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19 Cards in this Set
- Front
- Back
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Citation 560XL Certification Status |
FAR Part 25 |
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Citation Excel Engines and Specification |
Pratt & Whitney PW-545A 830# Dry Weight 3,804#'s Thrust Each 4.0:1 Bypass Ratio
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Citation Excel Aircraft Dimensions
Wingspan Length Height |
55' 8" 51' 10" 17' 2"
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Citation Excel Certificated Weights
Max Ramp Max Take-Off Max Landing Max Zero Fuel
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20,200# 20,000# 18,700# 15,000# |
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Citation Excel Maximum Usable Fuel Capacity
Pounds Gallons # Fuel Probe Sensing Units Per Wing |
6,790# 1006 Gal 7 |
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Citation Excel Basic Weights (560-5139)
Basic Empty Basic Operating (2 Crew) |
12,386# 12,786# |
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Citation Excel Maximum Certified Ceiling
2 Engine 1 Engine |
45,000' 28,600' |
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Citation Excel Pressurization System Differential |
9.3 psid
*Maintains SL Cabin up to 25, 247' |
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Citation Excel DC Electric Generators
Voltage Amperage
If the Aircraft Electrical System is 28-Volt, why are the generators rated more voltage than the electrical system? |
30 Volts 300 Amp Hour
To provide a charging voltage for the battery |
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Citation Excel Auxillary Power Unit (APU)
Model# Voltage Rated Amperage Max Starting Altitude Max Operating Altitude
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Allied Signal RE 100XL 28.5 Volts 300 Amps Limited to 230 20,000' 30,000' |
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Citation Excel Type of Hydraulic Fluid |
Phosphate Ester Based Hydraulic Fluid (Skydrol or Hyjet) |
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Citation Excel
Main Wheel Tire InflationPressure Nose Wheel Tire Inflation Pressure |
210 psi +/- 5 psi (Unloaded) 130 psi =/- 5 psi (Unloaded) |
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Citation Excel
Type Wing Flap and Construction Limitations |
Fowler Laminated Graphite Composite Do Not Retract Flaps when airspeed is >200 KIAS
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Citation Excel
Horizontal Stabilizer Operation Range of Travel Method of Control Limitations |
Operated by selection of Flap > 0 degrees Crew Has No Other Control of positioning. +1 to -2 degrees dependent on flap setting +1 with Flaps Up -2 With Flaps in any position >0 Hydromechanical Jack-Screw Stab will not move when airspeed is >215 KIAS
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Citation Excel
Number of Wing Vortex Generators Function Limitations |
26 VG's Per Wing Provide for more effective aileron control. 3 VG's may be missing for flight. Altitude is limited to FL410 with missing VG's |
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Citation Excel
Number of Static Wicks Limitations |
20 Static Wicks Total 6 Wicks On Each Wing 8 Wicks On Fuselage
Wicks may only be missing on wing-tips and/or stinger. NON MISSING ON WINGS |
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Citation Excel Avionics System
Manufacturer & Model |
Honeywell Primus 1000 Integrated Avionics System |
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Citation Excel
O2 System Cylinder Size Duratration with 2 Crew and 6 Pax at FL250 |
76 Cubic Foot
63 Minutes (1 hour)
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Vmca/Vmcg |
90KIAS/81KIAS |
