Fspilot Cessna 400TT Corvalis Alabeo M a G a Z I N E General Description & History of Design and Development
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March2019-Final.Pdf
The MARCH 2019 TWIN CESSNAFlyer 2019 FLY-IN CONVENTION MAY 15 - 18 (see page 8) FEATURING: HAMMER 414A CIRCUIT BREAKERS & INFLIGHT FIRES 310Q LANDING GEAR MISHAP MAGIC KINGDOM PILOT READERS WRITE SupportingSupporting TwinTwin CessnaCessna OwnersOwners WorldwideWorldwide sincesince 19881988 A RAM Engine A Cylinder for Every Situation IN-STOCK! for EVERY Budget RAM AIRCRAFT $695NICKEL All the bells Just the bells IO & TSIO! & whistles for $39,980 NO CORE REPAIRED RETURN! This repaired cylinder with a nickel bore is the perfect cylinder to get your high-time engine to TBO. No core return is required. RAM AIRCRAFT TSIO-520-NB $1,134NICKEL TSIO-520 NO CORE The standard, Legendary RAM engine The ValueTime TSIO-520-NB replacement OVERHAULED RETURN! package with all the bells and whistles engine is an industry standard overhaul This overhauled cylinder with a nickel bore is the that is ready to drop into your airplane by the Legendary RAM Craftsman built perfect cylinder for mid-time engines, top is still available. to RAM standards. overhauls and field overhauls. Protect your RAM STC. $1,425STEEL TSIO-520 We are the only overhauler in the world that overhauls to RAM STC standards. NO CORE NEW RETURN! The Superior Millenium cylinder is a NEW cylinder with a through-hardened steel barrel. It is the customer preferred cylinder and RAM’s choice for our premium overhauled engines. *Price does not include rocker arms or piston pins. New Continental Engine Parts RAM AIRCRAFT, LP • SINCE 1976 • PMA New Parts Available Now ©2019 RAM Aircraft, LP TTCF010919 The SM TWIN CESSNAFlyer FEATURES The Twin Cessna Flyersm P.O. -
Cessna 340 Page 1 of 14
Cessna 340 Page 1 of 14 Volume 34 • Number 2 • February 2004 Cessna 340 A fast, pressurized cabin-class twin that’s an excellent step-up from a Avionics Report high performance single. Used Aircraft Guide Maintenance Matters Accessories Although airplanes are often sold as Misc. business and transportation tools, the reality of ownership falls short of the ideal. They either lack the range, the carrying capacity or the ability to deal with real-world weather, thus an airline or a charter outfit gets the call. Still, there are plenty of pilot/businessmen who couldn’t function without an airplane. These owners typically start with single- The Cessna 340 is a standout thanks to engine airplanes and quickly outgrow payload/fuel flexibility and near 200-knot cruise them for the reasons stated above. A speeds. Pressurization is an added plus. serious business airplane needs a decent cabin, credible speed and the ability to hack it when there’s ice or thunder in the forecast. Pressurization is nice since the clients don’t want to spend several hours with a plastic hose stuck up their noses. Enter the Cessna 340. Owners looking to step-up from a high-performance single will inevitably make a pass or two through the 340 classified section. And well they should. Although not without its shortcomings—most notably certain loading limitations and an overly complex fuel system—the 340 is nevertheless an impressive, flexible and capable airplane that meets the business mission well and can do double duty as a family airplane. Model History The 340 owes its existence to the boom days of general aviation during the late 1960s and early 1970s. -
Cessna 350 Cessna 400 Cirrus SR22 Cirrus SR22 Turbo
Aircraft Comparison Cessna 350 Cessna 400 Cirrus SR22 Cirrus SR22 Turbo Sales Engineering, Piston Marketing Cessna Aircraft Company April, 2008 Cessna A Textron Company INTRODUCTION This comparative analysis examines the features of the Cessna 350 and the Cessna 400 in relation to the Cirrus SR22 and Cirrus SR22 Turbo. Subjects reviewed in the following pages include: BASIC PERFORMANCE FLIGHT PROFILES OPERATING ECONOMICS TECHNICAL EVALUATION BASIC SPECIFICATIONS & WEIGHTS Cessna A Textron Company EXECUTIVE SUMMARY This comparative analysis examines the benefits of purchasing the Cessna 350/400 versus the Cirrus SR22/SR22 Turbo. The Cessna 350/400 offers the better value for the following reasons: PERFORMANCE: The Cessna 350/400 offer superior performance • Fewer fuel stops by reason of its greater efficiency and range capability • Shorter flight times resulting from its higher cruise speeds leads to greater utilization AIRCRAFT DESIGN: The Cessna 350/400 offer a better design • Higher quality interior and exterior fit and finish • Greater avionics integration minimizes cockpit clutter and reduces pilot workload • Meets more stringent design criteria – Utility Category vs Normal Category • Engine manufacturer warranty support for turbocharged engine CUSTOMER SUPPORT: Cessna is an industry leader • Comprehensive warranty program • Extensive world-wide service station network • 24 hour, 7 days a week access to parts and technical assistance The following pages detail the greater value offered by the Cessna 350 and Cessna 400. Cessna A Textron Company CRUISE SPEEDS Cruise speed represents the true airspeed for each aircraft at various cruising altitudes. Airspeeds are based on the recommended cruise power setting published in each manufacturer's flight manual or operating/pilot manual (75% or Max Power for the Cessna 350 and Cirrus SR22; 85% Power for the Cessna 400 and Cirrus SR22 Turbo). -
Portola Valley Aircraft Noise Monitoring
Portola Valley Aircraft Noise Monitoring Prepared by San Francisco International Airport Aircraft Noise Abatement Office Technical Report #012017-978 January 2017 San Francisco International Airport Portola Valley Aircraft Noise Monitoring Report Page | 2 Table of Contents Executive Summary ................................................................................................................................ 3 Community and SFO Operations............................................................................................................ 3 Equipment ............................................................................................................................................... 3 Aircraft Noise Analysis........................................................................................................................... 4 Aircraft Operations ................................................................................................................................. 6 Track Density.......................................................................................................................................... 8 Noise Reporters....................................................................................................................................... 9 Conclusion ............................................................................................................................................ 10 Figure 1 ................................................................................................................................................ -
Cessna Model 150M Performance- Cessna Specifications Model 150M Performance - Specifications
PILOT'S OPERATING HANDBOOK ssna 1977 150 Commuter CESSNA MODEL 150M PERFORMANCE- CESSNA SPECIFICATIONS MODEL 150M PERFORMANCE - SPECIFICATIONS SPEED: Maximum at Sea Level 109 KNOTS Cruise, 75% Power at 7000 Ft 106 KNOTS CRUISE: Recommended Lean Mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve at 45% power. 75% Power at 7000 Ft Range 340 NM 22.5 Gallons Usable Fuel Time 3.3 HRS 75% Power at 7000 Ft Range 580 NM 35 Gallons Usable Fuel Time 5. 5 HRS Maximum Range at 10,000 Ft Range 420 NM 22. 5 Gallons Usable Fuel Time 4.9 HRS Maximum Range at 10,000 Ft Range 735 NM 35 Gallons Usable Fuel Time 8. 5 HRS RATE OF CLIMB AT SEA LEVEL 670 FPM SERVICE CEILING 14, 000 FT TAKEOFF PERFORMANCE: Ground Roll 735 FT Total Distance Over 50-Ft Obstacle 1385 FT LANDING PERFORMANCE: Ground Roll 445 FT Total Distance Over 50-Ft Obstacle 107 5 FT STALL SPEED (CAS): Flaps Up, Power Off 48 KNOTS Flaps Down, Power Off 42 KNOTS MAXIMUM WEIGHT 1600 LBS STANDARD EMPTY WEIGHT: Commuter 1111 LBS Commuter II 1129 LBS MAXIMUM USEFUL LOAD: Commuter 489 LBS Commuter II 471 LBS BAGGAGE ALLOWANCE 120 LBS WING LOADING: Pounds/Sq Ft 10.0 POWER LOADING: Pounds/HP 16.0 FUEL CAPACITY: Total Standard Tanks 26 GAL. Long; Range Tanks 38 GAL. OIL CAPACITY 6 QTS ENGINE: Teledyne Continental O-200-A 100 BHP at 2750 RPM PROPELLER: Fixed Pitch, Diameter 69 IN. D1080-13-RPC-6,000-12/77 PILOT'S OPERATING HANDBOOK Cessna 150 COMMUTER 1977 MODEL 150M Serial No. -
July2020.Pdf
The JULY 2020 TWIN CESSNA Flyer FEATURING: THORNTON 310 - Youtube “310 PILOT” INTERIOR RENOVATIONS - PT. 1 FLY LIKE A PRO - TEN TIPS READERS WRITE SupportingSupporting Twin Twin Cessna Cessna Owners Owners Worldwide Worldwide since since 1988 1988 The AdvantageBetter Parts • Better Engines Cessna • Beechcraft • Cirrus Cessna: T206 TSIO-520-M P210 TSIO-520-P, -AF Beechcraft Bonanza: T210 TSIO-520-R 414A TSIO-520-NB 421B GTSIO-520-H F33, A36 IO-520-BB 310R IO-520-MB A36 IO-550-B T310 TSIO-520-BB, EB 421C GTSIO-520-L, -N Stock & Turbo-Normalized T310 TSIO-520-NB A36TC TSIO-520-UB 320 TSIO-520-EB, -NB Beechcraft Baron: B36TC TSIO-520-UB 335 TSIO-520-EB 58 IO-520-CB 340/A TSIO-520-NB 58 IO-550-C Cirrus: 402 B/C TSIO-520-EB/-VB 58 P/ TC TSIO-520-LB SR22 IO-550-N 404 GTSIO-520-M 58 P/ TC TSIO-520-WB Stock & Turbo-Normalized 414 TSIO-520-NB Critical Gears In Stock! NEW Crankcases for: RAM PMA-New gears are back in stock. If you are overhauling an • Beechcraft Baron • Cessna T310 engine (of having someone overhaul yours), contact RAM to get (58, 58P/TC) • Cessna 320 the best parts for your engine at a fraction of the OEM price! • Beechcraft Bonanza • Cessna 335 Large Cam Gear (C33A, E33A/C, F33, S35, • Cessna 340/A Replaces OEM #: 656818, V35/A/B, A36, A36TC, B36TC) • Cessna 402B/C 656031, 655516, 631845 • Cessna 310R • Cessna 414 RAM PN: 2078-1 • Cessna 414A Dealer Price: $850 • Cirrus SR22 Cost-Effective relief from Continental Critical Service Bulletin CSB05-8D Large Crankshaft Gear Replaces OEM #: 656991, 632893 RAM PN: 2074-1 Dealer Price: $896 Small Crankshaft Gear Replaces OEM #: 657175, 656989, 653652, 632892, 629301 RAM PN: 2075-11 AIRCRAFT PARTS STORE Dealer Price: $395 • SINCE 1976 • RAM AIRCRAFT, LP • SINCE 1976 • ©2020 RAM Aircraft, LP TTCF052720 The SM TWIN CESSNA Flyer FEATURES sm The Twin Cessna Flyer Wolter, owner of Air Mod Inc., one of the P.O. -
2014 FACT BOOK Textron Inc
2014 FACT BOOK Textron Inc. is a $13.9 billion multi-industry company with approximately 34,000 employees. The company leverages its global network of aircraft, defense and intelligence, industrial and finance businesses to provide customers with innovative solutions and services. Textron is known around the world for its powerful brands such as Beechcraft, Bell Helicopter, Cessna, E-Z-GO, Greenlee, Hawker, Jacobsen, Kautex, Lycoming, Textron Systems, Textron Financial Corporation and TRU Simulation + Training. KEY EXECUTIVES SCOTT C. DONNELLY FRANK T. CONNOR Scott C. Donnelly was named chief Frank T. Connor joined Textron as executive executive officer in December 2009 and vice president and chief financial officer in chairman of the board in September 2010. August 2009. Connor came to Textron after Donnelly joined Textron as executive vice a 22-year career at Goldman, Sachs & Co. president and chief operating officer in where he was most recently managing June 2008 and was promoted to president director and head of Telecom Investment in January 2009. Prior to joining Textron, Banking. Prior to that, he served as Donnelly was president and CEO for Goldman, Sachs & Co.’s chief operating General Electric (GE) Aviation. officer of Telecom, Technology and Media Scott C. Donnelly Frank T. Connor Investment Banking. Chairman, President and Executive Vice President Chief Executive Officer and Chief Financial Officer Scott A. Ernest John L. Garrison Jr. Ellen M. Lord J. Scott Hall R. Danny Maldonado Textron Aviation Bell Helicopter Textron Systems Segment Industrial Segment Finance Segment President and CEO President and CEO President and CEO President and CEO President and CEO Revenue by Segment Revenue by Customer Type Revenue by Geography Textron Aviation 33% Commercial 65% U.S. -
Project Hegaasus
PROJECT HEGAASUS Loughborough University, UK Virginia Tech, USA Powertrain Department Structures Department Aircraft Systems Department Aircraft Performance Department Business and Sales Department Modelling Department HYBRID ELECTRIC GENERAL AVIATION AIRCRAFT 2018 AIAA UNDERGRADUATE DESIGN COMPETITION Hybrid Electric General Aviation Aircraft Proposal HAMSTERWORKS DESIGN TEAM Sammi Rocker (USA) Daniel Guerrero (UK) Kyle Silva (USA) Design and Modelling Aircraft Integration Landing Gear & Certification AIAA – 543803 AIAA – 921916 AIAA –921097 Ashley Peyton-Bruhl (UK) Danny Fritsch (USA) Nathaniel Marsh (UK) Business & Sales Flight Physics Propulsion Design AIAA – 921913 AIAA-921435 AIAA-921919 Troy Bergin (USA) Jennifer Glover (UK) Alexander Mclean (USA) Structural Design Powertrain Design Stability & Performance AIAA – 736794 AIAA - 921554 AIAA - 921291 Dhirun Mistry (UK) Pradeep Raj, Ph.D. (USA) James Knowles, Ph.D. (UK) Avionic Systems Virginia Tech Advisor Loughborough University Advisor AIAA – 921917 i Hybrid Electric General Aviation Aircraft Proposal CONTENTS HAMSTERWORKS DESIGN TEAM ................................................................................................................ I LIST OF FIGURES .............................................................................................................................................V LIST OF TABLES ........................................................................................................................................... VII LIST OF ABBREVIATIONS -
Lancair's Experimentalkitplane Is Revolutionary
lancair's Experimentalkitplane isrevolutionary _____ he air traffic controllers couldn't seem to get the name of Laneair's turboprop, the Evolution, quite right. During our short taxi for departure, both ground and local control• lers at Cincinnati Municipal Airport Lunken Field referred to the sleek, four-seat kit airplane as "Revolution." Cleared for takeoff on Runway 21 Left, Lancair dealer and demo pilot Doug Walker advanced the power lever on the 750-shaft-horse• power Pratt & Whitney PT6A-135A.As the four-blade Hartzell prop bit into the humid air and wisps of condensation swirled from the tips, it occurred to me that perhaps the controllers had it right. This high-fly• ing, 300-knot, carbon-fiber greyhound-with its standardized FAR Part 23-compliant construction, $1.3million price tag, and mandatory flight test and training programs-is seeking to completely redefine the top end of the Experimental marketplace. And if that kind of rapid, whole• sale change isn't the stuff of revolution, what is? Walker limits engine power at takeoff to 1,280 pound feet of torque (about 550 shp) so as not to overwhelm the rudder with left-turning P-factor. We're airborne after a 1,200-foot ground roll and free to add full power. Doing so at Vy will result in a maximum rate of climb touch• ing 4,000 fpm, but our goals on this evening flight aren't that ambitious. We're simply keeping pace with an IO-550-powered Bonanza A36 that's SO I AOPA PIlOT August 2012 - YOU SAY YOU WANT AN EVOLUTION,.,t. -
Pdf Appendix 4B2 Tonkin and Taylor Airnoise Contours Memo Pdf, 243 KB Download
Memo To: Emma Ensor Job No: 1013185 From: Darran Humpheson Date: 03 December 2020 Subject: Te Kowhai Airfield airnoise contours Tonkin & Taylor Ltd (T+T) has undertaken an assessment of aircraft noise on behalf of Waikato District Council (WDC) as part of their district plan review. T+T has modelled aircraft noise contours of the Te Kowhai Airfield as part of the review process and compared these contours against those provided by Marshall Day Acoustics (MDA) in their consultant advice note (CAN) dated 8 October 2018. MDA subsequently provided their noise model’s input in a spreadsheet on 23 October 2020. T+T received this information from WDC on 27 October 2020 and have used this information to generate new contours using the US FAA’s AEDT 3c1 aircraft noise modelling software. These new contours are near identical to those provided in the MDA CAN, which was generated using the FAA’s INM2 software. The additional noise contribution from taxiing aircraft has a minimal effect on the size and shape of the contours and has been ignored. WDC requested a further set of noise contours to reflect an operational scenario of 15,000 aircraft movements per year, no flights between 10pm and 7am and no flight training school or circuit training flights. The no flights request between 10pm and 7am was already included within the MDA contours. New 55 dB Ldn Outer Control Boundary (OCB) and 65 dB Air Noise Boundary (ANB) contours are included at Enclosure 1. The contours include a comparison to the MDA OCB and ANB contours, which were based on 21,000 aircraft flight movements per annum, which is the equivalent of 25,5538 annualised busy day movements. -
Amateur-Built Lancair 360, VH-ZNZ
ATSB TRANSPORT SAFETY INVESTIGATION REPORT Aviation Occurrence Report – 200601688 Final Engine power loss – Bankstown Airport – 5 April 2006 VH-ZNZ Amateur-built Lancair 360 ATSB TRANSPORT SAFETY INVESTIGATION REPORT Aviation Occurrence Report 200601688 Final Engine power loss – Bankstown Airport – 5 April 2006 VH-ZNZ Amateur-built Lancair 360 Released in accordance with section 25 of the Transport Safety Investigation Act 2003 - i - Published by: Australian Transport Safety Bureau Postal address: PO Box 967, Civic Square ACT 2608 Office location: 15 Mort Street, Canberra City, Australian Capital Territory Telephone: 1800 621 372; from overseas + 61 2 6274 6590 Accident and serious incident notification: 1800 011 034 (24 hours) Facsimile: 02 6274 6474; from overseas + 61 2 6274 6474 E-mail: [email protected] Internet: www.atsb.gov.au © Commonwealth of Australia 2007. This work is copyright. In the interests of enhancing the value of the information contained in this publication you may copy, download, display, print, reproduce and distribute this material in unaltered form (retaining this notice). However, copyright in the material obtained from non- Commonwealth agencies, private individuals or organisations, belongs to those agencies, individuals or organisations. Where you want to use their material you will need to contact them directly. Subject to the provisions of the Copyright Act 1968, you must not make any other use of the material in this publication unless you have the permission of the Australian Transport Safety Bureau. Please direct requests for further information or authorisation to: Commonwealth Copyright Administration, Copyright Law Branch Attorney-General’s Department, Robert Garran Offices, National Circuit, Barton ACT 2600 www.ag.gov.au/cca ISBN and formal report title: see ‘Document retrieval information’ on page iii. -
STC / TC KITS CONVERSION CATALOG Mccauley PROPELLERS for YOUR GRAND CARAVAN
STC / TC KITS CONVERSION CATALOG McCAULEY PROPELLERS FOR YOUR GRAND CARAVAN STC / TC KITS CONVERSION CATALOG [email protected] | 316.831.4021 | WWW.MCCAULEY.TEXTRON.COM Table of Contents Aircraft Manufacturer/Type Beechcraft Jetstream Single-Engine Piston Turboprop Twin-Engine Piston Turboprop Maule Single-Engine Piston Bellanca Single-Engine Piston Micco Single-Engine Piston Cessna Single-Engine Piston Mooney Twin-Engine Piston Single-Engine Piston Turboprop Spinner Kits Navion Single-Engine Piston Cirrus Single-Engine Piston Piper Single-Engine Piston De Havilland Twin-Engine Piston Turboprop Turboprop Grumman Socata Twin-Engine Piston Single-Engine Piston McCauley Propeller Systems 9709 E Central Wichita, KS 67206 (800) 621-7767 (316) 831-4021 www.mccauley.textron.com McCauley Conversion Abbreviation Guide PL-12345 — McCauley STC kit* PL — STC kit 12345 — Kit number BAR512-01PAC — McCauley TC kit** BAR — Relates to the application (BAR = Beech Baron models, CES = Cessna multiple models, 206 = Cessna 206 models, MLE = Maule multiple models, etc.) 512-01 — Abbreviated propeller assembly number (e.g., P5125358-01) P — Polished spinner assembly (if not present, indicates non-polished spinner assembly to be painted by customer) AC — Eligible for installation on aircraft with air-conditioning installed 180203-57-1 – McCauley TC kit** 180 — Cessna 180 models 203-57 — Abbreviated propeller assembly number (e.g., P2033909-57) -1 — Denotes variation with kit contents and/or eligibility (e.g., kits 180203-57-1 and 180203-57-2 contain the same P2033909-57 propeller, but a different spinner assembly is included due to eligibility for different 180 series aircraft) Determining if a kit is provided with or without icing protection.