With best in class range/payload and efficiency, the King Air® 350i is the aviation solution without compromise. The King Air 350i can take more passengers and cargo farther, on less fuel, allowing you to take your entire business team to important meetings and events.
Inspired Control
Rockwell Collins Pro Line 21 was created with pilot workload in mind. The system allows pilots to review data they receive in order to make clearer, more informed decisions. The heads-up placement of the Flight Director and Autopilot enhance situational awareness and increase safety.
Dispatch Reliability
A maintenance diagnostic computer, Central Line Replaceable Unit (LRU) detects logs, retrieves and displays current and past failures for specific aircraft information.
Standard Features
Standard Features
New Control Yokes
Std single and optional dual Flight Management Systems (FMS)
Digital Communication, Navigation, Surveillance (CNS) Radio
Dual Air Data Computer (ADC) Systems
Dual Altitude Heading Reference Systems (AHRS)
Terrain Awareness Warning System (TAWS)
Emergency Standby Instrumentation System (ESIS)
Four-Color Weather Radar with Doppler to detect turbulence
Automatic Flight Guidance System (AFGS)
Traffic Alert and Collision Avoidance System (TCAS II)
Cockpit Voice Recorder
Specifications
Dimensions
Length
46 ft 8 in (14.22 m)
Height
14 ft 4 in (4.37 m)
Wingspan
57 ft 11 in (17.65 m)
Wing Area
310 sq ft (28.8 sq m)
Wheelbase
16 ft 3 in (4.95 m)
Tread
16 ft 3 in (4.95 m)
Cabin Interior
Height
57 in (1.45 m)
Width
54 in (1.37 m)
Length
19 ft 6 in (5.94 m)
Maximum Passengers
11
Baggage Capacity
Weight
1,150 lb (521.6 kg)
Volume
71 cu ft (2.02 cu m)
Single Pilot Certified
Yes
Weights
Maximum Ramp Weight
15,100 lb (6,849 kg)
Maximum Takeoff Weight
15,000 lb (6,804 kg)
Maximum Landing Weight
15,000 lb (6,804 kg)
Maximum Zero Fuel Weight
12,500 lb (5,670 kg)
Usable Fuel Capacity
Weight
3,611 lb (1,638 kg)
Volume
539 gal (2,040 l)
Basic Operating Weight
10,070 lb (4,568 kg)
Useful Load
5,030 lb (2,282 kg)
Maximum Payload
2,430 lb (1,102 kg)
Full Fuel Payload
1,419 lb (644 kg)
Performance
Maximum Cruise Speed
312 ktas (578 km/h)
Maximum Range
1,792 nm (3,319 km)
Takeoff Field Length
3,300 ft (1,006 m)
Landing Distance
2,692 ft (821 m)
Maximum Operating Altitude
35,000 ft (10,668 m)
Maximum Climb Rate
2,731 fpm (832 mpm)
Maximum Limit Speed
263 kias (487 km/h)
Powerplant
Manufacturer
P&WC
Type
PT6A-60A
Power Rating
1,050 shp (783 kW)
With best in class range/payload and efficiency, the King Air® 350i is the aviation solution without compromise. The King Air 350i can take more passengers and cargo farther, on less fuel, allowing you to take your entire business team to important meetings and events.
Inspired Control
Rockwell Collins Pro Line 21 was created with pilot workload in mind. The system allows pilots to review data they receive in order to make clearer, more informed decisions. The heads-up placement of the Flight Director and Autopilot enhance situational awareness and increase safety.
Dispatch Reliability
A maintenance diagnostic computer, Central Line Replaceable Unit (LRU) detects logs, retrieves and displays current and past failures for specific aircraft information.
Standard Features
- New Control Yokes
- Std single and optional dual Flight Management Systems (FMS)
- Digital Communication, Navigation, Surveillance (CNS) Radio
- Dual Air Data Computer (ADC) Systems
- Dual Altitude Heading Reference Systems (AHRS)
- Terrain Awareness Warning System (TAWS)
- Emergency Standby Instrumentation System (ESIS)
- Four-Color Weather Radar with Doppler to detect turbulence
- Automatic Flight Guidance System (AFGS)
- Traffic Alert and Collision Avoidance System (TCAS II)
- Cockpit Voice Recorder
Specifications
Dimensions
| Length | 46 ft 8 in (14.22 m) |
| Height | 14 ft 4 in (4.37 m) |
| Wingspan | 57 ft 11 in (17.65 m) |
| Wing Area | 310 sq ft (28.8 sq m) |
| Wheelbase | 16 ft 3 in (4.95 m) |
| Tread | 16 ft 3 in (4.95 m) |
| Cabin Interior |
| Height | 57 in (1.45 m) |
| Width | 54 in (1.37 m) |
| Length | 19 ft 6 in (5.94 m) |
| Maximum Passengers | 11 |
| Baggage Capacity |
| Weight | 1,150 lb (521.6 kg) |
| Volume | 71 cu ft (2.02 cu m) |
| Single Pilot Certified | Yes |
Weights
| Maximum Ramp Weight | 15,100 lb (6,849 kg) |
| Maximum Takeoff Weight | 15,000 lb (6,804 kg) |
| Maximum Landing Weight | 15,000 lb (6,804 kg) |
| Maximum Zero Fuel Weight | 12,500 lb (5,670 kg) |
| Usable Fuel Capacity |
| Weight | 3,611 lb (1,638 kg) |
| Volume | 539 gal (2,040 l) |
| Basic Operating Weight | 10,070 lb (4,568 kg) |
| Useful Load | 5,030 lb (2,282 kg) |
| Maximum Payload | 2,430 lb (1,102 kg) |
| Full Fuel Payload | 1,419 lb (644 kg) |
Performance
| Maximum Cruise Speed | 312 ktas (578 km/h) |
| Maximum Range | 1,792 nm (3,319 km) |
| Takeoff Field Length | 3,300 ft (1,006 m) |
| Landing Distance | 2,692 ft (821 m) |
| Maximum Operating Altitude | 35,000 ft (10,668 m) |
| Maximum Climb Rate | 2,731 fpm (832 mpm) |
| Maximum Limit Speed | 263 kias (487 km/h) |
Powerplant
| Manufacturer | P&WC |
| Type | PT6A-60A |
| Power Rating | 1,050 shp (783 kW) |
