|
External
|
|
Length:
|
99.4 ft
|
 
|
 
|
30.3 m
|
|
Wingspan:
|
94 ft
|
 
|
 
|
28.6 m
|
|
Wing area (basic):
|
1,022 ft
|
² 
|
 
|
94.9 m
|
|
Height overall:
|
24.8 ft
|
 
|
 
|
7.6 m
|
|

|
|
Internal
|
|
Cabin length:
|
48.35 ft
|
 
|
 
|
14.7 m
|
|
(From cockpit divider to end of pressurized compartment)
|
|
Cabin maximum width: (Centerline)
|
8.17 ft
|
 
|
 
|
2.49 m
|
|
Cabin width: (Floorline)
|
6.92 ft
|
 
|
 
|
2.11 m
|
|
Cabin height:
|
6.25 ft
|
 
|
 
|
1.91 m
|
|
Floor area: (Excluding cockpit)
|
353 ft
|
²
|
 
|
31.1 m
|
|
Total volume:
|
2,140 ft
|
³
|
 
|
60.60 m
|
|
(From cockpit divider to end of pressurized compartment)
|
|

|
|
Weights
|
|
A. Maximum ramp weight:
|
98,250 lb
|
 
|
 
|
44,565 kg
|
|
B. Maximum takeoff weight:
|
98,000 lb
|
 
|
 
|
44,452 kg
|
|
C. Maximum landing weight:
|
78,600 lb
|
 
|
 
|
35,652 kg
|
|
D. Maximum zero fuel weight:
|
56,000 lb
|
 
|
 
|
25,401 kg
|
|
E. Basic operating weight:
|
51,500 lb
|
 
|
 
|
23,360 kg
|
|
F. Maximum fuel weight:
|
44,975 lb
|
 
|
 
|
20,400 kg
|
|
Manufacturer’s weight empty (±1%):
|
49,750 lb
|
 
|
 
|
22,566 kg
|
|
Maximum payload (D-E):
|
4,500 lb
|
 
|
 
|
2,041 kg
|
|
Payload – full fuel (A-E-F):
|
1,775 lb
|
 
|
 
|
805 kg
|
|
Fuel with maximum payload:
|
42,250 lb
|
 
|
 
|
19,162 kg
|
|
NBAA IFR fuel reserve (8 pax):
|
3,100 lb
|
 
|
 
|
1,406 kg
|
|
Operations at a reduced MGTOW:
|
75,000 lb
|
 
|
 
|
34,019 kg
|
|

|
|
PERFORMANCE
|
|
Range
|
|
Maximum range at M 0.85:
|
6,150 NM
|
|
11,389 km
|
|
(NBAA IFR Reserves, ISA, with 8 pax/4 crew and maximum fuel)
|
|

|
|
Speed
|
Mach
|
kts
|
mph
|
km/h
|
|
High-speed cruise
|
0.89
|
513
|
590
|
950
|
|
Typical cruise speed
|
0.85
|
488
|
562
|
904
|
|

|
|
Ceiling
|
|
Maximum operating altitude:
|
51,000 ft
|
 
|
 
|
15,545 m
|
|
Climb to cruise altitude of 43,000 ft
|
30 min
|
 
|
 
|
 
|
|
(13,106 m):
|
|

|
|
Cabin noise level
|
|
Average fleet:
|
51.8 dbM(SIL)/69.4 dbA
|
|