Performance

Max Cruise Speed
Value
Max Reach 4 Passengers
Value
Max Range 6 Passengers
Value
Max Altitude
Value
Takeoff Distance Over 50 ft Obstacle
Value
Landing Distance over 50 ft Obstacle
Value
Rate of Climb
Value
Time to Climb Sea Level to FL 450
Value
Stall Speed
Value

Weight

Max Ramp
Value
Max Take-Off
Value
Max Landing
Value
Max Zero Fuel
Value
Usable Fuel
Value
Max Payload
Value
Max Payload With Full Fuel
Value

Exterior Dimensions

(A) Length
Value
(B) Height
Value
(C) Horizontal tail span
Value
(D) Landing gear width
Value
(E) Wing span
Value
F G
(F) Cargo Door Width
Value
(G) Cargo Door Height
Value

Interior Dimensions

(A) Cabin Length
Value
(B) Cabin Width
Value
(C) Cabin Height
Value

Volume

Cabin Volume
Value
Baggage Compartment
Value

Interior Configurations

Air Ambulance

Air Ambulance

Cockpit

Advanced Cockpit Environment (ACE), Powered by Honeywell

2 12" Primary flight display flat panel units

Smartview synthetic vision system on each primary flight display

2 Primary flight display controllers

1 Integrated global navigation system sensor unit with satellite-based augmentation system receiver

2 Audio/marker panels

1 Dual channel autopilot with dual yaw damper

1 Flight guidance panel

2 12" Multi-function display flat panel units

1 Touch screen controller

1 Cursor control device

Switch panels

2 Mode S diversity transponders with Automatic Dependent Surveillance – Broadcast (ADS-B) OUT functionality

2 Multi-mode digital radios

2 Attitude reference systems comprising of 1 inertial reference system and 1 attitude heading reference system and magnetometer

1 Distance measuring equipment

1 Radar altimeter

1 Integrated enhanced ground proximity warning system class B

Traffic Collision Avoidance System (TCAS) I

Autothrottle system

Tactile feedback (roll and pitch)

Automatic yaw trim

Dual Flight Management System (FMS)

Localizer Performance with Vertical Guidance (LPV) approach capability

Required Navigation Performance (RNP) 0.3 capability

Other Flight Instrumentation

Utilities management system

Dual pitot-static systems

Dual angle of attack sensors

1 Required Navigation Performance 2100 weather radar

Radar Altimeter 5G Filter to operate safely within the 5G environment

1 Electronic standby instrument system with dedicated pitot-static system and magnetometer

1 Emergency Local Transmitter (ELT) 406 MHz with remote switch, global positioning system and navigation interface

1 Flight time recorder (Hobbs meter)

1 Lightweight data recorder

Other Cockpit Systems

2 Crew control yokes

2 Rudder pedal sets including brake pedals

2 Crew seats: adjustable, reclining with foldable armrest, headrest, upholstery, 4-point torso restraint system and life vest storage

Storage compartments, suitable for storing aeronautical handbooks and/or tablets

2 Cockpit speakers

1 Handheld microphone

2 Active noise reduction headsets with microphones

Cockpit roof, side walls, console panels finished in aviation standard leather, ultra-leather, fabric or paint

Floor carpet

1 Cockpit/cabin bulkhead divider with curtain

2 Adjustable sun visors

2 Cup holders each side

Notepad, pen holders

2 USB charging outlets (1 on each side)

1 LED dome light

5 LED flood lights for instrument and side panels

2 LED map reading lights

Ownership Experience

The Pilatus Brand