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How to find private jet charter empty legs with mlkjets1 - Starting an Aircraft Washing Business and Aircraft Charter

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So you love airplanes and you want to start an aircraft washing service? I cannot blame you, as I did the same thing. After cleaning Thousands of aircraft over the years, I have paid for my flight school, first aircraft and then started an aircraft washing franchise as a module of another franchising company I had founded. Named the Aircraft Wash Guys we learned early on what it takes to satisfy aircraft owners, FBOs Fixed Based Operators and Chief Pilots. We always specialized in washing and polishing aircraft. We’ve cleaned thousands of private planes, corporate jets, flying clubs, flight schools and helicopters. My Car Wash Guys company was originally founded over twenty years ago and started as an aircraft washing service.

As you know, aviation people are serious about flying and a clean plane makes flying more fun and enjoyable. Corporate Aviators need you to maintain their positive image. When in the aircraft washing business you will not only wash exteriors of planes, you must also have carpet-cleaning capabilities. Many of our crewmembers are also private pilots and it pays to have pilots as part of your employee team. To learn more about aircraft washing, I have put some additional ideas online to assist you.

http://www.Aircraftwashguys.com/aircraftbbs

We have always kept our prices low and gone for volume, you may wish to do this or charge the going rate. Our rates are at the lower end of the spectrum and this will give you a good starting point on pricing.

Single Engines $20.00-45.00 wash, waxing $60.00-140.00, weekly wash $20.00;

Twin Engines $45.00-90.00 wash, waxing $90.00-240.00, weekly wash $40.00; Corporate Jets $90.00-140.00 wash, waxing $180.00-400.00, weekly wash $80.00;

Helicopters $30.00-100.00 wash, waxing $45.00-180.00, weekly wash $30.00. Carpet Shampooing, Bright Work and Aluminum Polishing, etc. generally we will give the customers free estimates.

You will need to perform these services the customer’s schedule and usually accommodate, immediate services, day or night, evenings and weekends. Customizing your services with the customer’s requirements must become your specialty. You will also need the following things:

Two Million in Liability Insurance

Quiet Machines and Professional Crews in Uniform

Monthly Invoice by “N”-Number

Water Reclamation Device Onboard, EPA Compliant

Truck or Trailer Mounted Unit, Fully Self Contained, Painted Safety Yellow

Owning an Aircraft Washing Service small business can be quite rewarding and although hard work, it can be an extension of your flying hobby. Just think getting paid to wash some of the latest and greatest aircraft and hanging out at the airport all day? And yes, they will even pay you very well for doing just that. Think on this.

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Source by Lance Winslow

Categories : DESTINATIONS, EMBRAER, FALCON, GULFSTREAM, HAWKER, JET NEWS, LARGE SIZE BODY JETS, LIGHT SIZE BODY JETS, MEDIUM SIZE BODY JETS, PRIVATE JET AFRICA, PRIVATE JET ASIA, PRIVATE JET AUSTRALIA, PRIVATE JET AVIONICS, PRIVATE JET BUILDER, PRIVATE JET CHARTER, PRIVATE JET CHATER, PRIVATE JET EUROPE, PRIVATE JET MAINTENANCE, PRIVATE JET MIDDLE EAST, PRIVATE JET SOUTH AMERICA, PRIVATE JET TIPS, PRIVATE JET USA, PRIVATE JETS DEALS, TRANSATLANTIC, TRANSPACIFIC
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Corporate travel and jet travel solutio for jet corporate charter2 - Types of Boats and jet charter For Sale Vary

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Along with any announcement of ‘boats for sale’ would come not only a significant number of choices but also a wide range of types of each choice. Before deciding on size, shape, or color, the question is, what kind of boat is desired?

One website listed 63 types of floatables from which to choose, not including rafts and canoes. The various types of each would make a new buyer’s head spin. The best way to choose one is to understand what exactly one wants to do with their prospective new purchase. To begin with, one should know that there are generally three categories of watercraft: cruising crafts, fishing boats, and those used for sports.

Cruisers

Cruising ships are for spending leisure time on the water. Depending on size and cost, these can allow for day cruises or have cabins and amenities for staying overnight.

Cabin cruisers have a galley or kitchen, bathroom, and sleep area. The motor configuration can be inboard, fitted inside the vessel, or outboard, mounted on the outside at the stern or rear of the craft. The larger variety takes experienced skill to control and can better withstand choppy water.

A bowrider is a vehicle with seating up front to enjoy the breeze. It can be 35 feet long and can also tow skiers. A pontoon is a multi-hull ship relying on large tubes for buoyancy. This popular variety is built for leisure and comfort, offering wide decks and sofa-like seating. A trawler can be for pleasure or commercial fishing, and quickly resells as one of the most popular boats for sale.

Fishers

Fishing vessels usually have control panels in the back to allow easier fishing in the front or bow of the floating vehicle. Smaller ones may be cramped and offer limited seating; larger models could have cabins. While fishing can be done from any watercraft, some are specifically designed to allow easy fishing. A bassing vessel is usually short and flat, meant to traverse shallow waterways and allow easy angling for bass. Walkabout and center console vehicles tend to be larger fishers to allow space for more people while handling rough ocean currents. Often these offer rod holders and stowaway seating for large parties.

Sport Types

These vessels are made to accommodate skiing, wakeboarding, and even competitive sailing. Both skiing and wakeboarding types have towing capabilities and enhanced power for a faster ride. Jet skis are small, powerful vehicles with handlebar controls meant for one or two people. Jet and speed boats are built for speed on the water. Sailboats can be for either cruising or competing, and can rely wholly or partially on wind power. Like all watercraft, these vessels come in a vast range of choices regarding size, length, and amenities.

For a buyer considering boats for sale, the possibilities are near endless.

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Source by Andrea Avery

Categories : DESTINATIONS, EMBRAER, FALCON, GULFSTREAM, HAWKER, JET NEWS, LARGE SIZE BODY JETS, LIGHT SIZE BODY JETS, MEDIUM SIZE BODY JETS, PRIVATE JET AFRICA, PRIVATE JET ASIA, PRIVATE JET AUSTRALIA, PRIVATE JET AVIONICS, PRIVATE JET BUILDER, PRIVATE JET CHARTER, PRIVATE JET CHATER, PRIVATE JET EUROPE, PRIVATE JET MAINTENANCE, PRIVATE JET MIDDLE EAST, PRIVATE JET SOUTH AMERICA, PRIVATE JET TIPS, PRIVATE JET USA, PRIVATE JETS DEALS, TRANSATLANTIC, TRANSPACIFIC
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How to find the best private jet charter empty legs3 - Best Explanation of PW 100 Engine & Its Parts as private jets parts

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PW 100 series of engines are the forefront in modern, state of the art regional and commuter turboprop engines. With its three spool design, easy to maintain modular construction, and high power rating, the engine is a logical choice for medium to large turboprops including the Bombardier Q400, DeHavilland Dash 8 and Embraer EMB 120. Some consider the PW 100 to be the replacement to the venerable PT6, but in reality the PW 100 picks up where the PT6 Large version left off in terms of power, fuel economy, and reliability. The PW 100 series consists of a number of variations. There is no actual PW 100 engine; the engines start with the PW118 engine and end at the PW127J.

The engines are essentially the same, with, for the most part, a steady increase in power output, as well as slight variations in engine output speed and in the proportion of mechanical shaft horsepower vs. thrust produced. In other words, each turboprop is rated in equivalent shaft horsepower, (eshp) which is a combination of the actual mechanical horsepower provided at the output shaft combined with the amount of horsepower available as a conversion of the thrust that is produced at the tailpipe. The proportion varies, but is typically in the range of 80% power produced by the propeller, 20% produced by the tailpipe.

The Powerful Model PW 100 Engine is completely modular in its construction; that is, it is made up of a number of interchangeable modules that can easily be removed and replaced in the event that there is a problem with the engine. The modules consist of the turbo-machine, the power turbine assembly, the inlet housing, and the output reduction gearbox. The compact turbo-machine consists of the twin spool gas generator and the accessory gearbox. The power turbine connects to the rear of the turbo-machine and features a two stage power turbine which drives a shaft that runs forward up the center of the turbo-machine shafts. The inlet housing mounts to the front of the turbo-machine and provides the space for air to be drawn into the compressor and the support for the output reduction gearbox. The output reduction gearbox mounts to the front of the inlet housing and takes the high speed input from the power turbine shaft and converts it to a high torque, low rpm output taken off the propeller flange at the front of the gearbox.

Atmospheric air is drawn in through the engine nacelle behind the propeller into a passive particle separator, which is part of the nacelle. Clean intake air is drawn upward into the downward facing scroll type engine inlet. Air is drawn into the turbo-machine by the single stage, centrifugal compressor. The air is accelerated outward by the compressor and fed into numerous curved diffuser ducts which smoothly deposit the airflow to the face of the single stage, centrigugal, high pressure compressor. The high pressure compressor raises the pressure to a design pressure ratio of nearly 15:1 on some of the later models. The high pressure compressor feeds the airflow to a diffuser which converts the dynamic pressure into static pressure, as it enters the annular, reverse flow combustor. The compressed air enters the inner combustion liner where it is mixed with jet fuel and ignited. The resultant gas is expanded through the high pressure nozzle to impinge upon the single stage axial high pressure turbine, which drives the high pressure compressor and the accessory gearbox. The gas is then further expanded through the low pressure nozzle to drive the low pressure turbine, which drives the low pressure compressor. Finally, the gas is expanded through the two stage power turbine to drive a concentric shaft up to the front of the engine, which drives the output reduction gearbox. The exhaust is then directed out of the short, axial flow, fixed area exhaust outlet to provide close to 2,000 lbs. of thrust on some Popular Models of PW-100 Engine. The output reduction gearbox reduces power turbine speed down to a usable 1,200 or 1,300 rpm, to drive a four bladed, constant speed propeller. Accessories include a generator, oil pumps, fuel pumps, hydraulic pumps, and a FADEC fuel control.

The twin spool compressor offers many advantages over a similar single spool compressor. By allowing the two compressors to run at different speeds, the compressors can be optimized a wide range of airflows. This allows for a higher design pressure ratio, much better part power efficiency, and very rapid engine response. High pressure ratios and high turbine inlet temperatures allow for very low specific fuel consumption, and advanced cooling techniques and state of the art materials allow for long time between overhaul periods.

There are a couple of other variants of the PW 100 that are worth mentioning. The PW150 engine is a high power development of the PW 100; it is very similar in overall design and dimensions to the PW 100, except that the low pressure compressor is a single stage axial followed by a single stage centrifugal. Pressure ratio is a higher 18:1, and the engine produces power in the 5000 es-hp class, which makes it a suitable replacement for the Allison T56 or an alternative to the Rolls Royce AE1107C. There are also turbo-shaft versions of the PW 100, where the output reduction gearbox and inlet are removed and replaced with a screened bell-mouth inlet and a carrier bearing. The engine output is at power turbine speed. The engine could be an alternative to the CT7 (T700) turbo-shaft in medium helicopters, although so far it hasn’t been used in this application. There is a marine variant of this turbo-shaft available for modern military surface effect ships, however. These models are referred to as the ST18M. Power output is approximately 3,200 shaft horsepower.

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Source by Jhon Miller

Categories : DESTINATIONS, EMBRAER, FALCON, GULFSTREAM, HAWKER, JET NEWS, LARGE SIZE BODY JETS, LIGHT SIZE BODY JETS, MEDIUM SIZE BODY JETS, PRIVATE JET AFRICA, PRIVATE JET ASIA, PRIVATE JET AUSTRALIA, PRIVATE JET AVIONICS, PRIVATE JET BUILDER, PRIVATE JET CHARTER, PRIVATE JET CHATER, PRIVATE JET EUROPE, PRIVATE JET MAINTENANCE, PRIVATE JET MIDDLE EAST, PRIVATE JET SOUTH AMERICA, PRIVATE JET TIPS, PRIVATE JET USA, PRIVATE JETS DEALS, TRANSATLANTIC, TRANSPACIFIC
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Airline cargo charter for air charter solutions2 - The Downfall of Pratt & Whitney and the Rise of Ge: Indigo's Troublesome A320

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Indigo Airlines, the biggest low-cost carrier (LCC) of India is headquartered in Gurgaon, New Delhi. The airlines are now planning to replace its fleet of Airbus A320-neo aircraft with engines provided by GE after experiencing technical issues with the engines of Pratt & Whitney.

Currently, the low-cost carrier has ambitious plans to expand operations in the regional aviation market, as well as low-cost long haul international flights. Indigo Airlines, which currently holds the largest market share in the domestic aviation sector, has placed orders for a total of 430 NEO (new engine option) aircraft to meet the targeted expectations. The new aircraft shall help in covering longer flight distances, as well as help in economic savings on fuel costs, by a margin of 15%. The total passenger capacity is 189.

The low-cost carrier, Indigo (operating under the umbrella of Interglobe Aviation) is one of the largest customers of Airbus. Indigo is also the first airline in India and Asia to operate the Airbus A320-neo aircraft. Presently, the low-cost carrier suffers from the loss of seven narrow-body neo-aircraft. The aircraft has not been able to remain operational, owing to the technical issues faced by Pratt & Whitney’s PW1100 geared turbofan engines. Indigo airlines have a contractual agreement with Pratt & Whitney for providing the airlines with the full replacement, in situations related to engine problems. Slower deliveries from Pratt & Whitney shall further hamper the efforts of Indigo airlines to commence operations of their grounded flights. Currently, Indigo operates a fleet of 137, Airbus A320, including 22, Airbus A320-NEO aircraft, and has further placed orders for a total of 430 – A320-NEO aircraft. Owing to engine failures, the airline has canceled several flights. Furthermore, the problems caused by engine failures have resulted in a severe delay in the delivery of new aircraft, by Airbus, to its customers.

Indigo Airlines has continued to receive the necessary operations and technical support, including the provision of spare engines to help mitigate the operational impact. Pratt & Whitney have further confirmed to take one year to build new engines, according to the design changes.

The aircraft manufacturer company, Airbus has provided two engine options with the Airbus A320-neo aircraft, which include GE engines (GE (CGM) LEAP 1-A) or the Pratt & Whitney engines (Pratt & Whitney Pure Power 1100G). Problems faced by the Pratt & Whitney engines have led to many airline companies to modify their purchase orders. Many of the early airlines adopting the Pratt & Whitney engines, such as Indigo, Go Air, and Lufthansa has let the engines spool up and run for two-three minutes longer, before conducting airline operations.

Furthermore, the PW1100G engines are witnessing a phenomenon known as rotor bowing. This phenomenon occurs when the temperature differences within the engine lead to misalignment of certain parts (shaft, rotor blades) within the engine. The phenomenon of rotor bowing leads to degradation in the efficiency of the engines, engine life, the life of the rotor blades, and the engine compressor. As a result of this phenomenon, Indigo Airlines has issued altitude restrictions of 30,000 for the Airbus A320-neo air crafts. Increasing altitude leads to the shutting down of the engine’s bleed air system (which helps to start the engine and in-cabin pressurization). This, in turn, affects the anti-icing system installed on the aircraft. Making use of GE engines is expected to help the airline carrier to achieve fuel efficiency, reliability, as well as outstanding services in its operations.

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Source by Rohith Sampathi

Categories : DESTINATIONS, EMBRAER, FALCON, GULFSTREAM, HAWKER, JET NEWS, LARGE SIZE BODY JETS, LIGHT SIZE BODY JETS, MEDIUM SIZE BODY JETS, PRIVATE JET AFRICA, PRIVATE JET ASIA, PRIVATE JET AUSTRALIA, PRIVATE JET AVIONICS, PRIVATE JET BUILDER, PRIVATE JET CHARTER, PRIVATE JET CHATER, PRIVATE JET EUROPE, PRIVATE JET MAINTENANCE, PRIVATE JET MIDDLE EAST, PRIVATE JET SOUTH AMERICA, PRIVATE JET TIPS, PRIVATE JET USA, PRIVATE JETS DEALS, TRANSATLANTIC, TRANSPACIFIC
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Private jets charter jet leasing private corporate airliner mlkjets1 - New Car Prices Got You Reeling [Program Review]: New Car Prices Got You Reeling with best private jet services

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Granted, it can be understandably unbelievable to hear of a new car going for only $149, so most people will naturally see a headline offering “Brand New Cars For Just $149” as a misprint or gimmick; But a revolutionary strategy is actually, at this moment, making it possible for people to drive away in brand new cars for as low as $149.

It is everyone’s dream to own a car, and while owning one can be viewed in some circles as a luxury, the need for easy and convenient mobility, particularly in times of emergency, has nonetheless made car ownership for every home, more of a crucial necessity, than mere luxury. However, the relatively high cost of cars makes it essentially impossible for many people to afford brand new cars. It is not an exaggeration to say that the price tag on most new cars in the market today is simply enough to send most folks reeling in despair. Often, the only recourse available to them seems to be the financing option, which saddles patrons with years of onerous obligation.

The Shopfreemart Cash N Cars offer is, however, changing all that, by allowing individuals to own any car of their choice without paying more than $149.

With a one-time $149 entry fee, participants are given a personalized Online Web Page valued at $149.00, plus a $149 Cash and Cars Gift Token redeemable for valuable items, such as discounts on travel, vacations, hotels, and more.

The program allows participants to get paid in 3 different ways as they invite others to become a part of the revolutionary life-changing offer. Members can then use the accrued cash to purchase anything they desire: that new car they’ve been wanting for a while, a boat, a house, or as club owners whimsically quip, even a private jet.

The program is easy and quite straightforward, with a transparent process that ensures every participant is aware of the happenings on his or her account.

In addition to giving members the avenue to own brand-new cars at an unprecedented price of $149, FreeMart also offers some other great natural products designed to improve the quality of life of members, which include two amazing soap products, and a wide range of health products to ensure that car owners can drive and travel happily in their new rides.

To be sure, the Cash N Cars club is not the first ever program to hit the market
hoisting new cars as coveted rewards. But to this writer’s knowledge, it is alone in this bold and innovative strategy to empower members to drive away in brand-new cars without paying more than $149 one-time.

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Source by Benjamin Okeagu

Categories : DESTINATIONS, EMBRAER, FALCON, GULFSTREAM, HAWKER, JET NEWS, LARGE SIZE BODY JETS, LIGHT SIZE BODY JETS, MEDIUM SIZE BODY JETS, PRIVATE JET AFRICA, PRIVATE JET ASIA, PRIVATE JET AUSTRALIA, PRIVATE JET AVIONICS, PRIVATE JET BUILDER, PRIVATE JET CHARTER, PRIVATE JET CHATER, PRIVATE JET EUROPE, PRIVATE JET MAINTENANCE, PRIVATE JET MIDDLE EAST, PRIVATE JET SOUTH AMERICA, PRIVATE JET TIPS, PRIVATE JET USA, PRIVATE JETS DEALS, TRANSATLANTIC, TRANSPACIFIC
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Embraer LEGACY 650E Private Jet Charter EMBRAER LEGACY 650E PRIVATE JET HIRE EMBRAER PRIVATE CHARTER MLKJETS3 2 scaled - Unimpeachable Care Of The Critically One By Vedanta Air Ambulance emergency jet charter

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This Air Ambulance Cost is the loyalty and precedes Air travel provider to give out and execute the patient’s requirements of the moving process. This service makes presented the greatest and practised faculty of under the supervision of MD Doctors and the expert team to give out of the ordinary management during the evacuation process.

We comprehend the desires of this ability in others city also, so this Air Ambulance Service in Patna is always ready to take off your needy ones serve the necessity of the health transfer conveniences with the proper care and special inspection. Our Company preferred easy on the pocket rate air medical service 24 hours in the emergency case and require of the patient shifting facility.

We supply of the crisis medical group departure faculty of the patients relocate with all the ICU emergency equipment like Defibrillator, Cardiac Monitor, Ventilator, Oxygen Therapy – Re-breathing circuit, Suction kit, Spinal collars, Spine board, Inflatable splints, Collapsible wheelchair, Medical kits, Drugs, Blood pressure cuff, Pulse oximeter, Syringe pump, Scoop stretcher and many more basic and advanced life care support with the extraordinary team of the paramedics technician who can handle all these tools in effortlessness and the MD Doctors to accomplish the need of treatment.

In the ventilator cases transport of the needy ones because at the present remedial treatment center doctors couldn’t offer the crucial medical cure to the patients to their injuries, so you want to move your patient to another medical treatment centre in another place but could find the technique to reallocate those needy ones because the patients are with the Intensive Care Unit with Ventilation.

This is one of the top and with around the clock procuring casual health relocate amenities including MBBS doctor, Paramedical technician and a professional medicinal team you need there is not only saving the cost but we supply aggressive prices to the patient and there is no any an extra headache and hidden cost. This Air Ambulance Service in Delhi prefers their most excellent and advances service in Delhi, Bangalore, Kolkata, Guwahati, Chennai, Mumbai, Bhubaneswar and other aerial cities in India.

Air Ambulance from Patna work with capable and practised remedial dispatches by private charter aircraft and commercial jet with medical migration facility from one-bed hospital to another desire city hospital bed. This is one of the handpicked and sophisticated service providers in India which has health care service for transportation bedside to bedside and anywhere in India.

Vedanta Air Ambulance Guwahati are specialized in Air, Train and Ground Ambulance service we are available 24/7 hours and 365 days a year for the wounded and serious patient. The Air Ambulance fare is one of the most times saving and speedy and safe service provider by mass departure system. This Air Ambulance also has a preference for all handpicked and highly developed assessment which is illustrated city. This Company with avail compensation of best and an economic ICU carry Charted Air Ambulance Service from Delhi with complete peer to peer transfer facility from Patna city to Delhi, Mumbai, Kolkata, Chennai, Allahabad, Hyderabad and always available for patients. This Service is well-furnished and most-well-known where provides immediate transportation with the patient from one medical treatment centre to other any destination in India.

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Source by Ranjeet Kumar

Categories : DESTINATIONS, EMBRAER, FALCON, GULFSTREAM, HAWKER, JET NEWS, LARGE SIZE BODY JETS, LIGHT SIZE BODY JETS, MEDIUM SIZE BODY JETS, PRIVATE JET AFRICA, PRIVATE JET ASIA, PRIVATE JET AUSTRALIA, PRIVATE JET AVIONICS, PRIVATE JET BUILDER, PRIVATE JET CHARTER, PRIVATE JET CHATER, PRIVATE JET EUROPE, PRIVATE JET MAINTENANCE, PRIVATE JET MIDDLE EAST, PRIVATE JET SOUTH AMERICA, PRIVATE JET TIPS, PRIVATE JET USA, PRIVATE JETS DEALS, TRANSATLANTIC, TRANSPACIFIC
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How to find private jet charter empty legs with mlkjets1 - 5 Tips for Stress Free Long Haul Flights in best empty leg flights website uk

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The world is becoming smaller by the day. Flying long haul to distant locations for business or pleasure is becoming increasingly more popular. There are more aircraft, more airports to fly to and more people ready to spend half a day or longer in the air. It is quite simply easier and cheaper than it used to be fly long haul. Unfortunately, the experience of traveling to the other side of the world can very often be a stressful and exhausting affair, especially for the uninitiated or unprepared. This doesn’t have to be the case. Just follow this guide to a stress free long haul flight and you can sit back and enjoy the whole experience!

Step 1: Do Your Homework:

A little bit of homework will certainly help you to discover the right airline for you. The Internet is an excellent resource in this regard, but don’t ignore you’re local travel agent who may have a wealth of customer experience with various airlines.

You might want to find out who is going to offer the most leg-room, what the quality of food is like and how reputable their customer service is.
Most airlines now offer some sort of in-seat entertainment such as Singapore airline’s Krisworld system (Always very good) and I particularly enjoyed Japan airline’s onscreen camera views allowing you to see forwards from the nose of the aircraft or down over wherever you are flying. These systems are good way to kill a few hours of any flight.

Of course the price is important and shopping around really pays off. Don’t be afraid to go straight to the airline and check out any special offers they might have as well as using high street and Internet based agents.

Step 2: Airport Time:

You will usually be expected to check in 2 hours in advance of your long haul flight although it always pays to arrive a little earlier than this as most people will arrive in the queue around this time. You are better off spending 3 hours sat in the departure lounge with a good book than standing in the check-in queue!

Of course the earlier you are the better chance you have of reserving a good seat. Many airlines are now introducing services on their websites that allow you to reserve seats, order meals and allow you to check-in via automated express check-in systems; the best way to do it by far.

Step 3: Enjoy the flight:

On a 19 hour flight it is important to keep yourself occupied. The obvious solution is a good book. I always start a book a few days before I fly so that I’m already ‘into it’ before I get on the plane, ensuring a pre-planned slice of escapism.

These days we are blessed with in-seat technologies to keep us entertained, these will often include the latest blockbuster films, video games and all sorts of TV shows and in flight information. I still find, however, that the trusty book is the best way to kill some time.

The holy grail of long haul flight is being able to get some quality sleep. Air quality, light sources, noise and cramped upright seating is certainly not conducive to falling asleep. An Ezysleep inflatable travel pillow, for example is designed to deal with the issue of supporting your neck whilst upright but there are other things you can do. Ear plugs and an eye mask can help deal with light and noise so combine them with your travel pillow for some quality sleep.

If the food isn’t up to scratch, make sure you’re prepared with some healthy snacks and a good supply of water. It might be free but alcohol and coffee are very dehydrating and this is the last thing you want in an already arid environment. Stick to the water and fruit juices.

Most importantly, enjoy the flight! Enjoy that time away from the mobile phones and the boss and the traffic and relax. You’re 40,000 feet away from everything, make the most of it!

Step 4: Stay healthy:

Deep Vein Thrombosis (DVT) is a constant worry for long haul travelers. Although extremely rare, it is a very dangerous condition. The condition is avoided by ensuring that the blood flow around your body is kept moving.

Do the exercises advised by the in-flight video and magazines, take regular walks to the galley, the toilet or just up and down the aisles and drink plenty of water.

Step 5: Avoid Jet Lag:

The best way to avoid, or minimize, jet-lag is to start planning whilst on your flight. Set your watch to your destination time as soon as you can and do your best to sleep when it’s night time where you are going, even if that means missing onboard meals.

Keep drinking that water so you’re not dehydrated when you land. When you get to your destination, don’t hit the hay straight away. Try to stay awake until the evening and you’ll give yourself the best chance to adjust quickly to your new time zone.

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Source by James Wittering

Categories : DESTINATIONS, EMBRAER, FALCON, GULFSTREAM, HAWKER, JET NEWS, LARGE SIZE BODY JETS, LIGHT SIZE BODY JETS, MEDIUM SIZE BODY JETS, PRIVATE JET AFRICA, PRIVATE JET ASIA, PRIVATE JET AUSTRALIA, PRIVATE JET AVIONICS, PRIVATE JET BUILDER, PRIVATE JET CHARTER, PRIVATE JET CHATER, PRIVATE JET EUROPE, PRIVATE JET MAINTENANCE, PRIVATE JET MIDDLE EAST, PRIVATE JET SOUTH AMERICA, PRIVATE JET TIPS, PRIVATE JET USA, PRIVATE JETS DEALS, TRANSATLANTIC, TRANSPACIFIC
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Embraer LINEAGE 1000E Private Jet Charter EMBRAER LINEAGE 1000E PRIVATE JET HIRE EMBRAER PRIVATE CHARTER MLKJETS4 - The McDonnell - Douglas MD-80 the cheap private jet flights uk

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I

Fuselage stretchability, inherently incorporated in the basic DC-9 design, had characterized its program, resulting in four dimensionally divergent, higher-capacity versions, including the initially-elongated DC-9-30 over the baseline series -10/14/15, the subsequent DC-9-40, and the final DC-9-50, the latter accommodating 49 more passengers than the twin-jet’s original maximum.

The DC-9 itself, founded upon the four design tenets of ruggedness, simplicity, reliability, and low-cost, had been McDonnell-Douglas’s best-selling commercial aircraft-so much so, in fact, that it took off or landed somewhere in the world every seven seconds, serving more than 570 cities with some 6,050 daily flights, and by 1979, the collective fleet had carried more than one billion passengers and logged more than 18 million hours with an almost 99-percent dispatch reliability rate.

Its Pratt and Whitney JT8D engine, the most widely used powerplant and numbering in excess of 12,000 units, had not only provided propulsive thrust for all versions of the DC-9, but had also powered the Boeing 727, the Sud-Aviation SE.210 Super Caravelle, the Boeing 737, and the Dassault-Breguet Mercure 100.

Both the DC-9’s basic design and its JT8D turbofan therefore offered the most optimum, cost-effective platform on which to base a larger-capacity successor, which needed to equal the DC-9-30’s range capability, yet exceed the DC-9-50’s economics.

Its fuselage, not having reached its limit of stretchability, lent itself to still higher-capacity accommodation, but its obstacle had been a powerplant of sufficient thrust to maintain acceptable payload, range, and performance parameters for its operators.

Based upon the earlier, two-stage JT3D, which had powered both the 707 and the DC-8, the JT8D, a low, one-to-one bypass ratio turbofan, had first run on April 7, 1961, taking to the skies for the first time on May 1 of the following year mounted to a 707. Receiving FAA certification on February 9, 1963, as the 14,000 thrust-pound JT8D-1, it had powered the 727-100 before being employed by the DC-9-10 and was subsequently offered in several successively higher-thrust versions, the last of which had been the 17,400 thrust-pound JT8D-17R.

A new-generation variant, providing application for an ultimate DC-9 stretch and designated JT8D-109, had been one of six demonstration powerplants incorporating larger, single-stage fans developed for NASA’s Quiet Engine Program, which had run between 1972 and 1975, and two of its versions had logged more than 50 hours retrofitted to a modified DC-9-32. Design of a further development, the 18,500 thrust-pound JT8D-209, began in 1974 and first ran two years later, test flown on a McDonnell-Douglas Advanced Medium STOL Transport (AMST) in March of 1977.

Although a new, supercritical wing had also initially been considered, the aircraft, intended for short- to medium-range sectors which entailed higher ratios of climb-and-descent to actual cruise profiles, could not fully exploit such a new design, its benefits resultantly unable to justify its higher development costs. The existing DC-9 wing, incorporating root and tip extensions and modified high-lift devices, would provide the required performance, economy, and range parameters.

Several initial iterations, mostly based upon the DC-9-50 and all featuring fuselage stretches for higher capacities, larger-area wings, and two refanned turbofans, had included the refan-stretched DC-9-50RS, the refan-super stretched DC-9-50RSS, the DC-9-55, and the DC-9-60, while a DC-9QSF, intended for Japanese operators as an NAMC YS-11 twin turboprop replacement, mated a DC-9-40 airframe with two 18,000 thrust-pound JT8D-209 engines and a two-foot larger wing, enabling the 114,000-pound aircraft to operate from 4,000-foot runways with 120 passengers.

However, cost constraints and design complexities dictated a simpler, more straightforward version which incorporated the longer fuselage, increased-area wings, and JT8D-209 turbofans, yet retained cockpit commonality with all previous DC-9 variants. Skipping both the DC-9-60 and DC-9-70 sequences, the definitive aircraft, designated DC-9-80-or DC-9 Super 80, to more accurately reflect the intended year of service inauguration-had been launched on October 20, 1977 with the receipt of 27 firm and 13 optioned orders from Swissair, Austrian Airlines, and Southern Airways, along with a letter of intent from LAV Lineas Aeropostal Venezolanas, all of which had been previous DC-9 operators. Envisioned as a higher-capacity complement to its DC-9 airframe and a replacement for higher-cost tri-jets, it intended to provide service in maturing markets whose environmental and noise restrictions had precluded larger-capacity equipment substitution, the aircraft offering a significantly smaller noise footprint, greater range and capacity, and the lowest seat-mile costs of any comparable twin-jet.

According to then-President of the Douglas Aircraft Company, John C. Brizendine, “In recent years…we have become acutely aware of the need to conserve energy, to protect the environment, and to produce more and more economically efficient aircraft. (The DC-9 Super 80) is specifically designed to meet the requirements of our industry for years to come. These include environmental compatibility, energy efficiency, economical operation, and a spacious, comfortable interior.”

McDonnell-Douglas boasted of the aircraft, “The DC-9 Super 80 is a blend of proven design with available low-risk technology for enhanced effectiveness, (but) the remarkable DC-9 reliability and lower operating costs are maintained.”

Although it had been based upon this earlier-generation twin, it nevertheless introduced several advanced features.

A fuselage stretch, attained by means of an eight-frame plug forward of the wing and a single-frame insertion aft of it, resulted in a 147.10-foot overall length, increasing maximum capacity to 172, or 33 more than the DC-9-50 and a staggering 82 more than the initial DC-9-10, and producing the most massively stretched commercial airliner up to that time. The forward, left, and aft, ventral, exits, both equipped with extendible airstairs, had been retained, but an aft, left servicing door, located only feet from the engine, had been introduced. Aeritalia of Naples, Italy, manufactured its fuselage panels.

A new, 10.6-foot center section and two-foot parallel-chord tip extensions, resulting in the third dimensionally divergent DC-9 wing, yielded a 28-percent area, 57-percent fuel capacity, and 11-percent efficiency increase.

Measuring 107 feet, 10 1/4 inches, the airfoil, with a 24-degree sweep back at its quarter chord, a 9.62 aspect ratio, three degrees of dihedral, and a 1,239 square-foot area, had been comprised of four per-wing precision-machined skin panels which had been transformed from 14,000-pound ingots measuring 60 inches wide, 15 inches long, and 30 inches thick by the Reynolds Metal Company of McCook, Illinois.

The all-metal, two-spar structure, with riveted spanwise stringers, featured full-span, three-position leading edge slats with a new, intermediate setting to decrease take off drag and improve climb performance at higher gross weights; larger, doubled-slotted, trailing edge flaps which covered 67 percent of the span and lowered the aircraft’s stalling speed; three spoiler panels, the outer two of which were employable as both flight and ground lift dumpers; and ailerons. All but the latter were hydraulically actuated, while the ailerons themselves were manually operated. An underwing vortillon fence ensured proper airflow. Providing 1,520 US gallons of additional fuel tankage, it also offered an increased-area main undercarriage bay.

The variable-incidence, electrically-actuated horizontal tail, spanning 40.2 feet, or 3.6 feet more than that of the DC-9-50, retained the design’s characteristic t-tail configuration and sported assister tab-equipped elevators, while the vertical fin, rendering an overall aircraft height of 30.2 feet, featured a hydraulically-actuated rudder. It had been 1.4 feet higher than the DC-9-50’s.

Its Pratt and Whitney JT8D-209 turbofan, mounted on either side of the aft fuselage and retaining the original target-type thrust reversers, was based upon the core of the earlier JT8D-9, but introduced a 49-inch wider fan and an advanced, low-pressure compressor, producing 18,500 pounds of thrust along with an additional 750 pounds of automatic power reserve (APR), generated during engine-loss conditions. The larger-diameter, single-stage fan, driving a larger mass of hot core section-bypassing air, coupled with more efficient hot and cold exit duct intermixing air, and increased sound absorption material in its nacelle and surrounding casing, yielded numerous improvements, inclusive of increased thrust capability; a higher bypass ratio-of 1:1.78 as opposed to the earlier JT8D’s 1:1; a lower exit velocity; an 11-percent decrease in specific fuel consumption; and a significantly smaller noise footprint than that of the medium-range tri-jets it had been intended to replace.

Employing weight-reducing Kevlar-reinforced aluminum honeycomb stiffeners with graphite tape caps in the outer barrel of its nose cowl and its upper and two lower cowl doors, the nacelle, 21.1 feet long, was 4.5 feet longer than the JT8D-9’s and therefore presented engineering challenges relative to its mounting on the DC-9’s, albeit longer, body.

The DC-9 Super 80 retained the hydraulically-retractable, tricycle, dual-wheeled, Cleveland Pneumatic undercarriage, fitted with Goodyear wheels, tires, and disc brakes; Hydro-Aire Mk IIIA antiskid units; and Douglas ran air brake cooling. The nose wheel was steerable to 27 degrees to either side.

Although the Super 80 retained a common pilot type rating with the DC-9, it nevertheless offered several cockpit advancements, including a digital and flight guidance control system designed by the Sperry Flight Systems Division of Sperry Rand Corporation, which integrated the performance of seven flight control subsystems into two identical digital computers; cathode ray tube (CRT) displays; a digital fuel quantity gauge system; a dial-a-flap system; and Category IIIA autoland capability of 50-foot decision height (DH) and 700 feet of runway visual range (RVR). A later introduced Electronic Performance Management System provided automatic pitch and thrust to effectuate optimum speed and fuel burn during the aircraft’s climb, cruise, and descent profiles.

The 101-foot-long, “wide look” cabin, featured a broad, contoured, and sculpted acoustically-treated ceiling which blended in with the enclosable overhead storage compartments; aluminum sidewall panels sculpted round the windows; fluorescent lighting; a 19-inch aisle; and five-abreast, two-three or three-two, configured economy class seating, which reduced by half the number of middle seats traditionally associated with six-abreast arrangements.

Interior decor, which varied from conservative, business-oriented appointment to bold patterns and bright colors, was determined by the operator and custom-designed by McDonnell-Douglas whose interior design teams often made trips to airline home countries in order to absorb local culture and customs and then convert that experience into area- or country-reflective motifs. Wool and wool synthetic blends were standardly used for seat covers and carpets.

Class and seating configuration equally varied according to operator. A 137-passenger, dual-class arrangement, for instance, entailed 12 four-abreast first class seats at a 38-inch pitch and 125 five-abreast economy class seats at a 34-inch pitch, while single-class densities included 155 passengers at a 32/33-inch pitch, 167 charter seats at a 30-inch pitch, or a maximum of 172 high-density passengers, the latter accommodatable with a single galley installation.

Interior noise reduction was attained by means of an insulating blanket of fabric-reinforced Mylar over fiberglass.

The elongated DC-9 introduced a new pressurization and air circulation system, which replaced cabin air at greater frequencies, and its potable water system featured in-line heaters in all of its water lines. An increased-capacity auxiliary power unit (APU) ran its environmental control system on the ground.

The aircraft’s longer fuselage significantly increased its lower-deck baggage and cargo compartment volume, whose forward, center, and aft holds respectively encompassed 434, 376, and 443 cubic feet.

The DC-9-80 retained 80 percent of the DC-9-50’s key maintenance features.

Like all of its earlier, shorter-fuselage predecessors, the aircraft had been designed for short-sector, rapid-turnaround, self-sufficient operations from short, limited-facility airfields, with its increased thrust, larger-area wings, self-contained airstairs, auxiliary power unit for environmental conditioning and engine starts, low-to-ground profile to facilitate servicing, loading, and maintenance, and ability to operate two or more sectors without the need for refueling. Most turnarounds required little more than baggage carts.

With a maximum structural payload of 40,112 pounds, the DC-9-81, as designated in its initial variant, had a 147,000-pound gross weight, although this had been later increased to 149,500 pounds with uprated engines, and a maximum landing weight of 128,000 pounds. Its normal and maximum cruise speeds were, respectively, Mach 0.76 and 0.80. Range, with 155 single-class passengers and domestic reserves, was 1,564 nautical miles.
Piloted by Douglas Chief Engineering Pilot H. H. “Knick” Knickerbocker, Project Pilot John P. Laine, and Flight Test Engineer Virginia “Ginny” A. Claire, the first DC-9 Super 80 and the 909th twin-jet to roll off the Long Beach assembly line, made its maiden flight from Long Beach Municipal Airport’s Runway 30 on October 18, 1979 with call sign DACO 80-for “Douglas Aircraft Company 80.”

Following a 25-mile circular, overwater pattern, the long, slender-fuselage aircraft, accommodating 13,100 pounds of test equipment, completed a successful two-hour, 50-minute basic-maneuvers test sortie before landing at McDonnell-Douglas’s Flight Operations Facility in Yuma, Arizona, where the Chief Engineering Pilot concluded, “The ground handling of the Super 80 is even better than the other DC-9s. It also seemed quite stable in flight…The new engines were faultless, and the reverse thrust was very effective on landing…I believe the Super 80 is a great airplane and will live up to all our expectations.”

The 1,085-hour, $36 million, three-aircraft flight test program, which entailed first flights of prototype N1002G on December 6, 1979 and N1002W on February 29, 1980, led to FAA certification seven months later, on August 26, under an amendment to the DC-9’s original type certificate.

First delivered to launch customer Swissair on September 12, which had operated earlier DC-9-15, -30, and -50 series, it was inaugurated into scheduled service on October 5 from Zurich to Frankfurt, becoming the quietest commercial pure-jet. Co-launch customer Austrian Airlines, which had equally operated a fleet of DC-9-30s and -50s, inaugurated its first revenue service 21 days later, on October 26, from Vienna to Zurich.

In order to adopt the McDonnell-Douglas designation scheme, the DC-9-80, or DC-9 Super 80, was rebranded the “MD-80” in 1983, its initial version dubbed “MD-81.”

II

Development of the baseline Pratt and Whitney JT8D-209 engine, resulting in the uprated, 20,000 thrust-pound -217, augmented additional versions, the origin of which had been the 1979 requirement for a short take off and landing (STOL) aircraft to operate within the Japanese domestic market. A then-projected iteration, designated DC-9 Super 80SF, would have mated the DC-9-40’s fuselage with the DC-9-80’s wing and engines, but the higher-thrust JT8D-217, applied to existing fuselage dimensions, would have provided most of the desired performance. Resultantly, a second variant, designated MD-82 and first announced on April 16, 1979, featured the uprated, 20,000 thrust-pound turbofans with 850 pounds of automatic power reserve, a 44,024-pound payload, and a 2,050-mile range with 155 passengers. First flying on January 8, 1981, it received its FAA type certification six months later, on July 31, at an initial 147,000-pound maximum take off weight, although the 1982 option of JT8D-217A engines further increased this to 149,500 pounds, resulting in still-higher payload and range capabilities.

Republic Airlines, the July 1, 1978 amalgamation of North Central and Southern Airways, had been the version’s launch customer, having been the world’s largest DC-9 operator with series -10s, -30s, and -50s, to which its eight MD-82s were eventually added.

The variant had been involved in two unique programs. The first of these, occurring in October of 1982, entailed the innovative lease of 20 MD-82s to American Airlines, for which McDonnell-Douglas agreed to bear the maintenance and training costs. This let to the February 1984 purchase of 67 aircraft, at attractive prices and with low cancellation penalties, to be delivered in blocks of ten to 25 airframes, each block of which had been confirmable 24 months before the targeted delivery date. Becoming the mainstay of American’s short- to medium-range fleet to facilitate hub connections in Chicago and Dallas, the aircraft, configured for 142 first and economy class passengers, ultimately numbered 234, the world’s largest, single-type total outside of the former USSR.

The second innovative transaction occurred on April 12, 1985, when the Shanghai Aviation Industrial Corporation agreed to license-build 25 MD-82s in the People’s Republic of China.

An extended-range successor, designated MD-83 and first announced on January 31, 1982, introduced still higher-rated engines. The JT8D-219, rated at 21,000 pounds of thrust, featured a redesigned low-pressure turbine, a new high-pressure turbine, aerodynamically improved airfoils, a five-percent increase in thrust, and a two-percent reduction in fuel burn.

First flying on December 17, 1984, the twin-jet, with a 160,000-pound maximum take off weight, offered a 2,502-nautical mile range, attained by means of 1,160 US gallons of additional, lower deck hold-installed supplementary fuel tanks. Finnair, which had operated the DC-9-14/15, -40, and -50, served as the version’s launch customer, operating the longest, nonstop MD-80 flight on November 14, 1985, when it covered the 3,406-mile distance between Montreal and Helsinki in seven hours, 26 minutes. Transwede, of Sweden, inaugurated the first revenue-earning trans-Atlantic flight from Stockholm to Ft. Lauderdale with intermediate stops in Oslo and Gander.

In order to offer a lower-capacity counterpart more suitable to reduced-demand sectors, and to more effectively compete with the 737-300 Boeing designed for this market, McDonnell-Douglas offered the first, and only, dimensionally-divergent variant, the MD-87, which had evolved from its earlier, DC-9 Super XX studies for a 100- to 120-passenger aircraft powered either by Pratt and Whitney JT8D-200 series or CFM International CFM56-3 turbofans and offering a 110,000- to 120,000-pound gross weight. The variant, with a 16.5-foot shorter fuselage, featured a new, 130.5-foot overall length and had a 38,726-pound maximum payload, or the same as the DC-9-50’s.

Because of the decreased moment-arm of the shorter fuselage, vertical axis control required a larger-area, ten-inch taller fin, visible by the extension above its traditional t-tail mating point and resulting in a new, 31.2-foot overall height. It also introduced low-drag flap hinges and fairings, a fillet fairing between the fuselage and the engine pylon, and a reduced-drag, blade-shaped tailcone.

Initially powered by the 20,000 thrust-pound JT8D-217B, but later retrofitted with the lower fuel consumption -217C version, the MD-87 had a 2,372-nautical mile range with 130 passengers and domestic reserves, although additional, MD-83 type fuel tankage in the lower holds increased this to 2,833 miles.

First taking to the skies on December 4, 1986, it received its FAA type certificate on October 21 of the following year, and was inaugurated into service on December 17 with Austrian Airlines from Vienna to Zagreb.

The last, and most advanced, of the five versions, the MD-88, reintroduced the original fuselage dimensions and was announced on January 23, 1986 after launch customer Delta Air Lines placed an initial order to 80 of the type. Offered with 21,000 thrust-pound JT8D-219 turbofans, the version, most closely based on the MD-82, featured increased composite material to reduce structure weight, a new passenger cabin with a wider aisle and modernized overhead storage compartments, and an advanced, glass cockpit, the latter comprised of an electronic flight instrument system (EFIS), a flight management system (FMS), and an inertial reference system (IRS). It retained the MD-87’s blade-shaped tailcone.

First flying on August 15, 1987 and FAA-certified four months later on December 9, the MD-88 entered scheduled service with Delta on January 5, or just over 22 years after it had operated the world’s first passenger-carrying service with the -14 series on December 8, 1965. It had also operated the stretched DC-9-30 and the MD-82.
III
The 1,000th MD-80 had been delivered on March 29, 1992, and by December of 1997, 1,150 of the type had been in service with 60 worldwide airlines. The design, partially succeeded by its advanced, re-engined MD-90 counterpart and Boeing’s own Next Generation 737 family after that manufacturer’s acquisition of McDonnell-Douglas, nevertheless became its best-selling pure-jet commercial airliner, exceeding sales of the DC-8, the Super DC-8, the DC-9 itself, the DC-10, the MD-11, the MD-90, and the MD-95/717, the last delivery of which had occurred on December 21, 1999, when an MD-83 had been handed over to TWA, ending two decades of production. Combined with the 976 sales of the original, short-fuselage DC-9, it became the third best-selling twin-jet after Boeing’s 737 and Airbus Industrie’s A-320 family, with a collective 2,167 airframes having been built.

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Source by Robert Waldvogel

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Embraer PRAETOR 600 Private Jet Charter EMBRAER PRAETOR 600 PRIVATE JET HIRE EMBRAER PRIVATE CHARTER MLKJETS7 - The Beechcraft King Air 90 private jet hire cheap uk

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If you are looking for a small aircraft that is big on comfort for your next business trip, look no further than the Beechcraft King Air 90. This twin-engine turbo prop aircraft can fly farther and higher than its piston engine competitors, meaning you can get where you are going faster and with less hassle than ever before. The turbo prop plane makes it easy to get to smaller airports that may be closer to your final destination than using the huge, crowded airports found in large cities. It can land on shorter runways with no difficulty and needs less room to take off, making it efficient both in the air and on the ground. This aircraft performs well on wet runways or in climates that are hot or at high altitudes, making it a great choice for many varied destinations. With a 1,264 nautical mile range and a top speed of 256 knots, this plane will get you to that meeting or conference in another state quickly and effectively. Its improved climb rate makes reaching your cruising altitude a shorter experience and also makes the plane that much more fuel efficient.

With comfortable seating for six, the Beechcraft King Air 90 boasts leather seats that swivel and recline, making a working flight possible. Pull out tables, cabinets for refreshments and an accessible baggage area mean that you are never without that needed file or piece of equipment en route. The large windows allow light to enter and the fresh air outlets will ensure that you arrive refreshed and ready to take on your day.

The Beechcraft King Air 90 has been redesigned from its predecessors to have larger headroom and shoulder room space making it a comfortable trip for all in the party. It has been specifically engineered to be quiet while in the air and as the seats swivel, you can make groupings for conversations more easily than you could with standard seats on other aircraft. All of these innovations allow you to choose a productive flight or one where you simply relax in the comfort of the seats as you cruise to your destination.

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Source by Amanda J Hales

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Embraer LINEAGE 1000E Private Jet Charter EMBRAER LINEAGE 1000E PRIVATE JET HIRE EMBRAER PRIVATE CHARTER MLKJETS7 - The Historic TWA Terminal and Lockheed Consellation at JFK

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INTRODUCTION:

As I passed the curb-parked convertible and entered the doors of the Eero Saarinen-designed TWA Terminal with its winged, flight-suggesting roof at JFK International Airport on a mid-September day, nothing, I noted, had changed, except that the passenger check-in counters flanking either side were refreshingly devoid of lines. Perhaps that should have been a hint.

Mounting the dozen stairs and then redescending those that led to the familiar Sunken Lounge, I eyed the Solari split-flap arrivals and departures board, its panels periodically flipping and clacking like stacking poker chips, but they only revealed blank squares. There were no flight numbers, no times, and no destinations.

Yet by views of the vintage airliners on the ramp through the floor-to-ceiling angled glass displaying TWA’s red-and-white livery, but lacking a single jet engine, my destination today could only be labeled “history” or, even “aviation history.” Perhaps that was appropriate for the “luggage” I brought: a carry-on consisting of a clipboard and a pen.

The scene before me was a suspended one. The period music and the announcements echoing through my head transported me to the one I was not in.

“TWA Starstream Flight 802 to Paris, now boarding at gate one,” they said.

My eyes, scanning past the location of the once famous and familiar Brass Rail Restaurant toward the dual, main terminal connecting tubes still covered with chili red pepper carpeting to the departure area, I fully expected to take in one or more Boeing 707-320Bs with their bluntly pointed, radome noses, 35-degree swept wings, and Pratt and Whitney JT3D-3B low bypass ratio turbofans.

Yet the Lockheed L-1649A Starliner Constellation, representing the pinnacle-of-piston development, indicated that the era preserved and depicted “out there” was not the one my mind tried to convince me still existed “in here.” Instead, it was two decades earlier, of the 1960s, and I had entered a preserved pocket of time.

THE TWA TERMINAL:

As an expression, representation, and development of the post-World War II-fueled, technology-facilitated commercial airline industry and the then-named Idlewild International Airport whose evolution resulted from it, the TWA Terminal was and is an architecturally aesthetic symbol of it all. It captures the sensation of flight with its wing-resembling shell and the fluid, open interior beneath it.

Unlike many of today’s single-building, multiple-airline facilities, it traces its origin to 1954 when the Port Authority of New York devised its terminal city concept. Anticipating the need for infrastructure to cater to increasing travel demand, it implemented a plan in which each major carrier would design, build, and operate its own terminal, fostering, in the process, brand identity. Although the TWA facility was the architectural response to the Port Authority’s masterplan, its airline-association was one of its intentions from the start, as stated by the project commission, which first sought an efficient ground operations infrastructure, but secondarily wanted “to provide TWA with advertising, publicity, and attention” with it.

That the chosen site for it was at the apex of the airport’s access road, cemented the intention almost as much as the hardened substance which formed it, and that it still does today, despite the two-decade interval since the airline’s demise, serves this post-carrier purpose.

Eero Saarinen, a Finnish-American architect and designer and sometimes considered a mid-century master, was chosen to transform both Idlewild’s and TWA’s vision into concrete reality in 1955. Tracing his own genealogical roots to his father, Eliel Saarinen, an architect, and his mother, Loja Saarinien, a textile artist, he could claim that the talent ran through his veins just as freely as did his blood when he was born in 1910. After studying sculpture in Paris, architecture at Yale University, and design at the Cranbrook Academy of Art in Michigan, he transformed material into aesthetic function in such creations as the St. Louis Gateway Arch and Washington-Dulles International Airport.

Although Eero Saarinen achieved his goal of crafting an abstract representation of flight in the TWA Terminal, its inspiration was never definitely determined, some suggesting that a thumb depression into a hollowed grapefruit rind resulted in the eventual curved, concrete, symmetrically positioned roof sections that seamlessly flowed from the piers that supported them and were only separated by narrow skylights. The four met at a circular pendent center point.

The roof’s wing surface curvature or camber continued in the crimson and white interior by means of the upper walkaway supported columns that merged into both floor and ceiling as if they were integral to them. Its lack of rectangularity was evident in its other features. The stairways, for instance, were curved and its terminal and departure lounge connecting corridors were more like cylindrical tubes.

Its overall expression was one of 1960s neo-futurism and space-age Googie architecture.

Despite what ultimately proved to be Saarinen’s architectural achievement, it also became his legacy, since a year after he inspected its superstructure in 1961, he passed away at 52, never having seen his finished product.

While it was intended to serve small piston airliners whose capacities never exceeded a hundred, it was not suited to TWA’s narrow body jets, such as the 707 and the 727, much less its widebody ones, including the 747, the L-1011 TriStar, and the 767, requiring the addition of jetbridge-connected boarding satellites.

After the carrier’s 2001 demise, its signature terminal awaited purpose or preservation. Its demolition, at least, had already been spared. In 1994, it was designated a New York City landmark, at which time then Chairwoman of the Landmark Preservation Commission, Larie Beckelman, commented in “The New York Times,” “This is perhaps the quintessential modern form, expressing movement and the whole concept of flight.”

Eleven years later it was placed on the National Register of Historic Places. With its presence at least assured, it still awaited the two “p’s”-preservation and purpose.

THE TWA HOTEL:

Preservation and purpose, in the event, became two sides to the same coin-that is, restore the 392,000-square-foot terminal to recreate its 1960’s splendor and serve as the anchor and lobby to another two sides-in this case, two rectangular, black glass buildings with 512 hotel rooms developed by MCR/MORSE and four architectural firms at a $250 million-plus cost.

Architect Richard Southwick, who oversaw the project’s restoration, noted of the TWA Flight Center, “(It was) the perfect symbol of post-war optimism, the magic of flight, and the elegance of mid-century modern architecture.”

Its first guests were accepted in May of 2019.

As a “lobby,” it contains the Sunken Lounge with the Solari flight board; a cocktail lounge; a Sundries Shop with vintage copies of “Life,” “Time,” “Good Housekeeping,” and “Family Circle” magazines; an old-fashioned shoe shine station tucked in the corner (of course); a TWA Gift Shop whose every item, one way or the other, displays the airline’s logo; a 10,000-square-foot fitness center with a cycling studio, treadmills, ellipticals, a spa section, and personal trainers; and the Paris Café by Jean-Georges, which occupies the footprint of the original one, along with that of the Lisbon Lounge, on one of the two mezzanines and serves cuisine inspired by TWA in-flight menus. There is also 50,000 square feet of meeting and event space.

The two cylindrical tubes-the “Saarinen” to the left and the “Hughes” to the right-lead, by way of midway, originally nonexistent cutouts, to the two seven-story glass, metal, and concrete hotel structures, which were required to be complimentary to, but distinguishable from, the landmark terminal.

Seven layers of triple-glazed, 1,740-pound, insulated, floor-to-ceiling glass ensure in-room silence, despite the fact that ramp-taxiing aircraft are only yards away.

Rooms, which either overlook this scene or the terminal, rent for $250 per night, with lower priced intervals bookable for transit passengers who only seek a short sleep and a shower.

The roof features the Infinity Edge Pool and observation deck, along with a bar.

Only the “Saarinen” tube, back on the main level, leads out-or, in the reverse direction, in-to this preserved pocket of time, as expressed by the two floor designations-or eras-on which the elevator at its end alights: “1960s TWA Hotel” and “Present Day JetBlue,” according to the two buttons the passenger can press to travel there.

THE MUSEUM DISPLAYS:

While the Eero Saarinen designed terminal can be considered a collective, retro, but still-living arena, several areas serve to accentuate it in museum form.

“Located in various spots throughout the former TWA Terminal-the heart of our hotel-as well as in the event center and in the areas that connect our hotel flight tubes to JetBlue’s Terminal 5, the exhibits (curated by the New York Historical Society) allow visitors to experience the jet age through authentic artifacts, interactive displays, and personal narratives,” according to the TWA Hotel website.

Its 2,000 items hail from the TWA Museum in Kansas City, as well as from the former airline employees who donated them.

“Exhibitions focus on TWA’s history, including Howard Hughes tenure as owner, TWA uniforms from 1945 to 2001, and Saarinen’s development of the terminal at Idlewild Airport,” the website continues.

Stressing the latter’s importance, Mike Thornton, New York Historical Society curator, stated, “The Saarinen terminal is a monument to the optimism and vision of the jet age. These exhibitions invite people into the glamor and fun that Saarinen and TWA worked so hard to create and foster.”

A desk, old fashioned typewriter, and system timetable set-up next to the elevator, for instance, recreates a TWA corporate office, while wall displays tell the carrier’s story, along with its Howard Hughes influence and its historic aircraft.

Black-and-white photographs gracing the walls opposite the hotel check-in counter depict TWA’s early “airline of the stars” image, with the likes of Jimmy Durante, Marilyn Monroe, Lucille Ball, Elizabeth Taylor, Bob Hope, Frank Sinatra, the Beatles, and Mary Tyler Moore boarding aircraft as diverse as the Ford Trimotor and the Boeing 707.

A TWA flight crew uniform and luggage exhibit is located on the second of the two mezzanines.

“The glamor of air travel in the jet age catapulted TWA pilots to star statuses, many of them celebrated as much for their dashing good looks as their ability to navigate a transatlantic flight,” according to the exhibit. “Pilot uniforms with gold epaulets, pins, and jaunty hats burnished their admired role as those who could fly through the clouds on the new jets of the 1960s.”

The evolution of flight attendant uniforms, displayed on mannequin bodies, depict the five designers who created them: Don Loper (1960-1965), Dalton of America (1968-1971), Valentino (1971-1975), Stan Herman (1975-1978), and Ralph Lauren (1978-2001).

THE LOCKHEED CONSTELLATION:

Jotting notes in the Sunken Lounge as I awaited my flight, I realized that even here I was immersed in Saarinen’s world, bodily cradled by womb chairs at tulip tables, both of which he designed.

The board continued to click and clack, sometimes displaying departures by carriers such as Pan Am. Even it had taken off for a final time, deposited in that dimension known as “history.”

Ground attendants-I guess the in-flight “stewardess” counterpart was an acceptable, albeit sexist, title in those days-took drink orders.

Subliminally, subconsciously, and emotionally, I suddenly knew that it was time to board my flight. No one called it. History did-the lure and love of aviation history, that is. Responding, I rose from my Sunken Lounge seat, filing down the corridor past the library-cum-bookstore Reading Room, and finally opened the door to the tarmac. There were no lines. No one stopped me. No one asked me for a boarding pass. Flights destined for yesteryear apparently did not require them. What has already played out in time was free and available to anyone who wished to recreate or relive it.

Walking over the lines painted to represent mock Runway 04-Right/22-Left, I approached the airliner, poised on the ramp in its 1960’s glory. If I could have stood on a ladder, I could have faced it, nose-to-nose. As a six-decade technological interval, its propellers did nothing to detract it from its sleek design profile.

From the long, angled, aft-retracting nose gear strut, which touched the tarmac with its dual, equally angled tires to save rubber during tight ground turns, my eyes moved up to the black nose cone and the seven-pane cockpit windscreen. The fuselage, emulating an airfoil, gently sloped upward behind the cockpit and downward again at the rear, just before the triple vertical stabilizers, an engineering solution to low-ceilinged hangars. The straight, but tapered wings, mounted at a seven-degree dihedral and lined with deicing boots on their leading edges, sported four, three-bladed propeller, Wright Turbo-Compound engines. The aircraft, registered N8083H “Star of America,” had returned “home” and in many ways was Trans World Airlines.

Eagerly anticipating its refurbished cabin, I climbed the boarding steps, which proclaimed, “Up, up and away with TWA,” and stepped inside. “Away” I would.

THE EARLY CONSTELLATION VERSIONS:

Like the Eero Saarinen designed terminal, the Lockheed Constellation was a product of the same force-ever-increasing post-war demand, except the airliners, embodying advancing technology, also needed to remain competitive with other carriers that operated rival designs.

TWA, however, had an additional urgency for a modern fleet replacement. Compared to United’s northern and American’s southern route coverages, its mid-continent one placed it at a disadvantage.

What was needed (by all three airlines) was a larger capacity, longer-range, more comfortable counterpart to, if not replacement for, the ubiquitous twin-engine DC-3 on one-stop transcontinental routes.

“Howard (Hughes) had the idea he could steel a lot of the Hollywood crowd’s business away from the other fellows, if we had a super-deluxe airliner that could fly nonstop L.A. to New York, or even one-stop via Chicago,” according to Jack Frye, TWA’s Vice President of Operations in Douglas J. Ingells’ book, “L-1011 TriStar and the Lockheed Story” (Arco Publishers, 1973, p. 73). “He was talking eight or nine hours flying time, coast-to-coast, about post-posh interiors with a club car atmosphere in a day plane, and Pullman-style berths for night trips. It all sounded far out, but Hughes was dead serious.”

Three quad-engine, new-generation airliners were proposed by the three competing aircraft manufacturers at this time: the DC-4E from Douglas, the B-307 Stratoliner from Boeing, and the L-44 Excalibur from Lockheed, which, in April of 1939, served as the Constellation’s early foundation, featuring a triple vertical tail, a 36-passenger complement in a pressurized cabin, a 1,200-US gallon fuel capacity, and a 40,000-pound gross eight.

As a larger development of the Excalibur, the L-49, which would prove the first in a series of more ambitious versions, was powered by four 2,200-hp Wright Duplex Cyclone engines, and could carry a 6,000-pound payload at between 250 and 300 mph at a 20,000-foot cruising altitude. Its still-air range was 3,500 miles. Most unique to the design, however, was its fuselage.

“… The Constellation’s fuselage, of circular cross section throughout its length, featured a cambered centerline to give it an airfoil profile in side view,” according to M. J. Hardy in his book, “The Lockheed Constellation” (Arco Publishing Company, 1973, pp. 12-14). “This served both to increase the maximum width of level floor, especially in the nose and tail sections, and to shorten the nose wheel leg by drooping the front fuselage… “

After reviewing the design’s specifications and making corrections of his own, Hughes ordered the type-initially nine, but subsequently 40. Since TWA itself could not afford the expenditure, he had no choice but to pay for the aircraft himself. “Send the bill to the Hughes Tool Company,” he instructed.

First flying in prototype form on January 9, 1943, it demonstrated that all of its design goals had either been achieved or exceeded. Maximum (not cruise) speed was 347 mph and gross weight was incrementally increased from an initial 68,000- to a final 86,250-pound maximum.

Its intended commercial application, however, was placed on hold. The December 7, 1941 Pearl Harbor attack, opening war in the Pacific theatre, relegated the luxurious airliners to a troop and supply transport, and those L-49s rolling off the production line and modified for wartime service, were redesignated C-69s and were delivered to the US Army Air Force instead. On one such flight, an aircraft in TWA colors and piloted by Hughes during the first half of its transcontinental sector and by Frye on the second half of it, covered the 2,400-mile Burbank-Washington distance on April 17, 1944 in record time, clearly demonstrating the design’s potential.

“We did not deliberately set out to establish a new transcontinental record,” Frye later stated. “The trip was made in six hours, 58 minutes simply because the Constellation was designed and built to fly at such remarkable speeds.”

The first production Constellation, now designated L-049 to distinguish it from the original, pre-war variants, was certified by the Civil Aeronautics Board on December 11, 1945, and TWA inaugurated the type into transatlantic service between New York and Paris-Orly three months later, on February 5. Powered by R-3350 engines with three-bladed, 15.2-foot-diameter, reversible pitch, fully feathering propellers, the appropriately named “Star of Paris” carried 35 passengers to the City of Light via Gander and Shannon.

Ten days later it placed the type on the transcontinental route between New York and Los Angeles, completing the eastbound leg in 9.45 hours and the westbound one in 11. In comparison to American’s and United’s slower, unpressurized, two-stop DC-4s, the Constellation offered a distinct competitive advantage.

Lockheed’s “Of Men and Stars” history noted, “In the five months that followed introduction of the Model 049 to commercial airline service in February 1946, the majestic triple-tail transports set new standards of speed, comfort, and safety. They made 300-mph schedules a reality (and) ocean-to-ocean nonstop flights commonplace.”

While the type’s 92.5-foot length and 123-foot wingspan initially remained the same, two subversions introduced increased range and improved performance.

The L-749 intended for intercontinental services, carried 565 additional US gallons of fuel, for a new 5,820-gallon total, increasing its range by some 1,000 miles. Maximum take off and landing weights were respectively increased to 102,000 and 87,500 pounds.

Both versions introduced new propellers, flap deflection increases, and improved cabin heating, cooling, and ventilation systems.

A significant Constellation operator, TWA counted 12 L-749s and 25 modified L-749As in its fleet, over and above its original L-049s, enabling it to serve transatlantic routes to London, Paris, Rome, and then-named Bombay.

Accommodation varied according to market. Its “London Ambassador” service, for example, which was inaugurated on April 8, 1951, was configured with 18 berths. “Sleeper Flights” carried 32. Five-abreast, all-coach transatlantic services seated 60 and US domestic ones 81.

TWA retired its last L-049 at the end of 1961.

THE SUPER CONSTELLATION:

Technical advancements, along with increased speed, safety, and comfort introduced in the five years since the end of World War II, created unprecedented demand for both domestic and international air service, toward which Lockheed, with its three basic L-049, L-649, and L-749 variants made a significant contribution. Although subsequent updates, designated L-749B and L-849, would have offered even greater performance with, respectively, uprated piston and Napier Eland turboprop powerplants, passenger demand indicated the need for greater capacity instead, achieved through stretches of the existing fuselage. Because flight tests with L-749s demonstrated that its gross weight capability could be as high as 137,000 pounds with its original wing, no major design modifications were required.

Based upon studies for an earlier, 100-passenger, but never built L-949, the first and, in the event, only stretched version, the L-1049A Super Constellation, incorporated a new wind screen, an 18.5-foot fuselage insertion for a new 113.4-foot overall length, rectangular passenger windows that replaced the previous oval ones, and provision for 730 additional gallons of fuel in a new center section tank.

Powered by four 2,700-hp R-3350-956C18 CA-1 engines, it incorporated a larger fin to counteract the additional weight, a 728-cubic-foot underfloor baggage and cargo volume, an improved pressurization system to create a 5,000-foot altitude at 20,000 feet, a 6,550-US gallon fuel capacity, and a 120,000-pound maximum weight.

Certification, although initially only at a 100,000-pound gross weight, took place on November 29, 1951 and TWA, which ordered ten of the 24 L-1049As produced (Eastern operated the remaining 14) inaugurated them into service on September 10 of the following year.

“Model 1049 emerged as a stretched version of the original Army Air Corps cargo transports,” according to Ingells (op. cit., pp 80-82). “In its original form, Connie was designed to carry 65 passengers. Model 1049 could carry 99.”

“Connie was a lady, who simply had to keep up with the latest styles,” he went on to say (p. 83).

The new version enabled TWA to inaugurate transcontinental Ambassador Service on October 19, 1953, which retained the Chicago intermediate stop on westbound legs, but omitted it on eastbound ones. These were completed in under eight hours. Despite the competitive promise it carried when pitted against American’s DC-6Bs, it only lasted six weeks. Thereafter, its DC-7s could cover the distance nonstop in both directions.

The Super Constellation series culminated with two other versions. Power equaled payload and performance and the introduction of 3,250-hp Wright Turbo-Compound R-3350-972TC18 DA-3s, along with the optional installation of two 600-US gallon tip tanks, provisioned it with a 7,750-US gallon total, giving it a 4,620-mile range with reserves. Ninety-nine single-class passengers could be comfortably accommodated in the 92-foot-long, highly sound-proofed cabin. Northwest Orient, launch customer for the resultant L-1049G, took delivery of the type on January 22, 1955.

TWA placed orders for 12 and then eight L-1049Gs in October of 1953 and November of 1955. Its aircraft featured weather radar, the two wing tip fuel tanks, 700 pounds of cabin insulation, and two-compartment General Electric air circulation ovens that could simultaneously heat 60 pre-cooked meals.

THE STARLINER:

If any aircraft, and any version of that aircraft, were symbolic of Trans World Airlines, it was the Lockheed L-1649A Starliner. It seemed to make that statement today.

Necessity, as always, provided the direction and pointed to the destination, the latter being the long-range ones airlines had to cover without wind, seasonality, and payload restrictions, and Douglas, soon to introduce the intercontinental version of its DC-7C “Seven Seas” with its ten-foot greater wingspan, injected Lockheed with new impetus if it wished to remain competitive. Although the resultant L-1649A was a technical success, the year required for its considerable redesign alas placed it on the market too late for anything but paltry sales.

A modified wing, key to its improved capability, served as a foundation laid earlier for an L-1449 to have been powered by turboprops from either the US or UK, but which, in the event, had neither been proven suitable nor certifiable. Nevertheless, it incorporated 37-foot-long, integrally stiffened skin panels, full-depth tank end ribs for a new four-tank fuel system, closely spaced ribs, and a revised trailing edge and Fowler flaps.

While work on this version ceased in early-1955, engineering resources were reassigned to what would become the definitive, longest range version, the L-1649, which was later designated L-1649A Starliner. Overall length remained the same as that of the Super Constellation series, but a tapered, 150-foot, thinner wing of higher aspect ratio was mounted further back on the fuselage and four 3,400-hp Wright R-3350-988TC18 EA-1 Turbo-Compound engines were installed further outboard, reducing cabin decibel levels. The larger-diameter, synchronized, low tip-speed Hamilton Standard propellers, coupled with 900 pounds of additional cabin insulation, cemented its quiet interior.

Its maximum take off weight was 156,000 pounds.

The first of two flying prototypes in its three-aircraft test program took to the air from Burbank on October 11, 1956 and TWA took delivery of the first of 25 L-1649As the following April.

Configured for 30 first and 34 coach seats, along with an eight-berth first class sleeping compartment, it operated “Nonstop Ambassador” service from New York to Los Angeles and San Francisco, later introducing the concept from Boston and Washington. Its transatlantic service, “The Jetstream,” served London with 74-passenger coach cabins as of July 1, 1957 and was subsequently extended to Paris, Frankfurt, and Rome. Transpolar flights, from Los Angeles to London with an intermediate stop in San Francisco, commenced October 2. The following year, in March, the London-San Francisco sector was covered in 19 hours, 5 minutes, which beat its previous record. All-coach “Golden Barron” transcontinental services were also operated with the type.

Compared to the initial C-69 military transport, the L-1649A Starliner had weight, power, and capacity increase of, respectively, 44.5, 47, and 72 percent.

“Rugged, reliable, easily flyable, distinctly styled, and naturally graceful” is how TWA Captain Dave Richwine described the aircraft (Morgan, op. cit., pp 8-9). “The Lockheed Constellation has been a star performer… and is most certainly a candidate for one of the all-time great commercial transports… Conceived in love for aviation and in hope of enhancing the future of commercial air transportation, she was born in the last World War II years, first serving her country as a military air transport. Following her strenuous baptism as a 93,000-pound fledgling that started life sans steerable nosewheel and reversible props, she took her place in the commercial air transport industry. Since then, she has probably undergone more developmental stages than any other commercial air transport in history to finally emerge supreme as a member of the piston royalty in the form of a 160,000-pound 1649A Jetstream.”

A total of 856 military and commercial Constellations, which only featured two fuselage lengths and two wingspans, of all versions was built. Before TWA operated the last one, albeit in freighter form, on May 11, 1967-replaced by Boeing 707-120s-its Constellation fleet had transported an estimated 50 million passengers between 1946 and 1967, and during 1959, the type’s peak, it counted 32 L-049s, 12 L-749s, 27 L-749As, 9 L-1049As, 28 L-1049Gs, and 29 L-1649As in its inventory. I was in one of the latter ones today.

“STAR OF AMERICA:”

The Constellation that stood ready to accept passengers at the restored TWA Terminal on that mid-September day, N8083H, had rolled off of Lockheed’s Burbank production line in 1958, flying under the carrier’s colors, first as a passenger airliner, then as a freighter, for only four years.

As I entered the cabin, I thought of M. J. Hardy’s words. “An outstanding example of piston-engine airliner design at its peak, the Constellation well befits the dictionary definition of its name as ‘a group of fixed stars, or an assemblage of splendors or excellences,'” he said (Hardy, op. cit., p. 7).

While “Star of America” was configured as a cocktail lounge, there was enough of its design as an airliner left to inspect.

A view into the metallic green cockpit, in which the JFK tower frequency issued an unceasing barrage of instructions to active flights, provided a glimpse into what the pilots viewed-from the sky through the three forward and four side window panes to the half-moon yokes, engine indications on the center panel, the four throttles on the pedestal, and the flight engineer’s station, on whose table was laid both a normal and an emergency checklist. Aside from his own panel that sported a myriad of indicators, there were also throttles, engine superchargers, mixture controls, and fuel shut-off valves.

Behind and to the left of the cockpit was the separate navigator’s station, whose crew member determined the aircraft’s location by taking star fixes through the roof-installed astrodome.

The cabin-converted cocktail lounge was configured with both burnished gold upholstered banquets and traditional four-abreast seats with TWA headrest covers, and the carpeting was airline indicative bright red.

Since no boarding pass indicated the one assigned to me, I chose a window one on the port side, settling into the 1960’s dimension and studying the upper wing surface and the two projecting piston engines. Propellers they certainly sported!

A Royal Ambassador menu detailed what might have been served if I had been in flight at that time: hors d’oeuvres of American caviar and an assortment of delicacies from the cart; cream of asparagus soup; a garden salad with bleu cheese or French vinaigrette dressings; entrees such as chateaubriand, chicken champagne, lamb rib roast, and lobster thermidor; a cheese board with a selection of fresh fruit; cassata siciliana; and after-dinner coffees. Vintage wines, of course, flowed throughout the repast.

The Constellation’s cocktail menu today indicated purchasable items, such as “Cocktails 316,” spirits, wine and champagne, beer, nonalcoholic beverages, and snacks like a charcuterie, marinated olives, hummus, and a cheese board.

A cutout provided a view of the aircraft’s framework-that is, the outer skin and longerons of its fuselage.

Paris and Hollywood mural replicas adorning the aft sidewalls represented those eight-by-four-foot ones designed by Mario Zamparelli that depicted 25 TWA-served destinations from Boston to Bangkok in the Starlight Lounges of its Constellations.

As I deplaned through the aft, left door and descended its boarding stairs, I thought of Douglas J. Ingells’ concluding words about the airliner.

“Her sleek lines, the shark-like profile of her fuselage, her distinctive triple tail, and the many advanced features she pioneered, left a high heritage in the annals of commercial aviation. She had class, grace, and beauty. And of all the so-called ‘Sky Queens,’ her reign will never be forgotten,” (Ingells, op. cit., p. 83).

THE JOURNEY:

I spent some three hours immersed in the Eero Saarinen created era, and it took far less time than that to walk down the Constellation’s aisle, from its forward to its rear door. Yet as my feet once again made contact with the ground-and, perhaps, the 21st century-I realized that I had just completed a six-decade journey into history, not of motion, but of mind.

Bibliography

Hardy, M. J. “The Lockheed Constellation.” New York: Arco Publishing Company, 1973.

Ingells, Douglas J. “L-1011- TriStar and the Lockheed Story.” Fallbrook, California: Aero Publishers, Inc., 1973.

Morgan, Terry. “The Lockheed Constellation.” New York: Arco Publishing Company, 1967.

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Source by Robert Waldvogel

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