968a8e433fff23cd34195bf938db9a4590be5d1337926ff38148d86d02d9a413 Section "AFTER ENTERING THE COCKPIT" item count differs between passes (44 vs 21); verify nothing was dropped. Section "LANDING" item count differs between passes (21 vs 2); verify nothing was dropped.

Ejection seat secured Safety pins installed Parachute removed or secure Harness and lap belt secure ISOLATION VALVE Switch off FIRE EXT cover safety wired F/C STAT PRESS Lever NORMAL safety wired F/C DYN PRESS Lever NORMAL safety wired F/C ATT IND BANK Switch NORMAL F/C ATT IND PITCH Switch NORMAL LANDING LIGHT Switch NORMAL F/C LDG GEAR LOCK OUT OFF RAM AIR shut off lever CLOSED ENGINE+FUEL GAGES Priority switch F/C EXT STORES JETTISON safety wired SEC B switch ON MASTER switch ON ICS switches--(avionics--) AS REQUIRED EMERG BRAKE OFF, safety wired Pressure gauges proper reading Hand valves closed, safety wired Canopy closed External CABIN SEAL lever INFLATE

Parachute and harness tight and secure Shoulder harness lock as required Rudder pedals as required Oxygen equipment connect and hooked to LEFT CONSOLE chain Oxygen panel check pressure Emergency lever (RED) NORMAL Diluter demand lever (WHITE) NORMAL OXYGEN Supply lever (GREEN) ON CAB PRESS DUMP valve closed (CW) FIRE COCK LEVER OPEN, safety wired HYD DUMP VALVE lever CLOSED safety wired Throttle position idle Throttle friction as required FUEL SHUT OFF lever CLOSED DE-ICING lever OFF PNEU FILL DE -PRESS CLOSED (CW) ISOLATION VALVE switch OFF AIR START button covered, safety wired FIRE EXT COVER safety wired PITOT BOOM RIGHT safety wired PARACHUTE NO DELAY LANYARD ATT INSTRUMENT PANEL TAXI LIGHT switch OFF LANDING LIGHT switch OFF HP OXYGEN indication check min 100 kg's LDG GEAR buttons check out All instrument readings normal EXT STORES switch SAFE, safety wired EXT TANKS switch OFF Arming switch BLANK RAM AIR shut off lever as required RIGHT CONSOLE Electrical switches OFF EMERG BRAKE lever OFF, safety wired VHF & AVIONICS ALL OFF ICS panel --(avionics--) as required EMERG GEAR EXTENSION valve Closed, safety wired EMERG FLAP EXTENSION valve Closed, safety wired CABIN PRESS/ HEATING OFF CABIN HEAT AUTOMATIC Inverter select switch MAIN INV (down) All C/B's ON (in) Ejection pins in sockets

Helmet on Oxygen hose connect Radio cable connect Oxygen check complete Brake check 4kg/cm2 Control stick and rudder free and correct movement BATT switch ON VOLT/AM METER check button depress, 24v COMMS switch master on Intercome check External power unit connect APU ON light (green) illuminated VHF radio ON Start up clearance request GEN switch ON ENG switch ON C&W panel push to test, all lights Electrical gear position indicators push to test, all red lights illuminated

Be sure that the danger areas are clear before starting. GENERATOR light blinking DO NOT START light OUT GND START button depress for 3 sec Spark plugs igniting listen for sparking Throttle idle FUEL SHUT-OFF lever fully OPEN EGT (APU 700 degrees BATT 750 degrees) keep manually within Fuel/ oil pressure rising limits Idle RPM 35% within 60 sec's APU disconnect Fuel pressure 12 kg's Oil pressure 0.5 kgs EGT (idle) 550'c MAX GENERATOR light out

Stop the engine immediately if one of the following occurs - no sparking of spark plugs - No oil pressure indication - EGT exceeds 750’c The engine must be stopped if there is; - no RPM rise - Idle RPM 35% is not reached after 60 sec’s - Oil pressure stays below 0.5 kg’s To stop the engine Throttle idle FUEL SHUT OFF lever CLOSED In case of fire continue with the following steps; FIRE COCK lever SHUT FIRE EXT button DEPRESS All electric's switches OFF Aircraft Abandon

SEC B switch ON INV switch (PO-250) ON ICS panel recheck VHF/ AVIONICS ON Ext tank switch ON

Brakes apply Throttle idle 35% EGT 550’c MAX Fuel pressure 12 kg’s Oil pressure 0.5 kg’s Oil temperature 20’c MIN Throttle 52% (EGT, OP, OT, FP) C+W panel (T-9) check Attitude indicator (horizon) Erect RMI Compass synchronise with standby Fire warning check VOLTS/AMPS check 28V Throttle 65% (EGT, OP, OT, Flaps/ stabiliser check operation ,FP) Speed brakes check operation HYD PRESS gage check pressure EXT TANKS light (C+W) out Throttle 94% (EGT, OP, OT, FP) ISOLATION VALVE switch on (check light) RPM rise 1 to 3% RPM Throttle 97% (EGT, OP, OT, FP) Throttle 100%(EGT, OP, OT, FP) EGT 700'c max Fuel pressure 79 kgs max Oil pressure 1.8 to 2.5 kg's Oil temperature 110'c max Throttle idle (RPM stabilised) Throttle slam in 2 secs 12 to 14 sec's RPM swing 2% RPM max (5 times) EGT 730'c peak Throttle idle Flight controls recheck Taxi clearance request

Brakes apply Throttle idle 35% EGT 550'c max Fuel pressure 12 kg's Oil pressure 0.5 kg's Oil temperature 20'c min Throttle 52% (EGT, OP, OT, FP) C+W panel (T-9) check Attitude indicator erect Compass sycronize check standby Fire warning check VOLTS/ AMPS check 28V Throttle 65% (EGT, OP, OT, FP) Flaps/ stabiliser check operation (elc+mech Speed brake check operation ind) HYD PRESS gage check pressure EXT TANKS light (C+W) out Throttle idle Flight controls full & free Taxi clearance request

Altimeter set Engine instruments in green All safety pins removed and stowed Canopy closed Pressurisation as required

Brakes apply Chocks removed Throttle 80% Brakes release and test Turn check left/ right perform

Trim 2' rear Speed brakes check in Flaps 15' set Fuel quantity check Engine and flight instruments T's & P's check Oxygen check Canopy locked Harness secure Hydraulic pressure check C+W panel check Flight controls full & free All pins removed and stowed Cockpit pressurisation check (both cockpits)

Brakes apply Altimeter recheck Attitude indicator reset Compass RWY heading Radio compass needle check direction Throttle 90% RPM Engine instruments check Brakes release Throttle 100% max power Nose wheel lift off 140km/h Lift off 180km/h

LANDING GEAR UP button push (min 50ft AGL) FLAPS 0' button push (min 150ft AGL) Throttle 97% upon reaching 250 ELEV TRIM lever set km/hr Engine instruments check All warning lights out

100% RPM max of 6 mins, then reduce to 97% initial climb speed 350 kph CABIN ALT PRESSURE CHECK Oxygen check Engine instruments check (EGT, OP, OT, FP)

Level of maintain CAS or MACH number power about 90% Fuel quantity check Oxygen check Engine instruments check (EGT, OP, OT, FP) Location identify

Normal decent is at 65% AT 300 KPH Fuel quantity check Engine & flight instruments check (EGT, OP, OT, FP) Approach request Altimeter set QFE De-mist as required

Fuel quantity check All warning lights out Pneumatic & hydraulic gages check

Check speed/ distance for particular weight Approach 300 kph DOWN WIND LEG Airspeed 290 kph LANDING GEAR select down Landing gear check indicators Airspeed 270 kph FLAPS 15' button select 15' Flaps indicator check Airspeed 250 kph Throttle 90-94% BASE LEG Airspeed 240 kph Throttle 80-85% FLAPS 30' button select 30' Flaps indicator check Airspeed in turn 220 kph FINAL APPROACH Landing gear + flaps check indicators Airspeed 200 kph Throttle as required

Max braking speed 1300 lts 140 kph 1000 lts 145 kph 700 lts 150 kph 400 lts 160 kph

Trim neutral Speed brakes in Pitot heat off Flaps up Pressurisation off

Chocks in place Canopies open Ejector seat pins install Throttle idle for 30 sec's FUEL SHUT OFF lever closed SEC B switch off INV switch off Engine run down time check min 50 sec's After engine stop ENG switch off GEN switch off BATT switch off