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144 Cards in this Set
- Front
- Back
- 3rd side (hint)
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700 Max Taxi/Ramp weight |
75,250 |
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900 Max Taxi/Ramp weight |
85,000 |
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700 max takeoff weight |
75,000 |
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900 Max takeoff weight |
84,500 |
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700 max landing weight |
67,000 |
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900 max landing weight |
75,100 |
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700 max ZFW |
62,300 |
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900 max ZFW |
70,750 |
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When can we turn on Autopilot after takeoff? |
600 ft |
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When must Autopilot be turned off during a non-precision approach? |
400 ft. |
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When must Autopilot be turned off during a precision approach? |
80 ft |
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700 max weight fwd cargo |
1,000 lbs |
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900 max weight fwd cargo |
1, 700 lbs |
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700 max weight aft cargo |
3,300 lbs |
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900 max weight aft cargo |
3,740 lbs |
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Max crosswind T/O & landing |
27 kts |
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Max crosswind CAT II |
15 kts |
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Max headwind CAT II |
16 kts |
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Max tailwind T/O &landing |
10 kts |
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Max operating altitude |
41,000 ft |
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Except in an emergency, T/O & landing will not be attempted whenever PEAK wind value exceeds __________ kts. |
50 kts |
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Max positive differential pressure |
8.7 psi |
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Max altitude for single pack operation |
31,000 ft. |
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Use of the EMER DEPRESS switch above_______________ ft. is prohibited. |
15,000 ft. |
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Turbulence penetration speed |
280 KIAS / .75 M, whichever is lower |
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Max gear extension speed |
220 kts |
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Max gear extended speed |
220 kts |
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Max gear retraction speed |
200 kts |
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Max airspeed for windshield wiper operation |
220 kts |
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Max airspeed for windshield wiper operation failed in the non-parked position |
250 KIAS |
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Max cruise mach in RVSM airspace |
. 82 M |
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Max GS for tires |
700 - 182 kts 900 - 195 kts |
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Flap extended/operating speeds (Vfe & Vfo) |
Flaps 1...................230 KIAS Flaps 8...................230 KIAS Flaps 20.................220 KIAS Flaps 30.................185 KIAS Flaps 45.................170 KIAS |
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The APU starter motor duty cycle is limited to _________________ |
No more than 3 starts/start attempts within 1 hour with a 2 minute delay between each cranking attempts. |
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Max RPM APU |
106% |
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Max APU starting altitude |
37,000 ft |
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Max APU operating altitude |
41,000 ft |
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Max altitude for bleed air extraction from the APU |
25,000 |
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Max altitude for engine start using APU bleeding air |
21,000 ft |
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With the APU door not closed or the door position unknown, the airplane must be limit to |
220 KIAS or the APU must remain in operation. |
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Max time for ground operations with DC power only |
5 mins |
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During all starts, do not exceed ______% N1 for _______mins after start, or until all operating conditions are in the ________range, whichever is ____________ |
During all starts, do not exceed 75% N1 for 2 mins after start, or until all operating conditions are in the normal range, whichever is longer. |
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Operate engines at or near idle for ______ mins prior to shutdown |
2 mins |
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Airplane cold-soak |
B4 the 1st flight of the day, when the airplane is cold-soaked at an ambient air temp of -30°C or below for more than 8 hours. •The engines must be motored for 60 secs and fan rotation must be verified b4 an engine start is initiated •Thrust reverses must be actuated until the deploy and stow cycles are 2 secs or less. |
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Min oil temp for starting |
-30°C |
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Min Oil pressure steady state idle |
25 psi |
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Min Oil Pressure Takeoff Power |
45 psi |
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After cold start, engine must remain at ______ until Oil pressure returned to ____________ |
After cold start, engine must remain at idle until Oil pressure returnes to normal range. |
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Continuous ignition must be used for |
• Takeoff and landing on contaminated runways • Takeoff with high crosswind components (15 kts +) • Flight through moderate or heavier intensity rain • Flight through moderate or heavier intensity turbulence • Flight in the vicinity of thunderstorms |
There are 5 |
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Starter cranking limits (ground) |
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At initiation of thrust lever movement from SHUT OFF to IDLE: |
• ITT must be 120°C or less for all ground starts. • ITT must be 90°C or less for all air starts |
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Dry-Motoring Cycle |
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Thrust reversers limitation |
During landing, maximum reverse thrust is prohibited below 75 KIAS, & reverse idle should be achieved by 60 KIAS. |
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Engine operating limits due to wind direction |
< 5 kts or w/in 30° of nose - No. limitation >30° and between 5-30 kts: Apply max 75% N1 before brake release, then TOGA thrust >30° and >30 kts: Apply max idle/taxi thrust before brake release, then TOGA thrust
• NOTE • If Static/Standing takeoff data is generated and wind limits prevent a Static/Standing takeoff: A) Winds must be entered into ACARS B) For aircraft with ACARS inop, dispatch must manually insert the wind into the TLR data. |
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FLEX takeoff limitations |
1. Anti-Skid must be operative PROHIBITED: 2. On contaminated runways 3. If the airplane has been de-iced 4. If wing &/or cowl ice are in use 5. If windshear or downdrafts have been forecasted 6. With an engine that can't achieve full thrust 7. When a special DP specifies "FULL THRUST TAKEOFF" |
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Enroute use of slats/flaps is |
Prohibited |
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Min altitude for flight spoiler deployment |
1,000 ft AGL |
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Min airspeed for flight spoilers |
Vref + 17 KIAS |
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Max fuel imbalance between left and right wing tanks for takeoff |
300 lbs |
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Max fuel imbalance between left and right wing tanks during flight or landing |
800 lbs |
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Max fuel |
19,594 |
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Takeoff w/ a fuel load in excess of a)_______ lbs in the center tank is not permitted unless each wing tanks is above b)________ lbs |
a) 500 lbs b) 4,400 lbs |
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Powered crossflow and gravity crossflow must be _______ for takeoff |
Off |
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Min fuel quantity for a go-around per wing tank and assuming a max pitch up of 10° |
600 lbs |
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Takeoff with engine fuel temperature indications below ______ is prohibited |
5°C |
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Icing Conditions |
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Ground Contamination |
Runways, ramps, or taxiways with surface snow, ice, slush or standing water |
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Visible moisture |
• Visible moisture or precipitation in any form (such as fog with visibility of one mile or less, mist, rain, snow, sleet, and ice crystals or clouds inflight) • If visible moisture is present below 400' AGL with OAT 10°C or below activate Cowl anti-ice for takeoff. If OAT 5°C or below activate both cowl and wing anti-ice for takeoff |
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Do not hold in icing conditions with __________ or __________ extended |
Slats or flaps |
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Wing and/or cowl anti-ice selection inflight is _________ with the APU as a bleed source in manual mode |
Prohibited |
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Tactile check |
•The OAT is 10ﾟC or less, or •The bulk fuel temperature is 0ﾟC or less, or •The atmospheric conditions have been conductive to frost formation •Ice and frost may continue to adhere to wing surfaces for some time even at outside air temps above 10ﾟC |
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Taxi lights must be switched off whenever the airplane is stationary in excess of __________ |
10 minutes |
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Minimum brake cooling time is _____ mins, and all BTMS indicators must be ____________. |
15 mins. green and not increasing |
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CAT II approaches are prohibited when the breaking action is reported as less than ___________ |
Medium |
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900 - For precision approaches or approach procedures with vertical guidance, the minimum height for auto pilot use with one engine operating is ________ |
110 ft. AGL |
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Use of SPEED MODE with the flight director or autopilot coupled during approach is |
PROHIBITED |
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Use of VNAV with the flight director or autopilot coupled during the climb and approach phases of flight is |
Prohibited |
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RVSM required equipment list |
• Autopilot with Alt.Hold - must be operational. • Altitude alerting system - must be operational • Altitude reporting transponders - One must be operational • Air Data Computers - Two must be operational |
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Flights must be within _____minutes of suitable airport, if cargo is carried in either cargo compartment |
60 mins |
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Can we use flaps 1° during terminal phase of flight |
Yes |
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What is the maximum altitude we can use flaps? |
15,000 ft. |
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Breaking Loss / Asymmetry |
1. Wheel brakes ...... Release momentarily 2. PM will select ANTI-SKID to OFF 3. Wheel brakes......... Re-apply as required 4. Reverse Thrust.......Apply max until stopping assured |
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CABIN ALT or Emergency Decent |
1. Oxygen mask ..... don and 100% 2. Crew communications ....establish 3. Captain assumes PF duties |
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SMOKE / FIRE / FUMES |
1. O2 mask (if required).... Don & 100% 2. Crew communications....... Establish |
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Stabilizer Trim Runaway |
1. Control Wheel..... ASSUME manual control and OVERRIDE runaway 2. STAB TRIM DISC.....Push, Hold and release |
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CONFIG Warning |
1. Takeoff...... DISCONTINUE Immediately |
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Rejected Takeoff before V1 |
1. Thrust levers.......Idle 2. Wheel Brakes.......MAXIMUM until a safe stop. 3. Thrust reversers..... MAXIMUM consistent with directional control. |
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STALL RECOVERY |
1. Autopilot..... DISENGAGE, if required 2. Pitch attitude...... Lower nose to reduce AOA 3. Thrust levers..... advance to MAX POWER 4. Roll attitude..... wings level 5. FLIGHT SPOILER LEVER..... RETRACT 6. Declare low speed event with ATC. Report current hdg and alt and request further instructions. |
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Additional immediate action items |
1. L/R ENG OIL PRESS msg or OIL PRESS LOW 2. Aileron system jammed 3. Rudder system jammed 4. Elevator system jammed 5. Uncommanded Yaw motion 6. Unreliable Airspeed In-flight |
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Landing Configuration Stall |
Onset of stall:"Set Thrust, Check Spoilers"(Positive Rate)"Flaps 8, Gear Up"(Vt-10) "Flaps Up" |
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V1 Cut |
"Engine Failure" (Positive Rate) "Gear Up, Speed Mode, Bug V2" (400') "HDG/NAV MODE, Half Bank" (600') "Autopilot On" (1000') Select ALT (Vt-10) "Flaps Up" (Vt) Speed Mode, Half Bank Off "CLIMB" (verify CLIMB mode)"QRC L(R) ENG Failure" |
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Balked Landing |
"Go Around" TOGA "Set Thrust, Check Spoilers" (Positive rate) "Flaps 8, Gear up, Speed mode" (400') "HDG Mode" (600') "Autopilot On" (1000') "200 kts" (Vt-10) "Flaps Up, After Takeoff Checklist" |
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Single engine go-around |
"GO-AROUND! "*TOGA*"Set thrust, Flaps 8" (Positive Rate) "Gear Up, Speed Mode, Bug V2" (400') "HDG/NAV MODE, Half Bank" (600')"Autopilot On" (1000')Select ALT (Vt-10)"Flaps Up" (Vt)Speed Mode, Half Bank Off "CLIMB" "Single ENG after takeoff checklist" |
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When a wing tank fuel level drops below ________ of its total capacity, the fuel system computer will use the transfer ejectors to fill the respective low wing tank. |
93% |
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Maximum differential pressure for taxi, takeoff, and landing |
0.1 psi |
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Tactile check - when, why, how |
When: 1. The OAT is 10ﾟC or less, or 2. The wing fuel temp is 0ﾟC or less, or 3. The atmospheric conditions have been conductive to frost formation. 4. Ice and frost may continue to adhere to wing surfaces for some time even at OAT above 10ﾟC Why: To determine that the wing is free of frost How: During the external walk around inspect the wing leading edge, wing forward upper surface, and wing rear upper surface |
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Minimum runway width for takeoff and landing |
100 ft. |
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All contaminated performance data will be for __________ takeoffs |
Rolling |
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Bleed air 10th stage valves must be _______ for takeoff and landing if the anti-ice systems have been selected ON |
Closed |
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Operate engines at or near idle for _________ minutes prior to shut down |
2 mins |
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Take off with engine fuel temperatures below_______ is prohibited |
5ﾟC |
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What happens if A/C full cold is selected in MAN mode? |
If the pack discharge temp is<5°C the L or R PACK TEMP Caution msg is displayed. |
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When do we use windshield heat in HI position |
When LOW is not enough to shed accumulated ice |
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What stage pneumatic air is used for wing anti-ice |
6th stage bleed air unless the demand is exceeded, then the HPV is commanded open to supply 10th stage bleed air |
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If you forget to turn on the probes, will they turn on automatically? |
Yes, all probes turn on automatically regardless of switch position once airborne. |
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If an engine fails, can we get hot air to the other wing? |
Yes, via the wing anti-ice cross-bleed duct valve. |
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If the starter does not cut out, what is the quickest way to shut off air to the engine? |
Press the affected ENG STOP button associated with the engine being started |
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Why would we get an Amber BLEED MISCONFIG message |
APU manually selected as the bleed source and either cowl or wing anti-ice is selected on |
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Does the Ignition system ever come on automatically? |
Yes, when a high angle of attack is approached. |
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How many bottles does the APU have ? |
One |
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How many fire bottles do the engines have? |
Two |
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What does bleeds open mean? |
Engines supplying bleed air to the air conditioning system for takeoff |
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Landing gear system is powered by _____________ |
Hydraulic system 3 |
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When do we need a takeoff alternate? |
Anytime weather conditions at the departure airport are below the lowest CAT I approach minimums for the runways in use. |
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Do we ever takeoff with the window heat turned off? |
Yes, if the OAT is 30ﾟC + |
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When will the seat belt sign automatically come on in the AUTO position? |
Cabin altitude exceeds 10,000 ft., or flaps out of 0ﾟ or gear extended |
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When will emergency lights come on automatically? |
When the switch is selected to ARM and power is lost to either the AC or DC essential bus. |
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When would a charger message be displayed? |
APU or MAIN airplane battery is not charging or overheating |
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If the AUTO TRANSFER FAIL light comes on, is it a good thing? |
Yes, it prevents a failed BUS from disabling the next prioritized generator. Indicates a fault preventing auto transfer |
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When will a fault light up the IDG light? |
IDG will automatically disconnect when an over-temp or over-torque condition occurs. • Indicates a fault within IDG (HOTLOP) |
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Pressing the IDG DISC switch will do what? |
The IDG will be electrically disconnected from the engine accessory gearbox. An electrical solenoid is energized that causes the drive gear to retract from the engine accessory gear Box. It can only be reconnected on the ground by maintenance personnel. |
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How many TRUs and how many AMPS can they produce? |
4 & 120 AMPS |
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What do TRUs do? |
For devices requiring DC power, 115V AC power is converted to unregulated 28V DC power by transformer rectifier units. |
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What system will automatically deploy the passenger 02 mask and when? |
CPCP - Cabin Pressure Control Panel Microprocessor If cabin alt exceeds 14,000 ft., passenger 02 mask are deployed automatically |
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What does the RESIRC FAN do? |
Turns on both recirculation fans and allows recirculated air to be mixed with conditioned air for the flight deck and passenger cabin |
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What does the conditioned air switch do? |
•Controls air circulation in aft cargo Bay •OFF - closes intake and exhaust SOVs to seal aft cargo bay enclosure •AIR - SOVs opened, recirculated or conditioned air ventilates aft cargo bay •COND AIR -SOVs opened, recirculated or conditioned air ventilates the aft cargo bay. Electric heater maintains bays temperature. |
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What are the main and backup hydraulic pumps? |
Main - A Backup - B
- System 1&2 are powered by engine driven pumps and have AC motor backups. - System 3 is powered by two ACMPs |
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How are hydraulic systems 1 & 2 cooled? |
Air/hydraulic oil heat exchanger |
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Which hydraulic pump is powered by the ADG regardless of switch position? |
3B |
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When you press the EMER DEPRESS button, how does it depressurize the aircraft? |
The manual DC motor will drive the outflow valve fully open. The microprocessor restricts the cabin altitude to maximum of 14,500 ± 500 ft. |
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How many pressure controllers do we have? |
3. One manual controller and two automatic CPC's which control all automatic phases of pressurization. Only one CPC is active at any time, the other is in standby mode. Changing after the aircraft has landed and has been on the ground for 3 minutes. |
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When will the ADG auto deploy? |
AC BUS 1 and 2 are unpowered, no weight on wheels and an aircraft generator was the last power source online. |
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With the ADG deployed, what bus does it power? |
The ADG BUS, which then powers the AC essential BUS and hydraulic pump 3B. |
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Do we have fire detection system in cargo? |
No, only smoke detection. |
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How many bottles are used in cargo? |
2, bottles can be selected to either forward or aft cargo. Bottle 1 discharges immediately, and bottle 2 slowly over a 60 minute period. |
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Can the fire bottle be directed into either engine? |
Yes, they are directed to the engine when the associated ENG FIRE PUSH switchlight is selected. |
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If both bottles are fired into one engine, is there any remaining fire protection? |
No, there are only 2 bottles. |
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Why do we have gravity crossflow system ? |
In the event that auto or manual powered crossflow functions fail, fuel balance can be maintained using gravity crossflow line. |
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Does the APU have its own fuel pump or does it share? |
It has its own dedicated pump. |
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Do we use 6th and 10th stage bleed air at the same time, or one or the other? |
One or the other, a one-way check valve prevents the reverse flow of 10th stage bleed air to the lower pressure 6th stage duct. |
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When setting the cabin temp, are we setting temp or valve position? |
Automatic mode - output temp Man mode - valve position |
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At what percent N2 does the starter cut out? |
50% N2 |
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What detent do we use to get Max continuous thrust (MCT) during single engine climb? |
CLIMB detent |
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EICAS markings |
RED - Max and Min Limitations AMBER - Caution Range GREEN - Normal Operating Range |
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