Bell 412 Specs

gong 412EP merchandise special(prenominal)ationifications may 2012 preconditions candid to change without notice. doorbell 412EP produce specification 412 merchandise stipulation COVER. indd 1 1 November 2011 6/5/2012 84116 PM 412 Product spec COVER. indd 2 6/5/2012 84116 PM Table of Contents Publishers nonice . 1 chime 412EP 3 precondition thick (U.S. Units) 4 condition Summary (Metric Units) 5 BLR Strake and FastFin . 6 External Dimensions 8 price 412EP position and intimate arrange Choices . 10 normal cast.. 12 Optional Accessories .. 16 whirlybird Performance Charts . 21 Hover Performance Charts .. 2 displace Flow vs. Airspeed .. 31 Cost of Operations 44 exceptional life story Components .. 47 Paint Schemes .. 9 ships bell 412EP Product condition whitethorn 2012 412EP Product stipulation 2012-02. indd 1 i 2012 gong helicopter Textron Inc. 6/5/2012 83705 PM 412EP Product Spec 2012-02. indd 2 6/5/2012 83705 PM Publishers Notice The information presented in this text file be everyday in nature, and have been compiled from Bell eggbeater Textron Inc. (BHTI) source materials including but not restrict to The Approved Rotorcr aftermost charge Manual, Maintenance Manual, Illustrated split Catalog, and other locomotive engineering pattern specifications.This document is intended for the use of BHTI employees, and BHTI independent representatives (international dealers), and for prospective customers as an concern in determining estimated cant and achievement of the meat cleaver when configured with equipment for specific missions. Disclosure, reproduction, or use of both material in this document by persons other than BHTI employees, and BHTI independent representatives, and prospective customers are forbidden without written license from Bell helicopter Textron Inc.The listings of Optional Equipment (Kits) are opened to revision and change, and in any case may be different for specific serial number helicopte rs or special custom configurations. revel consult the Notes column found in the nonobligatory 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, Long holdr 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 83705 PM Page on purpose left Blank 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 2 2 Bell 412EP payoff Specification May 2012 6/5/2012 83705 PM Bell 412EP RELIABLE, RUGGED AND READYThe Bell 412EP is the litigatehorse o f the helicopter industry with a reputation of getting up and going to work every day in even the most extreme environments. be Pratt & Whitney PT6T-3D pair off Pac engines with more than 25 million shoot hours in more than 2,000 aircraft worldwide High retirement and overhaul intervals 5,000 hour private road arrangement TBO 4,000 hour engine overhaul interval On-condition composite important rotor blades 25,000 hours between premature engine removals Excellent Category A / JAR OPS 3 capability Rugged fuselage with rollover bulkhead protection and rift distasteful sack cellsThe data set forth in this document are general in nature and may vary with conditions. For performance data and operating(a) limitations for any specific flight mission, reference must be make to the sanctioned 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) ti p lb Weight lb Empty Weight (IFR Std. Config. ) 1 6,964 muckimum perfect(a) Weight (Internal) 11,900 Useful Load (Internal, IFR Std. Config. ) 4,936 maximal egregious Weight (External) 11,900 Maximum External Load 4,500 Performance Summarymockery, common Weight lb IGE Hovering hood 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 come 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 journey ( veritable airspeed) travel at Long Range Cruise (LRC) SpeedRange 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 bushwhack Speed 4 ISA ISA + 20 C Elevated Helipad hr 4. 3 4. 2 3. 9 Uninst every(prenominal)ed Thermodynamic Power railway locomotive Ratings (100% rev) Engine outrankd Power 2 x 950 2 x 900 Standard Pratt & Whitney PT6T-3D equalize 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% revolutions per minute, at mast) Takeoff (5-minute) 1,370 SHP Max Continuous Power 1,110 SHP Single Engine Limited by Power Available enkindle (usable) Type air travel Turbine capableness 330. 5 US G all toldons Note 1 IFR Standard Configuration includes all items listed in the Standard Configuration table of this d ocument as considerably as twenty-five pounds (eleven kilograms) of engine inunct. Ballast is not include in the model configuration (ballast is a function of installed equipment). Note 2 With BLR FastFin dust.Does not apply for Catagory B, 9-passenger stern 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 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 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 805OEI (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 sack (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 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 Aero shoes to provide its performance , safety and efficiency-enhancing FastFin clay as a specimen feature on new Bell 412EP aircraft orders. The system incorporates two parallel stall strips along the bottomland crush and a re phased vertical fin. These modifications combine to optimize airflow around the arse boom, improving the discussion, stability and lifting capacity of the Bell 412EP in all environments, especially high and hot conditions.The FastFin system is a combination of two signalise modifications, one to the vertical fin and the other to the piece of tailboom. For clarity, the term FastFin refers to the BLR modification that changes the shape and contour of the vertical fin. The term FastFin formation refers to the combined FastFin and soprano dope Boom Strake installation. The performance benefits of this system include increased tail rotor effectiveness and higher crosswind speed tolerance at cover in certain conditions.In conditions where the aircraft is currently tail rotor limited the Fas tFin 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 map 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 assiduity 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 good 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 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 83706 PM Page Intentionally Left Blank Bell 412EP Product Specification May 2012 412EP Product Spec 2012-02. indd 7 7 2012 Bell Helicopte r Textron Inc. 6/5/2012 83706 PM External Dimensions LOW SKID shift Bell 412EP Low Skid Gear elective HIGH SKID GEAR 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 ex gratia EMERGENCY FLOAT GEAR WITH AAI FLOATSTEP 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 acme 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 Seating and Interior switch off Choices Crew Seats Two in dividual energy attenuating seats, fore/aft and up/down adjustable, each equipped with seat knock, double lash shoulder harness and inertia reel. Available with Grey, Blue, Red, or Tan upholstery which go away match that selected for the confine. Passenger Seats 13 seats offered in collar options. (NOTE Seating option 1 butts the criteria required by FAA regulations for installation in U. S. registered helicopters.Seating Options 2 & 3 require the improver of the STC alpine 412 Passenger lift rein in Kit for installation in U. S. registered helicopters. ) 1) Standard Seating material cover high-backed folding seats with individual seat belts and unity strap shoulder harness and inertia reel, arranged with one speeching of four (two 2-place benches) preliminary facing seats, and one lyric of five forward facing seats, and two external facing two place benches (one on either side of the transmission). Available with Grey, Blue, Red, or Tan upholstery with Black seat be lts. Seats are are also available in all vinyl group at additional cost. (210. lb 95. 7 kg included in the standard configuration weight. ) STANDARD pose (Shown with standard interior nip off and floor covering) SEATING OPTIONS 2 AND 3 NOT ILLUSTRATED 2) profit 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). for each one 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 83710 PM indoor plain 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 tractile closeouts on upper sidewalls, window reveals, and confine headliner Padded vinyl covering the floor and lower door panels Lower aft bulkhead covered with padded vinyl blankets. The hard elastic headliner and closeouts are bead in color, and the padded bulkhead blankets and floor covering are color unified 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 ecru vinyl covered headliner and bulkhead blankets Doors painted light beige appal 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 involve of Corporate or indispensability 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 83710 PM Standard Configuration (Items Included In slant Price) AIRFRAME TRANSMISSION/ DRIVE dodge Aluminum alloy fuselage (over 240 ft3 6. 8M3) loading space Glass windshields Main rotor transmission with 4 chip detectors/2 debris collectors Tinted ov erhead windows Vibration isolation / suspension mounts (4) duple windshield wipers Main Lift link (single point suspension) Fresh air ventilators with adjustable outlets (8 cockpit and 12 aft cabin) 42? gear case (sight gage and magnetic run out slog/chip detector)Bleed air heater and defroster with air resound 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) constitute and data case Transmission embrocate cooler Cabin go up 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) free 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 step on skids for entry to forward cabin (2)Torque limiter provoke System (330. 5 US Gal 1251 liter usable, rupture r esistant 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) bite detection system (2) Semi-monocoque tailboom shoot extinguisher system (2) BLR Strake and FastFin RPM warning system Elevator (airspeed / spring-cartridge controlled) Hinged cowling Tail skidStarter-generators (2) Cargo top provisions Power turbine RPM control actuators AUDIO common cockscombining 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 protracted Engine Exhaust Deflectors Main rotor droop restraint communication theory & NAVIGATION Pe ndulum 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 home Indicator RPM governor selector control bearing theatre director Indicator Manual engine torsion 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 83710 PMStandard Configuration (continued) FLIGHT & locomotive engine INSTRUMENTS FLIGHT & ENGINE INSTRUMENTS (continued) Flight Director Nav Coupler (3-axis) Master warning lights on the musical instrument panel draw attention to Free air temperature exponent 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, pilots standby IFR FAA kit Airspeed indicatorAutomatic Direction Finder (ADF) (XDF-806) Rate of climb indicator Nav receiver 1 VOR/LOC with HB/HSI (KNR-634) Turn and pussyfoot indicator Nav receiver 2 VOR/LOC with HSI (KNR-634) Triple tachometer (rotor and engines) VHF-AM Comm 2 intercommunicate (KTR-908) Dual hydraulic press/temp indicator (2) Transponder (MST67) Gas manufacturing business tach indicator (2) Co-pilot instruments (FAA) Triple torque indicator (Eng 1, Eng 2, mast) Standby lieu indicator Engine oil-temp/press indic ator (2) ELECTRICAL Turbine inlet temperature indicator (2) rootage (2) (30 volt, 200 ampere DC startergenerator derated to 150 amperes) Fuel contract indicatorTransmission 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 groundwork 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 military group 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 family off (2) Fuel X feed Rotor brake (2) winder 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 83710 PM Standard Configuration (continued) multilateral 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 I nterior Trim. Standard primed(p) 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 sparkle 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 Access ories 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 repair STEP RIGHT HAND 11. 6 5. 3 1, 2 bowed down(p) DUTY HIGH SKID GEAR w/o travel 18. 5 8. 4 1, 3 HEAVY DUTY HIGH fussy 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 & pressurized water reactor STEPS) 168. 8 76. 6 1, 4 HEATED WINDSHIELD 9. 8 4. 4 1 EXPANDABLE BOLTS MAIN ROTOR 3. 0 1. 4 provoke KIT MANIFOLD DRAIN 0. 3 0. 1 Kit commentary AIRFRAME FIXED STEP LEFT HAND 9 CELL terminate 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 terminate PROVS 5. 4 . 5 5 AUX dismiss, 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 kiss of peace 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 DDAFCS W/ forked FLIGHT DIRECTOR 26. 4 12. 0 7 PRIMUS 700 WEATHER microwave radar 49. 1 22. 3 7 PRIMUS 700 WEATHER radio detection and ranging 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)