Dassault-Mirage F-1 CZ Procedures

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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