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The Citation II is approved for day and night, VFR and IFR operations. Flight into icing conditions is approved.
Aerobatic maneuvers and spins are prohibited. No intentional stalls permitted above 25,000’ or at engine
speeds between 61.0% and 65% N1.
Minimum Crew
Minimum Flight Crew for all operations:
Model 550 - 1 pilot and 1 copilot
Model 551 - 1 pilot in left seat
1 Autopilot with Approach Coupling
1 Flight Director
1 Boom Microphone
Transponder Ident Switch on Pilot’s Control Wheel
The pilot in command must have a C-500 type rating and meet the requirements of FAR 61.58 for two pilot
operation, or FAR 61.57 for single pilot operation (Model 551 only).
The copilot shall possess a multi-engine rating and meet the requirements of FAR 61.55.
Category II operation requires two pilots.
Thrust Reversing
Reverse thrust power must be reduced to the idle detent position at 60 KIAS on landing roll.
Maximum reverse thrust is limited to 94% N1 for ambient temperatures above -18ºC and 92% N1 for ambient
temperatures below -18ºC.
Maximum allowable thrust reverser deployed time is 15 minutes in any 1 hour period.
Thrust reversing on sod/dirt or gravel runways is not allowed.
Simultaneous usage of both the drag chute (if installed) and the thrust reversers is prohibited.
Pressurization Source Selector
Operation in BOTH HI mode is not approved for takeoff, landing or high power setting requirements.
Eaglesoft Development Group: Citation II SP/2 C551 Operating Manual
25
Weight and Balance
The Standard Empty Weight center of gravity for most Citation Iis is located approximately 291.0 inches aft of
the Reference Datum Line. Depending on airplane gross weight, the center of gravity of a loaded airplane can
move from 276.1 inches aft of Datum and remain within limits.
As the airplane is loaded, the center of gravity will shift. The amount of shift is dependent on not only the
weight added, but the distance the weight is from the
original center of gravity. Both of these factors can be
considered by multiplying the weight added by the distance
from the Reference Datum Line to produce the
loading moment. This information is presented in table
form in the following tables.
The contribution each load station makes to center of
gravity shift can be seen by comparing the respective
COG lengths given in the Weight and Moment Table
of the actual Citation II POH, but for sim purposes this
has been simplified considerably.
Each Station Load’s Moment Arm has been entered
into the Weight & Balance Form for your convenience.
The only data that needs to be looked up is in
the table on the right, where you will find the Moment
Arm for the actual fuel being loaded. Transfer this
number to the form when performing your calculations.
For each Station, multiply the Weight by the Moment
Arm, then divide by 100. Subtotal and Total as indicated
on the Form to obtain the final results.
Eaglesoft Development Group: Citation II SP/2 C551 Operating Manual
26
Weight and Balance Form (Sample)
Tailcone
Baggage
B T
Avionics Bay Nose Baggage
1 2
3
4
6
8
5
7
9
Pantry
Payload Computations
Item Weight Arm Moment/
100
Seat 1 170 131 223
Seat 2 131
Seat 3 170 170 289
Seat 4 200 217 434
Seat 5 217
Seat 6 253
Seat 7 253
Seat 8 288
Seat 9 288
Aft Toilet 325
Aft Closet 325
Nose Baggage 60 74 44
Tailcone Baggage 100 442 442
Pantry/Closet 120 170 204
Total Payload 820 -- 1636
Basic Empty Wt. 7100 -- 20661
Zero Fuel Wt.
Do not exceed
Max ZFW 9500 lbs.
7920 22297
Fuel Loading 3000 8555
*Ramp Weight
Do not exceed max.
Ramp wt. 12,700 lbs.
10920 30852
Less Taxi Fuel 200 571
*Takeoff Weight
Do not exceed max
TO wt. 12,500 lbs
10720 30281
Less Fuel Enroute 2000 5686
*Landing Weight
Do not exceed max.
Landing wt. 12,000 lbs.
8720 24595
* Totals must be within approved weight
and C.G. Limits. It is the responsibility of
the operator to insure that the airplane is
loaded properly. The Basic Empty
Weight C.G. is noted on the Airplane
Weight Form. If the airplane has been
altered, refer to the weight and balance
record for this information.
Eaglesoft Development Group: Citation II SP/2 C551 Operating Manual
27
Weight and Balance Form
Tailcone
Baggage
B T
Avionics Bay Nose Baggage
1 2
3
4
6
8
5
7
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Citation II SP/2 C551 Operating Manual(9)
