SPECIFICATIONS

(26.4 cm) displays provides critical flight information for crews at a glance, enhancing situational awareness and safety. The reliability, speed, performance, and maneuverability of the Bell 505 helicopter is integrated with a flat floor, open cabin that is configurable for a wide variety of missions and payloads. The spacious cabin can be configured to carry up to 4 passengers or for internal cargo missions by removing rear cabin seats and/or copilot seat. Passenger comfort is enhanced with a quiet and smooth ride along with a large rear cabin that provides ample legroom and headroom. Clamshell doors, located on the left (copilot) side, open to a wide 55 inches (140 cm) to allow for easy ingress/egress from the aircraft. Large rear cabin windows and wrap around windscreens in the cockpit provide excellent visibility for passengers and enhance situational awareness for the crew. These features combined with a proven and reliable drivetrain and rotor system make the Bell 505 a true multi-mission aircraft in the short light single-engine market. The Bell 505 design team has developed the aircraft with direct input from a council of customer advisors representing expertise in all facets of the helicopter industry. The customer advisory council has participated in the aircraft design process since 2011 and has provided critical input to the following areas: y Baggage capacity and access y Engine and avionics suppliers y Kit configurations y Maintenance access y Fleet integration y Training requirements y Operating economics y Payload range capability y Cockpit integration and situational awareness y Cabin comfort y Maintainability/supportability The platform is certified to the most recent TCCA, FAA and EASA Part 27 regulations and is the first helicopter in its class to utilize MSG-3 to develop the aircraft maintenance plan. Bell’s products are backed by our renowned in-service support. The Bell 505 proves you don’t have to sacrifice comfort for performance. The Bell 505. BELL 505 SPECIFICATIONS 2 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. The World’s Most Advanced Short Light Single GARMIN G1000H NXi INTEGRATED AVIONICS SYSTEM The Bell 505, featuring the Garmin G1000H NXi Integrated Avionics System, provides unparalleled crew situational awareness through the use of a fully integrated glass flight deck coupled with an advanced dual channel FADEC engine control system, resulting in enhanced safety levels and mission capabilities. The cockpit design features a wrap around windscreen offering excellent crew visibility that results in increased situational awareness and safety. The aircraft systems are fully-integrated with the Garmin G1000H NXi avionics suite to display critical flight instruments, audio alerts and Crew Alerting System (CAS) messages. One of the design goals for the Bell 505 team was to increase ease of operations and lower pilot workload. These goals have been realized through the combination of an advanced FADEC engine control system and a fully-integrated avionics suite. The Bell 505 Garmin G1000H NXi Flight Deck provides the next level of safety. SPECIFICATIONS BELL 505 FEBRUARY 2026 3 © 2026 Bell Textron Inc. Specifications subject to change without notice. The World’s Most Advanced Short Light Single BELL 505 DUAL CHANNEL FADEC ENGINE CONTROLS As the first helicopter in its class to offer a dual channel Full Authority Digital Engine Control (FADEC) and fully integrated glass cockpit, the Bell 505 is the future of safety. The Safran Arrius 2R engine control is provided through a dual channel FADEC which increases operational safety by lowering pilot workload. The dual channel FADEC offers added protection with the incorporation of an automatic backup Auxiliary Control Unit. There are many features on the Safran Arrius 2R engine that increase safety and truly differentiate it from the competition including: y Dual-channel FADEC y Auxiliary Control Unit (backup for HMU) y Automatic startup y Surge and flame-out protection y Engine parameter recording for maintenance (BOOST compatible) y Data stored in avionics for easy access y Automatic cycle and flight hour counting The Bell 505’s Safran Arrius 2R Engine features a dual channel FADEC with automatic backup. BELL 505 SPECIFICATIONS 4 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Specification Summary (U.S. Units) WEIGHTS (LB) Empty Weight (Base Aircraft) 2,180 External Load Gross Weight 4,475 Internal Gross Weight 3,680 Maximum External Load (Cargo Hook Limit) 2,000 Useful Load (Base Aircraft) 1,500 PERFORMANCE SUMMARY (International Standard Day except as noted) Takeoff Gross Weight (lb) 3,000 3,400 3,680 IGE Hovering Ceiling ISA ft 20,000 17,100 14,450 ISA + 20 °C ft 16,320 12,300 9,700 ISA + 30 °C ft 14,240 9,980 6,650 OGE Hovering Ceiling ISA ft 17,400 13,250 10,460 ISA + 20 °C ft 12,740 8,580 5,430 ISA + 30 °C ft 10,590 5,400 1,620 Service Ceiling (MCP), 100 ft/min ISA ft 20,000 20,000 18,610 ISA + 20 °C ft 20,000 17,020 14,590 ISA + 30 °C ft 19,000 15,160 12,410 Maximum Cruise Speed (True Airspeed) SL, ISA ktas 128 126 125 SL, ISA + 20 °C ktas 123 121 118 Cruise at Long Range Cruise Speed (LRC) Range (Standard Fuel, No Reserve) SL, ISA nmi 318 311 306 LRC Speed (Average True Airspeed) ktas 113 112 112 Range (Standard Fuel, No Reserve) 4000 ft, ISA nmi 355 344 333 LRC Speed (Average True Airspeed) ktas 112 113 112 Endurance at Loiter Speed (60 kias) (Standard Fuel, No Reserve) SL,ISA hr 4.1 4.0 3.9 4000 ft, ISA hr 4.5 4.3 4.2 ENGINE RATING TRANSMISSION RATING (Engine Output) Safran Arrius 2R (uninstalled thermodynamic rating) Takeoff Horsepower (5 minutes) 475 SHP Takeoff Horsepower 505 SHP Maximum Continuous 428 SHP Maximum Continuous 459 SHP FUEL CAPACITY (Usable) Type Aviation Turbine Standard 84.85 US Gallons FEBRUARY 2026 BELL 505 SPECIFICATIONS 5 © 2026 Bell Textron Inc. Specifications subject to change without notice. Specification Summary (Metric Units) WEIGHTS (KG) Empty Weight (Base Aircraft) 989 External Load Gross Weight 2,030 Internal Gross Weight 1,669 Maximum External Load (Cargo Hook Limit) 907 Useful Load (Base Aircraft) 680 PERFORMANCE SUMMARY (International Standard Day except as noted) Takeoff Gross Weight (kg) 1,361 1,542 1,669 IGE Hovering Ceiling ISA m 6,096 5,212 4,404 ISA + 20 °C m 4,974 3,749 2,957 ISA + 30 °C m 4,340 3,042 2,027 OGE Hovering Ceiling ISA m 5,304 4,039 3,188 ISA + 20 °C m 3,883 2,615 1,655 ISA + 30 °C m 3,228 1,646 494 Service Ceiling (MCP), 0.5 m/sec ISA m 6,096 6,096 5,672 ISA + 20 °C m 6,096 5,188 4,447 ISA + 30 °C m 5,791 4,621 3,783 Maximum Cruise Speed (True Airspeed) SL, ISA km/h 237 233 231 SL, ISA + 20 °C km/h 228 224 218 Cruise at Long Range Cruise Speed (LRC) Range (Standard Fuel, No Reserve) SL, ISA km 588 576 566 LRC Speed (Average True Airspeed) km/h 209 208 208 Range (Standard Fuel, No Reserve) 1,200 m, ISA km 657 638 617 LRC Speed (Average True Airspeed) km/h 208 208 208 Endurance at Loiter Speed (60 kias) (Standard Fuel, No Reserve) SL,ISA hr 4.1 4.0 3.9 1,200 m, ISA hr 4.5 4.3 4.2 ENGINE RATING TRANSMISSION RATING (Engine Output) Safran Arrius 2R (uninstalled thermodynamic rating) Takeoff Horsepower (5 minutes) 354 kW Takeoff Horsepower 377 kW Maximum Continuous 319 kW Maximum Continuous 342 kW FUEL CAPACITY (Usable) Type Aviation Turbine Standard 321 Liters BELL 505 SPECIFICATIONS 6 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Helicopter Dimensions EXTERNAL DIMENSIONS – STANDARD Bell 505 External Dimensions. Bell 505. FEBRUARY 2026 BELL 505 SPECIFICATIONS 7 © 2026 Bell Textron Inc. Specifications subject to change without notice. Helicopter Dimensions EXTERNAL DIMENSIONS – HIGH SKID GEAR Bell 505 External Dimensions. Bell 505 with high skid gear. BELL 505 SPECIFICATIONS 8 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Helicopter Dimensions INTERNAL DIMENSIONS Dimension * in cm Volume * US Units Metric A 56 142 Total cabin volume (excluding pilot area) 99 ft3 2.80 m3 B 53 135 Rear cabin volume 61 ft3 1.73 m3 C 33 84 Copilot volume 38 ft3 1.08 m3 D 53 135 Floor Loading * E 18 46 Total cabin floor area (excluding pilot area) 22 ft2 2.04 m2 F 55 140 Cabin floor loading 55 lb/ft2 269 kg/m2 G 32 82 Cargo loading not to exceed 425 lb 192 kg NOTE: * Volumes and dimensions are approximate. FEBRUARY 2026 BELL 505 SPECIFICATIONS 9 © 2026 Bell Textron Inc. Specifications subject to change without notice. Helicopter Dimensions INTERNAL DIMENSIONS Dimension * in cm Baggage compartment * A 32 82 Baggage volume 18 ft3 0.51 m3 B 55 140 Baggage Floor Loading * C 25 65 Baggage floor loading 50 lb/ft2 244 kg/m2 D 18 46 Total baggage floor capacity 250 lb 113 kg E 22.2 56.4 F 16.1 41 NOTE: * Volumes and dimensions are approximate. E F BELL 505 SPECIFICATIONS 10 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Garmin G1000H NXi Integrated Avionics System The Bell 505 is the first helicopter in its class to incorporate a fully integrated flight deck. The Garmin G1000H NXi Avionics System, featuring dual 10.4-inch (26.4 cm) displays, is designed to improve situational awareness and reduce pilot workload through easy to read displays of critical flight information, tuning of communication and navigation frequencies, and simple flight planning management. The Bell 505’s standard configuration Garmin G1000H NXi Flight Deck can be upgraded to include Helicopter Synthetic Vision Technology (HSVT) that gives pilots a 3D depiction of terrain, obstacles, traffic and more in any visibility condition. The PFD boasts a Power Situation Indicator (PSI) to provide critical flight information in a centralized location. The system has two SD card slots to facilitate data input/output tasks such as flight plan and database uploading or critical flight data downloads. The system takes advantage of the latest in display, computer processing, and digital data bus technology to provide a high degree of redundancy, reliability, and flexibility. The basic ship main components of the Garmin G1000H NXi Integrated Avionics system includes: y Two 10.4-inch (26.4 cm) GDU high-resolution LED displays y One GIA 64H integrated avionics units, including: – GPS / WAAS receiver – VHF COM transceiver – VHF NAV and glideslope receivers – Aural alert generation y GEA 71BH Engine and airframe unit (signal processing of engine parameters and major system sensors) y GMA350Hc Audio panel y GTX 335R Extended Squitter (ES) Mode S transponder y GSU 75H Air Data Attitude Heading Reference Unit (ADAHRS) y GMU 44 magnetometer y Standby Attitude Module (SAM) BELL 505 FLIGHT DECK System Description Two-display system Two 10.4-inch (26.4 cm) flat panel high-resolution LEDs, interchangeable for Primary Flight Display (PFD) or Multi-Function Display (MFD) Flight Instruments Integrated on PFD with stand-by Flight Display Engine Instruments Integrated on PFD / MFD with Power Situation Indicator (PSI), Engine Indication System (EIS), fuel flow, automated power assurance check EICAS & Audio Alerts Engine Indicating and Crew Alerting System (EICAS) integrated on PFD / MFD Audio alerts integrated into intercom system COM/NAV Single COM / NAV / GPS, WAAS, Mode S Transponder with Extended Squitter (ES), ADS-B out, FMS, auto-tuning Situational Awareness Integrated on PFD / MFD, Traffic Information System (TIS), Moving Map, Fuel and NAV range, optional TAS with active and passive (ADS-B) surveillance, HTAWS, and Synthetic Vision System Intercom 5-place ICS with recorder / playback, Headsets have Bluetooth support for phones, Garmin MP3 jack (customizing), Automatic Speech Recognition SPECIFICATIONS BELL 505 FEBRUARY 2026 11 © 2026 Bell Textron Inc. Specifications subject to change without notice. Garmin G1000H NXi Integrated Avionics System STANDBY ATTITUDE MODULE (SAM) The SAM is entirely self contained and provides attitude, altitude, airspeed and slip information in a small package measuring just two inches by five inches and weighing 1.6 lb (.72 kg). The SAM contains two LED-backlit LCDs, one displaying attitude and the other airspeed and altitude. The unit is powered by a back-up battery that runs for at least 60 minutes if primary aircraft power is lost. DISPLAYS The Garmin G1000H NXi flight deck presents critical flight information to the pilot at a glance for greater situational awareness, simplicity and safety. The pilot can easily and quickly select the information formats to display on the interchangeable Primary Flight Display (PFD) and Multi-Function Display (MFD). The Power Situation Indicator (PSI), located in the lower left-hand corner of the PFD provides a “one stop shop” for power indications and limits. Primary Flight Display (PFD) Typical User Selected Formats: The PFD displays all major flight parameters in an intuitive, easy to scan layout: Attitude, Airspeed, HSI, Altitude and VSI. Primary and inset screens can be user- selected to display a variety of additional functions, including “Pathways in the Sky”, Flight Path Vector, Synthetic Vision [1], HTAWS [1], and Traffic Information System (TIS) [2] . Notes: [1] Available as an optional kit. [2] The GTS 800 TAS (Traffic Advisory System) is available as an optional kit. MFD Traffic Display Standby Attitude Module (SAM) PFD Synthetic Vision with HIS Map and WireAware BELL 505 SPECIFICATIONS 12 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Garmin G1000H NXi Avionics Integrated Avionics System Multi-Function Display (MFD) Typical User Selected Formats: User-selectable MFD display options in the standard configuration Garmin G1000H NXi include System Status, checklists, flight planning, maintenance pages, engine pages, Power Assurance Screen, NAV map, Traffic Information System (TIS), engine and transmission information, fuel status, and calculated range. Optional features include satellite weather through an XM satellite datalink [1] (North America) and the Garmin GTS 800 Traffic Advisory System. Notes: [1] Subscription to XM Satellite Weather and/or Radio is the responsibility of the helicopter owner/operator. MFD Weight and Balance Display. MFD Moving Map Display. Power Situation Indicator (PSI): The PSI, shown in the dashed red circle, is a single indicator section of the PFD that provides the pilot quick information about power settings. The color-coded parameter display automatically highlights normal performance (green), near limits (yellow) or exceedances (red). Power Situation Indicator. SPECIFICATIONS BELL 505 FEBRUARY 2026 13 © 2026 Bell Textron Inc. Specifications subject to change without notice. Communication and Navigation The standard configuration Garmin GIA 64H Integrated Avionics Unit includes a GPS/WAAS receiver, VHF COM Transceiver and VHF NAV and Glideslope receivers. It also maintains a prioritized queue of aural alerts for Aural Alert Generation. AUDIO SYSTEM The GMA 350Hc Audio Control Panel incorporates Bluetooth technology for wireless access to music, phone and more. This adds to an impressive list of features including industry-first Telligence Voice Command technology, 3D audio processing and enhanced auto squelch capability and more. These features decrease heads-down time and increase overall situational awareness in the cockpit. The GMA 350Hc provides cockpit ICS, pilot and copilot volume control and dual stereo entertainment inputs. The COM interface supports up to three (3) transceivers and the NAV interface supports up to five (5) radios. The system can accommodate up to seven (7) mono/stereo headsets (two (2) for pilot/copilot and five (5) for passengers), and provides ICS audio isolation modes for the pilot, copilot and passenger headset positions. The GMA 350Hc features two (2) entertainment inputs (MUSIC 1 and MUSIC 2), with identical streaming content from the optional GDL 69AH XM Radio Datalink [2]. A 3.5 mm front panel mini-jack on the GMA 350Hc can be used as an entertainment input or as a telephone input EXTENDED SQUITTER (ES) MODE S TRANSPONDER The GTX 335R Extended Squitter (ES) Mode S Transponder functions are controlled by the PFD display and support European Mode S mandates for Extended Squitter, Elementary Surveillance and Enhanced Surveillance. In addition, the GTX 335R ES provides Traffic Information (TIS) display of all Mode A and Mode C transponder equipped aircraft, and Automatic Dependent Surveillance-Broadcast (ADS-B) out capability. With ADS-B out capability, position velocity and heading information are automatically transmitted to other aircraft and ground stations to improve situational awareness and flight safety. GARMIN SOFTWARE FEATURES The Weight and Balance Multi-Function Display (MFD) page provides information about the helicopter weight and center of gravity. It uses pilot data entry for the crew, passengers, baggage loads, helicopter empty weight and the fuel load. It can synchronize with fuel quantity indication instead of relying on manual entry. Longitudinal and lateral aircraft CG are automatically calculated and displayed graphically with a digital readout. The Longitudinal CG slider indicator includes a cyan bar to show CG migration due to fuel burn. The impending exceedances alert tone provides an aural alert to the pilot before encountering an engine exceedances. The aural alert tone is generated when any of the engine parameters are operating in a time-limited range. Profile and path views are selectable and displayed on the navigation map MFD page. When the profile view is enabled, it is displayed in a window below the navigation map. Altitude is shown along a vertical scale, with an aircraft icon positioned at the current altitude. Distance is represented horizontally along the bottom of the profile view, and increases from left (present position) to right. The profile view is based on the current aircraft track (or heading if track is unavailable) and shows the highest known terrain or obstacles within a predetermined width from the present aircraft position to the end of the profile range. The profile path displays the horizontal and lateral boundaries of the profile view. The path is shown as a white rectangle on the navigation map page and is only available when profile view is enabled. White range markers both edges of the profile path rectangle match the range markers along the distance scale inside the profile view display window whenever the profile range is at least 4 nm. BELL 505 SPECIFICATIONS 14 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. AVIONICS UPGRADE OPTIONS The Bell 505 optional avionics upgrade includes GRA-55, Helicopter Synthetic Vision Technology (HSVT™), Helicopter Terrain Avoidance Warning System (HTAWS) and Traffic Advisory System (TAS) GRA-55 Radar Altimeter: Designed to work with Garmin flight displays, the GRA-55 conveniently places The Above Ground Level (AGL) readout right in front of the pilot. The GRA-55 , when combined with the Garmin GTS 800 TAS and the Garmin GTX 335R ES transponder provides enhanced traffic situational awareness to the flight crew and other suitably equipped aircraft. HSVT (Helicopter Synthetic Vision): Using sophisticated computer modeling to recreate a virtual topographic landscape from the system’s terrain database, HSVT gives you a clear depiction of obstacles, traffic, ground and water features, airports and more - all shown in 3-D perspective on the primary flight display. HTAWS (Helicopter Terrain Avoidance Warning System): HTAWS works in the background to monitor terrain and obstacles. It issues audio & visual alerts for instances requiring attention. Voice callouts enhance situational awareness while allowing you to keep eyes looking forward. TAS (Traffic Advisory System): The TAS provides expanded traffic alerts through both active and passive surveillance capabilities. When installed, the optional GTS 800 TAS replaces the standard configuration Traffic Information System (TIS) using active interrogation of Mode A, C, and S transponders to provide traffic advisories to the pilot independent of the air traffic control system. Second VHF Comm - Garmin GTR 225B: The pedestal-mounted Garmin GTR 225B VHF COM Radio incorporates functions that can reduce cockpit workload, provides 16 watts transmit power with either 8.33 KHz spacing or 25 KHz spacing (selectable). Emergency Locator Transmitter (ACK Technologies Model E-04): In case of an accident, the Emergency Locator Transmitter (ELT) provides crucial location information to assist first responders. The ELT installs in the truss area of the aircraft on a dedicated shelf and the ELT antenna is mounted thru the aft body center panel. The kit provides an instrument panel mounted remote control panel indicator (RCPI) which includes ON and TEST/RESET switches. Also mounted behind the instrument panel is an audio alert. The ELT provides 121.5 MHZ and 406 MHz distress signals as well as GPS coordinates and is automatically activated when crash level impact is detected, or manually activated using the cockpit remote control (RCPI). Flight Stream 510: Wireless cockpit connectivity unlocks more capabilities from within the G1000H NXi integrated flight deck. Available as an option, Flight Stream 510 enables Database Concierge, the wireless transfer of aviation databases from the Garmin Pilot™ app on a mobile device to the G1000H NXi system. Flight Stream 510 also supports two-way flight plan transfer, the sharing of traffic, weather, GPS information, back-up attitude information and more, between the G1000H NXi and compatible mobile devices running Garmin Pilot™ or ForeFlight mobile. Transponder GTX 345R: The Garmin GTX 345R Transponder (ADS-B IN & OUT capability) replaces the basic ship GTX 335R. - 1090 MHz ADS-B “Out” enables aircraft to operate at any altitude, in airspace around the globe - Combines Mode S Extended Squitter (ES) transponder and optional WAAS/GPS position source in a single unit - Provides access to dual-link ADS-B “In” traffic and subscription-free weather on compatible displays - Wirelessly stream weather, traffic, GPS position and backup attitude² via Connext® link to Garmin Pilot™ and ForeFlight Mobile apps as well as the aera® 795/796 Garmin portables SPECIFICATIONS BELL 505 FEBRUARY 2026 15 © 2026 Bell Textron Inc. Specifications subject to change without notice. GDL 69AH XM Weather Radio Datalink: A customized remote-mounted XM satellite radio receiver capable of receiving digital datalink weather and digital audio entertainment from an XM satellite. XM Weather and Radio operate in the S-band frequency range to provide continuous uplink capabilities at any altitude throughout North America. An individual 3rd party XM / WX subscription is required to receive XM / WX data signals. Subscriptions are available for either weather or digital audio entertainment services separately or for both services. BELL 505 SPECIFICATIONS 16 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Seating and Interiors CREW SEATING Two individual ergonomically designed seats, each equipped with seat belt, double strap shoulder harness and inertia reel, are located in the cockpit. The color and upholstery material for the seats and interior trim of the cockpit match that which is selected for the cabin. Seats are mounted on in-line tracks to allow for easy entry and exit from the aircraft. Adjustable crew seat rails (optional kits) are available allowing the crew seats to be locked in the Aft position allowing the pilot and Forward passenger/Co-Pilot an extra 2.8” (71 mm) of leg room. PASSENGER SEATS Passenger seats are bulkhead mounted, forward facing, energy attenuating seats with incorporated fixed headrests and a four point restraint harness. The seats provide protection and restraint of occupants (passengers) in normal flight, emergency states and dynamic landing conditions. Standard equipped seats can be folded against the bulkhead for additional rear cabin storage and are mounted with quick disconnect fittings to easily remove the seats from the aircraft without the use of tools. Passenger seats can also be stowed in the baggage compartment. Leather passenger seats shown below are removable, non-foldable and available as optional equipment. Standard seating is provided in black fabric with optional leather provided in black, tan, and gray colors. Floor carpet is also available to match the selected seat colors. Bell 505 Interior Layout, Standard Equipped seats Bell 505 Interior Layout, Macaer "Magnificent" seats Bell 505 Interior Layout, Two Tone Premium Leather Gray seats SPECIFICATIONS BELL 505 FEBRUARY 2026 17 © 2026 Bell Textron Inc. Specifications subject to change without notice. Seating and Interiors INTERIOR TRIM AND CABIN ACCESS Clamshell cabin doors located on the left side of the aircraft open to a wide 55 inches (top right image), allowing easy ingress/egress for passengers or the ability to load and unload for various missions (bottom right image). Quick disconnect seats (bottom left image, shown with one seat removed) allow the rear cabin to be converted for utility missions. Bell 505 Interior and Cabin Access. BELL 505 SPECIFICATIONS 18 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Seating and Interiors BAGGAGE COMPARTMENT The Bell 505 is equipped with one large rectangular baggage compartment that is accessible from the pilot side with the option to add an access door to the other side. Standard equipment includes an integrated light that automatically activates/ deactivates when the baggage compartment door is opened or closed. Cargo of many different shapes and sizes can easily be stowed in the baggage bay including: several travel golf bags, up to four standard suitcases, or standard passenger seats. Leather non-folding seats will not fit. A uniform rectangular design allows for maximum usage of the full storage space without wasted space. The Bell 505’s flat floor cabin design and large rectangular baggage compartment lets the Bell 505 adapt to your changing mission needs. The baggage compartment has a large usable volume of 18 ft3 (0.51 m3). In fact, the baggage compartment can fit three standard travel golf bags, with some room to spare. Bell 505 Baggage Compartments SPECIFICATIONS BELL 505 FEBRUARY 2026 19 © 2026 Bell Textron Inc. Specifications subject to change without notice. UTILITY With an optional 2,000 lb (907 kg) capacity cargo hook, a highly configurable 22 ft2 (2.0 m2) fully flat cabin floor area with integrated tie downs, a large 18 ft3 (0.514 m 3 ) baggage compartment and superior crew visibility, the Bell 505 provides utility operators with the flexibility and performance they require to conduct their mission. The cargo hook features a load release button on the cyclic controls with a manual backup release to ensure the pilot can release external loads in flight. The cargo hook assembly also features fitting and disconnects that allow the whole assembly to be quickly removed from the aircraft. CORPORATE The Bell 505 is perfectly suited to accom- modate everything from VIP transporta- tion to corporate shuttle missions. Fea- tures such as a large cabin volume of 99 ft3 (2.80 m 3), comfortable 18-inch wide premium leather seats and ample leg- room/headroom combined with a smooth ride, superb range and the state of the art Garmin G1000H NXi flight deck make the Bell 505 an ideal choice for any business needs. Mission Profiles BELL 505 SPECIFICATIONS 20 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. ADVENTURE From breathtaking scenic flights to camping at remote destinations, find the places only a helicopter can take you. With the spacious cabin and integrated tie downs comfortably fit bikes, gear and more securely while saving room for passengers in the intelligent and powerful Bell 505. Mission Profiles PUBLIC SAFETY With a highly configurable cabin, superb speed and range, and points for mounting external equipment, the Bell 505 delivers multi-mission capability and flexibility for public safety operators. The Bell 505 displays its excellent capacity for public safety equipment with the ability to add features such as a searchlight, EO/IR Sensor, Public Address Speaker, large format high definition mission display, tactical radio, additional audio panels, and much more. This combination of Public Safety equipment, that can be tailored to your mission, paired with a wide cabin, removable seats, fully flat floor design, and large baggage compartment gives the crews ability to meet any mission without sacrificing their comfort. SPECIFICATIONS BELL 505 FEBRUARY 2026 21 © 2026 Bell Textron Inc. Specifications subject to change without notice. Mission Profiles TRAINING With optional dual pilot controls, the Bell 505 is an excellent aircraft for training pilots to fly today’s modern aircraft with FADEC controlled engines, integrated avionics system and other advanced technologies. These modern technologies coupled with proven dynamic systems and a high inertia rotor system for excellent autorotation capabilities create the optimal platform for helicopter training. The simplicity of engine automatic control and systems automation enhance the instructors ability to concentrate on the students "stick and rudder" skills. The student learns to fly quicker with less worry about exceeding parameters when starting or flying the helicopter. MEDICAL A flat floor cabin, 55’’ clam shell door, and easy install EMS interiors make the Bell 505 ideally suited for fast and efficient patient and medical personnel transport. Rear seat rails allow for a configurable equipment rack capable of handling a multitude of life saving medical equipment. The G1000H NXi avionics suite provides added situational awareness for flight into high traffic and complex terrain areas ensuring every rescue effort is a success. BELL 505 SPECIFICATIONS 22 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. External Paint Schemes For more color options, please visit config.bh.com or speak with a Sales Representative. Paint scheme: white lightning Paint scheme: black dynamic Paint scheme: silver dynamic SPECIFICATIONS BELL 505 FEBRUARY 2026 23 © 2026 Bell Textron Inc. Specifications subject to change without notice. AIRFRAME Hybrid composite / metallic structure with composite side panels and aft fuselage skins Doors (three), one large hinged pilot and copilot door on LH and RH side, one hinged passenger door on the copilot side, copilot side doors open to unobstructed 55 inches (140 cm). Landing gear, tubular skid type with replaceable skid shoes (painted black) Lock for luggage compartment Baggage Compartment: 18 ft3, 250 lb (0.51 m3, 113 kg) capacity with one composite door on pilot side Tail boom, monocoque structure with vertical fin and fixed horizontal stabilizer Tail Skid (tail rotor guard) Rupture Resistant Fuel Tank: 84.85 gallons (321 liters) Multiple paint schemes and color options available at config.bh.com INTEGRATED AVIONICS SYSTEM with GARMIN G1000H NXi SUITE Two 10.4-inch (26.4 cm) high resolution display units, providing Primary Flight Display (PFD) and Multi-Function Display (MFD) functionalities Integrated Avionics Unit, consisting of a 16-watt VHF communication transceiver with 8.33 kHz spacing, VHF navigation, WAAS GPS navigation, and glideslope receiver One audio control panel with clearance recording and Automatic Speech Recognition (ASR) capability One Air Data Attitude Heading Reference Unit (ADAHRS) with Outside Air Temperature (OAT) probe and Magnetometer Unit One Mode S transponder with extended squitter, including Traffic Information Service (TIS), with ADS-B out capability One engine and airframe interface unit Integrated Engine Indication and Crew Alerting System (EICAS), including Power Situation Indicator (PSI) that provides an integrated display presentation of all critical engine parameters into a single indicator to present the power “margin” remaining Fuel flow indication with range ring display capability Flight Data Recording of standard aircraft and engine parameters Electronic Standby Instrument System ELECTRICAL Auxiliary power outlet (28 VDC System) Battery, 17 amp-hour Lithium Ion External power and grounding receptacle Starter-generator (165 ampere) Solid state voltage regulator Heated pitot tube Static Ports, Unheated LED lighting (interior/exterior) Single LED landing light and dual LED taxi lights Lighted baggage compartment INTERIOR 5-place ICS allows audio access for all seats Handholds for ingress/egress Cargo tie-downs in cabin and baggage compartment Cabin heater and defogger LED cabin lighting and crew lighting Decals and exit lighting/labels 5-place energy crash attenuating seats with 4-point shoulder harnesses 3 bulkhead mounted passenger seats, foldable, quick disconnect Structural provisions for mounting of external hardware Helmet hooks (Pilot & Copilot) Fire extinguisher (Cockpit) First aid kit MANUAL (not included in empty weight) Garmin Pilot’s Handbook (Available Electronically) Garmin Cockpit Reference Guide (Available Electronically) Operating manuals: Rotorcraft flight manual, Aircraft log book, Engine log book Aircraft maintenance manuals*, Fault isolation manual, Wiring diagrams, Engine maintenance manual, Engine operating manual, Engine parts manual, Ground station software (aircraft data display) POWERPLANT Safran Arrius 2R gas turbo-shaft engine with dual channel FADEC and automatic backup Engine data recording system (Automatic cycle and flight hour counting, stored in cockpit avionics system) Bell 505 Standard Configuration * Aircraft maintenance manuals are available on ePubs located here: bellflight.com BELL 505 SPECIFICATIONS 24 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Automatic startup Surge and flame-out protection Interchangeable modules Engine Inlet Barrier Filter ROTORS AND CONTROLS Main rotor, semi-rigid, two-bladed, teetering type with precone and underslung feathering axis. All metal blades that are moisture proof and epoxy encapsulated. Flap restraints. High visibility main rotor blades Tail rotor, semi-rigid, two-bladed, teetering type Hydraulic boost system (pump and reservoir module) Adjustable pedals Mechanical flight control linkages throughout Cyclic mounted Intercom / Transmit Switch Pilot's cyclic grip has provisions for optional equipment control TRANSMISSION DRIVE SYSTEM Soft mounted LIVE pylon isolation system Main transmission 2 stage 15.22:1 planetary reduction Kaflex (non-lubricated) input drive shaft Gearbox, tail rotor with 2.3:1 spiral bevel gear reduction Freewheeling unit (between engine and main transmission) Hydraulic pump (for cyclic and collective boost controls) Oil Cooler Oil pump constant pressure Oil filter with replaceable type cartridge Bell 505 Standard Configuration SPECIFICATIONS BELL 505 FEBRUARY 2026 25 © 2026 Bell Textron Inc. Specifications subject to change without notice. OPTIONAL ACCESSORIES Kit Description Weight Notes lb kg AIRFRAME Adjustable Crew Seat Tracks L/H (2.8" adjustment) 3.2 1.5 23 Adjustable Crew Seat Tracks R/H (2.8" adjustment) 3.2 1.5 23 Air Conditioning System 72.3 32.8 3 Air Conditioning System - 3rd Evaporator 11.5 5.2 2 Automatic Door Openers for Co-Pilot Door 1.0 0.5 3 Automatic Door Openers for Pilot Door 1.0 0.5 3 Cowling Access Door (access to engine wash connection port) 0.4 0.2 Foreign Certification (Decal Kits) 0 0 19 Full Length Trainer Shoe 5.9 2.7 20 Frahm Provisions 1.2 0.5 3 Frahm Equipment 25.5 11.6 1, 3 Fresh Air Inlet Snow Deflector Kit 0.3 0.1 Hard Point (Forward Location) 12.9 5.9 4, 22 Hard Point (AFT Location) 6.1 2.8 4 Stowage Compartment with Cup Holders (x4 or x2 if Frahm installed) 4.3 2.0 23 Movable Ballast (Cabin Provisions & Equipment) 6.5 2.9 1, 21 Non-Halon Cockpit Fire Extinguisher 5.0 2.3 23 Quick Release Door Pins (crew doors and clamshell door) 0 0 Solar Advantage Windshields 0 0 Sliding Windows (Pilot & Co-Pilot) 1.2 0.5 Wire Strike Protection System 12.9 5.9 AVIONICS Avionics Upgrade (HTAWS. Synthetic Vision, TAS) 15.9 7.2 5 Avionics Shelf 2.3 1.0 5 Radar Altimeter (Garmin GRA-55) 6.5 2.9 5 Second VHF Communication (Garmin GTR 225B) 5.4 2.4 Emergency Locator Transmitter (ACK Technologies Model E-04) 6.1 2.8 Bose Headset Adapter (5 stations, wiring and jacks) 0.6 0.3 Headsets - H10-13H (David Clark) 1.5 0.7 6 Headsets - A20 (Bose) with or without Bluetooth 1.0 0.5 Transponder GTX 345R (Garmin) 0.3 0.1 Flight Stream 510 (Garmin) 0 0 EQUIPMENT Cargo Hook Provisions 4.4 2 Cargo Hook Equipment (2,000 lb / 907 kg) 8.1 3.7 1 Cargo Hook Weighing System 3.5 1.6 Bell 505 Kits Refer 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 configuration. BELL 505 SPECIFICATIONS 26 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. OPTIONAL ACCESSORIES Kit Description Weight Notes lb kg Cargo Hook Mirrors (Right and Left side available) 4.8 2.2 Dual Pilot Controls 10.6 4.8 Rotor Brake 14.1 6.4 3 INTERIOR Color Coordinated Carpet 4.6 2.1 3 Cabin & Cockpit Coin Mat Flooring 12.7 5.8 3 Seats - Standard Interior (Black) 0 0 7 Seats - Premium Interior (Black Leather) 29.6 13.4 3, 7 Seats - Premium Interior (Two Tone Tan or Two Tone Gray Leather) 29.6 13.4 7 OTHER No Exterior Paint -14.6 -6.6 Landing Gear Painted to Match Aircraft Color 0 0 Mechanical Ground Handling Wheels (Loose Equipment) NA NA Ground Handling Carrier Bracket (Qty 2) (Loose Equipment) NA NA 8 Operator Accessory Package (Loose Equipment) NA NA 9 VENDOR (STC) Avionics Rain Shield (AA) 6.7 3.0 18 Baggage Compartment Divider Kit (AA) 4.3 2.0 Baggage Door Kit - LHS (AA) 7.3 3.3 Bear Paws (Alpine Aerotech) 17.5 2.6 13 Bear Paws (DART) 10.6 4.8 14 Crew Flashlight Kit (AA) 0.5 0.2 Emergency Float Kit (Dart) 129.0 58.5 12, 20 Emergency Float Kit with Heavy Duty Wear Plates (Dart) 135.1 61.3 12, 20 EMS - Interior (Helifab) 94.2 42.7 16 EMS-LITE Medical Transport Interior (Med-Pac) 53.1 24.1 16 EMS - Interior (URC) (STC Pending) TBD TBD 16 Expanded Avionics Shelf (AA) 4.0 1.8 5 Expanded Instrument Panel - 12 inch monitor (AA) 8.9 4.0 Expanded Instrument Panel - 17 inch monitor (AA) 11.4 5.2 Flitestep (AA) - Standard or High Standard Landing Gear (AA) 17.6 8.0 Floor Protectors - Baggage Bay (AA) 7.2 3.3 Floor Protectors - Co-pilot (AA) 1.7 0.8 Floor Protectors - Passengers Cabin with Carpet (AA) 9.3 4.2 15 Floor Protectors - Passengers Cabin without Carpet (AA) 10.8 4.9 Floor Protectors - Pilot (AA) 1.7 0.8 Garmin 2-Axis Autopilot 15 6.8 17 Garmin 3-Axis Autopilot 18 8.2 17, 22 Genesys HeliSAS 2-Axis Autopilot 22.2 10.1 5, 17, 18 Genesys HeliSAS 3-Axis Autopilot 25.7 11.7 5, 17, 18 Headliner Kit (Black or Beige or Black with Tan or hydrographic Center)(AA) 16.2 7.3 FEBRUARY 2026 BELL 505 SPECIFICATIONS 27 © 2026 Bell Textron Inc. Specifications subject to change without notice. Notes: For commonality, notes shown below are identical in Product Specification and Price List. 1. Requires provision kit installed prior to or concurrently with equipment. 2. Requires Air Conditioning System installed prior to or concurrently with the 3rd Evaporator - Air Conditioning System kit. 3. Mecaer VIP MAGnificent Interior Kit requires the installation of Premium Seats, Automatic Door Openers, Rotor Brake , Air Conditioning, Frahm (Provisions & Equipment) & No Carpets. 4. Provides External Hardpoints to mount items such as cameras and searchlights, requires the High Skid Gear. 5. Avionics Upgrade, or Radar Altimeter or a Genesys HeliSAS Autopilot require an Avionics Shelf installed (only one Avionic Shelf allowed). 6. David Clark Headsets NOT compatible with Bose Headset Adapter kit 7. Only one Seat kit required. 8. This adaptor kit allows the 206L/407 series "Brackett" ground handling wheels to the standard 505 landing gear (not compatible with 206B wheels) 9. Operator Accessory Package includes Main Rotor Tie Down, Pitot Tube Cover, Tail Rotor Tie Down, Exhaust Cover Assembly and IBF Cover Assembly. 10. All Vendor Kits listed have FAA STC, other countries validations may be required. 11. High Skid Gear provides an additional 6.5 inches (16.5 cm) of ground clearance versus the standard Gear. 12. Emergency Float Kit is NOT compatible with High Skid Gear, Bear Paws or Full Length Training Shoes 13. Bear Paws (Alpine Aerotech) NOT compatible with Emergency Float Kit (Dart) or High Skid Gear (AAI) 14. Bear Paws (Dart) compatible with Emergency Float Kit (Dart) but NOT compatible with High Skid Gear (AAI) 15. Requires a carpet installed 16. Requires the removal of Co-Pilot and Aft LHS Passenger Seats and Co-Pilots control sticks (if installed) 17. Only install one Autopilot kit. 18. Genesys HeliSAS Autopilots are NOT compatible with Avionics Rain Shield 19. A Foreign Certification (Decal Kit) is required if 505 will be registered in any of the following counties: Argentina, Brazil, Chile, China, Colombia, Indonesia, Israel, Japan, Mexico, Russia, UAE, Ukraine, Uruguay, Vietnam. 20. Full Length Trainer Shoe is NOT compatible with High Skid Gear or Emergency Floats. 21. Tail Rotor Gearbox Cover is NOT compatible with Movable Ballast Kit. 22. Garmin 3-Axis Autopilot is NOT compatible with Hard Point (Forward Location). 23. Map Case with Cup Holders required when either the Adjustable Crew Seat Tracks or Non-Halon Cockpit Fire Extinguisher are installed. OPTIONAL ACCESSORIES Kit Description Weight Notes lb kg High Skid Gear (includes crew steps)(AA) 5.7 2.6 11, 20 Mecaer VIP MAGnificent Interior Kit - Offshore, Saddle, Sand, Sport 92.0 41.7 3 Nightscanner HID (500K or 700 candlepower) (AA) 10.0 4.5 NVG Cockpit/Cabin Lighting (AeroDynamix) 0 0 Passenger Headset Hanger Kit (AA) 0.5 0.2 Pre-Flight Step/Handle Kit (AA) 2.0 0.9 Pulselite Pulse Landing Lights (Precise Flight) 1.0 0.5 Solar Advantage Windows - Passenger Windows Light or Dark Grey (Crew & Passenger) (AA) 0 0 Tail Rotor Gearbox Cover (AA) 4.3 2.0 21 BELL 505 SPECIFICATIONS 28 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Helicopter Performance Charts IGE and OGE hover, and service ceiling performance chart data based on the following conditions: y Safran Arrius 2R engine y Barrier filter installed y Heater off y No wind FEBRUARY 2026 BELL 505 SPECIFICATIONS 29 © 2026 Bell Textron Inc. Specifications subject to change without notice. 22 24 26 28 30 32 34 36 38 40 42 44 46 GROSS WEIGHT - 100 LB 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 PRESSURE ALTITUDE - 1000 FT M505 IGE HOVER CEILING TAKEOFF POWER, BARRIER FILTER HEATER OFF, NO WIND 10 11 12 13 14 15 16 17 18 19 20 GROSS WEIGHT - 100 KG 0 5 10 15 20 25 30 35 40 45 50 55 60 PRESSURE ALTITUDE - 100 METERS SKID HEIGHT 3 FT (0.9 M) MAX INTERNAL GW 3680 LBS MAX EXTERNAL GW 4475 LBS ISA+30°C ISA+20°C ISA+10°C ISA 40°C 30°C 20°C 10°C 0°C -10°C -20°C -30°C -40°C MAXIMUM OAT (ISA+35°C) Helicopter Performance Charts IGE HOVER CEILING Conditions: y Safran Arrius 2R engine at takeoff power y Barrier filter installed y Heater off, No wind BELL 505 SPECIFICATIONS 30 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Helicopter Performance Charts OGE HOVER CEILING Conditions: y Safran Arrius 2R engine at takeoff power y Barrier filter installed y Heater off, No wind 22 24 26 28 30 32 34 36 38 40 42 44 46 GROSS WEIGHT - 100 LB 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 PRESSURE ALTITUDE - 1000 FT M505 OGE HOVER CEILING TAKEOFF POWER, BARRIER FILTER HEATER OFF, NO WIND 10 11 12 13 14 15 16 17 18 19 20 GROSS WEIGHT - 100 KG 0 5 10 15 20 25 30 35 40 45 50 55 60 PRESSURE ALTITUDE - 100 METERS MAX INTERNAL GW 3680 LBS MAX EXTERNAL GW 4475 LBS ISA+30°C ISA+20°C ISA+10°C ISA 40°C 30°C 20°C 10°C 0°C -10°C -20°C -30°C -40°C MAXIMUM OAT (ISA+35°C) FEBRUARY 2026 BELL 505 SPECIFICATIONS 31 © 2026 Bell Textron Inc. Specifications subject to change without notice. Helicopter Performance Charts SERVICE CEILING Conditions: y Safran Arrius 2R engine at MCP power y Barrier filter installed y Heater off, No wind 22 24 26 28 30 32 34 36 38 40 42 44 46 GROSS WEIGHT - 100 LB 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 PRESSURE ALTITUDE - 1000 FT M505 SERVICE CEILING MCP POWER, BARRIER FILTER HEATER OFF, NO WIND 10 11 12 13 14 15 16 17 18 19 20 GROSS WEIGHT - 100 KG 0 5 10 15 20 25 30 35 40 45 50 55 60 PRESSURE ALTITUDE - 100 METERS MAX INTERNAL GW 3680 LBS MAX EXTERNAL GW 4475 LBS ISA+30°C ISA+20°C ISA+10°C ISA MAXIMUM OAT (ISA+35°C) 40°C 30°C 20°C 10°C 0°C -10°C -20°C -30°C -40°C BELL 505 SPECIFICATIONS 32 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Fuel Flow vs. Airspeed Fuel Flow vs Airspeed chart data based on the following conditions: y ISA & ISA+20 °C y Safran Arrius 2R engine y Inlet Barrier Filter installed y Standard skid gear y Clean configuration (no external kits) y No wind Notes: The best allowable Cruise Speed is either Long Range Cruise Speed (LRC), or when speed is limited by Maximum Continuous Cruise Power (MCP) or VNE , the maximum speed permitted. FEBRUARY 2026 BELL 505 SPECIFICATIONS 33 © 2026 Bell Textron Inc. Specifications subject to change without notice. Fuel Flow vs. Airspeed PRESSURE ALTITUDE = SEA LEVEL, OAT = 15°C (ISA) FUEL FLOW VS AIRSPEED PRESSURE ALTITUDE = SEA LEVEL OAT = 15°C CLEAN CONFIGURATION ENGINE RPM 104% GENERATOR 50 AMPS ZERO WIND HEATER OFF BARRIER FILTER 40 50 60 70 80 90 100 110 120 130 140 150 TRUE AIRSPEED - KNOTS 40 50 60 70 80 90 100 110 120 130 140 INDICATED AIRSPEED - KNOTS 120 130 140 150 160 170 180 190 200 210 220 230 240 250 260 270 FUEL FLOW - LB/HR 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 TORQUE - % 60 70 80 90 100 110 120 FUEL FLOW - KG/HR VNE LRC MCP TORQUE LIMIT MAX ENDURANCE GW x 100 LB 22 26 30 34 36.8 BELL 505 SPECIFICATIONS 34 FEBRUARY 2026 © 2026 Bell Textron Inc. Specifications subject to change without notice. Fuel Flow vs. Airspeed PRESSURE ALTITUDE = 2,000 FT, OAT = 11°C (ISA) FUEL FLOW VS AIRSPEED PRESSURE ALTITUDE = 2000 FT OAT = 11°C CLEAN CONFIGURATION ENGINE RPM 104% GENERATOR 50 AMPS ZERO WIND HEATER OFF BARRIER FILTER 40 50 60 70 80 90 100 110 120 130 140 150 TRUE AIRSPEED - KNOTS 40 50 60 70 80 90 100 110 120 130 140 INDICATED AIRSPEED - KNOTS 110 120 130 140 150 160 170 180 190 200 210 220 230 240 250 260 FUEL FLOW - LB/HR 20 25 30 35 40 45 50 55 60 65 70 75 80 85 90 TORQUE - % 50 60 70 80 90 100 110 FUEL FLOW - KG/HR VNE LRC MCP TORQUE LIMIT MAX ENDURANCE GW x 100 LB 22 26 30 34 36.8