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25 Cards in this Set
- Front
- Back
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Maximum Limit Load Factors
- Flaps/slats Retracted? - Flaps and Slats extended? - Flaps retracted / slats extended? |
- Flaps / Slats retracted
+2.5g to -1.0g - Flaps and Slats extended? +2.0g to 0g - Flaps retracted / Slats extended? +2.0g to 0g |
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Max Ramp Weight?
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53,977 Kg
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Max T/O Weight?
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53,524 Kg
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Max Landing Weight?
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49,895 Kg
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Max ZFW?
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45,586 Kg
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Runway Slope Limitations?
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+1.7% to -2.0%
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Limiting tailwind component for T/O?
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10 kts
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Engine T/O wind limitations?
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Crosswind is 40kts
For components greater than 40kts crosswind and 10kts tailwind only taxi is permitted and N1 limited to 50% |
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Vmo?
Mmo? |
340 kts below 26,000 ft
0.82 M above 26,00 ft |
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Flaps / Slats Maximum Speeds:
Max Mach No? Flap Angle with slats extended: 0? 0 to 10? 10.1 to 20? 20.1 to 25? 25.1 to 40? |
Max Mach = 0.57
0 = 280 kts 0 to 10 = 280 kts 10.1 to 20 = 240 kts 20.1 to 25 = 220 kts 25.1 to 40 = 200 kts |
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Gear Down Speeds:
Max Mach No? Gear Retraction? Gear Extension? Gear Extended? |
Max Mach No = 0.70
Gear Retraction = 250 kts Gear Extension = 300 kts Gear Extended = 300 kts |
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Under what weather conditions are reduced thrust T/O's not permitted?
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When the runway is contaminated with: Standing water
Loose snow Slush Compacted snow or wet ice |
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Under what aircraft conditions are reduced thrust T/O's not permitted?
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When items affecting performance cause an increase in crew workload.
Example: Inop engine gauges Anti-skid (additional performane requirements Any situation requiring a non-standard T/O technique |
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Maximum Cabin Differential pressure?
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7.86 psi
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Maximum emergency relief pressure?
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8.27 psi
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Autoland wind component limitations?
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Headwind 25 kts
Tailwind 10 kts Crosswind 15 kts |
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During an autoland what RA must "ALIGN" be annunciated on FMA
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100 ft RA
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Can an autoland be conducted if "RUDDER PWR OFF" alert is displayed?
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No
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How long can the "STAB OUT OF TRIM" alert be displayed for an autoland?
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3 Seconds
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Can the FMS performance predictions be used for:
Range calculations Fuel management Engine out terrain clearance? |
No, it has not been demonstrated so therefore AFM must be used.
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When using an ILS with failed glideslope indications when must the use of PROF be discontinued?
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By the FAF
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When can the GPWS alert be switched to OVRD to avoid any unwanted alerts?
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- Flap below landing flap
- When landing at an airport not contained in the database - When the FMS NAV mode is in IRS ONLY NAVIGATION and the aircraft is over land |
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When can APU AIR not be used?
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T/O and inflight operations
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What is the APU starter motor duty cycle?
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3 start attempts then wait 30 mins before subsequent starts.
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What is the APU maximum EGT and maximum rotor speed?
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EGT - 100%
Rotor speed - 105% |
