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Citation --------------------------
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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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
Home
Citation CJ2 (CE525A)
Citation CJ2 CBT
Start your CJ1 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, which allows single-pilot operation.
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 29 V.
4. Fuel: Total each wing tank is 293 U.S. gallons. Combined usable fuel is 3,960 lb.
5. Powerplant: Two Williams-Rolls FJ-44-2C engines, each producing 2,400 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: Bleed air is conditioned to cool/heat the cabin and to defog windows.
10. Pressurization: 8.9 psid (8,000-foot cabin altitude when cruising at 45,000 ft), auto scheduling.
11. Hydraulic Power: 1,500 psi system for landing gear, flaps, speedbrakes and thrust attenuators.
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: Rockwell Collins Pro Line 21.
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 29 V.
4. Fuel: Total each wing tank is 293 U.S. gallons. Combined usable fuel is 3,960 lb.
5. Powerplant: Two Williams-Rolls FJ-44-2C engines, each producing 2,400 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: Bleed air is conditioned to cool/heat the cabin and to defog windows.
10. Pressurization: 8.9 psid (8,000-foot cabin altitude when cruising at 45,000 ft), auto scheduling.
11. Hydraulic Power: 1,500 psi system for landing gear, flaps, speedbrakes and thrust attenuators.
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: Rockwell Collins Pro Line 21.
15. Oxygen: Supplemental oxygen available to the flight crew at all times and to the passengers.
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