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150 Cards in this Set
- Front
- Back
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flight maneuvering acceleration limit in clean config |
-1 g to + 2.5 gflight |
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flight maneuvering load acceleration limit in other than clean configuration |
0 g to + 2 g |
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max altitude |
39800 ft |
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max take off and landing altitude |
9200 ft |
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min take off and landing altitude |
-2000 ft |
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runway slope (mean) limit |
+- 2 % |
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nominal runway width |
45m |
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minimal runway width |
30m |
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maximum certified crosswind for take off |
35 kts gust included |
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maximum demostrated crosswind for landing |
38 kt gust included |
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max tailwind for take off and landing |
15kt |
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Maximum wind for passenger door operation |
65 kt |
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flap setting for landing with tailwinds greater than 10kt |
flaps full |
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Maximum wind for cargo door operation |
40kt ( 50kt if aircraft nose is into the wind) |
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Cargo doors must be close before wind speed exceeds |
65 kt |
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max xwind take off damp, wet, frost, slush dry and wet snow up to 3mm (good) |
35 kt (38kt) |
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max xwind landing damp, wet, frost, slush dry and wet snow up to 3mm (good) |
38 kt |
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max xwind takeoff and landing compacted snow at or below -15•C (good to medium) |
29 kt |
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max xwind takeoff and landing dry wet snow more than 3mm compacted snow above -15•C, dry wet snow over compacted snow, slippery when wet (medium) |
25 kt |
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max xwind landing damp, wet, frost, slush dry and wet snow up to 3mm (good) |
38 kt |
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max xwind takeoff and landing compacted snow at or below -15•C (good to medium) |
29 kt |
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max xwind takeoff and landing dry wet snow more than 3mm compacted snow above -15•C, dry wet snow over compacted snow, slippery when wet (medium) |
25 kt |
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max xwind takeoff and landing water and slush more than 3mm up to 12.7mm (medium to poor) |
20 kt |
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max xwind for takeoff and landing ice (cold and dry) (poor) |
15 kt |
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Takeoff is not recommended on the following runway conditions |
-wet ice -water on top of compacted snow -Dry snow or wet snow over ice |
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max flap 0 speed |
VMO/MMO |
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max flap 1 speed |
230 kt |
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max flap 1 speed |
230 kt |
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max flap 1+F speed |
215 kt |
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max flap 2 speed |
200 kt |
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max flap 3 speed |
185 kt |
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max flap full speed |
177 kt |
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VMO |
350 kt |
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MMO |
M 0.82 |
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maximum speed with landing gear extended VLE |
280 kt M 0.67 |
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maximum speed with landing gear extended VLE |
280 kt M 0.67 |
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maximum speed at which landing gear may be extended VLO extension |
250 kt M 0.60 |
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Maximum speed at whichthe landing gear may be retracted VLO retraction |
220 kt M 0.54 |
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Maximum tire speed maximum ground speed |
195 kt |
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Minimum control speed for landing VMCL |
113kt |
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VMCA at 0 ft |
110 kt |
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Maximum tire speed maximum ground speed |
195 kt |
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Minimum control speed for landing VMCL |
113kt |
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VMCA at 0 ft |
110 kt |
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Maximum tire speed maximum ground speed |
195 kt |
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Minimum control speed for landing VMCL |
113kt |
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VMCA at 0 ft |
110 kt |
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VMCG at 0 ft conf 1+ F |
111 kt |
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Maximum wiper operating speed |
230 kt |
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maximum taxi weight |
75900kg (73900 kg) |
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Maximum takeoff weight |
75500kg (73500 kg) |
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maximum landing weight |
66000kg |
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maximum zero fuel weight |
62500 kg |
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minimum weight |
37230 kg |
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Maximum time on board with Passengers without air-conditioning |
20 minutes |
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APU bleed use with HP air start unit |
The flight crew must not use bleed air from the APU bleed and from the HP air start unit at the same time to prevent any adverse affect on the bleed air system |
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avionics ventilation limit on ground if OAT less than 49 •C |
no limitation |
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avionics ventilation limit on ground if OAT less than 49 •C |
no limitation |
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avionics ventilation limit on ground if OAT between 49•C and 55•C |
2 hours |
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avionics ventilation limit on ground if OAT between 55•C and 60•C |
1 hour |
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avionics ventilation limit on ground if OAT between 60•C and 64•C |
0,5 hours |
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Maximum positive differential pressure |
9 PSI |
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Maximum negative differential pressure |
-1 PSI |
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Safety relief valve setting |
8,6 PSI |
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Maximum differential pressure and safety valve setting tolerance |
0.1 PSI |
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Outflow valve closure |
15000ft |
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maximum cabin alt selection |
14000ft |
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cab alt warning |
9550ft +- 350ft |
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cab alt warning |
9550ft +- 350ft |
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max norm cab alt |
8000ft |
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autopilot at take off |
100ft or 5s |
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autopilot at landing NON PREC APP F-LOC F-G/S |
200ft AGL |
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autopilot at landing NON PREC APP V/S TRK FPA HDG V/S |
250ft AGL |
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autopilot at landing Circling |
500ft AGL for cat C 600ft AGL for cat D |
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autopilot at landing ILS cat1 |
160ft AGL |
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autopilot at landing ILS cat 2 cat 3 |
0ft AGL if Autoland |
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Autopilot after manual go around |
100ft AGL |
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min DH for cat 2 ILS |
100ft AGL |
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min DH for Cat 3 ILS fail passive (single) |
50ft |
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min DH for Cat 3 ILS fail passive (single) |
50ft |
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min alert height for ILS cat 3 fail operational |
100ft AGL |
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min DH for Cat 3 ILS fail passive (single) |
50ft |
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min alert height for ILS cat 3 fail operational |
100ft AGL |
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min RVR for cat 3 without DH |
75m |
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max headwind for ILS cat 2 cat 3 |
30kt |
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max headwind for ILS cat 2 cat 3 |
30kt |
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max tailwind for ILS cat 2 cat 3 |
10kt |
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max crosswind for ILS cat 2 cat 3 |
20 kt |
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autoland in config |
conf 3 conf full |
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autoland G/S angle |
-2.5• to -3.15• |
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autoland max altitide |
9200ft |
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autoland min altitude |
-1000ft |
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APU start sequence |
after 3 start attempt wait 60 min |
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Max APU N speed |
107% |
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max APU start EGT below 35000ft |
1090•C |
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Max APU start EGT above 35000ft |
1120•C |
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Max APU running EGT |
675•C |
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max APU operation and normal restart limit |
41000ft |
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max APU operation and normal restart limit |
41000ft |
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APU supplying bleed air and electrical power max alt |
22500ft |
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max APU operation and normal restart limit |
41000ft |
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APU supplying bleed air and electrical power max alt |
22500ft |
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APU battery restart limit (elec emer config) |
25000ft |
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max APU operation and normal restart limit |
41000ft |
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APU supplying bleed air and electrical power max alt |
22500ft |
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APU battery restart limit (elec emer config) |
25000ft |
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APU ground operation limits min and max alt |
-2000ft to 14500ft |
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APU max alt to assist engine start |
20000ft |
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APU max alt to assist engine start |
20000ft |
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APU max alt for air conditioning and pressurization SINGLE pack opeartion |
22500ft |
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APU max alt for air conditioning and pressurization DUAL pack operation |
15000ft |
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APU Bleed for wing anti ice |
NOT permitted |
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max EGT for take off and go around |
635•C for 5 min (10min for OEI) |
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EGT MCT |
610•C |
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EGT starting |
635•C |
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max N1 and N2 |
100% |
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max continuous oil temperature |
155•C |
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max continuous oil temperature |
155•C |
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max transient oil temperature (15min) |
165•C |
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minimum starting oil temp |
-40•C |
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min oil temp before IDLE is exceeded |
-10•C |
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min oil temp before take ofd |
50•C |
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min oil pressure |
60 PSI |
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max reverse max speed |
70 kt |
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max reverse max speed |
70 kt |
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idle reverse max speed |
0 kt |
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max flex temp |
ISA + 55•C |
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max crosswind for engine start |
35 kt |
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max alt flaps extended |
20000ft |
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min JETA1 temp |
-43•C |
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min JETA1 temp |
-43•C |
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max JETA1 temp |
54•C |
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fuel imbalance at TAKE OFF inner tanks |
if heavier tank is FULL—>500kg 3000kg—> 1050kg 1450kg—>1450kg |
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fuel imbalance at TAKE OFF inner tanks |
if heavier tank is FULL—>500kg 3000kg—> 1050kg 1450kg—>1450kg |
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fuel imbalance IN FLIGHT and LANDING |
if heavier tank is full—> 1500kg 4300kg—> 1600kg 2250kg —> 2250kg |
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min fuel for take off |
1500kg |
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max inner tank quantity |
5420kg x2 |
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max brake temp for take off |
300•C (150•C with brake fans ON) |
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nose wheel steering tow bar less operation max NWS angle |
85• |
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nose wheel steering tow bar less operation max NWS angle |
85• |
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max taxi speed in a turn with one tire deflated |
7kt |
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nose wheel steering tow bar less operation max NWS angle |
85• |
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max taxi speed in a turn with one tire deflated |
7kt |
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max taxi speed in a turn if two tires deflated on the same grar |
3 kt |
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max NWS angle with deflated tire |
30• |
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IR ground alignment between latitudes |
73 north 73 south |
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if all ADIRUs have the same magnetic variation will provide reference between latitudes |
73 north and 60 south |
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for ground starts a ___s pause is required between successive cycles |
15 (seconds) |
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a ____ min cooling period is required, subsequent to ___ failed cycles or ___ min of continuous crank |
30 (minutes) 3 (failed cycles) 5 (min of cont crank) |
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autopilot usage in all other phases |
500 ft AGL |
