032.02 + .03 CS-23/APPLICABLE OPERATIONAL REQUIREMENTS PERFORMANCE CLASS B

Question 1

V_REF for CS-23 aircraft is (V_S0/V_MCA) • (…).

Answer 1

V_REF for CS-23 aircraft is (V_S0) • (1.30).

- for CS-25 it is V_S0 • 1.23 -

Question 2

Screen height for a performance class B aircraft landing on a wet runway is (…) ft.

Answer 2

Screen height for a performance class B aircraft landing on a wet runway is (50) ft.

- all class B screen heights are 50 ft -

Question 3

If not stated in the AFM, the factor applied for a Class B aeroplane taking-off on a runway with short grass is (…).

Answer 3

Take-off distance required = take-off distance • 1.25 (for commercial operations)

Dry grass runway → • 1.2

Wet grass runway → • 1.3

Wet paved runway → • 1.0 (so nothing…)

Slope → • 1.05 for every % upslope (no decrease for downlope!)

Question 4

If not stated in the AFM, the factor applied for a Class B aeroplane landing on a runway with short grass is (…).

Answer 4

Landing distance required = landing distance • 1.43

Grass runway → • 1.15

Wet runway → • 1.15

Slope → • 1.05 for every % downslope (no decrease for upslope!)

Question 5

If not stated in the AFM, the factor applied for a Class B aeroplane landing on a wet runway is (…).

Answer 5

Landing distance required = landing distance • 1.43

Grass runway → • 1.15

Wet runway → • 1.15

Slope → • 1.05 for every % downslope (no decrease for upslope!)

Question 6

If not stated in the AFM, the factor applied for a Class B aeroplane landing on a runway with 1% downslope is (…).

Answer 6

Landing distance required = landing distance • 1.43

Grass runway → • 1.15

Wet runway → • 1.15

Slope → • 1.05 for every % downslope (no decrease for upslope!)

Question 7

If not stated in the AFM, the factor applied for a Class B aeroplane landing on a runway with 1% upslope is (…).

Answer 7

Landing distance required = landing distance • 1.43

Grass runway → • 1.15

Wet runway → • 1.15

Slope → • 1.05 for every % downslope (no decrease for upslope! No factor for this question)

Question 8

If not stated in the AFM, the factor applied for a Class B aeroplane taking-off on a runway with wet grass is (…).

Answer 8

Take-off distance required = take-off distance • 1.25 (for commercial operations)

Dry grass runway → • 1.2

Wet grass runway → • 1.3

Wet paved runway → • 1.0 (so nothing…)

Slope → • 1.05 for every % upslope (no decrease for downslope!)

Question 9

If not stated in the AFM, the factor applied for a Class B aeroplane taking-off on a wet paved runway is (…).

Answer 9

Take-off distance required = take-off distance • 1.25 (for commercial operations)

Dry grass runway → • 1.2

Wet grass runway → • 1.3

Wet paved runway → • 1.0 (so nothing…)

Slope → • 1.05 for every % upslope (no decrease for downslope!)

Question 10

If not stated in the AFM, the factor applied for a Class B aeroplane taking-off on a runway with 1% upslope is (…).

Answer 10

Take-off distance required = take-off distance • 1.25 (for commercial operations)

Dry grass runway → • 1.2

Wet grass runway → • 1.3

Wet paved runway → • 1.0 (so nothing…)

Slope → • 1.05 for every % upslope (no decrease for downslope!)

Question 11

If not stated in the AFM, the factor applied for a Class B aeroplane taking-off on a runway with 1% downslope is (…).

Answer 11

Take-off distance required = take-off distance • 1.25 (for commercial operations)

Dry grass runway → • 1.2

Wet grass runway → • 1.3

Wet paved runway → • 1.0 (so nothing…)

Slope → • 1.05 for every % upslope (no decrease for downslope!)

Question 12

The mininum speed at 50 ft above take-off surface level for multi-engine CS-23 aircraft must not be less than the (lowest/highest) of:

I) A speed that is shown to be safe for continued flight; or

II) (…) V_MC; or

III) (…) V_S1.

Answer 12

The mininum speed at 50 ft above take-off surface level for multi-engine CS-23 aircraft must not be less than the (highest) of:

I) A speed that is shown to be safe for continued flight; or

II) (1.10) V_MC; or

III) (1.20) V_S1.

Question 13

The mininum speed at 50 ft above take-off surface level for single-engine CS-23 aircraft must not be less than the (lowest/highest) of:

I) A speed that is shown to be safe for continued flight; or

II) (…) V_S1.

Answer 13

The mininum speed at 50 ft above take-off surface level for single-engine CS-23 aircraft must not be less than the (highest) of:

I) A speed that is shown to be safe for continued flight; or

II) (1.20) V_S1.

Question 14

For a CS-23 aircraft, reference landing approach speed (V_REF) must not be less than the (lesser/greater) of:

• V_MC with wing flaps (retracted/ in most extended take-off setting); and
• (…) • V_S0

Answer 14

For a CS-23 aircraft, reference landing approach speed (V_REF) must not be less than the (greater) of:

• V_MC with wing flaps (in most extended take-off setting); and
• (1.3) • V_S0

Question 15

The take-flight path of a Class B aircraft begins (…) ft above surface at end of TODR and ends at a height of (…) ft above the surface. Maximum bank before the aeroplane has reached the screen height is (…)°, therafter the angle of bank does not exceed (…)°.

Answer 15

The take-flight path of a Class B aircraft begins (50) ft above surface at end of TODR and ends at a height of (1 500) ft above the surface. Maximum bank before the aeroplane has reached the screen height is (0)°, therafter the angle of bank does not exceed (15)°.

Question 16

Regulatory minimum vertical clearance between a Class B aircraft and an obstacle is (…) ft.

Answer 16

Regulatory minimum vertical clearance between a Class B aircraft and an obstacle is (50) ft.

- 35 ft for Class A -

Question 17

For a performance class B aircraft, the actual landing distance on a dry runway shall be less than (…) • LDA.

Answer 17

For a performance class B aircraft, the actual landing distance on a dry runway shall be less than (0.7) • LDA.

- 0.6 • LDA for Class A -

Question 18

For a multi-engine performance class B aircraft used for commercial air transport, the take-off distance calculations must take into account not more than (…)% of the headwind component and not less than (…)% of the tailwind component.

Answer 18

For a multi-engine performance class B aircraft used for commercial air transport, the take-off distance calculations must take into account not more than (50)% of the headwind component and not less than (150)% of the tailwind component.

Question 19

The thrust of a fixed-pitch proppeler (increases/decreases) while the aeroplane speed builds up during take-off run.

Answer 19

The thrust of a fixed-pitch proppeler (decreases) while the aeroplane speed builds up during take-off run.

Question 20

For take-off climb performance (calculate obstacle avoidance questions), climb starts of TODR end height → (…) ft. The factor to be applied to the “all-engine climb gradient” is (…). When visual reference is lost (when reaching cloud base), (…) ROC should be used.

Answer 20

For take-off climb performance (calculate obstacle avoidance questions), climb starts of TODR end height → (50) ft. The factor to be applied to the “all-engine climb gradient” is (0.77). When visual reference is lost (when reaching cloud base), (OEI) ROC should be used.

Question 21

The minimum rate of climb for a performance class B aircraft is (100/300/500/1000) ft/min with all (all engines operating/OEI) (and the others) operating at maximum continuous power.

Answer 21

The minimum rate of climb for a performance class B aircraft is (300) ft/min with all (all engines operating) operating at maximum continuous power.