DOCSLIB.ORG

WINGS of SILVER PIPER J-3 Cub OPERATIONS MANUAL &

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
WINGS of SILVER PIPER J-3 Cub OPERATIONS MANUAL & WINGS OF SILVER PIPER J-3 Cub OPERATIONS MANUAL & POH (this Manual and POH is not intended for flight and is intended only for flight simulation use) Written by Mitchell Glicksman, © 2009 i Table of Contents Introduction..............................................................................................................................................................................................................1 The 747 Captain Who Forgot How to Fly................................................................................................................................................................8 A Short History of a Small Airplane......................................................................................................................................................................13 Quick Start Guide...................................................................................................................................................................................................18 System Requirements........................................................................................................................................................................................18 Installation.........................................................................................................................................................................................................20 Settings..............................................................................................................................................................................................................20 Quick Flying Tips..............................................................................................................................................................................................24 2D Panels................................................................................................................................................................................................................25 Controls..............................................................................................................................................................................................................25 Payload and Fuel Manager................................................................................................................................................................................26 Pilot's Map.........................................................................................................................................................................................................28 Portable Radio...................................................................................................................................................................................................29 Maintenance Hangar..........................................................................................................................................................................................30 General Description................................................................................................................................................................................................31 Seaplane (Float) Version....................................................................................................................................................................................32 Ski Version.........................................................................................................................................................................................................32 Tundra Tire Version...........................................................................................................................................................................................32 Performance.......................................................................................................................................................................................................32 Fuel....................................................................................................................................................................................................................33 Engine Limits ....................................................................................................................................................................................................33 Airspeed Limits.................................................................................................................................................................................................33 Propeller Limits.................................................................................................................................................................................................33 C.G. Range.........................................................................................................................................................................................................33 Maximum Weight..............................................................................................................................................................................................33 Number of Seats ...............................................................................................................................................................................................34 Maximum Baggage............................................................................................................................................................................................34 Fuel Capacity.....................................................................................................................................................................................................34 Oil Capacity.......................................................................................................................................................................................................34 Detail Specification for Engine, Aircraft Continental ......................................................................................................................................35 ii General Specifications .................................................................................................................................................................................36 Engine Performance......................................................................................................................................................................................36 Variants...................................................................................................................................................................................................................37 POH........................................................................................................................................................................................................................38 Flying the Cub...................................................................................................................................................................................................38 Opening It Up and Checking it Out...................................................................................................................................................................39 General Walk Around .......................................................................................................................................................................................40 Port Side........................................................................................................................................................................................................40 Tail................................................................................................................................................................................................................40 Starboard Side...............................................................................................................................................................................................40 Engine...........................................................................................................................................................................................................41 Cockpit..........................................................................................................................................................................................................41 Engine Starting..................................................................................................................................................................................................42 Warm up ...........................................................................................................................................................................................................45 Taxiing...............................................................................................................................................................................................................46
Load more

Recommended publications
  • Evaluation of Fighter Evasive Maneuvers Against Proportional Navigation Missiles
    TURKISH NAVAL ACADEMY NAVAL SCIENCE AND ENGINEERING INSTITUTE DEPARTMENT OF COMPUTER ENGINEERING MASTER OF SCIENCE PROGRAM IN COMPUTER ENGINEERING EVALUATION OF FIGHTER EVASIVE MANEUVERS AGAINST PROPORTIONAL NAVIGATION MISSILES Master Thesis REMZ Đ AKDA Ğ Advisor: Assist.Prof. D.Turgay Altılar Đstanbul, 2005 Copyright by Naval Science and Engineering Institute, 2005 CERTIFICATE OF COMMITTEE APPROVAL EVALUATION OF FIGHTER EVASIVE MANEUVERS AGAINST PROPORTIONAL NAVIGATION MISSILES Submitted in partial fulfillment of the requirements for degree of MASTER OF SCIENCE IN COMPUTER ENGINEERING from the TURKISH NAVAL ACADEMY Author: Remzi Akda ğ Defense Date : 13 / 07 / 2005 Approved by : 13 / 07 / 2005 Assist.Prof. Deniz Turgay Altılar (Advisor) Prof. Ercan Öztemel (Defense Committee Member) Assoc.Prof. Coşkun Sönmez (Defense Committee Member) ABSTRACT (TURKISH) SAVA Ş UÇAKLARININ ORANTISAL SEY ĐR YAPAN GÜDÜMLÜ MERM ĐLERDEN SAKINMA MANEVRALARININ DE ĞERLEND ĐRĐLMES Đ Anahtar Kelimeler : Orantısal seyir, sakınma manevraları, aerodinamik kuvvetler Bu tezde, orantısal seyir adı verilen güdüm sistemiyle ilerleyen güdümlü mermilere kar şı uçaklar tarafından icra edilen sakınma manevralarının etkinli ği ölçülmü ş, farklı güdümlü mermilerden kaçı ş için en uygun manevralar tanımlanmı ştır. Uçu ş aerodinamikleri, matematiksel modele bir temel oluşturmak amacıyla sunulmu ştur. Bir hava sava şında güdümlü mermilerden sakınmak için uçaklar tarafından icra edilen belli ba şlı manevraların matematiksel modelleri çıkarılıp uygulanılmı ş, görsel simülasyonu gerçekle ştirilmi ş ve bu manevraların de ğişik ba şlangıç de ğerlerine göre ba şarım çözümlemeleri yapılmıştır. Güdümlü mermi-uçak kar şıla şma senaryolarında güdümlü merminin terminal güdüm aşaması ele alınmı ştır. Gerçekçi çözümleme sonuçları elde edebilmek amacıyla uçu ş aerodinamiklerinin göz önüne alınmasıyla elde edilen yönlendirme kinematiklerini içeren geni şletilmi ş nokta kütleli uçak modeli kullanılmı ştır.
    [Show full text]
  • Certificated Aircraft Engines
    CERTIFICATED AIRCRAFT ENGINES SSP­110­1 DECEMBER 2013 652 Oliver Street Williamsport, PA 17701 U.S.A. Phone: Main OfficeU.S. and Canada Toll Free +1 (800) 258­3279 Direct +1 (570) 323­6181 Sales Department +1 (570) 327­7278 Facsimile +1 (570) 327­7101 Visit us on the World Wide Web at: http://www.lycoming.com ©2013 Avco Corporation All Rights Reserved. Lycoming Engines is a division of Avco Corporation. TABLE OF CONTENTS PISTON CERTIFICATED ENGINES – (4) Four Cylinder Series ....................................................................................................................................................... 1 (6) Six Cylinder Series ....................................................................................................................................................... 16 (8) Eight Cylinder Series .................................................................................................................................................... 32 PISTON ENGINE INSTALLATIONS (4) Four Cylinder Installations............................................................................................................................................ 33 (6) Six Cylinder Installations.............................................................................................................................................. 42 TURBOCHARGED .................................................................................................................................................... 46 GEARED...................................................................................................................................................................
    [Show full text]
  • PA46-350P Pilot's Operating Handbook
    MALIBU MIRAGE MALIBU MIRAGE PA-46-350P PA-46-350P SN 4636196 AND UP SN 4636196 AND UP PILOT’S PILOT’S OPERATING OPERATING HANDBOOK HANDBOOK AND AND FAA APPROVED FAA APPROVED AIRPLANE FLIGHT MANUAL AIRPLANE FLIGHT MANUAL AIRPLANE AIRPLANE AIRPLANE AIRPLANE SERIAL NO. ___________________________ REGIST. NO. _______________________ SERIAL NO. ___________________________ REGIST. NO. _______________________ PA-46-350P PA-46-350P REPORT: VB-1710 FAA APPROVED BY: REPORT: VB-1710 FAA APPROVED BY: PETER E. PECK FOR REFERENCEPETER E. PECK ONLY D.O.A. NO. SO-1 D.O.A. NO. SO-1 DATE OF APPROVAL: THE NEW PIPER AIRCRAFT, INC. DATE OF APPROVAL:NOT FOR FLIGHT THE NEW PIPER AIRCRAFT, INC. FEBRUARY 23, 1999 VERO BEACH, FLORIDA FEBRUARY 23, 1999 VERO BEACH, FLORIDA THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE THIS HANDBOOK INCLUDES THE MATERIAL REQUIRED TO BE FURNISHED TO THE PILOT BY THE FEDERAL AVIATION REGULATIONS AND ADDITIONAL INFORMATION PILOT BY THE FEDERAL AVIATION REGULATIONS AND ADDITIONAL INFORMATION PROVIDED BY THE MANUFACTURER AND CONSTITUTES THE FAA APPROVED PROVIDED BY THE MANUFACTURER AND CONSTITUTES THE FAA APPROVED AIRPLANE FLIGHT MANUAL. THIS HANDBOOK MUST BE CARRIED IN THE AIRPLANE FLIGHT MANUAL. THIS HANDBOOK MUST BE CARRIED IN THE AIRPLANE AT ALL TIMES. AIRPLANE AT ALL TIMES. TM TM WARNING WARNING EXTREME CARE MUST BE EXERCISED TO LIMIT THE EXTREME CARE MUST BE EXERCISED TO LIMIT THE USE OF THIS HANDBOOK TO APPLICABLE AIRCRAFT. USE OF THIS HANDBOOK TO APPLICABLE AIRCRAFT. THIS HAND- BOOK IS VALID FOR USE WITH THE THIS HAND- BOOK IS VALID FOR USE WITH THE AIRPLANE IDENTIFIED ON THE FACE OF THE TITLE AIRPLANE IDENTIFIED ON THE FACE OF THE TITLE PAGE.
    [Show full text]
  • ARTICLE 5 Assigned-Space Aircraft Parking
    ARTICLE 5 Assigned-Space Aircraft Parking Section 500. Assigned-space aircraft parking designation. 510. Assigned-space use and fees. 520. Assigned-space permit application. 530. Assigned-space permit. 540. Cancellation of an assigned-space permit. 550. Assigned-space permit lottery. 560. Assigned-space switch list. 570. Assigned-space wait list. 580. Birchwood airport transitional compliance requirements. 590. Definitions. 17 AAC 45.500. Assigned-space aircraft parking designation. (a) The commissioner will designate an airport for assigned-space aircraft parking if the commissioner determines in writing that the designation is in the best interest of the state. In making this determination, the commissioner will consider the applicable factors set out at 17 AAC 45.900 and the following: (1) the number of aircraft based at the airport, other than those based on leased premises, the demand for transient aircraft fee parking, and the amount of space available for assigned-space aircraft parking at the airport; (2) the potential impact of assigned-space aircraft parking fees on airport users; and (3) the department's estimate of the cost to implement the requirements of 17 AAC 45.500 - 17 AAC 45.590 at the airport compared to the potential revenue the department would receive for assigned-space aircraft parking at the airport. (b) The department will inform the public that the commissioner has designated an airport for assigned-space aircraft parking by giving notice in accordance with 17 AAC 45.400. The notice will include (1) the name
    [Show full text]
  • Garmin Reveals Autoland Feature Rotorcraft Industry Slams Possible by Matt Thurber NYC Helo Ban Page 45
    PUBLICATIONS Vol.50 | No.12 $9.00 DECEMBER 2019 | ainonline.com Flying Short-field landings in the Falcon 8X page 24 Regulations UK Labour calls for bizjet ban page 14 Industry Forecast sees deliveries rise in 2020 page 36 Gratitude for Service Honor flight brings vets to D.C. page 41 Air Transport Lion Air report cites multiple failures page 51 Rotorcraft Garmin reveals Autoland feature Industry slams possible by Matt Thurber NYC helo ban page 45 For the past eight years, Garmin has secretly Mode. The Autoland system is designed to Autoland and how it works, I visited been working on a fascinating new capabil- safely fly an airplane from cruising altitude Garmin’s Olathe, Kansas, headquarters for ity, an autoland function that can rescue an to a suitable runway, then land the airplane, a briefing and demo flight in the M600 with airplane with an incapacitated pilot or save apply brakes, and stop the engine. Autoland flight test pilot and engineer Eric Sargent. a pilot when weather conditions present can even switch on anti-/deicing systems if The project began in 2011 with a Garmin no other safe option. Autoland should soon necessary. engineer testing some algorithms that could receive its first FAA approval, with certifi- Autoland is available for aircraft manu- make an autolanding possible, and in 2014 cation expected shortly in the Piper M600, facturers to incorporate in their airplanes Garmin accomplished a first autolanding in followed by the Cirrus Vision Jet. equipped with Garmin G3000 avionics and a Columbia 400 piston single. In September The Garmin Autoland system is part of autothrottle.
    [Show full text]
  • Recreational Flyer January - February 2010 Elevated: Angus Watt’S Ch-750
    January - February 2010 Recreational Aircraft Association Canada www.raa.ca The Voice of Canadian Amateur Aircraft Builders $6.95 Elevated: Angus Watt's CH-750 Elevated: The original Zenith 701 was designed as an Angus Watt’s Ch-750 ultralight go-anywhere all metal bush plane that could be plans built by anyone with a 4 ft tabletop bending brake and a pair of snips. It was rarely described as a thing of beauty but so well does it fulfill its mission that these planes are found all over the world. They are inexpensive to construct, and because of their leading edge slats they can get in and out of extremely short patches of clear ground. 22 Recreational Flyer January - February 2010 Elevated: Angus Watt’s Ch-750 WITH THE ADVENT of the Light Sport category in and the only part interchangeable with the 701 is the US, Chris Heintz saw the need for an updated the signature Zenith all-flying rudder. Formerly the version, something with a larger cabin, greater skins were all .016” and they are now .020 to handle payload, and the ability to use an array of four the greater mass of the range of possible four stroke stroke engines. The CH 750 was the result and its engines and the 1320 pound gross weight on wheels, lineage is visually apparent but while the new plane 1430 on floats. resembles the 701 it is almost completely different in Chris Heintz correctly surmised that the US construction. CNC fabrication methods have made Light Sport category would be attractive to aging it possible to simplify the design, speed up the con- American pilots who wanted to bargain down to struction, and end up with a larger and faster plane their Sport Pilot category that allows a valid driver’s at only a slight weight penalty.
    [Show full text]
  • Unusual Attitudes and the Aerodynamics of Maneuvering Flight Author’S Note to Flightlab Students
    Unusual Attitudes and the Aerodynamics of Maneuvering Flight Author’s Note to Flightlab Students The collection of documents assembled here, under the general title “Unusual Attitudes and the Aerodynamics of Maneuvering Flight,” covers a lot of ground. That’s because unusual-attitude training is the perfect occasion for aerodynamics training, and in turn depends on aerodynamics training for success. I don’t expect a pilot new to the subject to absorb everything here in one gulp. That’s not necessary; in fact, it would be beyond the call of duty for most—aspiring test pilots aside. But do give the contents a quick initial pass, if only to get the measure of what’s available and how it’s organized. Your flights will be more productive if you know where to go in the texts for additional background. Before we fly together, I suggest that you read the section called “Axes and Derivatives.” This will introduce you to the concept of the velocity vector and to the basic aircraft response modes. If you pick up a head of steam, go on to read “Two-Dimensional Aerodynamics.” This is mostly about how pressure patterns form over the surface of a wing during the generation of lift, and begins to suggest how changes in those patterns, visible to us through our wing tufts, affect control. If you catch any typos, or statements that you think are either unclear or simply preposterous, please let me know. Thanks. Bill Crawford ii Bill Crawford: WWW.FLIGHTLAB.NET Unusual Attitudes and the Aerodynamics of Maneuvering Flight © Flight Emergency & Advanced Maneuvers Training, Inc.
    [Show full text]
  • Maneuver Descriptions
    2017-2018 Senior Pattern Association Section III Maneuver Descriptions NOTE: MANEUVER DESCRIPTIONS THAT FOLLOW ARE TAKEN VERBATIM FROM THE APPROPRIATE AMA RULE BOOKS FROM WHICH THE MANEUVERS WERE TAKEN. THE ONE EXCEPTION IS FOR THE SQUARE HORIZONTAL EIGHT, FOR WHICH EVERY APPEARANCE IN THE AMA RULE BOOK ENDED AS AN INCOMPLETE DESCRIPTION. THE SPA BOARD HAS CREATED WHAT WE THINK WOULD BE THE APPROPRIATE ENDING, WHICH IS SHOWN ON PAGE 34 IN ITALICS. Anatomy of an SPA Maneuver by Phil Spelt, SPA 177, AMA 1294 SPA pilots are flying what is called “Precision Aerobatics,” in the official AMA publications” -- the old-time way (pre turnaround). The emphasis in that name is on the word “Precision.” That means pilots are supposed to display precise control of their aircraft in front of the judges. This precision should, ideally, be shown from the moment the plane is placed on the runway until it stops at the end of the landing rollout. Technically, the judges are only supposed to “judge” during the actual maneuvers, but they will notice either wild or tame turnarounds – whether deliberately or accidentally. An SPA maneuver consists of five sections, which can be viewed as an onion sliced through the middle vertically – so there are 2 pairs of layers, or parts, surrounding the actual maneuver in the center, as illustrated. The outer pair (sections 1 and 5) comprises the “free flight” area, which is used to turn the aircraft around and get it lined up to enter the next maneuver. Most pilots use a Split-S maneuver for the turnaround, thus maintaining the track of the plane at the distance from the runway at which the maneuvers are performed.
    [Show full text]
  • NEWS RELEASE Continental Aerospace Technologies
    NEWS RELEASE For Immediate Release Continental Aerospace Technologies™ announces partnership with Piper Aircraft® to launch the Pilot 100 training aircraft Mobile, Alabama, April 2, 2019 — Continental®, an AVIC International Holding (HK) LTD company (HKEX: 232.HK), announces the partnership with Piper Aircraft® to launch the Pilot 100 and Pilot 100i training aircraft. Piper Aircraft® has selected the certified Continental IO-370-DA3A engine for the new Pilot 100/100i single engine trainer. After careful consideration, Piper® determined that the engine met their requirements to answer increasing requests from flight schools of all sizes for a robust, proven trainer platform at a lower price point in both VFR and IFR configurations With an all-time high demand for new pilots, Piper Aircraft® has announced the Pilot 100/100i, to meet the needs of a wide variety of training schools and curriculums. Based on the PA-28 airframe, one of the most successful training platforms in the history of general aviation, Piper® combined an airframe, avionics and engine package that allows the aircraft to be very aggressively priced and fills the need for a trainer tailored to the primary single- engine training needs of these schools. The Pilot 100/100i allows schools to invest in new initial trainers at a price point that is compatible with their needs while relying on a proven and tried design. “We congratulate Piper Aircraft® for their vision, ability to gauge the market trends, and their commitment to the training market. We are very excited to collaborate with Piper® on the new certified engine design. We worked with the Piper® engineering team to make sure that they benefit not only from an outstanding value, but also from all the enhancements that we have incorporated in our new engine line.
    [Show full text]
  • Federal Register/Vol. 86, No. 10/Friday, January 15, 2021/Rules
    Federal Register / Vol. 86, No. 10 / Friday, January 15, 2021 / Rules and Regulations 3769 Adjusted maximum civil Law Penalty description penalty amount 12 U.S.C. 5565(c)(2)(A) ............................................................. Tier 1 penalty ............................................................................. $5,953 12 U.S.C. 5565(c)(2)(B) ............................................................. Tier 2 penalty ............................................................................. 29,764 12 U.S.C. 5565(c)(2)(C) ............................................................. Tier 3 penalty ............................................................................. 1,190,546 15 U.S.C. 1717a(a)(2) ................................................................ Per violation ................................................................................ 2,074 15 U.S.C. 1717a(a)(2) ................................................................ Annual cap ................................................................................. 2,073,133 12 U.S.C. 2609(d)(1) .................................................................. Per failure ................................................................................... 97 12 U.S.C. 2609(d)(1) .................................................................. Annual cap ................................................................................. 195,047 12 U.S.C. 2609(d)(2)(A) ............................................................. Per failure,
    [Show full text]
  • Aircraft Specification No. A-691
    DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-691 Revision 32 PIPER J3C-40 J3C-50 J3C-50S J3C-65 J3C-65S PA-11 PA-11S October 1, 1997 AIRCRAFT SPECIFICATION NO. A-691 Type Certificate Holder The New Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida 32960 I - Model J3C-40, 2 PCLM, Approved July 14, 1938. Engine Continental A-40-4 (See Item 311A for optional engine) Fuel 73 minimum octane aviation gasoline Engine Limits For all operations, 2575 r.p.m. (40 hp) Airspeed Limits (CAS) Level flight or climb 85 mph ( 74 knots) Glide or dive 115 mph (100 knots) Propeller Limits Maximum permissible diameter 81 inches C. G. Range (+10.6) to (+22.7) See NOTE 3 for restricted limits on certain Serial Nos. below 4502. Empty Weight C. G. Range If placard "Solo flying in rear seat only" is installed (See NOTE 2): (+7.8) to (+20.0) When empty weight C. G. falls within range given, computation of critical fore and aft C. G. positions is unnecessary. Range is not valid for non-standard arrangements. Maximum Weight 1025 lb. Number of Seats 2 (one at +9 and one at +36) Maximum Baggage 20 lb. (+49) Fuel Capacity 12 gallons (-18) Oil Capacity 1 gallon (-39) Page No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 Rev. No. 32 31 31 31 31 31 31 32 31 31 31 31 31 31 31 31 31 31 31 31 31 A-691 Page 2 of 21 I - Model J3C-40 (cont'd) Control Surface Movements Elevator 34° Up 29° Down Rudder 30° Left 30° Right Aileron 18° Up 18° Down Stabilizer 2.5° Up 4° Down Serial Numbers Eligible 2325, 2327, 2339, 2340, 2342, 2344, 2345, 2347, 2349, 2351 and up; 2356-A and up; and 8277-1 through 8277-40.
    [Show full text]
  • Index to Cub Clues Newsletters #1 - #183 • December 2014
    Index to Cub Clues Newsletters #1 - #183 • December 2014 Articles, Books, Videos about Cubs or Pipers...............................................................1 FAA - Rules & Procedures........................................................................................1-2 Flying - Places to Go/Noteworthy Flights .................................................................2-3 Flying Techniques - Including Aerobatics.....................................................................3 Fuel & Oil................................................................................................................3-4 Hangaring, Towing, Pushing, Lifting, Tying Down ........................................................4 History - Aircraft Exploits ...........................................................................................4 History - Company ..................................................................................................4-5 History - War Time……………………………………………………………………………………………………..5 Maintenance, Repair, Alteration ...........................................................................5-21 Cockpit - doors, windows, floors..................................................................5-6 Cockpit - seat belts, harnesses........................................................................6 Cockpit - seat, upholstery, baggage area.........................................................6 Controls & control surfaces .........................................................................6-7 Converting
    [Show full text]