Dassault-Mirage F-1 CZ Procedures

 

PRE-START CABIN CHECK

 

q       Clock SET

q       Mach/Airspeed indicator ZERO

q       RPM indicator ZERO

q       A/B lights TESTED

q       Slaved Altimeter FLAG VISIBLE

q       Vertical speed indicator ZERO

q       Landing light switch OFF

q       Landing gear handle DOWN

q       Radio SET

q       Flap lever FULL FORWARD

q       Throttle lever CLOSED

q       Cockpit lights OPERATIONAL

q       Fuel gauge CHECKED

q       Cross-feed switch OFF

q       Radio Altimeter OFF

q       Alternator switch ON

q       Failure warning lights TESTED

 

ENGINE START

 

q       Parking brake ON

q       Fuel valve ON

q       Thrust lever IDLE

q       Start power ON

q       Oil light ON BELOW 2000 RPM

q       Engine STABLE AT 2900 RPM

q       JPT NORMAL

q       Oil, Hyd and Alt lights OFF

 

AFTER START CHECKS

 

q       Vertical reference ON

q       Heading selector NAV1 or HDG

q       VOR/ILS ON

q       Standby Horizon ON

q       Probe heat ON

q       Radio frequencies SET

 

PRE-TAXING CHECKS

 

q       Trims SET

q       Airbrakes CHECKED

q       Flaps CHECKED

q       Fuel cross-feed OFF

q       Fuel gauge quantities CHECKED

q       Hydraulic pressure NORMAL

q       V-Speeds COMPUTED

 

TAXING

 

q       Parking brake OFF

q       Wheel brakes CHECKED

q       Slaved altimeter SET

q       Standby horizon SET

 

LINEUP

 

q       Radio altimeter CHECKED / SET

q       Headings CHECKED

q       Flaps/Slats SET

q       Failure warning lights OUT

q       Pitot heat ON

q       Flight controls FREE

q       Takeoff power RPM SET

 

TAKEOFF

 

q       Landing lights ON

q       100 kt time-check CHECKED

q       AB IGNITED

q       RPM and JPT CHECKED

 

CLIMB

 

q       Gear UP / LOCKED

q       Flaps UP

q       RPM CHECKED

q       Landing lights OFF

 

NORMAL DESCENT

 

q       RPM approximately 6,500

q       Establish -10 deg flight path slope

q       Maintain M = 0.92 and final IAS of 450 kt

 

FAST DESCENT

 

q       RPM = 6,500

q       Airbrakes extended

q       Maintain IAS 300 kt

q       If rate of descent is to be reduced, retract airbrakes, maintain 300 kt, 6,500 RPM and a flight path of -5 degrees

 

DOWNWIND LEG CHECKS

 

q       Course / NAV SET

q       Hydraulic pressure CHECKED

q       Airbrakes RETRACTED

q       Gear DOWN / LOCKED

q       Flaps FULL

q       Remaining Fuel CHECKED

q       Cross-Feed ON

q       Nose wheel steering CHECKED

q       Brakes light OFF

q       Landing lights ON

q       RPM CHECKED

q       Incidence CHECKED

 

LANDING

 

q       Maintain velocity vector on runway by compromising angle of attack, glide slope and engine RPM

q       AOA = 9 TO 11 DEGREES

q       Engine RPM = 7,000 TO 7,600

q       At overrun AOA = 13 degrees

q       Engine RPM = 7,000 at

q       IAS = 135 kt

q       After touchdown, move throttle to idle.

q       Do not extend airbrakes during flare-out

 

AFTER CLEARING RUNWAY

 

q       Avionics OFF

q       Probe Heat OFF

q       Landing Light OFF

q       Flaps / Slats UP

q       Trims NEUTRAL

 

ON PARKING AREA

 

q       RPM STABILIZED

q       Radar OFF

q       Avionics OFF

q       SHUTDOWN

q       Throttle IDLE

q       Fuel valve OFF

q       Time RECORD

q       BATTERY OFF