Dassault-Mirage F-1 CZ Procedures

.

FLAPS OPERATION LIMITATIONS

Ø 1/2 FLAPS - IAS < 300 kt

Ø Full FLAPS - IAS < 225 kt

Ø Load factor (full flaps) - 2,5 g

JPT (Jet Pipe Temperature)

Ø On the ground : RPM - 8,400 JPT < 755 deg C

Ø In Flight: RPM = 8,400 JPT < 700 deg C

Ø RPM - 8,900 JPT < 735 deg C

Ø Peak JPT permissible on throttle movements is 780 deg C for a period of 30 seconds maximum and 840 deg C peak In flight, JPT generally exceeds 740 deg C at 8,400 RPM and 710 deg C at 8,900 RPM.

Ø High speed with AB or low speed at high altitude the JPT reading at maximum engine RPM could fall and must not go below 550 deg C

GEAR & WEIGHTS

Ø Maximum takeoff weight - 15,200 Kg

Ø Normal landing weight - 9,000 Kg

Ø Exceptional landing weight - 11,000 Kg

Ø Maximum rate of decent at touchdown:

Ø 9,000 Kg - 450 ft/min

Ø 11,000 Kg - 350 ft/min

FLIGHT ENVELOPE WITH AUTOPILOT

Gear and Flaps up

Ø 500 - 1000 ft IAS < 450 kt

Ø 1000 - 20,000 ft IAS < 650 kt

Ø 20,000 - 36-000 ft IAS < 700 kt

Ø 36,000 - 50,000 ft MACH < 2.0

INVERTED FLIGHT

Maximum of 15 seconds

SUPERSONIC CONDITIONS

Ø Half rolls only allowed up to:

Ø M - 1.5

Ø TAT - 135 deg C

Ø Crosswind - 25 kt

Ø Maximum dive allowed may not exceed -30 deg pitch

ENGINE RPM

Ø Maximum continuous operation - 9,000 RPM

Ø Instantaneous peak limit - 9,250 RPM

MAXIMUM SPEED

Ø IAS 700 kt between 0 and 20,000 ft

Ø IAS 750 kt above 20,000 ft

Ø MACH limit = 2.10

CEILING

Ø 55,000 ft