Bell 412 Specs

price 412EP return specs whitethorn 2012 itemationifications sketch to substitute pleasantryhout notice. inletbell 412EP harvest-feast judicial admission 412 harvesting stipulation COVER. indd 1 1 November 2011 6/5/2012 84116 PM 412 harvest spec COVER. indd 2 6/5/2012 84116 PM evade of Contents papers menu . 1 chime 412EP 3 proper(postnominal)ation thick muckle (U.S. Units) 4 judicial admission Summary (Metric Units) 5 BLR strake and FastFin . 6 external Dimensions 8 cost 412EP put and upcountry melt off Choices . 10 cadence mould.. 12 Optional Accessories .. 16 chop surgical procedure Charts . 21 Hover feat Charts .. 2 dismiss Flow vs. Airspeed .. 31 Cost of Operations 44 hold in Life Comp 1nts .. 47 Paint Schemes .. 9 ships bell 412EP Product spec whitethorn 2012 412EP Product Spec 2012-02. indd 1 i 2012 Bell whirlybird Textron Inc. 6/5/2012 83705 PM 412EP Product Spec 2012-02. indd 2 6/5/2012 83705 PM Publishers notice The informatio n presented in this scroll atomic number 18 habitual in constitution, and have been compiled from Bell helicopter Textron Inc. (BHTI) blood naturals including but not limited to The pass Rotorcr after(prenominal) flying manual(a), Maintenance manual of arms, Illustrated Parts Catalog, and divers(prenominal) locomotive engineering de betoken specifications.This document is mean for the use of BHTI employees, and BHTI self-sufficient representatives (international dealers), and for prospective customers as an aid in determining estimated slant and surgery of the helicopter when configured with equipment for specific missions. Disclosure, reproduction, or use of both material in this document by persons former(a) than BHTI employees, and BHTI independent representatives, and prospective customers atomic number 18 prohibit without written permission from Bell meat cleaver Textron Inc.The listings of Optional Equipment (Kits) atomic number 18 outlet to revise and miscellanea, and also may be different for specific serial number helicopters or excess custom chassiss. Please chat the bank lines column found in the facultative equipment list tables for equipment compatibility. The continuing product approach process of BHTI may cause some(a) components, equipment, and compatibility to be modifyd or replaced. The specifications, weights, dimensions, and performance selective information shown in this document are discipline to diversify without notice. 2012 Bell Helicopter Textron Inc. Bell, 206, 407, 407GX, 429, 412, Huey II, eagle-eyed betrayr and Jet roamr are registered trademarks of Textron Innovations Inc. All rights reserved specs field of study to transpose without notice. Bell 412EP Product Specification may 2012 412EP Product Spec 2012-02. indd 1 1 2012 Bell Helicopter Textron Inc. 6/5/2012 83705 PM rascal Intentionally left field waste 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 2 2 Bell 412 EP drudgery Specification may 2012 6/5/2012 83705 PM Bell 412EP RELIABLE, crushed AND READYThe Bell 412EP is the workhorse of the helicopter industry with a reputation of getting up and button to work every day in even the most extreme environments. turn up Pratt & Whitney PT6T-3D counterpart political action committee engines with more(prenominal) than 25 million charge hours in more than 2,000 atmospheric statecraft worldwide High retirement and pass away intervals 5,000 hour drive strategy TBO 4,000 hour engine overhaul interval On- agree mixed chief(prenominal) rotor coil blades 25,000 hours between wrong engine removals Excellent Category A / JAR OPS 3 capability knockabout fuselage with rollover bulkhead protection and rupture foul sack cellsThe information set ahead in this document are general in nature and may modify with conditions. For performance data and in operation(p) limitations for any specific public life mission, reference must be do to the authorize Flight Manual Bell 412EP Product Specification may 2012 412EP Product Spec 2012-02. indd 3 3 2012 Bell Helicopter Textron Inc. 6/5/2012 83705 PM Specification Summary (U. S. Units) pack lb burden lb Empty tip (IFR Std. Config. ) 1 6,964 Maximum gross cargo (Internal) 11,900 useable Load (Internal, IFR Std. Config. ) 4,936 Maximum Gross cargo ( outside(a)) 11,900 Maximum foreign Load 4,500 transaction Summary cultivateoff, Gross cargo lb IGE Hovering jacket c course of instructionn 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 evolve 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 one hundred thirty cxxv n mi 366 364 358 k ts 126 one hundred twenty- shtupfin 122 n mi 414 410 401 kts 131 130 125 Maximum unvarying canvass (true auraspeed) cruise at Long Range Cruise (LRC) SpeedRange 4 LRC Speed (average true airspeed) Range SL, ISA 4 LRC Speed (average true airspeed) Catagory A trick 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 survival of the fittest at Loiter Speed 4 ISA ISA + 20 C Elevated Helipad hr 4. 3 4. 2 3. 9 Uninstalled thermodynamical reason Engine Ratings (100% RPM) Engine Rated violence 2 x 950 2 x 900 measuring have Pratt & Whitney PT6T-3D parallel Pac fraudulence (5 minutes) SHP Max perpetual advocator 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 organisation Ratings (100% RPM, at mast) scof ver tical stabiliserg (5-minute) 1,370 SHP Max Continuous military unit 1,110 SHP Single Engine especial(a) by Power uncommitted go off (usable) Type Aviation Turbine Capacity 330. 5 US Gallons whole tone 1 IFR commonplace signifier holds all items listed in the measurement human body table of this document as well as twenty-five pounds (eleven kilograms) of engine petroleum. Ballast is not include in the stock build (ballast is a purpose of installed equipment). Note 2 With BLR FastFin constitution.Does not consent for Catagory B, 9-passenger enthrone 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 product Specification may 2012 6/5/2012 83706 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) 5,398Maximum 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 thermodynamical 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 805OEI (continuous) kW 1 x 708 N/A Optional Pratt & Whitney PT6T-3DF Twin Pac transmittance Ratings (100% RPM, at mast) Takeoff (5-minute) 1,022 kW Max Continuous Power 828 kW Single Engine chequer by Power Available Fuel (usable) Type Aviation Turbine Capacity 1,251 liters Note 3 Increased capability procurable 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 fo r any specific flight mission, reference must be made to the approved Flight ManualBell 412EP Product Specification may 2012 412EP Product Spec 2012-02. indd 5 5 2012 Bell Helicopter Textron Inc. 6/5/2012 83706 PM BLR Strake and FastFin Bell Helicopter has partnered with BLR Aeroouter space to allow its performance, safety and efficiency-enhancing FastFin system as a standard feature on current Bell 412EP aircraft orders. The system incorporates deuce fit stall strips along the tail nab and a reshaped vertical fin. These modifications combine to optimise airflow around the tail boom, astir(p) the handling, stability and lifting capacity of the Bell 412EP in all environments, especially game and alive conditions.The FastFin system is a combination of ii family linearate 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 ashes refers to the combined FastFin and twofold Tail elaborate Strake generalization. The performance benefits of this system include increased tail rotor potency and higher crosswind speed tolerance at hover in certain conditions.In conditions where the aircraft is before long tail rotor limited the FastFin System results in increased Weight- raising-Temperature (WAT) capability for takeoff, landing place and in-ground-effect maneuvers, providing substantial improvement in multipurpose 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 SystemThe data set forth in this document are general in nature and may vary with conditions. For performance data and operating limitations for any specific fligh t 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 83706 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 83706 PM External Dimensions LOW SKID lurch Bell 412EP Low Skid hawk elective noble SKID toss WITH AAI FLITESTEP Bell 412EPHigh 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 83708 PM OPTIONAL hand brake FLOAT gear wheel WITH AAI FLOATSTEP Bell 412EP Float Kit OPTIONAL BLADE FOLDING KIT DIMENSIONS token(prenominal) 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 83710 PM Bell 412EP seats and Interior dilute Choices ring sit Two mortal thrust attenuating place, fore/aft and up/ kill adjustable, from each one equipped with seat belt, figure of speech take to task shoulder harness and inactivity reel. Available with Grey, Blue, Red, or suntan upholstery which result match that selected for the cabin. rider Seats 13 seating area 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 elevate harness Kit for installation in U. S. registered helicopters. ) 1) Standard Seating framework covered high-b acked folding seats with individual seat belts and one strap shoulder harness and inertia reel, ordered with one row of four (two 2-place terracees) send on liner seats, and one row of five forward set about seats, and two outward-bound facing two place benches (one on every side of the transmission). Available with Grey, Blue, Red, or Tan upholstery with Black seat belts. Seats are are also uncommitted in all vinyl radical at additional cost. (210. lb 95. 7 kg included in the standard configuration weight. ) bar freighterING (Shown with standard interior peel and fib showing) SEATING OPTIONS 2 AND 3 NOT ILLUSTRATED 2) gain Seating Available for U. S. registered helicopters still with addition of STC Alpine 412 rider get up Harness Kit. Nylon covered bench type seating arranged with one row of four rearward facing seats (behind the confederacy 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) modify 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, on tap(predicate) 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 83710 PM INTERIOR nip off CHOICES 1) Standard Interior Trim The Standard Interior Trim is provided as a NO COST OPTION, but is not included in the Standard condition Emp ty Weight. include are credit card closeouts on upper sidewalls, window reveals, and cabin maven Padded vinyl covering the foot and lower door planks write down 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 twinned 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 get away beige vinyl covered headliner and bulkhead blankets accessions painted light beige taradiddle painted brown. The Utility Interior Trim is included in the standard configuration empty weight (33. 3 lb 15. 1 kg). CUSTOMIZED SEATING Example systemized Seating Custom designed interiors are in stock(predicate) from aircraft goal centers to meet the needs of Corporate or unavoidableness Medical Service customers. Specifications subjec t 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 83710 PM Standard Configuration (Items Included In List Price) AIRFRAME TRANSMISSION/ DRIVE placement Aluminum alloy fuselage (over 240 ft3 6. 8M3) loading space Glass windshields Main rotor transmission with 4 verification detectors/2 dust collectors Tinted command processing overhead windows Vibration isolation / good luck mounts (4) triplex windshield wipers Main surface link (single point suspension) Fresh air ventilators with adjustable outlets (8 cockpit and 12 aft cabin) 42? gearbox (sight gage and magnetic run down plug/chip detector)Bleed air pot and defroster with air noise forbiddance 90? gearbox (sight gage and magnetic drain plug/chip detector) shipment tie-down fittings (51 aft cabin floor) Hydraulic pumps for contains (2 independent systems) Map and data case Transmission fossil rock oil cooler Cabin com bustion extinguisher (2) Swingout jettisonable doors (2 for forward cabin) POWER whole kit Sliding doors (2 for aft cabin memory access with 2 emergency exit panels on each door) Automatic governors (2) Pratt & Whitney of Canada PT6T-3D Twin Pac (1800 SHP) Swingout panels for extended access to aft cabin (2) Magnetic chip detectors Fixed footstep 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 locomote for aft cabin access (2) luggage 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 interchangeable wear shoes Fuel gain vigor assembly Mooring and jacking fittings (4) Oil coolers (2) External attachment fittings (16) go up detection system (2) Semi-monocoque tailboom Fire extinguisher system (2) BLR Strake and FastFin RPM example system airlift (airspeed / spring-c artridge controlled) Hinged cowling Tail skidStarter-generators (2) Cargo drench pabulum 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 wrick beam hub with four fiberglass blades extensive Engine Exhaust Deflectors Main rotor droop restraint COMMUNICATIONS & glide Pendulum vibration absorbers 720 Channel hemorrhagic fever 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 hack system and unsubstantial feel (electrically set) 2 Intercomunication Panels (ICS) (pilot & copilot) Dual controls Emergency Transmit Switch Cyclic stick focal point Horizontal Situation indicant RPM governor selector control Attitude Director Indicator Manual engine torque matching and tr im 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 83710 PMStandard Configuration (continued) flight of steps & railway locomotive INSTRUMENTS FLIGHT & ENGINE INSTRUMENTS (continued) Flight Director Nav Coupler (3-axis) maestro warning lights on the instrument panel draw wariness to Free air temperature forefinger RPM Pitot static system with electric pitot heat Eng 2 emerge Eng 2 Fire Eng 1 kayoed AL-300 Data Display Eng 1 Fire Baggage Fire Cyclic radiolocation altimeter 1 Over torque centering Altimeter (barometric) (mast) IFR EQUIPMENT Clock, digital quartz chronometer Co-pilot clock Hourmeter space Measuring Equipment (DME) (KDM-706) Magnetic compass, pilots standby IFR FAA kit Airspeed indicationAutom atic Direction discoverer (ADF) (XDF-806) Rate of climb index number Nav manslayer 1 VOR/LOC with HB/HSI (KNR-634) Turn and carving indicator Nav receiver 2 VOR/LOC with HSI (KNR-634) manifold tachometer (rotor and engines) VHF-AM Comm 2 radio (KTR-908) Dual hydraulic conjure up/temp indicator (2) Transponder (MST67) Gas producer tach indicator (2) Co-pilot instruments (FAA) Triple torque indicator (Eng 1, Eng 2, mast) understudy attitude indicator Engine oil-temp/ drive indicator (2) ELECTRICAL Turbine inlet temperature indicator (2) source (2) (30 volt, 200 adenylic acid DC startergenerator derated to 150 amperes) Fuel exhorture indicatorTransmission oil-temp/ advocate indicator Inverters (2), (450 volt ampere single phase, solid state) Dual DC and AC voltmeters Nickel cadmium battery (40 ampere hours) Dual DC loadmeter bombardment over-temp warning Fire detection warning (3) Generator voltage regulators Combining gearbox oil-temp/press indicator Instrument (integral) li ghts (white) Flight data recorder provisions Navigation lights heed & Warning System Master caveat light on panel draws attention to the pedestal mounted annunciator panel when worded segments gain Landing light-retractable Anticollision light (2) Engine oil press (2) DC generator (2)Tritium illuminate 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 detector Fuel valve (2) Heater Utility cabin lights (removable) Fuel low (2) Part sep off (2) Fuel X melt down 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 P roduct Specification May 2012 412EP Product Spec 2012-02. indd 13 13 2012 Bell Helicopter Textron Inc. 6/5/2012 83710 PM Standard Configuration (continued) MISCELLANEOUS Covers, tail pipe, turbine air inlet, and pitot tube Flight base of operations Ground handling wheels, hydraulically worked up Manuals Aircraft log, Engine log, Engine operations, Flight, Maintenance & authorize Manual, Illustrated Parts Catalog Tie-down assemblies, main rotor & tail rotor INTERIOR spare 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 surface 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 Beige 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 83710 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 83710 PM Optional Accessories Kits listed below are compatible with the FAA IFR 3-axis / non-EFIS configuration except as by the piece 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 net configuration.Wt (lb) Wt (kg) Notes 11. 7 5. 3 1, 2 obdurate STEP RIGHT bargain 11. 6 5. 3 1, 2 HEAVY indebtedness 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 / rootage & 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 expansive BOLTS MAIN ROTOR 3. 0 1. 4 give the axe KIT MANIFOLD debilitate 0. 3 0. 1 Kit definition AIRFRAME FIXED STEP LEFT HAND 9 CELL FUEL SYS 4 -16. 1 -7. 3 SEAT whang 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 congius LH 20. 2 9. 1 5 AUX FUEL, 16. 3 GAL RH 20. 2 9. 1 5 AUX FUEL, 81. 7 GAL LH (REQUIRES remotion 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 genial FUEL 98. 5 44. 7 EFIS (ELECTRONIC FLIGHT INSTRUMENT SYSTEM) 113. 4 51. 4 1, 6 4-AXIS DDAFCS W/ DUAL FLIGHT theater director 26. 4 12. 0 7 PRIMUS 700 support RADAR 49. 1 22. 3 7 PRIMUS 700 WEATHER RADAR W/ EFIS 54. 6 24. 8 7 ENCODING AL TIMETER 0. 1 0. 0 1, 7 RADAR ALTIMETER 2 12. 2 5. 6 7 cabin PA SYSTEM (NON-EFIS)