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34 Cards in this Set
- Front
- Back
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BLEED MISCONGIF caution Why are they on and when (3) How to turn off (3) |
Because both 10th and 14th stage air is coming off the engines Appears when both bleeds and packs are using engine air and the flaps or gear are down Eliminated by, 10th air to APU or turning anti ice off or doing take off or landing with packs off |
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APU shutdown on ground |
APU shutdown first then transfer bleeds |
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APU shutdown in air |
Transfer bleeds to engines and then shut down the APU |
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N2 to extinguish "COWL ANTI ICE" caution |
78% |
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Turning in cowl anti ice at high power settings |
Turn on wing anti ice then cowl anti ice. Turn off wing anti ice if not required. |
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Before starts above the line |
"AEH SPA" APU Electrics Hydraulic pumps Seat belts Pressurization Anti-skid |
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Instrument check |
Flight director right Clock zeroed Needle color, course bar direction Heading bug Level off altitude Altitude pre select NAV radio as required Transponder code HCP mode "Set" PM "crosschecked" |
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Take off briefing |
Runway Flaps setting Thrust setting BLEED configuration Anti ice and ignition configuration Min take off visibility SID review Noise abatement Level off altitude Engine out procedure |
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Start flow below the line (FO) |
ACARS W&B OR FINAL WEB Request final TLR or post speed book Adjust take off reference speeds and STAB trim |
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Before starts below the line (captain) |
Doors Fuel pumps/quantity Beacon Nose wheel steering Transponder Parking brake |
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Ground crew clears to start |
Captain "continue" Packs Ignition |
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Max N2 split after a start |
2% |
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Oil pressure is outside of normal arc after start |
Might have slow response can be at 130 for max of 10 minutes
Do not advance throttle above idle |
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N2 is 57% or less and OAT -20°c |
Do NOT advance thrust above idle |
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N2 below 56.5% and OAT above -20°c |
Max N2 70% until core speed stabilizes |
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Started second engine and you get a FUEL LO PRESS caution |
Advance thrust to 5% above idle and verify message is out. |
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At idle thrust with zero oil pressure after start |
Shut down engine immediately |
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After starts above the line (captain) |
Gens Ignition Electrics (AC and DC) APR |
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After starts above the line (FO) |
APU Bleeds Packs Cargo air Anti ice Probes |
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Take off data briefing |
Takeoff weight Bleeds config Flap setting V speeds "Set" PM "crosschecked" |
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After starts below the line (captain) |
F/CTL page Rudder Steering |
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Before takeoff checks |
FFFFAAN Flaps Flight controls Flight instruments Fuel crossflow APU Anti ice N1 |
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Rise briefing |
Runway in use Instrument departure Stop altitude Engine out procedure |
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Line up checks (FO) |
CaTIE Cabin (chime) Transponder Ignition ED 1 and 2 |
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Line up checks (captain) |
ED 1 and 2 Lights |
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After take off checks |
F-BALT Fuel crossflow Bleeds APU lights Thrust reversers |
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Climb through 10000 |
"10000 feet, lights out, belts _____, Pressurization checks" Turn off recog/taxi |
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TSAFE briefing |
Type, first turn, all other turns, time of legs Speed Altitude Fuel (remaining and required) Expected further clearance time |
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Recommended holding speed |
Below 14000 flap 0 Vref + 30KIAS 14000-FL250 225KIAS FL250 or above drift down speed plus 10KIAS or 225KIAS which ever is higher |
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Approach checks |
Lights (recog on) Pressurization Cabin (seat belt twice) APU |
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Avionics cross check |
Course bar selection FMS is sequenced RTU frequencies HCP set up |
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Stabilized approach factors (8) |
Gear extended Flaps configured Spoilers retracted Correct vertical and lateral path Correct speed +10 or -5 Normal decent rate 500-900 FPM no turns below 500' Thrust is stabilized for speed |
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Landing flow |
GeCaT-SILF Gear Cabin Trust reversers Spoilers Ignition Landing lights Flaps
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TOGA button accomplishes on go around (5) |
Autopilot disconnects GA/GA on flight director Missed approach sequences HGS to PRI GA carrots on N1 gauge |
