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General Aviation Managing Sumped Aviation Gas (Avgas)
DEPARTMENT OF ENVIRONMENTAL HEALTH HAZARDOUS MATERIALS DIVISION P.O. BOX 129261, SAN DIEGO, CA 92112-9261 Phone: (858) 505-6700 or (800) 253-9933 Fax: (858) 505-6786 www.sdcdeh.org GENERAL AVIATION MANAGING SUMPED AVIATION GAS (AVGAS) County of San Diego Pollution Prevention Summary: Small amounts of AvGas fuel are “sumped” (sampled) during pre-flight safety inspections If safe to do so, clean AvGas may be returned to the aircraft fuel tank AvGas may be recycled by filtering with devices such as the GATS jar AvGas may be repurposed for use in certain motorized ground equipment If not recycled, waste AvGas must be disposed of lawfully as a hazardous waste Any water sumped from a fuel tank must be disposed of lawfully as a hazardous waste If you sump AvGas you must have a legal means of hazardous waste disposal readily available California law prohibits disposing of aviation gasoline (AvGas) to the ground, sewer, or storm drain. Violators are subject to fines up to $25,000 per incident. Refer to the California Health and Safety Code [HSC §25100] for more details. INTRODUCTION According to Federal Aviation Administration (FAA) data, there were approximately 140,000 active piston-powered General Aviation (GA) aircraft in the United States with over 12.9 million hours flown in 2014. Each of those aircraft rely on aviation gas (AvGas) to fuel their engines. AvGas is a highly flammable liquid containing organic lead and is a hazardous material. During the mandatory pre-flight safety inspection, pilots sample the fuel in the aircraft and inspect the fuel for contaminants. -
MANUAL REVISION TRANSMITTAL Manual 146 (61-00-46) Propeller Owner's Manual and Logbook
HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. Telephone: 937.778.4200 Fax: 937.778.4391 MANUAL REVISION TRANSMITTAL Manual 146 (61-00-46) Propeller Owner's Manual and Logbook REVISION 3 dated June 2012 Attached is a copy of Revision 3 to Hartzell Propeller Inc. Manual 146. Page Control Chart for Revision 3: Remove Insert Page No. Page No. COVER AND INSIDE COVER COVER AND INSIDE COVER REVISION HIGHLIGHTS REVISION HIGHLIGHTS pages 5 and 6 pages 5 and 6 SERVICE DOCUMENTS LIST SERVICE DOCUMENTS LIST pages 11 and 12 pages 11 and 12 LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES pages 15 and 16 pages 15 and 16 TABLE OF CONTENTS TABLE OF CONTENTS pages 17 thru 24 pages 17 thru 26 INTRODUCTION INTRODUCTION pages 1-1 thru 1-14 pages 1-1 thru 1-16 DESCRIPTION AND DESCRIPTION AND OPERATION OPERATION pages 2-1 thru 2-20 pages 2-1 thru 2-24 INSTALLATION AND INSTALLATION AND REMOVAL REMOVAL pages 3-1 thru 3-22 pages 3-1 thru 3-24 TESTING AND TESTING AND TROUBLESHOOTING TROUBLESHOOTING pages 4-1 thru 4-10 pages 4-1 thru 4-10 continued on next page Page Control Chart for Revision 3 (continued): Remove Insert Page No. Page No. INSPECTION AND INSPECTION AND CHECK CHECK pages 5-1 thru 5-24 pages 5-1 thru 5-26 MAINTENANCE MAINTENANCE PRACTICES PRACTICES pages 6-1 thru 6-36 pages 6-1 thru 6-38 DE-ICE SYSTEMS DE-ICE SYSTEMS pages 7-1 thru 7-6 pages 7-1 thru 7-6 NOTE 1: When the manual revision has been inserted in the manual, record the information required on the Record of Revisions page in this manual. -
Aviation Maintenance Alerts
ADVISORY CIRCULAR 43-16A AVIATION MAINTENANCE ALERTS ALERT SEPTEMBER NUMBER 2007 350 CONTENTS AIRPLANES BEECH ........................................................................................................................................1 CESSNA ......................................................................................................................................3 MAULE .......................................................................................................................................7 HELICOPTERS EUROCOPTER ...........................................................................................................................7 SIKORSKY..................................................................................................................................7 ACCESSORIES AEROTECH ALTERNATOR.....................................................................................................9 ECI CYLINDER........................................................................................................................10 WIPAIRE...................................................................................................................................10 AIR NOTES INTERNET SERVICE DIFFICULTY REPORTING (iSDR) WEB SITE...............................10 IF YOU WANT TO CONTACT US.........................................................................................11 AVIATION SERVICE DIFFICULTY REPORTS ...................................................................12 September -
Montebello Magic March 2017 Warmth of Winter’S Biggest Fly-In
THE JOURNAL OF THE CANADIAN OWNERS AND PILOTS ASSOCIATION COPAFLIGHT MONTEBELLO MAGIC MARCH 2017 WARMTH of Winter’S BIGGEST FLY-IN COMING UP SHORT THE 850-FOOT INVITATION LOTS OF NEW CLASSIFIED ADS TEENS FLY RV-12 BASICMED VS. CAT 4 CANSO READY TO FLY #42583014 BUILDING CAREERS ON MEDICAL REFORM CELEBRATE WITH M P THE ISLAND COMPARISON FAIRVIEW JUNE 18 NAVITIMER COPA Limited Edition Breitling proudly launches the Navitimer World COPA, a 50-piece limited edition chronograph honoring the Canadian Owners and Pilots Association and perfect for global flight. The Breitling Navitimer has been a favorite among pilots and aviation enthusiasts since it was introduced in 1952 – the same year that COPA was founded. Powered by a COSC-certified selfwinding chronograph movement, this new and exclusive addition to the Navitimer series paying tribute to COPA’s contribution to general aviation features a dial and caseback showcasing the COPA logo. BREITLING.COM COPA_NavitimerGMT_8,5x11inches-BR17480.indd 1 30/05/2016 11:30 COPAFLIGHT EDITOR Russ Niles CONTENTS [email protected] 250.546.6743 GRAPHIC DESIGN Shannon Swanson DISPLAY ADVERTISING SALES Katherine Kjaer 250.592.5331 [email protected] CLASSIFIED ADVERTISING SALES AND PRODUCTION COORDINATOR Maureen Leigh 1.800.656.7598 [email protected] CIRCULATION Maureen Leigh AccOUNTING Anthea Williams ASSISTANT ADMIN Rajei Gill COPA BOARD Bernard Gervais, President and CEO 34 Executive Committee Jean Messier Feature Departments Chair, Quebec Director Bram Tilroe Western Vice-Chair, Alberta -
DLE-20 Operator’S Manual
DLE-20 Operator’s Manual Specifications Displacement: 20cc [1.2cu. in.] Performance: 2.5HP / 9,000 rpm Idle Speed: 1,700 rpm Ignition Style: Electronic Ignition Recommended Propellers: 14u10, 15 u8, 16u6, 16u8, 17u6 Spark Plug Type: CM6 (Gap) 0.018in.– 0.020 in. [0.45mm –0.51mm] Diameter × Stroke: 1.26in. [32mm] u0.98in. [25 mm] Compression Ratio: 10.5 :1 Carburetor: DLE MP 148 100424 with Manual Choke Weight: Main Engine − 1.43 lb [650g] Muffler − 1.76 oz [50 g] Electronic Ignition − 4.23oz [120 g] ™ Fuel: 87− 93 Octane Gasoline with a 30:1 gas/2-stroke (2-cycle) oil mixture 1 © 2010 Hobbico®, Inc. DLEG0020 Mnl Parts List (1) DLE-20cc Gas Engine w/DLE MP 148 100424 (1) DLE Spark Plug (NGK CM6 size) with additional spring (1) Muffl er with gasket (2) 4 x 14 mm SHCS (muffl er mounting) (1) Electronic Ignition Module with additional tachometer lead (1) Silicone Pick-up Wire Cover / Ignition Wire Cover (1) Red Three Pin Connector Lead with Pig Tail (ignition switch) (1) Long Throttle Arm Extension with installation screw and nut (2) Three Pin Connector Securing Clips (1) DLE Decal (not pictured) Safety Tips and Warnings ● This engine is not a toy. Please place your safety and the safety of others paramount while operating. DLE will not be held responsible for any safety issues or accidents involving this engine. ● Operate the engine in a properly ventilated area. ● Before starting the engine, please make sure all components including the propeller and the engine mount are secure and tight. -
Relative Navigation Light Detection and Ranging (LIDAR) Sensor Development Test Objective (DTO) Performance Verification
NASA/TM2013-217992 NESC-RP-11-00753 Relative Navigation Light Detection and Ranging (LIDAR) Sensor Development Test Objective (DTO) Performance Verification Cornelius J. Dennehy/NESC Langley Research Center, Hampton, Virginia May 2013 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and NASA scientific and technical information (STI) technical conferences, symposia, seminars, program plays a key part in helping NASA maintain or other meetings sponsored or co- this important role. sponsored by NASA. The NASA STI program operates under the SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information Officer. technical, or historical information from It collects, organizes, provides for archiving, and NASA programs, projects, and missions, disseminates NASA’s STI. The NASA STI often concerned with subjects having program provides access to the NASA Aeronautics substantial public interest. and Space Database and its public interface, the NASA Technical Report Server, thus providing one TECHNICAL TRANSLATION. of the largest collections of aeronautical and space English-language translations of foreign science STI in the world. Results are published in scientific and technical material pertinent to both non-NASA channels and by NASA in the NASA’s mission. NASA STI Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing specialized research announcements and feeds, TECHNICAL PUBLICATION. Reports of providing information desk and personal search completed research or a major significant phase support, and enabling data exchange services. of research that present the results of NASA Programs and include extensive data or For more information about the NASA STI theoretical analysis. -
Mcdonnell Douglas (Boeing) MD-83
Right MLG failure on landing, Douglas (Boeing) MD-83, EC-FXI Micro-summary: The right main landing gear of this Douglas (Boeing) MD-83 failed immediately on landing. Event Date: 2001-05-10 at 1232 UTC Investigative Body: Aircraft Accident Investigation Board (AAIB), United Kingdom Investigative Body's Web Site: http://www.aaib.dft.gov/uk/ Note: Reprinted by kind permission of the AAIB. Cautions: 1. Accident reports can be and sometimes are revised. Be sure to consult the investigative agency for the latest version before basing anything significant on content (e.g., thesis, research, etc). 2. Readers are advised that each report is a glimpse of events at specific points in time. While broad themes permeate the causal events leading up to crashes, and we can learn from those, the specific regulatory and technological environments can and do change. Your company's flight operations manual is the final authority as to the safe operation of your aircraft! 3. Reports may or may not represent reality. Many many non-scientific factors go into an investigation, including the magnitude of the event, the experience of the investigator, the political climate, relationship with the regulatory authority, technological and recovery capabilities, etc. It is recommended that the reader review all reports analytically. Even a "bad" report can be a very useful launching point for learning. 4. Contact us before reproducing or redistributing a report from this anthology. Individual countries have very differing views on copyright! We can advise you on the steps to follow. Aircraft Accident Reports on DVD, Copyright © 2006 by Flight Simulation Systems, LLC All rights reserved. -
Lighting up to 7 Times Brighter Than Other LED Landing Lights!
Lighting FAA-PMA Approved AeroLEDs Lighting Increase safety and reduce operating cost! See the Difference... Lighting Know the Difference... • Increased safety • Direct replacement • Up to 80% reduced power consumption • Long life - over 50,000 hours! • Lighter weight - no heavy power supply - save up to 3 lbs • Reduced drag • Zero maintenance • 10x more efficient than incandescent! Increased Safety AeroLED lights allow you to comply with the latest FAA recommendations (Operation Lights On) regarding extended use of taxi, landing, and anti-collision lights without fear of reduced light performance or life. They all feature optimized light color (6500k sunlight equivalent) for proven superior air-to-air recognition. The landing and taxi lights also feature an optional pulsed recognition light mode. Reduced Power Consumption High efficiency LED lights use less than 1/3 the power of halogen bulbs. They significantly reduce the load on the electrical system and they won't dim due to low voltage, typical of low RPM final approaches when you need them most! Postition lights aerodynamic design results in less drag than original equipment! Longer Life - Zero Maintenance All AeroLED products are designed to be a "lifetime buy". They last over 50,000 hours when properly installed and do not degrade with on/off cycles. They are extremely rugged and hardened against all kinds of electrical damage, shock, and vibration. Up to 7 times brighter than other LED landing lights! PAR36 Landing Light Comparison Measured Brightness at 50 Ft. Manufacturer Intensity -
Aviation Investigation Report A06q0157 Engine Failure
AVIATION INVESTIGATION REPORT A06Q0157 ENGINE FAILURE CESSNA 172M C-FFRV MONTRÉAL, QUEBEC 10 SEPTEMBER 2006 The Transportation Safety Board of Canada (TSB) investigated this occurrence for the purpose of advancing transportation safety. It is not the function of the Board to assign fault or determine civil or criminal liability. Aviation Investigation Report Engine Failure Cessna 172M C-FFRV Montréal, Quebec 10 September 2006 Report Number A06Q0157 Summary A Cessna 172M, registration C-FFRV, serial number 17262394, with the pilot and two passengers on board, took off at 1545 eastern daylight time from Saint-Hubert Airport, Quebec, for a flight according to visual flight rules over Montréal, Quebec. About 15 minutes after take-off, when the aircraft was over the city, the engine (Lycoming O320-H2AD) lost power and stopped. The pilot tried to restart it, but without success. The pilot transmitted a distress message and quickly reported the situation to the control tower. The aircraft was approximately 1250 feet above ground level at the time. The pilot landed the aircraft on the northbound side of Parc Avenue, in Montréal. On landing, the left wing tip struck a traffic light post before the aircraft came to rest. The aircraft was substantially damaged, but there were no injuries. Ce rapport est également disponible en français. - 2 - Other Factual Information The pilot was certified and qualified for the flight in accordance with existing regulations. He had over 30 years of flying experience, including 22 years on this aircraft, and had about 5000 flying hours. The weather observation taken at 1600 eastern daylight time1 was as follows: visibility 9 statute miles, light winds and a few scattered clouds. -
Tilt Rotor Research Aircraft Familiarization Document
'. NASA TECHNICAL NASA TMX-62.407 MEMORANDUM -PTING Y. a c NASA/ARMY TILT ROTOR RESEARCH AIRCRAFT FAMILIARIZATION DOCUMENT Prepared by .Tilt Rotor Project Office .. .. -\ Coordinated by Martin Maid .. Ames Research Center ._ I rJ - ,.. -1 and , 1-1 c. U.S. Amy Air Mobility R&D Laboratory %\\-'?. \ Moffett Field, Calif. 94035 .-, 7 / --_ ---*_ c-, : January 1975 NASMARMY XV-15 TILT ROTOR RESEARCH AIRCRAFT FAMl LIARIZATION DOCUMENT Prepared by: Tilt Rotor Research Aircraft Project Office Staff Coordinated by: Martin D. Maisel Tilt Rotor Research Aircraft Project Office Approved by : - Dean C. Borgman Deputy Manager, Technical Tilt Rotor Research Aircraft Project Office David D. Few Manager Tilt Rotor Research Aircraft Project Office 1. Report No. 2. Ganmnmt hionNo. 3. Recipient's Catalog No. TM X-62,407 4. Titlr md Subtitlo 5. Rqwn D~te NASA/ARMY XV-15 TILT ROTOR RESEARCH AIRCRAFT FAMILIARIZATION DOCUMENT 7. Author(s) 8. PerformingOrgnizrtion Report No. Prepared by Tilt Rotor Project Office Staff, A-5870 coordinated by Martin Maisel 10. Work Unit No. 9. paforming ororriatia, "and MdNI 744-01-01 NASA Ames Research Center and 11. Canmct or Grant No. U.S. Army Air Mobility R&D Laboratory Moffett Field, Calif. 94035 13. Typ of RIpon and hid &ard 12. -nuring N.m md Addnr Technical Memorandum National Aeronautics and Space Administration 1;. Sponsoring Agmcy Code Washington, D.C. 20546 16. Abmrcr , The design features and general characteristics of the NASA/Army XV-15 Tilt Rotor Research Aircraft are described. This aircraft was conceived as a proof-of-concept vehicle and a V/STOL research tool for integrated wind tunnel, flight-simulation, and flight-test investigations. -
Large Capacity Oblique All-Wing Transport Aircraft
f Large Capacity Oblique All-Wing Transport Aircraft Thomas L. Galloway James A. Phillips Robert A. Kennelly, Jr. NASA Ames Research Center Moffett Field, CA Mr. Mark H. Waters Thermosciences Institute, ELORET Corp. Palo Alto, CA Transportation Beyond 2000: Engineering Design for the Future September 26-28, 1995 461 INTRODUCTION Dr. R. T. Jones first developed the theory for oblique wing aircraft in 1952, and in subsequent years numerous analytical and experimental projects conducted at NASA Ames and elsewhere have established that the Jones' oblique wing theory is correct. Until the late 1980's all proposed oblique wing configurations were wing/body aircraft with the wing mounted on a pivot. With the emerging requirement for commercial transports with very large payloads, 450 - 800 passengers, Jones proposed a supersonic oblique flying wing in 1988. For such an aircraft all payload, fuel, and systems are carded within the wing, and the wing is designed with a variable sweep to maintain a fixed subsonic normal Mach number. Engines and vertical tails are mounted on pivots supported from the primary structure of the wing. The oblique flying wing transport has come to be known as the Oblique All-Wing transport (OAW). Initial studies of the OAW were conducted by Van der Velden first at U.C. Berkeley(l) in 1989 and then at Stanford in collaboration with Kroo(2) in 1990. A final document summarizing this work is given in the thesis by Van der Velden(3). Many issues regarding the design were identified in these studies, among them the need for the OAW to be an unstable aircraft. -
Cessna 210 Back in The
HANGAR ECHOES September 2018 cessna 210 back in the air From Michael Stephan Experimental Aircraft Association! ! Chapter 168 ! Dallas With great fanfare, I am proud to announce that Ted Harrison’s “backyard” Article Index Cessna 210 is now flying. Actually it first Ted Harrison’s 210 Cover flew on May 25. Since that day it has spent time at the avionics show having Monthly Schedule page2 some modern Garmin avionics installled Presidents Message page 3 in the center stack, including a ADS-B In/ N168TX Sold page 3 Out compliant transponder installed. Then it was off to the paint shop. The 210 Walt Aronow Page 4 spent a few weeks at GLO Custom at Don Pellegreno Page 6 Northwest Regional Airport. Induction Leaks Page 7 Ted has been in aviation most of his life. FltPlan.com Page8 As a youngster Ted learned to fly in his Local Fly Ins Page 8 Dad’s Aeronca sedan. His cut his communication teeth on a narco “coffee Project Updates Page 9 grinder” that had three crystals. Once he Tool List PG 10 learned to solo, Ted would fly from Upcoming Events PG 10 Payson AZ, where he lived, to Falcon Field (east of Pheonix) for his flight For Sale PG 11 lessons. Since every lesson consisted of a September 2018 Volume 49 Issue 9 Page 1 HANGAR ECHOES Monthly Schedule Sept 4th Chapter Meeting September 4th Board Meeting The September Chapter meeting The September BOD meeting will be held on Tues Sept will be on Tuesday Sept 4th at 4th in Farmers Branch Library Auditorium at 5:30pm.