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53 Cards in this Set
- Front
- Back
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What emergency equipment items are located in the cockpit?
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- 4 Oxygen Masks/Smoke Goggles
- 4 Life jackets - 4 Fire fighting items: - Crash Axe - Halon Fire Extinguisher - PBE - Gloves - 2 Escape Ropes - 2 Flashlights |
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Maximum Crosswind Demonstrated (TO & LDG)
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38 Knots
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Maximum Tailwind (TO & LDG)
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10 Knots
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Maximum Wind for PAX door operations
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65 Knots
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Maximum Wind for Cargo Door operation
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40 Knots (and door must be closed before it exceeds 65 Knots)
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VLE
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280 Kts/ Mach .67
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VLO Extension
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250 Knots
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VLO Retraction
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220 Knots
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Maximum Altitude at which the landing gear my be extended
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25,000 Feet
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Maximum Tire Ground Speed
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195 Knots
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Maximum Brake Temperature for Takeoff
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300 Degrees C
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Maximum Speed with Windshield Wipers in Use
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230 Knots
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Maximum Speed with Flight Deck Window Open
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200 Knots
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When should you not use LP ground conditioned air? |
With Packs operating (Avoids valve chatter) |
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When should you not use HP ground pneumatic air? |
With APU Bleed Air on (Avoids damaging bleed system) |
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Minimum Height for use of AP in Straight IN Non-Precision Approach
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Applicable MDA(H)
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Minimum Height for use of AP in Circling Approach
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Applicable MDA(H) - 100 FT
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Minimum Height for use of AP with only CAT I displayed
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160 FT AGL
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Minimum height for use of AP on Go-Around
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100 FT AGL
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Min height for use of AP on Takeoff with SRS mode? |
100 FT AGL |
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Minimum height for use of AP in all other Phases
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500 FT AGL
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What modes should you not perform non-precision SE approaches? |
FINAL APP NAV V/S NAV FPA (FD use is permitted) |
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Maximum operating altitude with slats and/or flaps extended
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FL200
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Max Outer Tank Fuel Imbalance for Takeoff |
800 LBS |
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Max Inner Tank Fuel Imbalance for Takeoff |
1100 LBS |
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Maximum Outer Tank Fuel Imbalance Inflight and Landing
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1500 LB
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Maximum Inner Tank Fuel Imbalance Inflight and Landing
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3300 LB
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Limitations regarding Center Fuel Tanks |
Do not takeoff using Center Tank fuel Center tanks must be emptied first, then wing tanks |
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ISIS (Integrated Standby Instrument System) Limitation
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When both PFDs lost, do not use ISIS bug function
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APU Limitations
Max Altitude for dual pack operations |
15000 FT
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APU Limitations
Maximum Altitude for Engine Start Assist using APU Bleed Air |
20000 FT
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APU Limitations
Maximum Altitude Single Pack operations |
22500 FT
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APU Limitations
Starter Limits |
After 3 starter motor duty cycles, wait 60 minutes before attempting another start
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Can you use the APU Bleed air for Wing anti-icing?
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No
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Engine Limitations
Minimum Oil Temperature for Starting |
-40 degrees C
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Engine Limitations
Minimum Oil Temperature for Takeoff |
-10 degrees C
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Engine Limitations
Minimum Oil Quantity for Departure |
9.5 Quarts + 0.5/Hour of Flight
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Engine Limitations
Max Number of consecutive Start Cycles. |
4 Cycles
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Engine Limitations
Minimum Cooling Period after 4 Cycles |
15 minutes
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Engine Limitations
Maximum duration of a Start Cycle |
2 minutes
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Engine Limitations
Minimum Pause between Start Attempts |
20 Seconds
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Engine Limitations
Maximum N2 for Running re-engagement of Starter |
20%
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Engine Limitations
Speed below which maximum reverse thrust should not be used |
70 Knots
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Memory Item
EMERGENCY DESCENT |
Crew O2 Mask --------------- ON
Signs ---------------------------- ON ALT ----------------TURN & PULL HDG ---------------TURN & PULL SPD/MACH -------------ADJUST Thrust Lever (if a/t off) ----IDLE Spd Brk -----------------------FULL |
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Memory Item
LOSS OF BRAKING |
If Autobrake Selected
Brake Pedals ---------------PUSH If no braking available: Thrust Rev -------------------MAX Brake Pedals --------RELEASE A/Skid & NWS--------------OFF Brake Pedals------------PRESS Max Brake Press-------1000psi If still no Brake Parking Brake---------------USE |
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Memory Item
UNRELIABLE SPEED INDICATION (Immediate Action Items) |
AP/FD ---------------------------OFF
A/THR -------------------------- OFF PITCH THRUST -Below Thr Red Alt: 15deg/TOGA -Abv Thr Red Below 10000': 10deg/CLB -Abv Thr Red Above 10000': 5deg/CLB FLAPS -If 1,2,3 ----------- Maintain Config -If FULL ------ Select 3 & Maintain SPD Brakes ----- Check Retracted LDG GEAR ---------------- UP When at or above MSA or Circuit Altitude: - Level off for troubleshooting |
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Memory Item UNABLE TO MAINTAIN ALTITUDE ENGINE FAILURE DRIFTDOWN |
Thrust Levers ------MCT A/THR-----------------OFF SPD/MACH--------- Set .78 & Pull HDG----------------- Set & Pull ALT------------------- Set & Pull FL200 NOTE: IF ETOPS- Turn 45 degree left or right from present course to establish a 15NM offset from assigned track.IF NOT ETOPS- Turn to avoid traffic |
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Memory Item WINDSHEAR |
At Takeoff if Before V1: The takeoff should be rejected only if significant airspeed variations occur belowindicated V1 and the pilot decides that there is sufficient runway remaining to stopthe airplane If After V1: THR LEVERS ---------TOGA REACHING VR ------ROTATE SRS ORDERS --------FOLLOW Airborne, Initial Climb or Landing: -THR LEVERS AT TOGA ----SET or CONFIRM -AP (If engaged) ------- KEEP ON -SRS ORDERS ----------- FOLLOW DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR CLOSELY MONITOR FLIGHT PATH AND SPEEDRECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR |
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Memory Item WINDSHEAR AHEAD |
During the Takeoff Run: Takeoff------------------- Reject. (Predictive windshear alerts are inhibited above 100kt until 50 ft) When Airborne: -THR LEVERS----------- TOGA -AP (If engaged)------ KEEP ON -SRS ORDERS----------FOLLOW Landing: -GO AROUND --------PERFORM -AP (If engaged)------- KEEP ON |
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Memory Item TCAS WARNINGS |
-AP (If engaged)------------ OFF -BOTH FDs------------------- OFF -V/S---------------- ADJUST PITCH: (MAINTAIN GREEN AVOID RED) -ATC-------------------------NOTIFY |
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Memory Item EGPWS ALERTS |
Simultaneously: -AP-------------------------- OFF -PITCH-------------------- PULL UP(Pull to full backstick and maintain in that position) -THRUST LEVERS------------TOGA -SPEEDBRAKES LEVER----CHECK RETRACTED -BANK -------------WINGS LEVEL or ADJUST |
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Memory Item STALL RECOVERY |
Any Stall Indication Immediately: -NOSE DOWN PITCH CONTROL------------------APPLY (In case of lack of pitch down authority, reducing thrust may be necessary) -BANK --------------WINGS LEVEL When Out of Stall (no longer stall indications): -THRUST---------- INCREASE SMOOTHLY AS NEEDED -SPEEDBRAKES ---------CHECK RETRACTED -FLIGHT PATH--------- RECOVER SMOOTHLY If In Clean Configuration and Below 20,000 ft: -FLAP 1 ---------------------SELECT |
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Memory Item STALL RECOVERY AT LIFTOFF |
-THRUST ---------------------TOGA At the Same Time: -PITCH ATTITUDE -------------15° -BANK ------------------WINGS LEVEL |
