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CE525 CJ1
CE525A CJ2
CE550 II
CE550B Bravo
CE560 V
CE560 V Ultra
CE560 V Encore
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KA200/B200
KA300
KA350
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LR31/31A
LR35/36
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CE525 CJ1
CE525A CJ2
CE550 II
CE550B Bravo
CE560 V
CE560 V Ultra
CE560 V Encore
King Air --------------------------
KA200/B200
KA300
KA350
Learjet ---------------------------
LR31/31A
LR35/36
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Citation V Encore (CE560)
Citation V Encore CBT
Start your Citation V Encore pilot training online with our CBT. Featuring system simulators and detailed briefings. Request a free trial!
CBT Topics
1. Aircraft General
2. Master Warning
3. Electrial
4. Fuel
5. Powerplant
2. Master Warning
3. Electrial
4. Fuel
5. Powerplant
6. Fire Protection
7. Pneumatics
8. Ice & Rain Protection
9. Air Conditioning
10. Pressurization
7. Pneumatics
8. Ice & Rain Protection
9. Air Conditioning
10. Pressurization
11. Hydraulic Power
12. Landing Gear
13. Flight Controls
14. Avionics
15. Oxygen
12. Landing Gear
13. Flight Controls
14. Avionics
15. Oxygen
System Highlights
1. Aircraft General: Systems are designed for simplicity and easy access for maintenance.
2. Master Warning: Indicates malfunctions, unsafe operating conditions and normal system operation.
3. Electrical: Two engine-driven generators rated at 30 VDC and 300 amps regulated to 28.5 V.
4. Fuel: Usable each wing 403 gallons. Combined usable 5,440 lb.
5. Powerplant: Two Pratt & Whitney PW535A engines, each producing 3,400 lb of thrust at sea level.
6. Fire Protection: Engine fire/overheat detection and fire extinguishing systems.
7. Pneumatics: Distributes bleed air extracted from each engine compressor section.
8. Ice & Rain Protection: Bleed air anti-icing and pneumatic deicing systems.
9. Air Conditioning: An Air Cycle Machine provides conditioned air for the cabin and cockpit.
10. Pressurization: 8.9 psid (7,800-foot cabin altitude when cruising at 45,000 ft).
11. Hydraulic Power: 1,500 psi system for flaps, landing gear, speedbrakes and thrust reversers.
12. Landing Gear: Electrically controlled and hydraulically actuated. Anti-skid braking.
13. Flight Controls: Primary control surfaces manually operated through cables and bellcranks.
14. Avionics: Primus 1000 Integrated Avionics System.
15. Oxygen: Supplemental oxygen available to the flight crew at all times and to the passengers.
2. Master Warning: Indicates malfunctions, unsafe operating conditions and normal system operation.
3. Electrical: Two engine-driven generators rated at 30 VDC and 300 amps regulated to 28.5 V.
4. Fuel: Usable each wing 403 gallons. Combined usable 5,440 lb.
5. Powerplant: Two Pratt & Whitney PW535A engines, each producing 3,400 lb of thrust at sea level.
6. Fire Protection: Engine fire/overheat detection and fire extinguishing systems.
7. Pneumatics: Distributes bleed air extracted from each engine compressor section.
8. Ice & Rain Protection: Bleed air anti-icing and pneumatic deicing systems.
9. Air Conditioning: An Air Cycle Machine provides conditioned air for the cabin and cockpit.
10. Pressurization: 8.9 psid (7,800-foot cabin altitude when cruising at 45,000 ft).
11. Hydraulic Power: 1,500 psi system for flaps, landing gear, speedbrakes and thrust reversers.
12. Landing Gear: Electrically controlled and hydraulically actuated. Anti-skid braking.
13. Flight Controls: Primary control surfaces manually operated through cables and bellcranks.
14. Avionics: Primus 1000 Integrated Avionics System.
15. Oxygen: Supplemental oxygen available to the flight crew at all times and to the passengers.
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