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 following subjects critical in the decision making process.
• Summary / Takeaways
• Performance Capabilities
• Cabin Comfort
• Economics / Operating Costs
• Systems Overview
• Customer Support
• Specifications
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1
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.
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
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PERFORMANCE
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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 Runway Length - Temperature Citation Mustang Phenom 100
2,500 feet – 15°C/59°F 505 nm Unable to Depart 3,000 feet – 15°C/59°F 1,052 nm 814 nm 3,000 feet – 35°C/95°F 632 nm Unable to Depart
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Range vs Runway Length at Sea Level 1
200
400
600
800
1,000
1,200
2,000 2,500 3,000 3,500 4,000 4,500 5,000Runway Length Available (feet)
NB
AA
IFR
Ran
ge (n
autic
al m
iles)
Citation MustangPhenom 100
15°C/59°F35°C/95°F
1. NBAA IFR Reserves (100 nm alternate), Sea Level, ISA, Zero Wind, Dry Level Runway, High-Speed Cruise Power, FL410, Single Pilot, 3 Passengers.
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.
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 Citation Mustang Phenom 100 2 35,000 feet 18 min 20 min 39,000 feet 22 min 26 min 41,000 feet 27 min Unable Climb Direct
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Time to Climb 1 & 2
25,000
29,000
33,000
37,000
41,000
0 5 10 15 20 25 30Time from Sea Level (minutes)
Alti
tude
(fee
t)
Citation MustangPhenom 100
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.
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
Citation Mustang Phenom 100 DifferenceTypical Cruise Speeds 1 320 - 345 kt 360 - 395 kt
Flight Time - 200 nm Mission 2 0:40 0:36 0:04 Flight Time - 500 nm Mission 2 1:36 1:27 0:09 Flight Time - 1,000 nm Mission 2 3:16 3:01 0:15
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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.
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.
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.
Specific Fuel Consumption 1 Citation Mustang 2 Phenom 100 2
Cruise Speed 338 kt 373 kt Associated Fuel Flow 569 lb 687 lb
Specific Fuel Consumption 0.594 nm/lb 0.543 nm/lb
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Fuel Efficiency 1
0.40
0.45
0.50
0.55
0.60
0.65
0.70
300 325 350 375 400 425 450
Cruise Speed (knots)
Spe
cific
Fue
l Con
sum
ptio
n(n
autic
al m
iles
per p
ound
of f
uel)
Citation MustangPhenom 100
1. Mid-Cruise Weight, ISA, High-Speed Cruise Power. 2. Based on FL370.
The Citation Mustang will save fuel on each and
every mission.
Range Capability
The Citation Mustang and Phenom 100 have very similar range and payload capability.
Range Capability 1 Citation Mustang Phenom 100
NBAA Range – 2 Passengers 1,175 nm 1,170 nm NBAA Range – 4 Passengers 999 nm 969 nm NBAA Range – 6 Passengers 716 nm 705 nm
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Range versus Payload 1
0
200
400
600
800
1,000
1,200
1,400
0 200 400 600 800 1,000 1,200 1,400
NBAA IFR Range (nautical miles)
Pay
load
(pou
nds)
Citation Mustang
Phenom 100
1. NBAA IFR Reserves (100 nm alternate), ISA, Zero Wind, High-Speed Cruise Power, FL410, Single Pilot, Passengers at 200 Pounds Each.
The Citation Mustang has the same range capability as
the Phenom 100.
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 1
Knots Indicated Airspeed
Citation Mustang Phenom 100 DifferenceTakeoff Decision Speed - V1
Max Takeoff Weight 89 kt 95 kt 6
Takeoff Rotation Speed - VR Max Takeoff Weight
89 kt 95 kt 6
Landing Approach Speed - VApp Max Landing Weight
101 kt 105 kt 4
Landing Reference Speed - VRefMax Landing Weight
94 kt 100 kt 6
Landing Reference Speed - VRefTypical Landing Weight
87 kt (6,800 lb)
94 kt (8,500 lb)
7
Stall Speed - Max Takeoff Wght Flaps 0, 0 Bank
91 kt 100 kt 9
Stall Speed - Landing ConfigurationMax Landing Weight, Flaps Full, 0 Bank
73 kt 77 kt 4
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One of Cessna's two prestigious Collier Trophy awards was for
the Citation fleet's excellent safety record.
1. Sea Level, ISA, Zero Wind
Landing Performance
The Citation Mustang will always be able to land in a significantly shorter distance than the Phenom 100.
Landing Performance 1 Citation Mustang Phenom 100
Max Wght Landing Distance 2,380 ft 2,699 ft Typical Landing Distance 2 2,085 ft 2,473 ft
Typical VRef Speed 2 87 kt 94 kt
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Landing Distances 1
1,800
2,000
2,200
2,400
2,600
2,800
3,000
6,000 7,000 8,000 9,000 10,000
Landing Weight (pounds)La
ndin
g D
ista
nce
(feet
)
Citation MustangPhenom 100
●="Typical" 2
1. Sea Level, ISA, Zero Wind, Dry Level Runway. 2. Typical Landing Weight Reflects NBAA IFR Reserves (100 nm alternate), Single Pilot, 3 Passengers.
The Citation Mustang's short landing distances
and slow approach speeds enhance landing safety, particularly when
utilizing airports with minimal runways.
CABIN & BAGGAGE
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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.
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The Citation Mustang provides all of the comfort and amenities
for your travel needs.
1. Measured softgoods to softgoods with a typical interior installed.
Cabin Layout
Internal Dimensions 1 Citation Mustang Phenom 100
Cabin Height 54 in 59 in Cabin Width 55 in 61 in
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Standard interior configuration for both aircraft offers seating
for four passengers.
9' 0"(2.74 m)
11' 0"(3.35 m)
2' 0"(.61 m) ToiletStorage
WardrobeCloset
Tailcone
Baggage
NoseBaggage
Nose Baggage
Toilet
Tailcone
Baggage
5' 0"(1.52 m)
6' 10"(2.08 m)
2' 11"(.89 m)
14' 9"(4.49 m)
1. Measured softgoods to softgoods with a typical interior installed.
Citation Mustang Phenom 100
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.
Average Distance Between Seats Citation Mustang Phenom 100
Second row arm 299.10 in 214.68 in First row arm 252.89 in 176.97 in
Distance Between 46.21 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.
Citation Mustang Phenom 100
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ECONOMICS
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Operating Costs
Citation Mustang Phenom 100 Fuel ($ 4.10 per gallon) 2 $ 369.00 $ 430.50 Fuel Additives -- -- Maintenance Labor ($ 99.00 per hour) 3 $ 59.40 $ 62.37 Parts – Airframe/Engine/Avionics 3 $ 50.00 $ 43.98 Engine Restoration 4 $ 125.00 $ 120.13 Thrust Reverser Overhaul 5 -- -- APU Overhaul / Propeller Overhaul 6 -- -- Total Variable Cost per Hour $ 603.40 $ 656.98 Average Speed (kt) 2 310 313 Cost per Nautical Mile $ 1.95 $ 2.10
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According to a third party, the Citation Mustang is less
expensive to operate than the
Phenom 100.
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.
Operating Cost Comparison 1Estimated Variable Cost per Hour
SYSTEMS OVERVIEW
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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.
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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.
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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.
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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.
• Options: Chart View (Jeppesen charts), Honeywell
Traffic Advisory System, and Sirius XM radio.
The Citation Mustang's Garmin G1000 avionics offer
tremendous functionality while keeping pilot workload low.
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CUSTOMER SUPPORT
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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.
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Professional Pilot Product Support Survey-Jets 1
Overall Average Score on a Scale of 1 (Poor) to 10 (Excellent)
5
6
7
8
9
10
1998 1999 2000 2001 2002 2003 2004 2005 2006 2007 2008
Survey Year
Ove
rall
Ave
rage
Sco
re
Cessna
Top ScoreCessna's commitment to customer satisfaction and long-
term relationships is evident in its customer
ratings.
1. Professional Pilot magazine, August, 2008.
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 on-site 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.
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Cessna developed an extensive service organization to assure maximum control and utilization of your investment.
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.
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Cessna's company-owned facilities work only on Citation aircraft, allowing for greater specialization.
Sacramento
Newburgh
Wichita
Phoenix
Orlando
Milwaukee
San Antonio
Greensboro
Toluca
Lincoln
TorontoPortland
Dallas
E. Alton
Grand Junction
Cessna-Owned Service Centers
Authorized Service Centers
Battle Creek
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.
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All of Cessna's company-owned facilities are ISO 9002 certified and are open 7 days / 364 days per year.
Cessna-Owned Service Centers
Authorized Service Centers
(2010)
Warranty
The Cessna Citation warranty is one of the most comprehensive in the industry.
Warranty Coverage Citation Mustang Phenom 100
Major Airframe 3 Years / 1,000 Hours
3 Years / 1,500 Hours
Manufacturer's Components 3 Years / 1,000 Hours
3 Years / 1,500 Hours
Vendor Components 1 Year 3 Years / 1,000 Hours
Standard Avionics 2 Years (Garmin) 3 Years / 1,000 Hours
Engines 3 Years / 1,000 Hours
3 Years / 1,000 Hours
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Cessna covers 100% of the parts, labor and freight (both to and from the
factory) for the entire warranty period.
Cessna administers all warranty issues – there is
no need to deal with multiple vendors.
SPECIFICATIONS
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Specifications
Citation Mustang Phenom 100 External Dimensions Length 40 ft 7 in 42 ft 1 in Height 13 ft 5 in 14 ft 3 in Wing Span 43 ft 2 in 40 ft 4 in Cabin Specifics 1 Length - Overall 14 ft 9 in N/A - Passenger Cabin 9 ft 9 in 11 ft 0 in - Seating Area 6 ft 10 in 9 ft 0 in Height 54 in 59 in Width 55 in 61 in Passenger Seating (standard - maximum) 5 - 5 5 - 5 Baggage Capacity - Internal 6 cuft / 98 lb 11 cuft / 99 lb - External 57 cuft / 620 lb 60 cuft / 419 lb Engines Manufacturer Pratt & Whitney Pratt & Whitney Model (2) PW615F (2) PW617F Output 1,460 lb 1,695 lb
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1. All internal dimensions are with a typical interior installed.
Specifications
Citation Mustang Phenom 100 Performance Maximum Cruise Speed 340 kt 394 kt NBAA IFR Range - 4 Passengers (alternate distance, cruise power setting)
999 nm (100 nm, HSC, single pilot)
969 nm (100 nm, HSC, single pilot)
Takeoff Distance - MTOW, S.L., ISA 3,110 ft 3,493 ft Landing Distance - MLW, S.L., ISA 2,380 ft 2,699 ft Certified Ceiling 41,000 ft 41,000 ft Weights Maximum Ramp Weight 8,730 lb 10,516 lb Maximum Takeoff Weight 8,645 lb 10,472 lb Maximum Landing Weight 8,000 lb 9,766 lb Maximum Zero Fuel Weight 6,750 lb 8,444 lb Maximum Fuel Capacity 2,580 lb 2,806 lb Basic Operating Weight - includes pilots 1 5,550 lb
(single pilot) 7,200 lb
(single pilot) Useful Load 2 3,180 lb 3,316 lb Maximum Payload 1,200 lb 1,244 lb Full-Fuel Payload 3 600 lb 510 lb
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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.
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