CarterCopters. Cleaner Greener. Safer. Your affordable environmentally-friendly VTOL technology Carter Aviation Technologies, LLC

Size: px
Start display at page:

Download "CarterCopters. Cleaner Greener. Safer. Your affordable environmentally-friendly VTOL technology Carter Aviation Technologies, LLC"

Transcription

1 CarterCopters Cleaner Greener Your affordable environmentally-friendly VTOL technology Safer 2018 Carter Aviation Technologies, LLC

2 Carter Aviation Is a green VTOL possible? Genesis & Mission: The company has its roots in the wind industry. In the late 70s and early 80s, Carter Wind Systems developed the most efficient wind turbine of its time. The key enabler was the very lightweight high inertia wind turbine blades. This same core technology is a critical enabling element of Carter s Slowed Rotor Compound (SRC) technology. Jumpstarted by the success in the wind industry, Carter Aviation was founded with the mission to develop breakthrough vertical-lift technology Technology aimed at providing the world s safest and most efficient and environmentally friendly runway independent aircraft ever conceived. and they did it!

3 Technology Comparisons Assessment Factors Ducted Fan Helicopter Tiltrotor Fixed-Wing CarterCopter Speeds beyond 350 kts Hover Efficiency N/A Cruise Efficiency Engine Out Safety Stall Characteristics Easy to Fly Ease of Obtaining License Autonomous Potential CarterCopter Stands Out: All aircraft have varying levels of potential across a variety of assessment factors. From speed to hover and cruise efficiency, the CarterCopter hits them all. No other technology provides the level of performance, level of safety, and ease of operation in a single platform. All of this in a cleaner and more cost effective design. Because of these characteristics, the Carter- Copter will emerge in the future as the aircraft of choice. 20 years in the making, this runway independent technology offers the freedom of VTOL operations with the speed and efficiency of conventional fixedwing aircraft, but delivers this performance at an affordable price. this. No other technology has achieved how developed?

4 CarterCopters: Green Technology of Tomorrow Available Today! Gen II Prototype Flight Testing 2010-Present Gen I Prototype Flight Testing Wind Tunnel Test Model Founded Technology Demonstrations: Extreme Cruise Efficiency Jump Takeoffs Zero Roll Landings Broke mu-1 Barrier (Aviation First) Engine Out Safe Recovery and Landing how possible?

5 It s all about Drag Reduction CarterCopter is a simple fixed-wing aircraft first Rotor added for vertical takeoff & landing Rotor RPM greatly reduced for cruise CarterCopter Slowed Rotor: The slowing of the rotor all but eliminates its contribution to drag in cruise flight and thus you re back to a pure fixed-wing aircraft with all the performance benefits and efficiencies. The addition of the rotor and the subsequent slowing of it s RPM to eliminate drag is what gives CarterCopters VTOL performance without the baggage. The baggage being the debilitating impact of an open rotor system in forward flight with all of its associated drag and cruise inefficiency. how s it transition?

6 Seamless Transition from Vertical to Translational Flight 2. Transition: Aircraft accelerates & rotor RPM automatically begins to slow (no pilot input required). 4. Landing: Rotor RPM automatically speeds up as aircraft decelerates for landing. Pilot performs simple flare to arrest the sink rate and perform a zero-roll landing. 3. Cruise: Rotor continues to slow automatically to the minimum stable RPM with wings providing 90% of the lift. 1. Takeoff: Rotor is pre-rotated on the ground then disengaged for takeoff. A simple button press and the aircraft automatically jumps off the ground and begins to climb and accelerate. Pilot maintains throttle setting and aircraft pitch like a conventional fixed-wing aircraft. CarterCopter Flying Characterics: CarterCopters are designed to fly generally like conventional general aviation aircraft. With the exception of pre-rotating the rotor in preparation for a vertical takeoff, airmanship and handling of the aircraft will be familiar to fixed-wing pilots. This has been achieved by fully automating aspects of the aircraft control specific to the vertical flight elements and transition to wing borne flight. technologies involved?

7 Enabling Technologies High Inertia Rotor Permits Jump Takeoffs and Safe Engine Out Landings High Mu Ratio Rotor Enables High Speed Forward Flight Tilting Mast Controls Rotor RPM for High Cruise Efficiency High Energy Absorbing Landing Gear Improve Landing Safety All Composite Construction Reduces Weight which Improves Performance High Aspect Ratio Wings Optimized for Cruise Efficiency Safety & Efficiency Focus: Carter SRC technology has demonstrated efficency 3x better than helicopters Safety features are best-in-class for VTOLs and dramatically better than general aviation aircraft the results

8 Relative Comparisons I think we need a revolution in direct operating costs * *Dick Spivey, former director of the Army s AeroFlightDynamics Directorate (AFDD), made these remarks at the American Helicopter Society (AHS) annual forum 69 and published in the AHS Vertiflight magazine (Vol. 59, No. 4) % reduction in Direct Operating Costs Fuel Consumption 1 Operating 2 Acquisition 3 Costs CarterCopters are Sustainable: Consume 1/3 the fuel of Helicopters Operating cost 1/3 that of Helicopters Acquisition cost 1/2 that of Helicopters The Solution Helicopters CarterCopters details?

9 Sample Matchups Representative Helicopters Max Speed (kts) Range (nm) Payload (lbs) EC EC , Fuel per Mile (lbs per nm) 206B , R44 (Raven II) R Average lbs per nm CarterCopter , lbs per nm Data Source: Conklin & de Decker supplemented with OEM published specifications CarterCopter Performance Above based on the 4-place aircraft with a 45 ft rotor and 38 ft wingspan powered by the Lycoming TIO-540. At 17,500 ft altitude and best range cruise speeds, this aircraft can deliver a 976 nm range! Clean Technology: Farther Faster Carrying more Fraction of the cost On less fuel! how clean?

10 Emissions Billion Metric Tons of CO Carbon emissions per nautical mile Green Technology for a Brighter Future how achieved?

11 Effective Lift to Drag (L/D e ) Cruise Efficiency Better True Airspeed (mph) CarterCopter (4k ft) CarterCopter (25k ft) CarterCopter Advantage: Typical Helo L/De ~4 or slightly higher CarterCopter 3x better than Helos Represents world s most efficient VTOL VTOL Safety?

12 Rotor Energy / Pounds Gross Weight VTOL Safety 1400 World Class Better Minimal Margin Good Margin R22 OH A CarterCopter UH-60 CH AH-1 CarterCopter Soars: CarterCopters are equipped with an ultra high inertia rotor that generates tremendous energy. It is this energy that is harvested to perform safe zero roll landings time after time. For the world s helicopter fleet, landing on rotor energy alone is an emergency procedure and can result in significant damage to the aircraft or worse. CarterCopter rotor technology makes these landings routine. why important?

13 Safety Events Leading to Autorotation Helo Carter Copter Helo Implications CarterCopter Implications Engine Failure Fuel Starvation Main Gearbox Failure Tailrotor Driveshaft Failure Tailrotor Gearbox Failure Emergency procedure - Enter Autorotation. Specific helo type and pilot proficiency determine outcome Emergency procedure - Enter Autorotation. Specific helo type and pilot proficiency determine outcome Emergency procedure - Enter Autorotation. Specific helo type and pilot proficiency determine outcome Emergency procedure - Enter Autorotation. Specific helo type and pilot proficiency determine outcome Emergency procedure - Enter Autorotation. Specific helo type and pilot proficiency determine outcome Perform normal landing Perform normal landing Main gearbox not required in flight with a CarterCopter Tailrotor driveshaft not required in a CarterCopter Tailrotor gearbox not required in a CarterCopter Autorotations are a very tricky maneuver even for high time experienced pilots. Many factors determine the outcome. more on safety

14 Safety Helicopter vs Fixed-wings: Helicopter manufacturers have long claimed safety advantages over fixed-wing aircraft. The basis of the claim is that a helicopter can land practically anywhere since it can autorotate and doesn t require a runway. While this is true, successfully performing an autorotation in the real world typically results in substantial damage to the aircraft, banged up occupants or worse. The general safety record of helicopters is more troubling. Tourism Tourism may be one of the least Minor Injuries Serious Injuries Fatalities demanding helicopter missions, but it is not without issues. A study summarized accidents in Hawaii from There were 25 accidents & more than 1 fatality per year. CarterCopter Safety Trumps Them All: CarterCopters have the same advantages of helicopters over fixed-wings, but with a critical exception CarterCopters have enough rotor energy to make a normal landing after an engine failure No other flying machine ever devised can make this claim. Unique technology with exceptional safety. avoid areas

15 Height (feet) Dead Man s Curve Helicopter Height Velocity Sample Diagram Must Avoid Regions Low Speed Region Takeoff Corridor High Speed Region Airspeed (knots) CarterCopters Safe at all Speeds & Altitudes: All helicopters have height-velocity diagrams often referred to as dead man s curves. Although within the helicopter safe flight envelope, these airspeed and altitude combinations must be avoided. If the aircraft has a failure requiring an autorotation while in one of these regions, recovery will not be possible. CarterCopters have no avoid regions within the flight envelope nor a stall speed since lift seamlessly shifts between wing and rotor throughout all speeds regimes. CarterCopters Cleaner, Greener, & Safer. hard to fly?

16 Simple to Fly CarterCopters are Simple to Fly: A personal air vehicle (PAV) with point to point capabilities for the general population (like the Jetsons) is just around the corner. When you combine CarterCopter s inherent safety with the advances made with unmanned aerial vehicles (UAV) it makes for a personal air vehicle that grandparents will feel comfortable about flying to see their grandchildren rather than drive. The aircraft has the potential to very safely takeoff, fly (avoid other aircraft, restricted areas, weather) and land without any input from the pilot/passenger other than to enter the destination and OK the takeoff. Even if the passengers fall asleep and the aircraft runs out of fuel, the aircraft will pick an airport and land itself and if no airport is available, find a flat clear section of land to set down. in the end safety much better than an automobile. hear that?

17 Effective Perceived Noise Level (EPNdB) Acoustics Civil Helicopter Acoustic Requirements Cruise Airspeed S-92A Gross Weight (lbs) CarterCopter s Slowed- Rotor Compound Technology is EPNdB quieter than the least noisy helicopters CarterCopters Clean and Quiet: Recall that CarterCopters are essentially a fixed-wing aircraft. As such, they possess fixed-wing acoustic characteristics. Unlike helicopters where the rotor is loaded and therefore noisy throughout the flight envelope, CarterCopters cruise quietly, cleanly, and efficiently through the skies. in summary

18 CarterCopters Cleaner 1/3 the carbon Greener Fuel efficient, quietest VTOL Safer Engine failure means normal landing Your affordable environmentally-friendly VTOL technology

The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, The text included here is an approximate transcript

The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, The text included here is an approximate transcript The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, 2017. The text included here is an approximate transcript of the speech given by Jay Carter, founder and CEO of

More information

Product Comparison. F28F vs. Robinson R44

Product Comparison. F28F vs. Robinson R44 Product Comparison F28F vs. Robinson R44 F28F vs. R44 Specs Seats ENSTROM F28F ROBINSON R44 II 3 4 Continuous Engine Power (To Drivetrain) (hp) 225 205 Turbo-Charged? YES Empty Weight (As Configured )

More information

Gyroplane questions from Rotorcraft Commercial Bank (From Rotorcraft questions that obviously are either gyroplane or not helicopter)

Gyroplane questions from Rotorcraft Commercial Bank (From Rotorcraft questions that obviously are either gyroplane or not helicopter) Page-1 Gyroplane questions from Rotorcraft Commercial Bank (From Rotorcraft questions that obviously are either gyroplane or not helicopter) "X" in front of the answer indicates the likely correct answer.

More information

The Skycar 400 High-speed, 4-passenger VTOL aircraft

The Skycar 400 High-speed, 4-passenger VTOL aircraft The Skycar 400 High-speed, 4-passenger VTOL aircraft THE MOLLER SKYCAR 400 Over the past 30+ years Moller International and it predecessor companies have been working on the development of the technologies

More information

AIR TRACTOR, INC. OLNEY, TEXAS

AIR TRACTOR, INC. OLNEY, TEXAS TABLE OF CONTENTS LOG OF REVISIONS... 2 DESCRIPTION... 4 SECTION 1 LIMITATIONS... 5 SECTION 2 NORMAL PROCEDURES... 8 SECTION 3 EMERGENCY PROCEDURES... 8 SECTION 4 MANUFACTURER'S SECTION - PERFORMANCE...

More information

Flight Test Evaluation of C-130H Aircraft Performance with NP2000 Propellers

Flight Test Evaluation of C-130H Aircraft Performance with NP2000 Propellers Flight Test Evaluation of C-130H Aircraft Performance with NP2000 Propellers Lance Bays Lockheed Martin - C-130 Flight Sciences Telephone: (770) 494-8341 E-Mail: lance.bays@lmco.com Introduction Flight

More information

Product Comparison. 480B vs. Robinson R44

Product Comparison. 480B vs. Robinson R44 Product Comparison 480B vs. Robinson R44 480B vs. Robinson R44 Specifications Enstrom 480B Robinson R44 Seats 1/4 or 2/1 1/3 Continuous Engine Power (To Drivetrain) 277 shp/206 kw 205 shp/183 kw Gross

More information

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system:

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system: Idealized tilt-thrust (U) All of the UAV options that we've been able to analyze suffer from some deficiency. A diesel, fixed-wing UAV could possibly satisfy the range and endurance objectives, but integration

More information

Answer Key. Page 1 of 10

Answer Key. Page 1 of 10 Name: Answer Key Score: [1] When range and economy of operation are the principal goals, the pilot must ensure that the airplane will be operated at the recommended A. equivalent airspeed. B. specific

More information

THE RIGHT HELICOPTER FOR YOUR TRAINING

THE RIGHT HELICOPTER FOR YOUR TRAINING THE RIGHT HELICOPTER FOR YOUR TRAINING 1 Why Choose Enstrom? 50 years of business Price competitive on acquisition and operation Enstrom has won major contracts for training programs Japanese Ground Self-Defense

More information

Weight Effects Part 1

Weight Effects Part 1 Weight Effects Part 1 David F. Rogers Copyright c 1997-1999 David F. Rogers. All rights reserved. Most of us normally operate our aircraft at less than gross weight, yet weight significantly affects the

More information

This Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Corvalis TT.

This Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Corvalis TT. May 2010 TABLE OF CONTENTS This Flight Planning Guide is published for the purpose of providing specific information for evaluating the performance of the Cessna Corvalis TT. This guide is developed from

More information

AT-10 Electric/HF Hybrid VTOL UAS

AT-10 Electric/HF Hybrid VTOL UAS AT-10 Electric/HF Hybrid VTOL UAS Acuity Technologies Robert Clark bob@acuitytx.com Summary The AT-10 is a tactical size hybrid propulsion VTOL UAS with a nose camera mount and a large payload bay. Propulsion

More information

Key Drivers for evtol Design Christopher Silva From VTOL to evtol Workshop May 24, 2018

Key Drivers for evtol Design Christopher Silva From VTOL to evtol Workshop May 24, 2018 Key Drivers for evtol Design Christopher Silva From VTOL to evtol Workshop May 24, 2018 Can we use what we already know? Techniques and processes Aircraft / System design theory: Design Thinking, MDAO,

More information

American Helicopter Society Washington, DC 20 November 2013 Approved for Public Release

American Helicopter Society Washington, DC 20 November 2013 Approved for Public Release SIKORSKY & BOEING JMR TD UPDATE American Helicopter Society Washington, DC 20 November 2013 Approved for Public Release Vertical Lift / FVL Copyright 2010 Boeing. All rights reserved. Boeing Proprietary

More information

Prime Aircraft, LLC Aircraft Sales & Acquisitions

Prime Aircraft, LLC Aircraft Sales & Acquisitions King Air Modifications Probably because the King Air is the most popular corporate turboprop every built and Beechcraft has manufactured over 6,000 units since 1964, many third party companies have come

More information

Sierra. R/STOL High Lift Systems. Toll Free LANCAIR. Sierra R/STOL High Lift System Benefits DURING APPROACH AND LANDING DURING TAKEOFF

Sierra. R/STOL High Lift Systems. Toll Free LANCAIR. Sierra R/STOL High Lift System Benefits DURING APPROACH AND LANDING DURING TAKEOFF Sierra R/STOL High Lift Systems Complete R/STOL Systems include everything your aircraft needs for the utmost in performance. For expanded utility, increased safety and improved performance get off the

More information

Performance means how fast will it go? How fast will it climb? How quickly it will take-off and land? How far it will go?

Performance means how fast will it go? How fast will it climb? How quickly it will take-off and land? How far it will go? Performance Concepts Speaker: Randall L. Brookhiser Performance means how fast will it go? How fast will it climb? How quickly it will take-off and land? How far it will go? Let s start with the phase

More information

Evolution of Rotary Wing Technology, Enhanced Capabilities for Humanitarian Operations

Evolution of Rotary Wing Technology, Enhanced Capabilities for Humanitarian Operations Evolution of Rotary Wing Technology, Enhanced Capabilities for Humanitarian Operations Global Humanitarian Aviation Conference Lisbon, 11 th October 2017 Clive Scott, Director of Tiltrotor and Unmanned

More information

Innovating the future of disaster relief

Innovating the future of disaster relief Innovating the future of disaster relief American Helicopter Society International 33rd Annual Student Design Competition Graduate Student Team Submission VEHICLE OVERVIEW FOUR VIEW DRAWING INTERNAL COMPONENTS

More information

On-Demand Mobility Electric Propulsion Roadmap

On-Demand Mobility Electric Propulsion Roadmap On-Demand Mobility Electric Propulsion Roadmap Mark Moore, ODM Senior Advisor NASA Langley Research Center EAA AirVenture, Oshkosh July 22, 2015 NASA Distributed Electric Propulsion Research Rapid, early

More information

ADVANCED TECHNOLOGY. Automatic Clutch Engagement. Simplifies startup procedure and reduces the possibility of an overspeed.

ADVANCED TECHNOLOGY. Automatic Clutch Engagement. Simplifies startup procedure and reduces the possibility of an overspeed. ADVANCED TECHNOLOGY Advanced Warning Devices. The instrument panel includes low fuel warning light, main gearbox temperature and chip lights, tail gearbox chip light, low oil pressure light, engine fire

More information

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols Contents Preface Acknowledgments List of Tables Nomenclature: organizations Nomenclature: acronyms Nomenclature: main symbols Nomenclature: Greek symbols Nomenclature: subscripts/superscripts Supplements

More information

Sn: Registration: C-GGJS

Sn: Registration: C-GGJS R66, R44 &R22 ROBINSON HELICOPTER SALES Type: R44 Model: Raven II Year: 2008 Total Time: 2205 Time Since Overhaul: 10 hours Sn: 12254 Registration: C-GGJS Location: Calgary, Alberta, Canada Price: $405,000

More information

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA MT DIREION DE PERSONL ERONUTIO DPTO. DE INSTRUION PREGUNTS Y OPIONES POR TEM 1 TEM: 0645 OM-RT - ircraft Performance - hap. 8 OD_PREG: PREG20098661 (5208) PREGUNT: t higher elevation airports the pilot

More information

Product Comparison. 480B vs. Eurocopter EC120B

Product Comparison. 480B vs. Eurocopter EC120B Product Comparison 480B vs. Eurocopter EC120B 480B vs. Eurocopter EC120B Specifications Gross Weight = 2,800 lbs Gross Weight = 2,976 lbs Enstrom 480B Eurocopter EC120B Seats 1/4 or 2/1 1/4 or 2/3 Continuous

More information

Appenidix E: Freewing MAE UAV analysis

Appenidix E: Freewing MAE UAV analysis Appenidix E: Freewing MAE UAV analysis The vehicle summary is presented in the form of plots and descriptive text. Two alternative mission altitudes were analyzed and both meet the desired mission duration.

More information

FLASHCARDS AIRCRAFT. Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation.

FLASHCARDS AIRCRAFT. Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation. AIRCRAFT FLASHCARDS Courtesy of the Air Safety Institute, a Division of the AOPA Foundation, and made possible by AOPA Services Corporation. Knowing your aircraft well is essential to safe flying. These

More information

POWER. SAFETY. PERFORMANCE. ALL IN ONE PACKAGE.

POWER. SAFETY. PERFORMANCE. ALL IN ONE PACKAGE. POWER. SAFETY. PERFORMANCE. ALL IN ONE PACKAGE. Some missions require more from a helicopter. More speed. More power. More payload. More productivity. These missions require the MD 600N. This single-turbine

More information

AIRCRAFT FAMILIARIZATION. Some questions may not apply to the aircraft you are flying.

AIRCRAFT FAMILIARIZATION. Some questions may not apply to the aircraft you are flying. 541-895-5935 Name Date AIRCRAFT FAMILIARIZATION Note: If this information is not provided in the aircraft s flight manual give it your best guess. Some questions may not apply to the aircraft you are flying.

More information

XIV.C. Flight Principles Engine Inoperative

XIV.C. Flight Principles Engine Inoperative XIV.C. Flight Principles Engine Inoperative References: FAA-H-8083-3; POH/AFM Objectives The student should develop knowledge of the elements related to single engine operation. Key Elements Elements Schedule

More information

Beechcraft Bonanza. 550 Tuned Induction Conversion. STC for Teledyne Continental IO-550-R for the Beechcraft Bonanza

Beechcraft Bonanza. 550 Tuned Induction Conversion. STC for Teledyne Continental IO-550-R for the Beechcraft Bonanza Beechcraft Bonanza 550 Tuned Induction Conversion STC for Teledyne Continental for the Beechcraft Bonanza 1 (800) 334-2001 You Can Have More than a New Engine in Your Bonanza You Can Experience a New Aircraft

More information

31 st Annual American Helicopter Society Student Design Competition: Graduate Submission

31 st Annual American Helicopter Society Student Design Competition: Graduate Submission Rotorcraft Adaptive and Morphing Structures Lab The Emperor UAV: Executive Summary George Jacobellis Alex Angilella Jean-Paul Reddinger Andrew Howard Matthew Misiorowski Michael Pontecorvo Jayanth Krishnamurthi

More information

Initial / Recurrent Ground Take-Home Self-Test: The Beechcraft 58 Baron Systems, Components and Procedures

Initial / Recurrent Ground Take-Home Self-Test: The Beechcraft 58 Baron Systems, Components and Procedures Initial / Recurrent Ground Take-Home Self-Test: The Beechcraft 58 Baron Systems, Components and Procedures Flight Express, Inc. This take-home self-test partially satisfies the recurrent ground training

More information

Cessna Citation Model Stats

Cessna Citation Model Stats Cessna Citation Model Stats Cessna Citation Sovereign - Dimensions Length 63 ft 6 in (19.35 m) Height 20 ft 4 in (6.20 m) Wingspan 72 ft 4 in (22.04 m) Wing Wing Area Wing Sweep Wheelbase Tread 516 sq

More information

Skip the Traffic: Fly Your Car A User s Perspective

Skip the Traffic: Fly Your Car A User s Perspective Skip the Traffic: Fly Your Car A User s Perspective Wednesday October 11, 2017 3:30 pm - 4:30 pm PRESENTED BY: Brian Purdy Samson Switchblade Owner Switchblade Demonstrations Where s My Flying Car 2 Skip

More information

Technology for the Future of Vertical Lift

Technology for the Future of Vertical Lift Presented to: Italian Vertical Lift Community Technology for the Future of Vertical Lift Approved for public release; distribution unlimited. Review completed by the AMRDEC Public Affairs Office 15 Nov

More information

Test of. Boeing MH-47G Chinook. Produced by Area-51 Simulations

Test of. Boeing MH-47G Chinook. Produced by Area-51 Simulations Test of Boeing MH-47G Chinook Produced by Area-51 Simulations The Boeing MH-47G is a part of the Boeing CH-47 family which is a twin engine, tandem rotor, heavylift helicopter originally built by Boeing

More information

Introduction. Fuselage/Cockpit

Introduction. Fuselage/Cockpit Introduction The Moravan Zlin 242L is a fully aerobatic 2 seat aircraft designed to perform all advanced flight maneuvers within an envelope of -3.5 to +6 Gs. Many military and civilian flight-training

More information

Innovative Airship Solutions from Guardian Flight Systems

Innovative Airship Solutions from Guardian Flight Systems Innovative Airship Solutions from Guardian Flight Systems ITAR Disclaimer: This presentation does not contain Technical Data per 22 CFR 120.10 distribution unrestricted w/o 3282. Presentation Preview About

More information

Electric VTOL Aircraft

Electric VTOL Aircraft Electric VTOL Aircraft Subscale Prototyping Overview Francesco Giannini fgiannini@aurora.aero 1 08 June 8 th, 2017 Contents Intro to Aurora Motivation & approach for the full-scale vehicle Technical challenges

More information

Mercury VTOL suas Testing and Measurement Plan

Mercury VTOL suas Testing and Measurement Plan Mercury VTOL suas Testing and Measurement Plan Introduction Mercury is a small VTOL (Vertical Take-Off and Landing) aircraft that is building off of a quadrotor design. The end goal of the project is for

More information

Designing evtol for the Mission NDARC NASA Design and Analysis of Rotorcraft. Wayne Johnson From VTOL to evtol Workshop May 24, 2018

Designing evtol for the Mission NDARC NASA Design and Analysis of Rotorcraft. Wayne Johnson From VTOL to evtol Workshop May 24, 2018 Designing evtol for the Mission NDARC NASA Design and Analysis of Rotorcraft Wayne Johnson From VTOL to evtol Workshop May 24, 2018 1 Conceptual Design of evtol Aircraft Conceptual design Define aircraft

More information

BELL 206L4 A reliable multi-mission capable helicopter with low operating costs.

BELL 206L4 A reliable multi-mission capable helicopter with low operating costs. BELL 206L4 A reliable multi-mission capable helicopter with low operating costs. CORPORATE The Bell 206L4 is designed to be the ideal flying workplace. It comfortably seats up to six passengers with one

More information

Lockheed Martin. Team IDK Seung Soo Lee Ray Hernandez Chunyu PengHarshal Agarkar

Lockheed Martin. Team IDK Seung Soo Lee Ray Hernandez Chunyu PengHarshal Agarkar Lockheed Martin Team IDK Seung Soo Lee Ray Hernandez Chunyu PengHarshal Agarkar Abstract Lockheed Martin has developed several different kinds of unmanned aerial vehicles that undergo harsh forces when

More information

ADVENT. Aim : To Develop advanced numerical tools and apply them to optimisation problems in engineering. L. F. Gonzalez. University of Sydney

ADVENT. Aim : To Develop advanced numerical tools and apply them to optimisation problems in engineering. L. F. Gonzalez. University of Sydney ADVENT ADVanced EvolutioN Team University of Sydney L. F. Gonzalez E. J. Whitney K. Srinivas Aim : To Develop advanced numerical tools and apply them to optimisation problems in engineering. 1 2 Outline

More information

Clean Sky 2. LifeCraft Demonstrationt (IADP RC 2 & ITDs) Consultation meetings Brussels th December 2012 OUTLINE

Clean Sky 2. LifeCraft Demonstrationt (IADP RC 2 & ITDs) Consultation meetings Brussels th December 2012 OUTLINE Clean Sky 2 LifeCraft Demonstrationt (IADP RC 2 & ITDs) Consultation meetings Brussels 10-14 th December 2012 1 1 LifeCraft - The Compound Demo OUTLINE Presentation of the Compound R/C Concept Impact &

More information

550 T.I. ENGINE FOR THE BEECHCRAFT BONANZA STC FOR TELEDYNE CONTINENTAL IO-550-R FOR THE BEECHCRAFT BONANZA

550 T.I. ENGINE FOR THE BEECHCRAFT BONANZA STC FOR TELEDYNE CONTINENTAL IO-550-R FOR THE BEECHCRAFT BONANZA 550 T.I. ENGINE FOR THE BEECHCRAFT BONANZA STC FOR TELEDYNE CONTINENTAL IO-550-R FOR THE BEECHCRAFT BONANZA You Can Have More Than A New Engine In Your Bonanza You Can Experience A New Aircraft. Our company

More information

52 BACKYARDFLYER.COM FLY

52 BACKYARDFLYER.COM FLY 52 BACKYARDFLYER.COM FLY HELIS IN1O EASY STEPS by Klaus Ronge Photography by Hope McCall & Pete Hall Flying model helicopters is exciting and fun and looks very easy, that is, until you try it. Unlike

More information

How to use the Multirotor Motor Performance Data Charts

How to use the Multirotor Motor Performance Data Charts How to use the Multirotor Motor Performance Data Charts Here at Innov8tive Designs, we spend a lot of time testing all of the motors that we sell, and collect a large amount of data with a variety of propellers.

More information

Electric Drive - Magnetic Suspension Rotorcraft Technologies

Electric Drive - Magnetic Suspension Rotorcraft Technologies Electric Drive - Suspension Rotorcraft Technologies William Nunnally Chief Scientist SunLase, Inc. Sapulpa, OK 74066-6032 wcn.sunlase@gmail.com ABSTRACT The recent advances in electromagnetic technologies

More information

PA-28R 201 Piper Arrow

PA-28R 201 Piper Arrow Beale Aero Club Aircraft Written Test PA-28R 201 Piper Arrow (Required passing score: 80%) 1. If an engine power loss occurs immediately after take off, the pilot s reaction should be to: a. maintain safe

More information

Lip wing Lift at zero speed

Lip wing Lift at zero speed Lip wing Lift at zero speed Dusan Stan, July 2014 http://hypertriangle.com/lipwing.php dusan.stan@hypertriangle.com HyperTriangle 2014 Lip_wing_Lift_at_zero_speed_R2.doc Page 1 of 7 1. Introduction There

More information

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A11EA DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A11EA Revision 9 American General Aircraft Holding Co. AA-1 AA-1A AA-1B AA-1C June 7, 1995 TYPE CERTIFICATE DATA SHEET NO. A11EA This data sheet,

More information

SECTION 3 EMERGENCY PROCEDURES CONTENTS

SECTION 3 EMERGENCY PROCEDURES CONTENTS CONTENTS Page Definitions.................................. 3-1 Power Failure - General......................... 3-1 Power Failure Above 500 feet AGL................ 3-2 Power Failure Between 8 and 500

More information

Better Performance Starts with Better Technology THE BLR ADVANTAGE

Better Performance Starts with Better Technology THE BLR ADVANTAGE Better Performance Starts with Better Technology THE BLR ADVANTAGE Does it work? Ask a Pilot. THE BLR ADVANTAGE BLR Aerospace FastFin and Dual Tailboom Strakes will dramatically improve the performance

More information

Elmendorf Aero Club Aircraft Test

Elmendorf Aero Club Aircraft Test DO NOT WRITE ON THIS TEST FEB 2013 Elmendorf Aero Club Aircraft Test Cessna - 172 For the following questions, you will need to refer to the Pilots Information Manual for the C-172R (180hp). The bonus

More information

A short Company & Technology Overview

A short Company & Technology Overview A short Company & Technology Overview The Future of Rotary Wings Workshop Centro Alti Studi della Difesa (CASD) Rome, November 22 nd, 2012 An introduction to K4A K4A was founded in 2005 by Engineers and

More information

Innovation Takes Off

Innovation Takes Off Innovation Takes Off Clean Sky 2 Information Day Bonn, 20 February 2014 Fast Rotorcraft IADP: LifeRCraft Compound Rotorcraft Hans Barnerssoi, Airbus Helicopters Innovation Takes Off LifeRCraft 1 - The

More information

TRAINERS PIPER PROVEN

TRAINERS PIPER PROVEN TRAINERS PIPER PROVEN 2. FROM STUDENT TO PROFESSIONAL PILOT, PIPER LEADS THE WAY ARCHER TX... 4 ARROW... 6 SEMINOLE... 8 SENECA V...10 PIPER EXPERIENCED The Piper family of training aircraft have taught

More information

Tilt-rotor Ducted Fans and their Applications

Tilt-rotor Ducted Fans and their Applications Tilt-rotor Ducted Fans and their Applications Jacob A. Wilroy University of Alabama, Tuscaloosa, AL 35487 Introduction Ducted fans are capable of producing more efficient thrust, as well as decreasing

More information

CHAPTER 2 THE TUTOR. Introduction

CHAPTER 2 THE TUTOR. Introduction CHAPTER 2 THE TUTOR Introduction 1. AEFs. The Royal Air Force has 12 units throughout the country known as Air Experience flights (AEFs). Their role is to provide air experience flying for cadets and they

More information

USAF Aero Club T-41B (Cessna R-172E) Aircraft Exam Updated February 2017

USAF Aero Club T-41B (Cessna R-172E) Aircraft Exam Updated February 2017 USAF Aero Club T-41B (Cessna R-172E) Aircraft Exam Updated February 2017 Instructions Complete the supplement following exam using the answer sheet provided. Do not assume information not specifically

More information

AVIATION INVESTIGATION REPORT A08P0035 LOSS OF VISUAL REFERENCE / COLLISION WITH TERRAIN

AVIATION INVESTIGATION REPORT A08P0035 LOSS OF VISUAL REFERENCE / COLLISION WITH TERRAIN AVIATION INVESTIGATION REPORT A08P0035 LOSS OF VISUAL REFERENCE / COLLISION WITH TERRAIN SEQUOIA HELICOPTERS LIMITED BELL 212 (HELICOPTER) C-GERH GOLDEN, BRITISH COLUMBIA, 9 nm W 07 FEBRUARY 2008 The Transportation

More information

Test like you Train Train like you Fight

Test like you Train Train like you Fight War-Winning Winning Capabilities On Time, On Cost Test like you Train Train like you Fight How Today s s Complexity Drives Future Range Requirements Major General David J. Eichhorn AFFTC Commander This

More information

INDIAN INSTITUTE OF TECHNOLOGY KANPUR

INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR Removable, Low Noise, High Speed Tip Shape Tractor Configuration, Cant angle, Low Maintainence Hingelesss, Good Manoeuverability,

More information

Accelerating Innovation for Community Noise and Emissions Reduction

Accelerating Innovation for Community Noise and Emissions Reduction Commercial Airplanes Accelerating Innovation for Community Noise and Emissions Reduction Jeanne Yu Director, BCA Product Development Technology Integration and ecodemonstrator Program February 26, 2018

More information

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA)

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA) ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA) ATI D3 EVENT 8 TH MAY 2018 THE EMERGENCE OF ELECTRIFICATION IN AEROSPACE NICK SILLS, CONTRA ELECTRIC

More information

CESSNA 182 TRAINING MANUAL. Trim Control Connections

CESSNA 182 TRAINING MANUAL. Trim Control Connections Trim Control Connections by D. Bruckert & O. Roud 2006 Page 36 Flaps The flaps are constructed basically the same as the ailerons with the exception of the balance weights and the addition of a formed

More information

FLYING CAR NANODEGREE SYLLABUS

FLYING CAR NANODEGREE SYLLABUS FLYING CAR NANODEGREE SYLLABUS Term 1: Aerial Robotics 2 Course 1: Introduction 2 Course 2: Planning 2 Course 3: Control 3 Course 4: Estimation 3 Term 2: Intelligent Air Systems 4 Course 5: Flying Cars

More information

Robinson R22 Pilot s Technical Quiz

Robinson R22 Pilot s Technical Quiz Robinson R22 Pilot s Technical Quiz Version 1.0a 2002-10-21 Candidate Examiner Name Licence class Licence number Name Licence number Capacity Centre Date Mark (Pass is 80/100= 80%) Instructions: This is

More information

Welcome to the Airbus A380 Basic Manual for Virtual Air Cadet Airlines.

Welcome to the Airbus A380 Basic Manual for Virtual Air Cadet Airlines. Welcome to the Airbus A380 Basic Manual for Virtual Air Cadet Airlines. Performance figures: Max operating speed: 340kts / M0.89 Max gear speed: 250kts / M0.55 Max flap speeds: Code: Select all Flaps Speed

More information

On-Demand Mobility. Aviation s Path to High Speed Regional Mobility

On-Demand Mobility. Aviation s Path to High Speed Regional Mobility On-Demand Mobility Aviation s Path to High Speed Regional Mobility Mark Moore, ODM Senior Advisor Ken Goodrich, ODM Senior Advisor NASA Langley Research Center EAA AirVenture, Oshkosh July 21, 2015 Why

More information

Air Buzz. 32nd Annual AHS International Student Design Competition

Air Buzz. 32nd Annual AHS International Student Design Competition Air Buzz 32nd Annual AHS International Student Design Competition Faculty Advisor: Dr. Daniel Schrage, Daniel.Schrage@aerospace.gatech.edu Ezgi Selin Akdemir esakdemir@gmail.com Undergraduate Middle East

More information

THE KING OF PAYLOAD AND PERFORMANCE

THE KING OF PAYLOAD AND PERFORMANCE THE KING OF PAYLOAD AND PERFORMANCE TECHNICAL SPECIFICATIONS GROSS WEIGHT Standard Model FBA-2C3 GROSS WEIGHT Turbo Model FBA-2C3T > WEIGHT AND BALANCE Maximum Take-Off Weight (MTOW) 3,800 lb 1,724 kg

More information

3. What is the total fuel capacity with normal tanks? Usable? 4. What is the total fuel capacity with long range tanks? Usable?

3. What is the total fuel capacity with normal tanks? Usable? 4. What is the total fuel capacity with long range tanks? Usable? Pilot Name: Last, first, mi. Date: (mo/dy/yr) Instructor: Pass/Fail: Instructors Initials: 1. What is the engine Manufacturer: Model: Type: 2. What is the horsepower rating? 3. What is the total fuel capacity

More information

WHY TWO SPOOLS ARE BETTER THAN ONE: EQUIPPING OUR MILITARY WITH THE BEST TECHNOLOGY FOR EXISTING AND EMERGING THREATS

WHY TWO SPOOLS ARE BETTER THAN ONE: EQUIPPING OUR MILITARY WITH THE BEST TECHNOLOGY FOR EXISTING AND EMERGING THREATS WHY TWO SPOOLS ARE BETTER THAN ONE: EQUIPPING OUR MILITARY WITH THE BEST TECHNOLOGY FOR EXISTING AND EMERGING THREATS SUPERIOR TECHNOLOGY: ATEC s HPW3000 is the superior option to serve as the new engine

More information

New Design Concept of Compound Helicopter

New Design Concept of Compound Helicopter New Design Concept of Compound Helicopter PRASETYO EDI, NUKMAN YUSOFF and AZNIJAR AHMAD YAZID Department of Engineering Design & Manufacture, Faculty of Engineering, University of Malaya, 50603 Kuala Lumpur,

More information

Engines for Green Aviation s Future

Engines for Green Aviation s Future Engines for Green Aviation s Future Alan Epstein Vice President, Technology & Environment Pratt & Whitney EcoAviation Washington, June 2010 Evolution in By-Pass Ratio, Efficiency, & Noise Turbojets Turbofans

More information

AIAA Foundation Undergraduate Team Aircraft Design Competition. RFP: Cruise Missile Carrier

AIAA Foundation Undergraduate Team Aircraft Design Competition. RFP: Cruise Missile Carrier AIAA Foundation Undergraduate Team Aircraft Design Competition RFP: Cruise Missile Carrier 1999/2000 AIAA FOUNDATION Undergraduate Team Aircraft Design Competition I. RULES 1. All groups of three to ten

More information

Technical Challenges and Barriers Affecting Turbo-electric and Hybrid Electric Aircraft Propulsion

Technical Challenges and Barriers Affecting Turbo-electric and Hybrid Electric Aircraft Propulsion Technical Challenges and Barriers Affecting Turbo-electric and Hybrid Electric Aircraft Propulsion Dr. Ajay Misra Deputy Director, Research and Engineering NASA Glenn Research Center Keynote presentation

More information

OPERATING RECOMMENDATIONS

OPERATING RECOMMENDATIONS Operating Recommendations for TIO-540-AE2A Engine in Piper Aircraft Malibu Mirage Lycoming Part Number: SSP-400 OPERATING RECOMMENDATIONS FOR TIO-540-AE2A ENGINE IN PIPER AIRCRAFT MALIBU MIRAGE 2009 by

More information

Brain on Board: From safety features to driverless cars

Brain on Board: From safety features to driverless cars Brain on Board: From safety features to driverless cars Robyn Robertson, M.C.A. President & CEO Traffic Injury Research Foundation 18 th Annual Not By Accident Conference. London, ON, October 18 th, 2016

More information

Airships: A New Horizon for Science April 30 May 3, Worldwide Aeros Corp. Montebello, California. Presented by:

Airships: A New Horizon for Science April 30 May 3, Worldwide Aeros Corp. Montebello, California. Presented by: Airships: A New Horizon for Science April 30 May 3, 2013 Worldwide Aeros Corp. Montebello, California Presented by: Mr. Fred Edworthy V.P. Business Development www.aeroscraft.com 1 25 YEARS INNOVATION,

More information

The new Raisbeck/Hartzell C90 Swept Blade Turbofan Propeller

The new Raisbeck/Hartzell C90 Swept Blade Turbofan Propeller The new Raisbeck/Hartzell C90 Swept Blade Turbofan Propeller the new SWEPT BLADE TURBOFAN PROPELLER FOR THE ENTIRE KING AIR C90 FAMILY developed jointly by Raisbeck Engineering and Hartzell Propeller for

More information

GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E. Name: GACE #: Score: Checked by: CFI #:

GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E. Name: GACE #: Score: Checked by: CFI #: GACE Flying Club Aircraft Review Test 2018 N5312S & N5928E Name: GACE #: Score: Checked by: CFI #: Date: (The majority of these questions are for N5312S. All N5928E questions will be marked 28E) 1. What

More information

REPORT A-008/2008 DATA SUMMARY

REPORT A-008/2008 DATA SUMMARY REPORT A-008/2008 DATA SUMMARY LOCATION Date and time Wednesday, 5 March 2008; 08:25 local time 1 Site Yaiza (Island of Lanzarote) AIRCRAFT Registration Type and model EC-FJV AEROSPATIALE AS-350B2 Operator

More information

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999 AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update Presented to NIAC By Carl Grant November 9th, 1999 DIVERSITECH, INC. Phone: (513) 772-4447 Fax: (513) 772-4476 email: carl.grant@diversitechinc.com

More information

The new Raisbeck/Hartzell C90 Swept Blade Turbofan Propeller

The new Raisbeck/Hartzell C90 Swept Blade Turbofan Propeller The new Raisbeck/Hartzell C90 Swept Blade Turbofan Propeller 2 the new SWEPT BLADE TURBOFAN PROPELLER FOR THE ENTIRE KING AIR C90 FAMILY developed jointly by Raisbeck Engineering and Hartzell Propeller

More information

PRESS RELEASE Q & A. The company decided from the onset to operate under a Boeing licensing umbrella to design and produce parts to Boeing standards.

PRESS RELEASE Q & A. The company decided from the onset to operate under a Boeing licensing umbrella to design and produce parts to Boeing standards. Super98 PRESS RELEASE Q & A How was Super98 started and why? Super98 was started in 2007 by private entrepreneurs and investors with the vision to extend the economic life of the popular MDC heritage TwinJets.

More information

Flight Testing of Your Europa Equipped with the Airmaster Propeller By Bud Yerly Custom Flight Creations, Inc.

Flight Testing of Your Europa Equipped with the Airmaster Propeller By Bud Yerly Custom Flight Creations, Inc. Flight Testing of Your Europa Equipped with the Airmaster Propeller By Bud Yerly Custom Flight Creations, Inc. Once you've selected the desired blade and hub for your Airmaster constant speed propeller,

More information

W-3A Sokół DURABLE AND DEPENDABLE

W-3A Sokół DURABLE AND DEPENDABLE W-3A Sokół DURABLE AND DEPENDABLE OPERATING IN ALL CONDITIONS Highly effective, rugged and reliable, the W-3A Sokół is the intermediate helicopter of choice for multiple utility applications: Exceptional

More information

SCOUT TECHNICAL INFORMATION SAFETY & STABILITY. Autorotation speed. Landing Gears, Absorb System

SCOUT TECHNICAL INFORMATION SAFETY & STABILITY. Autorotation speed. Landing Gears, Absorb System SCOUT HELICOPTER TECHNICAL INFORMATION Seats Power plant 3 210-220 hp Gross Weight Empty Weight 1985 lbs (900 kg) 1169 lbs (530 kg) SAFETY & STABILITY Normal Cruise Max. IAS, Sea Level / Standard Day Autorotation

More information

International Journal of Scientific & Engineering Research, Volume 4, Issue 7, July ISSN BY B.MADHAN KUMAR

International Journal of Scientific & Engineering Research, Volume 4, Issue 7, July ISSN BY B.MADHAN KUMAR International Journal of Scientific & Engineering Research, Volume 4, Issue 7, July-2013 485 FLYING HOVER BIKE, A SMALL AERIAL VEHICLE FOR COMMERCIAL OR. SURVEYING PURPOSES BY B.MADHAN KUMAR Department

More information

First Civilian Tiltrotor Takes Flight

First Civilian Tiltrotor Takes Flight The MathWorks Aerospace & Defense Conference Reston, Virginia June 14-15, 15, 2006 First Civilian Tiltrotor Takes Flight 200608-1 David King Bell Helicopter BA609 Analytical Integration Leader RESTRICTED

More information

The Bird Ingestion Hazard to Commercial Aircraft Engines and How It Is Addressed

The Bird Ingestion Hazard to Commercial Aircraft Engines and How It Is Addressed University of Nebraska - Lincoln DigitalCommons@University of Nebraska - Lincoln 2011 Bird Strike North America Conference, Niagara Falls Bird Strike Committee Proceedings 9-2011 The Bird Ingestion Hazard

More information

Design and Development of Hover bike

Design and Development of Hover bike Available online at www.ijiere.com International Journal of Innovative and Emerging Research in Engineering e-issn: 2394-3343 p-issn: 2394-5494 Design and Development of Hover bike Umesh Carpenter (Asst.

More information

w w w. o n e r a. f r

w w w. o n e r a. f r www. onera. fr Pioneering concepts for Personal Air Transport Systems PPlane Project AMPERE Project Hybrid electrical propulsion study PPlane : a pioneering concept for Personal Air Transport Systems The

More information

UNMATCHED PERFORMANCE. This document does not contain data subject to the US ITAR, US EAR.

UNMATCHED PERFORMANCE. This document does not contain data subject to the US ITAR, US EAR. UNMATCHED PERFORMANCE PURPOSE-BUILT DESIGN MORE PERFORMANCE 6,000 LB EXTERNAL LOAD CAPACITY MAX HOT & HIGH CAPABILITY UNMATCHED DEPENDABILITY UNLIMITED AIRFRAME STRUCTURE LIFE RELIABLE POWER T5317A-1 TURBINE

More information

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE The Critical Engine The critical engine is the engine whose failure would most adversely affect the airplane s performance or handling

More information