DORNIER 128-6 WHEELS
REFERENCE INFORMATION

Unless annotated otherwise, all speeds are given for MTOW and
FLAPS UP (FLAPS 1 in parentheses) in KIAS.

For the most important speeds in relation to current total aircraft
weight open the Speed Card by clicking on the
-icon on the main panel.

For standard procedures, see the Checklists tab.  

Total Flight Simulator aircraft weight with full fuel (MTOW)   4350 kg / 9590 lbs


NOTE: To adjust fuel load, on the Aircraft menu, click Fuel and Load.
 

VMO - Maximum Operating Speed 150
VA - Maneuvering Speed 125
VMC - Minimum Control Speed 63
VFE - Maximum Flaps Extended / Operating Speed 107
VX - Best Angle of Climb Speed 80 (75)
VY - Best Rate of Climb Speed 90
Best Glide Speed both engines inoperative (FLAPS UP) 90

VR - Rotation Speed
4350 kg / 9590 lbs   82     (75)
<3200 kg / 7055 lbs (<3780 kg / 8333 lbs)   69.3 (69.3)

V2 - Takeoff Safety Speed
4350 kg / 9590 lbs   87 (80)
2800 kg / 6173 lbs (<3280 kg / 7231 lbs)   70 (69.3)

Cruise Climb   = Best rate of climb speed
Note: Maintain max continuous power 1108 lb ft and
propeller speed 1900 rpm.
4350 kg / 9590 lbs   92
4200 kg / 9259 lbs   91
3850 kg / 8488 lbs   90
3400 kg / 7496 lbs   88
3050 kg / 6724 lbs   86.5

1.3 x VS - Landing Approach Speed at 50 ft obstacle
FLAPS UP   (FLAPS 1)   [FLAPS 2] 
4350 kg / 9590 lbs   94.5   (87.5)   [82]
3850 kg / 8488 lbs   89      (81.5)   [76.5]
3450 kg / 7606 lbs   84      (76.7)   [72.1]
2800 kg / 6173 lbs   75.4   (69.3)   [65.5 1]
1 WARNING: Approach speed not below 69.3 KIAS
   as long as landing is not assured.

Demonstrated crosswind component for landing is 25 KIAS.
This was the maximum crosswind component available during
LBA certification.

VS - Stall Speeds engines idling
VS1 FLAPS UP   (VS1 FLAPS 1)   [VSO FLAPS 2] 
4350 kg / 9590 lbs   72.7   (67.3)   [63]
3850 kg / 8488 lbs   68.3   (62.7)   [59]
3450 kg / 7606 lbs   64.5   (59)      [55.5]
2800 kg / 6173 lbs   58      (53)      [50]

NOTE: For explanations of speeds used on this tab, see
"V-speeds" in the Learning Center Glossary or click here.