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Lernkarten
350 ft for each
>20 full-time employees
Longitude difference / 2 x sin average latitude
NPA RVR/VIS + 1000 m, ceiling at or above MDH + 200 ft
0200-0559
To reduce aircraft weight in an emergency unless capable of 2.7% climb with OEI and 3.2% with all engines
After 2008: 1 auto ELT; before 2008: 1 ELT of any type
VAT = VSO x 1.3
>5700 kg
3 hours
15000 ft
Operational need
CAT I RVR
Even FLs between FL285 and FL420
Circling visibility, MDH & ceiling for ETA +/- 1 hour
Physically affected at 6000 ft; crew efficiency not impaired at 8000 ft
15 min same track & same Mach; 10 min with Mach number technique; 5 min absolute minimum/leading aircraft higher speed
MCTOM >5700 kg & MOPSC >19
Conversion angle = Earth convergence / 2
Headwind/tailwind x 2; at centre = 0
GTAP NH, TGAP SH
ICAO Doc 7030
15° x h x sin Lm
V2 + 10 kt until 800 ft, thrust reduction to climb power, then VZF + 10 kt until 3000 ft
Below 2500 ft or under 1500 ft (under 500 m or 0 to 150 m)
Turbine: 45 min; reciprocating: 30 min at 1500 ft above aerodrome
At or above FL60 or 2000 ft above ground, whichever is greater
Flight crew can fly at 10000 ft without supplemental oxygen with no time limit; all crew above 13000 ft; 100% of passengers for entire flight above 15000 ft, but not less than 10 min
Friction measurement: H) X/X/X [5-4-3-2-1]; contamination: F) X/X/X
Provided a report is sent to the AUTHORITY after flight
32000 ft
When 2 independent runways are available, weather conditions are 500 ft above MDA/2000 ft AAL, and visibility >5 km
Change of longitude x sin mean latitude
0: 300 m (1000 ft); >900 m and <1500 m: 450 m (1476 ft); >1500 m: 600 m (1969 ft)
Westbound day: 1130-1900 UTC; eastbound night: 0100-0800 UTC; 1901-0059 and 0801-1129 UTC are outside validity
AIP ENR 5.6
800 m
3 minutes
Best above FL60; within 15 minutes
If the threshold is more than 2 m below aerodrome elevation