When government, military and commercial customers want airborne solutions for critical missions, they turn to Beechcraft. Our aircraft provide the high performance and flight characteristics required to address the unique challenges of special mission operations.
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
9
Baggage Capacity
Weight
N/A
Volume
N/A
Single Pilot Certified
Yes
Weights
Maximum Ramp Weight
16,600 lb (7,530 kg)
Maximum Takeoff Weight
16,500 lb (7,484 kg)
Maximum Landing Weight
15,675 lb (7,110 kg)
Maximum Zero Fuel Weight
13,000 lb (5,897 kg)
Usable Fuel Capacity
Weight
5,192 lb (2,355 kg)
Volume
775 gal (2,934 l)
Basic Operating Weight
9,720 lb (4,409 kg)
Useful Load
6,880 lb (3,121 kg)
Maximum Payload
3,280 lb (1,488 kg)
Full Fuel Payload
1,688 lb (766 kg)
Performance
Maximum Cruise Speed
303 ktas (561 km/h)
Maximum Range
2,678 nm (4,960 km)
Takeoff Field Length
4,057 ft (1,237 m)
Landing Distance
N/A
Maximum Operating Altitude
35,000 ft (10,668 m)
Maximum Climb Rate
N/A
Maximum Limit Speed
N/A
Powerplant
Manufacturer
P&WC
Type
PT6A-60A
Power Rating
1,050 shp (783 kW)
When government, military and commercial customers want airborne solutions for critical missions, they turn to Beechcraft. Our aircraft provide the high performance and flight characteristics required to address the unique challenges of special mission operations.
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 | 9 |
| Baggage Capacity |
| Weight | N/A |
| Volume | N/A |
| Single Pilot Certified | Yes |
Weights
| Maximum Ramp Weight | 16,600 lb (7,530 kg) |
| Maximum Takeoff Weight | 16,500 lb (7,484 kg) |
| Maximum Landing Weight | 15,675 lb (7,110 kg) |
| Maximum Zero Fuel Weight | 13,000 lb (5,897 kg) |
| Usable Fuel Capacity |
| Weight | 5,192 lb (2,355 kg) |
| Volume | 775 gal (2,934 l) |
| Basic Operating Weight | 9,720 lb (4,409 kg) |
| Useful Load | 6,880 lb (3,121 kg) |
| Maximum Payload | 3,280 lb (1,488 kg) |
| Full Fuel Payload | 1,688 lb (766 kg) |
Performance
| Maximum Cruise Speed | 303 ktas (561 km/h) |
| Maximum Range | 2,678 nm (4,960 km) |
| Takeoff Field Length | 4,057 ft (1,237 m) |
| Landing Distance | N/A |
| Maximum Operating Altitude | 35,000 ft (10,668 m) |
| Maximum Climb Rate | N/A |
| Maximum Limit Speed | N/A |
Powerplant
| Manufacturer | P&WC |
| Type | PT6A-60A |
| Power Rating | 1,050 shp (783 kW) |
