Denali Brochure
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Serialization List Year Produced MODEL 18 D18S A-1 Thru A-37 1945 37
Commercial Genealogy Travel Air 1926 Beech Aircraft 1932 Beechcraft (A Raytheon Company) 1980 Raytheon Corporate Jets 1993 Raytheon Aircraft 1994 Hawker Beechcraft 2007 Beechcraft 2013 Textron Aviation 2014 Serialization 1945 thru 2020 21 May 2021 HAWKER 4000 BRITISH AEROSPACE AIRCRAFT HAWKER 1000 HAWKER 900XP HAWKER SIDDELEY 125-400 BEECHCRAFT HAWKER 125-400 U125A HAWKER 800 • HAWKER SIDDELEY 125 HAWKER 800XP HAWKER 800XPi HAWKER 850 HAWKER 800XPR SERIES 1 HAWKER 125-700 HAWKER 750 HAWKER 125-600 MODEL 400 BEECHJET • HAWKER SIDDELEY 125 400A BEECHJET 400A HAWKER 400XP HAWKER 400XPR SERIES 3 S18A T1A XA-38 GRIZZLY MODEL 2000 STARSHIP PREMIER I PREMIER IA S18 AT-10 KING AIR 350ER F2 KING AIR 350 • • • UC-45 U-21J SUPER KING AIR 300 KING AIR 350i KING AIR 350i D18S C45H SUPER E18 • • KING AIR B200 MODEL 18 SUPER H18 • • TWIN BEECH SUPER KING AIR 200 KING AIR B200GT KING AIR 250 KING AIR 250 C-12 AIR FORCE C-12 NAVY JRB-1 C-12 ARMY 1300 AIRLINER • • • • RC-12K C-12K JRB-2 • JRB-6 C-12 AIR FORCE U21F AT-11 • C-12 NAVY/MARINES KING AIR 100 • • • AT-7 KING AIR A100 B100 C-12 ARMY VC-6A B90 KING AIR B100 Legendary Innovation— • • • C90 SNB-1 MODEL 90 KING AIR T-44A E90 F90 KING AIR C90A Yesterday, Today and Tomorrow. SNB-2 • SNB-5P • • KING AIR C90B KING AIR C90GT KING AIR C90GTx KING AIR C90GTx U-21 RU-21 KING AIR F90-1 With a rich history dating back more than 80 years, Beechcraft Corporation continues to design, build NU-8F MODEL 99 AIRLINER B99 • and support a versatile and globally renowned fl eet of aircraft. -
Download the Pbs Auxiliary Power Units Brochure
AUXILIARY POWER UNITS The PBS brand is built on 200 years of history and a global reputation for high quality engineering and production www.pbsaerospace.com AUXILIARY POWER UNITS by PBS PBS AEROSPACE Inc. with headquarters in Atlanta, GA, is the world’s leading manufacturer of small gas turbine propulsion and power products for UAV’s, target drones, small missiles and guided munitions. The demonstrated high quality and reliability of PBS gas turbine engines and power systems are refl ected in the fact that they have been installed and are being operated in several thousand air vehicle systems worldwide. The key sector for PBS Velka Bites is aerospace engineering: in-house development, production, testing, and certifi cation of small turbojet, turboprop and turboshaft engines, Auxiliary Power Units (APU), and Environmental Control Systems (ECS) proven in thousands of airplanes, helicopters, and UAVs all over the world. The PBS manufacturing program also includes precision casting, precision machining, surface treatment and cryogenics. Saphir 5 Safir 5K/G MI Saphir 5F Safir 5K/G MIS Safir 5L Safir 5K/G Z8 PBS APU Basic Parameters Basic parameters APU MODEL Electrical power Max. operating Bleed air fl ow Weight output altitude Units kVA, kW lb/min lb ft 70.4 26,200 S a fi r 5 L 0 kVA 73 → Up to 60 kVA of electric power Safír 5K/G Z8 40 kVa N/A 113.5 19,700 output Safi r 5K/G MI 20 kVa 62.4 141 19,700 Up to 70.4 lb/min of bleed air flow Safi r 5K/G MIS 6 kW 62.4 128 19,700 → Main features of PBS Safi r 5 product line → Simultaneous supply of electric -
Citation X+ There Is Nothing Faster
CITATION X+ THERE IS NOTHING FASTER Period. Fly the uncontested speed leader up to Mach 0.935 (717 mph) to a max altitude of 51,000 feet, way ahead of your competition. Combining cross-continental range, a technologically advanced flight deck and cabin, and legendary performance makes the Citation X®+ unmatched in more than just speed. Max Range Max Cruise Speed Max Passengers 3,460 nm 528 ktas 12 Useful Load Takeoff Distance 14,769 lb 5,250 ft HIGH-PERFORMANCE BOARDROOM Relax in the wide, reclining seats with plenty of legroom, and enjoy the view through 13 large windows. Exceptional leathers and fabrics, hand-finished hardwoods, and a contemporary vanity and lavatory complete the fit and finish of the Citation X+ cabin. STAY CONNECTED IN FLIGHT Manage cabin lighting, window shades, temperature and entertainment with simple touch-screen commands, and stay connected with in-cabin high-speed Internet and Wi-Fi. AN INTERIOR DESIGNED FOR YOUR NEEDS Thirteen large windows Standard belted Executive tables Additional storage Class-leading Fully tracking, Large galley with flushing lavatory stow neatly between seats legroom berthable room for food swing-out seats preparation CUSTOMIZED COMFORT Choose customized interior finishes and personalized touches throughout to make the Citation X+ your own. Multiple cabin compartments and additional storage space are just a few of the available options. Standard Seating Optional Seating LEADING-EDGE AVIONICS The Garmin™ G5000™ avionics suite allows pilots to individualize their layouts, providing such features as full-dimensional renderings of terrain and precise weather pattern and traffic monitoring, all from a touch-screen, intuitive interface. -
Propeller Operation and Malfunctions Basic Familiarization for Flight Crews
PROPELLER OPERATION AND MALFUNCTIONS BASIC FAMILIARIZATION FOR FLIGHT CREWS INTRODUCTION The following is basic material to help pilots understand how the propellers on turbine engines work, and how they sometimes fail. Some of these failures and malfunctions cannot be duplicated well in the simulator, which can cause recognition difficulties when they happen in actual operation. This text is not meant to replace other instructional texts. However, completion of the material can provide pilots with additional understanding of turbopropeller operation and the handling of malfunctions. GENERAL PROPELLER PRINCIPLES Propeller and engine system designs vary widely. They range from wood propellers on reciprocating engines to fully reversing and feathering constant- speed propellers on turbine engines. Each of these propulsion systems has the similar basic function of producing thrust to propel the airplane, but with different control and operational requirements. Since the full range of combinations is too broad to cover fully in this summary, it will focus on a typical system for transport category airplanes - the constant speed, feathering and reversing propellers on turbine engines. Major propeller components The propeller consists of several blades held in place by a central hub. The propeller hub holds the blades in place and is connected to the engine through a propeller drive shaft and a gearbox. There is also a control system for the propeller, which will be discussed later. Modern propellers on large turboprop airplanes typically have 4 to 6 blades. Other components typically include: The spinner, which creates aerodynamic streamlining over the propeller hub. The bulkhead, which allows the spinner to be attached to the rest of the propeller. -
Comparison of Helicopter Turboshaft Engines
Comparison of Helicopter Turboshaft Engines John Schenderlein1, and Tyler Clayton2 University of Colorado, Boulder, CO, 80304 Although they garnish less attention than their flashy jet cousins, turboshaft engines hold a specialized niche in the aviation industry. Built to be compact, efficient, and powerful, turboshafts have made modern helicopters and the feats they accomplish possible. First implemented in the 1950s, turboshaft geometry has gone largely unchanged, but advances in materials and axial flow technology have continued to drive higher power and efficiency from today's turboshafts. Similarly to the turbojet and fan industry, there are only a handful of big players in the market. The usual suspects - Pratt & Whitney, General Electric, and Rolls-Royce - have taken over most of the industry, but lesser known companies like Lycoming and Turbomeca still hold a footing in the Turboshaft world. Nomenclature shp = Shaft Horsepower SFC = Specific Fuel Consumption FPT = Free Power Turbine HPT = High Power Turbine Introduction & Background Turboshaft engines are very similar to a turboprop engine; in fact many turboshaft engines were created by modifying existing turboprop engines to fit the needs of the rotorcraft they propel. The most common use of turboshaft engines is in scenarios where high power and reliability are required within a small envelope of requirements for size and weight. Most helicopter, marine, and auxiliary power units applications take advantage of turboshaft configurations. In fact, the turboshaft plays a workhorse role in the aviation industry as much as it is does for industrial power generation. While conventional turbine jet propulsion is achieved through thrust generated by a hot and fast exhaust stream, turboshaft engines creates shaft power that drives one or more rotors on the vehicle. -
Aerospace, Defense, and Government Services Mergers & Acquisitions
Aerospace, Defense, and Government Services Mergers & Acquisitions (January 1993 - April 2020) Huntington BAE Spirit Booz Allen L3Harris Precision Rolls- Airbus Boeing CACI Perspecta General Dynamics GE Honeywell Leidos SAIC Leonardo Technologies Lockheed Martin Ingalls Northrop Grumman Castparts Safran Textron Thales Raytheon Technologies Systems Aerosystems Hamilton Industries Royce Airborne tactical DHPC Technologies L3Harris airport Kopter Group PFW Aerospace to Aviolinx Raytheon Unisys Federal Airport security Hydroid radio business to Hutchinson airborne tactical security businesses Vector Launch Otis & Carrier businesses BAE Systems Dynetics businesses to Leidos Controls & Data Premiair Aviation radios business Fiber Materials Maintenance to Shareholders Linndustries Services to Valsef United Raytheon MTM Robotics Next Century Leidos Health to Distributed Energy GERAC test lab and Technologies Inventory Locator Service to Shielding Specialities Jet Aviation Vienna PK AirFinance to ettain group Night Vision business Solutions business to TRC Base2 Solutions engineering to Sopemea 2 Alestis Aerospace to CAMP Systems International Hamble aerostructure to Elbit Systems Stormscope product eAircraft to Belcan 2 GDI Simulation to MBDA Deep3 Software Apollo and Athene Collins Psibernetix ElectroMechanical Aciturri Aeronautica business to Aernnova IMX Medical line to TransDigm J&L Fiber Services to 0 Knight Point Aerospace TruTrak Flight Systems ElectroMechanical Systems to Safran 0 Pristmatic Solutions Next Generation 911 to Management -
BONANZA G36 Specification and Description
BONANZA G36 Specifi cation and Description E-4063 THRU E-4080 Contents THIS DOCUMENT IS PUBLISHED FOR THE PURPOSE 1. GENERAL DESCRIPTION ....................................2 OF PROVIDING GENERAL INFORMATION FOR THE 2. GENERAL ARRANGEMENT .................................3 EVALUATION OF THE DESIGN, PERFORMANCE AND EQUIPMENT OF THE BONANZA G36. IT IS NOT A 3. DESIGN WEIGHTS AND CAPACITIES ................4 CONTRACTUAL AGREEMENT UNLESS APPENDED 4. PERFORMANCE ..................................................4 TO AN AIRCRAFT PURCHASE AGREEMENT. 5. STRUCTURAL DESIGN CRITERIA ......................4 6. FUSELAGE ...........................................................4 7. WING .....................................................................5 8. EMPENNAGE .......................................................5 9. LANDING GEAR ...................................................5 10. POWERPLANT .....................................................5 11. PROPELLER .........................................................6 12. SYSTEMS .............................................................6 13. FLIGHT COMPARTMENT AND AVIONICS ...........7 14. INTERIOR ...........................................................12 15. EXTERIOR ..........................................................12 16. ADDITIONAL EQUIPMENT .................................12 17. EMERGENCY EQUIPMENT ...............................12 18. DOCUMENTATION & TECH PUBLICATIONS ....13 19. MAINTENANCE TRACKING PROGRAM ...........13 20. NEW AIRCRAFT LIMITED WARRANTY .............13 -
Beech 18 There Have Been Other Beechcraft Twins, but Only One "Twin Beech."
NSREWTADSGYI• S )E ~:ii (y~ Beech 18 There have been other Beechcraft twins, but only one "Twin Beech." BY PETER M. BOWERS Honors for the most versatile, noncombat twin-engine airplane ever built certainly must go to the Beechcraft Model 18. It first ....,,:"!'/. - - flew on January 15, 1937, and the last one was delivered on November 26,1969. In the years between, it underwent various air• frame and powerplant modifications and served in a variety of civil and military roles. Its continuous production life of more than 32 years, during which 9,226 were built (or extensively rebuilt), set a record that has been exceeded only by the Taylor/ Piper "Cub" line of 1931 through 1982. The Model 18 was never given a catchy Beech saw a need for an executive aircraft between the big singles and the twin-engine popular name, like the later "Bonanza"; it air/hlers and designed the Mode/18. The 18A (top) was converted to an 18B and is simply was referred to by its civil users as "The Twin Beech" and, by the military, by still in existence. The 18D (bottom) was one of three Mode/18 variants produced under ATC-684. its various service designations. When other utive aviation a relatively large and roomy weeks after its first flight, the Beech 18 re• twin-engine Beech designs were introduced eight-seater with the twin-engine capability ceived Approved Type Certificate (ATC) A• in the 1950s, the civil references had to get and reliability of an airliner. Most corporate 630. Selling price was $37,500, which was a bit more specific. -
Model 162 SERIAL NUMBER
Model 162 SERIAL NUMBER Serials 16200001 and On REGISTRATION NUMBER This publication includes the material required to be furnished to the pilot by ASTM F2245. COPYRIGHT © 2009 ORIGINAL ISSUE - 22 JULY 2009 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA REVISION 3 - 28 SEPTEMBER 2010 162PHUS-03 U.S. CESSNA INTRODUCTION MODEL 162 GARMIN G300 PILOT’S OPERATING HANDBOOK AND FLIGHT TRAINING SUPPLEMENT CESSNA MODEL 162 SERIALS 16200001 AND ON ORIGINAL ISSUE - 22 JULY 2009 REVISION 3 - 28 SEPTEMBER 2010 PART NUMBER: 162PHUS-03 162PHUS-03 U.S. i/ii CESSNA INTRODUCTION MODEL 162 GARMIN G300 CONGRATULATIONS Congratulations on your purchase and welcome to Cessna ownership! Your Cessna has been designed and constructed to give you the most in performance, value and comfort. This Pilot’s Operating Handbook has been prepared as a guide to help you get the most utility from your airplane. It contains information about your airplane’s equipment, operating procedures, performance and suggested service and care. Please study it carefully and use it as a reference. The worldwide Cessna Organization and Cessna Customer Service are prepared to serve you. The following services are offered by each Cessna Service Station: • THE CESSNA AIRPLANE WARRANTIES, which provide coverage for parts and labor, are upheld through Cessna Service Stations worldwide. Warranty provisions and other important information are contained in the Customer Care Handbook supplied with your airplane. The Customer Care Card assigned to you at delivery will establish your eligibility under warranty and should be presented to your local Cessna Service Station at the time of warranty service. • FACTORY TRAINED PERSONNEL to provide you with courteous, expert service. -
Helicopter Turboshafts
Helicopter Turboshafts Luke Stuyvenberg University of Colorado at Boulder Department of Aerospace Engineering The application of gas turbine engines in helicopters is discussed. The work- ings of turboshafts and the history of their use in helicopters is briefly described. Ideal cycle analyses of the Boeing 502-14 and of the General Electric T64 turboshaft engine are performed. I. Introduction to Turboshafts Turboshafts are an adaptation of gas turbine technology in which the principle output is shaft power from the expansion of hot gas through the turbine, rather than thrust from the exhaust of these gases. They have found a wide variety of applications ranging from air compression to auxiliary power generation to racing boat propulsion and more. This paper, however, will focus primarily on the application of turboshaft technology to providing main power for helicopters, to achieve extended vertical flight. II. Relationship to Turbojets As a variation of the gas turbine, turboshafts are very similar to turbojets. The operating principle is identical: atmospheric gases are ingested at the inlet, compressed, mixed with fuel and combusted, then expanded through a turbine which powers the compressor. There are two key diferences which separate turboshafts from turbojets, however. Figure 1. Basic Turboshaft Operation Note the absence of a mechanical connection between the HPT and LPT. An ideal turboshaft extracts with the HPT only the power necessary to turn the compressor, and with the LPT all remaining power from the expansion process. 1 of 10 American Institute of Aeronautics and Astronautics A. Emphasis on Shaft Power Unlike turbojets, the primary purpose of which is to produce thrust from the expanded gases, turboshafts are intended to extract shaft horsepower (shp). -
Citation Sovereign+ Redraw Your Range Map
CITATION SOVEREIGN+ REDRAW YOUR RANGE MAP Range-enhancing winglets combined with powerful engines allow the CESSNA CITATION SOVEREIGN+ aircraft to land on smaller runways and at airports surrounded by obstacles. This reduces travel time and grants access to popular destinations such as Aspen, Hilton Head and Ocean Reef. The sizable cabin makes every business trip a pleasure. Maximum Range Maximum Cruise Speed Maximum Passengers Useful Payload Takeoff Distance 3,200 nm 460 ktas 12 12,794 lb 3,530 ft UNMATCHED INGENUITY CITATION SOVEREIGN+ SPECIFICATIONS INTERIOR Cabin Height 68 in 1.73 m Cabin Width 66 in 1 .68 m Cabin Length 25 ft 3 in 7.70 m TOUCH-SCREEN SPACIOUS CABIN HEATED BAGGAGE AVIONICS The spacious, versatile cabin features COMPARTMENT BAGGAGE CAPACITY electrically operated windows and a Weight 1,435 lb 651 kg NextGen-capable GARMIN double-club seating configuration. The heated baggage compartment can G5000 avionics streamline the hold up to 1,000 pounds and 100 cubic Volume 135 cu ft 3.82 cu m pilot experience with advanced feet of cargo. autothrottles and touch-screen WEIGHTS simplicity. Max Takeoff 30,775 lb 1 3,959 kg Basic Operating Weight 1 8,235 lb 8,27 1 kg Useful Load 12,790 lb 5,801 kg MAX PASSENGERS 12 ENGINES Manufacturer Pratt & Whitney Canada Model (2) PW306D Thrust 5,907 lb 26.28 kN ea PERFORMANCE Takeoff Field Length (MTOW) 3,530 ft 1,076 m Max Range 3,200 nm 5,926 km Max Cruise Speed 460 ktas 852 km/h FUEL-EFFICIENT ENGINES Time to Climb FL 450 in 27 min POWERFUL CLASS-LEADING Pratt & Whitney Canada engines deliver low-cost ELECTRICAL SYSTEM TAKEOFF FIELD LENGTH maintenance, high reliability and fuel efficiency for Performance data is based on standard conditions with zero wind. -
PILOT REPORT Grand Caravan EX Cessna’S Big Utility Turboprop Single Is a Capable and All-Around Solid Performer
PILOT REPORT Grand Caravan EX Cessna’s big utility turboprop single is a capable and all-around solid performer. by Matt Thurber The Cessna Caravan has been in production since of the big single-engine turboprop. 1984, and earlier this year I had my first opportu- While it’s common to be told the Caravan “flies nity to fly the single-engine utility turboprop from just like a heavy 172,” the airplane is not simply Textron Aviation’s private airport—Beech Factory a stretched and beefed-up version of any Cessna Airport—in Wichita. single. The configuration may be similar—there www.ainonline.com My demo pilot was Terry Allenbaugh, the per- aren’t many options when it comes to designing fect pilot to show me the Caravan’s capabili- a tricycle-gear single-engine turboprop for rough- ties. During his early flying career, Allenbaugh field operations—but the Caravan employs many flew one of the first Caravans, Serial Number features found on larger airplanes. 8, for Mission Aviation Fellowship in Ethio- The strut-braced wing has massive flaps that pia. Although he has flown all the Citations extend to 70 percent of each wing’s length. Spoil- and King Airs, Allenbaugh returned to flying ers mounted inboard of the ailerons improve the Caravan as a sales demonstration pilot two low-speed handling. Elevator trim tabs have dual years ago, and he is an enthusiastic proponent actuators. A pressure fuel system is optional and © 2017 AIN Publications. All Rights Reserved. For Reprints go to AVIATION INTERNATIONAL NEWS • OCTOBER 2017 PILOT REPORT typically installed on float-equipped Caravans.