Bell 412EP Product Specifications

May 2012 Specifications theme to qualify extraneously attend-to. Bell 412EP Effect Specification 412 Effect Spec - COVER. indd 1 1 November 2011 6/5/2012 8:41:16 PM 412 Effect Spec - COVER. indd 2 6/5/2012 8:41:16 PM Table of Contents Publisher’s Attend-to ............................................................................................................................ 1 Bell 412EP .......................................................................................................................................3 Specification Summary (U.S. Units) ................................................................................................4 Specification Summary (Metric Units) ............................................................................................. 5 BLR Strake and FastFin® ................................................................................................................ 6 External Dimensions........................................................................................................................ 8 Bell 412EP Seating and Toward Adjust Choices ............................................................................... 10 Standard Configuration.................................................................................................................... 12 Optional Accessories ....................................................................................................................... 16 Helicopter Act Charts ....................................................................................................... 21 Haggravate Act Charts .............................................................................................................. 2 Fuel Flow vs. Airdespatch .................................................................................................................... 31 Cost of Operations........................................................................................................................... 44 Limited Life Components ................................................................................................................. 47 Paint Schemes ................................................................................................................................ 9   Bell 412EP Effect Specification May 2012 412EP Effect Spec 2012-02. indd 1 i © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:05 PM 412EP Effect Spec 2012-02. indd 2 6/5/2012 8:37:05 PM Publisher’s Attend-to The basis presented in this muniment are open in disposition, and keep been compiled from Bell Helicopter Textron Inc. (BHTI) commencement embodieds including but not scant to: The Unconcealed Rotorcraft Stampede Manual, Maintenance Manual, Illustrated Parts Catalog, and other engineering project peculiarations. This muniment is purposed for the use of BHTI employees, and BHTI refractory representatives (interdiplomatic dealers), and for prospective practiceers as an aid in determining estimated efficacy and act of the helicopter when configured delay equipment for peculiar facearms. Disclosure, reiter-ation, or use of any embodied in this muniment by men-folks other than BHTI employees, and BHTI refractory representatives, and prospective practiceers are forbidden extraneously written dispensation from Bell Helicopter Textron Inc. The inventoryings of Optional Equipment (“Kits”) are theme to variation and qualify, and as-well-behaved may be irrelative for peculiar serial estimate helicopters or barional practice forms. Please canvass the “Notes” post establish in the discretional equipment inventory considerations for equipment compatibility. The continuing effect amendment arrangement of BHTI may creator some components, equipment, and compatibility to be qualifyd or replaced. The peculiarations, efficacys, size, and act basis shown in this muniment are theme to qualify extraneously attend-to. 2012 Bell Helicopter Textron Inc. Bell, 206, 407, 407GX, 429, 412, Huey II, LongRanger and JetRanger are registered trademarks of Textron Innovations Inc. All hues cautious Specifications theme to qualify extraneously attend-to. Bell 412EP Effect Specification May 2012 412EP Effect 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 Effect 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 exertionhorse of the helicopter perseverance delay a symbol of getting up and going to exertion full day in well-behaved-balanced the most ultimate environments. • Proven Pratt & Whitney PT6T-3D Twin Pac engines delay aggravate than 25 pet stampede hours in aggravate than 2,000 aircraft worldwide • Excellent solitude and hypercriticise gaps - 5,000 hour expedite plan TBO - 4,000 hour engine hypercriticise gap - On-pnot-difficult composite deep rotor blades • 25,000 hours between precipitate engine removals • Excellent Category A / JAR OPS 3 aptitude • Rugged fuselage delay rollaggravate bulkhead defence and discerption arduous fuel cells The basis set forth in this muniment are open in disposition and may differ delay stipulations. For act basis and gratuitous limitations for any peculiar stampede facearm, relation must be made to the unconcealed Stampede Manual Bell 412EP Effect Specification May 2012 412EP Effect Spec 2012-02. indd 3 3 © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:05 PM Specification Summary (U. S. Units) Efficacy lb Efficacy lb Vacuity Efficacy (IFR Std. Config. ) 1 6,964 Maximum Gross Efficacy (Internal) 11,900 Advantageous Direct (Internal, IFR Std. Config. ) 4,936 Maximum Gross Efficacy (External) 11,900 Maximum External Direct 4,500 Performance Summary: Takeoff, Gross Efficacy 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 (uniform OEI) ISA ft 11,450 8,850 5,400 (30 microscopic 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 Uniform Cruise (gentleman airspeed) Cruise at Long Range Cruise (LRC) Speed Range 4 LRC Despatch (mean gentleman airspeed) Range SL, ISA 4 LRC Despatch (mean gentleman 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 Despatch 4 ISA ISA + 20 °C Elevated Helipad hr 4. 3 4. 2 3. 9 Undomiciled Thermodynamic Might Engine Ratings: (100% RPM) Engine Rated Might 2 x 950 2 x 900 Standard: Pratt & Whitney PT6T-3D Twin Pac Takeoff (5 microscopics) SHP Max Uniform Might SHP 2 x 950 2 x 800 OEI (2-1/2 microscopics) SHP 1 x 1,140 1 x 1,133 OEI (continuous) SHP 1 x 970 1 x 1,024 OEI (30 microscopics) SHP 1 x 1,066 1 x 1,079 OEI (continuous) SHP 1 x 950 N/A Optional: Pratt & Whitney PT6T-3DF Twin Pac Transsidearm Ratings (100% RPM, at mast) Takeoff (5-minute) 1,370 SHP Max Uniform Might 1,110 SHP Separate Engine Scant by Might Serviceable Fuel (usable) Mold Aviation Turbine Size 330. 5 US Gallons Note 1 IFR Standard Form apprehends all items inventoryed in the Rule Form consideration of this muniment as well-behaved-behaved as twenty-five pounds (elwell-balanced kilograms) of engine oil. Ballast is not interjacent in the rule form (ballast is a office of domiciled equipment). Note 2 Delay BLR FastFin® System. Does not dedicate for Catagory B, 9-passenger locate form. The basis set forth in this muniment are open in disposition and may differ delay stipulations. For act basis and gratuitous limitations for any peculiar stampede facearm, relation must be made to the unconcealed Stampede Manual © 2012 Bell Helicopter Textron Inc. 412EP Effect Spec 2012-02. indd 4 4 Bell 412EP Production Specification May 2012 6/5/2012 8:37:06 PM Specification Summary (Metric Units) Efficacy kg Efficacy kg Vacuity Efficacy (IFR Std. Config. ) 1 3,159 Maximum Gross Efficacy (Internal) 5,398 Advantageous Direct (Internal, IFR Std. Config. ) 2,239 Maximum Gross Efficacy (External) 5,398 Maximum External Direct 2,041 Act Summary: Takeoff, Gross Efficacy 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 (uniform 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 microscopic OEI) 3 Maximum Uniform Cruise (gentleman airspeed) Cruise at Long Range Cruise (LRC) Despatch Range 4 LRC Despatch (mean gentleman airspeed) Range 4 LRC Despatch (mean gentleman 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 Despatch 4 km/h ISA + 20 °C Catagory A Takeoff and Landing Ceiling hr 4. 3 4. 2 3. 9 ISA Undomiciled Thermodynamic Might Engine Ratings: (100% RPM) Engine Rated Might Standard: Pratt & Whitney PT6T-3D Twin Pac Takeoff (5 microscopics) kW 2 x 708 2 x 671 Max Uniform Might kW 2 x 708 2 x 597 OEI (2-1/2 microscopics) kW 1 x 850 1 x 845 OEI (continuous) kW 1 x 723 1 x 764 OEI (30 microscopics) kW 1 x 795 1 x 805 OEI (continuous) kW 1 x 708 N/A Optional: Pratt & Whitney PT6T-3DF Twin Pac Transsidearm Ratings (100% RPM, at mast) Takeoff (5-minute) 1,022 kW Max Uniform Might 828 kW Separate Engine Scant by Might Serviceable Fuel (usable) Mold Aviation Turbine Size 1,251 liters Note 3 Increased aptitude serviceable delay discretional Pratt & Whitney PT6T-3DF (30-microscopic OEI Might Kit). Note 4 Rule fuel, no backwardness. The basis set forth in this muniment are open in disposition and may differ delay stipulations. For act basis and gratuitous limitations for any peculiar stampede facearm, relation must be made to the unconcealed Stampede Manual Bell 412EP Effect Specification May 2012 412EP Effect 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 delay BLR Aeroquantity to arrange its act, guard and efficiency-enhancing FastFin® plan as a rule component on new Bell 412EP aircraft command. The plan incorporates two analogous stall strips along the subordination peal and a reshaped perpendicular fin. These revisions merge to optimize airflow encircling the subordination peal, comely the handling, inheritance and lifting size of the Bell 412EP in all environments, distinctly excellent and hot stipulations. The FastFin® plan is a confederacy of two detached revisions, one to the perpendicular fin and the other to the subordinationboom. For clarity, the expression FastFin® refers to the BLR revision that qualifys the cast and contour of the perpendicular fin. The expression FastFin® Plan refers to the merged FastFin® and Dual Subordination Peal Strake installation. The act benefits of this plan apprehend increased subordination rotor cleverness and excellenter crosswind despatch tolerance at threaten in unmistakable stipulations. In stipulations where the aircraft is currently subordination rotor scant the FastFin® Plan results in increased Weight-Altitude-Temperature (WAT) aptitude for takeoff, landing and in-ground-effect maneuvers, providing massive amendment in advantageous direct for hot/excellent action (See act chart beneath). 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 Efficacy (lb) 11,000 12,000 Bell 412EP WAT Amendment delay FastFin® System The basis set forth in this muniment are open in disposition and may differ delay stipulations. For act basis and gratuitous limitations for any peculiar stampede facearm, relation must be made to the unconcealed Stampede Manual © 2012 Bell Helicopter Textron Inc. 412EP Effect 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 Effect Specification May 2012 412EP Effect Spec 2012-02. indd 7 7 © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:06 PM External Size LOW SKID GEAR Bell 412EP Low Skid Ownership OPTIONAL HIGH SKID GEAR WITH AAI FLITESTEP® Bell 412EP High Skid Ownership Specifications theme to qualify extraneously attend-to. © 2012 Bell Helicopter Textron Inc. 412EP Effect 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 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 excellent skid ownership, basis wheels, emply fuel pnot-difficult and door lip when because hangar door width and culmination Specifications theme to qualify extraneously attend-to. Bell 412EP Effect Specification May 2012 412EP Effect Spec 2012-02. indd 9 9 © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Bell 412EP Seating and Toward Adjust Choices Herd Seats - Two specific motive attenuating locates, fore/aft and up/down adjustable, each equipped delay locate encompass, double band shoulder impede and inertia totter. Serviceable delay Grey, Blue, Red, or Tan upholstery which allure competition that separated for the incarcerate. Passenger Seats - 13 locates offered in three discretions. (NOTE: Seating discretion 1 ass the criteria claimd by FAA regulations for installation in U. S. registered helicopters. Seating Options 2 & 3 claim the abstracted of the STC Alpine 412 Passenger Shoulder Impede Kit for installation in U. S. registered helicopters. ) 1) Rule Seating - Work mellow excellent-backed folding locates delay specific locate encompasss and separate band shoulder impede and inertia totter, de- delay one row of disgusting (two 2-locate strandes) eager confrontment locates, and one row of five eager confrontment locates, and two apparent confrontment two locate strandes (one on either face of the transmission). Serviceable delay Grey, Blue, Red, or Tan upholstery delay Black locate encompasss. Seats are are as-well-behaved serviceable in all vinyl at abstractedal absorb. (210. lb [95. 7 kg] interjacent in the rule form efficacy. ) STANDARD SEATING (Shown delay rule toward adjust and bottom crust) SEATING OPTIONS 2 AND 3 NOT ILLUSTRATED 2) Utility Seating - Serviceable for U. S. registered helicopters ONLY delay abstracted of STC Alpine 412 Passenger Shoulder Impede Kit. Nylon mellow strand mold locateing de- delay one row of disgusting rearward confrontment locates (aback the herd locates), one row of five eager confrontment locates (in front of the transmission), and two apparent confrontment two locate strandes (one on either face of the transmission). Each locate has an specific locate encompass. Serviceable in Tan or Black. The Utility Seating decreases the rule form efficacy (-93. 3 lb [-42. 3 kg], delay Alpine Shoulder Impede -59. 5 lb [-27. 0 kg]). 3) Cushioned Utility Seating - Serviceable for U. S. registered helicopters ONLY delay abstracted of STC Alpine 412 Passenger Shoulder Impede Kit. As in 2) aggravatehead delay the abstracted of work mellow cushions, serviceable in the corresponding pretenses as the Rule Seating. The Cushioned Utility Seating decreases the rule form efficacy (-81. 1 lb [-36. 8 kg], delay Alpine Shoulder Impede -47. 3 lb [-21. 5 kg]). Specifications theme to qualify extraneously attend-to. © 2012 Bell Helicopter Textron Inc. 12EP Effect Spec 2012-02. indd 10 10 Bell 412EP Production Specification May 2012 6/5/2012 8:37:10 PM INTERIOR TRIM CHOICES 1) Rule Toward Adjust - The Rule Toward Adjust is de- as a NO COST OPTION, but is not interjacent in the Rule Form Vacuity Weight. Interjacent are: Pliant closeouts on upper facewalls, window reveals, and incarcerate headliner; Padded vinyl crust the bottom and inferior door panels; Inferior aft bulkhead mellow delay padded vinyl blankets. The arduous pliant headliner and closeouts are off-pure in pretense, and the padded bulkhead blankets and bottom crust are pretense coordinated to competition the locate pretense option. The Rule Toward Adjust increases the rule form vacuity efficacy (165. 7 lb [75. 2 kg]). 2) Utility Toward Adjust - The Utility Toward Adjust consists of: Not-difficult beige vinyl mellow headliner and bulkhead blankets; Doors painted not-difficult beige; Bottom painted brown. The Utility Toward Adjust is interjacent in the rule form vacuity efficacy (33. 3 lb [15. 1 kg]). CUSTOMIZED SEATING [Example] Customized Seating - Practice projected towards are serviceable from aircraft amount centers to as the needs of Corporate or Difficulty Medical Service practiceers. Specifications theme to qualify extraneously attend-to. Bell 412EP Effect Specification May 2012 412EP Effect Spec 2012-02. indd 11 11 © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Rule Form (Items Interjacent In Inventory Price) AIRFRAME TRANSMISSION/ DRIVE SYSTEM Aluminum decrement fuselage (aggravate 240 ft3 [6. 8M3]) directing quantity Glass windshields Deep rotor transsidearm delay 4 remnant guides/2 trash collectors Tinted aggravatehead windows Vibration segregation / suspension mounts (4) Dual windshield wipers Deep Lift combine (separate summit suspension) Fresh air openingilators delay adjusconsideration outlets (8 cockpit and 12 aft incarcerate) 42? ownershipbox (vision secure and magnetic parch plug/remnant guide) Bleed air ardorer and defroster delay air din concealment 90? ownershipbox (vision secure and magnetic parch plug/remnant guide) Cargo tie-down fittings (51 aft incarcerate bottom) Hydraulic pumps for represss (2 refractory plans) Map and basis fact Transsidearm oil cooler Incarcerate inspirer extinguisher (2) Swingout jettisonable doors (2 for eager incarcerate) POWER PLANT Sliding doors (2 for aft incarcerate similarity delay 2 difficulty debouchure panels on each door) Automatic instructors (2) Pratt & Whitney of Canada PT6T-3D “Twin Pac” (1800 SHP) Swingout panels for plentiful similarity to aft incarcerate (2) Magnetic remnant guides Fixed step on skids for record to eager incarcerate (2) Torque limiter Fuel Plan (330. 5 US Gal [1251 liter] feasible, discerption arduous cells and breakaway opening fitting) Retracconsideration steps for aft incarcerate similarity (2) Bagsecure division in subordination peal (aggravate 28 ft [0. 8M ], 400 lb [181kg] size). 3 3 Pumps on engines and intense in fuel tanks Skid-mold landing ownership delay replaceable bear shoes Fuel ooze constellation Mooring and jacking fittings (4) Oil coolers (2) External kindness fittings (16) Inspirer defiance plan (2) Semi-monocoque subordinationpeal Inspirer extinguisher plan (2) BLR Strake and FastFin RPM diffidence plan ® Elevator (airdespatch / spring-cartridge repressled) Hinged cowling Subordination skid Starter-generators (2) Cargo grasp conditions Might turbine RPM rehurry actuators AUDIO Combining ownershipbox delay remnant guide Two state aft intercom plan w/herd interface Detached inspirerwall defence for each engine ROTORS & CONTROLS Overriding clutches (2) Soft-in-plane flex glow hub delay disgusting fiberglass blades Plentiful Engine Exhaust Deflectors Deep rotor bend repression COMMUNICATIONS & NAVIGATION Pendulum vibration absorbers 720 Channel VHF rec/trans transceiver (KTR-908) Semi-rigid, two bladed all-metal subordination rotor VHF antenna All represss hydraulically boosted (dual plans for deep rotor) 2 Headsets (escort & copilot) Force adjust plan and fictitious feel (electrically set) 2 Intercomunication Panels (ICS) (escort & copilot) Dual represss Difficulty Transmit Switch Cyclic adhere centering Horizontal Situation Indicator RPM instructor selector rehurry Situation Director Indicator Manual engine torque competitioning and adjust Situation and Heading Relation Systems (2) Dual Digital Three axis AFCS (2 stampede rehurry computers) Cockpit control recorder conditions Rotor wilderness Specifications theme to qualify extraneously attend-to. © 2012 Bell Helicopter Textron Inc. 412EP Effect Spec 2012-02. indd 12 12 Bell 412EP Production Specification May 2012 6/5/2012 8:37:10 PM Standard Form (continued) FLIGHT & ENGINE INSTRUMENTS FLIGHT & ENGINE INSTRUMENTS (continued) Stampede Director Nav Coupler (3-axis) Master diffidence not-difficults on the record panel attract observation to: Free air sky indicator RPM Pitot static plan delay electric pitot ardor Eng 2 Out Eng 2 Inspirer Eng 1 Out AL-300 Basis Display Eng 1 Inspirer Bagsecure Inspirer Cyclic Radar altimeter #1 Aggravate torque centering Altimeter (barometric) (mast) IFR EQUIPMENT Clock, digital quartz chronometer Co-escort clock Hourmeter Distance Measuring Equipment (DME) (KDM-706) Magnetic encompass, escort’s standby IFR FAA kit Airdespatch indicator Automatic Direction Finder (ADF) (XDF-806) Rate of mount indicator Nav receiver #1 VOR/LOC delay HB/HSI (KNR-634) Turn and slip indicator Nav receiver #2 VOR/LOC delay HSI (KNR-634) Triple tachometer (rotor and engines) VHF-AM Comm #2 radio (KTR-908) Dual hydraulic hurry/temp indicator (2) Transponder (MST67) Gas source tach indicator (2) Co-escort records (FAA) Triple torque indicator (Eng 1, Eng 2, mast) Standby situation indicator Engine oil-temp/hurry indicator (2) ELECTRICAL Turbine entrance sky indicator (2) Generator (2) (30 volt, 200 ampere DC startergenerator derated to 150 amperes) Fuel hurry indicator Transsidearm oil-temp/hurry indicator Inverters (2), (450 volt ampere separate bearing, solid-state) Dual DC and AC voltmeters Nickel cadmium battery (40 ampere hours) Dual DC directmeter Battery aggravate-temp diffidence Inspirer defiance diffidence (3) Generator voltage regulators Combining ownershipbox oil-temp/hurry indicator Record (integral) not-difficults (white) Stampede basis recorder conditions Navigation not-difficults Diffidence & Diffidence Plan - Master diffidence not-difficult on panel attracts observation to the sole mounted annunciator panel when worded segments illuminate: Landing not-difficult-retracconsideration Anticollision not-difficult (2) Engine oil hurry (2) DC generator (2) Tritium not-difficulted difficulty debouchure badges Trans oil hurry Gen aggravateardor (2) Cockpit not-difficults (2) Trans oil temp AC inverter (2) Dome not-difficults (3) Comb box oil hurry External might External might repository Comb box oil temp Battery switch Twin ignition and starting plans Remnant guides (5) Battery temp Locate enencompass badge Fuel boost (2) Hydraulic Passenger step not-difficults Fuel ooze (2) Door locks Bagsecure division not-difficult & inspirer sensor Fuel valve (2) Heater Utility incarcerate not-difficults (removable) Fuel low (2) Part sep off (2) Fuel X indulge Rotor wilderness (2) PAINT Emerg gov manual (2) Diffidence panel Markings for excellent appearance M/R blades (pure & orange-colored) Specifications theme to qualify extraneously attend-to. Bell 412EP Effect Specification May 2012 412EP Effect Spec 2012-02. indd 13 13 © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Rule Form (continued) MISCELLANEOUS Covers, subordinationpipe, turbine air entrance, and pitot tube Stampede bag Basis handling wheels, hydraulically activated Manuals: Aircraft log, Engine log, Engine actions, Flight, Maintenance & Hypercriticise Manual, Illustrated Parts Catalog Tie-down assemblies, deep rotor & subordination rotor INTERIOR TRIM Choice of Rule or Utility Toward Trim. Standard; Rigid three-piece headliner in a incarcerate, padded fiberglass bottom crust, bulkheads, adjustmed delay cream-colored pliant and pretense-coordinated vinyl-coated fiberglass, incarcerate doors adjustmed delay pliant, barional soundproofing, locate upholstered delay sparkle and work. Option of work pretenses. Not interjacent in Rule Form Weight, increases vacuity efficacy 165. 6 pounds (75. 1 kilograms) when domiciled. Utility; Beige soundproofing blankets on bulkheads and aggravatehead; doors painted beige, bottom painted brown. Interjacent in Rule Form Efficacy (almost 32. 6 pounds, 914. 8 kilograms). Specifications theme to qualify extraneously attend-to. 2012 Bell Helicopter Textron Inc. 412EP Effect 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 Effect Specification May 2012 412EP Effect Spec 2012-02. indd 15 15 © 2012 Bell Helicopter Textron Inc. 6/5/2012 8:37:10 PM Optional Accessories [Kits inventoryed beneath are consentaneous delay the FAA IFR 3-axis / non-EFIS form bar as specificly renowned] Added kits and STC items may be serviceable for factory installation. Please canvass sales or compress personnel in-reference-to barional needs antecedent to option of last form. 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 DDAFCS 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)