DCS AERGES MIRAGE F1, Flight Manual

Page: 115 / 132

DCS: Mirage F1 Flight Manual Version 1.0
115
5. LIMITATIONS
5.1 CLEAN AIRCRAFT LIMITATIONS
Figure 5-1 Clean Aircraft Configuration
Fast roll maneuvers
Fast roll maneuvers should be limited to avoid:
- Excessive skids (high Mach at low altitudes)
- Divergent flight conditions (high Mach at high altitudes)
In case of damper failure:
- In subsonic flight:
o
Do not perform successive rolls
- In supersonic flight:
o
Half rolls permited:

Up to M 1.5 with full roll control travel if load factor is higher than 0
below 40,000 ft and higher than 1 above 40,000 ft

Beyond M 1.5, half roll with half roll travel if load factor is higher than 1

Up to M 2.1

i = 17° except at transonic range i = 15°

Crosswind ≤ 25 kts

In supersonic flight, dive ≤ 30°

n ≤ 0 limited to 15 sec (due to engine fuel supply)
H ft x 1000
50
40
30
20
Permissible load factor
-3 < n < +7.2
Permissible load factor
-3 < n < +6
1 1.05 1.5 2.1
Half-roll
α stk
1
____ if n > 1
Half-roll
α stk
2
if n > 1
____
Half-roll
α stk
1
____
if n > 0