Range Map
Origin: → · two fingers to move map
Payload vs. Range
Fuel on board
Cargo
nm
Range
Trip Preview
Name a destination in the map header above and this becomes your trip: time en route, what you burn, what it costs, and whether you get there without stopping — at the load you have set.
→
Over max payload by . At this load it cannot lift a single occupant. Please adjust your payload inputs.
We do not have a cruise speed on file for this aircraft, so there is no honest time or cost to give you for this leg.
En route
Fuel burned
Direct cost
Fuel cost
Tanks run dry about past before at this burn.
Mission Profile
- High-Altitude
- Pressurization
- Multi-Engine
- Instrument
Estimated Ownership Costs
Create a free account to view or request ownership cost data.
About the Cessna Citation Bravo
Type certificated 1997
Overview
The Cessna Citation Bravo (Model 550) is the modern, final development of the straight-wing Citation 550 line, produced from 1997 through 2006. It re-engined the earlier Cessna Citation II with Pratt & Whitney Canada PW530A turbofans (2,887 lbf each), replaced the analogue panel with a Honeywell Primus 1000 EFIS glass cockpit, and added trailing-link main landing gear, keeping the proven 550 fuselage and short-field manners while resolving the original II’s avionics and engine-economics shortcomings.
For the GA buyer, the Bravo is a strong owner-operator entry into the cabin-class light-jet bracket. Its PW530A engines burn less fuel than the JT15D-4 Citation II (170 versus 180 GPH) and run a longer 4,000-hour overhaul interval, and the modern flight deck, trailing-link gear, and 45,000 ft ceiling lift comfort and capability over the earlier II. As with every light jet, engine condition dominates resale value, so a clean PW530A status at pre-buy carries outsized weight.
Key Features for GA Buyers
- PW530A turbofans. The 2,887 lbf PW530A burns less fuel than the Citation II’s JT15D-4 (170 versus 180 GPH) and carries a longer 4,000 hr TBO, the main reason a buyer steps up from the II to the Bravo.
- Honeywell Primus 1000 glass cockpit. Modern EFIS displays and integrated autopilot come standard, where the original II requires expensive retrofit programs to match.
- Trailing-link main gear. The Bravo’s trailing-link gear forgives imperfect arrivals and is a feature owners of the late Citation line consistently praise.
- 45,000 ft ceiling with short-field access. The Bravo climbs above weather and most traffic, yet still operates from runways under 4,000 ft, reaching regional fields that faster swept-wing jets must avoid.
Trade-offs
- Aging Primus 1000 avionics. The Primus 1000, while reliable, is a 1990s-generation system; CRT and display parts are increasingly expensive, and many owners invest in flat-panel upgrades.
- Block speed. Cruise tops out near 400 KTAS, the enduring straight-wing trade against newer swept-wing light jets such as the Cessna Citation CJ3 and Embraer Phenom 300.
- Required two-pilot operation. The Model 550 Bravo is not single-pilot certificated; owner-operator economics must include a second pilot or contract crew.
- Modest cabin by modern standards. The 550-series cabin seats seven to eight comfortably but is modest next to current stand-up-cabin jets such as the Cessna Citation Excel / XLS, and retains the dropped center aisle.
See Also
- Cessna Citation II – the JT15D-4 predecessor the Bravo modernised; the more affordable straight-wing 550 entry. Compare
- Cessna Citation I – the foundational, smaller straight-wing Citation two steps down. Compare
- Cessna Citation V – the larger, faster Model 560 family (V, Ultra, Encore) one step up. Compare
- Cessna Citation Excel / XLS – the stand-up-cabin mid-light Citation that supplanted the Bravo at the upper end of the bracket. Compare
- Beechcraft King Air 200 – the turboprop alternative for owners prioritising operating cost over speed in the same cabin class. Compare
Technical Specifications
Dimensions & Weights
- Height
- 15 ft
- Length
- 47 ft
- Parking area (ft²2)
- 3,222 ft²
- Max Takeoff Weight
- 14,800 lbs
- Max Landing Weight
- 13,500 lbs
- Useful Load
- 5,500 lbs
- Fuel Capacity
- Source: FAA Type Certificate Data Sheet 720 gal
Performance
- Cruise Speed
- 401 KTAS
- Never-Exceed (VNE)
- Source: FAA Type Certificate Data Sheet 260 KIAS
- Max Structural Cruise (VNO)
- Source: FAA Type Certificate Data Sheet 260 KIAS
- Approach Speed
- 102 KIAS
- Stall, Clean (VS1)
- 82 KIAS
- Range
- 1740 NM
- Service Ceiling
- 45,000 ft
- Rate of Climb
- 3195 fpm
- Takeoff over 50 ft obstacle
- 3,600 ft
- Landing over 50 ft obstacle
- 2,517 ft
Engines
Log in to view or request powerplant data.
Sources
Where the figures on this page come from. Cessna Citation Bravo specifications are traced to published references; estimated values are flagged inline next to the figure.
Similar to the Cessna Citation Bravo
Similar TurbofansCessna Citation Encore
Cessna Citation Ultra
Cessna Citation V
Learjet 75
Cessna Citation II
Cessna Excel/XLS
North American Rockwell Sabre 75
Pilatus PC-24
North American Rockwell Sabre 40/60
Learjet 45
Compare the Cessna Citation Bravo to other aircraft
External Media
Videos
Articles and other links
-
Cessna Citation II / Bravo - Wikipedia en.wikipedia.org
-
II for the road (Citation II family review) - AOPA www.aopa.org
-
Bravo to a beautiful jet - Asian Aviation asianaviation.com
-
Citation Bravo Performance, Specifications and Comparisons - Liberty Jet www.libertyjet.com
-
Cessna Citation Bravo - Air Charter Service www.aircharterserviceusa.com
-
Citation Bravo | Article - Jet Advisors jetadvisors.com
-
PlanePhD: Cessna 550 Citation Bravo operating cost wizard planephd.com