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102 Cards in this Set
- Front
- Back
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RUNWAY SLOPE -BOTH
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+/- 2%
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Maximum Takeoff and Landing Tailwind
Component -8/-4 |
15 KTS -8
10 KTS -4 |
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Maximum Operating Altitude-8/-4
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41,000FT -8
37,000FT -4 |
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Maximum Takeoff and Landing Altitude -BOTH
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8,400FT
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MAX CROSSWIND - 30M DRY - TKOF AND LDG -BOTH
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25KTS
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MAX CROSSWIND - 30M - WET - TKOF AND LDG - BOTH
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20KTS
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MAX CROSSWIND - 30M - STANDING WATER/SLUSH - TKOF AND LDG -8/-4
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5KTS -8
0KTS -4 |
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MAX CROSSWIND - 30M - SNOW (NO MELTING) - TKOF AND LDG -8/-4
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10KTS -8
0KTS -4 |
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MAX CROSSWIND - 30M - ICE (NO MELTING) -BOTH
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0KTS
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MAX CROSSWIND - 45M - DRY - TKOF/LDG -8/-4
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33KTS -8
35KTS -4 |
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MAX CROSSWIND - 45M - WET - TKOF/LDG -BOTH
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25KTS
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MAX CROSSWIND - 45M - STANDING WATER/SLUSH - TKOFF/LDG -BOTH
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15KTS
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MAX CROSSWIND - 45M - SNOW - NO MELTING - TKOF/LDG -BOTH
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20KTS
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MAX CROSSWIND - 45M - ICE NO MELTING - TKOF ONLY
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5KTS
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MAX CROSSWIND - 45M - ICE NO MELTING - LDG ONLY -BOTH
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10KTS
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The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations -BOTH
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200FT
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RVSM - UP TO 5000FT - ON GROUND - Max Difference
Between Captain & F/O -8/-4 |
50FT -8
40FT -4 |
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RVSM - UP TO 5000FT - ON GROUND - Max Difference
Between Captain or F/O & Field Elevation -BOTH |
75FT
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VH-VXA - VH-VXU - MTW
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79 242 (79.2)
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VH-VXA - VH-VXU - MTOW
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79 015 (79.0)
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ALL -800 - MLW
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66 360 (66.3)
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ALL -800 - MZFW
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61 688 (61.6)
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VH-VYA - VH-VZE - MTW
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75 296 (75.2)
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VH-VYA - VH-VZE - MTOW
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75 069 (75.0)
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maximum cabin differential pressure (relief valves) -8/-4
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9.1 psi -8
8.65psi -4 |
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With engine bleed air switches ON, do not operate the air conditioning packs in _______ for takeoff, approach or landing. -BOTH
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HIGH
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Do not engage the autopilot for takeoff below ____ feet AGL -8/-4
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400 ft -8
1000 ft -4 |
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For single channel operation during approach, the autopilot shall not remain engaged below ____ feet AGL. -BOTH
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50 ft
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Use of _______ trim with the autopilot engaged is prohibited -BOTH
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aileron
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AUTOLAND - MAX HEADWIND -8/-4
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25KTS -8
35KTS -4 |
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AUTOLAND - MAX CROSSWIND -BOTH
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20KTS
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AUTOLAND - MAX TAILWIND -8/-4
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15KTS -8
10KTS -4 |
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Maximum and minimum glideslope angles for autoland are ___degrees and ___ degrees respectively. -BOTH
|
3.25 , 2.5 DEGREES
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Autoland capability may only be used with flaps ____ and ____ engine/s
operative. -BOTH |
F30 OR 40 AND BOTH ENGINES
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Engine ignition must be on for (5 CASES) -BOTH
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•takeoff
•landing •operation in heavy rain •anti-ice operation - severe turbulence - FLT. |
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Inflight - APU bleed + electrical load: max alt -BOTH
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10,000 ft.
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Ground only - APU bleed + electrical load: max alt -8 ONLY
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15,000 ft
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APU bleed: max alt -BOTH
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17,000 ft
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APU electrical load: max alt.-8/-4
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41,000 ft -8
35,000 ft -4 |
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APU bleed valve must be closed when: (3 CASES) -BOTH
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•ground air connected and isolation valve open
•engine no. 1 bleed valve open •isolation and engine no. 2 bleed valves open. EXCEPT, APU bleed valve may be open during engine start, but avoid engine power above idle. |
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Max flap extension altitude is ______ -BOTH
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20,000 ft.
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Holding in icing conditions with flaps extended is ________. -BOTH
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prohibited
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Do not deploy the speedbrakes in flight at radio altitudes less than --------- -BOTH
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1,000 feet.
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In flight, do not extend the SPEED BRAKE lever beyond the _______ -BOTH
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FLIGHT DETENT
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QFE operations are _______ -800 ONLY
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prohibited.
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Maximum tank fuel temperature: -BOTH
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49°C
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Minimum inflight tank fuel temperature: -8/-4
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3°C above the freezing point of the fuel
being used or -43°C -8/-45°C -4, whichever is higher. |
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Lateral imbalance between main tanks 1 and 2 must be scheduled to be ___. - BOTH
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zero
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Random fuel imbalance must not exceed ____ kgs for taxi, takeoff, flight or landing. - BOTH
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453
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Main tanks 1 and 2 must be full if centre tank contains more than ____kgs. - BOTH
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453
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Operation with assumed temperature reduced takeoff thrust is not permitted WHEN (4 CASES) - BOTH
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anti-skid inop
EEC/PMC inop Contaminated Rwy Windshear |
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MINIMUM DISPATCH OXY PRESSURE - BOTH
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1400PSI
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ON GROUND - Centre tank fuel pump switches should be positioned ON only if the fuel quantity in the centre tank exceeds _______kgs. - BOTH
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453 KG
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MINIMUM BRAKE PRESSURE - HYDRAULICS ON - BOTH
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2800PSI
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MINIMUM HYDRAULIC PRESSURE - BOTH
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2800PSI
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MINIMUM PNEUMATIC START PRESSURE - BOTH
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30PSI
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ENGINE START WHEN N1 ROTATION IS SEEN AND N2 IS AT _____% - BOTH
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25%
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ENGINE START SWITCH MOVES OFF/AUTO AT WHAT % N2 -8/-4
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56% -8
46% -4 |
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maximum allowable fuel weight in either the left or right main tank is______ -8/-4
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4147 kg (4.1) -8
4827 kg (4.8) -4 |
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maximum allowable fuel weight in the centre tank is_______-8/-4
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13 843 kg. (13.8) -8
7 448 kg (7.4) -4 |
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SG.79 - WING FUEL ONLY -TOTAL -8 ONLY
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7.7
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SG.79 TOTAL FUEL (WINGS + CENTRE) -8/-4
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20.5 -8
15.8 -4 |
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Engine EGT - TAKE OFF -8/-4
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950-5mins/10min 1inop -8
940-20SECS/930-5MINS -4 |
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Engine EGT - MAX CONT -8/-4
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925 -8
895 -4 |
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Engine EGT - STARTING - BOTH
|
725
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TURBULENCE PENETRATION SPEED -8/-4
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280/.76 -8
280/.73 -4 250 BLW FL150 - BOTH |
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For landing, reduce the crosswind limit by_____kts on wet and contaminated runways when using
asymmetric reverse thrust - BOTH |
5KTS
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Use rolling takeoff procedure when crosswind exceeds_______ - BOTH
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20KTS
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On approach for Autoland, dual channel operation should be engaged prior to_____ AGL. - BOTH
|
800FT
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On approach for Autoland, dual channel operation, Check FLARE arm
annunciation at approximately ____ AGL - BOTH |
500FT
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Vmo/Mmo - BOTH
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340/.82
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minimum obstacle distance from wingtip -8/-4
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4.9m -8
4.6m -4 |
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minimum obstacle distance from nose -8/-4
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7.1m -8
6.7m -4 |
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minimum turn area - 180 DEGREE TURN -8/-4
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24m -8
21.9m -4 |
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TJE-TJW - MTW
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68,265
(68.2) |
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TJE-TJW - MTOW
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68,038
(68.0) |
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ALL -400 - MLW
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56,245
(56.2) |
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ALL -400 - MZFW
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53,070
(53.0) |
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TJX-TJZ - MTW
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64,863
(64.8) |
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TJX-TJZ - MTOW
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64,636
(64.6) |
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MAXIMUM FUEL DISCREPANCY DEPARTURE/ARRIVAL FUEL - BOTH
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+/-600KGS
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STARTER DUTY CYCLE - BOTH
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2MINUTES EACH ATTEMPT
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MINIMUM TIME BETWEEN START ATTEMPTS - 8/-4
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10 SECS -8
1->2 20 SECS, 2->3 3MINTUES |
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MAX MOTORING DURING START DEFN - BOTH
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N2 ACCELERATION IS LESS THAN 1% IN APPROX 5 SECS
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ABORTED ENGINE START WHEN - 4CASES - BOTH
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-SLOW/NO N1 OR N2 WHEN EGT RISING
-NO OIL PX BY STABLE -NO EGT RISE 10 SECS AFTER FUEL ON -EGT NEARS 725 DEGREES |
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WINGSPAN -8/-4
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35.8M -8
28.9M -4 |
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MAX OIL TEMPERATURE -8/4
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140C - CONT, 140-155C - 45 MINUTES -8
160C - CONT, 160-165C -15MINUTES -4 |
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MIN OIL PX - BOTH
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13 PSI
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APU EGT MAX -4 ONLY
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760C
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APU EGT - CONT -4 ONLY
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710C
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SEVERE TURBULENCE PENTRATION - ACFT CONFIG
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YAW DAMPER - ENGAGED
ENGINE IGNITION - ON (FLT) AUTOTHROTTLE - DISENGAGE USE CWS, DO NOT USE ALT HOLD |
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Vfe1-BOTH
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250 KIAS
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Vfe2 -BOTH
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250 KIAS
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Vfe5 -BOTH
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250 KIAS
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Vfe10 -8/-4
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-8 210 KIAS
-4 215 KIAS |
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Vfe15 -8/4
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-8 200 KIAS
-4 205 KIAS |
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Vfe25 - BOTH
|
190 KIAS
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Vfe30 -8/-4
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-8 175 KIAS
-4 185 KIAS |
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Vfe40 - BOTH
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162 KIAS
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Vlo - RETRACT - BOTH
|
235 KIAS
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Vlo/Mlo - EXTEND - BOTH
|
270/.82
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Vle/Mle - BOTH
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320/.82
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