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)

Racism in America Essay Example | Topics and Well Written Essays - 750 words

Racism in America - Essay Example The quote from one of the characters named Hilly Holbrook in the book or movie ‘The Help’. His words show racism that is in Mississippi. In America, racism was once prominent but it is going down with time (Cozic and Dudley). After her return, Skeeter became uncomfortable with the way the house bits of help were treated by her friends. Her friend Hilly had a separate bathroom for the blacks her reason being that her family may get infected with the black’s diseases. Because of this, Skeeter decided to publish a book by the name ‘The Help’. At first, the maids were reluctant to share their problems with her, but they later felt that their problems could be solved. One of the maids named Aibileen shared with Skeeter after finding out that her friend had been fired because she used her bosses’ bathroom. Minny, the maid, who was sent away, also shared her story. She later finds a job in Celia’s mansion who is Johnny’s wife where she i s treated well compared to the other boss. One of the themes that are both in the book and the movie is racial injustice. This theme is more evident in the book than the movie because in the movie Skeeter takes a seat to talk to Aibileen about her idea of publishing a book. This could not have occurred in the book as there was an apparent difference between the whites and the blacks. This is manifested in the way that most blacks are the ones who are employed by the whites and they are being mistreated because of their color. Aibileen who was a dedicated house help has spent almost her life taking care of white children. Minny also is a maid and because of her outspokenness, she always gets fired. This shows that blacks are not allowed to give their views because their views are considered to be of no importance. Racism is also seen when Hilly, Minny’s boss fires her after finding out that she used their bathroom during a thunderstorm instead of using hers which is outside th e house. Hilly believes that blacks have diseases and therefore they have to use their own bathrooms. This is evident when he says, â€Å"All these houses they are building without maid’s quarters? It’s just plain dangerous. Everybody knows they carry different diseases than we do† (Stockett 8). Hilly spoils Minny’s reputation, making it difficult for her to find a job. Minny’s daughter, therefore, has to stop schooling and look for an occupation as a maid. Aibileen finds a job for Minny where she is treated better than where she was before. Skeeter later finds out that their maid Constantine was sent away because her mother did not want Constantine to be seen by other guests during a celebration. Her mother was guilty about it but they found out that Constantine died just after leaving Jackson. Aibileen was sent away after Hilly insisted that she had stolen silver from her boss Elizabeth. The second theme both in the movie and the book is class an d gender. However, it is more evident in the book than the movie because, in the book, the difference between the social classes is more intense. The whites do not share the bathroom with the blacks than in the movie where we see the maids sharing bathrooms with their bosses. This theme is prominent when we see that most ladies in the area went to the university to look for husbands.

Perpetuation of adolescence in the workplace Essay

Perpetuation of adolescence in the workplace - Essay Example In Nine to Five, the female protagonists certainly cause trouble and disrupt the office, but in a positive way, a way that is driven by a legitimate sense of injustice, and which ends up creating positive results in the office (Resnick and Higgins). There is little resemblance to the aimless, unproductive antics of the overgrown adolescent boys who comprise the rest of our examples. Even in the comparatively staid Dilbert, the random workplace shenanigans fall mostly to Dilbert and Wally, while Tina acts out of a sense of ambition and legitimate grievance. Of course, given Dilbert creator Scott Adams’ ideas about gender, he’s the last place we should look for nonstereotypical gender roles (Adams). This strict gendering is part of a cultural narrative, seen (among other places) on most sitcoms of the past 20 years, wherein men are immature wastrels with crude habits, and women are unfunny, joyless buzzkills. It is worth noting that the second-wave feminist hijinks of Nin e to Five were thirty years ago, and have not been significantly repeated. In this narrative, men must be the pranksters, and women the stern, disapproving â€Å"straight men,† like Margaret Dumont in all the Marx Brothers movies. This gendering arises partly from the cultural perception of â€Å"Peter Pan Syndrome,† so named in the 1983 book of the same name (Kiley). It describes men (and only men) who refuse to â€Å"grow up† and accept what are generally seen as adult roles and responsibilities. The role of women in their lives is to become â€Å"Wendies,† temporary surrogate mothers who enable this lifestyle. As a concept, it’s an old one; the Romans called Bacchus, eternally young god of wine and madness, the puer aeturnus, or â€Å"eternal boy.† (Kiley) Of course, all of this cultural context is really just â€Å"boys will be boys† in greater detail. There are cultural currents and narratives into which the office-adolescent con cept fits, but is that all there is to it? What if the puer aeturnus narrative is just a cover for something deeper? A closer look at some of the preeminent examples of the trope provide some interesting insights, suggesting that the gendering of the trope in narrative is just a cultural gloss on a deeper problem. Given its prevalence, an exhaustive review of examples of this narrative trope would be impossible, but it is worth examining a few in detail. The popular British sitcom The Office opens with a perfect example, as the character of Gareth is outraged to discover that his stapler, about which he is neurotically possessive, has been neatly encased in jelly. This is part of a campaign of similar pranksterism being conducted against him by Tim, the closest thing the show has to a direct protagonist. Other examples include gluing his phone headset down, sending him a series of romantic emails under the guise of an imaginary woman, and locking him in an office. Tim’s behav ior is presented partly as a semi-admirable effort to puncture Gareth’s self-important pretentions, but largely as an outlet for a directionless energy that his job does not channel into anything useful (BBC). The characters in Joshua Ferris’s Then We Came To The End face a similar problem; a job-related ennui that expresses itself in the most non-job-related activities possible. â€Å"Our boredom was ongoing, a collective boredom, and it would never

Enviromental Ethics of Cleaning up the Oceans Term Paper

Enviromental Ethics of Cleaning up the Oceans - Term Paper Example There are many reasons to affirm that all citizens of this world have ethical and moral responsibility to maintain the oceanic health, starting with the cleaning of its waters. Since, ages oceans have provided around half of the required oxygen to all living bodies on earth. Nevertheless, the detection of Dead Zones in several seas and oceans reveal that the marine life within such zones is starving for oxygen. This is mainly due to large scale dumping of agricultural and industrial waste into the oceanic waters. The exploitation of oceans has resulted in extinction of many races of sharks and other predatory fishes along with other species like turtles. Hence, it is the moral responsibility of all global citizens to gear up the efforts towards aggressive ocean cleaning. Various moral theories come up when discussing about the moral responsibility of human kind in saving the environment of this planet. However, main aspects of moral theory include the issues related to sustainability, compassion and participation. It is the duty of every citizen of world to ensure that all creatures and human beings are treated equally. The sustainability is the extension of this moral obligation, which defines the purpose of meeting the requirements of present generation, while ensuring that future generations are able to meet their needs sufficiently. It is in this context that human kind needs to understand its moral duty towards the preservation for oceanic marine life, which is one of the important supporters of human life system. If the ocean waters are not clean, the formation of dead zones will be frequent. This will deprive these waters of the vibrant marine life. We need to preserve marine life for the sake of our present and future generations. The action, which ensures that every one gets sufficient quantity of goods required to live in a

Adapting to Changes and Situational Leadership Assignment

Adapting to Changes and Situational Leadership - Assignment Example The researcher further delivered some of the insinuations, findings and study limitations of integrated leadership roles in the public subdivision. One of the strengths presented in the article is increased morale due to better communication whereby the leader needs to constantly remain aware of the needs of his followers. Pauliene (2012) argues that’s successful leaders should examine the ability of employees and communicate effectively. This can enable the leaders to lead the followers successfully; hence enabling them to perform their task effectively. Secondly, situational leaders should develop a positive and sizeable effect on the performance level of the federal agencies; hence achieving success (Fernandez, Cho and Perry, 2010). However, situation leadership creates confusion; thus it is likely to impact the work performance. Lastly, leaders might lose credibility and trustworthiness by their followers; hence poor work performance in the public sectors. One of the examples of that applies to situation leadership is an example of a director that was working in one the HR department in one of the clothes industry in U.S. The director was involved in a situation whereby he was about to leave for a holiday and his task was to be handled by an experienced assistant director. The assistant was very familiar with his responsibilities; thus he was excited to perform the task. However, instead, the director could trust the knowledge and skills of the assistant director; he decided to spend hours drafting a detailed list of work tasks for the assistant director. Therefore, in this situation, the work will be done perfectly, but the director damages a good relationship with the assistant director due to lack of trust and not being confidence towards the assistant director. Therefore, based on Hersey and Blanchard theories, the situation leadership applies to the above example of the director and his assistant. This is because situational leadership according to Hersey and  Blanchard focus on adapting managerial styles vital for meeting the distinct requirements in a given situation (Gong, Jia-Chi, and Jiing-Lih (2009).  

Australia Term Paper Example | Topics and Well Written Essays - 500 words

Australia - Term Paper Example Due to its location, the country experiences mild winter, making the winter and summer temperatures to be almost the same (Oliver, 2005). This kind of weather is what most people find enjoyable, as the cool ocean breeze that do sweep across the land compliments it. Nevertheless, there are quite a number of beautiful landscapes such as the grassland of Queensland and mountain ranges located near Proserpine. Sydney is also famous for the Handa Opera, a masterful monumental practice held during summer that is unique to this part of the world only. The opera is a combination of various activities that include fine dining and champagne, with a stunning view of sunset from the harbor and lots of entertainment under the beautiful night sky (â€Å"Handa Opera,† 2015). The fete is characterized by a fantastic music projection through concealed speakers with the Australian Opera and Ballet Orchestra sheltered below the stage. The country has a good number of beautiful sites that any visitor should strive to visit. A good example is the Grampians National Park. Located within Victoria at the official end of the Great Ocean Road, the park is home to marvelous indigenous rock art and angled sandstone ridges. The Fraser Island is another place that one should never fail to visit when in Australia. Being the largest island in the world, Fraser Island is gifted with lovely beaches, unique flora and fauna that are dominant in the surrounding rainforests, among others (â€Å"Work and travel Australia,† (2015). This country is definitely a favorite tourism destination that is worth marking in a travel diary. From the elegant Handa Opera to the beautiful sandy beaches of Fraser Island, Australia has more to offer that an individual will find

Complaint Management in Social Media - A Comparative Linguistic Essay

Complaint Management in Social Media - A Comparative Linguistic analysis between Company Websites and Facebook - Essay Example Research findings indicate that complaints are rarely responded to and usually only where the language used is complimentary to and/or helpful to the firm. Therefore, contrary to Hirschman’s theory of exit-voice, companies are not taking advantage of defensive marketing tools calculated to retain customers. Social media is defined as any online forum or site on which users may exchange information, opinions or knowledge. In other words the term social media refers to websites in which users are able to freely post to those websites. Brunty and Helenek define social media as a â€Å"social medium† which facilitates communications between users and communications between users and those who created or manage the website or page. Social media also includes a forum in which users can exchange content. Social media websites provide a variety of ways for users to communicate and include email, message boards, instant messaging, video or audio chatting. The idea is to provide a â€Å"sense of community among users†. ... In this regard, businesses are looking at various ways in which they can benefit from social media via social networking tools such as YouTube, Facebook and Twitter.3 Businesses are now entering unchartered territories in that they can now engage consumer-to-consumer discussions through various online social networking strategies. These communications are uncensored for the most part and permit the consumers to speak to one another freely about businesses and their products. Social media also provides a platform for consumers to speak directly to business management.4 From the perspective of business, the â€Å"quality of user-general content† can range from â€Å"excellent to abuse and spam.†5 Previously, consumers merely went online to explore content and information relative to a business and its products and/or services. Increasingly, consumers are adding their own content to a company’s profile, blogs or websites.6 Thus social media has the capacity to impac t a business’s reputation, sales and might even impact its success.7 This is all the more important because social media tools are increasing alongside internet users who are gathering at social network sites. For example a Pew Report demonstrates that young adults in the US between the ages of 18 and 29 have increased the use of social networks online via cellular telephones. Between 2006 and 2008 online social networking via cellular telephones, among young adults in the US increased by 10% (from 55% to 65%).8 Overall, access points to social networking via the internet have increased exponentially over the years. Globally, users engaged in social networking increased from 54% to 77% by