Cessna Citation Mustang Embraer Phenom 100

Transcription

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
9
9
9
9
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
9
9
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Lower acquisition cost
More economical to operate
Consumes less fuel on every mission
Customer Support: Cessna is an industry leader in
Product Support
9
9
9
9
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
PERFORMANCE
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
2,500 feet – 15°C/59°F
Citation Mustang
505 nm
Phenom 100
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
Range vs Runway Length at Sea Level
1
1,200
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.
15°C/59°F
35°C/95°F
1,000
800
600
Citation Mustang
400
Phenom 100
200
2,000
2,500
3,000
3,500
4,000
4,500
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.
5,000
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
Time to Climb
Phenom 100 2
20 min
26 min
Unable Climb Direct
1&2
41,000
Altitude (feet)
37,000
33,000
29,000
Citation Mustang
Phenom 100
25,000
0
5
10
15
20
Time from Sea Level (minutes)
25
30
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
Phenom 100
360 - 395 kt
Difference
Typical Cruise Speeds 1
Citation Mustang
320 - 345 kt
Flight Time - 200 nm Mission 2
Flight Time - 500 nm Mission 2
Flight Time - 1,000 nm Mission 2
0:40
1:36
3:16
0:36
1:27
3:01
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.
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
1
0.70
Specific Fuel Consumption
(nautical miles per pound of fuel)
Citation Mustang
0.65
Phenom 100
0.60
0.55
0.50
0.45
0.40
300
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.
Range Capability
The Citation Mustang and Phenom 100 have very similar range and payload capability.
Range Capability 1
NBAA Range – 2 Passengers
Citation Mustang
1,175 nm
999 nm
716 nm
The Citation Mustang has
the same range capability as
the Phenom 100.
Phenom 100
1,170 nm
969 nm
705 nm
Range versus Payload 1
1,400
Citation Mustang
Payload (pounds)
1,200
Phenom 100
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.
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
Takeoff Decision Speed - V1
Citation Mustang
89 kt
Phenom 100
95 kt
Difference
6
Takeoff Rotation Speed - VR
89 kt
95 kt
6
Landing Approach Speed - VApp
101 kt
105 kt
4
Landing Reference Speed - VRef
94 kt
100 kt
6
7
Max Takeoff Weight
Max Takeoff Weight
Max Landing Weight
One of Cessna's
two prestigious
Collier Trophy
awards was for
the Citation
fleet's excellent
safety record.
Max Landing Weight
Landing Reference Speed - VRef
87 kt
94 kt
Typical Landing Weight
(6,800 lb)
(8,500 lb)
Stall Speed - Max Takeoff Wght
91 kt
100 kt
9
73 kt
77 kt
4
Flaps 0, 0 Bank
Stall Speed - Landing Configuration
Max Landing Weight, Flaps Full, 0 Bank
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 Distances
1
3,000
●="Typical" 2
Landing Distance (feet)
2,800
2,600
2,400
2,200
Citation Mustang
2,000
The Citation Mustang's
short landing distances
and slow approach
speeds enhance landing
safety, particularly when
utilizing airports with
minimal runways.
1,800
6,000
Phenom 100
7,000
8,000
9,000
10,000
Landing Weight (pounds)
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.
CABIN & BAGGAGE
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.
Cabin Layout
Citation Mustang
Phenom 100
Nose
Baggage
Nose Baggage
5' 0"
(1.52 m)
Wardrobe
Closet
2' 11"
(.89 m)
14' 9"
Internal Dimensions 1
Toilet
(4.49 m)
9' 0"
(2.74 m)
Cabin Height
Cabin Width
11' 0"
(3.35 m)
Citation Mustang
54 in
55 in
Phenom 100
59 in
61 in
6' 10"
(2.08 m)
2' 0"
(.61 m)
Storage
Tailcone
Tailcone
Baggage
Baggage
Toilet
Standard interior configuration
for both aircraft offers seating
for four passengers.
1. Measured softgoods to softgoods with a typical interior installed.
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.
ECONOMICS
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
Phenom 100
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
$ 369.00
-$ 59.40
$ 50.00
$ 125.00
---
$ 430.50
-$ 62.37
$ 43.98
$ 120.13
---
Total Variable Cost per Hour
Average Speed (kt) 2
Cost per Nautical Mile
$ 603.40
310
$ 1.95
$ 656.98
313
$ 2.10
2
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.
SYSTEMS OVERVIEW
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.
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
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.
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.
engines are fuel-efficient
and easy to operate.
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.
CUSTOMER SUPPORT
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
1
Overall Average Score on a Scale of 1 (Poor) to 10 (Excellent)
10
Cessna
Top Score
9
Overall Average 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
2004
2005
2006
2007
2008
Survey Year
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 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.
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
Milwaukee
Lincoln
Sacramento
Wichita
Phoenix
Authorized
Service Centers
E. Alton
Greensboro
Dallas
San Antonio
Cessna-Owned
Service Centers
Battle Creek
Toronto
Newburgh
Orlando
Toluca
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.
Warranty
The Cessna Citation warranty is one of the most comprehensive in the industry.
Warranty Coverage
Vendor Components
Citation Mustang
3 Years / 1,000
Hours
3 Years / 1,000
Hours
1 Year
Standard Avionics
2 Years (Garmin)
Engines
3 Years / 1,000
Hours
Major Airframe
Manufacturer's Components
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.
SPECIFICATIONS
Specifications
Citation Mustang
Phenom 100
40 ft 7 in
13 ft 5 in
43 ft 2 in
42 ft 1 in
14 ft 3 in
40 ft 4 in
Cabin Specifics 1
Length - Overall
- Passenger Cabin
- Seating Area
Height
Width
Passenger Seating (standard - maximum)
Baggage Capacity - Internal
- External
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
N/A
11 ft 0 in
9 ft 0 in
59 in
61 in
5-5
11 cuft / 99 lb
60 cuft / 419 lb
Engines
Manufacturer
Model
Output
Pratt & Whitney
(2) PW615F
1,460 lb
Pratt & Whitney
(2) PW617F
1,695 lb
External Dimensions
Length
Height
Wing Span
1. All internal dimensions are with a typical interior installed.
Specifications
Citation Mustang
Performance
Maximum Cruise Speed
NBAA IFR Range - 4 Passengers
(alternate distance, cruise power setting)
340 kt
999 nm
Phenom 100
394 kt
969 nm
(100 nm, HSC, single pilot)
(100 nm, HSC, single pilot)
Takeoff Distance - MTOW, S.L., ISA
Landing Distance - MLW, S.L., ISA
Certified Ceiling
3,110 ft
2,380 ft
41,000 ft
3,493 ft
2,699 ft
41,000 ft
Weights
Maximum Ramp Weight
Maximum Takeoff Weight
Maximum Landing Weight
Maximum Zero Fuel Weight
Maximum Fuel Capacity
Basic Operating Weight - includes pilots 1
8,730 lb
8,645 lb
8,000 lb
6,750 lb
2,580 lb
5,550 lb
10,516 lb
10,472 lb
9,766 lb
8,444 lb
2,806 lb
7,200 lb
(single pilot)
(single pilot)
3,180 lb
1,200 lb
600 lb
3,316 lb
1,244 lb
510 lb
2
Useful Load
Maximum Payload
Full-Fuel Payload 3
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.

Cessna Citation Mustang Embraer Phenom 100

Transcription

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