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.