learjet 45xr vs. citation xls+

Transcription

learjet 45xr vs. citation xls+
2013
VS. PHENOM 300
LEARJET HAS VISION
LEARJET EXECUTIVE SUMMARY
Bombardier is in a stronger
financial situation than Cessna:
Learjet 70: Spacious seating for 6
provides enhanced comfort
Faster and burns comparable fuel to the
much smaller Phenom 300
Despite flying faster, the Learjet 70 has
a longer range than the P300
Save over $100,000 in operating costs
alone in 5 years
Part 25 certification ensures the
following:
Learjet 70
Phenom 300
Jam proof
flight controls
Not jam proof
Bird-strike
tested
Not tested
Stringent
icing tests
Less stringent
icing
requirements
BOMBARDIER CAPTURED MORE ORDERS
THAN THE REST OF THE INDUSTRY COMBINED
2012 Industry Net Orders
+329
343
70
62
58
14
Fiscal year 2012
Note: Excludes very light jets, ACJs, BBJs and Embraer Lineage 1000
Source: Manufacturer disclosures and Bombardier estimates
-10
TRUSTED LEARJET NAME
Gov’t Montenegro
Gov’t Pakistan
COCKPIT
BOMBARDIER VISION FLIGHT DECK ON A LEARJET AIRCRAFT
• Bombardier signature Vision* Flight Deck
• Brand new Garmin G5000 state-of-the-art avionics suite
*
Trademark(s) of Bombardier Inc. or its subsidiaries.
SYNTHETIC VISION
The LEARJET 70 features a standard synthetic vision system.
Provides the pilots with VFR-like visibility even in IFR conditions
NEW GRAPHICAL FLIGHT PLANNING FEATURES CONTROLLED
BY A UNIQUE TOUCH SCREEN
• Graphical flight planning

Reduced Pilot Workload
• Unique glass touch screen controller

Infrared grid technology
GARMIN WINS TOP HONORS ON AVIONICS PRODUCT SUPPORT
• In the cockpit avionics sector,
Garmin takes top honors for how it
looks after its customers.
• Garmin 1st for 8 years.
THE MOST COMFORTABLE
CABIN IN ITS CLASS
LEARJET 70 INTERIOR FEATURES
• Spacious, individual seating for 6 passengers
o
Can seat 7 with the standard belted lavatory
• Flat floor throughout the entire cabin provides
enhanced comfort
FLOOR PLAN
• 1 extra belted
lavatory seat
• Extended lavatory
with standard sink
and belted seat
PHENOM 300
• No sink available
• Optional lavatory sink
The LEARJET 70 provides comfortable seating for 6 passengers
*Finished cabin dimensions measured from actual drawings of cross sections
CROSS-SECTION
PHENOM 300
4’10”
(1.47m)
3’2” (0.96m)
5’ (1.52m)
The LEARJET 70 provides 3” more cabin height,
more head and shoulder space, and a flat floor
*Finished cabin dimensions measured from actual drawings of cross sections
OBSERVATIONS ON THE PHENOM 300
• The dropped aisle is steep and narrow
o Movement is more difficult around the cabin, especially in the vicinity of
the lavatory
The PHENOM 300 stepped aisle provides uncomfortable seating
and increases the risk of tripping
*Finished cabin dimensions measured from actual drawings of cross sections
THE FASTEST AIRCRAFT IS
ALSO THE MOST EFFICIENT
LEARJET 70: THE FAST AND THE EFFICIENT
+12%
458 kts
Better
Speed
430 kts
Learjet’s long range
cruise is the
competitor’s high
speed cruise
424 kts
385 kts
Long range cruise
High speed cruise
Better
Fuel
Phenom 300
3,886 lbs
-5%
Block fuel
4 pax
1,500 nm still air
similar speed (436 kts)
3,674 lbs
Learjet’s fuel burn
advantageously
compares to the much
smaller Phenom 300
Phenom 300
While the LEARJET 70 is the fastest aircraft in its class,
it is also the one with the best fuel economy
*Speeds based on mid-cruise weight (BOW + 4 pax+ ½ full fuel). Mission based on 4 pax, zero wind, 436 kts for both aircraft and NBAA IFR 100 nm fuel reserves
SAVE TIME
Flight time (1,900 nm)
LEARJET 70
4:38
PHENOM 300
5:02
SAVE OVER 20 MINUTES
ON THE
On a typical trans-European flight,
the LEARJET 70 saves 30 minutes over the PHENOM 300
Assumptions
4 passengers, 2 crew (200lbs each)
3% airways allowance
ISA conditions en route
NBAA IFR (100 NM) fuel reserves
Standard Configuration BOW
MORE RANGE, FASTER SPEED
Phenom 300
Assumptions
3% airway allowance
6 passengers (at 200 lbs), 2 crew
85% Boeing annual winds
ISA conditions en route
L70: 432 kts cruise speed
P300: 417 kts cruise speed
NBAA IFR (100 NM) fuel reserves
Optimum climb, cruise and descent
Level hard surface, dry paved runway
Specific departure requirements not considered
MORE RANGE, FASTER SPEED
Phenom 300
Assumptions
3% airway allowance
6 passengers (at 200 lbs), 2 crew
85% Boeing annual winds
ISA conditions en route
L70: 432 kts cruise speed
P300: 417 kts cruise speed
NBAA IFR (100 NM) fuel reserves
Optimum climb, cruise and descent
Level hard surface, dry paved runway
Specific departure requirements not considered
MORE RANGE, FASTER SPEED
Phenom 300
Assumptions
3% airway allowance
6 passengers (at 200 lbs), 2 crew
85% Boeing annual winds
ISA conditions en route
L70: 432 kts cruise speed
P300: 417 kts cruise speed
NBAA IFR (100 NM) fuel reserves
Optimum climb, cruise and descent
Level hard surface, dry paved runway
Specific departure requirements not considered
MORE RANGE, FASTER SPEED
Phenom 300
Assumptions
3% airway allowance
6 passengers (at 200 lbs), 2 crew
85% Boeing annual winds
ISA conditions en route
L70: 432 kts cruise speed
P300: 417 kts cruise speed
NBAA IFR (100 NM) fuel reserves
Optimum climb, cruise and descent
Level hard surface, dry paved runway
Specific departure requirements not considered
THE MORE RANGE, FASTER SPEED
Phenom 300
Assumptions
3% airway allowance
6 passengers (at 200 lbs), 2 crew
85% Boeing annual winds
ISA conditions en route
L70: 432 kts cruise speed
P300: 417 kts cruise speed
NBAA IFR (100 NM) fuel reserves
Optimum climb, cruise and descent
Level hard surface, dry paved runway
Specific departure requirements not considered
LARGER AIRCRAFT FOR SIMILAR FUEL
AND MAINTENANCE COSTS
-3%
$1,599
$1,641
$288
Engines
$346
Airframe
$170
$352
Cost Assumptions (5 Year Average):
• Fuel flow (takeoff to touchdown)
based on 600 nm mission, standard
configuration, similar cruise speeds and
NBAA IFR (100 nm) R fuel reserves.
• Learjet 70 parts based on Smart Parts and
labor based on scheduled inspections.
• Phenom 300 parts and labor based on
Embraer
EEC
Enhanced
program,
estimated in USD. Engines costs based on
manufacturer program.
Fuel
$1,083
$1,001
• Actual costs may vary. All costs in USD.
Phenom 300
Save over $ 100, 000 in operating costs alone over 5 years
LEARJET 70: SUPERIOR BRAKES
Heavier landing weight…
…Similar landing distances
+2,335 lbs.
-1%
19,200 lbs.
2,660 ft.
2,681 ft.
16,865 lbs.
Phenom 300
Phenom 300
The superior carbon brakes of the Learjet 70 combined with brake-by-wire
technology enable it to land in a similar distance to the Phenom 300
LEARJET 70: HIGHER CERTIFICATION STANDARDS
• Trailing link design
o Smoother taxiing and landings
• Independent Anti-Skid Systems on each
wheel
• Dual Tires & Wheels
o Redundancy
o Dual Carbon Brakes
o Designed to stop a 36,000 lb. aircraft
o “Brake-by-wire” technology
Aircraft fitted with dual wheel assembly
LEARJET 70

Phenom 300

CJ3

CJ4

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THE
TECHNOLOGY
BEHIND A
TITLE25
STYLE
PART
AIRCRAFT
THE LEARJET 70 ADHERES TO STRINGENT
CERTIFICATION STANDARDS
First business jet certified to both FAA and JAA standards
• Certified to FAA, 14CFR Part 25, amendment 1 to 77
o
HIGHER THAN AIRBUS 330/340
• Certified to JAA, JAR 25 change 13
o SAME AS BOEING 777
Examples of the demanding standard the Learjet 70 aircraft meets:
• 16G seat certification
o improves seat attachment and restraint system loading
• Higher bird strike tolerances
o demand the ability to continue safe flight following impact events
• Flight control redundancy
o ensures control of the aircraft in the event of system failure or jamming
• Degradation applied in takeoff performance
o more accurately depicts rejected takeoff performance
• More stringent ice testing requirements
The LEARJET 70 certification levels testify to the technological benchmark
the aircraft represents and the safety and reliability its operators can expect
THE LEARJET 70 ADHERES TO STRINGENT
CERTIFICATION STANDARDS
Redundancy in systems:
dual primary flight controls
Bird strike standards
for a 8 lb. bird
on the empennage
leading edges
Degradation applied in takeoff
and landing performance
in accordance with FAR 25
Amendment 92
Bird strike standards for a 4 lb. bird
on the windshield and wing leading edges
16 G dynamic
seat certification
Stringent ice testing
The LEARJET 70 certification levels testify to the technological benchmark
the aircraft represents and the safety and reliability its operators can expect
CERTIFICATION BASIS
“This AC uses terminology similar to AC 25.1309-1A. However, the specific means of
compliance for § 25.1309 of part 25 are defined differently due to the higher level of safety
required for transport category airplanes.” 1
• Per the FAA’s own documentation, a Part 25 or TRANSPORT CATEGORY
AIRPLANES require a higher level of safety:
Part 23
Part 25
NORMAL, UTILITY, ACROBATIC, AND
COMMUTER CATEGORY AIRPLANES
TRANSPORT CATEGORY AIRPLANES
• Phenom 100/300
• CJ1 to CJ4
• Premier 1A
• Learjet 70/75
• All other business jets
1. AC 23.1309-1D System safety analysis and assessment for Part 23 airplanes
EXAMPLES OF CERTIFICATION DIFFERENCES
BETWEEN PART 23 AND PART 25
Part 23
No bird strike requirements
Empennage structure and
aircraft systems must
withstand the impact
of an 8 lb. bird at Vc
Aircraft must be “controllable”
with icing on unprotected surfaces
1) All handling tests must
be repeated with 3 in. of icing
on unprotected surfaces
2) Aircraft must demonstrate it can
fly with an additional 1.5 in. of icing
on all normally protected surfaces
1) One (1) second recognition time
2) New tires
3) New brakes
1) Three (3) seconds recognition time
2) 50% worn tires
3) 90% worn brakes
Bird Strike
Icing
Takeoff
Part 25
The LEARJET 70 Part 25:
More stringent certification requirements
EXAMPLE: FLIGHT CONTROL SYSTEM REDUNDANCY
Phenom 300
Learjet 70
Part 23.671
Part 25.671
(A) Each control must operate easily,
smoothly, and positively enough
to allow proper performance
of its functions
(B) Controls must be arranged and
identified to provide for convenience
in operation and to prevent
the possibility of confusion and
subsequent inadvertent operation
…(C) The airplane must be shown
by analysis, tests, or both to be
capable of continued safe flight and
landing after any of the failures or
jamming in the flight control system
and surfaces…
FLIGHT CONTROL SYSTEM REDUNDANCY
Learjet 70 Part 25.671
Roll Control System
Pitch Control System
If the aileron controls become jammed,
the pilot control wheel can be disconnected
from the aileron control cables and airplanes
roll can be controlled with spoilerons alone.
The copilot control wheel remains connected
to the aileron control system
If either elevator mechanical
control circuit jams, the two circuits
can be disconnected by pulling
the disconnect Tee-handle
ELEV DISC, located at the forward
left side of the center pedestal.
The aircraft can then be controlled
with the unjammed elevator
Phenom 300 Part 23.671
No redundancy required
LEARJET EXECUTIVE SUMMARY
Bombardier is in a stronger
financial situation than Cessna:
Learjet 70: Spacious seating for 6
provides enhanced comfort
Faster and burns comparable fuel to the
much smaller Phenom 300
Despite flying faster, the Learjet 70 has
a longer range than the P300
Save over $100,000 in operating costs
alone in 5 years
Part 25 certification ensures the
following:
Learjet 70
Phenom 300
Jam proof
flight controls
Not jam proof
Bird-strike
tested
Not tested
Stringent
icing tests
Less stringent
icing
requirements
Document produced by the Sales Engineering Group, Business Aircraft. All data in the document is based on available or published information and is for discussion purposes only. By this document, Bombardier Inc.
does not intend to make, and is not making, any offer, commitment, representation or warranty of any kind whatsoever. All data are subject to change without prior notice. The final configuration and performance
of the aircraft shall be the specifications that are contractually agreed to.