Challenger 605
Years Manufactured: 2006-2015. Aircraft in Fleet: 284. _____________________________________________________________________________
The Challenger series is arguably the most successful heavy class
business jet due to it having the largest cabin size,
excellant dispatch reliability, and low operating costs. The
Challenger 605 is the fifth generation in the Challenger series and
the succesor to the Challenger 604 model. 290 aircraft were
manufacturered in years 2006-2015, 284 of which comprise the fleet
currently in service.
The Challenger 605 includes more standard features, upgrades the avionics with the Proline 21 suite,
and
redesigns the cabin, galley, windows and tail cone.
executive floorplan 1
Nine passenger configuration with extended passenger compartment, four club chairs forward and a three place divan opposite two club chairs aft.
executive floorplan 2
Eleven or Twelve passenger configuration with extended passenger compartment, four club chairs forward and a standard three place divan or optional four place divan opposite a four place conference group aft.
executive floorplan 3
Nine passenger configuration with four club chairs forward and a three place divan opposite two club chairs aft. The extended lavatory doubles as a full-szie changing room.
GENERAL
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CAPACITY
Crew - 2 + 1
Passengers - up to 12
ENGINES
General Electric CF34-3B turbofans
Thrust: 8,729 lb (38.84 kN)
Thrust with APR: 9,220 lb (41.0 kN)
CABIN DIMENSIONS
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Cabin length: 28.42 ft (8.66 m)
Cabin width: 8.17 ft (2.49 m)
Cabin height: 6.08 ft (1.85 m)
PERFORMANCE
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RANGE
Max range at M 0.74: 4,045 NM
Max range at M 0.80: 3,732 NM
(NBAA IFR Reserves, ISA, with 5 pax/2 crew and maximum fuel)
SPEED
High-speed: M 0.82 (470
Cruise Speed: M 0.80 (459
Long-range:
speed 0.74 425 489 787
AIRFIELD PERFORMANCE
Takeoff distance (SL, ISA, MTOW):
5,840 ft (1,780 m)
Landing distance (SL, ISA, MLW):
2,777 ft (846 m)
OPERATING ALTITUDE
Maximum operating altitude:
41,000 ft (12,497 m)
Climb to Cruise Altitude of
37,000 ft (11,278 m): 22 minutes
WEIGHTS
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A.) Max Ramp Weight:
48,300 lb
(21,909 kg)
B.) Max Takeoff Weight:
48,200 lb
(21,863 kg)
C.) Max Landing Weight:
38,000 lb
(17,237 kg)
D.) Max Zero Fuel Weight:
32,000 lb
(14,515 kg)
E.) Basic Operating Weight:
26,985 lb
(12,240 kg)
F.) Max Fuel Weight:
20,000 lb
(9,072 kg)
Payload - Max Fuel (A-E-F):
1,315 lb (596
kg)
Maximum Payload (D-E):
5,015 lb
(2,275 kg)
Fuel with Maximum Payload:
16,300 lb
(7,394 kg)
Contact Us for a FREE Market Report.
Email:
sales@aviaamericas.com
Phone: +1 754.204.4444
