DOCSLIB.ORG

Wheels Brakes Landing Gear

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text

Load more

Wheels Brakes English V04/2021 Landing Gear 2021 Ambassadors Bryan Bowen, Bowen Aero LLC After STOL Drag racing for 3 years at the High Sierra Fly-in and Reno air races around the corner, I had to come up with a better braking system. I originally had a Cleveland system and swit- ched to a grove double piston caliper system but still wasn’t happy with the braking power. I turned to Beringer to help me come up with a solution, however nobody had put a Beringer brake system on a Kitfox before. After working closely with the wonderful people at Beringer we developed a parts list that would work on all Kitfox models. The results were amazing. The braking improvement brought STOL #4 back into compe- titive times in the STOL Drags, but more than that it made it an all around better performing off-airport airplane. The big- Mike Goulian, USA gest noticeable difference is the lack of brake fade with the Edge 540 /Extra 330SC Beringer system. You have firm braking all the way to a stop, Air Show Pilot unlike the other systems that fade and leave you pushing the Red Bull Air Race Pilot brake pedal through the firewall trying to stop the airplane. I "I switched to BERINGER couldn’t be happier with the performance of the braking and brakes on my Red Bull Air Race they are the most beautiful wheels ever put on an airplane. Edge 540 and absolutely love them. The BERINGERsystem is much lighter than the Nicolas IVANOFF, Edge 540 legacy system on my plane but the stopping power Air Show Pilot makes all the difference in the world. I simply had to Red Bull Air Race Pilot have the BERINGER brakes on my Extra 330 as well." BERINGER wheel/brake kit for Extra 330 and Extra NG was developped with Nicolas. " I would define the BERINGER brakes in few words: lightness and endurance but espe- cially a higher efficiency and a better feeling Luca Bertossio at braking. Everything is a matter of balance Planeur Jet Swift and BERINGER has found the right one! " Air Show Pilot «I use BERINGER because I fell in love with the feeling on the brake handle when I used it for the first time...BERINGER is just the best feeling, feed- back and performances!» 2021 Catalogue Page 2 Index History BERINGER History - Company Values .......................................... Pages 4 - 5 Values Contacts ...................................................................................... Page 6 Contacts ® SensAIR ..................................................................................... Page 8 - 9 SensAIR Complete Kits for Aircraft/Light Aircraft/Gliders .......................... Pages 10 - 71 Complete Kits Landing Gear : ALG / Shock Wheel ............................................... Pages 72 - 75 Landing Gear Wheels / Brakes ........................................................................... Pages 76 - 82 Wheels Brakes Nose Wheels / Tailwheels ............................................................ Pages 83 - 87 Nose wheel Tailwheel Tires ............................................................................................. Pages 88 - 89 Tires Wheel Axles .................................................................................. Pages 90 - 93 Axles Brake Master Cylinders : pedal/cockpit/stick ............................... Pages 94 - 114 Master Cylinders Regulator - Anti-skid / Pressure limiter ........................................ Pages 115 - 117 Limiters Parking Brake Valve ...................................................................... Page 118 Anti-skid Parking Hydraulic Hoses/Fittings .............................................................. Page 119 Brake Valve Brake lines Tools ............................................................................................. Page 120 Fittings Spare Parts ................................................................................... Pages 121 - 122 Tools Spare BERINGER AERO Technology ......................................................... Pages 123 - 128 Parts BERINGER They trust us ................................................................................ Page 129 Technology They trust 2021 Catalogue Page 3 us ... BERINGER history - Company values History Values Quality - Innovation - Customer Service Contacts 1985 Gilbert Béringer created BERINGER Company helped by his wife Véronique. He has been manufacturing wheels, forks and side SensAIR cars for motorbikes and then brakes, in the same spirit of quality and performance for 30 years. BERINGER won many tiltles in the World Endurance Championships thanks to a team of exceptional mechanical engineers who have studied and developed new products whose Complete performance/weight ratio is without precedent. Kits BERINGER Wheels & Brakes was born, when Gilbert Béringer, also a pilot and Aircraft builder fond of aviation, decided to apply Landing 2002 Gear his patented high performance braking solutions to the aeronautical world. Wheels 2009 BERINGER AERO was born and the Company leaved the motorbike and car business to BERINGER BRAKES. Brakes 2011 BERINGER AERO moved to Gap-Tallard airfield. Claire BERINGER, Gilbert's and Véronique's daughter, joined the Company after Nose wheel she graduated as Aeronautical & Energy Dipl. Engineer (including 5 months at Oakland University–Detroit, MI) topped with a Master’s Tailwheel degree in Commercial and Management Operations. Tires 2012 BERINGER AERO USA Inc. was born in Chicago to answer the US customer needs. The headquarters have since moved to Greenville, SC in 2016. Axles 2015 BERINGER Company celebrated her 30 year anniversary and started to diversify the products by designing the ALG landing gear to improve the safety of Taildragger Aircraft. Master Cylinders 2017 Lukas STUTZER, born in Alaska, Mechanical Dipl. Engineer, joined BERINGER team. Limiters Anti-skid An advanced technology BERINGER makes wheels and braking systems for a wide range of aircraft, from light aircraft up to its now-standard STC for the Pilatus PC-6, Parking Brake Valve and the Cirrus SR20/22 plus complete kits for many popular aircraft, that include everything for a bolt-on conversion. These innovations are covered by 11 patents and have allowed BERINGER brakes to take a decisive technological lead. Brake lines Fittings Quality and Certification Tools BERINGER AERO is certified by the Alternative Procedures to Design Organisation Agreement given by EASA in 2006 and by the Production Organisation Agreement given by DGAC in 2008. Spare Parts BERINGER Technology They trust us ... 2021 Catalogue Page 4 BERINGER history - Company values History Sustainable Development - BERINGER AERO's Commitments Values Contacts Respect for the environment Toxic substances and non recyclable materials are avoided from the fabrication process. Workshop trash is sorted prior to disposal. SensAIR An environmental awareness campaign is in force and consistently reviewed. Reduction of Energy Consumption Complete Kits Our specially-designed bioclimatic building (BBC) made of local wood only consumes only 10% of the energy required to heat or cool a conventional steel building. 98% of the energy used to heat our water is solar-powered Landing BERINGER employs vehicles using propane (LPG): they have reduced CO2 emissions and have no particulate emissions. Gear Eco-conception for products Wheels Innovative BERINGER products are covered by 11 patents. They are designed to have a virtually unlimited service life, because pieces Brakes that are worn down can be replaced. Components are 99% recyclable and 98% of the products are made in France, within a radius of Nose wheel 200 miles. This process reduces transportation and energizes local industrial bases. Tailwheel Respect for Human Dignity in the Workplace From one end of the assembly line to another, from in-house to subcontractors, BERINGER staff members work in optimal conditions Tires following the regulations of OIT (International Work Organization). BERINGER does not award contracts based on “lowest-cost,” and does not use outsourcing. Axles Respect for the Ethics of Economics Master BERINGER partners (suppliers, subcontractors, banks, clients) are chosen based on ethical criteria, not only the lowest price Cylinders BERINGER commits to projects based on their moral philosophy : BERINGER wheels are not involved in projects that could intentionally threaten human life and BERINGER has partnerships in eco-friendly projects (e.g., Green challenge, SolarImpulse). Limiters Zero Compromise on Quality Anti-skid At BERINGER, quality is not only respect for procedures that the EASA certifies, such as the Design Approval Organization and the Pro- Parking duction Approval Organization (Part 21G). Quality is a pledge of trust to our clients: our clients entrust us with their lives. To remain Brake Valve worthy of this trust, we offer a lifetime warranty ( liability insurance) on materials and craftsmanship on all our products. Brake lines BERINGER integrates its partners in the projects, from the design stage to commercialization Fittings AeroProviders, PEGASE/SAFE Cluster, lHautes Alpes Development Agency. Tools In 2010 the MADE IN RESPECT label has been recognizing BERINGER AERO’s commitment to sustainable development. Spare On February 4th, 2012 BERINGER AERO won the Trophée RSE PACA TPE (Social Responsibility of the Companies). Parts In July 2015, the specific Know-how of BERINGER AERO has been recognized through the Label "Entreprise du Patrimoine Vivant" EPV. BERINGER Technology They trust 2021 Catalogue Page 5 us ... Contacts : sales and customer support
Recommended publications
  • Lancair ES (Lancair-LES.Pdf)

    Lancair ES (Lancair-LES.Pdf)

    18850 Adams Ct Phone: 408/738-3959 Morgan Hill, CA 95037 Toll Free (U.S.): 800/777-6405 www.AircraftCovers.com Fax: 408/738-2729 Email: [email protected] manufacturer of the finest custom-made aircraft covers Tech Sheet: Lancair ES (lancair-LES.pdf) Lancair ES Engine Inlet Plugs Lancair ES Engine Inlet Plugs Section 1: Canopy/Cockpit/Fuselage Covers Canopy Covers help reduce damage to your airplane's upholstery and avionics caused by excessive heat, and they can eliminate problems caused by leaking door and window seals. They keep the windshield and window surfaces clean and help prevent vandalism and theft. The Lancair ES Canopy Cover is custom-designed for each model, as well as your aircraft's specific antenna and temperature probe placements, if applicable. The Canopy Cover is designed to enclose the windshield, side windows and canopy roof. The Canopy Cover attaches using adjustable "belly straps", which run under the belly and connect to the other side of the cover with a quick-release plastic buckle. When requested, it is also sometimes possible to design Canopy covers that can attach to the aircraft fuselage using pop-riveted snap-heads at the rear and snap-head screws on the engine cowl. This cover type is made from Silver Acrylic Sunbrella canvas and is 100% lined with a soft and smooth microfiber. Bruce's Custom Covers developed this material combination especially for aircraft protection. The outer material is medium weight and treated for water resistance, UV resistance and anti-static buildup. The inner lining is a very soft and smooth microfiber to prevent scratching.
  • MT Propeller

    MT Propeller

    mt-propeller Installationlist Edition Report No.: E-546 Entwicklung GMBH 01st July 2009 EMP Min Blade Max Blade Max R- Counter- Aircraft Engine Propeller Spinner Assy Governor STC Angle Angle Reverse Station Weight TC [ ° ] [ ° ] [ ° ] [ cm ] [ ° ] EASA/FAA A-150Luftschiff Lyc.IO-360 MTV-25-1-D-C-R(M)/CR165-06 P-492 P-480-1 7 22 -18 58 CWT+27 EASA A-1Husky Lyc.IO-360-A1P MTV-14-B/183-301a P-238-A P-860-4 10,5 30 68,5 A-1Husky Lyc.O-360-C1G MTV-12-B/180-17 P-208-X P-860-4 13 30 63 EASA/FAA A-1Husky Lyc.IO-360-A1P/-C1G MTV-15-B/210-58 P-277-B P-860-4 9 24 79 EASA AA-200 Lyc.IO-360-() MTV-18-B/LD178-17 P-246 P-120-U/2700-24V 14 35 63 CWT+35 FAA ACA SCOUT 8GCBC Lyc. O-360- MTV-9-B/190-18a P-282-1-A P-860-4 9 28 71 FAA ACA SCOUT 8GCBC Lyc. O-360- MTV-15-B/203-58 P-271-2-C P-860-4 9 28 76 EASA/FAA ACA Scout 9GCBC Lyc. IO-540- MTV-9-B/198-58 P-810-1 P-860-3 8,5 28 74 Accord 201 SR-305-230 MTV-9-B-C-F-R(M)/CFR198-58B P-907 P-980-() 14,5 81 -18 74 CWT+3 ACRO Lyc.AEIO-360-A1B MTV-9-B-C/C190-11 P-208 P-880-4 9,5 34 70 CWT+26 ACRO Lyc.AEIO-540-C4B5 MTV-9-B-C/C200-15 P-208 P-880-3 10,5 34 70 CWT+26 Acrobatic Aircraft Chevy V8 550 hp MTV-16-1-E-C/C250-27 P-542 9,5 36 87,5 CWT+26 ACRO-MONOPLANE Lyc.AEIO-540-L1B5D MTV-9-B-C/C200-15 P-208 P-880-3 10,5 34 70 CWT+26 ACROZENITHCH-180 Lyc.IO-360-A1B6D MTV-2-B-C/193-02 P-029 P-860-4 9,5 34 67,5 CWT+30 ACV 120PS MTE-176/RD113-23 - - 22,2 - 43 ACV BMW MTE-106/LD119-10 - - 20 - 45 ACV ROBIN EC-60-PL MTE-176/LD113-23 - - 22,2 - 43 ACV Rotax503(2:1) MTE-176/RD91-37 - - 21 - 32 AEASATROSS 4 UACL PT6A-15AG MTV-27-1-E-C-F-R(P)/CFR208-15c
  • Adaptive Brake by Wire from Human Factors to Adaptive Implementation

    Adaptive Brake by Wire from Human Factors to Adaptive Implementation

    UNIVERSITY OF TRENTO Doctoral School in Engineering Of Civil And Mechanical Structural Systems Adaptive Brake By Wire From Human Factors to Adaptive Implementation Thesis Tutor Doctoral Candidate Prof. Mauro Da Lio Andrea Spadoni Mechanical and Mechatronic Systems December 2013 - XXV Cycle 1 Adaptive Brake By Wire From Human Factors to Adaptive Implementation 2 Adaptive Brake By Wire From Human Factors to Adaptive Implementation Table of contents TABLE OF CONTENTS .............................................................................................................. 3 LIST OF FIGURES .................................................................................................................... 6 LIST OF TABLES ...................................................................................................................... 8 GENERAL OVERVIEW .............................................................................................................. 9 INTRODUCTION ................................................................................................................... 12 1. BRAKING PROCESS FROM THE HUMAN FACTORS POINT OF VIEW .................................... 15 1.1. THE BRAKING PROCESS AND THE USER -RELATED ASPECTS ......................................................................... 15 1.2. BRAKE ACTUATOR AS USER INTERFACE ................................................................................................. 16 1.3. BRAKE FORCE ACTUATION : GENERAL MOVEMENT -FORCE DESCRIPTION ......................................................
  • Oxygen Systems

    Oxygen Systems

    OXYGEN SYSTEMS AEROX HIGH-DURATION AVIATION AEROX PRO-O2 EMERGENCY OXYGEN SYSTEMS HANDHELD OXYGEN SYSTEMS Add to your flying comfort by using oxygen Provides oxygen until the aircraft can reach a lower at altitudes as low as 5000 ft. Aerox Oxygen altitude. And because Pro-O2 is refillable, there is no CM Systems include lightweight aluminum cyl in- need to purchase replacement O2 cartridges. During ders, regulators, all hardware, flow meter, short flights at altitudes between 12,500ft. MSL and and nasal cannulas (masks available as 14,000ft. MSL where maneuvering over mountains or turbulent weather option). Oxysaver oxygen saving cannulas is necessary, the Pro-O2 emergency handheld oxygen system provides & Aerox Flow Control Regulators increase oxygen to extend these brief legs. Included with the refillable Pro-O2 is WP the duration of oxygen supply about 4 times, a regulator with gauge, mask and a refillable cylinder. and prevent nasal irritation and dryness. Pro-O2-2 (2 Cu. Ft./1 mask)........................P/N 13-02735 .........$328.00 Aerox 2D Aerox 4M Complete brochure available on request. Pro-O2-4 (2 Cu. Ft./2 masks) ......................P/N 13-02736 .........$360.00 system system AEROX EMT-3 PORTABLE 500 SERIES REGULATOR – AN AIRCRAFT SPRUCE EXCLUSIVE! OXYGEN SYSTEM ME A small portable system designed for the occasional user • Low profile who wants something smaller and less costly than a full • 1, 2, & 4 place portable system. The EMT-3 is also ideal for use as an • Standard Aircraft filler for easy filling emergency oxygen system. The system lasts 25 minutes at • Convenient top mounted ON/OFF valve 2.5 LPM @ 25,000 FT.
  • Cresis UAV Critical Design Review: the Meridian

    Cresis UAV Critical Design Review: the Meridian

    CReSIS UAV Critical Design Review: The Meridian William Donovan University of Kansas 2335 Irving Hill Road Lawrence, KS 66045-7612 http://cresis.ku.edu Technical Report CReSIS TR 123 June 25, 2007 This work was supported by a grant from the National Science Foundation (#ANT-0424589). Executive Summary This report briefly describes the development of the three preliminary configuration designs proposed for the Meridian UAV. This report details the selection of the primary configuration and further, more detailed, analysis including Class II weight and Balance, Class II Stability and Control, Performance Analyses, Systems Design, Class II landing gear, structural arrangement, a manufacturing breakdown and a cost analysis. The design mission for this aircraft is to takeoff from a snow or ice runway, fly to a designated area, then use low frequency radar to perform measurements of ice sheets in Greenland and Antarctica. Three designs were developed: • A Monoplane with Structurally Integrated Antennas • A Monoplane with Antennas Hanging from the Wing • A Biplane with Antennas Structurally Integrated Into the Lower Wing The monoplane with antennas hanging from the wing was selected as the primary configuration for further development. This report describes the Class II design and analysis of that vehicle. i Acknowledgments This material is based upon work supported by the National Science Foundation under Grant No. AST-0424589. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author(s) and
  • Meritor Drivetrain Plus Product Identification Guide

    Meritor Drivetrain Plus Product Identification Guide

    Brought to you by Pro Gear & Transmission. For parts or service call: 877-776-4600 407-872-1901 www.globaldifferentialsupply.com 906 W. Gore St. Orlando, FL 32805 [email protected] sect1.fm Page -3 Thursday, July 29, 2004 11:39 AM ~MERITOR® an ArvinMeritor brand Publication TP-03167 DriveTrain PlusTM by ArvinMeritor Product Identification Guide Issued 03-04 partsID.book Page -2 Tuesday, March 2, 2004 2:57 PM Overview This publication provides identification information for Meritor, Meritor WABCO and Gabriel products. Product pictures and drawings, identification tag locations and model nomenclatures are provided. How to Obtain Maintenance and Service Information On the Web Visit the DriveTrain PlusTM by ArvinMeritor Tech Library at drivetrainplus.com to easily access product and service information. The Library also offers an interactive and printable Literature Order Form. ArvinMeritor’s Customer Service Center Call ArvinMeritor’s Customer Service Center at 800-535-5560. Technical Electronic Library on CD The DriveTrain PlusTM by ArvinMeritor Technical Electronic Library on CD contains product and service information for most Meritor and Meritor WABCO products. The cost is $20. Specify TP-9853. Information contained in this publication was in effect at the time the publication was approved for printing and is subject to change without notice or liability. Meritor Heavy Vehicle Systems, LLC, reserves the right to revise the information presented or to discontinue the production of parts described at any time. -2 Meritor TP-03167 partsID.book
  • 2021 Chevrolet Tahoe / Suburban 1500 Owner's Manual

    2021 Chevrolet Tahoe / Suburban 1500 Owner's Manual

    21_CHEV_TahoeSuburban_COV_en_US_84266975B_2020AUG24.pdf 1 7/16/2020 11:09:15 AM C M Y CM MY CY CMY K 84266975 B Cadillac Escalade Owner Manual (GMNA-Localizing-U.S./Canada/Mexico- 13690472) - 2021 - Insert - 5/10/21 Insert to the 2021 Cadillac Escalade, Chevrolet Tahoe/Suburban, GMC Yukon/Yukon XL/Denali, Chevrolet Silverado 1500, and GMC Sierra/Sierra Denali 1500 Owner’s Manuals This information replaces the information Auto Stops may not occur and/or Auto under “Stop/Start System” found in the { Warning Starts may occur because: Driving and Operating Section of the owner’s The automatic engine Stop/Start feature . The climate control settings require the manual. causes the engine to shut off while the engine to be running to cool or heat the Some vehicles built on or after 6/7/2021 are vehicle is still on. Do not exit the vehicle vehicle interior. not equipped with the Stop/Start System, before shifting to P (Park). The vehicle . The vehicle battery charge is low. see your dealer for details on a specific may restart and move unexpectedly. The vehicle battery has recently been vehicle. Always shift to P (Park), and then turn disconnected. the ignition off before exiting the vehicle. Stop/Start System . Minimum vehicle speed has not been reached since the last Auto Stop. If equipped, the Stop/Start system will shut Auto Engine Stop/Start . The accelerator pedal is pressed. off the engine to help conserve fuel. It has When the brakes are applied and the vehicle . The engine or transmission is not at the components designed for the increased is at a complete stop, the engine may turn number of starts.
  • Assembly Manual

    Assembly Manual

    MS:160 ASSEMBLY MANUAL “Graphics and specifications may change without notice”. Specifications: Wing span ------------------------------70.9in (180cm). Wing area -----------------613.8sq.in (39.6sq dm). Weight ------------------------9.7-10.6lbs (4.4-4.8kg). Length ------------------------------58.8in (149.3cm). Engine ------------------ 0.75-0.91cu.in -----2-stroke. 1.00-1.25cu.in -----4-stroke. Radio ------------------- 6 channels with 11 servos. Electric conversion: optional LANCAIR LEGACY Instruction Manual. INTRODUCTION. Thank you for choosing the LANCAIR LEGACY ARTF by SEAGULL MODELS COMPANY LTD. The LANCAIR LEGACY was designed with the intermediate/advanced sport flyer in mind. It is a semi scale airplane which is easy to fly and quick to assemble. The airframe is conventionally built using balsa, plywood to make it stronger than the average ARTF , yet the design allows the aeroplane to be kept light. You will find that most of the work has been done for you already.The motor mount has been fitted and the hinges are pre-installed . Flying the LANCAIR LEGACY is simply a joy. This instruction manual is designed to help you build a great flying aeroplane. Please read this manual thoroughly before starting assembly of your LANCAIR LEGACY . Use the parts listing below to identify all parts. WARNING. Please be aware that this aeroplane is not a toy and if assembled or used incorrectly it is capable of causing injury to people or property. WHEN YOU FLY THIS AEROPLANE YOU ASSUME ALL RISK & RESPONSIBILITY. If you are inexperienced with basic R/C flight we strongly recommend you contact your R/C supplier and join your local R/C Model Flying Club.
  • 9-15K Complete Catalog.Pdf

    9-15K Complete Catalog.Pdf

    HEAVY DUTY UTILITY AXLES 9,000 - 15,000 lbs. Capacity www.dexteraxle.com 2900 Industrial Parkway East • Elkhart, IN 46516 Fax: 574-295-8666 • Ph. 574-295-7888 5/10 © 2010 Dexter Axle Company www.dexteraxle.com LIT-123-00 Introduction This information is intended as a guide for the proper specification and application of Dexter Axle running gear, associated components and accessories. Dexter offers a full line of trailer axles that can be used in many different applications. When specifying any pre-engineered components such as axles, it is the responsibility of the trailer designer to insure compatibility with the vehicle and all of its sub-systems. Information The information presented is meant to assist trailer manufacturers in the specification of their running gear components. Dexter Axle does not warrant that the information given constitutes an approved trailer design or application. Dynamic loading, travel requirements unique to the trailer design, unusual service conditions, trailer configurations, unequal load distribution, hitch or coupler arrangements and towing vehicle suspension characteristics can significantly affect the performance of any trailer axle and/or suspension systems. It remains the responsibility of the trailer manufacturer to evaluate, specify and test their trailer/running gear combination before production and to certify it as such. While the information presented at the time of this writing is current, it is subject to change as designs and components evolve over time. Disclaimer of Warranty and Limitation
  • Lancair Legacy RG

    Lancair Legacy RG

    Legacy PILOT’S OPERATING HANDBOOK and AIRPLANE FLIGHT MANUAL for the LEGACY Mfgr’s Serial No. ___________________________ Registration No. ___________________________ Owners will need to develop a Pilot’s Operating Handbook as part of the aircraft airworthiness process, and are encouraged to modify this document to help in that process. Legacy Legacy Published by Lancair International Inc. Redmond, Oregon 97756 Authorized Dealer Neico Aviation Inc. 2244 Airport Way Redmond, Oregon 97756 February 2008 iii Legacy Legacy PILOT’S OPERATING HANDBOOK and AIRPLANE FLIGHT MANUAL February 2008 Log of Revisions PAGES DESCRIPTION February 2008 iii Legacy Legacy INTRODUCTION This Lancair International Pilot’s Operating Handbook and Airplane Flight Manual is in the format and contains most data recommended in the GAMA (General Aviation Manufacturers Association) Handbook Specification Number 1. Use of this specification provides the pilot the same type data in the same place in all of the handbooks. For example, attention is called to Section X, SAFETY INFORMATION. We feel it is very important to have this information in a condensed and readily available location and format for the pilots immediate use when needed. This SAFETY INFORMATION should be read and studied by all opera- tors of the Lancair Legacy aircraft and will provide a periodic review of good piloting techniques for this aircraft. This manual will not replace safe flight instruction or good piloting techniques. NOTE Owner modifications to your Lancair may alter the applicability of this handbook which meets the GAMA specification #1 for pilots operating handbooks. WARNING Use only genuine Lancair approved parts obtained from authorized Lancair dealers when repairing and maintaining your Lancair Legacy.
  • SRAM Hydraulic Disc Brakes Overview

    SRAM Hydraulic Disc Brakes Overview

    HYDRAULIC DISC BRAKES 02 Introduction 03 The Lever 03 The Brake Hose 04 The Caliper OVERVIEW 05 Closed and Open Systems 07 Braking Power 11 Four-Piston Calipers 14 Heat and Fade 16 Care INTRODUCTION HYDRAULIC FACTORS AT WORK IN A DISC BRAKE HYDRAULIC DISC BRAKE Actuation force Leverage A hydraulic disc brake incorporates a (lever squeeze) (mechanical and hydraulic) master piston in the lever, a hydraulic brake DISC BRAKE line, two or more opposing slave pistons in the caliper, and hydraulic fluid (DOT brake A disc brake is comprised of a handlebar- fluid or mineral oil). There are several factors at work when using mounted lever, a frame or fork-mounted Clamping force Brake pad a hydraulic disc brake. The amount of lever caliper, and a hub-mounted rotor. at the caliper material In a hydraulic brake system, braking is actuation combined with the leverage of the When the lever is actuated, a brake accomplished by actuating the lever, which brake lever and hydraulic system create a pad (friction material) clamps onto the advances the master piston inside the lever clamping force at the caliper. That clamping rotor creating a frictional force at the body and forces fluid into the brake hose. force combined with the brake pad material rotor/caliper interface. This frictional Rotor diameter Friction at The fluid then moves into the caliper and produces friction at the rotor. The amount force slows the wheel by converting the the rotor presses against the slave pistons. Brake of friction combined with the diameter of kinetic energy of the spinning wheel into pads are attached to the slave pistons so the rotor generates braking power.
  • New Homebuilts No Renum 2013 to 2014 Xlsx

    New Homebuilts No Renum 2013 to 2014 Xlsx

    N# Registered Manufacturer Registered Model Name Catalog Name S/N 2214 JUNGSTER 1 1 130 440SS SEGA GARY E 5 5 S 94040013 482FD DAVID R DANTONIO 404 404 X69 66EM MATHERNE EWELL P 582 582 158 2428L SALTERS DANIEL L 7B-15 7B-15 001 498NS SHOWKER JAMES S A26 A26 A2610 495PA DANIEL K SAUL ADE RZ-7 ADE RZ-7 1001 967RJ WATKINS ROBERT M AEROBAT 100 AEROBAT 100 1001 101E NELSON ROGER AERONICA T AERONICA T 1 72417 MERLIN D. PEAY HOBBY-COPTER AH 1 AH 1 2001 503NS SHEKLETON NOEL AIR COMMAND 503 AIR COMMAND 503 S-1 175EC CHARLES D REICHERT AL3 AL3 TX-1033 49AX DENNY ROGER A ALASKA 18 ALASKA 18 0050 312TJ BALENTINE THOMAS J ALLIED T J ALLIED T J 023 504WM MARTIN WILLIAM S ALLIED T J ALLIED T J 022 914AG ABID FAROOQUI APOLLO AG1 APOLLO AG1 USA220713 58835 MCKINSTRY JIM H ARESTI GANADOR ARESTI GANADOR JM-4AG 805PV PEACHEY SAM ARION LIGHTNING ARION LIGHTNING 160 87HC JOHN FRANKLIN AURORA BUTTERFLY AURORA BUTTERFLY B146 342DZ DANIEL ZELAZO AUTOGYRO CALIDUS AUTOGYRO CALIDUS C00342 509PH JOSHUA HUMPHREYS AUTOGYRO CAVALON AUTOGYRO CAVALON V00139 509QB MICHAEL BURTON AUTOGYRO CAVALON AUTOGYRO CAVALON V00138 832TX JASON KNIGHT AUTOGYRO GMBH MTO SP AUTOGYRO GMBH MTO SP M01088 271SF JOHN CHEDESTER AUTOGYRO MTO SPORT AUTOGYRO MTO SPORT M01050 504RD RODNEY L DRISKELL AUTOGYRO MTO SPORT AUTOGYRO MTO SPORT M01072 508FM CRAIG MCPHERSON AUTOGYRO MTO SPORT AUTOGYRO MTO SPORT M01096 502NP ALEXANDER ROLINSKI AVENTURA II AVENTURA II AA2A0166 2378E AVIOTEC SRL AVIASTOL AVIASTOL 001 846WT NOBLE TRAVIS E AVID C AVID C 846 341RP PRANGE RICHARD L AVID C PLUS AVID C PLUS 001