General
Certification FAR 25

Engines:
Pratt & Whitney
JT15D-1A 2,200 LBS of Thrust

Exterior Dimensions:
Length 43' 6"
Wing Span 47' 1"
Height 14' 4"

Internal Dimensions:
Length 210"
Height 52"
Passenger Cabin Volume 300 Cu. Ft.

Accomodations:
Passenger Seats 5-6
Baggage Capacity 77 Cu. Ft./ 1000 lbs
Pressurization:
Differential 8.5 PSI
8,000 Ft Cabin at 41,000 Ft.

Altitudes:
Certified 41,000 Ft
Service Ceiling 1 engine (MGTOW) 21,000 Ft

Certified Weights:
Maximum Ramp Weight 12,000 lbs
Maximum Take Off Weight 11,850 lbs
Maximum Fuel Capacity 3,780 lbs

Basic Operating Weights:
Typical Empty Weights 6,546 lbs
Basic operating Weight (2 crew) 6,926 lbs

Payload:
Useful Payload and Fuel 5,054 lbs
Payload at Full Fuel 1,274 lbs

Typical Trip Time and Burns
900 NM Trip, 2:45 2.250 lbs

General
Certification Status FAR 25

Engines
Manufacturer Pratt & Whitney
Model JT15D-4
Thrust 2,500 lbs

Exterior Dimensions
Length 47' 3"
Wing Span 52' 2"
Height 15' 0"

Internal Dimensions
Length 249"
Height 57"
Passenger Cabin Volume 343 Cu. Ft.

Accomodations
Passenger Seats 6-9
Baggage Capacity 77 Cu. Ft. / 1,450 lbs

Pressurization
Differential 8.8 PSI
8,000 ft Cabin at 43,000 Ft

Altitudes
Certified 43,000 Ft.
Service Ceiling 1 Engine (MGTOW) 23,500 Ft.

Certified Weights
Maximum Ramp Weight 14,300 lbs
Maximum Take Off Weight 14,100 lbs
Maximum Fuel Capacity 4,972 lbs

Basic Operating Weights
Typical Empty Weight 8,500 lbs
Basic Operating Weight 8,900 lbs

Payload
Usefull Payload and fuel 5,400 lbs
Payload at Full Fuel 428 lbs

Typical Trip Time and Burns
900 NM Trip 2:28 2,600 Lbs

()=Ultra

General
Certification Status FAR 25

Engines
Manufacturer Pratt & Whitney
Model JT15D-5A (5D)
Thrust 2,900 LBS (3,045 LBS)

Exterior Dimensions
Length 48' 11"
Wing Span 52' 6"
Height 15' 0"

Internal Dimensions
Length 269"
Heigth 57"
Passenger Cabin Volume 370 Cu. Ft.

Accomodations
Passenger Seats 6-9
Baggage Capacity 67 Cu Ft. / 1,450 lbs

Pressurization
Differential 8.9 PSI
8,000 Ft. Cabin at 45,000 Ft.

Altitudes
Certified 45,000 Ft.
Service Ceiling 1 Engine MGTOW 26,000 Ft.

Certified Weights
Maximum Ramp Weight 16,100 Lbs (16,500 Lbs)
Maximum Take Off Weight 15,900 Lbs (16,300 Lbs)
Maximum Fuel Capacity 5,771 Lbs

Basic Operating Weights
Typical Empty Weight 9,300 Lbs (9,550 Lbs)
Basic Operating Weight 9,700 Lbs (9,950 Lbs)

Payload
Useful Payload and Fuel 6,400 Lbs (6,550 Lbs)
Payload at Full Fuel 630 Lbs (779 Lbs)

Typical Trip Time and Burns
900 NM Trip 2:18 2,940 Lbs
(2:14 3,067 LBS)

General
Certification Status FAR 25

Engines
Manufacturer Pratt & Whitney
Model PW 545A
Thrust 3,804 Lbs

Exterior Dimensions
Length 51' 10"
Wing Span 55' 8"
Height 17' 2"

Internal Dimensions
Length 24' 3"
Height 5' 8"
Passenger Cabin Volume 400 Cu. Ft.

Accomodations
Passenger Seats 7-9
Baggage Capacity 83 Cu. Ft. / 700 Lbs

Pressurization
Differential 9.3 PSI
8,000 Ft Cabin at 45,000 Ft.

Altitudes
Certified 45,000 ft.
Service Ceiling 1 Engine MGTOW 28,600 Ft.

Certified Weights
Maximum Ramp Weight 20,200 Lbs
Maximum Take Off Weight 20,000 Lbs
Maximum Fuel Capacity 6,740 Lbs

Basic Operating Weights
Typical Empty Weight 12,150 Lbs
Basic Operating Weight 12,550 Lbs

Payload
UseFul Payload and Fuel 7,650 Lbs
Payload at Full Fuel 910 Lbs

Typical Trip Time and Burns
900 NM Trip 2:12 3,662 Lbs

()=CJ1
(())= CJ1+

General
Certification Status Part 23

Engines
Manufacturer Williams
Model FJ-44-1A
Thrust 1,900 Lbs
FJ44-1AP 1,965 Lbs CJ1+

Exterior Dimensions
Length 42' 7"
Wing Span 46' 10"
Height 13' 10"

Internal Dimensions
Length 15" 9"
Height 4' 9"
Passenger Cabin Volume 186 Cu. Ft.

Accomodations
Passenger Seats 5-6
Baggage Capacity 59 Cu. Ft. / 825 lbs

Pressurization
Differential 8.5 PSI
8,000 Ft. Cabin at 41,000 Ft.

Altitudes
Certified 41,000 Ft.
Service Ceiling 1 Engine MGTOW 23,000 Ft

Certified Weights
Maximum Ramp Weight 10,500 (10,700)((10,800)) Lbs
Maximum Take Off Weight 10,400 (10,600) ((10,700)) Lbs
Maximum Fuel Capacity 3,220 Lbs

Basic Operating Weights
Typical Empty Weight 6,550 (6,605) ((6,765)) Lbs
Basic Operating Weight Single Pilot 6,750 (6,805) ((6,965))

Payload
Useful Payload and Fuel 3,759 (3,895)((3,835))
Payload at Full Fuel 530 (675)((615))

Typical Trip Time and Burns
900 NM Trip 2:40 1900 Lbs

General
Certification Status Part 23

Engines
Manufacturer : William-Rolls
Model : FJ-44-2C
Thrust 2,300 Lbs

Exterior Dimensions
Length 46' 10"
Wing Span 49' 6"
Height 13' 10"

Internal Dimensions
Length 18'11"
Height 4'9"

Accomodations
Passenger Seats 6-8
Baggage Capacity 74 Cu. Ft / 1,100 Lbs

Pressurization
Differential 8.9 PSI
8,000 Ft. Cabin at 45,000 Ft.

Altitudes
Certified 45,000 Ft

Certified Weights
Maximum Ramp Weight
Maximum Take Off Weight
Maximum Fuel Capacity

Basic Operating Weights
Typical Empty Weight 7,625 lbs
Basic Operating Weight (SP) 7,825

Payload
Useful Payload and Fuel 4,600 lbs
Payload at Full Fuel 600 lbs

Typical Trip Tiem and Burns
900 NM trip 2:26 2,200lbs

Ceiling 45,000 ft (13,716 m) maximum certified

Airspeed Limits Vmo at sea level to 8,000 ft (2,438 m) / 260 KCAS (482 km/hr)
Vmo at 8,000 ft (2,438 m) to 29,300 ft (8,931 m) / 275 KCAS (509 km/hr)
Mmo at 29,300 ft (8,931 m) and above / 0.72 Mach

Climb Performance Single engine 1,020 fpm (311 mpm)

Stall speed 86 KCAS (159 km/hr) in landing configuration at 12,750 lbs (5,783 kg)

Maximum Cruise Speed 417 KTAS (772 km/hr), 33,000 ft (10,058 m)

Pressurization Nominal pressure differential is 8.9 psi

Range 1,900 nautical miles (3,518 km) VFR with 45-minute reserve

Engine Williams-Rolls FJ44-3A Turbofan
Takeoff thrust 2,780 lbs ea. (12.36 kN)

Outside dimensions Wingspan 52' 11" (16.13 m)
Overall height 15' 2" (4.62 m)
Overall length 51' 2" (15.61 m)

Cabin Dimensions (with typical interior installed) Height 4' 9" (1.45 m)
Width 4' 8" (1.43 m)
Length (forward pressure bulkhead to aft pressure bulkhead) 20' 10" (6.35 m)


Design Weights & Fuel Capacity
ENGLISH (METRIC)


Maximum ramp weight 14,070 lbs (6,382 kg)
Maximum takeoff weight 13,870 lbs (6,291 kg)
Maximum fuel weight @ 6.7 lbs/gal 4,710 lbs (2,136 kg)
Basic empty weight* 8,160 lbs (3,701 kg)
Useful payload and fuel at ramp 5,510 lbs (2,500 kg)
Payload with maximum fuel (two pilots) 800 lbs (363 kg)
Maximum payload 1,950 lbs (884 kg)
Maximum landing weight 12,750 lbs (5,783 kg)
Maximum zero fuel weight 10,510 lbs (4,767 kg)
Two pilots and furnishings 400 lbs (182 kg)
Basic operating weight (two pilots) 8,560 lbs (3,883 kg)

Citation Mustang Preliminary Specifications
Cruise Speed340 KTAS (630 km/hr) at 35,000 ft (10,668 m)
Ceiling 41,000 ft (12,497 m) maximum certified
Range 1,300 nm (2,408 km) VFR with 45-minute reserves
Takeoff Distance3,120 ft (951 m) at MTOW
EnginesTakeoff thrust 1,350 lbs ea. (6.01 kN)
Outside Dimensions WingspanOverall height Overall length
Cabin Dimensions 42'3"13'9"39'11"
HeightWidth 4'6"4'7"
Length (forward pressure bulkhead to aft pressure bulkhead)
Exterior Baggage Compartments (2)
14'6" (4.42 m) Total Volume
45.0 cu ft (1.27 m cu) Payload with maximum fuel anda single pilot600 lbs (272 kg)