEOPLE POWERING THE FUTURE KAMAN CORPORATION · ANNUAL REPORT 2016 POWERING THE FUTURE CORPORATE AND SHAREHOLDER INFORMATION KAMAN CORPORATION AND SUBSIDIARIES CORPORATE HEADQUARTERS Kaman Corporation 1332 Blue Hills Avenue Bloomfield, Connecticut 06002 (860) 243-7100 STOCK LISTING Kaman Corporation’s common stock is traded on the New York Stock Exchange under the symbol KAMN. INVESTOR, MEDIA, AND PUBLIC RELATIONS CONTACT Eric B. Remington Vice President, Investor Relations (860) 243-6334 [email protected] ANNUAL MEETING The Annual Meeting of Shareholders is scheduled to be held on Wednesday, April 19, 2017 at 9:00 am local time at the offices of the Company, 1332 Blue Hills Avenue, Bloomfield, Connecticut, 06002. TRANSFER AGENT Computershare P.O. Box 30170 College Station, Texas 77842-3170 (866) 339-2742 www.computershare.com/investor Overnight correspondence should be sent to: Computershare 211 Quality Circle, Suite 210 College Station, Texas 77845 PEOPLE POWERING INNOVATION PEOPLE POWERING VALUE-ADDED SOLUTIONS PEOPLE POWERING GLOBAL SUCCESS PEOPLE POWERING NEW RELATIONSHIPS PEOPLE POWERING KAMAN KAMAN ANNUAL REPORT 2016 1 “ When I consider the future of Kaman, it’s the people who inspire the most confi dence in our continued success. We have an exceptional team across all of our businesses. They are truly the future of this company.” Neal J. Keating Chairman, President and Chief Executive Offi cer DEAR SHAREHOLDERS, When thinking about Kaman’s future, what excites me delivering outstanding experiences to our customers, most is not our products, solutions, technologies, and resulting in record satisfaction scores. In Aerospace, infrastructure, important as these are to our continued strong growth put pressure on our people to step up success. -
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. -
Build> Plan> Deliver>
2/18/12 4:53 PM > deliver > build > plan Kaman corporation AnnuAl RepoRt 2011 plan> build> deliver> Kaman Aerospace produces complex metallic and composite structures for commercial and military aircraft, military and bomb fuzing systems for the U.S. and allied militaries, our SH–2G Super Seasprite maritime helicopters and K–MAX medium-to-heavy lift helicopters, and proprietary aircraft components. Kaman Industrial Distribution is one of the nation’s leading industrial distributors, offering a wide variety of bearings, and transmission, motion control, material handling and electrical components. 227976_Kaman_CVR_R2.indd 2 annual report 2011 Two thousand and eleven was a strong year for Kaman, with double-digit increases in revenues and income over 2010. This performance is the direct result of a long-term strategic growth plan which we continue to implement. In every area of our opera tions, we develop a PLAN that is both ambitious and realistic, then build our company’s future through careful execution. The result: Kaman was able to deliver strong performance in 2011, positioning our company for continued growth in the future. 227976_Kaman_Text_R5.indd 1 2/21/12 6:46 AM neal j. keating Chairman, President and Chief Executive Officer We have always been a company focused on the future, developing strategies “ that will enable us to meet the changing needs of the industries we serve. ” 227976_Kaman_Text_R5.indd 2 2/21/12 6:46 AM DEAR SHAREHOLDERS, Strong revenue and earnings growth, along with significant progress toward achieving our long-term strategic goals, combined to make 2011 an outstanding year for Kaman. While the economic outlook remains uncertain, I am confident that Kaman is making meaningful progress in both of our businesses, with the products, services and most importantly, the people we need to continue to prosper. -
Vietnam War Turning Back the Clock 93 Year Old Arctic Convoy Veteran Visits Russian Ship
Military Despatches Vol 33 March 2020 Myths and misconceptions Things we still get wrong about the Vietnam War Turning back the clock 93 year old Arctic Convoy veteran visits Russian ship Battle of Ia Drang First battle between the Americans and NVA For the military enthusiast CONTENTS March 2020 Click on any video below to view How much do you know about movie theme songs? Take our quiz and find out. Hipe’s Wouter de The old South African Page 14 Goede interviews former Defence Force used 28’s gang boss David a mixture of English, South Vietnamese Williams. Afrikaans, slang and techno-speak that few Special Forces outside the military could hope to under- stand. Some of the terms Features 32 were humorous, some Weapons and equipment were clever, while others 6 We look at some of the uniforms were downright crude. Ten myths about Vietnam and equipment used by the US Marine Corps in Vietnam dur- Although it ended almost 45 ing the 1960s years ago, there are still many Part of Hipe’s “On the myths and misconceptions 34 couch” series, this is an about the Vietnam War. We A matter of survival 26 interview with one of look at ten myths and miscon- This month we look at fish and author Herman Charles ceptions. ‘Mad Mike’ dies aged 100 fishing for survival. Bosman’s most famous 20 Michael “Mad Mike” Hoare, characters, Oom Schalk widely considered one of the 30 Turning back the clock Ranks Lourens. Hipe spent time in world’s best known mercenary, A taxi driver was shot When the Russian missile cruis- has died aged 100. -
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. -
KA-6D Intruder - 1971
KA-6D Intruder - 1971 United States Type: Tanker (Air Refueling) Min Speed: 300 kt Max Speed: 570 kt Commissioned: 1971 Length: 16.7 m Wingspan: 16.2 m Height: 4.8 m Crew: 2 Empty Weight: 12070 kg Max Weight: 27500 kg Max Payload: 15870 kg Propulsion: 2x J52-P-409 Weapons / Loadouts: - 300 USG Drop Tank - Drop Tank. OVERVIEW: The Grumman A-6 Intruder was an American, twin jet-engine, mid-wing all-weather attack aircraft built by Grumman Aerospace. In service with the U.S. Navy and U.S. Marine Corps between 1963 and 1997, the Intruder was designed as an all-weather medium attack aircraft to replace the piston-engined Douglas A-1 Skyraider. As the A-6E was slated for retirement, its precision strike mission was taken over by the Grumman F-14 Tomcat equipped with a LANTIRN pod. From the A-6, a specialized electronic warfare derivative, the EA-6 was developed. DETAILS: The A-6's design team was led by Lawrence Mead, Jr. He later played a lead role in the design of the Grumman F-14 Tomcat and the Lunar Excursion Module. The jet nozzles were originally designed to swivel downwards for shorter takeoffs and landings. This feature was initially included on prototype aircraft, but was removed from the design during flight testing. The cockpit used an unusual double pane windscreen and side-by-side seating arrangement in which the pilot sat in the left seat, while the bombardier/navigator sat to the right and slightly below. The incorporation of an additional crew member with separate responsibilities, along with a unique cathode ray tube (CRT) display that provided a synthetic display of terrain ahead, enabled low-level attack in all weather conditions. -
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. -
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.