ATPL (A)
Review Worksheets
033 FLIGHT PLANNING
& MONITORING
BY KDMN
2020
, I/VFR NAVIGATION
01 RADIO NAVIGATION CHART
a) RESTRICTED AIRSPACES:
➔ P area: strictly prohibited to air traffic.
➔ R area: restricted area, subject to certain condition.
➔ D area: danger area.
b) MINIMUM HEIGHT:
➔ Over high-density area: 1000ft above the highest obstacle in a 600m radius around the a/c.
➔ Otherwise, 500 ft above ground level or water level.
c) MINIMUM SAFE ALTITUDE MSA:
➔ If obstacle height ≤ 5000ft -> obstacle clearance is 1000ft.
➔ If obstacle height > 5000ft -> obstacle clearance is 2000ft.
➔ Shown by a magenta color on chart: 43=4300ft, within a rectangle.
➔ On VAC, MSA is represented by (upper right corner on the VAC chart):
d) ALTITUDE CORRECTION:
➔ From pressure: 1 HPa=28 ft or 30ft.
Ex1: Aerodrome Altitude = 2000 ft, QNH = 993. Δ(HPa) = 1013 – 993 = 20. Δ(ft)= 600ft -> PA =
2000 + 300 = 2600ft.
Ex2: Aerodrome Altitude = 2000ft QNH = 1023. Δ(HPa) = 1013 – 1023 = -10. Δ(ft)= -300ft ->
PA = 2000 - 300 = 1700ft.
To know if you have to add/subtract Δ(HPa), draw a schema knowing that pressure decreases
with altitude.
PA = 2600ft 2000ft
QNH = 993
1013
Review Worksheets
033 FLIGHT PLANNING
& MONITORING
BY KDMN
2020
, I/VFR NAVIGATION
01 RADIO NAVIGATION CHART
a) RESTRICTED AIRSPACES:
➔ P area: strictly prohibited to air traffic.
➔ R area: restricted area, subject to certain condition.
➔ D area: danger area.
b) MINIMUM HEIGHT:
➔ Over high-density area: 1000ft above the highest obstacle in a 600m radius around the a/c.
➔ Otherwise, 500 ft above ground level or water level.
c) MINIMUM SAFE ALTITUDE MSA:
➔ If obstacle height ≤ 5000ft -> obstacle clearance is 1000ft.
➔ If obstacle height > 5000ft -> obstacle clearance is 2000ft.
➔ Shown by a magenta color on chart: 43=4300ft, within a rectangle.
➔ On VAC, MSA is represented by (upper right corner on the VAC chart):
d) ALTITUDE CORRECTION:
➔ From pressure: 1 HPa=28 ft or 30ft.
Ex1: Aerodrome Altitude = 2000 ft, QNH = 993. Δ(HPa) = 1013 – 993 = 20. Δ(ft)= 600ft -> PA =
2000 + 300 = 2600ft.
Ex2: Aerodrome Altitude = 2000ft QNH = 1023. Δ(HPa) = 1013 – 1023 = -10. Δ(ft)= -300ft ->
PA = 2000 - 300 = 1700ft.
To know if you have to add/subtract Δ(HPa), draw a schema knowing that pressure decreases
with altitude.
PA = 2600ft 2000ft
QNH = 993
1013