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the calculated fuel burn to "… account for less than ideal operating conditions."
3. Maintenance costs reflect scheduled, unscheduled, and on-condition maintenance for airframe, avionics, and minor engine
maintenance. "New aircraft maintenance costs show the benefit of warranty coverage. An aging factor is applied based on the age
of the aircraft. Labor/parts cost estimates reflect a 10-year time period to balance warranty with mature aircraft costs."
4. Based on "…a 10 year average of the Jet Support Services, Incorporated Complete program. JSSI Complete covers scheduled and
unscheduled maintenance, all required inspections and overhauls, airworthiness directives, service bulletins, and loaner engines."
5. "The parts and costs required to overhaul the thrust reversers with a set overhaul interval. Routine costs for on-condition thrust
reversers are included in the maintenance-parts and labor."
6. Costs associated with overhauling the component at its stated overhaul interval. Excludes routine and minor maintenance.
Operating Cost Comparison 1
Estimated Variable Cost per Hour
SYSTEMS OVERVIEW
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Systems Architecture
The Citation Mustang incorporates proven, reliable systems that have become the
hallmark of the Citation fleet.
Flight Controls
• All primary flight controls are operated through cables and
mechanical linkage – reduces complexity and increases dispatch
reliability.
• Electric trim systems for all three axis. Also, a manual pitch trim
wheel.
• Speed brake panels on both the upper and lower wing.
• Large fowler-type flaps.
Hydraulics
• Open-center, 1,500 psi system powered by an electric motor.
• System operates on demand which reduces wear on the pump
and system components, thus a lower chance of leaks.
• Powers the landing gear and wheel brakes. Two independent pneumatic systems provide backup.
Electrical
• 28 volt, parallel bus architecture system driven by two 300 ampere starter / generators.
• Each generator connected to a generator control unit (GCU) to allow load sharing and shedding.
• 28 ampere-hour battery located in the tailcone features easy disconnects for removal between flights.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Systems Architecture
Fuel
• All fuel is contained within the wings – each wing supplies its respective engine. System is fully automatic.
• Fuel is heated through an oil heat exchanger – no anti-ice additive required.
Environmental
• Digital controller regulates cabin pressure – maximum 8.30 psi.
• Standard vapor cycle system for additional cabin cooling – can be operated on the ground.
• Separate cockpit and cabin temperature control zones.
Landing Gear / Brakes
• Trailing-link main landing gear – offers superior shock absorption on landing.
• Anti-skid brakes are powered by the hydraulic system with an emergency
pneumatic back-up system.
Ice Protection
• Wing leading edges and
horizontal stabilizer is
protected by pneumatic
boots.
• Windshield is electrically
anti-iced and defogged and coated for rain removal.
The Citation Mustang's
straightforward systems contribute
to higher dispatch reliability and
reduced downtime.
Simplicity = less can go wrong.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Powerplants
The Citation Mustang utilizes Pratt & Whitney's PW615F engine.
• High-efficiency turbofans featuring counter-rotating,
twin-spool design with three compression stages
and two turbine stages.
• Engines provide 1,460 pounds of thrust each at sea
level up to ISA + 10C.
• Full Authority Digital Engine Control (FADEC)
system – greatly reduces pilot workload and
enhances engine protection and diagnostics
capabilities. Detents in the throttle for takeoff, climb,
cruise and idle ensure optimal power settings.
• Time between overhaul (TBO) is 3,500 hours.
The Citation Mustang's
engines are fuel-efficient
and easy to operate.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Avionics
The Citation Mustang utilizes the Garmin G1000 fully-integrated avionics suite.
• Two large 10.4" PFDs plus a 15" MFD active matrix liquid crystal, high resolution displays.
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Cessna Citation Mustang compared to the Embraer Phenom 100(4)
