FOKKER-100 Tay-620 AIRCRAFT
REFERENCE INFORMATION
For detailed instructions on how to fly this aircraft, use the PF10070v2
Flight Example flight
in conjunction with the instructions for this flight.
See also the PF10070 website at
http://fokker.avsim.net
For standard procedures, see the Checklists tab.
Weight and Speed specifications
Maximum Take Off Weight - MTOW | 95,500 lbs |
Maximum Landing Weight - MLW | 85,500 lbs |
Maximum Zero Fuel Weight - MZFW | 79,000 lbs |
Maximum Operating Speed - VMO | 320 KIAS |
Maximum Operating Speed Mach - MMO | .77 Mach |
Rough Air Speed - VRAS/MRAS | 250 KIAS/.65 Mach |
Maximum Gear Operating Speed - VLO | 200 KIAS |
Maximum Landing Gear Extension Speed - VLE | 200 KIAS/.82 Mach |
Maximum altitide (ceiling) | 35,000 ft |
Maximum range (with full payload) | 1,600 NM |
Maximum # of passenger @ 200 lbs payload ea. | 107 |
Maximum Flap Placard Speeds
Flaps degrees | KIAS |
8 | 250 kts/0.50 Mach |
15 | 220 Kts/0.45 Mach |
25 | 220 Kts/0.45 Mach |
45 | 180 Kts/0.36 Mach |
V1 = VR - Takeoff Decision
and Rotation Speed at weight 44,000 lbs
Standard temperature, sea level pressure altitude,
dry runway
Flaps 0 | 147 KIAS |
Flaps 8 | 139 KIAS |
Flaps 15 | 136 KIAS |
V2 - Takeoff Safety Speed at weight 44,000 lbs
Standard temperature, sea level pressure altitude, dry runway
Flaps 0 | 150 KIAS |
Flaps 8 | 142 KIAS |
Flaps 15 | 138 KIAS |
VREF - Landing Approach Speed with flaps 42, gear down
Standard temperature, sea level pressure altitude, dry runway
28,000 kg | 109 KIAS |
44,000 kg | 133 KIAS |
NOTE: For explanations of speeds used on this tab, see "V-speeds" in the Learning Center Glossary.