2016 Program Guide
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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 -
Lancair Tigress
Lancair Tigress We found one dictionary with English definitions that includes the word lancair tigress: Click on the first link on a line below to go directly to a page where "lancair tigress" is defined. General (1 matching dictionary). Lancair Tigress: Wikipedia, the Free Encyclopedia [home, info]. ▸ Words similar to lancair tigress. ▸ Words that often appear near lancair tigress. ▸ Rhymes of lancair tigress. ▸ Invented words related to lancair tigress. Search for lancair tigress on Google or Wikipedia. Manufacturing the Lancair MAKO, a new 4-seat aircraft from a legendary company. Explore Preowned Lancair Kits. Genuine. Lancair Parts & Accessories. FACTORY PARTS. Meet the Lancair Family of Aircraft. Over 3 Decades of Aviation Innovation. Lancair 320-360. The Lancair Tigress was an American homebuilt aircraft that was designed by Lance Neibauer and intended for production by Lancair of Redmond, Oregon. Introduced in mid-late 1990s, it was essentially a Lancair IV with a much more powerful engine. When the engine was cancelled just as it was entering production, the Tigress project ended with it. Only prototypes were produced.[1]. For faster navigation, this Iframe is preloading the Wikiwand page for Lancair Tigress. Home. News. Category:Lancair Tigress. From Wikimedia Commons, the free media repository. Jump to: navigation, search. Media in category "Lancair Tigress". This category contains only the following file. The Civil Aerospace Medical Institute.jpg 1,200 × 795; 1.02 MB. Retrieved from "https://commons.wikimedia.org/w/index.php? title=Category:Lancair_Tigress&oldid=208852982". Lancair Tigress. Model year. Production years. Format You get all formats when you buy the drawing. -
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 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 -
Oxygen Systems
2006_594-603.qxd 6/28/06 8:16 PM Page 594 OXYGENOXYGEN SYSTEMS SYSTEMS AEROX HIGH-DURATION AEROX PRO-O2 EMERGENCY CM AVIATION OXYGEN SYSTEMS HANDHELD OXYGEN SYSTEMS Prior to the introduction of the Aerox sys- tem, the wise pilot reserved the use of The Aerox Pro-O2 is refillable and light- oxygen for situations where it was legal- weight, emergency handheld oxygen system. ly necessary, i.e. above 12,500 ft. This In the event that the primary oxygen system WP was often a practical decision based upon factors like: Short duration of sup- fails, the Pro-O2 emergency handheld oxy- ply, uncomfortable masks, difficult and gen system provides oxxygen until the air- costly refills, heavy weight and large craft can reach a lower altitude. And because bulk. Aerox systems remove the forego- Aerox 2D system Aerox 4M system ing objections, plus one more. The price Pro-O2 is refillable, there is no need to pur- ME is right. Add to your flying comfort by chase replacement O2 cartridges. using oxygen at altitudes as low as 5000 ft. Aerox Oxygen Systems include light- During short flights at altitudes between weight aluminum cylinders, regulators, all hardware, flow meter, and nasal can- 12,500ft. MSL and 14,000ft. MSL where HA nulas (masks available as option). maneuvering over mountains or turbulent Oxysaver oxygen saving cannulas & Aerox Flow Control Regulators weather is necessary, the Pro-O2 emergency increase the duration of oxygen supply about 4 times, and prevent nasal irritation and dryness. Complete brochure available on request. handheld oxygen system provides oxygen to extend these brief legs. -
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. -
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. -
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 -
Revised Listing of Amateur Built Aircraft Kits
REVISED LISTING OF AMATEUR-BUILT AIRCRAFT KITS Updated on: June 22, 2021 The following is a revised listing of aircraft kits that have been evaluated and found eligible in meeting the “major portion” requirement of Title 14, Code of Federal Regulations (14 CFR) Part 21, Certification Procedures for Products and Parts, specifically, § 21.191(g). • This listing is only representative of those kits where the kit manufacturer or distributor requested an evaluation by the Federal Aviation Administration (FAA) for eligibility and should not be construed as meaning the kit(s) are FAA “certified,” “certificated,” or “approved.” • There are other aircraft kits that may allow a builder to meet the “major portion” requirement of § 21.191(g), but those manufacturers or distributors have not requested an FAA evaluation. • The placement of an aircraft kit on this list is not a prerequisite for airworthiness certification. • The primary purpose of this listing is to assist FAA Inspectors/Designees and other interested individuals by eliminating the duplication of evaluations for “major portion” determination when the aircraft is presented for airworthiness certification as an “Amateur-Built Experimental.” • Kit manufacturers or distributors whose status is unknown are identified with a question (?) mark and their address has been deleted. Additional Information and Guidance • Advisory Circular (AC) 20-27G, Certification and Operation of Amateur-Built Aircraft. • FAA Order 8130.35B, Amateur-Built Aircraft National Kit Evaluation Team • Contact your local FAA Flight Standards District Office (FSDO) or Manufacturing Inspection District Office (MIDO). Those publications and other information pertaining to amateur-built experimental aircraft are available online at http://www.faa.gov/aircraft. -
Manufacturer Model/Variation AASI Jetcruiser AC Design Stallion AC
Manufacturer Model/Variation AASI Jetcruiser AC Design Stallion AC Design Stallion 2 ACA 7-ECA Citabria Aurora ACA 7-GCAA Adventure ACA 7-GCBC Explorer ACA 8-GCBC Super Decathlon ACA 8-KCAB ACA Adventure Ace Aircraft Ace_front Ace Aircraft Ace_second AcroSport Acrosport 2 AdventureAir Adventurer Aero L-39_FCP Aero L-39_RCP Aeroalcool Quasar AeroCad AeroCanard AeroCad AeroCanard-round AeroCad AeroCanard-wide AeroCanard AeroCanard Left Panel AeroCanard AeroCanard Right Panel Aerocomp CompMonster (CompAir 6) AeroDesign Pulsar Aerospool WT9-Dynamic Aerotronics Elshire Air Tractor AT 802 Front Air Tractor AT 802 Rear Air Tractor AT 802 Side Air Tractor AT 802 Rear Side Aircraft Tech Atlantis Alpha Aviation 160A Alpha Aviation 160A Alt American Legend AL11C Legend Cub American Legend AL3C Legend Cub Arion Lightning Avid Bandit Avid Catalina Avid MK-4 Avid Magnum Avitat 35218-2G Avitat 37220-2 Bearhawk Patrol Bede BD-5 Beechcraft A36 Beechcraft A36-84 Beechcraft B200 Beechcraft BE 35G Beechcraft BE 55-69 Beechcraft BE 95 Beechcraft Baron 58 Beechcraft Baron TC Beechcraft Baron TE Beechcraft Beech 18 Beechcraft Beech 35H Beechcraft Beech 58 Beechcraft Bonanza Beechcraft Bonanza 74 Beechcraft C 23 Beechcraft C E F 33 Beechcraft Duchess Beechcraft Duke 60 Beechcraft Duke Subpanels Beechcraft KingAir 90 Beechcraft T 34 Beechcraft T 34-1 Beechcraft Twin Bonanza Beechcraft KingAir B200 Beechcraft KingAir 200 subpanel Beechcraft Beechjet with glare shield Beechcraft Beechjet no glare shield Beechcraft KingAirC90A right Beechcraft KingAirC90A left Beechcraft -
Aircraft Towing Vehicle Ap88 Series Ap89 Series
AIRCRAFT TOWING VEHICLE AP88 SERIES AP89 SERIES TABLEProperty OF ofCAPTURE American METHOD Airlines BY AIRCRAFT TYPE Capture Table 01 Nov. 2016 TABLE OF CAPTURE METHOD BY AIRCRAFT TYPE - AP88 - AP89 SERIES Chapter 2b Intentionally left blank Property of American Airlines LEKTRO PAGE 2b - 2 01 Nov. 2016 TABLE OF CAPTURE METHOD BY AIRCRAFT TYPE - AP88 - AP89 SERIES Chapter 2b TABLE OF CAPTURE 1 Table Key ........................................................................................................................3 2 Table of Capture by Aircraft type ...................................................................................5 Property of American Airlines LEKTRO PAGE 2b - 3 01 Nov. 2016 TABLE OF CAPTURE METHOD BY AIRCRAFT TYPE - AP88 - AP89 SERIES Chapter 2b 2b Table of Capture Method by Aircraft Type: .01 Table Key The table on the following pages is intended to provide general planning and operational guidelines to define tug model capability, capture method and special adapters and / or precautions for specific aircraft model, weight range and nose/tail wheel design. CAUTION: Final verification must be based on the actual aircraft weight, load distribution, undercarriage condition and ramp condition at the time of towing. Table Key: MAKE = Manufacturer (Original Equipment Manufacturer (OEM) /licensee/ upgrader). MODEL= Specific aircraft model or comparable / derivative series. MTOW= Maximum take off weight. Highest weight in each series is used. NOTE: Max Ramp Weight (including taxi fuel) which exceeds MTOW by a small margin may be substituted. (See note 1). OEW = Operating empty weight. Heaviest version is shown. E.g.: Passenger version over cargo version. If the OEW is not avail- able, empty weight with equipment is used. NOTE 1: If two (2) values, separated by a "-" or "/" are shown, the values are interpreted in the following manner: - = Multiple values within the weight range. -
Valid Business Aircraft Types for Toronto Pearson
Valid Business Aircraft Types for Toronto Pearson type mfgr model JUN1 KAMINSKAS Jungster 1 JUN2 KAMINSKAS Jungster 2 A002 IRKUT A-002 A1 DOUGLAS AD Skyraider A10 FAIRCHILD (1) OA-10 Thunderbolt 2 A109 AGUSTA Grand A119 AGUSTA AW-119 Koala A122 AEROTEC (1) A-122 Uirapuru A124 ANTONOV An-124 Ruslan A129 AGUSTA T-129 A139 AGUSTAWESTLAND AW-139 A140 ANTONOV An-140 A148 ANTONOV An-148 A149 AGUSTA AW-149 A158 ANTONOV An-158 A16 AVIADESIGN A-16 Sport Falcon A169 AGUSTAWESTLAND AW-169 A178 ANTONOV An-178 A189 AGUSTAWESTLAND AW-189 A19 AEROPRACT A-19 A19N AIRBUS A-319neo A20 DOUGLAS A-20 Havoc A205 OSKBES-MAI MAI-205 A20J SCHLEICHER ASW-20J A20N AIRBUS A-320neo A21 AEROPRACT Solo A210 AQUILA AT-01 A211 ALFA-M A-211 A21N AIRBUS A-321neo A22 SADLER Piranha A223 OSKBES-MAI Kityonok A225 ANTONOV An-225 Mriya A23 AEROPRACT Dragon A25 AEROPRACT A-25 Breeze A251 AVIATIK-ALYANS Aleks-251 A27 AEROPRACT A-27 A270 AERO (2) Ibis A29 AVANTAGE A-29 A2RT KAZAN Ansat 2RT A3 DOUGLAS A-3 Skywarrior A306 AIRBUS A-300B4-600 A30B AIRBUS A-300B2 A31 AVANTAGE Spectrum A310 AIRBUS Polaris A318 AIRBUS Elite A319 AIRBUS VC-1 ACJ A320 AIRBUS A-320 Prestige A321 AIRBUS A-321 A33 AEROPRACT A-33 A332 AIRBUS Voyager A333 AIRBUS A-330-300 A337 AIRBUS A-330-700 Beluga XL A338 AIRBUS A-330-800 A339 AIRBUS A-330-900 A342 AIRBUS A-340-200 Prestige A343 AIRBUS A-340-300 Prestige A345 AIRBUS A-340-500 Prestige A346 AIRBUS A-340-600 Prestige A35 AVANTAGE A-35 Scanner A359 AIRBUS A-350-900 XWB A35K AIRBUS A-350-1000 XWB A37 CESSNA Dragonfly A388 AIRBUS A-380-800 Prestige A3ST AIRBUS