DCS AERGES MIRAGE F1, Flight Manual

Page: 117 / 132

DCS: Mirage F1 Flight Manual Version 1.0
117
5.3 ENGINE LIMITATIONS
Figure 5-3 Engine Envelope
Avoid flying outside this envelope, it can cause compressor stall or engine damage.
Inverted flight: 15 seconds.
5.4 ELEMENTS EXTENDED LIMITATIONS
COMBAT HIGH-LIFT DEVICES IAS / MACH LOAD FACTOR AND INCIDENCE
Auto slats only 470 kts / 1.1 -3 G +7.2 G or i < 17°
Combat slats and flaps 335 kts / 0.85 -3 G +7.2 G or i < 17°
TAKEOFF/LANDING HIGH-LIFT DEVICES IAS LOAD FACTOR AND INCIDENCE
Half flaps 300 kts i < 17°
Full flaps 225 kts 0 G +2.5 G or i < 17°
LANDING GEAR
Maximum takeoff weight 15200 kg (33510 lbs)
Normal landing weight 9000 kg (19842 lbs) Max R/D 550 ft/min
Exceptional landing weight 11000 kg (24251 lbs) Max R/D 395 ft/min
Emergency landing >11000 kg Lowest possible R/D (< 300 ft/min)
LIM warning light and warning horn when IAS ≥ 240 kts
TRAIN warning light when IAS ≤ 215 kts and throttle lever less than 8100 rpm
BRAKE CHUTE ≤ 210 kts
LANDING LIGHT < 240 KTS
H ft x 1000
Envelope valid in standard
atmosphere ±10°
M
in
w
in
d
mi
lli
n
g
sp
ee
d
1
1
0
0
rp
m
Relight
envelope
RPM reduction
prohibited