FAA-H-8083-23-2 Seaplane Handbook
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Design of Seaplanes
APPENDIX C3: Design of Seaplanes This appendix is a part of the book General Aviation Aircraft Design: Applied Methods and Procedures by Snorri Gudmundsson, published by Elsevier, Inc. The book is available through various bookstores and online retailers, such as www.elsevier.com, www.amazon.com, and many others. The purpose of the appendices denoted by C1 through C5 is to provide additional information on the design of selected aircraft configurations, beyond what is possible in the main part of Chapter 4, Aircraft Conceptual Layout. Some of the information is intended for the novice engineer, but other is advanced and well beyond what is possible to present in undergraduate design classes. This way, the appendices can serve as a refresher material for the experienced aircraft designer, while introducing new material to the student. Additionally, many helpful design philosophies are presented in the text. Since this appendix is offered online rather than in the actual book, it is possible to revise it regularly and both add to the information and new types of aircraft. The following appendices are offered: C1 – Design of Conventional Aircraft C2 – Design of Canard Aircraft C3 – Design of Seaplanes (this appendix) C4 – Design of Sailplanes C5 – Design of Unusual Configurations Figure C3-1: A Lake LA-250 Renegade, shown here during climb after T-O, is a popular option for amphibious aircraft. The large deflected flap on the horizontal tail is a hydraulically actuated trim tab used for slow speed operations only. It trims out the thrust effect of the highly mounted piston-propeller, improving its handling. -
China's Aircraft Carrier Ambitions
CHINA’S AIRCRAFT CARRIER AMBITIONS An Update Nan Li and Christopher Weuve his article will address two major analytical questions. First, what are the T necessary and suffi cient conditions for China to acquire aircraft carriers? Second, what are the major implications if China does acquire aircraft carriers? Existing analyses on China’s aircraft carrier ambitions are quite insightful but also somewhat inadequate and must therefore be updated. Some, for instance, argue that with the advent of the Taiwan issue as China’s top threat priority by late 1996 and the retirement of Liu Huaqing as vice chair of China’s Central Military Commission (CMC) in 1997, aircraft carriers are no longer considered vital.1 In that view, China does not require aircraft carriers to capture sea and air superiority in a war over Taiwan, and China’s most powerful carrier proponent (Liu) can no longer infl uence relevant decision making. Other scholars suggest that China may well acquire small-deck aviation platforms, such as helicopter carriers, to fulfi ll secondary security missions. These missions include naval di- plomacy, humanitarian assistance, disaster relief, and antisubmarine warfare.2 The present authors conclude, however, that China’s aircraft carrier ambitions may be larger than the current literature has predicted. Moreover, the major implications of China’s acquiring aircraft carriers may need to be explored more carefully in order to inform appropriate reactions on the part of the United States and other Asia-Pacifi c naval powers. This article updates major changes in the four major conditions that are necessary and would be largely suffi cient for China to acquire aircraft carriers: leadership endorsement, fi nancial affordability, a relatively concise naval strat- egy that defi nes the missions of carrier operations, and availability of requisite 14 NAVAL WAR COLLEGE REVIEW technologies. -
NASA's Real World: Mathematics
National Aeronautics and Space Administration NASA’s Real World: Mathematics Educator Guide “Preparing for a Soft Landing” Educational Product Educators & Students Grades 6-8 www.nasa.gov NP-2008-09-106-LaRC Preparing For A Soft Landing Grade Level: 6-8 Lesson Overview: Students are introduced to the Orion Subjects: Crew Exploration Vehicle (CEV) and NASA’s plans Middle School Mathematics to return to the Moon in this lesson. Thinking and acting like Physical Science engineers, they design and build models representing Orion, calculating the speed and acceleration of the models. Teacher Preparation Time: 1 hour This lesson is developed using a 5E model of learning. This model is based upon constructivism, a philosophical framework or theory of learning that helps students con- Lesson Duration: nect new knowledge to prior experience. In the ENGAGE section of the lesson, students Five 55-minute class meetings learn about the Orion space capsule through the use of a NASA eClips video segment. Teams of students design their own model of Orion to be used as a flight test model in the Time Management: EXPLORE section. Students record the distance and time the models fall and make sug- gestions to redesign and improve the models. Class time can be reduced to three 55-minute time blocks During the EXPLAIN section, students answer questions about speed, velocity and if some work is completed at acceleration after calculating the flight test model’s speed and acceleration. home. Working in teams, students redesign the flight test models to slow the models by National Standards increasing air resistance in the EXTEND section of this lesson. -
The SKYLON Spaceplane
The SKYLON Spaceplane Borg K.⇤ and Matula E.⇤ University of Colorado, Boulder, CO, 80309, USA This report outlines the major technical aspects of the SKYLON spaceplane as a final project for the ASEN 5053 class. The SKYLON spaceplane is designed as a single stage to orbit vehicle capable of lifting 15 mT to LEO from a 5.5 km runway and returning to land at the same location. It is powered by a unique engine design that combines an air- breathing and rocket mode into a single engine. This is achieved through the use of a novel lightweight heat exchanger that has been demonstrated on a reduced scale. The program has received funding from the UK government and ESA to build a full scale prototype of the engine as it’s next step. The project is technically feasible but will need to overcome some manufacturing issues and high start-up costs. This report is not intended for publication or commercial use. Nomenclature SSTO Single Stage To Orbit REL Reaction Engines Ltd UK United Kingdom LEO Low Earth Orbit SABRE Synergetic Air-Breathing Rocket Engine SOMA SKYLON Orbital Maneuvering Assembly HOTOL Horizontal Take-O↵and Landing NASP National Aerospace Program GT OW Gross Take-O↵Weight MECO Main Engine Cut-O↵ LACE Liquid Air Cooled Engine RCS Reaction Control System MLI Multi-Layer Insulation mT Tonne I. Introduction The SKYLON spaceplane is a single stage to orbit concept vehicle being developed by Reaction Engines Ltd in the United Kingdom. It is designed to take o↵and land on a runway delivering 15 mT of payload into LEO, in the current D-1 configuration. -
Orientation Sheet for Horizon Updated: 2017-Apr-21
Orientation Sheet for Horizon Updated: 2017-Apr-21 General • All voyages should be documented in the ship’s log book. Report any damage or deficiencies to [email protected] and to boat manager [email protected] / 410-203-2673 Specifications Registration #: MD 5596 AC Hull#: XLY 595267 Make: Islander 36 Year: 1977 Engine: Perkins 4.108; 4-cyl Diesel 48-HP Displacement: 13,450 lbs Draft: 5’ 02” Mast Height Fuel Capacity: 30 gal. Holding tank: 18 gal. (from waterline): 52’ 06” Water Capacity: 54 gal. 2 tanks, below Salon Settees LOA: 36’ 08" Batteries: House battery 1 and 2 (Starboard lazaret) LWL: 28’ 25” Starting Battery (under companionway steps) Beam: 11’ 17” Sails: Main, Genoa on furler, staysail with boom Safety Equipment First Aid Kit: Drawer port side Rescue Sling: Stern Rail PFDs: V-berth Fire Extinguishers: (2) – Starboard side cabin, Port quater berth Day/Night Flares: Aerial & Hand-held – Drawer port side above seats in salon Sounds (Horn, Bell & Whistle): Drawer port side above seats in salon Auto-Switched Bilge Pump: Wired directly to House Battery (must be switched to Auto when leaving boat). The switch is located on the starboard side inside the cabin above the galley sink Old Bilge Pump: Wired to Electric Panel on the engine compartment wall (manual mode only). Do not use this pump unless the other one is not working. Manual Bilge Pump: Cockpit Port side (handle located in drawer port side above seats) Anchors: Danforth (35 lbs) bow; Rode: 15’ of chain & 150’ of line (marked every 30’) Thru-hulls/Sea-cocks: Engine -
The Felixstowe Flying-Boats
842 FLIGHT, 2 December 1955 The Porte Baby prototype No. 9800 in A its original form; later the bow section was lengthened. HISTORIC MILITARY AIRCRAFT Noll Part I By J. M. BRUCE, M.A. THE FELIXSTOWE FLYING-BOATS N 1909 a young British Naval officer named John Cyril Porte WITH this article on a famous family of flying-boats—about which made his first practical entry into the field of aviation by little detailed information has ever before appeared in print—Mr. Brace building a small glider which, in company with Lt. W. B. resumes his popular series. He wishes to make grateful acknowledgement I to Mr. Bruce Robertson, who has provided, together with certain other Pirie, R.N., he attempted to fly at Portsdown Hill, Portsmouth. information, the data on serial numbers which will be published with By the summer of 1910 Porte was experimenting with a little the final instalment of this article. monoplane of the Santos Dumont Demoiselle type, powered by a 35 h.p. Dutheil-Chalmers engine. At that time he was stationed at the Submarine Depot, Portsmouth, and his monoplane's trials several years. In that year he also made a three-wheeled road were conducted at Fort Grange. vehicle propelled by a crude airscrew which was driven by a small By the following year Po«e had fallen victim to pulmonary engine of his own design. tuberculosis, and his Naval career was apparently prematurely Curtiss had enjoyed a considerable amount of success with his terminated when he was invalided out of the Service. Despite his lightweight engines, a fact which had not escaped the attention of severe disability (for which medical science could at that time do the well-known American balloonist Thomas Scott Baldwin. -
Constraints for STOL Operations in South Florida Conurbation Cedric Y
Constraints for STOL Operations in South Florida Conurbation Cedric Y. Justin June 2021 Based on research previously published: Development of a Methodology for Parametric Analysis of STOL Airpark Geo-Density, Robinson et al. AIAA AVIATION 2018 Door-to-Door Travel Time Comparative Assessment for Conventional Transportation Methods and Short Takeoff and Landing On Demand Mobility Concepts, Wei et al. AIAA AVIATION 2018 Wind and Obstacles Impact on Airpark Placement for STOL-based Sub-Urban Air Mobility, Somers et al., AIAA AVIATION 2019 Optimal Siting of Sub-Urban Air Mobility (sUAM) Ground Architectures using Network Flow Formulation, Venkatesh et al, AIAA AVIATION 2020 Comparative Assessment of STOL-based Sub-Urban Air Mobility Operations in Massachusetts and South Florida, Justin et al. AIAA AVIATION 2020 Current Market Segmentation ? VTOL CTOL CTOL CTOL CTOL Capacity ? 200-400+ pax Twin Aisle Are there 120-210 pax scenarios where Single Aisle an intermediate solution using 50-90 pax STOL vehicles and Regional Aircraft sitting in- Design range below 300 nm Commuters between UAM 9-50 pax Flight time below 1.5 hours Thin-Haul and thin-haul 9 to 50 seat capacity operations exists? 4-9 pax Sub-Urban Missions 50-150 nm Air Mobility 4 to 9 revenue-seats Missions below 50 nm Urban Air Mobility 1-4 pax 1 to 4 revenue-seats 50 nm 300 nm 500 nm 3000 nm 6000+ nm Artwork Credit Uber Design Range 2 Introduction • Population, urbanization, and congestion Atlanta, GA Miami, FL Dallas, TX Los Angeles, CA have increased steadily over the past several decades • Increasing delays damage the environment and substantially impact the economy Driving time: 8 min. -
Gannet Electronics
Gannet Electronics A Summary of the Electronic Equipment Fitted to early Model R.A.N Gannet A.S.1 Aircraft Prepared by David Mowat Ex-L.R.E.M.(A) 21st. August 2003 Page 1 Page 2 GANNET ELECTRONIC EQUIPMENT Introduction The ‘Heart’ of the Gannet as a Weapons System was its Electronic Equipment. It contained a comprehensive range of electronic equipment to enable it to perform the various roles for which it was designed. Its Primary Role was to detect, locate, and destroy enemy submarines. For this Role, the Aircraft was fitted with a Search Radar and Sonobuoy Systems. Other electronic systems were also installed for Communications, both internal and external, and Navigation. The various equipments were allocated an ‘Aircraft Radio Installation’ (ARI) number, which specified the actual equipment used in each installation. These may vary between aircraft depending on the role that the particular aircraft was to perform. A cross- reference List of ARI’s is shown at Appendix ‘A’. The various equipments can be grouped into four major categories as follows: a.! Communications b.! Navigation c.! Warfare Systems d.! Stores Communications Equipment The Communications Equipment was used to enable the crew to talk to each other (internal communications) and other aircraft, ships or bases (external communications). They are as follows: a.! Audio Amplifier Type A1961 The Type A1921 was used to amplify the Microphone outputs from the three crew members and feed it back into the earphones. It was located on the port side of the rear cockpit at about seat height just forward of the Radio Operator. -
WATER WINGS Story and Photos by Guy R Maher
OWNERS’ MANUAL: WATER WINGS Story and Photos by Guy R Maher VWDEOLVKHGRQEDVHOHJ,KDYHWKHÀDSVVHW 7XUQLQJ¿QDOWKHÀDSVDUHORZHUHGWRIXOO EDWGHJUHHVRXWRIDSRVVLEOH7KH DQGWKHSRZHULVVHWWRLQFKHVRIPDQLIROG SURSFRQWUROLVVHWWRKLJK5307XUQLQJ¿QDO SUHVVXUH0DLQWDLQLQJDWRNQRW ,PDNHRQHODVWFKHFNRIWKHODQGLQJJHDU DSSURDFKVSHHGIROORZHGE\DJHQWOHÀDUH DQGFRQ¿UPWKDWLWLVGH¿QLWHO\LQWKH³83´ DQGZHVHWWOHQLFHO\LQWRWKHODNH3RZHU SRVLWLRQ<HV\RXUHDGWKDWFRUUHFWO\7KH immediately to idle and full back pressure on ODQGLQJJHDUPXVWEHLQWKH³8S´SRVLWLRQIRU the control wheel after splashdown yields a ,DPDERXWWRODQGRQZDWHU smooth deceleration of this plane now turned ERDW7KDW¶VZKDW,FDOOIXQ 2828 CessnaCCeessssnana PilotsPililotots AssociationAAssssoociciatatiioon | JulyJJullyy 2018201018 VanFleet’s 172XP is equipped with Wipaire, Inc.’s Wipline 2350 amphibious floats. www.cessna.orgwwwww.w ceesssnan ..orgg 299 VanFleet’s 172XP has a modified engine that increases the horsepower from 195 to 210. 7KHDLUSODQH,¶PÀ\LQJLVDEHDXWLIXOUHGDQGZKLWH 6HYHUDO\HDUVODWHUVKHPRYHGWR*HRUJLDWREHFRPHWKH &HVVQD;3HTXLSSHGZLWKDVHWRI:LSDLUH dietitian for Athens Regional Hospital. At last she was ,QF¶V:LSOLQHDPSKLELRXVÀRDWV7KHRULJLQDO able to pursue her lifelong dream - to obtain her private 7&0,2.HQJLQHKDVDOVREHHQPRGL¿HGXSSLQJ SLORWOLFHQVHLQD&HVVQDLQ&KDQJLQJMREVWR WKHKRUVHSRZHUIURPWR7KHRZQHURIWKLV Ross Abbott as a pharmaceutical representative, getting VSHFLDO;3DIIHFWLRQDWHO\FDOOHGSamanthaLV6XVDQ PDUULHGKDYLQJDFKLOGDQGEX\LQJD&HVVQD VanFleet, owner/operator of VanFleet Aviation based in WREXLOGWLPHNHSWWKLQJVEXV\IRU9DQ)OHHW7KH -
Aviation Investigation Report A04w0114 Upset on Water
Transportation Safety Board Bureau de la sécurité des transports of Canada du Canada AVIATION INVESTIGATION REPORT A04W0114 UPSET ON WATER LANDING BIG RIVER AIR LTD. CESSNA A185F SEAPLANE C-GVYE TALTSON RIVER (FERGUSON’S CABIN) NORTHWEST TERRITORIES 07 JUNE 2004 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 Upset on Water Landing Big River Air Ltd. Cessna A185F Seaplane C-GVYE Taltson River (Ferguson’s Cabin) Northwest Territories 07 June 2004 Report Number A04W0114 Summary The Cessna A185F seaplane (registration C-GVYE, serial number 18503778) operated by Big River Air Ltd., departed Four Mile Lake, Alberta, on a visual flight rules flight to the Taltson River, Northwest Territories. The purpose of the flight was to transport three passengers to a site on the river known as Ferguson’s Cabin. At approximately 1700 mountain daylight time, as the aircraft was landing on the water near Ferguson’s Cabin, the left float dug in and the left wing struck the water. The aircraft immediately cartwheeled and came to rest floating inverted in the river, with only the bottoms of the floats visible at the surface. The pilot and the front seat passenger sustained serious injuries; however, they managed to exit the submerged and damaged aircraft through a broken window in the left cabin door. Four fishermen in boats responded to the accident, removed the survivors from the cold water, and transported them to a warm shelter. -
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner
A Conceptual Design of a Short Takeoff and Landing Regional Jet Airliner Andrew S. Hahn 1 NASA Langley Research Center, Hampton, VA, 23681 Most jet airliner conceptual designs adhere to conventional takeoff and landing performance. Given this predominance, takeoff and landing performance has not been critical, since it has not been an active constraint in the design. Given that the demand for air travel is projected to increase dramatically, there is interest in operational concepts, such as Metroplex operations that seek to unload the major hub airports by using underutilized surrounding regional airports, as well as using underutilized runways at the major hub airports. Both of these operations require shorter takeoff and landing performance than is currently available for airliners of approximately 100-passenger capacity. This study examines the issues of modeling performance in this now critical flight regime as well as the impact of progressively reducing takeoff and landing field length requirements on the aircraft’s characteristics. Nomenclature CTOL = conventional takeoff and landing FAA = Federal Aviation Administration FAR = Federal Aviation Regulation RJ = regional jet STOL = short takeoff and landing UCD = three-dimensional Weissinger lifting line aerodynamics program I. Introduction EMAND for air travel over the next fifty to D seventy-five years has been projected to be as high as three times that of today. Given that the major airport hubs are already congested, and that the ability to increase capacity at these airports by building more full- size runways is limited, unconventional solutions are being considered to accommodate the projected increased demand. Two possible solutions being considered are: Metroplex operations, and using existing underutilized runways at the major hub airports. -
Towards the End of an Era Master Copy
Poole Flying Boats Celebration (Charity No.1123274) Part Six: Towards the end of an Era at Poole ‘Au Revoir’ © PFBC BCC Ward a flying boat enthusiast living in Parkstone, noted that during this period as many as 4 were moored together at Poole, having flown in, often with BOAC personnel brought back, before heading to Hythe, and then to the breakers ! First back to Poole was G-ADHL Canopus in the Autumn of 1946, and coinciding with delivery of the last set of Hythes. A little later, others followed: G-AFRA Cleopatra on 4th. November. Next G-ADUV Cambria & G-AEUF Cameronian. Capt. James Peers brought in G-ADVB Corsair January 1947; then sadly witnessed its scrapping at R.J.Coley & Sons. The 3 former QEA C-Class that had been swapped with BOAC G-AFBJ Carpentaria (also in January), G-AFBL Cooee , and G-AEUI Coorong (Feb.) were dismantled. [Later their counterpart G-AETV Coriolanus was scrapped at Rose Bay.] Meanwhile, the Poole stalwarts G-AFKZ Cathay and G-AFCT Champion finished the routine weekly service to Lisbon. Also, G-ADUW Castor wound up the last remaining easterly section of the Horseshoe service between Calcutta & Cairo. Although G-AEUD Cordelia was the last to be dismantled G-ADHM Caledonia was last home fittingly , with Capt. Horn and his crew (leaving Durban on 12th. March), to then depart Poole at the beginning of April on its final flight to Hythe. © PFBC Picture: G-ADVB Corsair brought to Poole Harbour by Captain James Peers... Photo. by Sidney Batting BA & PFBC’s Collections The harsh winter weather of 1946/47 mirrored the great freeze of January 1940 when the C-Class were moored at Poole.