1.3.0.12 ECCAIRS Aviation Data Definition Standard
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Project No.: R. 089145.001
Project No.: R. 089145.001 Section 01 01 50 Mission Minimum Institution GENERAL INSTRUCTIONS 33737 Dewdney Trunk Road, Mission, BC Page 1 of 18 EXPANSION OF HEALTH CARE 1 SUMMARY OF WORK .1 Work covered by Contract Documents: .1 Work under this Contract comprises construction of a health care building expansion and renovation work as indicated, located at Mission Minimum Institution, Mission, B.C. .2 Contractor’s Use of Premises: .1 Contractor has controlled use of site within the construction area for Work, storage, and access as directed by the Departmental Representative. .2 Use of areas inside Mission Institution, for access to the construction site is controlled, by the Departmental Representative. .3 Obtain and pay for use of additional storage or work areas needed for operations under this Contract. .4 The new building will be constructed inside the security fence. The institution will be fully operational during work of this Contract. Provide temporary construction fence around site until new security fencing is installed. .3 Conform to National Building Code 2015 or British Columbia Building Code 2012 as applicable. .4 Contractor to apply for Building Permit before construction and Occupancy Permit upon Substantial completion. .1 Departmental Representative will supply the required drawings and Letters of Assurance for such applications. .2 Contractor to pay for all required fees for Building Permit and Occupancy Permit. .3 Before issuing the Substantial Completion certificate, Contractor must provide fire alarm verification report and Occupancy Permit from local authority having jurisdiction. 2 WORK RESTRICTIONS .1 Notify, Departmental Representative of intended interruption of disconnected services and provide schedule for review. -
Bibliography on Ignition and Spark-Ignition Systems
Bibliography on Ignition and Spark-Ignition Systems U.S. Department of Commerce National Bureau of Standards Miscellaneous Publication 251 ; THE NATIONAL BUREAU OF STANDARDS Functions and Activities The functions of the National Bureau of Standards include the developm and maintenance of the national standards of measurement and the provision of means and methods for making measurements consistent with these standards; the determination of physical constants and properties of materials ; the develop- ment of methods and instruments for testing materials, devices, and structures advisory services to government agencies on scientific and technical problems; invention and development of devices to serve special needs of the Government;I and the development of standard practices, codes, and specifications, including assistance to industry, business and consumers in the development and accepi ance of commercial standards and simplified trade practice recommendation!I The work includes basic and applied research, development, engineering, instru- mentation, testing, evaluation, calibration services, and various consultation andd information services. Research projects are also performed for other govern- ment agencies when the work relates to and supplements the basic program of the Bureau or when the Bureau's unique competence is required. The scope of activities is suggested by the listing of divisions and sections on page 26. Publications The results of the Bureau's research are published either in the Burea>au'g own series of publications or in the journals of professional and scientific societies. The Bureau itself publishes three periodicals available from the Gov- ernment Printing Office: The Journal of Research, published in four separai sections, presents complete scientific and technical papers ; the Technical Ne Bulletin presents summary and preliminary reports on work in progress ; a Central Radio Propagation Laboratory Ionospheric Predictions provides da for determining the best frequencies to use for radio communications througho the world. -
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. -
Crab Fishing Vessel Capsizes and Drowns Three Crew Members TIME
FATALITY INVESTIGATION REPORT INCIDENT HIGHLIGHTS DATE: January 19, 2016 Crab fishing vessel capsizes and drowns three crew members TIME: 8:15 p.m. REPORT#: 2016-06-1, 2, 3 REPORT DATE: Mar. 2020 ________________________________________________________ VICTIMS: 52-year-old male Crewman SUMMARY On January 19, 2016, a commercial fishing vessel left a harbor on 37-year-old male Crewman Oregon’s coast with four crewmembers to place crab pots. The 31-year-old male Crewman vessel’s Captain proceeded out, despite being warned about poor INDUSTRY/NAICS CODE: weather conditions and heavy seas. He was escorted across the bar Commercial Fishing/114 by a Coast Guard motor lifeboat. That afternoon while crabbing, the vessel’s external lights failed and the Captain decided to return to EMPLOYER: Commercial Crab Fishing port. While returning across the bar, a wave washed over the stern, capsizing the vessel. It rolled and broke apart on the rock jetty. A SAFETY & TRAINING: rescue locator beacon (Emergency Position Indicating Radio Beacon Safety meetings & training were limited at this or EPIRB) on the vessel activated, and was noted by the local Coast employer Guard station. Search and rescue operations began shortly after. The Captain was thrown from the capsized vessel, swam clear of the SCENE : Employees were returning debris, and was pushed by waves onto the jetty. He found someone from fishing in heavy seas to take him to the Coast Guard station where he reported the and rough weather and the incident. He refused medical treatment and the required drug and vessel capsized. Only the Captain survived. alcohol testing, and left the station. -
Epic Performance for Tнe Entire King Air 200 Family
BEECHCRAFT KING AIR B200GT EPIC PERFORMANCE FOR THE B200 ENTIRE KING AIR 200 FAMILY... 200 ...utilizing Swept Blade Technology Simply more of what you bought your King Air for! THE ELEMENTS OF RAISBECK’S 200-SERIES EPIC PERFORMANCE PACKAGE (Elements available separately) SWEPT BLADE TURBOFAN PROPELLERS RAM AIR RECOVERY SYSTEM ENHANCED PERFORMANCE LEADING EDGES DUAL AFT BODY STRAKES HIGH FLOTATION GEAR DOORS OPTIONAL CROWN WING LOCKERS Diaphragm Seal Particle Separator with flap Ice Shedder Turning Vane Flap Bypass Door Seal Benefits Benefits Benefits Benefits Benefits Benefits • Stunning ramp presence • Significantly increases climb and cruise • Cruise speeds and range are increased • Passenger ride quality is improved • Climb and cruise performance of standard- • FAA-certified to carry 600 pounds total cargo in • Quiet and virtually vibrationless operation performance in both normal and anti-ice • Stall speeds and characteristics are improved • Pilot control and handling qualities are gear King Airs is restored 17 cubic feet of luggage space from takeoff to touchdown operating modes • Air conditioning and cooling are more efficient enhanced • Cruise speed is increased 8 to 12 knots • Returns your cabin to your passengers • Certified around the world to meet the most • Protects against FOD—deployable for all • Outboard wing fatigue life is inherently • Air Minimum Control Speed is inherently depending on altitude • Handles skis, snowboards, camping and stringent regulations and noise requirements ground, takeoff and landing operations -
Dispersant Use Operational Planning & Implementation Guidance 2
APPENDIX VIII TABLE OF CONTENTS SECTION PAGE Dispersant Use Operational Planning & Implementation Guidance 2 • ICS Organization Chart for Dispersant Use 5 • ICS Dispersant Use Organizational Relationships 6 Dispersant Use Decision and Implementation Element Checklist 7 Dispersant Application Platform Capability Decision Matrix 10 Dispersant Application Operational Feasibility Form 12 Dispersant Operation Plan • Dispersant Operation Plan Checklist 13 • Dispersant Effectiveness Monitoring Aerial Checklist 16 • Dispersant Effectiveness Monitoring Waterborne Checklist 17 Dispersant Application Logistics and Support Checklist 18 Documentation/Application Form From Regional Response Team Dispersant Pre-Approval Policy • Region IV Region 20 Incident Command Functional Checklists for Dispersant Use 23 • Dispersant Operation Group Supervisor 24 • Spotter Aircraft / Spotter 26 • Spray Aircraft / Spray Vessel / Sprayer 28 - Sprayer Log Sheet 29 • Monitoring Aircraft / Vessel and Monitor 30 • Observation Aircraft / Vessels/ Observers 31 - Dispersant Observation Job Aid 32 - Dispersant Observation Equipment & Pre-Flight Safety Brief Checklist 34 - Dispersant Observation Final Reporting Form 37 • Common ICS Responsibilities for Each Position 38 Site Safety Plan Template for Dispersant Operations 39 1 ICS ORGANIZATION CHART FOR DISPERSANT USE FOSC or Incident Commanders (Unified Command) Operations Planning Section Section Dispersant SSC/ Operation Group Technical Supervisor Specialists Spotter Aircraft Monitoring Spray Observation Aircraft/Vessel Aircraft/Vessel -
PRELIMINARY KNKT.17.10.31.04 Aircraft
KOMITE NASIONAL KESELAMATAN TRANSPORTASI REPUBLIC OF INDONESIA PRELIMINARY KNKT.17.10.31.04 Aircraft Accident Investigation Report PT. Batik Air Boeing 737-800; PK-LBY Inflight from Jakarta to Medan Republic of Indonesia 24 October 2017 JETPHOTOS.NET Image copyright : Dimas Satrio Baringgo 2017 This Preliminary Report was produced by the Komite Nasional Keselamatan Transportasi (KNKT), Transportation Building, 3rd Floor, Jalan Medan Merdeka Timur No. 5 Jakarta 10110, Indonesia. The report is based upon the initial investigation carried out by the KNKT in accordance with Annex 13 to the Convention on International Civil Aviation Organization, the Indonesian Aviation Act (UU No. 1/2009) and Government Regulation (PP No. 62/2013). The preliminary report consists of factual information collected until the preliminary report published. This report will not include analysis and conclusion. Readers are advised that the KNKT investigates for the sole purpose of enhancing aviation safety. Consequently, the KNKT reports are confined to matters of safety significance and may be misleading if used for any other purpose. As the KNKT believes that safety information is of greatest value if it is passed on for the use of others, readers are encouraged to copy or reprint for further distribution, acknowledging the KNKT as the source. When the KNKT makes recommendations as a result of its investigations or research, safety is its primary consideration. However, the KNKT fully recognizes that the implementation of recommendations arising from its investigations will in some cases incur a cost to the industry. Readers should note that the information in KNKT reports and recommendations is provided to promote aviation safety. -
Wärtsilä 32 PRODUCT GUIDE © Copyright by WÄRTSILÄ FINLAND OY
Wärtsilä 32 PRODUCT GUIDE © Copyright by WÄRTSILÄ FINLAND OY COPYRIGHT © 2021 by WÄRTSILÄ FINLAND OY All rights reserved. No part of this booklet may be reproduced or copied in any form or by any means (electronic, mechanical, graphic, photocopying, recording, taping or other information retrieval systems) without the prior written permission of the copyright owner. THIS PUBLICATION IS DESIGNED TO PROVIDE AN ACCURATE AND AUTHORITATIVE INFORMATION WITH REGARD TO THE SUBJECT-MATTER COVERED AS WAS AVAILABLE AT THE TIME OF PRINTING. HOWEVER, THE PUBLICATION DEALS WITH COMPLICATED TECHNICAL MATTERS SUITED ONLY FOR SPECIALISTS IN THE AREA, AND THE DESIGN OF THE SUBJECT-PRODUCTS IS SUBJECT TO REGULAR IMPROVEMENTS, MODIFICATIONS AND CHANGES. CONSEQUENTLY, THE PUBLISHER AND COPYRIGHT OWNER OF THIS PUBLICATION CAN NOT ACCEPT ANY RESPONSIBILITY OR LIABILITY FOR ANY EVENTUAL ERRORS OR OMISSIONS IN THIS BOOKLET OR FOR DISCREPANCIES ARISING FROM THE FEATURES OF ANY ACTUAL ITEM IN THE RESPECTIVE PRODUCT BEING DIFFERENT FROM THOSE SHOWN IN THIS PUBLICATION. THE PUBLISHER AND COPYRIGHT OWNER SHALL UNDER NO CIRCUMSTANCES BE HELD LIABLE FOR ANY FINANCIAL CONSEQUENTIAL DAMAGES OR OTHER LOSS, OR ANY OTHER DAMAGE OR INJURY, SUFFERED BY ANY PARTY MAKING USE OF THIS PUBLICATION OR THE INFORMATION CONTAINED HEREIN. Wärtsilä 32 Product Guide Introduction Introduction This Product Guide provides data and system proposals for the early design phase of marine engine installations. For contracted projects specific instructions for planning the installation are always delivered. Any data and information herein is subject to revision without notice. This 1/2021 issue replaces all previous issues of the Wärtsilä 32 Project Guides. Issue Published Updates 1/2021 15.03.2021 Technical data updated. -
Model 162 SERIAL NUMBER
Model 162 SERIAL NUMBER Serials 16200001 and On REGISTRATION NUMBER This publication includes the material required to be furnished to the pilot by ASTM F2245. COPYRIGHT © 2009 ORIGINAL ISSUE - 22 JULY 2009 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA REVISION 3 - 28 SEPTEMBER 2010 162PHUS-03 U.S. CESSNA INTRODUCTION MODEL 162 GARMIN G300 PILOT’S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT CESSNA MODEL 162 SERIALS 16200001 AND ON ORIGINAL ISSUE - 22 JULY 2009 REVISION 3 - 28 SEPTEMBER 2010 PART NUMBER: 162PHUS-03 162PHUS-03 U.S. i/ii CESSNA INTRODUCTION MODEL 162 GARMIN G300 CONGRATULATIONS Congratulations on your purchase and welcome to Cessna ownership! Your Cessna has been designed and constructed to give you the most in performance, value and comfort. This Pilot’s Operating Handbook has been prepared as a guide to help you get the most utility from your airplane. It contains information about your airplane’s equipment, operating procedures, performance and suggested service and care. Please study it carefully and use it as a reference. The worldwide Cessna Organization and Cessna Customer Service are prepared to serve you. The following services are offered by each Cessna Service Station: • THE CESSNA AIRPLANE WARRANTIES, which provide coverage for parts and labor, are upheld through Cessna Service Stations worldwide. Warranty provisions and other important information are contained in the Customer Care Handbook supplied with your airplane. The Customer Care Card assigned to you at delivery will establish your eligibility under warranty and should be presented to your local Cessna Service Station at the time of warranty service. • FACTORY TRAINED PERSONNEL to provide you with courteous, expert service. -
19730021074.Pdf
NASA TECHNICAL NOTE NASA TN D-7328 CO LE CORY STEADY-STATE AND DYNAMIC PRESSURE PHENOMENA IN THE PROPULSION SYSTEM OF AN F-111A AIRPLANE by Frank W. Burcbam, Jr., Donald L. Hughes, and Jon K. Holzman Flight Research Center Edwards, Calif. 93523 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • JULY 1973 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA TN D-7328 4. Title and Subtitle 5. Report Date STEADY-STATE AND DYNAMIC PRESSURE PHENOMENA IN THE July 1973 PROPULSION SYSTEM OF AN F-111A AIRPLANE 6. Performing Organization Code 7. Author(s) 8. Performing Organization Report No. Frank W. Burcham, Jr., Donald L. Hughes, and Jon K. Holzman H-741 10. Work Unit No. 9. Performing Organization Name and Address 136-13-08-00-24 NASA Flight Research Center P. O. Box 273 11. Contract or Grant No. Edwards, California 93523 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Technical Note National Aeronautics and Space Administration 14. Sponsoring Agency Code Washington, D. C. 20546 15. Supplementary Notes 16. Abstract Flight tests were conducted with two F-111A airplanes to study the effects of steady-state and dynamic pressure phenomena on the propulsion system. Analysis of over 100 engine compressor stalls revealed that the stalls were caused by high levels of instantaneous distortion. In 73 per- cent of these stalls, the instantaneous circumferential distortion parameter, Kg, exhibited a peak just prior to stall higher than any previous peak. The Kg parameter was a better indicator of stall than the distortion factor, K_, and the maximum-minus-minimum distortion parameter, D, was a poor indicator of stall. -
89Th Meeting of the National Boating Safety Advisory Council
89th Meeting of the National Boating Safety Advisory Council Holiday Inn Arlington Arlington, Virginia April 13-14, 2012 MEMBERS PRESENT: JAMES P. MULDOON Chairman, National Boating Organization Member TOM DOGAN Public Member MIKE FIELDS State Member CHUCK HAWLEY Manufacturer Member JEFF JOHNSON State Member LES JOHNSON National Boating Organization Member BRIAN KEMPF State Member MARCIA KULL Manufacturer Member DAVE MARLOW Manufacturer Member DAN MAXIM Public Member RICHARD MOORE State Member ROB RIPPY Manufacturer Member CHRIS STEC Public Member MEMBERS ABSENT: DICK ROWE Manufacturer Member USCG STAFF: CAPT PAUL THOMAS Deputy Director of Prevention Policy CAPT MARK RIZZO NBSAC Designated Federal Officer; Chief, Office of Auxiliary and Boating Safety JEFF HOEDT Chief, Boating Safety Division, Office of Auxiliary and Boating Safety BRANDI BALDWIN Lifesaving and Fire Safety Division, Office of Design and Engineering Standards MIKE BARON Program Operations Branch, Boating Safety Division VANN BURGESS Program Operations Branch, Boating Safety Division JO CALKIN Program Operations Branch, Boating Safety Division PHIL CAPPEL Chief, Product Assurance Branch, Boating Safety Division JOSEPH CARRO Program Operations Branch, Boating Safety Division CARLIN HERTZ Grants Management Branch, Boating Safety Division PHILIPPE GWET Program Management Branch, Boating Safety Division KURT HEINZ Chief, Lifesaving and Fire Safety Division, Office of Design and Engineering Standards HARRY HOGAN Program Management Branch, Boating Safety Division ED HUNTSMAN -
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