Bell 429 Product Specifications - Africair, Inc.

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationTable of ContentsPublisher’s Notice............................................................................................................................1World’s Most Advanced Light Twin..................................................................................................3Specification Summary (U.S. Units).................................................................................................4Specification Summary (Metric Units)..............................................................................................5Bell BasiX-Pro Integrated Avionics System..................................................................................6Safety Enhancements......................................................................................................................9Bell 429 External Dimensions and Heliport Design Data.................................................................10Bell 429 Interior ...............................................................................................................................11Standard Configuration....................................................................................................................14Optional Accessory Kits...................................................................................................................16Helicopter Performance Charts........................................................................................................21Fuel Flow vs. Airspeed ....................................................................................................................27Bell 429 Maintenance Program........................................................................................................41Bell 429 Training..............................................................................................................................43Bell 429 Product Specification - 7,500 lb IGW i © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationPublisher’s NoticeThe data presented in this document are general in nature, and have been compiled from Bell HelicopterTextron 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 (internationaldealers), and for prospective customers as an aid in determining estimated weight and performance of thehelicopter when configured with equipment for specific missions.Disclosure, reproduction, or use of any material in this document by persons other than BHTI employees, andBHTI independent representatives, and prospective customers are forbidden without written permission fromBell Helicopter Textron Inc.The listings of Optional Equipment (“Kits”) are subject to revision and change, and also may be different forspecific serial number helicopters or special custom configurations. Please consult the “Notes” column foundin the optional equipment list tables for equipment compatibility. The continuing product improvement processof 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 changewithout notice.© 2012 Bell Helicopter Textron Inc. Bell 206, Bell 407, Bell 429, Bell 412, and JetRangerare registered trademarks of Textron Innovations Inc.All rights reservedSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 1 © 2012 Bell Helicopter Textron Inc.January 2012

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7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationWorld’s Most Advanced Light TwinCertified for Single or Dual Pilot IFR, Cat. A at MGW 1Certified to FAR Part 27, Amendment 44, 2008 2••Transport Canada Type Certificate Data SheetH-107, Issue 3••Complies with latest crashworthiness requirementamendments of 14 CVR Part 27State of the Art Glass CockpitBest in Class WAAS Navigation & IFR Capability••Safer flights in rigorous IFR flight environments--greater situational awareness--decreased pilot workload••Fully coupled 4-axis autopilot integration toexecute LPV (Localizer Precision with Verticalguidance) approaches--up to and including 9 degree glide path angle--at speeds down to 45 KIAS••Enables flight on WAAS (Wide Area AugmentationSystem) enabled low-level IFR rotorcraftinfrastructuresFast Flexible Re-configuration for Changing Mission Requirements••Largest cabin in class, 204 ft 3 / 5.78 m 3••Open cabin with flat floor••6 passenger standard cabin seating with individual quick release for each seat••62 inch / 159 cm wide cabin door opening••Optional rear clamshell doorsFirst Helicopter certified through the MSG-3 Process (Maintenance Steering Group-3) for enhancedmaintenance efficiency and safety••First rotorcraft to have an approved EASA Maintenance Program••Ensures Continuing Airworthiness – How and when maintenance will be performed••Benefits show in significantly lower maintenance costs••Same systems level maintenance & safety standards used in latest product development by major largecommercial aircraft OEM’s.1 Catagory A Operations require installation of the following equipment:• 200 Amp Starter Generators• Increased Capacity Battery (53 AmpH or 44 AmpH)• Articulated Landing Light• Radar Altimeter2 Operation at 7,500 lbs increased internal gross weight requires installation of the following equipment:• Flashing Forward Light• Radar Altimeter• Helicopter Terrain Avoidance and Warning System (HTAWS), #1 Garmin GNS-530W NAV/COM/GPS with HTAWS orequivalent HTAWS system• Cockpit Voice Recorder/Flight Data RecorderThe 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 429 Product Specification - 7,500 lb IGW 3 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationSpecification Summary (U.S. Units)Weight Lb Weight LbEmpty Weight (Std.Config.) 1 4,478 lb Max Gross Weight (Internal) 7,500 lbUseful Load (Internal, Std Config.) 3,022 lb Max Gross Weight (External Load) 7,500 lbMinimum Empty Weight (SPIFR) 2 4,235 lb Cargo Hook Capacity 3,000 lbMax Useful Load (Internal, SPIFR)3,265 lbPerformance Summary:Takeoff, Gross Weight lb 6,000 6,500 7,000 7,500IGE Hovering Ceiling ISA ft. 18,577 16,301 14,132 12,072ISA+20°C ft 15,487 13,102 10,839 8,687OGE Hovering Ceiling ISA ft 15,888 13,535 11,282 9,148ISA+20°C ft 12,744 10,287 7,963 5,657Service Celing (MCP) - AEO ISA ft 20,000+ 20,000+ 18,714 16,687(30 minute) - OEI ISA ft 14,209 11,871 9,629 7,532(continuous) - OEI ISA ft 13,153 10,728 8,443 6,256Maximum Cruise Speed (true airspeed) SL, ISA ktas 153 152 150 148SL, ISA+20°C ktas 153 151 149 1474,000 ft, ISA ktas 155+ 155+ 155 1514,000 ft, ISA+20°C ktas 151 149 145 140Cruise at Long Range Cruise (LRC) SpeedRange (standard fuel, no reserve)nmi 376 381 372 365SL, ISALRC Speed (average true airspeed) ktas 128 129 130 130Range (standard fuel, no reserve)nmi 413 418 411 4034,000 ft, ISALRC Speed (average true airspeed) ktas 129 130 129 130Endurance at Loiter Speed (60 kts) SL, ISA hr 4.2 4.2 4.1 3.9(standard fuel, no reserve) 4,000 ft, ISA hr 4.6 4.5 4.5 4.3Engine Ratings: (100% RPM)Pratt & Whitney Canada PW207D1 with Full Authority Digital Electronic Control (FADEC)UninstalledThermodynamic PowerEngine Rated PowerTakeoff (5 minutes) SHP 2 x 719 2 x 598Max Continuous Power SHP 2 x 635 2 x 586OEI (30 seconds) SHP 1 x 826 1 x 729OEI (2 minutes) SHP 1 x 784 1 x 701OEI (30 minutes) SHP 1 x 753 1 x 663OEI (continuous) SHP 1 x 719 1 x 655Transmission Ratings: (100% RPM)Takeoff (5-minute) SHP 1,100Max Continuous SHP 1,100OEI (30 seconds) SHP 729OEI (2 minutes) SHP 650OEI (30 minutes & continuous) SHP 550Fuel Capacity (usable):Standard216.9 US GallonsAuxiliary (optional)39.2 US GallonsNote 1 Standard Configuration includes all items listed in the Standard Configuration Table of this document, equipment required for 7,500 lbincreased internal gross weight operations, and 24 pounds of engine oil. Ballast is not included in the standard configuration (ballast is afunction of installed equipment). Also, see Note 1 on page 14.Note 2 See Note 2 on page 15.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. 4 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationSpecification Summary (Metric Units)Weight Kg Weight KgEmpty Weight (Std.Config.) 1 2,031 kg Max Gross Weight (Internal Load) 3,402 kgUseful Load (Internal, Std Config.) 1,371 kg Max Gross Weight (External Load) 3,402 kgMinimum Empty Weight (SPIFR) 2 1,921 kg Cargo Hook Capacity 1,361 kgMax Useful Load (Internal, SPIFR)1,481 kgPerformance Summary:Takeoff, Gross Weight kg 2,722 2.948 3,175 3,402IGE Hovering Ceiling ISA m 5,662 4,969 4,307 3,679ISA+20°C m 4,720 3,993 3,304 2,648OGE Hovering Ceiling ISA m 4,843 4,125 3,439 2,788ISA+20°C m 3,884 3,135 2,427 1,724Service Celing (MCP) - AEO ISA m 6,096+ 6,096+ 5,704 5,086(30 minute) - OEI ISA m 4,331 3,618 2,935 2,296(continuous) - OEI ISA m 4,009 3,270 2,573 1,907Maximum Cruise Speed (true airspeed) SL, ISA km/hr 283 281 278 274SL, ISA+20°C km/hr 283 280 276 2721,220 m, ISA km/hr 287+ 287+ 287 2791,220 m, ISA+20°C km/hr 280 276 269 260Cruise at Long Range Cruise (LRC) SpeedRange (standard fuel, no reserve)km 696 706 689 676SL, ISALRC Speed (average true airspeed) km/hr 237 239 241 241Range (standard fuel, no reserve)km 765 774 761 7461,220 m, ISALRC Speed (average true airspeed) km/hr 239 241 239 241Endurance at Loiter Speed (60 kts) SL, ISA hr 4.2 4.2 4.1 3.90(standard fuel, no reserve) 1,220 m, ISA hr 4.6 4.5 4.5 4.3Engine Ratings: (100% RPM)Pratt & Whitney Canada PW207D1 with Full Authority Digital Electronic Control (FADEC)UninstalledThermodynamic PowerEngine RatedPowerTakeoff (5 minutes) kW 2 x 536 2 x 446Max Continuous Power kW 2 x 473 2 x 437OEI (30 seconds) kW 1 x 616 1 x 544OEI (2 minutes) kW 1 x 585 1 x 523OEI (30 minutes) kW 1 x 561 1 x 494OEI (continuous) kW 1 x 536 1 x 488Transmission Ratings: (100% RPM)Takeoff (5-minute) kW 820Max Continuous kW 820OEI (30 seconds) kW 544OEI (2 minutes) kW 485OEI (30 seconds & continuous) kW 410Fuel Capacity (usable):Standard821.1 litersAuxiliary (optional)148.4 litersNote 1 Standard Configuration includes all items listed in the Standard Configuration Table of this document, equipment required for 3,402 kgincreased internal gross weight operations, and 11 kilograms of engine oil. Ballast is not included in the standard configuration (ballast is afunction of installed equipment). Also, see Note 1 on page 14.Note 2 See Note 2 on page 15.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 429 Product Specification - 7,500 lb IGW 5 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell BasiX-Pro Integrated Avionics SystemThe Bell BasiX-Pro Avionics System has been specifically designed to meet the requirements of twin enginehelicopters and is optimized for IFR, Category A, and JAROPS-3 compliant operations. The system is highlyflexible and configurable to meet various operating and customization needs. The system takes advantageof the latest in display, computer processing, and digital data bus technology to provide a high degree ofredundancy, reliability, and flexibility.Standard Configuration SPIFRThe primary components of the Bell BasiX-Pro Avionics System in the Bell 429 include the following:Two Multi-FunctionDisplay Units (DUs) with6 x8 inch high-resolutiondisplays.Dual Channel AircraftData Interface Unit(ADIU)Dual Digital 3-axisAutomatic Flight ControlSystem (AFCS)Dual Channel AirData Attitude HeadingReference System(ADAHRS)Course/Heading/FlightDirector Panel (CHFD)The standard configuration for the Bell 429 provides single-pilot IFR capability with 3-axis stability and controlaugmentation (SCAS) and a coupled flight director capability. All Engine Indication and Crew Alerting System(EICAS) display functions are provided through the Bell BasiX-Pro Avionics System. The system works inconjunction with the engine control units (EECs) for the dual Pratt & Whitney electronically-controlled PW-207D1 engines. Other aircraft systems interfaces, warnings, cautions, aural alerts, and automated performancefeatures are provided through the remotely located Aircraft Data Interface Unit (ADIU).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. 6 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell BasiX-Pro Integrated Avionics System (continued)COMMUNICATIONS & NAVIGATION -- The Bell 429 standard configuration for Communications Navigationand Surveillance (CNS) consists of dual Garmin GNS-430W NAV/COM/WAAS GPS systems, with a kit optionto replace one of these with a GNS-530W. The standard system also includes a GTX-330 ELS compliantMode S transponder, a PMA-7000H Audio/Intercom Panel with VOX and Integral Marker Beacon Receiver,and an ARTEX C406-N-HM Emergency Locator Transmitter (ELT).DISPLAY UNITS -- The Multi-Function display units are “smart displays”, which include the processing requiredto collect sub-system information and generate display formats and graphics for the following:••All primary flight and navigation instrumentation••Presentation of flight director and autopilot status••Engine and rotor drive system indications••Electrical, hydraulic, and fuel system monitoring••Crew alerting system (warnings / cautions / advisories and aural alerts)••Navigation route mapping display••Presentation of optional Traffic Collision Avoidance Symbology (TCAS)••Presentation of optional weather radar or search radar information••Presentation of optional Forward Looking Infrared (FLIR) / Enhanced Vision Systems (EVS) video display(either NTSC or PAL standard)••Presentation of general color video display or digital map display (NTSC or PAL standard in either S-Videoor Component RGB video)••Presentation of electrical, AFCS, and fuel / weight and balance summary information••Presentation of automated power assurance, Category A performance, and hover performance calculations••Presentation of maintenance and diagnostic dataAutomatic Flight Control 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 ManualBell 429 Product Specification - 7,500 lb IGW 7 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell BasiX-Pro Integrated Avionics System (continued)Configuration Flexibility to Meet Operational NeedsThe Basix-Pro includes built-in provisions to allow customized configuration of the following equipment:••Alternate FMS / GPS systems••Alternate ARINC-429 radio navaids••UHF / VHF Direction Finder or 2nd ADF••Weather / Search Radar••FLIR / EVS display (either NTSC or PAL standard)••Designator Control Panel (allows FLIR or radar cursor designated positions to be captured as waypoints)••General color video display or digital map display••Velocity Sensor (for hover cues and / or search and rescue approach options)••Programmable CAS messages (cautions / warnings / advisories)A third display unit for the copilot position is available for the Bell 429 as an optional accessory.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. 8 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationSafety EnhancementsBell Helicopter is at the forefront in providing multiple ways of satisfying evolving requirements in helicoptertraffic management, flight following and terrain awareness safety. The Bell 429 is the first helicopter in thelight twin category to provide fully-coupled steep (9-degree) LPV WAAS (Localizer Precision with Verticalguidance Wide Area Augmentation System) approaches. The Bell BasiX-Pro Integrated Avionics Systemconcentrates on providing true operational capabilities and flexibility to our customers to address rapidlychanging regulatory requirements and technologies, with an open architecture and flexible avionics systemssolutions.The enhancements available for the Bell 429 through optional accessory kits and customizing include:Traffic Advisory System (TAS): Two TAS systems available:••Avidyne TAS605 (recommended) features 13 nm range; 5,500 ft vertical separation; and 55,000 ftservice ceiling.--Will be upgradable to Avidyne TAS605A for ADS-B when available from Avidyne.••Avidyne TAS620 features a 21 nm range, 10,000 foot vertical separation maximum, and 55,000 footservice ceiling.--Upgradable to Avidyne TAS620A for ADS-BHelicopter Terrain Awareness and Warning System / Enhanced Ground Proximity Warning System:Three H-TAWS and EGPWS H-TAWS options are available to satisfythe 7,500 lb Increased Internal Gross Weight equipment requirement.••Garmin GNS-530W with H-TAWS: Class B H-TAWS system,available as a Bell Helicopter optional accessory kit for the GNS-530W NAV/COM/GPS with Garmin system software 4.0 roll-out--Light weight, lowest cost solution--Displays on GNS-530W only••Honeywell Mark XXI EGPWS H-TAWS: Class B H-TAWS systemavailable as customizing--Installation with or without weather radar--Displays on BasiX-Pro Display Units, underlaid on PFD HSIformat or MFD Map / Radarformat--Uses same input as weatherradar--Provides only one TAWSimage (one range setting only)••Honeywell Mark XXII EGPWSH-TAWS: Class A H-TAWSsystem available as customizing,adds the following features:--Interfaces with ADC andRad Alt--Provides dual TAWS imageswith independent rangecontrolGarmin GNS-530W with H-TawsH-TAWS Displays “Under Glass”Available with Either Mark XXI or XXII EGPWS H-TAWSThe 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 429 Product Specification - 7,500 lb IGW 9 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell 429 External Dimensions and Heliport Design DataCG PositionLanding Gear Loading at Maximum Gross Weight (7,500-Pounds)Based on 1G Static Conditions for both Structural CG LimitLoading (lb) Contact Area (in 2 ) Contact Pressure (lb/in 2 )FWD AFT FWD AFT FWD AFTFWD CG 3,290 4,210 10.8 19.8 305 213AFT CG 2,950 4,550 10.8 19.8 273 230The 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. 10 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell 429 InteriorCREW SEATING: Two individual ergonomically designed energy attenuating seats with adjustable lumbarsupport, each equipped with seat adjustment controls forward and aft, up and down, adjustable lumbar support,a four-point restraint system, and adjustable pedals. The color and upholstery material for the seats match thecolor scheme selected for the cabin.The cockpit crew station was designed from the outset to accommodatepilots from the 5th percentile female to the 95th percentile male(standing height 5 ft. ½ inch to 6 ft. 2 inches; sitting height 31.3 inchesto 38.3 inches, reference U.S. FAA Human Factors Design Standard,HF-STD-001, dated May 2003). The pilot and co-pilot seats and pedalsare also adjustable to enable the cockpit crew to adjust their seatpositions for comfortable access to cockpit controls, so that they caneasily carry out normal and emergency duties without hindrance.••Forward and aft 6” (15 cm)••Up and down 4.5” (11.4 cm)••Adjustable pedalsThe cockpit ceiling provides ample clearance for the 95th percentile male wearing a flight helmet in either thepilot or co-pilot seat.PASSENGER / CARGO COMPARTMENT: The passenger / cargo compartment occupies the middlesection of the cabin. The compartment has a volume of 130 cubic feet (3.68 m3), which can be used in astandard or corporate configuration for passenger seating, or as cargo area. The aft cabin has an additionalvolume of 74 cubic feet (2.10 m3), giving a total contiguous cabin volume of 204 cubic feet (5.78 m3).A forward hinged and aft sliding door on each side of the cabin provide a 61.9” wide x 44.25” high (158.7 x112.3 cm) unobstructed door opening on each side of the helicopter for easy passenger compartment loadingand unloading. The two forward doors are hinged to open forward and the two sliding doors open aft and flushalong the cabin exterior. The passenger/cargo compartment doors can be opened individually or at the sametime.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 429 Product Specification - 7,500 lb IGW 11 © 2012 Bell Helicopter Textron Inc.January 2012

STANDARD SEATING AND TRIM7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationStandard Configuration six-place seating consists of two rows of three energy-absorbing seats, with individual4-point restraint system, quick release disconnects and fixed provisions for the optional passenger cabin ICSsystem. Two standard seating configurations are available:••6-place seating with 15.5“ wide seats, which can be quickly arranged into either an airline configurationwith both rows facing forward, or a club seating configuration with two rows facing each other••6-place seating with 18.5” wide seats in a club seating configuration.Each individual passenger seat assembly is installed on two transverse seat rail tracks that are attached to thecabin floor. The quick release disconnects enable the seats to be quickly arranged, or to remove individualseats to meet special mission configuration requirements. The seats are upholstered in fabric or optional vinyl.Standard interior trim consists of full thermoplastic closeouts on all airframe areas, a molded thermoplasticheadliner with two fixed slotted air vents, and a choice of either durable low loop nylon blend carpeting oroptional “Aermat” vinyl floor covering.Standard 6-place 15.5” wide passenger seats in ForwardFacing Airline Seating ArrangementStandard 6-place 18.5” wide passenger seats in ClubSeating ArrangementStandard Headliner with slotted air ventsOptional Headliner with LED lights& adjustable air ventsADDITIONAL INTERIOR OPTIONS: The following additional optional accessory kits are also available forselection on aircraft equipped with standard interior and seating. See Optional Accessory Kits, page 18 foradditional information on part numbers, availability and weights.••Aft Cabin ICS – 6 Place (Headsets not included)••Headliner with LED lights & adjustable Air Vents (recommended when optional air conditioning equipmentis selected)••Soundproofing••Aft Bulkhead Closeout Panel, available with or without soundproofingThe 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. 12 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationCORPORATE SEATING AND INTERIOR TRIMThree corporate seating options are available:Six place seating with 18.5” wide seatsAll corporate seating options include plush “OverstuffedStyle” seats with individual 3-point restraint system,quick release disconnects and fixed provisions for apassenger cabin ICS system. For the five place clubseating option, the quick release disconnects enablethe seats to be quickly arranged with the two 21.5” seatsfacing either forward or aft. The seats are upholsteredin premium leather.The corporate interior trim consists of full thermoplasticpanels on all airframe areas with color coordinatedleather or fabric trim, plush wool color coordinated carpet,and a molded thermoplastic corporate headliner withLED lights, adjustable air vents and color coordinatedleather trim.Five place club seating with a row of two 21.5” seatsseparated by a center console facing a row ofthree 18.5” seats with a center seat fold-down tableADDITIONAL INTERIOR OPTIONS: The followingadditional optional accessory kits are also available forselection on aircraft equipped with a corporate interiorand seating.••Aft Cabin ICS – 6 Place (Headsets not included)••Soundproofing••Aft Bulkhead Closeout Panel, available with orwithout soundproofing••6-place 18.5” corporate seats with fold-down centertables as a customizing optionFour place club seating with two 21.5” seatsseparated by a center console in each rowNote: Corporate passenger seats, interior trim andplush wool carpeting, corporate head liner, aftbulkhead closeout panel, and soundproofingare optional accessory kits, not included inStandard Configuration weight and price. SeeOptional Accessory Kits, page 18, for additionalinformation.A molded thermoplastic corporate headliner withLED lights, adjustable air vents and colorcoordinated leather trimThe 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 429 Product Specification - 7,500 lb IGW 13 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationStandard Configuration(Items Included in List Price)Certified for Single Pilot IFR; Certification Basis: FAR Part 27Amendments 27-1 through 27-40, andAmendment 27-44 (2008, requirements pertaining to flight performance and flight characteristics).AIRFRAMEFuselage: Machined alloy airframe with single piecemachined roof beams, lift frames, cabin keel beams and nosebeams; carbon fiber composite side-bodies, belly panels, noseskins, floor panels, decks and engine cowlsCorrosion resistant design with wet installed fasteners andsealed surfaces where dissimilar materials are found, toprovide exceptional resistance to adverse environmentalconditionsDoors (six, carbon fiber): Hinged pilot & co-pilot doors withsliding windows; hinged forward and sliding aft passengerdoors on both sides.Passenger doors provide 61.9 inches unobstructed openingon each side of the cabin.Door Locks for cockpit, cabin and luggage compartment, withcommon keying.Luggage compartment: Aft cabin (74 cubic feet), with 16discrete tie-down hardpoints and R/H side external luggagedoorLanding gear: Tubular skid type with replaceable wear shoesTailboom: Carbon fiber tailboom, vertical fin and horizontalstabilizerFuselage mounted passenger cabin steps, forward mountedcrew steps, and aft maintenance stepProvisions for mooring, jacking and single point liftingWindows: Gray tinted acrylic windows and windshieldsWire Strike Protection System Fixed Provisions , Cabin andNose Provisions (Bristol/AAI)Air Conditioning Drive Quill (Required for installation of any AirConditioning system)Air Conditioning Fixed ProvisionsThree color exterior paint schemes, Sample illustrationsavailable upon requestPOWERPLANTTwo Pratt & Whitney Canada 207D1 Engines, 1,172 shp(Mechanical) Kaximum Continiuous Rating (589 shp perengine)Electronic Engine Controls (EEC)Fuel Management Module (FMM)Fuel system: 216.9 gal. (821 liter) usable capacity, with threerupture resistant fuel cells located under the cabin floor paneland suction type fuel feed systemPOWERPLANT (continued)Electrical Provisions for Inlet Barrier FilterEngine Fire Detector & Fire Extinguisher SystemTRANSMISSION AND DRIVE SYSTEMSTwo-stage dual input drive main transmission, 1,100 shpMaximum Continuous PowerTwo fluid filled pylon mounts LIVE suspension (left and rightvertical axis mounts)Two elastomeric forward/aft restraintsThree main transmission chip detectors (fuzz burning)Two transmission-mounted hydraulic pumpsTail rotor drive shaft:Two steel forward drive shafts in engine deck/fire zoneTwo interchangeable carbon fiber composite aft drive shaftsin tailboom zoneSingle stage 90° tail rotor gearboxOne tail rotor gearbox chip detector (fuzz burning)ROTORS AND CONTROLSMain rotor: Soft-in-plane system, 36 ft. diameter, fourinterchangeable M/R blades, with stacked compositeyokes, titanium drive plate and CF fittings, elastomericCF (Centrifugal Force) bearings and shear restraints, andelastomeric lead/lag dampersComposite M/R blades with Nickel-Cobalt leading edgeabrasion strips and tip caps, HIGH VISABILITY (orange/whitetop - white bottom) paint schemeTail rotor: Four blade stacked system, 65” diameter, with lowtip speed, scissor arrangement, composite T/R blades withswept blade tips, Nickel-Cobalt leading edge abrasion strips,and elastomeric flapping bearingsDual Hydraulic System with integrated hydraulic modulesMechanical flight controls throughoutCollective mounted throttle controlsRotor Brake ProvisionsFLIGHT & ENGINE INSTRUMENTS – Bell BasiX-ProIntegrated Avionics SystemEFIS/EICAS (Electronic Flight Instruments System/ EngineIndicating & Crew Alerting System)Two 6” x 8” color LCD displays with video display capability“Smart” programmable display unit provisions for futureinterface required for customized equipment installationsNote 1: Standard Configuration includes:••Fixed provisions for Cat A. Operations equipment, Inlet Barrier Fliter, Air Conditioning, Rotor Brake & WSPS••ELT••Pilot & Copilot seats, 6 place Passenger Seating with 18.5” wide seats••Standard Interior, Headliner panels and CarpetThe 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. 14 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationStandard Configuration (continued)FLIGHT & ENGINE INSTRUMENTS (continued)Aircraft Data Interface Unit, Dual ChannelAFCS (3-axis), Dual digital autopilotDual channel SCAS and trim actuatorsAD/AHRS (Air Data/Attitude Heading Reference System),Dual Channel (Honeywell KSG7200)Course/Heading/Flight Director PanelStandby Instruments: Attitude, Altitude, Heading and AirspeedElectronic Data Recorder embedded in the IAS (IntegratedAvionics System) (non-crashworthy)COMMUNICATIONS & NAVIGATIONNav/Comm/GPS: VOR/ILS/GS/COMM/GPS and WAAS(Wide Area Augmentation System), with two 1.8” high x 3.3”wide displays (Garmin GNS 430W)Transponder: ELS compliant Mode S (Garmin GTX 330)Dual Keyed and/or VOX Intercom SystemPMA-7000H Audio Panel with Integral Marker BeaconReceiverELT (ARTEX C406-N-HM)INTERIOROpen cabin design with flat floor, total contiguous cabinvolume 232 cu. ft. (passenger and aft cabin/ area volume 204cu. ft.)Standard cockpit seating (2 seats), adjustable forward & aft,up & down, with lumbar support and adjustable pedalsPassenger Seat RailsStandard 6-place passenger seating with 4-point restraintsystem, individual seat quick release disconnects & ICS fixedprovisions (choice of 5.5” wide or 18.5” wide Seats)Ram air cockpit and cabin ventilation system, with cockpitWindshield defogging vent blowersStandard Interior: Thermoplastic panels covering all doorsand interior trim areas, & choice of durable low loop nyloncarpet or “Aermet” vinyl floor coveringStandard Headliner, Passenger Cabin, with two fixed slottedside air ventsELECTRICAL28 volt DC system, dual generator configuration25 AmpH Valve Regulated Lead-Acid (VRLA) batteryTwo 150 Amp Starter Generators, with two generator-regulatorcontrol unitsExternal power source connectionLED Cockpit instrument, annunciator, utility and map lightingwith programmable lighting power supply to ensure lightbalancing across all cockpit display and control panelsAll LED basic external lighting system:••One forward & two sideward facing fixed LED arraylanding lights••Three high intensity LED position lights••One flashing LED anti-colllision lightDigital maintenance interface available from cockpit for alldigital aircraft systemsRADS wiring for sensors embetted in basic aircraft wiringBaggage compartment lightingElectrical Provisions Kit (Required for Cat.A Operations)7,500 lb INCREASED INTERNAL GROSS WEIGHT KITEQUIPMENT (see Note 3)Flashing Forward LightRadar AltimeterHTAWSCockpit Voice Recorder/Flight Data RecorderLOOSE EQUIPMENTKeys for crew, passenger and baggage doorsManuals – Flight, Maintenance and IllustratedPartsBreakdown / Special Tools CatalogueMain and Tail Rotor tie downsCargo tie downsPitot CoverEngine Inlet CoversEngine Exhaust CoversEngine Exhaust CoversOil Cooler CoverGround Handling wheels, hydraulicNote 2: Minimum SPIFR Configuration includes:••Provisions for optional equipment including Cat A. Operations, Inlet Barrier Fliter, Air Conditioning, Rotor Brake & Wire Strike Protection Systemfixed provisions••ELT••Pilot seatNote 3: Operation at 7,500 lb increased internal gross weight requires installation of the following equipment:••Flashing Forward Light••Radar Altimeter••Helicopter Terrain Avoidance and Warning System (HTAWS), #1 Garmin GNS-530W NAV/COM/GPS with HTAWS or equivalent HTAWS system••Cockpit Voice Recorder/Flight Data RecorderThe 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 429 Product Specification - 7,500 lb IGW 15 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationOptional Accessory KitsRefer to notes for kit compatibility. 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 configurationKit DescriptionProjectedAvailability StatusAIRFRAMEDual Pilot Control Provisions 5.3 2.4 3Dual Pilot Controls Equipment (does not include co-pilot head set)(required for Dual Pilot operation) 10.5 4.8 3Pilot Cyclic Stick Locking Device 0.2 0.1200 Amp Starter Generator (dual) (required for Cat. A operations) 7.8 3.5 1, 22Increased Capacity Battery, 53 AmpH (Cat. A compliant) 35.1 15.9 1, 22Increased Capacity Battery, 44 AmpH (Cat. A Compliant) 28.2 12.8 1, 2236 AmpH Battery 19.2 8.7 22Articulated Landing Light (Required for Cat. A Operations) 9.2 4.2 1Rotor Brake Equipment 9.8 4.4Aux. Fuel Tank Equipment (39 US Gal.) 60.2 27.3Windshield Wiper (Pilot) (ECE) 9.8 4.4 5Windshield Wiper (Co-pilot) (ECE) 6.9 3.1 5Rear Clamshell Doors with windows 28.8 13.1Emergency Float Provisions (Electrical & Fixed) - for Floats without Life Rafts 23.3 10.6 6Emergency Floats without life rafts (Aerazur) (life vests not included) 129.6 58.8 6Emergency Float Provisions (Electrical & Fixed) - for Floats with Life Raft(s) 23.4 10.6 6Emergency Floats with one life raft, Left side (Aerazur) (life vests not included) 175.3 79.5 6Emergency Floats with two life rafts, Left & Right sides (Aerazur) (life vests notincluded) 220.9 100.2 6Emergency Floats Hoist Protection Cover (required for operation of rescue hoistwith with emergency floats installed) 1.6 0.7Ditching Kit (additional strengthening to a/c nose and belly) 3.4 1.5 7Life Vest Provisions, 4 place Stowage Pouches 0.5 0.2 7Life Vest Provisions. 5 place Stowage Pouches 0.6 0.3 7Life Vest Provisions, 6 place Stowage Pouches 0.8 0.4 7Emergency Egress, Standard Interior (push-out windows for hinged passengerdoors) 8.1 3.7 8Protected Tail-Rotor System 11.9 5.4 9Flashing Forward Light 0.6 0.3 4Passenger Steps - Single step each side -8.2 -3.7 10AUDIOAft Cabin ICS - 6 Place (Headsets not included) 2.5 1.1AVIONICSRadar Altimeter (Honeywell KRA 405B) (Required for Cat. A Operations) 5.5 2.5 1, 43rd Display Unit & 2nd Standby Compass (Required for Dual Pilot IFR) 23.6 10.7 3ADF (Honeywell KR 87) 10.6 4.8GNS-530W NAV/COMM/GPS (replaces Standard Equipment #1 GNS-430W) 2.2 1.0 4Wt(lb)Wt(kg)NotesThe 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. 16 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

AVIONICS (continued)7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationOptional Accessory Kits (continued)Kit DescriptionHTAWS Modification for GNS-530W:Wiring Provisions & HTAWS Data CardProjectedAvailability StatusWt(lb)Wt(kg)Notes 0.4 0.2 4Traffic Advisory System (Avidyne TAS620) 17.7 8.0 11Traffic Advisory System (Avidyne TAS605) 11.5 5.2 114th Axis Autopilot 4.5 2.0Weather Radar (Primus 660) 28.0 12.7ENGINEEngine Fuel Heater (PW207D2 Engine) (P&W) 4.3 2.0Compressor Wash Kit 1.4 0.6Inlet Barrier Filter 20.5 9.3Engine Fire Extinguisher - 2nd bottle 6.6 3.0ENVIRONMENTSingle Evaporator Air Conditioning with manual controls (AirComm) 84.5 38.3 12, 13Dual Evaporator Air Conditioning with manual controls (AirComm) 113.3 51.4 12, 13Bleed Air Heater Provisions (AirComm) 16.6 7.5Bleed Air Heater Equipment (with chin bubble defrost capability) 21.1 9.6EQUIPMENTCargo Hook Provisions (Onboard Systems) 12.0 5.4Cargo Hook Equipment, 3,000 lb. capacity (Onboard Systems) 31.4 14.2High Gross Weight Towing kit (AAI) (Required for towing at weight > 5,850 lb) N/A N/AMain Rotor Blade Folding Kit (2-fwd, 2-aft) (Paravion) 2nd Quarter 2012 1.0 0.5Quick Release Main Rotor Blade Bolts (4 bolts, 1 per blade; required for usewith Main Rotor Blade Folding Kit) 3.2 1.5Rescue Hoist Provisions, including Interior Trim modification 40.5 18.4 14, 15Rescue Hoist Equipment, Goodrich 600 lb. capacity 184.2 83.6 14, 15FLIGHT & ENGINE INSTRUMENTSCockpit Voice Recorder/Flight Data Recorder, Crashworthy 14.2 6.4Health & Usage Monitoring System (AAI) 18.0 8.2NVG Compatible Pilot Display Units and Flight Director (CHFD) 0.0 0.0 163rd Display Unit & 2nd Standby Compass with NVG Compatible 3rd DU 23.6 10.7 16NVG compatible lighting for all other light sources (may be US ITAR Controlled)Available ascustomized TBD TBD 16installationINTERIORHeadliner with LED lights & adjustable Air Conditioning vents 11.5 5.2 13Corporate Headliner with LED lights, adjustable Air Conditioning vents andcolour coordinated leather trim 11.8 5.4 13Corporate Interior, Single Pilot--Corporate Interior Trim--Plush Wool Carpets (for use with Single Pilot Controls) 9.3 4.2 18The 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 429 Product Specification - 7,500 lb IGW 17 © 2012 Bell Helicopter Textron Inc.January 2012

INTERIOR (continued)7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationKit DescriptionCorporate Interior, Dual Pilot--Corporate Interior Trim--Plush Wool Carpets (for use with Dual Pilot Controls)ProjectedAvailability StatusWt(lb)Wt(kg)Notes 9.0 4.1 18Cabin Soundproofing 10.0 4.5 17Aft Bulkhead Closeout panel 9.6 4.4 14, 17Aft Bulkhead Closeout panel with soundproofing 26.5 12.0 14, 17Utility Light Weight InteriorOptional Accessory Kits (continued)Available ascustomizedinstallation-20.0 -9.1Note: All interior option weight values are delta increase or decrease from standard configuration weights.PASSENGER SEATING OPTIONSCorporate 6-Place Seating, 18.5" wide seats with 3-point restraint system, quickrelease disconnects & ICS fixed provisions. 22.8 10.3Corporate 5-Place club seating with 1 centre console and side arm rests, 3-pointrestraint system, quick release disconnects & ICS fixed provisions. 31.6 14.3Corporate 4-Place club seating with centre consoles and side arm rests, 3-pointrestraint system, quick release disconnects & ICS fixed provisions. 33.2 15.1Seat Rail Removal -6.0 -2.7 2, 21Note: All passenger seating option weight values are weight increase or decrease from the standard configuration weights.VENDOR KITS - STCSliding Passenger Door Photo (Sliding) Window, L/H (AAI) 4.4 2.0 19Sliding Passenger Door Photo (Sliding) Window, R/H (AAI) 4.4 2.0 19Automatic Door Openers, Crew (2 door kit) (AAI) 1.9 0.9Automatic Door Openers, Passenger (2 door kit) (AAI) 2.2 1.0Wire Strike Protection System Detachable Equipment, skid gear a/c (AAI)RECOMMENDED 21.4 9.7 20Crew Floor Protectors - L/H & R/H (AAI) 5.2 2.4Cabin Floor Protectors (AAI) (Fwd & Aft) 9.1 4.1Cabin Floor Protector, Forward (AAI) 4.0 1.8Cabin Floor Protector, Aft (AAI) 5.1 2.3Cargo Mirror (AAI) 3.2 1.5Hard Point (Rappelling System) (AAI) 0.4 0.2 23Hard Point (Ceiling, Spotter) (AAI) 0.3 0.1 23Hard Point (Floor, Spotter) (AAI) 0.4 0.2 23Fuel Filler Area Protector (AAI) 0.1 0.0The 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. 18 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationOptional Accessories Explanatory Notes:1. Kits required for Category A Operations:••200 Amp Starter Generator (Dual)••Increased Capacity Battery (53 AmpH or 44 AmpH)••Articulated Landing Light••Radar Altimeter2. Standard Configuration kits removable and / or replaceable by customizing or optional accessory kit.3. Kits required for Dual Pilot IFR:••Dual Pilot Control Provisions••Dual Pilot Controls Equipment••3rd Display Unit and 2nd Standby CompassOptional Accessory Kits (continued)4. Optional Accessory Kits required for 7,500 lb. Internal Gross Weight Operations (ref. Transport Canadaapproved Flight Manual Supplement BHT-429-FMS-11):••Flashing Forward Light••Radar Altimeter••GNS-530W NAV/COMM/GPS (replaces Standard Equipment #1 GNS-430W)••HTAWS Modification for GNS-530W••Cockpit voice Recorder/Flight Data Recorder, Crashworthy5. The Bell 429 helicopter is certified for IFR operations without windshield wipers.••Installation of the Pilot Windshield Wiper kit does not require installation of the Co-pilot Windshield Wiperkit.••Installation of the Co-pilot Windshield Wiper requires installation of the Pilot windshield Wiper Kit.6. Emergency Floats Electrical and Fixed Provisions kits are required for installation of Emergency Floats.Each Emergency Float kit (removable equipment) consists of two removable integrated skid mountedmodules containing inflatable floats, inflation bottles and, if selected, an optional JAROPS compliant6-person life raft with survival equipment, giving customers a choice among three Emergency Floatconfigurations:••Emergency Floats without life rafts••Emegency Floats with one life raft (left side)••Emergency Floats with two life rafts••Towing or pushing the Bell 429 helicopter with ground handling wheels when the helicopter is equippedwith the emergency flotation system requires each flotation module to be removed from the landing gearand temporarily stowed on the ground handling wheels, using a float carrier pad and strap7. Ditching certification is is required for operations under European Joint Aviation Regulation JAR-OPS3.843(a) for Performance Class 1 or 2 flights over water in a hostile environment at a distance fromland corresponding to more than 10 minutes flying time at normal cruise speed. If ditching certificationis required, the following kits must be installed: Ditching Kit, Emergency Floats, and Life Vest ProvisionKits.8. Emergency Egress Kit is required for front row passenger emergency exit when Emergency Floats and5.5” standard 6-place seating kits are installed with passenger seats in airline seating arrangement withfront row of seats facing forward.9. The Protected Tail Rotor System is designed to prevent injury and provide a safe working environmentfor personnel who are in the vicinity of the aircraft.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 429 Product Specification - 7,500 lb IGW 19 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationOptional Accessory Kits (continued)10 Optional kit to replace full length standard configuration passenger steps, if full length steps are notrequired. Single step kit is not compatible with airline configuration passenger seat installation.11. Avidyne TAS605 Traffic Avoidance System is a lighter weight system available as a customizedinstallation. See page 9 of the Bell 429 Product Specification for features comparison.12. Air Conditioning Quill Drive and Provisions are included in Standard Configuration.13. Headliner with adjustable air vents, p/n 429-706-202-107 or 429-706-202-109, is recommended for moreeffective cooling when air conditioning is installed.14. Aft Cabin Bulkhead Closeout, if installed, must be removed for Rescue Hoist Operations.15. Right side aft passenger seat must be removed for installation of the Rescue Hoist Control Box PendentBracket. Pendent bracket is removable when pendent is not installed for mission use.16. Complete NVG compatible lighting consists of the following optional accessories:••p/n 429-706-022-101, -105 , or -109 replaces the standard #1 & #2 Display Units and CHFD panel withNVG compatible units••p/n 429-706-022-103, -107, or -111 should be selected instead of p/n 429-706-026-101, -103, or -105 forNVG compatible 3rd Display Unit••NVG compatible lighting treatment for other internal and external light sources, including NVG lightingfor the standby compasses and cabin black-out curtains, will vary depending upon specific aircraftconfiguration. Aerodynamix STC’d NVG lighting is avaliable as a customized installation.17. For effective internal noise reduction, Aft Cabin Bulkhead panel, p/n 429-706-060-103 or 429-706-060-105, is strongly recommended when cabin soudproofing is installed.18. Standard Configuration floor covering includes a customer choice of materials, either durable low loopnylon blend carpet or ”Aermat” vinyl floor covering. Either single pilot or dual pilot standard carpet isincluded in Standard Configuration Price. Corporate Interior floor covering is plush 100% wool carpet,colour coordinated to match leather seat upholstery.19. Three Passenger Door Sliding Window colour options available:••p/n 429-564-007, L/H (Gray)••p/n 429-564-009, L/H (Medium Gray)••p/n 429-564-011, L/H (Dark Gray)••p/n 429-564-008, R/H (Gray)••p/n 429-564-010, R/H (Medium Gray)••p/n 429-564-012, R/H (Dark Gray)20. Wire Strike Protection System Provisions are included in Standard Configuration.21. Passenger Seat Rail Removal kit required for installation of AMC or Aerolite EMS Interior Systems.22. Installation of 53 AmpH, 44 AmpH or 36 AmpH battery requires installation of the 200 Amp StarterGenerator kit. However, installation of 200 Amp Starter Generator does not require installation of the 53AmpH battery.23. At least one Spotter hardpoint is required for Rescue Hoist or Rappelling Operations.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. 20 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationHelicopter Performance ChartsIGE & OGE Hover and Service CeilingsPratt & Whitney Canada PW207D1/D2 EnginesMinimum Specification Engine PowerBasic Inlet or Barrier Filter InstalledAir Conditioning / Heater OffSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 21 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationM429 IGE HOVER CEILINGTWIN ENGINE OPERATION IGE Hover Ceiling AT TAKEOFF POWERCLEAN Twin INLET Engine BARRIER Operation FILTER at Takeoff INSTALLEDPowerClean Inlet ZERO Filter WIND Installed, ORZero HEADWIND Wind or HeadwindGROSS WEIGHT - 100 KG21 22 23 24 25 26 27 28 29 30 31 32 33 34201918ISA+30°CISA+20°CISA+10°CISA60561752PRESSURE ALTITUDE - 1000 FT1615141312111098765- 10 °CMAX OAT LIMIT (ISA+36 . 7°C)30°C20°C10°C- 40 °C- 30 °C- 20 °C0°C40°C484440363228242016PRESSURE ALTITUDE - 100 METERS43210SKID HEIGHT 4 FT (1 . 2M)46 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76GROSS WEIGHT - 100 LBMAX INT GW 7000 LBSALTERNATE MAXINT GW & MAX EXTGW 7500 LBS12840Specifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 22 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationM429 OGE HOVER CEILINGTWIN ENGINE OPERATION OGE Hover Ceiling AT TAKEOFF POWERCLEAN Twin INLET Engine BARRIER Operation FILTER at Takeoff INSTALLEDPowerClean Inlet ZERO Filter WIND Installed, ORZero HEADWIND Wind or HeadwindGROSS WEIGHT - 100 KG21 22 23 24 25 26 27 28 29 30 31 32 33 34PRESSURE ALTITUDE - 1000 FT201918171615141312111098765ISA+20°CISA+10°CISAISA+30°CMAX OAT LIMIT (ISA+36 . 7°C)0°C10°C40°CMAX INT GW 7000 LBS- 40 °C30°C- 30 °C- 20 °C- 10 °CALTERNATE MAX INT GW& MAX EXT GW 7500 LBS20°C605652484440363228242016PRESSURE ALTITUDE - 100 METERS41232184046 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76GROSS WEIGHT - 100 LB0Specifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 23 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationM429 SERVICE CEILINGTWIN ENGINE AT Service MAX CONTINUOUS Ceiling POWERCLEAN Twin Engine INLET at BARRIER Maximum FILTER Continuous INSTALLED PowerClean Inlet ZERO Filter WIND Installed, ORZero HEADWIND Wind or HeadwindGROSS WEIGHT - 100 KG21 22 23 24 25 26 27 28 29 30 31 32 33 34201918ISA+30°CISA+20°CISA+10°CISA- 40 °C- 30 °C605617MAX OAT LIMIT (ISA+36 . 7°C)- 20 °C52PRESSURE ALTITUDE - 1000 FT16151413121110987654321010°CMAX INT GW 7000 LBS- 10 °C0°C20°C30°CALTERNATE MAX INT GW& MAX EXT GW 7500 LBS48444036322824201612840PRESSURE ALTITUDE - 100 METERS46 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76GROSS WEIGHT - 100 LBSpecifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 24 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationM429 OEI SERVICE CEILINGOEI OEI 30 Sevice MINUTECeilingPOWERCLEAN INLETOEI BARRIER 30-Minute FILTER Power INSTALLEDClean Inlet ZERO Filter WIND Installed, ORZero HEADWIND Wind or HeadwindGROSS WEIGHT - 100 KG21 22 23 24 25 26 27 28 29 30 31 32 33 34PRESSURE ALTITUDE - 1000 FT201918171615141312111098765ISA+30°CISA+20°CISA+10°CMAX OAT LIMIT (ISA+36 . 7°C)ISA0°C40°C30°C- 40 °C- 30 °CMAX INT GW 7000 LBS- 20 °C- 10 °C20°CALTERNATE MAX INT GW& MAX EXT GW 7500 LBS10°C605652484440363228242016PRESSURE ALTITUDE - 100 METERS412321050°C46 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76GROSS WEIGHT - 100 LB840Specifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 25 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationM429 OEI SERVICE CEILINGOEI CONTINUOUS OEI Sevice Ceiling POWERCLEAN INLET OEI BARRIER Continuous FILTER Power INSTALLEDClean Inlet ZERO Filter WIND Installed, ORZero HEADWIND Wind or HeadwindGROSS WEIGHT - 100 KG21 22 23 24 25 26 27 28 29 30 31 32 33 34PRESSURE ALTITUDE - 1000 FT201918171615141312111098765ISA+30°CISA+20°CISA+10°CMAX OAT LIMIT (ISA+36 . 7°C)ISAMAX INT GW 7000 LBS20°CALTERNATE MAX INT GW& MAX EXT GW 7500 LBS- 40 °C- 30 °C- 20 °C- 10 °C0°C10°C605652484440363228242016PRESSURE ALTITUDE - 100 METERS430°C1232184046 48 50 52 54 56 58 60 62 64 66 68 70 72 74 76GROSS WEIGHT - 100 LB50°C40°C0Specifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 26 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationFuel Flow vs. AirspeedISA & ISA+20°CNew Pratt & Whitney CanadaPW207D1/D2 EnginesBasic Inlet or Barrier Filter InstalledClean Configuration with Standard Skid GearAir Conditioning / Heater OffSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 27 © 2012 Bell Helicopter Textron Inc.January 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA) _ 00K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) SEA LEVELPressure OAT Altitude= 15°C = Sea LevelOAT = 15°C (ISA)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680100660640TRANSMISSION LIMIT30029095620280TORQUE - %90858075706560555045403530FUEL FLOW - LB/HR600580560540520500480460440420400380360340320300280260656055507570MAXENDUR .GW x 100 LBLRCV NE270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150 160 170INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 28 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA) _ 02K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 2000 FTPressure OAT Altitude= 11°C = 2,000 FTOAT = 11°C (ISA)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680100660640TRANSMISSION LIMIT300290TORQUE - %959085807570656055FUEL FLOW - LB/HR620600580560540520500480460440420MAXENDUR .LRC280270260250240230220210200190FUEL FLOW - KG/HR5040018045403530380360340320300280260706560555075GW x 100 LBV NE17016015014013012040 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150 160 170INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 29 © 2012 Bell Helicopter Textron Inc.January 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA) _ 04K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 4000 FTPressure OAT Altitude= 7°C = 4,000 FTOAT = 7°C (ISA)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300TORQUE - %1009590858075706560555045403530FUEL FLOW - LB/HR640620600580560540520500480460440420400380360340320300280260TRANSMISSION LIMIT706560555075MAXENDUR .GW x 100 LBLRCV NE290280270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150 160INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 30 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA) _ 06K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 6000 FTPressure OAT Altitude= 3°C = 6,000 FTOAT = 3°C (ISA)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300TORQUE - %100959085807570656055FUEL FLOW - LB/HR640620600580560540520500480460440420400TRANSMISSION LIMITMAX CONTINUOUS POWERMAXENDUR .LRC290280270260250240230220210200190180FUEL FLOW - KG/HR5045403530380360340320300280260507065605575GW x 100 LBV NE17016015014013012040 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150 160INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 31 © 2012 Bell Helicopter Textron Inc.January 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA) _ 08K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 8000 FTPressure OAT Altitude= - 1 °C = 8,000 FTOAT = -1°C (ISA)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300100640620290280TORQUE - %9590858075706560555045403530FUEL FLOW - LB/HR600580560540520500480460440420400380360340320300280260MAX CONTINUOUS POWER656055507075MAXENDUR .GW x 100 LBLRCV NE270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 32 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA) _ 10K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 10 , 000 FTPressure OAT Altitude= - 5 =°C 10,000 FTOAT = -5°C (ISA)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300100640620290280TORQUE - %9590858075706560555045403530FUEL FLOW - LB/HR600580560540520500480460440420400380360340320300280260MAX CONTINUOUS POWER7065605550MAXENDUR .75GW x 100 LBLRCV NE270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 33 © 2012 Bell Helicopter Textron Inc.January 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA+20) _ 02K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 2000 FTPressure OAT Altitude= 31°C = 2,000 FTOAT = 31°C (ISA + 20)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680TORQUE - %1009590858075706560555045403530FUEL FLOW - LB/HR66064062060058056054052050048046044042040038036034032030028026050MAX CONTINUOUS POWER7060556575MAXENDUR .GW x 100 LBLRCV NE300290280270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150 160INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 35 © 2012 Bell Helicopter Textron Inc.January 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA+20) _ 04K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 4000 FTPressure OAT Altitude= 27°C = 4,000 FTOAT = 27°C (ISA + 20)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300100640290TORQUE - %9590858075706560555045403530FUEL FLOW - LB/HR620600580560540520500480460440420400380360340320300280260MAX CONTINUOUS POWER656055507075MAXENDUR .GW x 100 LBLRCV NE280270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150 160INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 36 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA+20) _ 06K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 6000 FTPressure OAT Altitude= 23°C = 6,000 FTOAT = 23°C (ISA + 20)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300100640290TORQUE - %9590858075706560555045403530FUEL FLOW - LB/HR620600580560540520500480460440420400380360340320300280260MAX CONTINUOUS POWER656055507075MAXENDUR .GW x 100 LBLRCV NE280270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 37 © 2012 Bell Helicopter Textron Inc.January 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA+20) _ 08K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 8000 FTPressre OAT Altitude= 19°C = 8,000 FTOAT = 19°C (ISA + 20)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300100640290TORQUE - %9590858075706560555045403530FUEL FLOW - LB/HR620600580560540520500480460440420400380360340320300280260MAX CONTINUOUS POWER6055506570MAXENDUR .75GW x 100 LBLRCV NE280270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140 150INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.© 2012 Bell Helicopter Textron Inc. 38 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

FILENAME: M429 _ FFL _ CHART _ (WNE __ ISA+20) _ 10K . EMFDATED: 21 NOVEMBER 20117,500 lb (3,402 kg) Increased InternalFUEL Gross FLOW Weight VS Configuration AIRSPEEDFuel Flow vs. AirspeedZERO WINDCLEAN INLET BARRIERZero WindFILTER INSTALLED(MCP BASED ON WORSE NEWClean Inlet Barrier Filter InstalledENGINE)PRESSURE (MCP Based ALTITUDE on New = Engine) 10 , 000 FTPressre Altitude OAT = 15°C = 10,000 FTOAT = 15°C (ISA + 20)TRUE AIRSPEED - KM/HR80 100 120 140 160 180 200 220 240 260 280 300 320680660300100640290TORQUE - %9590858075706560555045403530FUEL FLOW - LB/HR620600580560540520500480460440420400380360340320300280260MAX CONTINUOUS POWER5550606570MAXENDUR .75GW x 100 LBLRCV NE280270260250240230220210200190180170160150140130120FUEL FLOW - KG/HR40 50 60 70 80 90 100 110 120 130 140 150 160 170 180TRUE AIRSPEED - KNOTS40 50 60 70 80 90 100 110 120 130 140INDICATED AIRSPEED - KNOTSSpecifications subject to change without notice.Bell 429 Product Specification - 7,500 lb IGW 39 © 2012 Bell Helicopter Textron Inc.January 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationPage Intentionally Left Blank© 2012 Bell Helicopter Textron Inc. 40 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell 429 Maintenance ProgramDesigned through Maintenance Steering Group - 3 (MSG-3)Bell Helicopter understands the importance of aircraft reliability to meet your mission needs. That’s why ourmaintenance philosophy is to streamline maintenance requirements to ensure low direct operating costs, lowdirect maintenance costs, and improved reliability by utilizing the Maintenance Steering Group – 3 (MSG-3)while increasing occupant safety.The Bell 429 is the first rotorcraft designed through the MSG-3 in the creation of a maintenance schedule on acommercial helicopter with the support of the Aviation authorities, mainly Transport Canada (TC), the FederalAviation Administration (FAA) and the European Aviation Safety Agency (EASA).During the Customer Maintenance Advisory Panel (CMAP) meetings, the team analyzed every aircraftsystem, including airframe structure and wiring installation, to determine the failure modes, their criticality,the ease of detection, the level of inspection required and the ideal recurrence of inspection. This is wherethe varied experience of the team came in to play; Aircraft Maintenance Engineers (AME) / Airframe & PowerPlant (A&P) technicians also provided input as to the system detailed functions and used their many yearsof experience in aircraft operation, respectively. From this resulted a maintenance schedule that requires35% less maintenance man hours versus a comparable aircraft, thus improving the cost of ownership for theBell 429.The following are excellent features derived through MSG-3 for the Bell 429:••Approved Maintenance Program (TC)--First rotorcraft to use the MSG-3 Process••Certification through MSG-3 Process--Same process used by commercial airlines to ensure continued airworthiness--Determines how and when maintenance will be performed--Helicopter designed and built for maintenance••Accessible panels to aircraft systems••Maintenance Program--Task Intervals* Every 200 hours* 800 hours/12 month* Zonal InspectionProgram introduced--Life Limited Parts* CompositeComponents –On Condition* Metallic Components –10,000 + hours (Goal)* ElastomericComponents – 5000hoursBell 429 Product Specification - 7,500 lb IGW 41 © 2012 Bell Helicopter Textron Inc.January 2012

--Zonal Inspections* General Visual Inspections7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell 429 Maintenance Program (continued)* Part of Scheduled Inspection Program* Start at 12-month* Extent out to 10-Years* Reduce Scheduled Inspection repeats••Instructions for Continued Airworthiness (ICA)* Maintenance Manual & Flight Manual* Maintenance Manual accepted by TC* Maintenance Program approved by TC* Flight Manual approved by TC* Wear and repair damage limits included in initial release to customers••Scheduled Maintenance and Component InspectionsBell 429 Scheduled Maintenance InspectionsInspection Individual Task Hours Cumulative Task Hours Notes200 hour 0.16 hrs 0.16 hrs400 hour 5.00 hrs 5.16 hrs includes 200 hr600 hour 3.16 hrs 3.32 hrs includes 200 hr600 hour / 12 month 4.00 hrs 4.00 hrs800 hour 15.892 hrs 21.212 hrs includes 200 & 400 hr12 month 2.038 hrs 2.038 hrs2 year 5.68 hrs 7.718 hrs includes 12 month3 year 1.19 hrs 3.228 hrs includes 12 month4 year 13.12 hrs 20.838 hrs includes 12 month & 2 year5 year 2.50 hrs 4.538 hrs includes 12 month6 year 5.15 hrs 14.058 hrs includes 12 month, 2 & 3 year8 year 10.00 hrs 30.838 hrs includes 12 month, 2 & 4 year10 year 8.19 hrs 18.408 hrs includes 12 month, 2 & 5 yearBell 429 Scheduled Component InspectionsComponent Interval Removal Overhaul Installation Follow Up TotalSwashplate andSupport5000hr 1hr 33hr 1hrFriction check1.5hrMast Assembly 5000hr 1hr 20hr 1hr N/A 22hrMain RotorGearbox5000hr 11hr 150hr 16hr N/A 177.5hrT/R Gearbox 5000hr 2hr 27hr 4hr T.Q. check 1hr 34hrMain RotorHead5000hr 2hr 80hr 3hr T.Q. check 1hr 85hrT/R Hub 5000hr 1hr 12hr/hub 2hr T.Q. check 1hr 14hr/hub36.5hr© 2012 Bell Helicopter Textron Inc. 42 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell 429 TrainingBell Helicopter has trained more than 120,000 pilotsand maintenance technicians from over 120 countriessince opening the Bell Helicopter Training Academy(BTA) in 1946. The Training Academy currently trainsapproximately 2,000 pilots and 1,800 maintenancetechnicians each year.Highly trained professionals in courseware developmentand classroom instruction are part of the Bell Helicopterteam. BTA courseware developers and technicalinstructors have over 200 years of combined maintenanceexperience, and BTA instructor pilots have an averageexperience level of 12,500 flight hours.Pilot and maintainer courses have been developed forthe Bell 429 to ensure that the training suite matches thecapabilities of the Bell 429 helicopter. The complete suiteconsists of advanced course materials complemented bya Flight Training Device constructed to U.S. FAA Level7 certification requirements (certified to Level 6), and acomposite maintenance trainer which provides hands-ontraining for maintenance tasks.The Bell Helicopter Training Academyoffers World Class Training Solutions••FAA Certified••Over 60 years of continuous operations••Over 120,000 pilot and maintenanceengineers trained from over 120 countries••Flight Training Devices (FTD) available forenhanced pilot training• • Maintenance and technical instructorshave over 375 years of combined trainingexperienceFor additional information about the BTA, please visit ourwebsite, www.bellhelicopter.com, and click on “Training”.Bell 429 Training Course SummaryThe courses offered for the Bell 429 helicopter are listedin the table below. Complimentary training is offered witheach new Bell 429 helicopter delivery for two positions inBell Helicopter Training Academy (BTA)Alliance Airport north of Fort Worth, Texas.the Bell 429 Pilot Transition Course and one position each in the Bell 429 Field Maintenance and IntegratedAvionics Systems (IAS) courses.Course Training Hours DurationBell 429 Pilot Transition Course (Ground & Flight Procedures): VFR IFR TotalClassroom Training20 4 24Flight Training Device4 2 65 to 8 daysTransition Flight Training in BTA’s Bell 429 2up to 5 up to 3 up to 8Bell 429 Pilot Refresher CourseClassroom Training16 hoursFlight Training Device2 hours~ 3 daysFlight Training2 hoursBell 429 Field Maintenance 120 hours 3 weeksBell 429 Ingegrated Avionics Systems (IAS) 40 hours 1 weekBell 429 Field Maintenance Refresher Course 24 hours ~ 3 daysBell 429 Component Overhaul 80 hours 2 weeksBell 429 Product Specification - 7,500 lb IGW 43 © 2012 Bell Helicopter Textron Inc.January 2012

Bell 429 Course DescriptionsPilot Training:7,500 lb (3,402 kg) Increased InternalGross Weight ConfigurationBell 429 Training (continued)Bell Helicopter recognizes that pilots have different backgrounds and experience levels. For that reason theclassroom instruction, flight training device (FTD) and flight training are designed to prepare each attendeeto successfully meet the course standards. The standards followed by the instructor reflect the standardsrequired for aircraft operation by FAA regulations and Bell Helicopter. Training is considered complete withdemonstrated knowledge of aircraft systems and proficiency in flight maneuvers appropriate to the course ofinstruction.This course provides pilots with a comprehensive knowledge of the aircraft systems and components anda thorough understanding of the operational characteristics and flight limitations. Classroom presentationscover the cockpit controls and instrumentation, airframe, power-plant and all aircraft systems. In addition,normal procedures, emergency procedures, operating limitations and performance are studied.The flight training includes complete familiarization of the Bell 429 helicopter, instruction in the turbine engineoperation and flight instruction in normal flight maneuvers and emergency procedures. Instruction in theflight training device (FTD) simulates emergency procedures including FADEC failure modes, hydraulic boostfailure, auto-rotations and tail rotor failure.Maintenance Training:Bell 429 Field Maintenance CourseThis three weeks course provides a comprehensive coverage of the description, function, and maintenanceprocedures required for field maintenance of the Bell 429 helicopter. The following topics are covered duringclassroom or shop work: Airframe, Ground Handling and Servicing, Main Rotor, Mast, Rotating Controls,Transmission, Main Drive Shaft, Power-plant Interface (installation and rigging as related to the airframe), FuelSystem, Tail Rotor, Tail Rotor Drive, Hydraulic System, Flight Controls, Electrical System, and Utility Systems.This course meets the EASA Part 66 B1.3 requirements.Bell 429 Integrated Avionics CourseThis three week 429 Integrated Avionics Systems course will cover Wiring and Installation, Integrated AvionicsSystem, DC Power System, DC Power Distribution, Engine Electrical and Electronic Engine Control System,Drive System Electrical, Airframe Systems Electrical, and an Examination and Review. This course meetsEASA B.2 requirements.The following additional courses are available:••Bell 429 Component Overhaul (2 weeks course)••Bell 429 Pilot Refresher Course (3 days)••Bell 429 Field Maintenance Refresher (3 days)Note:Actual flight training time flown will be based on student pilot proficiency and is not intended as an absolute value.© 2012 Bell Helicopter Textron Inc. 44 Bell 429 Production Specification - 7,500 lb IGWJanuary 2012

P.O. Box 482, Fort Worth, Texas 76101Phone: 817-280-2800Fax: 817-278-8802www.bellhelicopter.comBell Helicopter Textron Canada Limited12,800 rue de l’ AvenirMirabel, Quebec, Canada J7J1R4Phone: 450-437-3400Fax: 450-437-2006©2012 Bell Helicopter Textron Inc.All Rights Reserved. Printed in the USA.429 Manual Cover-IGW.indd 2 2/8/12 10:32 AM