Procedures

Question 1

Wind correction for approach speed is calculated by:

Answer 1

Vref + 1/2 steady wind + all gust

maximum is +20 KIAS

Question 2

The crew must confirm that the auto throttles have achieved the required takeoff thrust setting prior to ___ KIAS. At the point, the ATS mode changes to ___ until ___ ft radio altitude.

Answer 2

80 KIAS
N1 HOLD
320 ft

Question 3

The RETARD mode of the auto throttles is activated upon reaching ___ feet radar altitude.

This function is only available when the flaps are at ___ deg. For landings with flaps NOT at ___ deg, the pilot must ___.

Answer 3

50 feet

45 deg

45 deg; pilot must disengage ATS prior to landing flare

Question 4

Prior to conducting an ILS or localizer approach, select PFD format to ___ in order to preview the localizer and glideslope.

Answer 4

ROSE

Question 5

Takeoff power must be set within ____ feet of runway threshold.

Answer 5

1000

Question 6

A performance takeoff (static) is required whenever takeoff distance available is less than ___.

Answer 6

the takeoff distance required plus 1000 ft

Question 7

Authothrottle equipped aircraft should select TOGA only when ___ to prevent premature takeoff power application.

Answer 7

taxiing into takeoff position

Question 8

During takeoff/departure, flaps should be selected to 0 deg once the aircraft is above ___ feet and a minimum of ___ minus ___ knots.

Answer 8

400 feet AGL; Vfto - 5 its

Question 9

The minimum altitude to select autopilot ON after takeoff is ___ feet AGL

Answer 9

320

Question 10

A RWY approach will be indicated in the FMS by ___ on the FMS legs page. The approach may have minimums based on ___ or just ___. In either case a VNAV approach ___ (may/may not) be conducted to minimums.

In this case the glide path is calculated from 50 feet above the runway threshold to the FAF altitude at an angle of approx ___ degrees. This will guarantee obstacle clearance from the FAF to the MAP.

Answer 10

letter RWY abeam the RWY fix on the LEGS page

LNAV/VNAV (DA) or just LNAV (MDA)

May

3 deg

Question 11

The normal configuration for a circling approach is ___.

Answer 11

gear down, flaps 30, speed 150KIAS

Question 12

For circling approaches use category ___ minima which gives ___ miles protected airspace (FAA only and before change to align with Europe).

Answer 12

D; 2.3nm

Question 13

With the autopilot engage, turning the HDG knob generates 27 deg of bank and results in ___ nm turn diameter at 150 KIAS.

Answer 13

1.3 nm