206L4 Spec Book 22013-Web

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206L4 Spec Book 22013-Web

Transcript of 206L4 Spec Book 22013-Web

  • FEBRUARY 2013PRODUCT SPECIFICATIONS

  • Bell 206L4 Product Specification i 2013 Bell Helicopter Textron Inc. February 2013

    Publishers Notice ............................................................................................................................1

    Exterior Dimensions ........................................................................................................................2

    Cabin Dimensions ...........................................................................................................................4

    Door Dimensions .............................................................................................................................4

    Specification Summary (U.S. Units) ................................................................................................6

    Specification Summary (Metric Units) .............................................................................................7

    Bell 206L4 Seating ..........................................................................................................................8

    Base Aircraft Configuration ..............................................................................................................10

    Standard Configuration....................................................................................................................11

    Optional Accessories .......................................................................................................................12

    Helicopter Performance Charts .......................................................................................................15

    Fuel Flow vs. Airspeed ....................................................................................................................23

    Cost of Operations...........................................................................................................................35

    Limited Life Components .................................................................................................................38

    Paint Schemes ................................................................................................................................39

    Training ............................................................................................................................................40

    Table of Contents

  • Specifications subject to change without notice.

    Bell 206L4 Product Specification 1 2013 Bell Helicopter Textron Inc. February 2013

    Publishers Notice

    The data presented in this document are general in nature, and have been compiled from Bell Helicopter Textron Inc. (BHTI) source materials including but not limited to: The Approved Rotorcraft Flight Manual, Maintenance Manual, Illustrated Parts Catalog, and other engineering design specifications.

    This document is intended for the use of BHTI employees, and BHTI independent representatives (international dealers), and for prospective customers as an aid in determining estimated weight and performance of the helicopter when configured with equipment for specific missions.

    Disclosure, reproduction, or use of any material in this document by persons other than BHTI employees, and BHTI independent representatives, and prospective customers are forbidden without written permission from Bell Helicopter Textron Inc.

    The listings of Optional Equipment (Kits) are subject to revision and change, and also may be different for specific serial number helicopters or special custom configurations. Please consult the Notes column found in the optional equipment list tables for equipment compatibility. The continuing product improvement process of BHTI may cause some components, equipment, and compatibility to be changed or replaced.

    The specifications, weights, dimensions, and performance data shown in this document are subject to change without notice.

    2013 Bell Helicopter Textron Inc. Bell, 206, 407, 407GX, 429, 412, Huey II, LongRanger and JetRanger are registered trademarks of Textron Innovations Inc.

    All rights reserved

  • 2013 Bell Helicopter Textron Inc. 2 Bell 206L4 Product Specification February 2013

    Bell 206L4 Low Gear

    Bell 206L4 High Skid Gear

    LOW SKID GEAR

    HIGH SKID GEAR WITH AA FLITESTEPExterior Dimensions

  • Bell 206L4 Product Specification 3 2013 Bell Helicopter Textron Inc. February 2013

    Bell 206L4 Float Kit

    Minimum Hanger Size* 8.1 ft x 42.5 ft

    (2.5 m x 13.0 m)

    * Allowance should be made for high skid gear, ground wheels, empty fuel condition and door lip when considering hangar door width and height

    EMERGENCY FLOAT GEAR WITH AA FLOATSTEP

    Exterior Dimensions

  • 2013 Bell Helicopter Textron Inc. 4 Bell 206L4 Product Specification February 2013

    Cabin Dimensions

    Approximate Cargo SpaceAft Cabin 2.2 cubic meters (80 cubic feet)Left front 0.6 cubic meters (20 cubic feet)Baggage compartment 0.45 cubic meters (16 cubic feet)

    Floor LoadingCabin 3.7 kg/sq. meter (75 lb/ sq. foot)Baggage 4.2 kg/sq. meter (86 lb/sq. foot)

    Max Baggage weight 113 kg (250 pounds)

    cm in cm in cm inA 49.5 19.5 E 91.4 36 J 27.9 11B 78.7 31 F 43.2 17 K 70 24C 104 41 G 36.8 14.5 L 94 37D 152.4 60 H 76.2 30 M 58.4 23

    Door Dimensions

  • Bell 206L4 Product Specification 5 2013 Bell Helicopter Textron Inc. February 2013

    Page Intentionally Left Blank

  • The data set forth on 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.

    2013 Bell Helicopter Textron Inc. 6 Bell 206L4 Product Specification February 2013

    Specification Summary (U.S. Units)

    Weights lbEmpty Weight (Base Aircraft) [1] 2,331Maximum Gross Weight (Internal) 4,450Maximum Gross Weight (External Load) 4,550Useful Load (Internal Aircraft Base) 2,119Cargo Hook Capacity 2,000

    Performance Summary (International Standard Day Except as Noted)Takeoff, Gross Weight lb 3,600 4,000 4,450

    IGE Hovering Ceiling [2] (2.5 ft skid height) ISA ft 20,000+ 17,600 10,000ISA+20 C ft 18,340 15,110 7,730ISA+30 C ft 16,560 13,150 6,660

    OGE Hovering Ceiling [2] ISA ft 16,500 13,490 6,510ISA+20 C ft 13,850 10,420 4,240ISA+30 C ft 11,530 7,750 3,170

    Service Ceiling (MCP), 100 ft/min ISA ft 20,000+ 20,000+ 10,000ISA+20 C ft 20,000+ 19,280 7,730ISA+30 C ft 20,000+ 17,250 6,660

    Maximum Cruise Speed (True Airspeed) SL, ISA ktas 115 113 109SL, ISA+20 C ktas 118 115 1114,000 ft, ISA ktas 120 116 112

    4,000 ft, ISA+20 C ktas 121 118 109Range at Long Range Cruise (LRC) Speed (Average Gross Weight, Standard Fuel, No Reserve)

    SL, ISA nmi 336 331 325ktas 116 115 113

    4,000 ft, ISA nmi 373 365 352ktas 119 118 115

    Endurance at Loiter Speed (57 kias) (Standard Fuel, No Reserve)

    SL, ISA hr 3.9 3.8 3.74,000 ft, ISA hr 4.4 4.2 4.0

    Engine Power Ratings(Rolls-Royce 250-C30P) Uninstalled Thermodynamic Rating Takeoff SHP 726Maximum Continuous, SHP 630Transmission RatingTakeoff (5 Minutes) SHP 490Maximum Continuous SHP 370Fuel Capacity (Usable)Type Aviation TurbineStandard 110.7 US Gallons

    Notes: [1] Includes thirteen (13.0) pounds of engine oil. Ballast is not included in base aircraft weight (ballast is a function of installed equipment).

    [2] Refer to demonstrated takeoff and landing and maximum operating altitude notes on the performance charts.

  • The data set forth on this document are general in nature and may vary with conditions. For performance data and operating limitations for any specific flight mission, reference must be made to the approved Flight Manual.

    Bell 206L4 Product Specification 7 2013 Bell Helicopter Textron Inc. February 2013

    Specification Summary (Metric Units)

    Weights kgEmpty Weight (Base Aircraft) 1 1,057Maximum Gross Weight (Internal) 2,018Maximum Gross Weight (External Load) 2,064Useful Load (Base Aircraft) 961Cargo Hook Capacity 907

    Performance Summary (International Standard Day Except as Noted)Takeoff, Gross Weight kg 1,633 1,814 2,064

    IGE Hovering Ceiling [2] (0.8 m skid height) ISA m 6,096+ 5,364 3,048ISA+20 C m 5,590 4,606 2,356ISA+30 C m 5,047 4,008 2,030

    OGE Hovering Ceiling [2] ISA m 5,029 4,112 1,984ISA+20 C m 4,221 3,176 1,292ISA+30 C m 3,514 2,362 966

    Service Ceiling (MCP), 0.5 M/S ISA m 6,096+ 6,096+ 3,048ISA+20 C m 6,096+ 5,877 2,356ISA+30 C m 6,096+ 5,258 2,030

    Maximium Cruise Speed (True Airspeed) SL, ISA km 213 210 203SL, ISA+20 C km/h 218 213 2061,220 m, ISA km/h 221 215 207

    1,220 m, ISA+20 C km/h 224 218 201Range at Long Range Cruise (LRC) Speed (Average Gross Weight, Standard Fuel, No Reserve)

    SL, ISA km 622 613 602km/h 216 213 209

    1,220 m, ISA km 691 677 653km/h 220 219 214

    Endurance at Loiter Speed (57 kias) (Standard Fuel, No Reserve)

    SL, ISA hr 3.9 3.8 3.71,220 m, ISA hr 4.4 4.2 4.0

    Engine Power Ratings(Rolls-Royce 250-C30P) Uninstalled Thermodynamic Rating Takeoff kW 541Maximum Continuous kW 470Transmission RatingTakeoff kW 365Maximum Continuous kW 276Fuel Capacity (Usable)Type Aviation TurbineStandard 419 Liters

    Notes: [1] Includes 5.9 kilograms of engine oil. Ballast is not included in base aircraft weight (ballast is a function of installed equipment).

    [2] Refer to demonstrated takeoff and landing and maximum operating altitude notes on the performance charts.

  • Specifications subject to change without notice.

    2013 Bell Helicopter Textron Inc. 8 Bell 206L4 Product Specification February 2013

    Bell 206L4 Seati