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2.III.1 Type design definition
Aircraft name is a maximum 22 occupants, tri-jet, long range, large aeroplane category. It has a low, high swept airfoil, mid-height horizontal stabilizer and tricycle landing gear. Flight controls are fly-by-wire.
Three Engine manufacturer and model engines are rear mounted, two on side of fuselage and one in center position.
2.III.2 Dimensions
Length  23.38 m 
Span  26.21 m 
Height  7.93 m 
Gross wing area  70.7 m2 

2.III.3  Engines Model: Engine manufacturer and model Engine TCDS: NAA TCDS CODE and Number Note: Engine is approved for operation with thrust reverser p/n ZZZZZ Number: 3 Ratings:
-Maximum takeoff static thrust :  2 849 daN (6405 lbs) limited to 5 minutes
-Max continuous : 2 849 daN (6405 lbs) 
Engine limits: Refer to the Airplane Flight Manual and to the relevant Engine Type Certificate Data Sheet
2.III.4  Auxiliary power unit (APU) Model:   APU manufacturer and model APU limits: Refer to the Airplane Flight Manual. APU is usable for ground
operation only.
2.III.5  Fluids (Fuel/Oil/Additives): Approved Fuel, oils and additives: Refer to the Airplane Flight Manual. 
2.III.6  Fluid capacities: Fuel capacity
USABLE FUEL  Liters  kg (*)  US Gallons  lbs (*) 
Left circuit  5944  4773  1570  10522 
Right circuit  5944  4773  1570  10522 
Center circuit  6154  4942  1626  10896 
Total usable  18042  14488  4766  31940 
UNUSABLE FUEL 
Drainable  65  52  17  115 
Undrainable  41  33  11  72 
Total unusable  106  85  28  187 

* assuming a fuel density of 0,803 kg/liter
Engine Oil Tank Capacity*:
Liters  kg (**)  US gallons  lbs (**) 
Max oil level 
Left engine  7.87  7.67  2.08  16.90 
Right engine  7.87  7.67  2.08  16.90 
Center engine  7.87  7.67  2.08  16.90 
Total  23.61  23.01  6.24  50.70 
Min oil level 
Left engine  6.23  6.07  1.64  13.38 
Right engine  6.23  6.07  1.64  13.38 
Center engine  6.23  6.07  1.64  13.38 
Total  18.69  18.21  4.92  40.14 

(*)  Tank quantities do not include undrainable oil or residual oil in the Accessory Gearbox, oil filter bowl or air-cooled oil cooler (ACOC)
(**)  Based on specific gravity of 0.975
2.III.7  Airplane speed limits (Unless otherwise specified, speeds are indicated airspeeds )
VMO  at sea level .........................................................  350 kts 
VMO  straight line variation up to 10,000 ft...................  370 kts 
VMO  from 10,000 ft to 28,000 ft  .................................  370 kts 
MMO  from 28,000 to 51,000 ft ....................................  0,9 
VA  maneuvering speed ...........................................  218 kts 
VFE  SF1 ....................................................................  200 kts 
SF2 ....................................................................  190 kts 
 SF3 .....................................................................  180 kts 

Note.–  Above 20 000 ft., do not establish, nor maintain a configuration with the slats and the
flaps extended.
VLO Landing gear operation ...................................... 
　
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