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Of 1600-1800 psi)
Hydraulic Fluid (Resevoir) 65 Gallons
Engines
Type JT15D-4 Turbofan
Manufacturer Pratt & Whitney Aircraft of Canada, Ltd.
Dry Weight 557 Lbs.
Thrust (TO, Standard Day at Sea Level) 2500 Lbs.
Bypass Ratio 2.5:1
OPERATING LIMITATIONS
Thrust
Setting
Time Limit
(Minutes)
% Fan
RPM (N1)
ITT
º C
% Turbine
RPM (N2)
Oil Temp
º C
Oil Pressure
PSI
Takeoff 5 104 700 96 10 to 121 70 to 85
Maximum
Continuous
Continuous 104 680 96 0 to 121 70 to 85
Maximum
Cruise
Continuous 104 670 96 0 to 121 70 to 85
Idle Continuous -- 580 49
*
Minus 40
To 121
35
Minimum
Starting -- -- 700º for
2 seconds
-- Minus 40
Minimum
--
Acceleration -- 104 700 96 0 to 121 --
* Idle turbine RPM is 49% +/-0.5% with ignition on. A minimum decrease
of 0.5% will be noted with ignition off.
Eaglesoft Development Group: Citation II SP/2 C551 Operating Manual
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OPERATING LIMITATIONS
Duration % Fan RPM (N1) % Turbine RPM (N2) Action Required
Transient
104-110 Logbook Entry
96-98 None
Exceeds 110 Exceeds 98 Refer to
Maintenance Manual
Steady State Exceeds 104 Exceeds 96
Overspeed Conditions
ITT
Inter-Turbine Temperature indications in excess of 700ºC or in excess of 680ºC for more than 5 minutes
require reference to the Maintenance Manual.
Maneuver Load Factor
G Limit
Flaps Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . -1.52 to +3.8
Flaps Extended . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0 to +2.0
Weight Model 550 Model 551
Max Ramp Weight 13,500 lbs. 12,700 lbs.
Max Takeoff Weight 13,300 lbs. 12,500 lbs.
Max Landing Weight 12,700 lbs. 12,000 lbs.
Max Zero Fuel Weight (Standard) 9,500 lbs. 9,500 lbs.
Max Zero Fuel Weight (Optional) 11,000 lbs. 11,000 lbs.
Maximum takeoff and landing weights may be additionally restricted due to altitude, temperature and field
length.
Center of Gravity
Forward limit:
At 8,540 lbs or less - 18.0% MAC (276.1” aft of reference datum)
At 13,300 lbs - 22.6% MAC (279.8” aft of reference datum)
At 12,500 lbs - 21.8% MAC (279.9” aft of reference datum)
(Note: Straight line variation between 18.0 and 22.6% MAC)
Altitude
Maximum Operating Altitude: 43,000’
Eaglesoft Development Group: Citation II SP/2 C551 Operating Manual
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OPERATING LIMITATIONS
Airspeed
Max Operating Speed (Vmo/Mmo)
Above 28,000’ .705 Mach
Between 14,000 and 28,000’ 277 KIAS
(with 11,000 lbs ZFW, 14,000’ to 30,500’) 262 KIAS
Below 14,000’ 262 KIAS
Maneuvering Speed (Va) Refer to Section II of the FAA Approved Airplane Flight Manual
Flaps - 15º (Takeoff and Approach) 202 KIAS
Flaps - 40º (Landing) 176 KIAS
Landing Gear Operating Speed (Vlo) 176 KIAS
Landing Gear Extended Speed (Vle) 176 KIAS
Speed Brake Operation Speed (Vsb) Vmo/Mmo
Minimum Control Speed - Airborne (Vmca) 77 KIAS
Minimum Control Speed - Ground (Vmcg) 62 KIAS
Maximum Tire Ground Speed 165 KIAS
Takeoff and Landing
Maximum Altitude 14,000’
Crosswind Component 23 knots (Demonstrated, not limiting)
Maximum Runway Water/Slush Accumulation 0.4”
Maximum Ambient Temperature at Sea Level 50ºC (51ºC with Thrust Reversers)
Minimum Ambient Temperature at Sea Level -54ºC
Autopilot and Yaw Damper must be OFF
Vertical navigation system must be OFF below 500’ AGL
Starting
With External Power (Starter Limit) Three starts in 30 minutes with 30 seconds between cycles
With Battery Power (Battery Limit) Three battery starts per hour. If exceeded, deep-cycling and
inspection required
Starting ITT of over 500ºC is NOT NORMAL
Minimum starting oil temperature is -40ºC
Eaglesoft Development Group: Citation II SP/2 C551 Operating Manual
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OPERATING LIMITATIONS
Pressurization Differential
Normal (Both Valves) 0 to 8.8 psi
Cabin
Seats: For takeoff and landing, all seats must be upright and outboard. The seat adjacent to the emergency
exit must be fully tracked toward the rear of the airplane, and facing forward.
Fan: To meet smoke detection criteria, the cabin fan must be operating any time the aft cabin privacy curtain
is closed. If the fan is inoperable, the curtain must remain open unless the toilet is in use.
Authorized Operations
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Citation II SP/2 C551 Operating Manual(8)
