Toxicological Profile for Hydraulic Fluids
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Sl Premium Universal Tractor Hydraulic Fluid
UNIVERSAL TRACTOR HYDRAULIC FLUID Sinclair Universal Tractor Fluid is a premium quality universal tractor hydraulic fluid formulated with high quality base oils and anti-wear and extreme pressure (EP) additives providing excellent load carrying capacity and wear protection for a wide temperature range and long-term service under severe conditions. It is designed for equipment using a common sump or requiring a single fluid for hydraulic systems, transmission, differential, wet brakes/wet clutches, power take off (PTO) units and final drive. Sinclair Universal Tractor Fluid protects against foam and corrosion and resists the negative effects of water contamination and is highly resistant to oxidation. APPLICATIONS Sinclair Universal Tractor Fluid meets or exceeds most tractor manufacturers’ specifications and can be used where any of the following are specified: • AGCO, Allis Chalmers & Deutz-Allis: 821XL • Massey Ferguson: Permatran III, M-1141 • John Deere: J20C, J20A, J14B, J21A, • Ford M2C134C/D, FNHA-2-C-200.00, M2C86-B, M2C41-B Hygard, 303 Fluid • White: Q1826, Q1705, Q1766, Q1802 • Case International Harvester: MS 1209 (Hy-Tran ULTRA), MS 1207 • Caterpillar: TO-2 (Hy-Tran Plus), MS 1210 (TCH Fluid), MS-1206, MS1230, JIC-144, JIC-143 • Allison: C-4 Fluid • Oliver: Type 55, Universal HTF, Q1766 • Renk 873 and 874 A/B Transmissions • International Harvester: B-6 • Kubota: UDT • Minneapolis-Moline Fluids UNIVERSAL TRACTOR HYDRAULIC FLUID TYPICAL PHYSICAL PROPERTIES METHOD TYPICAL RESULTS Viscosity Grade Universal Tractor Hydraulic Fluid Gravity, °API ASTM D287 30.99 Specific Gravity @ 60°F (15.6°C) ASTM D4052 0.8708 Viscosity @ 40°C cSt ASTM D445 59.34 Viscosity @ 100°C cSt ASTM D445 9.34 Viscosity Index ASTM D2270 138 Pour Point °C (°F) ASTM D5950 -42C (-44 F) Brookfield Viscosity at -35°C, cP ASTM D2983 37,292 Brookfield Viscosity at -20°C, cP ASTM D2983 3,819 Color ASTM D1500 2 Zinc, wt. -
Hydraulic Fluids 1
HYDRAULIC FLUIDS 1 1. PUBLIC HEALTH STATEMENT This public health statement tells you about hydraulic fluids and the effects of exposure. The Environmental Protection Agency (EPA) identifies the most serious hazardous waste sites in the nation. These sites make up the National Priorities List (NPL) and are the sites targeted for long-term federal cleanup. Hydraulic fluids have been found in at least 10 of the 1,428 current or former NPL sites. However, it’s unknown how many NPL sites have been evaluated for these substances. As more sites are evaluated, the sites with hydraulic fluids may increase. This is important because exposure to these substances may harm you and because these sites may be sources of exposure. When a substance is released from a large area, such as an industrial plant, or from a container, such as a drum or bottle, it enters the environment. This release does not always lead to exposure. You are exposed to a substance only when you come in contact with it. You may be exposed by breathing, eating, or drinking the substance or by skin contact. If you are exposed to hydraulic fluids, many factors determine whether you’ll be harmed. These factors include the dose (how much), the duration (how long), and how you come in contact with it. You must also consider the other chemicals you’re exposed to and your age, sex, diet, family traits, lifestyle, and state of health. 1 .1 WHAT ARE HYDRAULIC FLUIDS? Hydraulic fluids are a very large class of materials that are used in machines and equipment to. -
Mk 7 Aircraft Recovery Equipment
CHAPTER 3 MK 7 AIRCRAFT RECOVERY EQUIPMENT Present-day aircraft normally require the use of then opened, allowing fluid to be forced from the runways that are 5,000 to 8,000 feet long in order to accumulator back into the engine cylinder, forcing the land ashore. On an aircraft carrier, these same aircraft ram out. As the ram moves out of the cylinder, the are stopped within 350 feet after contacting the deck. crosshead is forced away from the fixed sheave This feat is accomplished through the use of aircraft assembly, pulling the purchase cables back onto the recovery equipment, including an emergency barricade engine until the crosshead is returned to its BATTERY that brings a landing aircraft to a controlled stop by position and the crossdeck pendant is in its normal absorbing and dispelling the energy developed by the position on the flight deck. landing aircraft. This recovery equipment is commonly called arresting gear. PRERECOVERY PREPARATIONS The sole purpose of an aircraft carrier is to provide Prior to recovery of aircraft, all recovery equipment a means of launching a strike against an enemy and landing area must be made ready and all personnel anywhere in the world. After the aircraft complete their properly positioned. The following is a general listing mission, the carrier must provide a means of safely of the events that must be accomplished prior to the recovering them. The Mk 7 arresting gear provides this recovery of aircraft: means. • All operational retractable sheaves raised to the full up position AIRCRAFT RECOVERY • LEARNING OBJECTIVE: Describe aircraft All aft deckedge antennas positioned, as arrestments aboard aircraft carriers. -
NOTICE FEDERAL AVIATION ADMINISTRATION Effective Date: National Policy 8/3/16 Cancellation Date: 8/3/17
U.S. DEPARTMENT OF TRANSPORTATION N 8900.374 NOTICE FEDERAL AVIATION ADMINISTRATION Effective Date: National Policy 8/3/16 Cancellation Date: 8/3/17 SUBJ: Revised FAA-Approved Deicing Program Updates, Winter 2016-2017 1. Purpose of This Notice. This notice provides inspectors with information on holdover times (HOT) and recommendations on various other ground deicing/anti-icing issues. 2. Audience. The primary audience for this notice is Flight Standards District Office (FSDO) principal operations inspectors (POI) responsible for approving an air carrier’s deicing program. The secondary audience includes Flight Standards Service (AFS) personnel in FSDOs, branches, and divisions in the regions and at headquarters (HQ). 3. Where You Can Find This Notice. You can find this notice on the MyFAA employee Web site at https://employees.faa.gov/tools_resources/orders_notices. Inspectors can access this notice through the Flight Standards Information Management System (FSIMS) at http://fsims.avs.faa.gov. Operators can find this notice on the Federal Aviation Administration’s (FAA) Web site at http://fsims.faa.gov. This notice is available to the public at http://www.faa.gov/regulations_policies/orders_notices. Note: The FAA Holdover Time Guidelines for 2016-2017 and related tables referenced in this document can be found on the Air Transportation Division’s (AFS-200) Aircraft Ground Deicing Web site at http://www.faa.gov/other_visit/ aviation_industry/airline_operators/airline_safety/deicing. 4. Cancellation. Notice N 8900.335, Revised FAA-Approved Deicing Program Updates, Winter 2015-2016, dated November 18, 2015, is canceled. 5. Background. Title 14 of the Code of Federal Regulations (14 CFR) part 121, § 121.629(c) requires that part 121 certificate holders have an approved ground deicing/anti-icing program. -
Environmental Health Criteria 110 Tricresyl Phosphate
Environmental Health Criteria 110 Tricresyl phosphate Please note that the layout and pagination of this web version are not identical with the printed version. Tricresyl phosphate (EHC 110, 1990) INTERNATIONAL PROGRAMME ON CHEMICAL SAFETY ENVIRONMENTAL HEALTH CRITERIA 110 TRICRESYL PHOSPHATE This report contains the collective views of an international group of experts and does not necessarily represent the decisions or the stated policy of the United Nations Environment Programme, the International Labour Organisation, or the World Health Organization. Published under the joint sponsorship of the United Nations Environment Programme, the International Labour Organisation, and the World Health Organization World Health Orgnization Geneva, 1990 The International Programme on Chemical Safety (IPCS) is a joint venture of the United Nations Environment Programme, the International Labour Organisation, and the World Health Organization. The main objective of the IPCS is to carry out and disseminate evaluations of the effects of chemicals on human health and the quality of the environment. Supporting activities include the development of epidemiological, experimental laboratory, and risk-assessment methods that could produce internationally comparable results, and the development of manpower in the field of toxicology. Other activities carried out by the IPCS include the development of know-how for coping with chemical accidents, coordination of laboratory testing and epidemiological studies, and promotion of research on the mechanisms of the biological action of chemicals. WHO Library Cataloguing in Publication Data Tricresyl phosphate. (Environmental health criteria ; 110) 1.Tritolyl phosphates - adverse effects 2.Tritolyl phosphates - toxicity I.Series Page 1 of 84 Tricresyl phosphate (EHC 110, 1990) ISBN 92 4 157110 1 (NLM Classification: QV 627) ISSN 0250-863X The World Health Organization welcomes requests for permission to reproduce or translate its publications, in part or in full. -
Hydraulic Fluid Quick Reference Hägglunds Products
RE 15414/08.2019 Replaces: 01.2015 Hydraulic fluid quick reference Hägglunds products Contents 1 Hydraulic fluid quick reference 2 1.1 Applicable fluids 2 1.2 Viscosity Limits 3 1.3 Down-rating 3 1.4 Seal and primer compatibility 3 1.5 Additional demands 4 RE 15414/08.2019, Bosch Rexroth AB 2/4 Hägglunds products | Hydraulic fluid quick reference 1 Hydraulic fluid quick reference 1.1 Applicable fluids Only hydraulic fluids by the standards given in Table 1 are Bosch Rexroth’s Hägglunds radial piston hydraulic motors suggested. Fluids complying to other standards only, are are primarily designed to operate on conventional petro- not approved. leum based hydraulic fluids. Table 1: Standards for detailed requirements of respective fluid group. To get a well working drive system it is very important to ISO 11158 ISO 15380 ISO 12922 follow the recommendations given in this instruction. Mineral oil based and Environmentally Fire resistant Improper hydraulic fluid might cause a shorter service life mineral oil related acceptable hydraulic hydraulic fluids or in worst case lead to instant failure. hydraulic fluids fluids Within these standards, not all fluid classes are allowed, and only some are recommended (see Table 2). NOTICE Wrong hydraulic fluid for Hägglunds motors Table 2: Applicable fluids by designation according to ISO 6743-4. Risk of damage to equipment and impact on service Recommended Allowed Not allowed life for Hägglunds motors HM HV [mineral] 1) HH ▶ Fluids HFDU other than polyol esters are not allowed HV no VI improver HEPR HL [e.g. PAO] HEES [saturated] HETG HR Wrong hydraulic fluid for Hägglunds accessories HEES [un-saturated] HG Risk of damage to equipment and impact on service life HFB 2) 3) HFA for accessories Hägglunds MDA brakes (HFAE and HFAS) ▶ Fluids HFB, HFC and HFD are not allowed HFC 2) 3) HEPG HFDU 2) 3) 5) HFDU [Non-polyol ester] HFDR 2) 3) 4) Wrong hydraulic fluid for CBm motors Risk of damage to equipment and impact on service life 1) Recommended to be without VI improver. -
Operator's Manual
OPERATOR'S MANUAL WE225, WE235 Trailer Wood Splitter Rev May-2019 Part Number: Z97112_En WE225, WE235 Introduction Trailer Wood Splitter 1. Introduction Review all safety, operation and maintenance information contained in this manual. 1.1 Foreword WARNING! Congratulations on choosing a Wallenstein Trailer Wood Do not attempt to start or operate the machine Splitter! without thoroughly reviewing this manual for This high-quality machine is designed and manufactured safe and proper operation. to meet the needs of an efficient wood splitting operation. Keep this manual with the machine at all times. This manual covers the Wallenstein 20 ton WE Series W034 trailer wood splitters. Model Variants Covered in this Manual • WE225 (Horizontal splitting only) • WE235 (Horizontal and vertical splitting) Units of measurement in Wallenstein Equipment technical manuals are written as: US Customary (SI metric) Keep this manual handy for frequent reference and to pass on to new operators or owners. Call your Wallenstein dealer or distributor if you need assistance, information or additional copies of the manuals. Wallenstein Equipment Inc. • © 2019 www.wallensteinequipment.com 2 WE225, WE235 Trailer Wood Splitter Introduction Table of Contents 1. Introduction ............................................................2 7. Storing the Wood Splitter ...................................32 1.1 Foreword .........................................................2 7.1 Removing from Storage .................................32 1.2 Delivery Inspection Report ..............................4 -
80, 70, 65 SERIES QUEEN AIR Ground Handling Anti-Ice Reservoir
80, 70, 65 SERIES QUEEN AIR Ground Handling Anti-ice Reservoir Access to the anti-ice reservoir is gained by opening a panel located in the left wing, between the nacelle and the fuselage. Capacity: 3 gals.; Fluid type: Spec TT-I-735 Battery The aircraft electrical system utilizes a 24V, Ni-Cad battery, located in the left engine nacelle behind the firewall. Access is gained by removing the electrical equipment compartment door. NOTE: There are two optional installations where the battery may be on the left forward side of baggage compartment and accessible through the left baggage door, or in the nosecone and accessible by removing the nosecone. Emergency Exits Left rear cabin door. Rear cabin window on right side has emergency release. External Power An external power receptacle is located on the outboard side of the left engine nacelle and uses a standard AN-type plug. This aircraft requires a 28V, DC, negative ground power unit. CAUTION: Battery switch must be ON and all electrical switches OFF prior to connecting ground power unit plug; assure that avionics power is OFF prior to turning the ground power unit ON. Battery must be ON anytime ground power unit is in use. Alternator or generator switch must be OFF while using external power. Fueling Standard configuration incorporates one main G tank and two aux tanks in each wing. The main tank is located inboard of the engine nacelles and the aux tanks are outboard. There are also two optional fuel configurations which may have been used. System capacity: LEADING MAINS EDGE AUXS BOX SECTION AUX Std. -
Southern Music and the Seamier Side of the Rural South Cecil Kirk Hutson Iowa State University
Iowa State University Capstones, Theses and Retrospective Theses and Dissertations Dissertations 1995 The ad rker side of Dixie: southern music and the seamier side of the rural South Cecil Kirk Hutson Iowa State University Follow this and additional works at: https://lib.dr.iastate.edu/rtd Part of the Folklore Commons, Music Commons, Social and Cultural Anthropology Commons, and the United States History Commons Recommended Citation Hutson, Cecil Kirk, "The ad rker side of Dixie: southern music and the seamier side of the rural South " (1995). Retrospective Theses and Dissertations. 10912. https://lib.dr.iastate.edu/rtd/10912 This Dissertation is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Retrospective Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. INFORMATION TO USERS This manuscript has been reproduced from the microfilm master. UMI films the text directly from the original or copy submitted. Thus, some thesis and dissertation copies are in typewriter face, while others may be from any type of computer printer. The quality of this reproduction is dependent upon the quality of the copy submitted. Broken or indistinct print, colored or poor quality illustrations and photographs, print bleedthiough, substandard margins, and improper alignment can adversely affect reproductioiL In the unlikely event that the author did not send UMI a complete manuscript and there are missing pages, these will be noted. Also, if unauthorized copyright material had to be removed, a note will indicate the deletion. -
Hydraulic Power Units
STANDARD HYDRAULIC POWER UNITS NV - VERTICAL STYLE POWER UNIT NH - HORIZONTAL STYLE POWER UNIT NSP STYLE POWER UNIT Table of Contents NV VERTICAL STYLE POWER UNIT....................................................................Page General Information...................................................................................................................................3 Technical Information - Table “A” & “B”.................................................................................................4 How-to-Order - Reservoir.............................................................................................................................5 How-to-Order - Manifold..............................................................................................................................6 Unit Specification Work Sheet..................................................................................................................7 Hydraulic Schematics.................................................................................................................................8 Unit Drawing..........................................................................................................................................9-10 Manifold Dimensional Information.........................................................................................................11 Optional Component Information and Bolt Kit Model Numbers.........................................................12 NH HORIZONTAL STYLE POWER -
Research Article Modeling and Simulation of Arresting Gear System with Multibody Dynamic Approach
Hindawi Publishing Corporation Mathematical Problems in Engineering Volume 2013, Article ID 867012, 12 pages http://dx.doi.org/10.1155/2013/867012 Research Article Modeling and Simulation of Arresting Gear System with Multibody Dynamic Approach Wenhou Shen,1,2 Zhihua Zhao,1 Gexue Ren,1 and Jiapeng Liu1 1 Tsinghua University, Beijing 100084, China 2 Naval Aviation Institute, Huludao 125001, China Correspondence should be addressed to Wenhou Shen; [email protected] Received 17 July 2013; Revised 19 September 2013; Accepted 19 September 2013 Academic Editor: Song Cen Copyright © 2013 Wenhou Shen et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. The arresting dynamics of the aircraft on the aircraft carrier involves both a transient wave propagation process in rope and a smooth decelerating of aircraft. This brings great challenge on simulating the whole process since the former one needs small time-step to guarantee the stability, while the later needs large time-step to reduce calculation time. To solve this problem, this paper proposes a full-scale multibody dynamics model of arresting gear system making use of variable time-step integration scheme. Especially, a kind of new cable element that is capable of describing the arbitrary large displacement and rotation in three-dimensional space is adopted to mesh the wire cables, and damping force is used to model the effect of hydraulic system. Then, the stress of the wire ropes during the landing process is studied. Results show that propagation, reflection, and superposition of the stress wave between the deck sheaves contribute mainly to the peak value of stress. -
Challenger 300 Flight Crew Operating Manual (Volume 2)
HYDRAULICS Table of Contents Introduction ......................................................................................................................... 13-01-01 Left and Right Hydraulic System ......................................................................................... 13-01-01 Description................................................................................................................. 13-01-02 Components and Operation....................................................................................... 13-01-03 Engine-Driven Pumps ................................................................................................ 13-01-03 DC Motor-Driven Pump.............................................................................................. 13-01-03 Hydraulic Shutoff Valve.............................................................................................. 13-01-03 Hydraulic Reservoir.................................................................................................... 13-01-03 Ecology Bottle ............................................................................................................ 13-01-04 Unloading of Hydraulic Pump for Inflight Restarts ..................................................... 13-01-04 Left and Right Hydraulic System Cooling ..................................................................13-01-04 Hydraulic Reservoir Quantity Percentages ................................................................ 13-01-04 Left Hydraulic System