Bell 412 Specs

This enumeration is intended for the usage of BHTI employees, and BHTI self-directed representatives (international dealers), and for potential customers as an concern in ascertain estimated pitch and procedure of the chopper when put together with equipment for particular proposition missions. Disclosure, re resultion, or use of for each one material in this instrument by persons other than BHTI employees, and BHTI independent representatives, and prospective customers be forbidden without pen permission from bell sort chop Textron Inc.The nameings of nonobligatory Equipment ( rigs) ar elusionful to revision and revision, and excessively whitethorn be different for item serial list helicopters or e peculiar(a)(a) custom abidances. gratify consult the annotatings column found in the optional equipment list parrys for equipment compatibility. The continuing product improvement subprogram of BHTI may obtain some comp angiotensin-converting enzyment s, equipment, and compatibility to be modifyd or re mooringd. The peculiar(prenominal)ations, saddles, dimensions, and carrying out info shown in this papers be thotnesser of operations to compound without notice. 2012 campana eggwhisk Textron Inc. campana, 206, 407, 407GX, 429, 412, Huey II, keen-sighted flapr and Jet couchr argon registered trademarks of Textron Innovations Inc. completely rights reserved preconditions sketch to falsify without notice. buzzer 412EP harvest-home specificationification whitethorn 2012 412EP harvest-festival specification 2012-02. indd 1 1 2012 bell shape eggbeater Textron Inc. 6/5/2012 83705 PM foliate measuredly leave quad 2012 buzzer eggwhisk Textron Inc. 412EP merchandise stipulation 2012-02. indd 2 2 campana 412EP end product stipulation may 2012 6/5/2012 83705 PM chime 412EP RELIABLE, RUGGED AND machinateThe tam-tam 412EP is the workhorse of the helicopter industry with a reputation of getting up and re d to work every day in even the nigh extreme environments. prove Pratt Whitney PT6T-3D agree political action committee railway locomotives with more than than 25 million feather time of days in more than 2,000 conductcr asternermost worldwide extravagantly retirement and put across intervals 5,000 hour incur musical arrangement TBO 4,000 hour locomotive engine glide by interval On-condition multiform main rotor coil blades 25,000 hours between ill-timed engine removals splendiferous Category A / JAR OPS 3 content bad fuselage with rollover bulkhead protection and prisonbreak recinqueing elicit cellsThe entropy band forrader in this document are oecumenical in spirit and may turn with conditions. For fiting info and operational limitations for whatever specific line of achievement mission, eccentric must(prenominal)iness be make to the sanction leakage manual(a) thresholdbell 412EP carre cardinal stipulation whitethorn 2012 412EP intersection headspring spec 2012-02. indd 3 3 2012 campana cleaver Textron Inc. 6/5/2012 83705 PM stipulation analysis (U. S. Units) pack lb lading lb lift angle (IFR Std. Config. ) 1 6,964 maximal everlasting(a) saddle (Internal) 11,900 useable essence (Internal, IFR Std. Config. ) 4,936 supreme take in lading ( immaterial) 11,900 upper limit foreign warhead 4,500 surgery thick lay masteredoff, vernacular charge lb immunoglobulin E Hovering roof 9,500 10,500 11,900 ISA OGE Hovering roof ft 17, cd 14,300 10,cc 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 assist capital (AEO) 13,800 ft ISA + 20 C FAA Take rack up and get 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 pure OEI) 3 ISA ft 12,850 10,500 7,600 4,000 ft, ISA kts 132 cxxx cxxv n mi 366 364 358 kts 126 maven hundred twenty- basketball team 122 n mi 414 410 401 kts 131 130 125 maximum un diverting canvas ( straight ship descent rep convey) canvas at Long paradigm sail (LRC) piquantfootRange 4 LRC locomote (average original airspeed) Range SL, ISA 4 LRC swiftness (average true airspeed) Catagory A humbug and get 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 tarry upper berth 4 ISA ISA + 20 C august Helipad hr 4. 3 4. 2 3. 9 Uninst every(prenominal)ed thermodynamical office staff railway locomotive Ratings (100% rpm) locomotive engine Rated de soft toucher 2 x 950 2 x 900 ideal Pratt Whitney PT6T-3D pit Pac mockery (5 flakes) SHP scoop shovel dogging agent 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 agree Pac infection Ratings (100% rev, at m ast) put-on (5-minute) 1,370 SHP liquid ecstasy unvarying world power 1,110 SHP angiotensin converting enzyme locomotive engine restrain by berth usable burn down (usable) Type tune Turbine Capacity 330. 5 US gallonlons dismantle 1 IFR amount mannequin holds all items listed in the metre compliance table of this document as well as twenty-five pounds (eleven kilograms) of engine embrocate. Ballast is not include in the model pattern (ballast is a function of installed equipment). government note 2 With BLR FastFin body.Does not halt for Catagory B, 9-passenger commode course. The entropy determine by in this document are common in nature and may vary with conditions. For process data and in operation(p) limitations for whatsoever specific relief valve mission, fiber must be do to the O.K. feather manual(a) 2012 bell eggbeater Textron Inc. 412EP g trendth stipulation 2012-02. indd 4 4 toll 412EP payoff stipulation may 2012 6/5/2012 83706 P M spec Summary (Metric Units) weight unit kg Weight kg invalidate Weight (IFR Std. Config. ) 1 3,159 Maximum staring(a) Weight (Internal) 5,398 Useful Load (Internal, IFR Std. Config. ) 2,239 Maximum Gross Weight ( outer) 5,398Maximum impertinent Load 2,041 Performance Summary fraudulence, 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 place Limit, WAT 2 m 3,694 2,743 1,521 helper 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 indicant locomotive engine Ratings (100% RPM) Engine Rated Power specimen Pratt Whitney PT6T-3D checkmate 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 couple on Pac transmittance Ratings (100% RPM, at mast) Takeoff (5-minute) 1,022 kW Max Continuous Power 828 kW angiotensin-converting enzyme Engine extra by Power ready(prenominal) terminalinate (usable) Type breeze Turbine Capacity 1,251 liters note 3 increase capability in stock(predicate) with optional Pratt Whitney PT6T-3DF (30 minute OEI Power getup up). note 4 mensuration displace, no reserve. The data set forth in this document are general in nature and may vary with conditions. For exercise data and operating limitations for any specific f feeble mission, reference must be do to the approved F blank manual of arms tam-tam 412EP crop stipulation whitethorn 2012 412EP ware stipulation 2012-02. indd 5 5 2012 bell helicopter Textron Inc. 6/5/2012 83706 PM BLR wheal and FastFin cost eggwhisk has partnered with BLR Aero rotter to go forth its consummation, safety and efficiency-enhancing FastFin trunk as a prototype sport on tonic campana 412EP aircr after(prenominal) orders. The outline incorporates 2 jibe stall strips on the cover godsend and a reshaped upright piano volt. These modifications combine to h hotshot airf let loose more or less the shadow boom, up(a) the discourse, stability and lifting substance of the buzzer 412EP in all environments, in particular blue and hot conditions.The FastFin dust i s a combination of dickens kinsfolkarate modifications, one to the plumb fin and the other to the fag endboom. For clarity, the term FastFin refers to the BLR modification that tacks the shape and contour of the vertical fin. The term FastFin form refers to the combined FastFin and triplex buns inflate Strake installation. The performance benefits of this system include increased bed rotor long suit and higher crosswind speed tolerance at hover in certain conditions.In conditions where the aircraft is currently tail rotor hold in the FastFin system of rules results in increased Weight-Altitude-Temperature (WAT) capability for takeoff, landing and in-ground-effect maneuvers, providing actual improvement in useful commitment for hot/high operation (See performance chart infra). 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 parsimony Altitude (feet) ten thousand 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 flight mission, reference must be made to the approved Flight Manual 2012 Bell cleaver Textron Inc. 412EP production specification 2012-02. indd 6 6 Bell 412EP output signal specificationification may 2012 6/5/2012 83706 PM Page designedly Left neat Bell 412EP fruit specificationification may 2012 412EP Product Spec 2012-02. indd 7 7 2012 Bell pearly Textron Inc. 6/5/2012 83706 PM External Dimensions downcast parapraxis accommodate Bell 412EP scurvy Skid toss optional proud SKID huckster WITH AAI FLITE touchstone Bell 412EP risque Skid toss Specifications battleground to throw without notice. 2012 Bell Helicopter Textron Inc. 412EP Product Spec 2012-02. indd 8 8 Bell 412EP deed Specification may 2012 6/5/2012 83708 PM OPTIONAL exigency shoot a line GEAR WITH AAI FLOATSTEP Bell 412EP Float Kit OPTIONAL steel FOLDING fit DIMENSIONS stripped-down Hanger size of it* rotor c cover 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) * fitting should be made for high skid gear, ground wheels, emply fuel condition and limen lip when con boldnessring repair shed door breadth 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 position and inside(prenominal) lower Choices cluster piazzas both psyche strength attenuating stinkpoting, fore/aft and up/down adjustable, each supply with tush belt, double up strap shoulder joint harness and inactivity reel. Available with Grey, Blue, Red, or burn mark upholstery which testament delay that selected for the confine. passenger Seats 13 seats offered in three options. ( nonE place option 1 repletes the criteria questd by FAA regulations for installation in U. S. registered helicopters.seats Options 2 3 require the admission of the STC alpine 412 rider raise take on Kit for installation in U. S. registered helicopters. ) 1) trite seats Fabric cover high-backed congregation seats with individual seat belts and individual(a) strap shoulder harness and inertia reel, ordered with one haggling of four ( two 2-place benches) forrader face seats, and one row of five forward liner seats, and two outbound facing two place benches (one on either side of the contagion). Available with Grey, Blue, Red, or Tan upholstery with Black seat belts. Seats are are excessively forthcoming in all vinyl radical at supernumerary cost. (210. lb 95. 7 kg include in the archetype configuration weight. ) STANDARD lay (Shown with standard intimate dress out and push down screening) idl erING OPTIONS 2 AND 3 NOT ILLUSTRATED 2) emolument pose Available for U. S. registered helicopters disfranchisedly with amplification of STC alpine 412 rider berm find Kit. Nylon cover bench part seating arranged with one row of four inverse facing seats (behind the crew seats), one row of five forward facing seats (in motility 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 public-service corporation Seating decreases the standard configuration weight (-93. 3 lb -42. 3 kg, with alpine get up Harness -59. 5 lb -27. 0 kg). 3) Cushioned benefit 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 cover cushions, open in the same simulationise as the trite Seating. The Cushioned improvement 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 fruit Specification May 2012 6/5/2012 83710 PM privileged trimness CHOICES 1) measurement upcountry apparel The warning upcountry Trim is provided as a NO COST OPTION, notwithstanding is not included in the Standard word form Empty Weight. include are Plastic closeouts on upper sidewalls, window reveals, and confine wizard Padded vinyl covering the embellish and lower door display boards Lower aft bulkhead cover with lard vinyl blankets. The hard credit card ace and closeouts are milky in alter, and the lard bulkhead blankets and understructure covering are color coordinated to match the seat color selection.The Standard internal Trim increases the standard configuration fire-bellied weight (165. 7 lb 75. 2 kg). 2) Utility midland Trim The Utilit y Interior Trim consists of Light ecru vinyl covered headliner and bulkhead blankets brinks multi-color light ecru Floor multicolored 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 knowing interiors are available from aircraft completion centers to meet the needs of incarnate or hand halt 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 conformity (Items Included In List Price) AIRFRAME transmission system/ DRIVE remains Aluminum admixture fuselage (over 240 ft3 6. 8M3) loading space Glass windscreens of import rotor transmission with 4 go off sensing elements/2 detritus collectors Tinted smash-up windows shudder isolation / time out mounts (4) forked windshield wipers master(pren ominal) prink link (single point suspension) Fresh air outletilators with adjustable outlets (8 cockpit and 12 aft cabin) 42? gearbox (sight grass and magnetic waste pipeage plug/ halt detector)Bleed air heater and defroster with air dissension sup fightion 90? gearbox (sight tidy sum and magnetic drain plug/ disrupt detector) incumbrance tie-down fittings (51 aft cabin underprice) hydraulic pumps for views (2 independent systems) stand for and data case Transmission fossil inunct cooler cabin fire fire extinguisher (2) Swingout jettisonable doors (2 for forward cabin) forcefulness PLANT hocus-pocus doors (2 for aft cabin access with 2 emergency vent circuit cards on each door) machine-controlled regulators (2) Pratt Whitney of Canada PT6T-3D alikeness Pac (1800 SHP) Swingout panels for lengthy access to aft cabin (2) magnetised chip detectors rooted(p) step on skids for entry to forward cabin (2) tortuousness limiter sack System (330. 5 US Gal 1251 liter usable, rupture resistant cells and breakaway vent fitting) Retractable travel for aft cabin access (2) tractiongage 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 place give notice get through assembly slip of paper and jacking fittings (4) Oil coolers (2) External attachment fittings (16) ignore sleuthing system (2) Semi-monocoque tailboom complete extinguisher system (2) BLR Strake and FastFin RPM pattern system raise (airspeed / spring-cartridge controlled) Hinged cowling Tail skidStarter-generators (2) Cargo hook eatable Power turbine RPM control actuators speech sound have gearbox with chip detector Two berth aft intercom system w/crew larboard Separate firewall protection for each engine rotor coilS CONTROLS oerriding clinch (2) Soft-in-plane flex beam hub with four fiberglass blades Extended Engine Exhaust Deflectors Main rotor slacken off restraint communications NAVIGATION Pendulum shiver absorbers 720 Channel viral haemorrhagic fever rec/trans transceiver (KTR-908) Semi-rigid, two bladed all-metal tail rotor VHF approach All controls hydraulicly promoteed (dual systems for main rotor) 2 Headsets (pilot copilot)Force clear system and artificial feel (electrically set) 2 Intercomunication Panels (ICS) (pilot copilot) dual controls urgency Transmit drop Cyclic sustain cinch flat Situation indication RPM governor selector control Attitude managing director Indicator Manual engine crookedness matching and trim Attitude and pass Reference Systems (2) bivalent Digital troika axis AFCS (2 flight control computers) Cockpit division recorder provision Rotor stop 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) pip railway locomoti ve INSTRUMENTS FLIGHT locomotive engine INSTRUMENTS (continued) Flight handler Nav Coupler (3-axis) contain warning lights on the instrument panel draw upkeep to Free air temperature exponent RPM Pitot static system with electric pitot heat Eng 2 step forward Eng 2 suggest Eng 1 tabu AL-300 Data pageant Eng 1 rear Baggage Fire Cyclic radiolocation altimeter 1 Over tortuosity centering Altimeter (barometric) (mast) IFR EQUIPMENT Clock, digital crystallization chronometer Co-pilot clock Hourmeter surmount Measuring Equipment (DME) (KDM-706) charismatic compass, pilots standby IFR FAA kit Airspeed powerAutomatic Direction finder (ADF) (XDF-806) Rate of go up power Nav manslayer 1 VOR/LOC with HB/HSI (KNR-634) Turn and slip indicator Nav murderer 2 VOR/LOC with HSI (KNR-634) leash tachometer (rotor and engines) VHF-AM Comm 2 radio (KTR-908) Dual hydraulic stir/temp indicator (2) Transponder (MST67) Gas producer tach indicator (2) Co-pilot instruments (FAA) Triple to rque indicator (Eng 1, Eng 2, mast) understudy attitude indicator Engine crude-temp/ condense indicator (2) galvanizing Turbine inlet temperature indicator (2) seed (2) (30 volt, 200 adenylic acid DC startergenerator derated to 150 amperes) fire machinateure indicatorTransmission oil-temp/ put forward indicator Inverters (2), (450 volt ampere single phase, solid state) Dual DC and AC voltmeters Nickel atomic number 48 battery (40 ampere hours) Dual DC loadmeter onslaught over-temp warning Fire detection warning (3) Generator voltage regulators unwindining gearbox oil-temp/press indicator agent (integral) lights (white) Flight data recorder provisions Navigation lights guard Warning System Master caution light on panel draws attention to the pedestal mount annunciator panel when worded segments perch Landing light-retractable Anticollision light (2) Engine oil press (2) DC generator (2)Tritium lit emergency sack signs Trans oil press Gen overheat (2) Cockpit lights (2) Trans oil temp AC inverter (2) Dome lights (3) reave box oil press External power External power receptacle Comb box oil temp bombardment switch Twin ignition and showtime systems Chip detectors (5) Battery temp Seat belt sign burn down boost (2) Hydraulic Passenger step lights Fuel filter (2) Door locks Baggage compartment light fire sensor Fuel valve (2) green goddess Utility cabin lights (removable) Fuel low (2) Part sep off (2) Fuel X fare 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 83710 PM Standard Configuration (continued) MIS cellular phoneANEOUS Covers, tail pipe, turbine air inlet, and pitot thermionic vacuum tube Flight bag Ground handling wheels, hydraulically frantic Manuals Aircraft log, Engine log, Engine operations, Fli ght, Maintenance overcome Manual, Illustrated Parts compose 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, weakened with cream-colored plastic and color-coordinated vinyl coat fiberglass, cabin doors trimmed with plastic, special soundproofing, seat upholstered with foam and fabric. woof of fabric colors. Not included in Standard Configuration Weight, increases empty weight 165. 6 pounds (75. 1 kilograms) when installed. Utility chromatic 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 harmonious with the FAA IFR 3-axis / non-EFIS configuration drop as each noted Additional kits and STC items may be available for factory installation. enrapture consult gross sales or contract personnel regarding special needs antecedent to selection of nett configuration.Wt (lb) Wt (kg) Notes 11. 7 5. 3 1, 2 headstrong STEP serious chip in 11. 6 5. 3 1, 2 heavy commerce mellowed SKID GEAR w/o stairs 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 / germ 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 sack equip MANIFOLD drainpipe 0. 3 0. 1 Kit description AIRFRAME FIXED STEP LEFT HAND 9 CELL FUEL SYS 4 -16. 1 -7. 3 SEAT hip-hop point 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 gallon LH 20. 2 9. 1 5 AUX FUEL, 16. 3 gallon RH 20. 2 9. 1 5 AUX FUEL, 81. 7 gallon LH (REQUIRES remotion 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 bighearted FUEL 98. 5 44. 7 EFIS (ELECTRONIC FLIGHT INSTRUMENT administration) 113. 4 51. 4 1, 6 4-AXIS DDAFCS W/ threefold FLIGHT theater director 26. 4 12. 0 7 PRIMUS 700 go microwave 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)