Mustang Phenom Comparison
Content
Cessna Citation Mustang
compared to the
Embraer Phenom 100
Cessna Aircraft Company Alessandro Barizzi, Director of Sales March, 2009
Contents
This Comparative Analysis Report examines the features and benefits of the Cessna Citation Mustang relative to the Embraer Phenom 100. This report will consider the 1 following subjects critical in the decision making process.
• Summary / Takeaways • Performance Capabilities • Cabin Comfort • Economics / Operating Costs • Systems Overview • Customer Support • Specifications
1. This comparative analysis utilizes data from Embraer's FAA Aircraft Flight manual (AFM-2656), dated 12/12/2008 and Pilot's Operating Handbook (POH-2761). At this time, information on the Phenom's "Enhanced" takeoff performance" is not available. All takeoff analysis in this report is based on "standard" takeoff performance.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Takeaways
The Cessna Citation Mustang offers greater value than the Embraer Phenom 100:
Performance: The Citation Mustang is more versatile
Able to use hundreds of additional airports due to its shorter runway requirements Superior high altitude / hot temperature takeoff performance provides greater mission flexibility Climbs to more fuel-efficient altitudes faster and transitions through weather more quickly Slower critical airspeeds enhance safety during takeoff and landing
Economics: The Citation Mustang costs less
Lower acquisition cost More economical to operate Consumes less fuel on every mission
Customer Support: Cessna is an industry leader in Product Support
Consistently high-rated organization by Professional Pilot's Product Support survey Extensive network of company-owned facilities that only service Citation aircraft MSG-3 based maintenance program plus state-of-the-art diagnostic systems reduce downtime and maintenance expense Comprehensive warranty program administered entirely by Cessna – no need to deal with a separate vendor for engine issues, and its transferable
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
PERFORMANCE
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Takeoff Performance
The Citation Mustang's excellent takeoff performance offers far greater mission capability than the Phenom 100 when using short runways.
Range versus Runway Length 1
NBAA IFR Range (nautical miles)
When departing from airports with short runways, the Citation Mustang will be able to complete more of its mission's non-stop. The Phenom 100 will require significantly more fuel stops to complete its missions.
Runway Length - Temperature 2,500 feet – 15°C/59°F 3,000 feet – 15°C/59°F 3,000 feet – 35°C/95°F
Citation Mustang 505 nm 1,052 nm 632 nm
Phenom 100 Unable to Depart 814 nm Unable to Depart
1
Range vs Runway Length at Sea Level
1,200
15°C/59°F 35°C/95°F
1,000 800 600 400 200 2,000 Citation Mustang Phenom 100
2,500
3,000
3,500
4,000
4,500
5,000
Runway Length Available (feet)
1. NBAA IFR Reserves (100 nm alternate), Sea Level, ISA, Zero Wind, Dry Level Runway, High-Speed Cruise Power, FL410, Single Pilot, 3 Passengers.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Climb Performance
The Citation Mustang will climb to altitude faster than the Phenom 100 as well as climbing direct to its certified ceiling of 41,000 feet.
Time to Climb 1
Altitude 35,000 feet 39,000 feet 41,000 feet Citation Mustang 18 min 22 min 27 min Phenom 100 2 20 min 26 min Unable Climb Direct
Time to Climb
41,000
1&2
37,000
33,000
29,000 Citation Mustang Phenom 100 25,000 0 5 10 15 20 25 30 Time from Sea Level (minutes)
The Citation Mustang can reduce fuel expense and provide a more comfortable flight because it can reach fuel-efficient cruise altitudes faster and transition through weather quicker.
1. From Sea Level, Maximum Rate Climb Schedule, Maximum Takeoff Weight, ISA. 2. Phenom 100 climb performance starts at 1,500 feet per the Pilots Operating Handbook and not sea level like the Citation Mustang.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Altitude (feet)
Cruise Performance
The Phenom 100 does exhibit faster cruise speeds than the Citation Mustang. Those speeds, however, translate into a minimal total flight time difference when you examine typical missions.
Cruise Performance
Typical Cruise Speeds 1 Flight Time - 200 nm Mission 2 Flight Time - 500 nm Mission 2 Flight Time - 1,000 nm Mission 2 Citation Mustang 320 - 345 kt 0:40 1:36 3:16 Phenom 100 360 - 395 kt 0:36 1:27 3:01 Difference
0:04 0:09 0:15
The Phenom 100 will complete its missions only a few minutes before that of the Citation Mustang.
If the Citation Mustang can utilize an airport closer to your final destination due to its superior takeoff advantage, the reduction in drive time could more than offset any flight time savings by the Phenom 100.
1. Mid-Cruise Weight, ISA, High-Speed Cruise Power. 2. NBAA IFR Reserves (100 nm alternate), ISA, Zero Wind, Optimal Cruise Altitudes, High-Speed Cruise Power, Single Pilot, 3 Passengers.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Fuel Efficiency
The Citation Mustang is more fuel efficient than the Phenom 100. The Phenom 100 incurs a significant fuel burn penalty for its higher cruise speeds.
Fuel Efficiency
0.70 Citation Mustang Specific Fuel Consumption
(nautical miles per pound of fuel)
1
0.65 0.60 0.55 0.50 0.45 0.40 300
Phenom 100
325
350
375
400
425
450
Cruise Speed (knots)
Specific Fuel Consumption 1
Cruise Speed Associated Fuel Flow Specific Fuel Consumption Citation Mustang 2 338 kt 569 lb 0.594 nm/lb Phenom 100 2 373 kt 687 lb 0.543 nm/lb
The Citation Mustang will save fuel on each and every mission.
1. Mid-Cruise Weight, ISA, High-Speed Cruise Power. 2. Based on FL370.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Range Capability
The Citation Mustang and Phenom 100 have very similar range and payload capability.
Range Capability 1
NBAA Range – 2 Passengers NBAA Range – 4 Passengers NBAA Range – 6 Passengers Citation Mustang 1,175 nm 999 nm 716 nm Phenom 100 1,170 nm 969 nm 705 nm
The Citation Mustang has the same range capability as the Phenom 100.
Range versus Payload 1
1,400 Citation Mustang 1,200 Payload (pounds) 1,000 800 600 400 200 0 0 200 400 600 800 1,000 1,200 1,400 NBAA IFR Range (nautical miles)
1. NBAA IFR Reserves (100 nm alternate), ISA, Zero Wind, High-Speed Cruise Power, FL410, Single Pilot, Passengers at 200 Pounds Each.
Phenom 100
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Critical Airspeeds
The lower takeoff and landing speeds of the Citation Mustang offer greater margins of safety while maneuvering in close proximity to the ground. Its slower speeds allow pilots more reaction time for changing flight conditions.
Critical Airspeeds
Takeoff Decision Speed - V1
Max Takeoff Weight
1
Knots Indicated Airspeed
Citation Mustang 89 kt 89 kt 101 kt 94 kt 87 kt
(6,800 lb)
Phenom 100 95 kt 95 kt 105 kt 100 kt 94 kt
(8,500 lb)
Difference 6 6 4 6 7 9 4
Takeoff Rotation Speed - VR
Max Takeoff Weight
Landing Approach Speed - VApp
Max Landing Weight Max Landing Weight
One of Cessna's two prestigious Collier Trophy awards was for the Citation fleet's excellent safety record.
Landing Reference Speed - VRef Landing Reference Speed - VRef
Typical Landing Weight Flaps 0, 0 Bank
Stall Speed - Max Takeoff Wght Stall Speed - Landing Configuration
Max Landing Weight, Flaps Full, 0 Bank
91 kt 73 kt
100 kt 77 kt
1. Sea Level, ISA, Zero Wind
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Landing Performance
The Citation Mustang will always be able to land in a significantly shorter distance than the Phenom 100.
Landing Distances
3,000 1
●="Typical" 2
2,800 Landing Distance (feet) 2,600 2,400 2,200 2,000 1,800 6,000 Citation Mustang Phenom 100
The Citation Mustang's short landing distances and slow approach speeds enhance landing safety, particularly when utilizing airports with minimal runways.
7,000
8,000 Landing Weight (pounds)
9,000
10,000
Landing Performance 1
Max Wght Landing Distance Typical Landing Distance 2 Typical VRef Speed 2 Citation Mustang 2,380 ft 2,085 ft 87 kt Phenom 100 2,699 ft 2,473 ft 94 kt
1. Sea Level, ISA, Zero Wind, Dry Level Runway. 2. Typical Landing Weight Reflects NBAA IFR Reserves (100 nm alternate), Single Pilot, 3 Passengers.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
CABIN & BAGGAGE
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Cabin Design
The Citation Mustang offers a spacious and well-designed travel environment for this class of aircraft.
• Constant cross section offers a 54 inch high by 55 inch wide cabin.1 • Passenger cabin measures 9 feet 9 inches long. • Passenger seating area length of 6 feet 10 inches. • Four individual seats in a club seating arrangement. Two aft facing seats recline up to 25 degrees. Two forward facing seats are separated by a center console with a storage compartment and fold down armrest • Standard RH forward, side-facing, non-belted toilet – can also be used for baggage storage on top of the lid. • Left and right hand storage cabinets aft of the pilot seats. • Two executive tables installed in the sideledges.
The Citation Mustang provides all of the comfort and amenities for your travel needs.
1. Measured softgoods to softgoods with a typical interior installed.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Cabin Layout
Citation Mustang Phenom 100
Nose Baggage
Nose Baggage
5' 0"
(1.52 m)
Wardrobe Closet
2' 11"
(.89 m)
14' 9"
(4.49 m)
Toilet
9' 0"
Internal Dimensions 1
(2.74 m)
11' 0"
(3.35 m)
Cabin Height Cabin Width
Citation Mustang 54 in 55 in
Phenom 100 59 in 61 in
6' 10"
(2.08 m)
2' 0"
(.61 m)
Storage
Toilet
Tailcone Baggage
Tailcone Baggage
Standard interior configuration for both aircraft offers seating for four passengers.
1. Measured softgoods to softgoods with a typical interior installed.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Cabin Comfort
The Citation Mustang offers more seated legroom than the Phenom 100. Proof is from the Weight and Balance section of the respective Aircraft Flight Manuals.
Citation Mustang Phenom 100
Average Distance Between Seats
Citation Mustang Second row arm 299.10 in First row arm 252.89 in Distance Between 46.21 in Phenom 100 214.68 in 176.97 in 37.71 in
The Mustang offers an additional eight and one half inches of legroom between occupants in the club seats.
The Citation Mustang has more legroom between opposing seats for increased comfort.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
ECONOMICS
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Operating Costs
Operating Cost Comparison 1 According to a third party, the Citation Mustang is less expensive to operate than the Phenom 100.
Estimated Variable Cost per Hour
Citation Mustang
Fuel ($ 4.10 per gallon) Fuel Additives Maintenance Labor ($ 99.00 per hour) 3 Parts – Airframe/Engine/Avionics 3 Engine Restoration 4 Thrust Reverser Overhaul 5 APU Overhaul / Propeller Overhaul 6
2
Phenom 100
$ 430.50 -$ 62.37 $ 43.98 $ 120.13 --$ 656.98 313 $ 2.10
$ 369.00 -$ 59.40 $ 50.00 $ 125.00 --$ 603.40 310 $ 1.95
Total Variable Cost per Hour Average Speed (kt) 2 Cost per Nautical Mile
1. Source: Conklin & deDecker's The Aircraft Cost Evaluator (2008 Vol 1), electronic version. Fuel price and hourly shop rate are not Conklin supplied data. Total costs excludes non-aircraft related items such as crew expenses, supplies/catering, and miscellaneous items. Cessna does not warranty this information but merely provides this data for the customer's convenience. 2. Based on a 600 nautical mile trip using performance data derived from flight manuals – includes ground fuel. Conklin adds 15% to 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.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
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
The Citation Mustang's straightforward systems contribute to higher dispatch reliability and reduced downtime. Simplicity = less can go wrong.
• Wing leading edges and horizontal stabilizer is protected by pneumatic boots. • Windshield is electrically anti-iced and defogged and coated for rain removal.
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. • Dual Interface Adapter Units behind the PFDs (within the pressure vessel) are the heart of the system incorporating all communication, navigation, flight control and data management functions. • MFD is capable of displaying traffic, terrain, radar, graphical weather, airspace, airports, navaids, roads, Garmin's FlightCharts and Safe Taxi (U.S.), all standard. • Garmin FMS with dual WAAS enabled GPS navigation. • Standard Engine Indicating and Crew Alerting System information displayed on the left side of the MFD. • Additional standard features: Weather Avoidance Radar, Traffic Information System, Terrain Avoidance Warning System, dual Air Data Computers, and dual Attitude Heading Reference System.
The Citation Mustang's Garmin G1000 avionics offer tremendous functionality while keeping pilot workload low.
• Options: Chart View (Jeppesen charts), Honeywell Traffic Advisory System, and Sirius XM radio.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
CUSTOMER SUPPORT
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Customer Support
Cessna has consistently demonstrated a high level of industry leadership in the customer support area. Professional Pilot's annual Product Support Survey of jet operators consistently shows that Cessna is a highly rated, if not the best, support organization in the industry.
Professional Pilot Product Support Survey-Jets
10
1
Overall Average Score on a Scale of 1 (Poor) to 10 (Excellent) Cessna 9 Overall Average Score Top Score
Cessna's commitment to customer satisfaction and longterm relationships is evident in its customer ratings.
8
7
6
5 1998
1999
2000
2001
2002
2003 Survey Year
2004
2005
2006
2007
2008
1. Professional Pilot magazine, August, 2008.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Customer Support
Cessna maintains the largest customer support organization in the industry dedicated solely to maintaining the Citation fleet.
• Nine (soon 10) company-owned service facilities. • A network of 30+ authorized service facilities. • Field Service Representatives located around the world provide onsite service calls, AOG support, diagnostic help and assistance in establishing in-house maintenance programs. • Service "Teams" in Wichita that specialize by model 24/7/364. Each aircraft team has several members that maintain a specific realm of expertise to readily answer any maintenance questions. • CESCOM, Cessna's own on-line maintenance tracking program, tracks all service work on the aircraft and alerts you to upcoming maintenance events. • CPDXpress is an on-line, parts inquiry and ordering system and allows for filing warranty claims. • ProAdvantage cost control programs that allow you to manage your maintenance expenditures for most every component on the aircraft.
Cessna developed an extensive service organization to assure maximum control and utilization of your investment.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Service Facilities – Domestic
Cessna maintains the largest factory-owned service networks in existence, including eight facilities in North America along with eight Authorized Service Centers.
Cessna's company-owned facilities work only on Citation aircraft, allowing for greater specialization.
Portland Grand Junction Sacramento Phoenix Lincoln Wichita Dallas San Antonio Orlando Milwaukee Battle Creek E. Alton Greensboro Toronto Newburgh
Cessna-Owned Service Centers Authorized Service Centers
Toluca
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Service Facilities – International
Cessna's service network extends around the globe with 9 company-owned facilities (soon to be 10) and 34 Authorized Service Centers for your support needs.
(2010)
Cessna-Owned Service Centers Authorized Service Centers
All of Cessna's company-owned facilities are ISO 9002 certified and are open 7 days / 364 days per year.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Warranty
The Cessna Citation warranty is one of the most comprehensive in the industry.
Warranty Coverage
Major Airframe Manufacturer's Components Vendor Components Standard Avionics Engines Citation Mustang 3 Years / 1,000 Hours 3 Years / 1,000 Hours 1 Year 2 Years (Garmin) 3 Years / 1,000 Hours Phenom 100 3 Years / 1,500 Hours 3 Years / 1,500 Hours 3 Years / 1,000 Hours 3 Years / 1,000 Hours 3 Years / 1,000 Hours
Cessna administers all warranty issues – there is no need to deal with multiple vendors.
Cessna covers 100% of the parts, labor and freight (both to and from the factory) for the entire warranty period.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
SPECIFICATIONS
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Specifications
Citation Mustang
External Dimensions Length Height Wing Span Cabin Specifics 1 Length - Overall - Passenger Cabin - Seating Area Height Width Passenger Seating (standard - maximum) Baggage Capacity - Internal - External Engines Manufacturer Model Output 40 ft 7 in 13 ft 5 in 43 ft 2 in 14 ft 9 in 9 ft 9 in 6 ft 10 in 54 in 55 in 5-5 6 cuft / 98 lb 57 cuft / 620 lb Pratt & Whitney (2) PW615F 1,460 lb
Phenom 100
42 ft 1 in 14 ft 3 in 40 ft 4 in N/A 11 ft 0 in 9 ft 0 in 59 in 61 in 5-5 11 cuft / 99 lb 60 cuft / 419 lb Pratt & Whitney (2) PW617F 1,695 lb
1. All internal dimensions are with a typical interior installed.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Specifications
Citation Mustang
Performance Maximum Cruise Speed NBAA IFR Range - 4 Passengers
(alternate distance, cruise power setting)
Phenom 100
394 kt 969 nm
(100 nm, HSC, single pilot)
340 kt 999 nm
(100 nm, HSC, single pilot)
Takeoff Distance - MTOW, S.L., ISA Landing Distance - MLW, S.L., ISA Certified Ceiling Weights Maximum Ramp Weight Maximum Takeoff Weight Maximum Landing Weight Maximum Zero Fuel Weight Maximum Fuel Capacity Basic Operating Weight - includes pilots 1 Useful Load Maximum Payload Full-Fuel Payload 3
2
3,110 ft 2,380 ft 41,000 ft 8,730 lb 8,645 lb 8,000 lb 6,750 lb 2,580 lb 5,550 lb
(single pilot)
3,493 ft 2,699 ft 41,000 ft 10,516 lb 10,472 lb 9,766 lb 8,444 lb 2,806 lb 7,200 lb
(single pilot)
3,180 lb 1,200 lb 600 lb
3,316 lb 1,244 lb 510 lb
1. Typically-equipped empty weight of the aircraft (reflects typical interior, typical options, engine oil, unusable fuel) plus the weight of the pilots at 200 pounds each. 2. Total amount of fuel and payload the aircraft can carry, over and above the crew. 3. Passengers and/or cargo capacity with full fuel on-board.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
compared to the
Embraer Phenom 100
Cessna Aircraft Company Alessandro Barizzi, Director of Sales March, 2009
Contents
This Comparative Analysis Report examines the features and benefits of the Cessna Citation Mustang relative to the Embraer Phenom 100. This report will consider the 1 following subjects critical in the decision making process.
• Summary / Takeaways • Performance Capabilities • Cabin Comfort • Economics / Operating Costs • Systems Overview • Customer Support • Specifications
1. This comparative analysis utilizes data from Embraer's FAA Aircraft Flight manual (AFM-2656), dated 12/12/2008 and Pilot's Operating Handbook (POH-2761). At this time, information on the Phenom's "Enhanced" takeoff performance" is not available. All takeoff analysis in this report is based on "standard" takeoff performance.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Takeaways
The Cessna Citation Mustang offers greater value than the Embraer Phenom 100:
Performance: The Citation Mustang is more versatile
Able to use hundreds of additional airports due to its shorter runway requirements Superior high altitude / hot temperature takeoff performance provides greater mission flexibility Climbs to more fuel-efficient altitudes faster and transitions through weather more quickly Slower critical airspeeds enhance safety during takeoff and landing
Economics: The Citation Mustang costs less
Lower acquisition cost More economical to operate Consumes less fuel on every mission
Customer Support: Cessna is an industry leader in Product Support
Consistently high-rated organization by Professional Pilot's Product Support survey Extensive network of company-owned facilities that only service Citation aircraft MSG-3 based maintenance program plus state-of-the-art diagnostic systems reduce downtime and maintenance expense Comprehensive warranty program administered entirely by Cessna – no need to deal with a separate vendor for engine issues, and its transferable
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
PERFORMANCE
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Takeoff Performance
The Citation Mustang's excellent takeoff performance offers far greater mission capability than the Phenom 100 when using short runways.
Range versus Runway Length 1
NBAA IFR Range (nautical miles)
When departing from airports with short runways, the Citation Mustang will be able to complete more of its mission's non-stop. The Phenom 100 will require significantly more fuel stops to complete its missions.
Runway Length - Temperature 2,500 feet – 15°C/59°F 3,000 feet – 15°C/59°F 3,000 feet – 35°C/95°F
Citation Mustang 505 nm 1,052 nm 632 nm
Phenom 100 Unable to Depart 814 nm Unable to Depart
1
Range vs Runway Length at Sea Level
1,200
15°C/59°F 35°C/95°F
1,000 800 600 400 200 2,000 Citation Mustang Phenom 100
2,500
3,000
3,500
4,000
4,500
5,000
Runway Length Available (feet)
1. NBAA IFR Reserves (100 nm alternate), Sea Level, ISA, Zero Wind, Dry Level Runway, High-Speed Cruise Power, FL410, Single Pilot, 3 Passengers.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Climb Performance
The Citation Mustang will climb to altitude faster than the Phenom 100 as well as climbing direct to its certified ceiling of 41,000 feet.
Time to Climb 1
Altitude 35,000 feet 39,000 feet 41,000 feet Citation Mustang 18 min 22 min 27 min Phenom 100 2 20 min 26 min Unable Climb Direct
Time to Climb
41,000
1&2
37,000
33,000
29,000 Citation Mustang Phenom 100 25,000 0 5 10 15 20 25 30 Time from Sea Level (minutes)
The Citation Mustang can reduce fuel expense and provide a more comfortable flight because it can reach fuel-efficient cruise altitudes faster and transition through weather quicker.
1. From Sea Level, Maximum Rate Climb Schedule, Maximum Takeoff Weight, ISA. 2. Phenom 100 climb performance starts at 1,500 feet per the Pilots Operating Handbook and not sea level like the Citation Mustang.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Altitude (feet)
Cruise Performance
The Phenom 100 does exhibit faster cruise speeds than the Citation Mustang. Those speeds, however, translate into a minimal total flight time difference when you examine typical missions.
Cruise Performance
Typical Cruise Speeds 1 Flight Time - 200 nm Mission 2 Flight Time - 500 nm Mission 2 Flight Time - 1,000 nm Mission 2 Citation Mustang 320 - 345 kt 0:40 1:36 3:16 Phenom 100 360 - 395 kt 0:36 1:27 3:01 Difference
0:04 0:09 0:15
The Phenom 100 will complete its missions only a few minutes before that of the Citation Mustang.
If the Citation Mustang can utilize an airport closer to your final destination due to its superior takeoff advantage, the reduction in drive time could more than offset any flight time savings by the Phenom 100.
1. Mid-Cruise Weight, ISA, High-Speed Cruise Power. 2. NBAA IFR Reserves (100 nm alternate), ISA, Zero Wind, Optimal Cruise Altitudes, High-Speed Cruise Power, Single Pilot, 3 Passengers.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Fuel Efficiency
The Citation Mustang is more fuel efficient than the Phenom 100. The Phenom 100 incurs a significant fuel burn penalty for its higher cruise speeds.
Fuel Efficiency
0.70 Citation Mustang Specific Fuel Consumption
(nautical miles per pound of fuel)
1
0.65 0.60 0.55 0.50 0.45 0.40 300
Phenom 100
325
350
375
400
425
450
Cruise Speed (knots)
Specific Fuel Consumption 1
Cruise Speed Associated Fuel Flow Specific Fuel Consumption Citation Mustang 2 338 kt 569 lb 0.594 nm/lb Phenom 100 2 373 kt 687 lb 0.543 nm/lb
The Citation Mustang will save fuel on each and every mission.
1. Mid-Cruise Weight, ISA, High-Speed Cruise Power. 2. Based on FL370.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Range Capability
The Citation Mustang and Phenom 100 have very similar range and payload capability.
Range Capability 1
NBAA Range – 2 Passengers NBAA Range – 4 Passengers NBAA Range – 6 Passengers Citation Mustang 1,175 nm 999 nm 716 nm Phenom 100 1,170 nm 969 nm 705 nm
The Citation Mustang has the same range capability as the Phenom 100.
Range versus Payload 1
1,400 Citation Mustang 1,200 Payload (pounds) 1,000 800 600 400 200 0 0 200 400 600 800 1,000 1,200 1,400 NBAA IFR Range (nautical miles)
1. NBAA IFR Reserves (100 nm alternate), ISA, Zero Wind, High-Speed Cruise Power, FL410, Single Pilot, Passengers at 200 Pounds Each.
Phenom 100
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Critical Airspeeds
The lower takeoff and landing speeds of the Citation Mustang offer greater margins of safety while maneuvering in close proximity to the ground. Its slower speeds allow pilots more reaction time for changing flight conditions.
Critical Airspeeds
Takeoff Decision Speed - V1
Max Takeoff Weight
1
Knots Indicated Airspeed
Citation Mustang 89 kt 89 kt 101 kt 94 kt 87 kt
(6,800 lb)
Phenom 100 95 kt 95 kt 105 kt 100 kt 94 kt
(8,500 lb)
Difference 6 6 4 6 7 9 4
Takeoff Rotation Speed - VR
Max Takeoff Weight
Landing Approach Speed - VApp
Max Landing Weight Max Landing Weight
One of Cessna's two prestigious Collier Trophy awards was for the Citation fleet's excellent safety record.
Landing Reference Speed - VRef Landing Reference Speed - VRef
Typical Landing Weight Flaps 0, 0 Bank
Stall Speed - Max Takeoff Wght Stall Speed - Landing Configuration
Max Landing Weight, Flaps Full, 0 Bank
91 kt 73 kt
100 kt 77 kt
1. Sea Level, ISA, Zero Wind
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Landing Performance
The Citation Mustang will always be able to land in a significantly shorter distance than the Phenom 100.
Landing Distances
3,000 1
●="Typical" 2
2,800 Landing Distance (feet) 2,600 2,400 2,200 2,000 1,800 6,000 Citation Mustang Phenom 100
The Citation Mustang's short landing distances and slow approach speeds enhance landing safety, particularly when utilizing airports with minimal runways.
7,000
8,000 Landing Weight (pounds)
9,000
10,000
Landing Performance 1
Max Wght Landing Distance Typical Landing Distance 2 Typical VRef Speed 2 Citation Mustang 2,380 ft 2,085 ft 87 kt Phenom 100 2,699 ft 2,473 ft 94 kt
1. Sea Level, ISA, Zero Wind, Dry Level Runway. 2. Typical Landing Weight Reflects NBAA IFR Reserves (100 nm alternate), Single Pilot, 3 Passengers.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
CABIN & BAGGAGE
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Cabin Design
The Citation Mustang offers a spacious and well-designed travel environment for this class of aircraft.
• Constant cross section offers a 54 inch high by 55 inch wide cabin.1 • Passenger cabin measures 9 feet 9 inches long. • Passenger seating area length of 6 feet 10 inches. • Four individual seats in a club seating arrangement. Two aft facing seats recline up to 25 degrees. Two forward facing seats are separated by a center console with a storage compartment and fold down armrest • Standard RH forward, side-facing, non-belted toilet – can also be used for baggage storage on top of the lid. • Left and right hand storage cabinets aft of the pilot seats. • Two executive tables installed in the sideledges.
The Citation Mustang provides all of the comfort and amenities for your travel needs.
1. Measured softgoods to softgoods with a typical interior installed.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Cabin Layout
Citation Mustang Phenom 100
Nose Baggage
Nose Baggage
5' 0"
(1.52 m)
Wardrobe Closet
2' 11"
(.89 m)
14' 9"
(4.49 m)
Toilet
9' 0"
Internal Dimensions 1
(2.74 m)
11' 0"
(3.35 m)
Cabin Height Cabin Width
Citation Mustang 54 in 55 in
Phenom 100 59 in 61 in
6' 10"
(2.08 m)
2' 0"
(.61 m)
Storage
Toilet
Tailcone Baggage
Tailcone Baggage
Standard interior configuration for both aircraft offers seating for four passengers.
1. Measured softgoods to softgoods with a typical interior installed.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Cabin Comfort
The Citation Mustang offers more seated legroom than the Phenom 100. Proof is from the Weight and Balance section of the respective Aircraft Flight Manuals.
Citation Mustang Phenom 100
Average Distance Between Seats
Citation Mustang Second row arm 299.10 in First row arm 252.89 in Distance Between 46.21 in Phenom 100 214.68 in 176.97 in 37.71 in
The Mustang offers an additional eight and one half inches of legroom between occupants in the club seats.
The Citation Mustang has more legroom between opposing seats for increased comfort.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
ECONOMICS
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Operating Costs
Operating Cost Comparison 1 According to a third party, the Citation Mustang is less expensive to operate than the Phenom 100.
Estimated Variable Cost per Hour
Citation Mustang
Fuel ($ 4.10 per gallon) Fuel Additives Maintenance Labor ($ 99.00 per hour) 3 Parts – Airframe/Engine/Avionics 3 Engine Restoration 4 Thrust Reverser Overhaul 5 APU Overhaul / Propeller Overhaul 6
2
Phenom 100
$ 430.50 -$ 62.37 $ 43.98 $ 120.13 --$ 656.98 313 $ 2.10
$ 369.00 -$ 59.40 $ 50.00 $ 125.00 --$ 603.40 310 $ 1.95
Total Variable Cost per Hour Average Speed (kt) 2 Cost per Nautical Mile
1. Source: Conklin & deDecker's The Aircraft Cost Evaluator (2008 Vol 1), electronic version. Fuel price and hourly shop rate are not Conklin supplied data. Total costs excludes non-aircraft related items such as crew expenses, supplies/catering, and miscellaneous items. Cessna does not warranty this information but merely provides this data for the customer's convenience. 2. Based on a 600 nautical mile trip using performance data derived from flight manuals – includes ground fuel. Conklin adds 15% to 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.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
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
The Citation Mustang's straightforward systems contribute to higher dispatch reliability and reduced downtime. Simplicity = less can go wrong.
• Wing leading edges and horizontal stabilizer is protected by pneumatic boots. • Windshield is electrically anti-iced and defogged and coated for rain removal.
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. • Dual Interface Adapter Units behind the PFDs (within the pressure vessel) are the heart of the system incorporating all communication, navigation, flight control and data management functions. • MFD is capable of displaying traffic, terrain, radar, graphical weather, airspace, airports, navaids, roads, Garmin's FlightCharts and Safe Taxi (U.S.), all standard. • Garmin FMS with dual WAAS enabled GPS navigation. • Standard Engine Indicating and Crew Alerting System information displayed on the left side of the MFD. • Additional standard features: Weather Avoidance Radar, Traffic Information System, Terrain Avoidance Warning System, dual Air Data Computers, and dual Attitude Heading Reference System.
The Citation Mustang's Garmin G1000 avionics offer tremendous functionality while keeping pilot workload low.
• Options: Chart View (Jeppesen charts), Honeywell Traffic Advisory System, and Sirius XM radio.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
CUSTOMER SUPPORT
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Customer Support
Cessna has consistently demonstrated a high level of industry leadership in the customer support area. Professional Pilot's annual Product Support Survey of jet operators consistently shows that Cessna is a highly rated, if not the best, support organization in the industry.
Professional Pilot Product Support Survey-Jets
10
1
Overall Average Score on a Scale of 1 (Poor) to 10 (Excellent) Cessna 9 Overall Average Score Top Score
Cessna's commitment to customer satisfaction and longterm relationships is evident in its customer ratings.
8
7
6
5 1998
1999
2000
2001
2002
2003 Survey Year
2004
2005
2006
2007
2008
1. Professional Pilot magazine, August, 2008.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Customer Support
Cessna maintains the largest customer support organization in the industry dedicated solely to maintaining the Citation fleet.
• Nine (soon 10) company-owned service facilities. • A network of 30+ authorized service facilities. • Field Service Representatives located around the world provide onsite service calls, AOG support, diagnostic help and assistance in establishing in-house maintenance programs. • Service "Teams" in Wichita that specialize by model 24/7/364. Each aircraft team has several members that maintain a specific realm of expertise to readily answer any maintenance questions. • CESCOM, Cessna's own on-line maintenance tracking program, tracks all service work on the aircraft and alerts you to upcoming maintenance events. • CPDXpress is an on-line, parts inquiry and ordering system and allows for filing warranty claims. • ProAdvantage cost control programs that allow you to manage your maintenance expenditures for most every component on the aircraft.
Cessna developed an extensive service organization to assure maximum control and utilization of your investment.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Service Facilities – Domestic
Cessna maintains the largest factory-owned service networks in existence, including eight facilities in North America along with eight Authorized Service Centers.
Cessna's company-owned facilities work only on Citation aircraft, allowing for greater specialization.
Portland Grand Junction Sacramento Phoenix Lincoln Wichita Dallas San Antonio Orlando Milwaukee Battle Creek E. Alton Greensboro Toronto Newburgh
Cessna-Owned Service Centers Authorized Service Centers
Toluca
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Service Facilities – International
Cessna's service network extends around the globe with 9 company-owned facilities (soon to be 10) and 34 Authorized Service Centers for your support needs.
(2010)
Cessna-Owned Service Centers Authorized Service Centers
All of Cessna's company-owned facilities are ISO 9002 certified and are open 7 days / 364 days per year.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Warranty
The Cessna Citation warranty is one of the most comprehensive in the industry.
Warranty Coverage
Major Airframe Manufacturer's Components Vendor Components Standard Avionics Engines Citation Mustang 3 Years / 1,000 Hours 3 Years / 1,000 Hours 1 Year 2 Years (Garmin) 3 Years / 1,000 Hours Phenom 100 3 Years / 1,500 Hours 3 Years / 1,500 Hours 3 Years / 1,000 Hours 3 Years / 1,000 Hours 3 Years / 1,000 Hours
Cessna administers all warranty issues – there is no need to deal with multiple vendors.
Cessna covers 100% of the parts, labor and freight (both to and from the factory) for the entire warranty period.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
SPECIFICATIONS
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Specifications
Citation Mustang
External Dimensions Length Height Wing Span Cabin Specifics 1 Length - Overall - Passenger Cabin - Seating Area Height Width Passenger Seating (standard - maximum) Baggage Capacity - Internal - External Engines Manufacturer Model Output 40 ft 7 in 13 ft 5 in 43 ft 2 in 14 ft 9 in 9 ft 9 in 6 ft 10 in 54 in 55 in 5-5 6 cuft / 98 lb 57 cuft / 620 lb Pratt & Whitney (2) PW615F 1,460 lb
Phenom 100
42 ft 1 in 14 ft 3 in 40 ft 4 in N/A 11 ft 0 in 9 ft 0 in 59 in 61 in 5-5 11 cuft / 99 lb 60 cuft / 419 lb Pratt & Whitney (2) PW617F 1,695 lb
1. All internal dimensions are with a typical interior installed.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
Specifications
Citation Mustang
Performance Maximum Cruise Speed NBAA IFR Range - 4 Passengers
(alternate distance, cruise power setting)
Phenom 100
394 kt 969 nm
(100 nm, HSC, single pilot)
340 kt 999 nm
(100 nm, HSC, single pilot)
Takeoff Distance - MTOW, S.L., ISA Landing Distance - MLW, S.L., ISA Certified Ceiling Weights Maximum Ramp Weight Maximum Takeoff Weight Maximum Landing Weight Maximum Zero Fuel Weight Maximum Fuel Capacity Basic Operating Weight - includes pilots 1 Useful Load Maximum Payload Full-Fuel Payload 3
2
3,110 ft 2,380 ft 41,000 ft 8,730 lb 8,645 lb 8,000 lb 6,750 lb 2,580 lb 5,550 lb
(single pilot)
3,493 ft 2,699 ft 41,000 ft 10,516 lb 10,472 lb 9,766 lb 8,444 lb 2,806 lb 7,200 lb
(single pilot)
3,180 lb 1,200 lb 600 lb
3,316 lb 1,244 lb 510 lb
1. Typically-equipped empty weight of the aircraft (reflects typical interior, typical options, engine oil, unusable fuel) plus the weight of the pilots at 200 pounds each. 2. Total amount of fuel and payload the aircraft can carry, over and above the crew. 3. Passengers and/or cargo capacity with full fuel on-board.
HOME | SUMMARY | PERFORMANCE | CABIN & BAGGAGE | ECONOMICS | SYSTEMS OVERVIEW | CUSTOMER SUPPORT | SPECIFICATIONS
