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Cessna Aircrafts
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Specifications, Description
& Performance
The
transcontinental Large Cabin
Cessna Citation Columbus is a
swept-wing aircraft with
retractable tricycle landing
gear and a “T” style tail. A
flat floor, stand-up pressurized
cabin accommodates a crew of two
plus eight passengers. Two Pratt
& Whitney Canada (P&WC) PW810
FADEC controlled turbofan
engines are pylonmounted on the
rear fuselage. Fuel stored in
the wings and a forward fairing
tank offers generous range for
missions typical of this class
aircraft. Space for baggage is
provided in the pressurized
walk-in aft baggage compartment.
Multiple structural load paths
and system redundancies have
been built into the aluminum
airframe. Metal bonding
techniques have been used in
many areas for added strength
and reduced weight. Certain
parts with non-critical loads
such as the nose radome and
fairings are made of composite
materials for formability. The
airframe design incorporates
anti-corrosion applications and
lightning protection.
Cessna provides a third-party
training package for pilots and
mechanics as well as a
comprehensive warranty as
described in this book. Cessna's
worldwide network of authorized
service centers offers a
complete source forall servicing
needs.
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| Dimensions |
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Overall Height |
24
ft 7 in |
7.49
m |
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Overall Length |
77 ft |
23.4 m |
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Overall Width |
80 ft |
24.3 m |
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Wing |
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Span (overall) |
80 ft |
24.3 m |
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Area |
709.3 ft2 |
65.90 m2 |
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Sweepback (at 25% chord) |
29.9o |
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Horizontal Tail |
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Span (overall) |
26 ft 4 in |
8.04 m |
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Area |
132.9 ft2 |
12.35 m2 |
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Sweepback (at 25% chord) |
35o |
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Vertical Tail |
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Span (overall) |
13 ft |
3.96 m |
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Area |
140.6 ft2 |
13.06 m2 |
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Sweepback (at 25% chord) |
40o |
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Cabin |
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Height (maximum over aisle) |
6.1 ft |
1.86 m |
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Width (max) |
6.8 ft |
21 m |
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Length (excluding cockpit) |
36.3 ft |
11.1 m |
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Landing Gear |
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Tread (main to main) |
11 ft 3 in |
41.27 m |
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Wheelbase (nose to main) |
32 ft |
9.75 m |
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| Landing
Performance |
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Takeoff Runway
Length
(Maximum Takeoff Weight, Sea Level,
ISA) |
5,400 ft |
1,646 m |
Climb Performance
Maximum Takeoff Weight, Sea Level,
ISA) |
.27 min to 41,000 ft |
12,497 m |
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Maximum Altitude |
45,000 ft |
13,716 m |
Maximum Cruise Speed (±3%)
(Mid-Cruise Weight, 35,000 ft,
(10,668 m) ISA) |
488 KTAS |
904 km/hr or 562 mph |
NBAA IFR Range (200 nm alternate) (±
4%)
(Max Takeoff Weight, Full Fuel, Full
Fuel Payload, 0.80 Mach) |
4,000 nm |
7,408 km, 4,603 mi) |
Landing Runway Length
(Maximum Landing Weight, Sea Level,
ISA) |
3,500 ft |
1067 m |
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Certificated Noise
Levels |
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Takeoff |
TBD EPNdB |
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Sideline |
TBD EPNdB |
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Approach |
TBD EPNdB |
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| Structural
Design Criteria |
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Limit
Speeds |
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VMO at
Sea Level to 8,000 ft (2,438 m) |
275
KCAS |
509
km/hr, 316 mph |
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VMO at
8,000 ft (2,438 m) to 30,590 ft (9,324
m) |
325
KCAS |
602
km/hr, 374 mph |
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MMO
above 30,590 ft (9,324 m) |
M 0.86
(True) |
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Flap Extension Speeds |
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VFE at
Takeoff and Approach (20° Flaps) |
TBD |
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VFE at
Landing (Full Flaps) |
TBD |
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Landing Gear
Operating and Extended Speed |
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VLO
(Retracting) |
TBD |
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VLE
(Extending) |
TBD |
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