Pacific Jetcorp Ltd.
 
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Specifications, Description & Performance

The Cessna Citation CJ2+ is an all-metal, pressurized, low-wing monoplane with provisions for up to eight passengers plus a crew of two. Suitable allowance for luggage and optional equipment is also provided.

Two Williams International Co., LLC (Williams) FJ44-3A-24 turbofan engines are pylon-mounted on the rear fuselage.

The model 525A is certified to the requirements of U.S. FAA Federal Aviation Regulation Part 23 including day, night, VFR, IFR, single pilot, and flight-into-known icing conditions.

Takeoff Performance
 (15° Flaps) Required Field Length per FAR 25 
  TAKEOFF DISTANCE (ft)
WEIGHT (lbs) SEA LEVEL 59°F 5000 ft 41°F 5000 ft 77°F
12,375
12,000
11,000
10,000
3,420
3,240
2,800
2,650
4,190
3,970
3,400
2,890
5,080
4,770
4,060
3,430
Note: Takeoff and landing field lengths are based on level, hard surface, dry runways with no wind.
 
Landing Performance
Sea Level, Standard Day     Distance From 50 ft Above the Runway 
WEIGHT (lbs) DISTANCE (ft)
11,500
11,000
10,000
9,000
8,000
2,980
2,900
2,720
2,530
2,330
 
Climb Performance
 Time (min)    TAKEOFF WEIGHT (lbs) 
Altitude (ft) 10,000 11,000 12,375
25,000
33,000
37,000
41,000
45,000
7
10
12
16
21
8
11
14
18
25
9
13
17
22
36
 
Distance (nm) TAKEOFF WEIGHT (lbs) 
Altitude (ft) 10,000 11,000 12,375
25,000
33,000
37,000
41,000
45,000
23
38
48
62
86
26
43
55
74
107
31
52
68
93
157
 
Fuel (lbs) TAKEOFF WEIGHT (lbs) 
Altitude (ft) 10,000 11,000 12,375
25,000
35,000
37,000
41,000
45,000
198
263
298
339
395
222
296
338
390
467
257
348
402
472
620
 
Cruise Performance
WEIGHT (lbs) 9,500 10,500 12,000
Altitude (ft) Speed (KTAS)/Fuel Flow (lbs/hr)
33,000
37,000
41,000
43,000
45,000
410/1,151
405/969
404/833
400/758
394/689
410/1,165
405/985
400/829
394/753
385/680
408/1,165
402/995
391/823
380/741
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* Maximum cruise thrust