The Cessna Citation Bravo is a development of the Citation II in the Cessna Citation business jet line.
By 1994, the Citation II and S/II had been in production for 10 years, and it was time to integrate new technology. Cessna thus announced the development of the Citation Bravo. While it was built on the basic II airframe, the new aircraft was powered by Pratt & Whitney Canada PW530A engines. The main landing gear was replaced by the smoother-riding trailing link configuration adopted by other members of the Citation line, and the standard avionics suite was updated to the Honeywell Primus 1000 glass cockpit. The new aircraft first flew on April 25, 1995, but certification did not come for over a year, finally being granted in August 1996.Production of the Bravo ceased in late 2006 after 337 had been built.
Specs
Weight (lb)
- Max Ramp: 15,000
- Max Takeoff: 14,800
- Max Landing: 13,500
- Zero Fuel: 11,300
- Max Payload: 1,800
- Useful Load: 5,500
- Executive Payload: 1,400
- Max Fuel: 4,824
- Avail Payload Max Fuel: 676
- Avail Fuel Max Payload: 3,700
- Avail Fuel Exec Payload: 4,100
Limits
- MMO: 0.700
- Transition Altitude FL/VMO FL: 279/275
- Cabin Pressurization (PSI): 8.9
Airport Performance
- TO (Sea Level, ISA Temp): 3,600
- TO (5000′, @25C): 5,520
- V2 @ SL ISA, MTOW: 121
- VREF: 102
- Landing Distance with 4 Passengers: 2,517
Climb and Cruise
Ceilings
- Certificated: 45,000
- All Eng Srv: 43,000
- Eng Out Srv: 27,750
Climb
- Time to Climb/Alt: 19/FL 370
- Engine Out Rate fpm: 845
- FAR 25 Engine-Out Grad (ft/nm): 419
Long Range Cruise
- KTAS: 342
- Fuel Flow: 607
- Altitude: FL450
- Specific Range: 0.563
High Speed Cruise
- KTAS: 399
- Fuel Flow: 1,135
- Altitude: FL350
- Specific Range: 0.352
Aircraft help
| Key
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Function
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| Del
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Toggle thrust reversers
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| Ctrl+b
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Toggle speedbrakes
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| Ctrl+d
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Open/close cabin door
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