曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

Maximum Cruise Speed (± 3%) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 340 KTAS (630 km/hr or 391 mph)
(Mid-Cruise Weight, 35,000 ft (11,668 m), ISA)
NBAA IFR Range (100 nm alternate) (± 4%) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,150 nm (2,130 km or 1,323 mi)
(Maximum Takeoff Weight, Full Fuel, Optimal Climb
and Descent, Maximum Cruise Thrust at 41,000 feet)
Landing Runway Length . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2,390 ft (728 m)
(Maximum Landing Weight, Sea Level,
ISA, per Part 23 Commuter Category)
Certificated Noise Levels
Takeoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 73.9 EPNdB
Sideline . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85.0 EPNdB
Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 86.0 EPNdB
* Takeoff distance criteria under Part 23 Commuter Category accounts for the greater of accelerate-stop, accelerate-go, or 115% of
the all-engine takeoff distance.
2. PERFORMANCE
1.3 Design Weights and Capacities
Maximum Ramp Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8,730 lb (3,960 kg)
Maximum Takeoff Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8,645 lb (3,921 kg)
Maximum Landing Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8,000 lb (3,629 kg)
Maximum Zero Fuel Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6,750 lb (3,062 kg)
Standard Empty Weight * . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5,350 lb (2,427 kg)
Useful Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3,380 lb (1,533 kg)
Fuel Capacity (useable) at 6.70 lb/gal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2,580 lb (1,170 kg)
* Standard empty weight includes unusable fuel, full oil, standard interior, and standard avionics.
1. GENERAL DESCRIPTION (Continued)
September 2006
7
4. FUSELAGE
3 . S T RUCTURAL DESIGN CRITERIA
The Citation Mustang airframe is conventional in
design, incorporating aluminum alloys, steel and other
materials as appropriate. Engineering principles using
multiple load paths, low stress levels and small panel
size are incorporated in the primary structure. The
structure supports a nominal maximum cabin pressure
differential of 8.3 psi (.57 bar).
The fuselage has a slightly out of round cross section at
the floor level to increase foot room. There are no fuselage
penetrations for the wing structure. A dropped aisle
runs the length of the cabin. The keyed cabin door is
located on the forward left-hand side of the fuselage. It
has eight locking pins (four on each side), a passive blade
type pressure seal, and is hinged forward with a folding
two-step entry stair mounted just inside the entrance. The
door is monitored to ensure it is latched and locked. A
plug-type emergency exit is located on the right-hand side
of the cabin in-between the fore and aft seats. The windshields
are designed to meet bird resistance requirements
of 14 CFR Part 23, Commuter category. Framing assemblies
surround the main door opening, emergency exit,
and windshields to provide structural continuity.
The nose section includes a generous baggage compartment
from which the oxygen tank, hydraulic power
pack, hydraulic accumulator, the emergency gear and
brake bottles, and some avionics are accessible. Behind
the composite radome is the high-resolution weather
radar antenna and processor.
The tailcone houses the major components of the environmental,
electrical distribution, and engine fire extinguishing
systems. A baggage compartment is also located
in the tailcone with room for skis. External access to
both the equipment and the baggage area is provided
through a baggage door on the lower left-hand side of
the tailcone.
5. WING
The Mustang's wing incorporates a new high-lift airfoil
designed for low stall speeds while at the same time producing
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Specification & Description(4)