Free Essays on Chasepeak Vs. New England In 1700s

â€Å"Community organizing refers to the entire process of organizing relationships, identifying issues, mobilizing around those issues, and building an enduring organization†. (Stoecker and Stall, 1996). Although New England and the Chesapeake region were both settled largely by the people of English origin, by 1700 the regions had evolved into two distinct societies. The reasons for this distinct development were mostly based on the level of religious idealism, motives of people who came to settle in these colonies, the environment, & area around them, and the source of economy along with their social life. The first and maybe the most important factor that resulted in two different colonies at the same time period was the motivation of people who migrate to these regions. On one hand, the puritans, who colonized the New England, were very religious. They wanted to create a model society in which there were limits to legitimate commercial behavior, and the religious idealism would turn into a renewed sense of community. They were very strict in their religious beliefs. From the Article of Agreement, Springfield, Massachusetts it is clear that religion was the basis for general laws. It uses the phrase "being by God’s providence engaged together to make a plantation", showing that everything was done in God’s name. The Wage and Price Regulations in Connecticut is an example of common laws being justified by the bible. Also in this document the word "community " is emphasized, just as Winthrop emphasizes it saying: "we must be knit together in this work as one man". The i mmigrants to New England formed very religiously oriented communities. They considered themselves as spiritual members of Church of England, and created a system of self-governing congregations that completely ignored the authority of Anglican bishops, and was governed by Saints. Yet on the other hand Chesapeake society was based on the personal gain and pr... Free Essays on Chasepeak Vs. New England In 1700's Free Essays on Chasepeak Vs. New England In 1700's â€Å"Community organizing refers to the entire process of organizing relationships, identifying issues, mobilizing around those issues, and building an enduring organization†. (Stoecker and Stall, 1996). Although New England and the Chesapeake region were both settled largely by the people of English origin, by 1700 the regions had evolved into two distinct societies. The reasons for this distinct development were mostly based on the level of religious idealism, motives of people who came to settle in these colonies, the environment, & area around them, and the source of economy along with their social life. The first and maybe the most important factor that resulted in two different colonies at the same time period was the motivation of people who migrate to these regions. On one hand, the puritans, who colonized the New England, were very religious. They wanted to create a model society in which there were limits to legitimate commercial behavior, and the religious idealism would turn into a renewed sense of community. They were very strict in their religious beliefs. From the Article of Agreement, Springfield, Massachusetts it is clear that religion was the basis for general laws. It uses the phrase "being by God’s providence engaged together to make a plantation", showing that everything was done in God’s name. The Wage and Price Regulations in Connecticut is an example of common laws being justified by the bible. Also in this document the word "community " is emphasized, just as Winthrop emphasizes it saying: "we must be knit together in this work as one man". The i mmigrants to New England formed very religiously oriented communities. They considered themselves as spiritual members of Church of England, and created a system of self-governing congregations that completely ignored the authority of Anglican bishops, and was governed by Saints. Yet on the other hand Chesapeake society was based on the personal gain and pr...

Bell 412 Specs

This document is intended for the use of BHTI employees, and BHTI independent representatives (international dealers), and for prospective customers as an aid in determining estimated weight and performance of the helicopter when configured with equipment for specific missions. Disclosure, reproduction, or use of any material in this document by persons other than BHTI employees, and BHTI independent representatives, and prospective customers are forbidden without written permission from Bell Helicopter Textron Inc. The listings of Optional Equipment (â€Å"Kits†) are subject to revision and change, and also may be different for specific serial number helicopters or special custom configurations. Please consult the â€Å"Notes† column found in the optional equipment list tables for equipment compatibility. The continuing product improvement process of BHTI may cause some components, equipment, and compatibility to be changed or replaced. The specifications, weights, dimensions, and performance data shown in this document are subject to change without notice. 2012 Bell Helicopter Textron Inc. Bell, 206, 407, 407GX, 429, 412, Huey II, LongRanger and JetRanger are registered trademarks of Textron Innovations Inc. All rights reserved Specifications subject to change without notice. Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 1 1  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:05 PM Page Intentionally Left Blank  © 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 2 2 Bell 412EP Production Specification May 2012 6/5/2012 8:37:05 PM Bell 412EP RELIABLE, RUGGED AND READY The Bell 412EP is the workhorse of the helicopter industry with a reputation of getting up and going to work every day in even the most extreme environments. †¢ Proven Pratt Whitney PT6T-3D Twin Pac engines with more than 25 million flight hours in more than 2,000 aircraft worldwide †¢ High retirement and overhaul intervals 5,000 hour drive system TBO 4,000 hour engine overhaul interval On-condition composite main rotor blades †¢ 25,000 hours between premature engine removals †¢ Excellent Category A / JAR OPS 3 capability †¢ Rugged fuselage with rollover bulkhead protection and rupture resistant fuel cells The data set forth in this document are general in nature and may vary with conditions. For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight Manual Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 3 3  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:05 PM Specification Summary (U. S. Units) Weight lb Weight lb Empty Weight (IFR Std. Config. ) 1 6,964 Maximum Gross Weight (Internal) 11,900 Useful Load (Internal, IFR Std. Config. ) 4,936 Maximum Gross Weight (External) 11,900 Maximum External Load 4,500 Performance Summary: Takeoff, Gross Weight lb IGE Hovering Ceiling 9,500 10,500 11,900 ISA OGE Hovering Ceiling ft 17,400 14,300 10,200 ISA + 20  °C ft 14,400 10,900 6,200 ISA 10,400 5,200 10,300 6,050 (11,890 lb @ SL) ISA ft 14,000 11,270 7,270 ft 12,120 9,000 4,990 ISA Service Ceiling (AEO) 13,800 ft ISA + 20  °C FAA Take Off and Landing Limit, WAT 2 ft ISA + 20  °C ft 19,840 18,760 16,290 (continuous OEI) ISA ft 11,450 8,850 5,400 (30 minute OEI) 3 ISA ft 12,850 10,500 7,600 4,000 ft, ISA kts 132 130 125 n mi 366 364 358 kts 126 125 122 n mi 414 410 401 kts 131 130 125 Maximum Continuous Cruise (true airspeed) Cruise at Long Range Cruise (LRC) Speed Range 4 LRC Speed (average true airspeed) Range SL, ISA 4 LRC Speed (average true airspeed) Catagory A Takeoff and Landing Ceiling 4,000 ft, ISA ft 6,000 3,400 (11,580 lb @ SL) ft 3,750 1,200 (10,800 lb @ SL) SL, ISA hr 4. 0 3. 9 3. 6 4,000 ft, ISA Endurance at Loiter Speed 4 ISA ISA + 20  °C Elevated Helipad hr 4. 3 4. 2 3. 9 Uninstalled Thermodynamic Power Engine Ratings: (100% RPM) Engine Rated Power 2 x 950 2 x 900 Standard: Pratt Whitney PT6T-3D Twin Pac Takeoff (5 minutes) SHP Max Continuous Power SHP 2 x 950 2 x 800 OEI (2-1/2 minutes) SHP 1 x 1,140 1 x 1,133 OEI (continuous) SHP 1 x 970 1 x 1,024 OEI (30 minutes) SHP 1 x 1,066 1 x 1,079 OEI (continuous) SHP 1 x 950 N/A Optional: Pratt Whitney PT6T-3DF Twin Pac Transmission Ratings (100% RPM, at mast) Takeoff (5-minute) 1,370 SHP Max Continuous Power 1,110 SHP Single Engine Limited by Power Available Fuel (usable) Type Aviation Turbine Capacity 330. 5 US Gallons Note 1 IFR Standard Configuration includes all items listed in the Standard Configuration table of this document as well as twenty-five pounds (eleven kilograms) of engine oil. Ballast is not included in the standard configuration (ballast is a function of installed equipment). Note 2 With BLR FastFin ® System. Does not apply for Catagory B, 9-passenger seat configuration. The data set forth in this document are general in nature and may vary with conditions. For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight Manual  © 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 4 4 Bell 412EP Production Specification May 2012 6/5/2012 8:37:06 PM Specification Summary (Metric Units) Weight kg Weight kg Empty Weight (IFR Std. Config. ) 1 3,159 Maximum Gross Weight (Internal) 5,398 Useful Load (Internal, IFR Std. Config. ) 2,239 Maximum Gross Weight (External) 5,398 Maximum External Load 2,041 Performance Summary: Takeoff, Gross Weight kg IGE Hovering Ceiling ISA 4,309 4,763 5,398 m 5,304 4,359 3,109 ISA + 20  °C m 4,389 3,322 1,890 ISA OGE Hovering Ceiling m 4,206 3,170 1,585 ISA + 20  °C m 3,139 1,844 (5,393 kg @ SL) ISA m 4,267 3,435 2,216 ISA + 20  °C FAA Take Off and Landing Limit, WAT 2 m 3,694 2,743 1,521 Service Ceiling (AEO) ISA m 6,047 5,718 4,919 (continuous OEI) ISA m 3,490 2,697 1,646 ISA m 3,917 3,200 2,316 1,219 m, ISA km/h 244 241 232 km 678 674 663 (30 minute OEI) 3 Maximum Continuous Cruise (true airspeed) Cruise at Long Range Cruise (LRC) Speed Range 4 LRC Speed (average true airspeed) Range 4 LRC Speed (average true airspeed) SL, ISA 1,219 m, ISA km/h 233 232 226 km 767 757 743 243 241 232 m 1,829 1,036 (5,253 kg @ SL) m 1,143 366 (4,899 kg @ SL) SL, ISA hr 4. 0 3. 9 3. 6 1,219 m, ISA Elevated Helipad Endurance at Loiter Speed 4 km/h ISA + 20  °C Catagory A Takeoff and Landing Ceiling hr 4. 3 4. 2 3. 9 ISA Uninstalled Thermodynamic Power Engine Ratings: (100% RPM) Engine Rated Power Standard: Pratt Whitney PT6T-3D Twin Pac Takeoff (5 minutes) kW 2 x 708 2 x 671 Max Continuous Power kW 2 x 708 2 x 597 OEI (2-1/2 minutes) kW 1 x 850 1 x 845 OEI (continuous) kW 1 x 723 1 x 764 OEI (30 minutes) kW 1 x 795 1 x 805 OEI (continuous) kW 1 x 708 N/A Optional: Pratt Whitney PT6T-3DF Twin Pac Transmission Ratings (100% RPM, at mast) Takeoff (5-minute) 1,022 kW Max Continuous Power 828 kW Single Engine Limited by Power Available Fuel (usable) Type Aviation Turbine Capacity 1,251 liters Note 3 Increased capability available with optional Pratt Whitney PT6T-3DF (30 minute OEI Power Kit). Note 4 Standard fuel, no reserve. The data set forth in this document are general in nature and may vary with conditions. For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight Manual Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 5 5  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:06 PM BLR Strake and FastFin ® Bell Helicopter has partnered with BLR Aerospace to provide its performance, safety and efficiency-enhancing FastFin ® system as a standard feature on new Bell 412EP aircraft orders. The system incorporates two parallel stall strips along the tail boom and a reshaped vertical fin. These modifications combine to optimize airflow around the tail boom, improving the handling, stability and lifting capacity of the Bell 412EP in all environments, especially high and hot conditions. The FastFin ® system is a combination of two separate modifications, one to the vertical fin and the other to the tailboom. For clarity, the term FastFin ® refers to the BLR modification that changes the shape and contour of the vertical fin. The term FastFin ® System refers to the combined FastFin ® and Dual Tail Boom Strake installation. The performance benefits of this system include increased tail rotor effectiveness and higher crosswind speed tolerance at hover in certain conditions. In conditions where the aircraft is currently tail rotor limited the FastFin ® System results in increased Weight-Altitude-Temperature (WAT) capability for takeoff, landing and in-ground-effect maneuvers, providing substantial improvement in useful load for hot/high operation (See performance chart below). 14,000 Be ll 41 M 2EP ax G wit Be ro h ss Fa ll 41 W stF 2E ei in gh TM P M tL S ax im ys G it tem ro ss W ei gh tL im it 12,000 Density Altitude (feet) 10000 8,000 6,000 4,000 2,000 0 8,000 9,000 10,000 Gross Weight (lb) 11,000 12,000 Bell 412EP WAT Improvement with FastFin ® System The data set forth in this document are general in nature and may vary with conditions. For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight Manual  © 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 6 6 Bell 412EP Production Specification May 2012 6/5/2012 8:37:06 PM Page Intentionally Left Blank Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 7 7  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:06 PM External Dimensions LOW SKID GEAR Bell 412EP Low Skid Gear OPTIONAL HIGH SKID GEAR WITH AAI FLITESTEP ® Bell 412EP High Skid Gear Specifications subject to change without notice.  © 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 8 8 Bell 412EP Production Specification May 2012 6/5/2012 8:37:08 PM OPTIONAL EMERGENCY FLOAT GEAR WITH AAI FLOATSTEPâ„ ¢ Bell 412EP Float Kit OPTIONAL BLADE FOLDING KIT DIMENSIONS Minimum Hanger Size* Rotor Not Folded 33. 0 ft x 49. 6 ft (10. 1 m x 15. 2 m) Minimum Hanger Size* Rotor Folded 9. 5 ft x 55. 8 ft (2. 9 m x 17. 1 m) *Allowance should be made for high skid gear, ground wheels, emply fuel condition and door lip when considering hangar door width and height Specifications subject to change without notice. Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 9 9  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Bell 412EP Seating and Interior Trim Choices Crew Seats Two individual energy attenuating seats, fore/aft and up/down adjustable, each equipped with seat belt, double strap shoulder harness and inertia reel. Available with Grey, Blue, Red, or Tan upholstery which will match that selected for the cabin. Passenger Seats 13 seats offered in three options. (NOTE: Seating option 1 meets the criteria required by FAA regulations for installation in U. S. registered helicopters. Seating Options 2 3 require the addition of the STC Alpine 412 Passenger Shoulder Harness Kit for installation in U. S. registered helicopters. ) 1) Standard Seating Fabric covered high-backed folding seats with individual seat belts and single strap shoulder harness and inertia reel, arranged with one row of four (two 2-place benches) forward facing seats, and one row of five forward facing seats, and two outward facing two place benches (one on either side of the transmission). Available with Grey, Blue, Red, or Tan upholstery with Black seat belts. Seats are are also available in all vinyl at additional cost. (210. lb [95. 7 kg] included in the standard configuration weight. ) STANDARD SEATING (Shown with standard interior trim and floor covering) SEATING OPTIONS 2 AND 3 NOT ILLUSTRATED 2) Utility Seating Available for U. S. registered helicopters ONLY with addition of STC Alpine 412 Passenger Shoulder Harness Kit. Nylon covered bench type seating arranged with one row of four rearward facing seats (behind the crew seats), one row of five forward facing seats (in front of the transmission), and two outward facing two place benches (one on either side of the transmission). Each seat has an individual seat belt. Available in Tan or Black. The Utility Seating decreases the standard configuration weight (-93. 3 lb [-42. 3 kg], with Alpine Shoulder Harness -59. 5 lb [-27. 0 kg]). 3) Cushioned Utility Seating Available for U. S. registered helicopters ONLY with addition of STC Alpine 412 Passenger Shoulder Harness Kit. As in 2) above with the addition of fabric covered cushions, available in the same colors as the Standard Seating. The Cushioned Utility Seating decreases the standard configuration weight (-81. 1 lb [-36. 8 kg], with Alpine Shoulder Harness -47. 3 lb [-21. 5 kg]). Specifications subject to change without notice.  © 2012 Bell Helicopter Textron Inc. 12EP Product Spec 2012-02. indd 10 10 Bell 412EP Production Specification May 2012 6/5/2012 8:37:10 PM INTERIOR TRIM CHOICES 1) Standard Interior Trim The Standard Interior Trim is provided as a NO COST OPTION, but is not included in the Standard Configuration Empty Weight. Included are: Plastic closeouts on upper sidewalls, window reveals, and cabin headlin er; Padded vinyl covering the floor and lower door panels; Lower aft bulkhead covered with padded vinyl blankets. The hard plastic headliner and closeouts are off-white in color, and the padded bulkhead blankets and floor covering are color coordinated to match the seat color selection. The Standard Interior Trim increases the standard configuration empty weight (165. 7 lb [75. 2 kg]). 2) Utility Interior Trim The Utility Interior Trim consists of: Light beige vinyl covered headliner and bulkhead blankets; Doors painted light beige; Floor painted brown. The Utility Interior Trim is included in the standard configuration empty weight (33. 3 lb [15. 1 kg]). CUSTOMIZED SEATING [Example] Customized Seating Custom designed interiors are available from aircraft completion centers to meet the needs of Corporate or Emergency Medical Service customers. Specifications subject to change without notice. Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 11 11  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Standard Configuration (Items Included In List Price) AIRFRAME TRANSMISSION/ DRIVE SYSTEM Aluminum alloy fuselage (over 240 ft3 [6. 8M3]) loading space Glass windshields Main rotor transmission with 4 chip detectors/2 debris collectors Tinted overhead windows Vibration isolation / suspension mounts (4) Dual windshield wipers Main Lift link (single point suspension) Fresh air ventilators with adjustable outlets (8 cockpit and 12 aft cabin) 42? gearbox (sight gage and magnetic drain plug/chip detector) Bleed air heater and defroster with air noise suppression 90? gearbox (sight gage and magnetic drain plug/chip detector) Cargo tie-down fittings (51 aft cabin floor) Hydraulic pumps for controls (2 independent systems) Map and data case Transmission oil cooler Cabin fire extinguisher (2) Swingout jettisonable doors (2 for forward cabin) POWER PLANT Sliding doors (2 for aft cabin access with 2 emergency exit panels on each door) Automatic governors (2) Pratt Whitney of Canada PT6T-3D â€Å"Twin Pac† (1800 SHP) Swingout panels for extended access to aft cabin (2) Magnetic chip detectors Fixed step on skids for entry to forward cabin (2) Torque limiter Fuel System (330. 5 US Gal [1251 liter] usable, rupture resistant cells and breakaway vent fitting) Retractable steps for aft cabin access (2) Baggage compartment in tail boom (over 28 ft [0. 8M ], 400 lb [181kg] capacity). 3 3 Pumps on engines and submerged in fuel tanks Skid-type landing gear with replaceable wear shoes Fuel filter assembly Mooring and jacking fittings (4) Oil coolers (2) External attachment fittings (16) Fire detection system (2) Semi-monocoque tailboom Fire extinguisher system (2) BLR Strake and FastFin RPM warning system  ® Elevator (airspeed / spring-cartridge controlled) Hinged cowling Tail skid Starter-generators (2) Cargo hook provisions Power turbine RPM control actuators AUDIO Combining gearbox with chip detector Two station aft intercom system w/crew interface Separate firewall protection for each engine ROTORS CONTROLS Overriding clutches (2) Soft-in-plane flex beam hub with four fiberglass blades Extended Engine Exhaust Deflectors Main rotor droop restraint COMMUNICATIONS NAVIGATION Pendulum vibration absorbers 720 Channel VHF rec/trans transceiver (KTR-908) Semi-rigid, two bladed all-metal tail rotor VHF antenna All controls hydraulically boosted (dual systems for main rotor) 2 Headsets (pilot copilot) Force trim system and artificial feel (electrically set) 2 Intercomunication Panels (ICS) (pilot copilot) Dual controls Emergency Transmit Switch Cyclic stick centering Horizontal Situation Indicator RPM governor selector control Attitude Director Indicator Manual engine torque matching and trim Attitude and Heading Reference Systems (2) Dual Digital Three axis AFCS (2 flight control computers) Cockpit voice recorder provisions Rotor brake Specifications subject to change without notice.  © 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 12 12 Bell 412EP Production Specification May 2012 6/5/2012 8:37:10 PM Standard Configuration (continued) FLIGHT ENGINE INSTRUMENTS FLIGHT ENGINE INSTRUMENTS (continued) Flight Director Nav Coupler (3-axis) Master warning lights on the instrument panel draw attention to: Free air temperature indicator RPM Pitot static system with electric pitot heat Eng 2 Out Eng 2 Fire Eng 1 Out AL-300 Data Display Eng 1 Fire Baggage Fire Cyclic Radar altimeter #1 Over torque centering Altimeter (barometric) (mast) IFR EQUIPMENT Clock, digital quartz chronometer Co-pilot clock Hourmeter Distance Measuring Equipment (DME) (KDM-706) Magnetic compass, pilot’s standby IFR FAA kit Airspeed indicator Automatic Direction Finder (ADF) (XDF-806) Rate of climb indicator Nav receiver #1 VOR/LOC with HB/HSI (KNR-634) Turn and slip indicator Nav receiver #2 VOR/LOC with HSI (KNR-634) Triple tachometer (rotor and engines) VHF-AM Comm #2 radio (KTR-908) Dual hydraulic press/temp indicator (2) Transponder (MST67) Gas producer tach indicator (2) Co-pilot instruments (FAA) Triple torque indicator (Eng 1, Eng 2, mast) Standby attitude indicator Engine oil-temp/press indicator (2) ELECTRICAL Turbine inlet temperature indicator (2) Generator (2) (30 volt, 200 ampere DC startergenerator derated to 150 amperes) Fuel pressure indicator Transmission oil-temp/press indicator Inverters (2), (450 volt ampere single phase, solid state) Dual DC and AC voltmeters Nickel cadmium battery (40 ampere hours) Dual DC loadmeter Battery over-temp warning Fire detection warning (3) Generator voltage regulators Combining gearbox oil-temp/press indicator Instrument (integral) lights (white) Flight data recorder provisions Navigation lights Caution Warning System Master caution light on panel draws attention to the pedestal mounted annunciator panel when worded segments illuminate: Landing light-retractable Anticollision light (2) Engine oil press (2) DC generator (2) Tritium lighted emergency exit signs Trans oil press Gen overheat (2) Cockpit lights (2) Trans oil temp AC inverter (2) Dome lights (3) Comb box oil press External power External power receptacle Comb box oil temp Battery switch Twin ignition and starting systems Chip detectors (5) Battery temp Seat belt sign Fuel boost (2) Hydraulic Passenger step lights Fuel filter (2) Door locks Baggage compartment light fire sensor Fuel valve (2) Heater Utility cabin lights (removable) Fuel low (2) Part sep off (2) Fuel X feed Rotor brake (2) PAINT Emerg gov manual (2) Caution panel Markings for high visibility M/R blades (white orange) Specifications subject to change without notice. Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 13 13  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Standard Configuration (continued) MISCELLANEOUS Covers, tail pipe, turbine air inlet, and pitot tube Flight bag Ground handling wheels, hydraulically activated Manuals: Aircraft log, Engine log, Engine operations, Flight, Maintenance Overhaul Manual, Illustrated Parts Catalog Tie-down assemblies, main rotor tail rotor INTERIOR TRIM Choice of Standard or Utility Interior Trim. Standard; Rigid three-piece headliner in cabin, padded iberglass floor covering, bulkheads, trimmed with cream-colored plastic and color-coordinated vinyl coated fiberglass, cabin doors trimmed with plastic, special soundproofing, seat upholstered with foam and fabric. Selection of fabric colors. Not included in Standard Configuration Weight, increases empty weight 165. 6 pounds (75. 1 kilograms) when installed. Utility; Be ige soundproofing blankets on bulkheads and overhead; doors painted beige, floor painted brown. Included in Standard Configuration Weight (approximately 32. 6 pounds, 914. 8 kilograms). Specifications subject to change without notice. 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 14 14 Bell 412EP Production Specification May 2012 6/5/2012 8:37:10 PM Page Intentionally Left Blank Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 15 15  © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Optional Accessories [Kits listed below are compatible with the FAA IFR 3-axis / non-EFIS configuration except as individually noted] Additional kits and STC items may be available for factory installation. Please consult sales or contract personnel regarding special needs prior to selection of final configuration. Wt (lb) Wt (kg) Notes 11. 7 5. 3 1, 2 FIXED STEP RIGHT HAND 11. 6 5. 3 1, 2 HEAVY DUTY HIGH SKID GEAR w/o STEPS 18. 5 8. 4 1, 3 HEAVY DUTY HIGH CROSS TUBES FOR EMER. FLOATS 3. 8 1. 7 EMERGENCY FLOATS (provisions) 51. 0 23. 2 EMERGENCY FLOATS /RESERVOIR NOSE 97. 5 44. 2 4 EMERGENCY FLOATS (L. G. w/ FLOATS PWR STEPS) 168. 8 76. 6 1, 4 HEATED WINDSHIELD 9. 8 4. 4 1 EXPANDABLE BOLTS MAIN ROTOR 3. 0 1. 4 FUEL KIT MANIFOLD DRAIN 0. 3 0. 1 Kit Description AIRFRAME FIXED STEP LEFT HAND 9 CELL FUEL SYS 4 -16. 1 -7. 3 SEAT BELT SIGN STD INTR 0. 3 0. 1 SEAT BELT SIGN DLX INTR 0. 3 0. 1 AUX FUEL PROVS 5. 4 . 5 5 AUX FUEL, 16. 3 GAL LH 20. 2 9. 1 5 AUX FUEL, 16. 3 GAL RH 20. 2 9. 1 5 AUX FUEL, 81. 7 GAL LH (REQUIRES REMOVAL OF 2 OUTBOARD-FACING PAX SEATS) 50. 3 22. 8 5 AUX FUEL, 81. 7 GAL RH (REQUIRES REMOVAL OF 2 OUTBOARD-FACING PAX SEATS) 50. 3 22. 8 5 5 INDICATOR, FUEL QTY, AUX FUEL -0. 1 0. 0 TOLERANT FUEL 98. 5 44. 7 EFIS (ELECTRONIC FLIGHT INSTRUMENT SYSTEM) 113. 4 51. 4 1, 6 4-AXIS D DAFCS W/ DUAL FLIGHT DIRECTOR 26. 4 12. 0 7 PRIMUS 700 WEATHER RADAR 49. 1 22. 3 7 PRIMUS 700 WEATHER RADAR W/ EFIS 54. 6 24. 8 7 ENCODING ALTIMETER 0. 1 0. 0 1, 7 RADAR ALTIMETER #2 12. 2 5. 6 7 CABIN PA SYSTEM (NON-EFIS)

South Africa Apartheid History Essay Example | Topics and Well Written Essays - 1250 words - 1

South Africa Apartheid History - Essay Example Apartheid (1948-1994) cannot be considered as ‘the best solution’ for the country because it violated human rights and freedoms of black populations and caused separation between white minority and black majority. Primarily, apartheid was one of the main forms of racial discrimination, separation of white minority and black majority. Social divisions in this colonial society increasingly took on a rigid racial character1. Between 1950s – 1970s white power was used to forge one of the most extreme forms of racial discrimination in the twentieth-century world. For instance, whereas the strength and size of the settler population in the United States or Australia meant that race relations were for many years relegated to the peripheries of national historiography, race was an abiding concern even in the most inward-looking settler histories of South Africa2. Apartheid cannot be the best solution for South African because this term coincides with the concepts of racism, segregation and oppression of black population. Segregation in South Africa encompassed many different social relationships. It is often discussed as a series of legislative Acts which removed and restricted the rights of ‘non-whites’ in every possible sphere. Segregation was more than a set of restrictive legislation: it refers as well to a composite ideology and set of practices seeking to legitimize social difference and economic inequality in every aspect of life3. For instance, "Coloured" was the official apartheid designation for persons of mixed raceâ€Å"4. Many of the spatial and social elements of segregation, such as the division of churches on the basis of color, were initially governed by convention rather than law. It is important to mention the exclusion of blacks from skilled work, and especially from the exercise of supervisory functions ove r whites, was determined by custom as well as legislative

EVA Calculation and comparison Essay Example | Topics and Well Written Essays - 750 words

EVA Calculation and comparison - Essay Example The chart below indicates that Walgreens EVA scores have been on the rise in the past three years. CVS' EVA scores have been falling and indicate that CVS needs to examine its resource utilization methods and decide what to do turn its scores around. The goal of any organization is to lower its costs while increasing profitability. There are many methods organizations can use. In the three year window examined (2004, 2005, 2006). Initially Walgreens' total assets were slightly higher than CVS'. Then CVSs were reported as slightly higher than Walgreens. Walgreens consistently outspends CVS for cost of goods sold. The higher the cost of goods sold the lower the profits. But, Walgreens consistently reports 10% on ROA (return on assets). CVS reports between 6.3% and 8% ROA. Walgreens has a bigger share of the market and consistently outperforms CVS. But, the difference is not so big that n any one year CVS could come out on top. The current earnings are so close that a good year could put CVS ahead. Both pharmacies could benefit from strategies to differentiate them in the market and draw in a greater share of the market in pharmacy sales. Walgreens has begun doing so by advertising itself as "your pharmacy" and "there's my pharmacy next to work""there's my pharmacy close to home"(TV commercials). .. Sales $37,006,200 Cash $513,400 N/P $774,200 COGS $27,105,000 A/R $2,080,700 A/P $3,988,900 Gross $9,901,200 Inventory $5,719,800 Accrd Exp $59,500 Prepaids $78,800 SG&A $7,881,700 TTL Cur $8,392,700 TTL Cur $4,822,600 EBIT $2,019,500 PP&E $3,952,600 LTD $1,594,100 Interest $110,500 GoodWill $1,789,900 TTL Liabilities $6,416,700 EBT $1,909,000 intangible $802,200 Other Assets $223,500 Equity $535,500 33.96% Tax $648,300 LTA Charges $122,500 EAT $1,260,700 TTL Assets $15,283,400 TTL Liab & Equity $6,952,200 ROA 8.20% ROE 235.40% Debt $2,368,300 0.8200 0.01 0.82% equity $535,500 0.1800 1.4894 26.81% $2,903,800 27.63% 18.25% EVA -10.05% Table 2 Table 3 31-Dec-03 Assets Liabilities & Equity Sales $26,588,000 Cash $843,200 N/P $3,166,000 COGS $26,588,000 A/R $1,601,700 A/P 0 Gross $26,588,000 Inventory $4,016,500 Accrd Exp $323,200 Prepaids $35,100 SG&A $5,439,400 TTL Cur $6,496,500 TTL Cur $3,489,200 EBIT $1,423,600 PP&E $2,542,100 LTD $1,032,100 Interest $48,100 GoodWill $889,000 TTL Liabilities $4,521,300 EBT $1,375,500 Intangible $403,700 Other Assets $211,800 Equity $207,800 38.40% Tax $528,200 LTA Charges 0 EAT $847,300 TTL Assets $10,543,100 TTL Liab & Equity $4,729,100 ROA 8.00% ROE 407.70% Debt $4,198,100 0.9500 0.010639 1.01% equity $207,800 0.0500 0.3538 1.77% $4,405,900 2.78% 1.71% EVA 6.29% Works Cited: Ecoach. EVA. Retrieved 2007-02-09

Essay example --

The First Silesian War The First Silesian War inaugurated, and is generally seen in the context of, the wider ranging War of the Austrian Succession. It owed its origins to the Pragmatic Sanction of 19 April 1713 whereby the Habsburg emperor Charles VI decreed the imperial succession arrangements as set out in his will, according precedence to his own daughters over the daughters of his (by now deceased) elder brother Joseph I. This proved prescient: in May 1717 the emperor’s own eldest daughter was born and on his death in 1740, she duly succeeded as Archduchess of Austria as well as to the thrones of the Bohemian and Hungarian lands within the Habsburg Monarchy as Queen Maria Theresa. During the emperor’s lifetime the Pragmatic Sanction was generally acknowledged by the Imperial States; however, upon his death it was promptly contested both by the Hohenzollern scion Frederick II, who had just ascended the throne of the King in Prussia, and by the Wittelsbach elector Charles Albert of Bavaria. While Charles launched a claim to the Imperial throne and the Habsburg territories, King Frederick II aimed at the annexation of the Silesia, a Bohemian crown land since 1526. Frederick based his demands on a 1537 inheritance treaty of the Silesian duke Frederick II of Legnica with the Hohenzollern elector Joachim II of Brandenburg, whereby the Silesian duchies of Legnica, WoÅ‚Ã ³w, and Brzeg were to pass to the Electorate of Brandenburg on the extinction of the Silesian Piasts. The Bohemian king Ferdinand of Habsburg, aware of the Hohenzollern ambitions, had immediately rejected the agreement; nevertheless, in 1675 the "Great Elector" Frederick William of Brandenburg raised claim to the principalities, when with the death of Duke George Will... ...ides, and in this war, they supported Prussia against their former allies the Austrians. After battles in 1761–1762 went well for Russian and Austrian forces, in January 1763 Russia had suddenly abandoned Austria after the rise of Peter III who recalled his army from within Berlin and Pomerania upon the death of Queen Elizabeth of Russia Peter was soon assassinated and Catherine the Great succeeded him and could once again bring Russia into an alliance. Peace talks that were already in progress, war had ended in February 1763. worse for Austria, Peter had mediated an agreement between Prussia and Sweden, allowing Frederick II's forces to consolidate his position and bolster Prussia's claims in January and February. All these events were against Austria's interests. Consequently, Prussia was then confirmed with her Silesian possessions in the Treaty of Hubertusburg.

Toilet Facilities in All Schools

Toilet Facilities in All Schools ——————————————————————————– Toilet Facilities in All Schools Encourage and contribute to developing the necessary partnership between the state of Maharashtra and the Government of India’s programmes to establish toilet facilities in all schools. The Indian government has launched a focused campaign to increase the households in the country that have toilets by 2010. Additionally, we will target the urgent need for separate toilets for boys and girls, together with a hand-washing facility in every school in Maharashtra. Name: Toilet Facilities in all Schools Status: Theme: Region and Country: Maharashtra, India Partners: Beneficiaries: Funding Need: Budget: Duration: Contact: Programme Activities: Each year two million children die from diarrhoeal diseases, making it the second most serious killer of children under the age of five. The main source of diarrhoeal infection is human excreta. It seems clear therefore, that human excreta should be managed as a potentially dangerous material. The construction of latrines is a relatively simple technology that may be used to control the spread of infectious diseases. Studies have shown that latrine coverage has to reach 90% of a population to have an impact on community health. In Maharashtra, 85% of rural households and 54% of all households have no access at all to a toilet facility. While the Indian government is making great strides in the availability of toilets, this programme looks to increase advocacy and education necessary to convince people to use the toilets, and to create separate male and female toilets in schools together with hand-washing facilities. It is important to gain political support and government commitment to the programme. A mix of mass media and interpersonal communication is the best way to deliver the key programme messages. Demonstration sites for the selected technologies are important, as is the training of local people in operation and maintenance methods. It is also necessary to provide reasonable funding options and incentives to make the technology affordable. Intended Results: Latrine facilities, separate for boys and girls, with a hand-washing facility will be established in all schools. A latrine promotion programme will teach students and the local people about why and how to use the latrines through community involvement, radio messages, and other social marketing strategies. The construction of this latrine system in schools will be used to control the spread of infectious diseases, and promote toilet usage at a young age to school children to convey proper usage and knowledge at home. Programme Management and Implementation: This programme has numerous phases of implementation. Background Data: The first step is to become familiar with the local area and school systems. The acceptance of latrines varies from culture to culture and it is important to understand where the areas of potential resistance lie so as to direct promotion efforts efficiently. Conducting interviews can help to determine users likes and dislikes as well as identify current hygiene practices. This information is essential to the planning of a sanitation promotion program that will match the customs and attitudes of the users. Planning Phase: The information gathered during the background study of the local people can be used to plan a custom tailored sanitation promotion program. The initial lanning phase should consist of selection of the key messages to be promoted and a matching appropriate technology. The key messages need to be based on existing ideas, because it is much harder to introduce radical or rapid changes in a population. The core ideas should be kept simple and to the point. It is easiest for people to grasp a few straightforward ideas, rather than a long list of suggested improvements. The type of latrine selected should be low-cost, appropriate for the geographic area, and match with existing customs of anal cleaning and defecation habits as much as possible. Once the key messages and technology have been selected a marketing approach must be developed. Recent efforts in promotion programs related to socio-cultural issues have focused on social marketing techniques. Social marketing uses the approaches of economics to advance social change. Social marketing advocates a demand driven approach to sanitation. Therefore, a successful sanitation program needs to create a demand for latrines. This is accomplished by offering affordable technology, but also by increasing the social desirability of latrines. Studies have shown that the reasons people want latrines are less for health concerns than for social status, privacy, comfort and convenience (WHO, 2000). It should therefore, be the goal of any sanitation program to foster these feelings to increase the social demand for latrines. Since social status is one of the driving factors in latrine demand, it is important to recruit prominent people and community leaders to the cause of sanitation. Sanitation promotion by these leaders will increase the acceptability of latrines (Ikin, 1994). While the role of community leaders may be important, so is the participation of the average community member. Community based efforts have been shown to be more effective than external intervention (WHO, 2000). The marketing approach must select key populations within the community to act as agents of change and use appropriate channels of communication to reach the target audience. Implementation: Implementing a latrine promotion program requires outreach and education of the masses, as well as, cost reduction strategies. It is also important to consider the interactions of any institutions involved in the project schools, government, and construction company) and the issue of sustainability. The most effective method of outreach is person-to-person visits (UNICEF, 2002). These visits are used to share hygiene and technical information, as well as encourage sanitary behaviour changes. Other methods, such as radio and television programming, discussion groups, and school curriculum' s, may be incorporated depending on the community reception of these types of media. Radio or television programming has worked well in areas with high coverage by these media. Broadcast programming is most effective when done in the native language. Discussion groups are a good way to encourage community participation in the project. They may also be a way to disperse technical information to a large population through demonstration sites. Introducing hygiene curriculum in the local schools works well in areas of high school attendance and reliable school systems. Children can act as powerful agents of change when they practice proper hygienic behaviours in the classroom and then bring these behaviours home with them (UNICEF, 2002). It is also hoped that children will retain these positive traits into adulthood. A significant factor to consider in any sanitation program is the cost to the new technology. High cost is the number one deterrent for the spread of latrine construction (Cotton, 1998). It is important to select low-cost technologies for sanitation projects in the developing world. Many sanitation promotion programs rely on the support of both the local government and NGO. Whenever there are multiple institutions working together on a project it is important to have a clear structure of goals and methods of implementation. Care must be taken not to duplicate efforts or damage the working relationship between the partner institutions. Where large institutions are involved it is helpful to establish community contacts to ensure effective communication from the field to the institute headquarters. Although the introduction of improved sanitation services may be difficult, ensuring the sustainability of these services may be even more so. The most important step towards sustainability is the involvement of the community from the start of the project. People, students, and the school must learn to take ownership and pride in their latrines. Social marketing strategies can aid in the increased acceptance and demand for latrines. School programming is also an important step towards educating the future of sanitary behaviour. Another tactic is to train local artisans to construct and maintain latrines. These artisans may build small businesses to market their skills, thus increasing the economy drive behind latrine use. Above all the program must be adaptable and flexible enough to change with the needs and demands of the people being served. Programme Monitoring and Evaluation: Programme monitoring and evaluation will occur to oversee the instalment of toilets in schools, how many children are using the toilets, and possible reasons for not using the toilets. Community attitudes will also be monitored and surveys will be conducted to see if toilet usage increases in surrounding school communities. Learning and Dissemination: Related Resources: Sanitation and hygiene promotion programs started in India in the 1980s with the support of UNICEF. The initial emphasis was on technical solutions, specifically the promotion of twin-pit pour-flush latrines. The government and UNICEF advocated the construction of these latrines as the national standard for cost-effective sanitation. However, the idea was never widely accepted and latrine coverage in rural areas remained less than 10 percent. The cost of latrine construction was considered too high and people saw little motivation for use. Between 1986-1987, UNICEF performed several micro-field studies to determine alternative methods to sanitation promotion. The results indicated that the lack of community involvement was detrimentally to the program. The studies also revealed several reasons behind people’s reluctance to use the new latrines. People avoided latrine use for fear of breaking it, or because they believed it more sanitary to defecate in the fields away from the house, or because they preferred to use the latrine as a storage facility. The high cost of the twin-pit pour-flush toilets was also often beyond the means of many poor communities. The results of these studies lead to a new approach in sanitation promotion in India in the 1990s. The new emphasis was on lower-cost latrines and sanitary behaviour changes. A community-based approach was used to promote behaviour change. Efforts were made to increase household visits, school programming and considerations for gender issues. Sanitation issues were linked with other health concerns in an attempt to increase motivation for latrine usage. A program evaluation in the mid 1990s indicated that person-to-person visited could be highly effective, but that 3-4 visits were required for every latrine installed. The labour costs associated with this method of promotion are therefore quite high. School programs were developed to teach children hygienic behaviours, including the use of a latrine. The hope is that the children will than bring these behaviours home with them, thereby acting as agents of change in their communities. The new promotion plan also stressed the role of women in sanitation and household hygiene management. Lack of proper sanitation facilities has traditionally been more detrimental to women than to men. Due to the lack of privacy, many women may wait until nightfall to relieve themselves, leading to serious health problems and kidney failure. The lack of sanitation facilities has also been a barrier to girls attending school. The restructuring of the sanitation promotion program has attempted to address these issues by including women in health discussions and the operation and maintenance of the new latrines. The key to sanitation promotion in India has been balancing the technical and social aspects of sanitation services. Since the introduction of community based promotion methods, rural India has seen sanitation coverage increase from nearly zero to 14% while total sanitation coverage increased to 31%. Community involvement and self-financing methods lead to the construction of more than 350,000 latrines in one county alone. An impact evaluation in 1999 showed consistently better excreta disposal practices in communities participating in the promotion programs. The study indicated that future sanitation promotion efforts should focus on social marketing techniques and community management of latrines.

The Great Gatsby By F. Scott Fitzgerald - 850 Words

A perfect world may be where there is money, a perfect, house, a wonderful spouse, beautiful and smart kids. The perfect lifestyle may only include having a job you’ve always wanted, or something simple as retaining the freedom given when entering the country. Ellen Truax was someone who saw the way people envisioned the American Dream, and those who couldn’t achieve it. She proposed an act called DREAM Act, which stands for Development, Relief, and Education for Alien Minors. By this proposal she sought to give those who have been through tragic events such as deportation, a change to recreate themselves, a chance to give themselves a better life; the American Dream. (Stockwell, Diane, trans. Dreamers: An Immigrant Generation’s Fight For Their American Dream.† Publisher Weekly (2014): 59-60. Literary Reference Center. Web. 8 Apr. 2015.) The writer F. Scott Fitzgerald is well known for his book The Great Gatsby that was written in 1926. Fitzgerald had ways of achieving the American Dream, but fell short before the reward. He struggled in college which led him to the enlistment of WWI. Fitzgerald never went to combat and believes it to be one of his greatest regrets. AFter getting out of the war, he met the most beautiful â€Å"southern bell† named Zelda. Zelda came from a lot of money, which made her father very skeptical who she chose to date. (F Scott Fitzgerald The Great American Dreamer Part 1. Adapt. Dorian Grayantiques. Perf. F. Scott Fitzgerald. YouTube, 2013.Show MoreRelatedThe Great Gatsby by F. Scott Fitzgerald1393 Words   |  6 PagesF. Scott Fitzgerald was the model of the American image in the nineteen twenties. He had wealth, fame, a beautiful wife, and an adorable daughter; all seemed perfect. Beneath the gilded faà §ade, however, was an author who struggled with domestic and physical difficu lties that plagued his personal life and career throughout its short span. This author helped to launch the theme that is so prevalent in his work; the human instinct to yearn for more, into the forefront of American literature, where itRead MoreThe Great Gatsby By F. Scott Fitzgerald1343 Words   |  6 PagesHonors English 10 Shugart 18 Decemeber 2014 The Great Gatsby F. Scott Fitzgerald s 1925 novel The Great Gatsby is a tragic love story, a mystery, and a social commentary on American life. The Great Gatsby is about the lives of four wealthy characters observed by the narrator, Nick Carroway. Throughout the novel a mysterious man named Jay Gatsby throws immaculate parties every Saturday night in hope to impress his lost lover, Daisy Buchanan. Gatsby lives in a mansion on West Egg across from DaisyRead MoreThe Great Gatsby By F. Scott Fitzgerald1155 Words   |  5 PagesThe Great Gatsby The Jazz Age was an era where everything and anything seemed possible. It started with the beginning of a new age with America coming out of World War I as the most powerful nation in the world (Novel reflections on, 2007). As a result, the nation soon faced a culture-shock of material prosperity during the 1920’s. Also known as the â€Å"roaring twenties†, it was a time where life consisted of prodigality and extravagant parties. Writing based on his personal experiences, author F. ScottRead MoreThe Great Gatsby By F. Scott Fitzgerald1166 Words   |  5 Pagesin the Haze F. Scott Fitzgerald lived in a time that was characterized by an unbelievable lack of substance. After the tragedy and horrors of WWI, people were focused on anything that they could that would distract from the emptiness that had swallowed them. Tangible greed tied with extreme materialism left many, by the end of this time period, disenchanted. The usage of the literary theories of both Biographical and Historical lenses provide a unique interpretation of the Great Gatsby centered aroundRead MoreThe Great Gatsby by F. Scott Fitzgerald845 Words   |  3 PagesIn F. Scott Fitzgerald’s novel, The Great Gatsby, colors represent a variety of symbols that relate back to the American Dream. The dream of being pure, innocent and perfect is frequently associated with the reality of corruption, violence, and affairs. Gatsby’s desire for achieving the American Dream is sought for through corruption (Schneider). The American Dream in the 1920s was perceived as a desire of w ealth and social standings. Social class is represented through the East Egg, the WestRead MoreThe Great Gatsby By F. Scott Fitzgerald Essay970 Words   |  4 Pagesrespecting and valuing Fitzgerald work in the twenty-first century? Fitzgerald had a hard time to profiting from his writing, but he was not successful after his first novel. There are three major point of this essay are: the background history of Fitzgerald life, the comparisons between Fitzgerald and the Gatsby from his number one book in America The Great Gatsby, and the Fitzgerald got influences of behind the writing and being a writer. From childhood to adulthood, Fitzgerald faced many good andRead MoreThe Great Gatsby By F. Scott Fitzgerald2099 Words   |  9 Pagesauthor to mirror his life in his book. In his previous novels F. Scott Fitzgerald drew from his life experiences. He said that his next novel, The Great Gatsby, would be different. He said, â€Å"In my new novel I’m thrown directly on purely creative work† (F. Scott Fitzgerald). He did not realize or did not want it to appear that he was taking his own story and intertwining it within his new novel. In The Great Gatsby, by F. Scott Fitzgerald, he imitates his lifestyle through the Buchanan family to demonstrateRead MoreThe Great Gatsby By F. Scott Fitzgerald1607 Words   |  7 Pages The Great Gatsby is an American novel written in 1925 by F. Scott Fitzgerald. One of the themes of the book is the American Dream. The American Dream is an idea in which Americans believe through hard work they can achieve success and prosperity in the free world. In F. Scott Fitzgerald s novel, The Great Gatsby, the American Dream leads to popularity, extreme jealousy and false happiness. Jay Gatsby’s recent fortune and wealthiness helped him earn a high social position and become one of the mostRead MoreThe Great Gatsby By F. Scott Fitzgerald1592 Words   |  7 PagesMcGowan English 11A, Period 4 9 January 2014 The Great Gatsby Individuals who approach life with an optimistic mindset generally have their goals established as their main priority. Driven by ambition, they are determined to fulfill their desires; without reluctance. These strong-minded individuals refuse to be influenced by negative reinforcements, and rely on hope in order to achieve their dreams. As a man of persistence, the wealthy Jay Gatsby continuously strives to reclaim the love of hisRead MoreThe Great Gatsby By F. Scott Fitzgerald1646 Words   |  7 PagesThe 1920s witnessed the death of the American Dream, a message immortalized in F. Scott Fitzgerald’s The Great Gatsby. Initially, the American Dream represented the outcome of American ideals, that everyone has the freedom and opportunity to achieve their dreams provided they perform honest hard work. During the 1920s, the United States experienced massive economic prosperity making the American Dream seem alive and strong. However, in Fitzgerald’s eyes, the new Am erican culture build around that