Epic Performance for Tнe Entire King Air 200 Family
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Propeller Operation and Malfunctions Basic Familiarization for Flight Crews
PROPELLER OPERATION AND MALFUNCTIONS BASIC FAMILIARIZATION FOR FLIGHT CREWS INTRODUCTION The following is basic material to help pilots understand how the propellers on turbine engines work, and how they sometimes fail. Some of these failures and malfunctions cannot be duplicated well in the simulator, which can cause recognition difficulties when they happen in actual operation. This text is not meant to replace other instructional texts. However, completion of the material can provide pilots with additional understanding of turbopropeller operation and the handling of malfunctions. GENERAL PROPELLER PRINCIPLES Propeller and engine system designs vary widely. They range from wood propellers on reciprocating engines to fully reversing and feathering constant- speed propellers on turbine engines. Each of these propulsion systems has the similar basic function of producing thrust to propel the airplane, but with different control and operational requirements. Since the full range of combinations is too broad to cover fully in this summary, it will focus on a typical system for transport category airplanes - the constant speed, feathering and reversing propellers on turbine engines. Major propeller components The propeller consists of several blades held in place by a central hub. The propeller hub holds the blades in place and is connected to the engine through a propeller drive shaft and a gearbox. There is also a control system for the propeller, which will be discussed later. Modern propellers on large turboprop airplanes typically have 4 to 6 blades. Other components typically include: The spinner, which creates aerodynamic streamlining over the propeller hub. The bulkhead, which allows the spinner to be attached to the rest of the propeller. -
Aircraft Service Manual
Propeller Technical Manual Jabiru Aircraft Pty Ltd JPM0001-1 4A482U0D And 4A484E0D Propellers Propeller Technical Manual FOR 4A482U0D and 4A484E0D Propellers DOCUMENT No. JPM0001-1 DATED: 1st Feb 2013 This Manual has been prepared as a guide to correctly operate & maintain Jabiru 4A482U0D and 4A484E0D propellers. It is the owner's responsibility to regularly check the Jabiru web site at www.jabiru.net.au for applicable Service Bulletins and have them implemented as soon as possible. Manuals are also updated periodically with the latest revisions available from the web site. Failure to maintain the propeller, engine or aircraft with current service information may render the aircraft un-airworthy and void Jabiru’s Limited, Express Warranty. This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled. Should you have any questions or doubts about the contents of this manual, please contact Jabiru Aircraft Pty Ltd. This document is controlled while it remains on the Jabiru server. Once this no longer applies the document becomes uncontrolled. ISSUE 1 Dated : 1st Feb 2013 Issued By: DPS Page: 1 of 32 L:\files\Manuals_For_Products\Propeller_Manuals\JPM0001-1_Prop_Manual (1).doc Propeller Technical Manual Jabiru Aircraft Pty Ltd JPM0001-1 4A482U0D And 4A484E0D Propellers 1.1 TABLE OF FIGURES ............................................................................................................................................. 3 1.2 LIST OF TABLES ................................................................................................................................................. -
P180E User Guide IMPORTANT INFORMATION
P180E User Guide IMPORTANT INFORMATION This manual is for flight simulation use only. Do not attempt to use any part for real flight operations. This software is an artistic representation of the subject matter. Military Visualizations Inc. does not endorse, nor in turn, is endorsed by the manufacturer(s) of the depicted subject matter. End User License Agreement By purchasing the Milviz P180E, you are consenting to be bound by and agree to the following: COPYRIGHT: Copyright © 2021 Military Visualizations (Milviz). Milviz retains FULL copyright on the entire P180E package. DISTRIBUTION: You may NOT redistribute the P180E package in whole or in part. Any such distribution is strictly prohibited. GRANT OF LICENSE: A limited license is granted to use the Milviz P180E for personal entertainment purposes only. Commercial, training or any other use without the express permission of Military Visualizations Inc. is expressly prohibited. Any such usage will be litigated to the full extent of the law. This does NOT give you the license to modify in anyway part or whole based on the designers original work except for your own personal use. You MAY of course use the paint kit provided to create new liveries for public distribution, provided no charge is made for them! Any inquiries regarding use of this product in a commercial or training capacity should be directed via e-mail to [email protected]. DISCLAIMER: Milviz and all associates shall NOT be held responsible for any damages arising from the use of the P180E product. Copyright © 2021 Military -
1976 Cessna T210L Turbo Centurion II for Sale
1976 Cessna T210L Turbo Centurion II Wolfe Aviation Business Aircraft Acquisitions, Appraisals, Sales and Service Verlyn Wolfe, PSCA ASA Accredited Senior Aircraft Appraiser Wolfe Aviation Stockton Metropolitan Airport (KSCK) 2050 East Sikorsky Street, Hangar 7 Stockton, California 95206 P.O. Box 31592, Stockton, California 95213-1592 Telephone: (209) 983-0117 Ext. 233 Cellular: (209) 607-9804 Email: [email protected] Wolfe Aviation believes the following information to be accurate but does not warrant nor guarantee the information accordingly; purchasers should rely upon their own inspection of the aircraft. There shall be no agreement between parties unless set forth in a written contract signed by buyer and seller. 1 Details: • Registration: N2803S • Serial Number: 21061049 • Airframe Time: 2,983 Hours total time since new • Engine: Teledyne Continental Motors TSIO-520-H4B sn: 217325-R; 285 HP 1,005 Hours since factory remanufacture; 1,400 hour TBO Compressions at last annual: #1 68, #2 75, #3 72, #4 68, #5 62, #6 60 Remanufactured by Teledyne Continental Motors 08/30/1994 Turbo overhauled by Main Turbo Systems, Inc. 08/08/2019 @ 83 hours ago 500 Hour magneto inspections c/w 01/26/2018 @ 86 hours ago Knisley Welding exhaust system installed 08/08/2018 • Propeller: Hartzell PHC-J3YF-1RF/F7691 three blade Scimitar propeller 27 Hours since new propeller installed; 2,000 hour TBO Propeller manufactured new by Hartzell Propeller 2018 New McCauley Propeller governor installed 10/21/2019 @ 24 hours ago • Inspection: Annual inspection -
2009 Pocket Reference
Raisbeck Performance Systems 2009 for the Beechcraft King Air Family 2009 POCKET REFERENCE Performance Engineering Directory EPIC Performance Packages............................................................................. .2 Systems Overview............................................................................................... .3 The Seven Points of Airplane Productivity................................................ .6 EPIC Performance The.EPIC Performance Advantage......................................................................... .7 200/B200.EPIC PLATINUM.Elements..................................................................... .8 200/B200.EPIC GOLD.Elements............................................................................ .9 200/B200.EPIC PLATINUM.Benefits..................................................................... .10 200/B200.EPIC GOLD.Benefits............................................................................ .11 200/B200.EPIC PLATINUM.Performance.Comparisons....................................... .12 200/B200.EPIC GOLD.Performance.Comparisons............................................... .13 200/B200.EPIC PLATINUM.Noise.Characteristics................................................ .14 200/B200.EPIC PLATINUM.MATOW.Benefits....................................................... .15 EPIC.for.King.Airs.with.PT6A-41.Engines............................................................. .16 EPIC.for.King.Airs.with.PT6A-61.Engines............................................................ -
Speed, Power and Control Depend on Innovation
Discover Speed, Power and Control Depend on Innovation he latest innovation from Lancair is a new T2-seat “little brother” to the groundbreaking Mako — the Barracuda. Establishing a new standard for value, Barracuda offers high per- formance, operational economy and Lancair’s trademark aerodynamic style in a cost-effective package for two. nnounced at EAA AirVenture 2018, Barracuda is the latest design from Lancair’s legendary innovators. AA beautiful 2-place composite single with exceptional performance and style at an affordable price point. Speed, Power and Control Barracuda Specifications Start with Innovation. Base Engine Continental IO-550-N Horsepower 310 Power to climb. Speed to take you to new places. Innovation that Hartzell Propeller 3-blade “Scimitar” only Lancair can bring you. Three decades after revolutionizing the Landing Gear (Base Configuration) Fixed Mains, Retractable Nose world of two-seat aircraft, a rich history of unparalleled innovation Useable Fuel 65 gal and record-setting performance continues with the Lancair Gross Weight (lb) 2200 Barracuda. Updated and optimized from tip to tail, Barracuda is Empty Weight (lb) 1450 faster, more agile and quicker to build than its predecessors. Useful Load (lb) 750 Full Fuel Payload (lb) 360 It’s All About The Options. Glass Panel G3X Touch AmSafe Seat Belts optional You’ll enjoy a wealth of options to customize your Barracuda. Speed Brakes optional Speed Brakes from Precise Flight, Wheel Brakes from Beringer and Built-in Oxygen optional convenient access to the baggage area via an openable rear window Wingspan 25.5 ft are just a sample. Choose a Hartzell 3-blase ‘Scimitar’ propeller to Length 22 ft boost performance. -
2012 Edition Raisbeck Systems
Raisbeck Systems for your King Air 2012 Edition Raisbeck Performance Systems for the entire Beechcraft King Air Family 2012 POCKET REFERENCE A Message from the CEO Performance Systems for the entire UR PERFORMANCE SYSTEMS ARE ON King Air Family OFACTORY-NEW KING AIRS. Hawker Beechcraft and their predecessors have 350ER/350i/350/300 Series added Raisbeck Engineering Systems to • Dual Aft Body Strakes their King Air factory production line. Typical • High Flotation Gear Doors of these has been our Dual Aft Body Strakes • Crown Wing Lockers (2001), Nacelle Wing Lockers (2004) on the King Air 350. In 2011, our Ram Air Recovery System was added to the new King Air 250. And...King Air new aircraft salesmen offer our systems as optional 250/B200GT/B200/200 Series additions prior to delivery. • Power Props • Ram Air Recovery System WHY IS THIS IMPORTANT TO OUR CUSTOM- • Enhanced Performance Leading Edges ERS, OUR DEALERS, AND OUR BUSINEss? • Dual Aft Body Strakes In a word: market acceptance. There is James D. Raisbeck, C.E.O. • High Flotation Gear Doors no question that factory acceptance and [email protected] • Crown Wing Lockers endorsement has been a major milestone in our market penetration. Many millions of flight hours on thousands C90GTx/C90GTi/C90GT/C90/90/E90 Series of King Airs, and not one FAA Airworthi- • Power Props WHY HAVE OUR SYSTEMS BEEN SO UNIVER- ness Directive or FAA-Mandatory Service • Dual Aft Body Strakes SALLY ACCEPTED? Raisbeck Engineering Bulletin! • Crown Wing Lockers has dedicated itself for the past 30 years • Increased Gross Weight to developing systems which measurably FOR ME, A PLEASANT AND REWARDING improve all King Air models. -
Crash Following In-Flight Fire Fresh Air, Inc. Convair CV-440-38, N153JR, San Juan, Puerto Rico, March 15, 2012
Crash Following In-Flight Fire Fresh Air, Inc. Convair CV-440-38, N153JR San Juan, Puerto Rico March 15, 2012 Accident Report NTSB/AAR-14/04 National PB2015-101257 Transportation Safety Board NTSB/AAR-14/04 PB2015-101257 Notation 8601 Adopted November 17, 2014 Aircraft Accident Report Crash Following In-Flight Fire Fresh Air, Inc. Convair CV-440-38, N153JR San Juan, Puerto Rico March 15, 2012 National Transportation Safety Board 490 L’Enfant Plaza, S.W. Washington, D.C. 20594 National Transportation Safety Board. 2014. Crash Following In-Flight Fire, Fresh Air, Inc., Convair CV-440-38, N153JR, San Juan, Puerto Rico, March 15, 2012. Aircraft Accident Report NTSB/AAR-14/04. Washington, DC. Abstract: This report discusses the March 15, 2012, accident involving a Convair CV-440-38, N153JR, operated by Fresh Air, Inc., which crashed into a lagoon about 1 mile east of the departure end of runway 10 at Luis Muñoz Marín International Airport, San Juan, Puerto Rico. The two pilots died, and the airplane was destroyed by impact forces. Safety issues include inadequate Federal Aviation Administration (FAA) oversight of 14 Code of Federal Regulations (CFR) Part 125 operations, inadequate evaluation of Fresh Air’s compliance with FAA-approved procedures, and evaluation of 14 CFR Part 125 pilots using another operator’s operations specifications. Safety recommendations are addressed to the FAA. The National Transportation Safety Board (NTSB) is an independent federal agency dedicated to promoting aviation, railroad, highway, marine, and pipeline safety. Established in 1967, the agency is mandated by Congress through the Independent Safety Board Act of 1974 to investigate transportation accidents, determine the probable causes of the accidents, issue safety recommendations, study transportation safety issues, and evaluate the safety effectiveness of government agencies involved in transportation. -
(JAR)/Federal Aviation Regulations (FAR) 23 Harmonization
Federal Aviation Administration Aviation Rulemaking Advisory Committee General Aviation Certification and Operations Issue Area JAR/FAR 23 Harmonization Working Group Task 4 – Flight test Task Assignment IIIII~IMIIirt•·•·llllllllll .. ll .. lllllllllt•r•::rlrllllllllllllllllllllllllllllllllllll~ to aDd 6:01Bpatible witla tlaat as8ipecl ao D. Draft a separate Notice of Proposed Federal Aviation Admlnlatnitlon the Avi.ation RulemakiJJs Advisory Rulemakina for Tasks 2-5 proposing CoiMriHee. The General Avielion and new or revised requirements, a Aviation Rulemaklng Advlaory Business AU-plaae Subcommittee, supportina economic analysis. and other Commmee; Gener11l Av.. tlon 8IKI consequently, estalliiebed t8e JAR/FAR required analysis, with any other Buslne.. Airplane SubcommlttH: Z3 HannenizatiOit Workiat Greup. conateral documeRts (sucb as. Advisory JAR/FAR 23 HarmonlzaUon Working Specifical1J, dae Work.ina Grevp's Circulars) the Workina Group Group tasb are tbe foliowing: The JAR/FAR 23 determines to be needed. Harmonization Working Group ii E. Give a status reporl oa each task at AGENCY: Federal Aviation ct:arged wUh making recommendations each meetina of the Subcommittee. Administration (FAA), DOT. to the General A viatton and Bulinest The JAR/FAR 23 Harmonization ACTION: Notice of establishment of JAR/ Airplane Subcommittee concerning the Working Croup win be comprised of FAR 23 Harmonization Working Group. FAA disposition of the CoDowing experts from those orpnlzations having rulemalcing subj.ecta recently an interest in the task assigned to it. A SUMMARY: Notice is given of the coordinated between ttse JAA 1111d the working group member need not establishment of the JAR/FAR Z3 FAA~ necessarily be a representative or one of Harmonization Working Group by the Task 1-Review/AR Issue$: Review the organizations of the parent General General Aviation and Business Airplane JAR 23 Issue No. -
Fire and Ice
Volume 12 Number 3 Summer 2003 Fire and Ice by Robert Mills Page 30 America’s Ancient City: St. Augustine A Pre-Convention Tour by Jeff Schweitzer Page 42 Representing Owners and Pilots of High Performance Single Engine Pressurized Aircraft Worldwide Trade-in and land an incredible deal on a Meridian. Deal your way into a Piper Meridian. Now with 15% MORE useful load. There are more reasons than ever to get a new Piper Meridian • Now with up to 1740 pounds of useful load • Optional Honeywell Integrated Hazard (15% more!) Avoidance System (IHAS) 8000 • New cutting edge digital Magic 1500 autopilot – Weather uplink – Traffic avoidance designed especially for the Meridian – Color moving map – L3 WX-500 Stormscope • Piper Insurance and Financial Services – Terrain awareness – Weather radar display standing by to work for you • 2 year Factory Warranty Now that’s freedom. There’s never been a better time to buy! Take advantage of this limited time offer today. To find out more, call Piper at 866-648-1945 or visit www.newpiper.com ™ The New Piper Aircraft, Inc. Table of Contents ... 6 Letter From the Editor by Jeff Schweitzer 10 Malibu Maintenance by Kevin Mead 12 Aviation News by Doug Leet 14 Note from the President by Richard Bynum 15 Coats Corner by David Coats M.D. 18 Malibu Trivia Q & A by Mary Bryant 21 Piper Perspective: The View From Vero Beach by Chuck Suma 24 Views from a JetProp by Robert Conrad 27 Turbine Times by Cody Ramsey 52 Notes from M-MOPA Headquarters by Russ Caauwe 57 M•MOPA Classifi eds 62 Advertising Rates 62 Calendar 62 Training Update FEATURE ARTICLES 30 Alaska Adventure by Robert Mills 42 America’s Ancient City: St. -
Table of Contents
P.180 Avanti EVO Aircraft Specification Revision 7.3 October 2019 Revision 7.3 October 2019 Avanti EVO Aircraft Specification 1 TABLE OF CONTENTS Title Page 1 INTRODUCTION .................................................................................................................................................... 4 1.1 APPLICABLE DOCUMENTS AND REFERENCES .................................................................................................................... 5 2 GENERAL DESCRIPTION ........................................................................................................................................ 6 3 SPECIFICATIONS ................................................................................................................................................... 8 3.1 EXTERNAL DIMENSIONS .............................................................................................................................................. 8 3.2 INTERNAL DIMENSIONS AND VOLUMES .........................................................................................................................10 3.3 WEIGHTS ................................................................................................................................................................11 3.4 PRESSURIZATION ......................................................................................................................................................12 3.5 POWERPLANT ..........................................................................................................................................................12 -
2.10. ENGINES the Airplane Is Powered by Two Counter-Rotating Pratt & Whitney PT6A-66 Turboprop Engines, Each Flat Rated to 850 SHP
PILOT’S OPERATING HANDBOOK P.180 AVANTI II DESCRIPTION AND OPERATION ENGINES 2.10. ENGINES The airplane is powered by two counter-rotating Pratt & Whitney PT6A-66 turboprop engines, each flat rated to 850 SHP. The rated power can be maintained during cruise to approximately 25,000 feet on a standard day. Inlet air enters the engine through an annular plenum chamber, formed by the compressor inlet case. The four-stage axial and single-stage centrifugal compressor is driven by a single-stage turbine. Downstream the compressor the air is routed through diffuser tubes to the combustion chamber liner. The flow of air changes direction of 180 degrees as it enters and mixes with fuel. The fuel/air mixture is ignited by two spark igniters, which protrude into the combustion chamber, and the resultant expanding gases are directed to the compressor turbine and then to the power turbine. The compressor and power turbines are located in the approximate center of the engine with their respective shafts extending in opposite directions. The exhaust gas from the power turbine is collected and ducted in the bifurcated exhaust duct and directed to atmosphere via twin opposed exhaust stubs. The fuel supplied to the engine from the airplane fuel system is routed through an oil-to-fuel heater to an engine-driven fuel pump where it is further pressurized. The fuel pump delivers the fuel to a fuel control unit, which determines the correct fuel schedule for engine steady state operation, both with and without power augmentation and acceleration. A flow divider supplies the metered fuel flow to the primary or to both primary and secondary fuel manifolds as required.