BELL HELICOPTER BELL 430 Manuale operativo

Product Data

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

DISCLAIMER

THIS INFORMATION CONTAINED HEREIN WAS PREPARED AND INTENDED, ONLY,

AS A MARKETING AID. IT CANNOT BE USED AS A SUBSTITUTE FOR THE

ROTORCRAFT FLIGHT MANUAL, MAINTENANCE MANUAL, ILLUSTRATED PARTS

BREAKDOWN OR OTHER PUBLICATIONS APPROVED BY AIR REGULATORY

AUTHORITIES FOR THE OPERATION, AND/OR MAINTENANCE OF ANY BELL

AIRCRAFT.

PUBLISHERS NOTICE

The data presented herein is general in nature and is intended for the use of BHTI

Sales Personnel and International Sales Representatives as an aid in describing

the features and benefits of Bell Helicopters to prospective customers.

This data includes proprietary material of BHTI. Disclosure, reproduction, or use of

anyofthematerialhereinbypersonsotherthanBHTIemployees,andBHTIIndependent

Representatives [International Dealers] is forbidden without written permission from

BHTI.

ThePHOTOGRAPHSandDRAWINGS appearing herein arefor illustrationonly,and

maydifferfromtheactualaircraft,astheBHTIcontinuingproductimprovementprocess

causessome components, specifications,and procedures tobe changed orreplaced.

THEWEIGHTS, DIMENSIONS, AND PERFORMANCE DATA SHOWN MAY NOT BE

CURRENT. For the most current tabular data, and performance and fuel flow charts

refer to the current year’s Technical Information Booklets.

©Copyright, Bell Helicopter Textron, Inc., 2003 ®™, Bell Helicopter, Bell Helicopter Textron Inc., Bell

206B3, 206L-4, 407, 427, 430, 412, 609, JetRanger and

LongRanger are registered trademarks of Bell

Helicopter Textron Inc.

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

BELL 430

PRODUCT DATA

CONTENTS

SECTION ONE GENERAL DESCRIPTION OF

THE STANDARD CONFIGURATION

SECTIONTWO OPTIONAL EQUIPMENT

FACTORY INSTALLED

BHTC &VENDOR STC KITS

SECTIONTHREE DIMENSIONS,

DESIGN SPECIFICATIONS

AND WEIGHTS

ALPHABETICAL INDEX

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

GLOSSARY

INTERNATIONALLY APPROVED ABBREVIATIONS

Atmosphere

Rate of Climb

Speed and Distance

Weights

Performance

Definitions

ISA

ISA+20 C

ISA+30 C

R/C

ft/min

m/s

km/h

mph

IGE

OGE

max

Maximum Endurance

Speed

Long Range Cruise

Speed

Pressure Altitude

Service Ceiling

Degrees Celsius (° is not required if meaning is clear.)

International standard atmosphere. (Standard temperature is defined

as 15°C at sea level, with a lapse rate of -1 °C for each 150 meters (500

feet) increase in pressure altitude.)

International standard temperatures increased at each altitude by a

constant 20 C or 30 C.

Sea level.

Rate of climb.

Feet per minute.

Meters per second. (One meter per second is 3.28 ft/s )

Hour/hours.

Kilometer/kilometers.

Kilometers per hour. (One kilometer per hour equals 0.54

knots or 0.62 statute miles per hour.)

Knots. (Nautical miles per hour.)

Meter/meters. (One meter equals 3.28 feet.)

Statute miles per hour. (One mile per hour equals 0.87

knots. )

Nautical miles.

Statute miles.

Kilogram/kilograms.

Pound/pounds. (One pound equals 0.45 kilograms.)

In ground effect. (Hovering near the ground creates a

cushion of air that increases the weight carrying capability

of the helicopter (the ground effect). This effect generally

is present up to one rotor diameter above the ground.)

Out of ground effect. (Since the ground effect extends up to

one rotor diameter out of ground effect refers to flight that is

higher than this height above the ground.)

Maximum.

The speed at which power required to fly is a minimum.

The higher of the two speeds at which 99% of maximum

range occurs. Cruising at this speed is a tradeoff of one

percent in maximum range for 20 to 30 kilometers per hour

(10 to 15 knots), higher speed.

The altitude indicated on an altimeter or barometer when

the sea level standard pressure reading is the reference

(1013 millibars (29.92 inches) of mercury).

The altitude at which the maximum rate of climb capability

is 0.5 meters per second, 100 feet per minute.

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

SECTION ONE

GENERAL DESCRIPTION OF

THE STANDARD CONFIGURATION

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

ADVANCED

FOUR-BLADED

MAIN ROTOR

The Bell 430, a 9 to 11 place twin turbine powered helicopter, is the latest version of

Bells' well proven INTERMEDIATE TWIN helicopter series whose heritage reaches

back almost 20 years. This latest model in the series blends the attractive lines of the

222/230 family with Bells' advanced Model 680 Rotor Design.

SYSTEMS OVERVIEW

Introduction

The Bell 430 FOUR-BLADED bearingless rotor system features primary structural

elementsconstructedofcompositematerialstoavoidcorrosionandtoprovidebenign,

easilydetectablefailuremodes,alongwith"on-condition"(noretirementlife)operation.

Main rotor blade pitch change as well as flapping and lead/lag motions occur through

flexing and bending the two composite yokes (with fluid filled dampers and shear

restraints), rather than by means of the customary hinges and lubricated bearings.

The four blades of the main rotor are of all composite construction with a replaceable

metal leading edge abrasion strip. They are designed for on-condition replacement

and are fully interchangeable. A simplified pylon support system attaches the rotor

and transmission systems to the fuselage.

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

The passenger cabin is longer than that of the Bell 222/230 to give each of the three

main cabin seat rows more pitch, making the accommodations more comfortable and

theridemorepleasant.Anoptionalhingedpaneldoorkit isavailabletoprovidegreater

easeof accessforcargoor litters.Locatedbetweentheleft crewandpassengerdoors

it is attached by hinges to the fuselage and the passenger door in a manner similar to

the Litter Door of the Bell LongRanger & 407 series.

CABIN STRETCH WITH OPTIONAL LITTER DOOR

OPTIONAL LITTER DOOR

BAGGAGE DOOR

MAIN PASSENGER DOOR

COMFORT FEATURES

The spacious cabin is easily entered

through the wide (nearly 180°) opening

passengerdoors,andprovidescomfortable

seating for seven (standard seats), with

ample room for baggage. The 1.05 cubic

meter (37.2 cubic feet) aft baggage

compartmentisaccessiblethroughit'sown

door, or through the rear cabin partition.

Cabinfurnishingsincludethehighbacked

non-folding seats with three-point lap /

shoulder restraints, and the standard

deluxe interior trim, headliner /

soundproofing, hard thermoplastic wall

covering,andvinylfloorcovering. TheSIX

large cabin windows afford each

passenger a panoramic view. The cabin

ventilation system directs fresh outside

air toeach seat from individual overhead

outlets. In flight, the cabin's occupants

receive a smooth vibration-free ride,

courtesy of the LIVE®suspension.

STRETCHED FUSELAGEWITH OPTIONAL PANEL DOOR

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

ROLLS-ROYCE 250-C40B ENGINES FADEC ELECTRONIC CONTROL UNIT

TheprimarydesignparametersoftheBell

430 emphasize safety in every aspect of

the aircraft. All critical flight systems are

either duplicated or isolated / separated

tomeet/exceedthespecificationsofFAR

Part29CategoryA. Redundantloadpaths

areincorporatedthroughoutallsafety-of-

flightcomponents,suchasthemainrotor

blades,transmissionattachment,andflight

control linkage. Fuselage integrity is

ensured through two integral roll-over

bulkheadsatthefrontandrearofthecabin.

The fuel supply is contained in rupture-

resistantfabricandrubbercellswhichhave

been drop-tested when75% full from 15

meters(50feet) withoutspillage,andare

interconnected with break-away self-

sealing fittings.

The engines selected for the Bell 430 are the Rolls-Royce 250-C40B. These are a

growth version of the well - proven 250-C30 engine series from Rolls-Royce which

providereliablepowerundertheextremesofclimaticconditions.TheRolls-Royce250

engine series has accumulated over 100 million hours of flight time, with deliveries

totaling over 30,000 engines. Controlling each engine is a Full Authority Digital

Electronic Control (FADEC). The FADEC provides automatic starting, is able to

maintainrotor speed and engine matchingwithinclosertolerances,and to offera 30-

second single engine rating to enhance Category A operations. Additionally, as in all

BellHelicopters,MANUALpowermanagementofeachengineisimmediatelyavailable

to the pilot through the collective-mounted twist grip throttles.

ROLLOVER BULKHEADS

OCCUPANT PROTECTION BY REDUNDANT

FUSELAGE LOAD PATHS

ROLLS-ROYCE 250-C40B ENGINESWITH FADEC

SAFETY FEATURES

THIS IS AN UNCONTROLLED DOCUMENT.

THIS ELECTRONIC DOCUMENT MAY HAVE BEEN SUPERCEDED.

THE MOST CURRENT DOCUMENT INFORMATION IS AVAILABLE

FROM YOUR BELL HELICOPTER TEXTRON REPRESENTATIVE.

PRODUCT DATA JANUARY 2003

Another new feature of the Bell 430 is the Integrated Instrument Display System

(IIDS) which reduces the size of the instrument panel and gives the flight crew more

forward field of view. The Dual Displays help the flight crew to track, as well as to

control,essentialparametersofcriticalhelicoptersystems.TheIIDSalsocontrolsthe

ChipDetector/FuzzBurnerFunctionsforbothengines(2each)andthetransmission

/ tail rotor (6/1). Additionally, the IIDS has new maintenance and power assurance

functions. As a bonus, the IIDS is a valuable tool which also helps to increase the

helicopter's reliability and maintainability.

INTEGRATED INSTRUMENT DISPLAY SYSTEM (IIDS) - SHOWN WITH OPTIONAL EQUIPMENT

MAINTAINABILITY FEATURES

The Bell 430 is engineered for reliability and ease of maintenance. Built in steps and

work platforms, along with plentiful access panels, doors, and inspection windows

provide for quick and thorough preflight checks and servicing. Primary components

andsystemsaredesignedforroutineservicingwhileremaininginstalledontheaircraft.

Major service intervals are among the longest in the rotorcraft industry due to Bell's

traditionallylongTimeBetweenOverhaul/RetirementLifecomponents.Somethings

have not, and will not change ; Bell Helicopter'scommitment tosafety, low cost of

operation, and reliable, responsive helicopters that are supportable and economic

through their lifetimes.

INTEGRATED INSTRUMENT DISPLAY SYSTEM (IIDS)

Indice

Altri manuali BELL HELICOPTER Giocattolo

BELL HELICOPTER

BELL HELICOPTER 214B Series Manuale utente

BELL HELICOPTER

BELL HELICOPTER 206L4T Manuale utente

BELL HELICOPTER

BELL HELICOPTER 430 Manuale utente

BELL HELICOPTER

BELL HELICOPTER 205A-1 Manuale utente

BELL HELICOPTER

BELL HELICOPTER 222 Manuale utente

BELL HELICOPTER

BELL HELICOPTER 212 Manuale di servizio

BELL HELICOPTER

BELL HELICOPTER 407 Series Manuale utente

BELL HELICOPTER

BELL HELICOPTER 214ST Manuale utente

Manuali Giocattolo popolari di altre marche

marklin

marklin 37321 Manuale utente

Canon

Canon PAPER CRAFT Manuale utente

GREAT PLANES

GREAT PLANES Pitts M-12S Manuale utente

NOCH

NOCH 14261 Manuale utente

Hausler

Hausler 450 SE V2 Manuale utente

Dynaflite

Dynaflite Daydream Manuale utente

MiniacRC

MiniacRC MIGHTY MINI P40 WARHAWK Manuale

Kenner

Kenner Batman 63651 Manuale utente

LEGO

LEGO 8527 Manuale utente

iKarus

iKarus ECO 8 Manuale utente

Multiplex

Multiplex EasyStar II Manuale di istruzioni

Walkera

Walkera 38 Manuale di istruzioni

Hasbro

Hasbro TRANSFORMERS BUMBLEBEE Manuale utente

MD MXION SWD Manuale utente

Mattel

Mattel Disney Pixar Cars Cozy Cone Spiral Rampway Manuale utente

marklin

marklin 39671 Manuale utente

Meccano

Meccano 15103 Manuale utente

LEGO

LEGO TECHNIC 8735 Manuale utente