B-777

Question 0

When must the captain make the landing?

Answer 0

• CAT II/III approaches
• Reduced vis approaches requiring use of HUD
• Cat I with High Mins Captain

Question 1

Stabilized Approach Criteria

Answer 1

• final landing configuration
• all briefings & checklists complete
• descent angle & rate are appropriate for type of approach being flown (all available landing aids ILS,VASI,PAPI, etc must be used)
• vertical and lateral displacement from normal approach path is in accordance with CFM tolerances
• sink rate no greater than 1000 FPM and if an approach requires greater, a special briefing shall be conducted
• airspeed Vapp or target with a variance no greater than +10 and no less than -5 kts. momentary and minor deviations are only tolerated if immediate corrections are made
• as airplane crosses runway threshold it should be on target airspeed within +5 kts and positioned to make a normal landing

Question 2

When is autoland required?

Answer 2

All Cat II/III approaches

Question 3

When is a Coupled Approach required?

Answer 3

-All non-ILS until adequate visual reference is acquired
-All Cat II/III Approaches
-Cat I High-mins Captains
* Recommended Cat I < 3/4 (4000RVR/1200M)
or Cat I < 2400RVR/600m but use of FD,AP, or HUD to DA is required

Question 4

Define the Decision Region and it’s tolerances

Answer 4

It’s between 500ft above TDZE and touchdown

• Maximum localizer deviation is 1/3 of a dot
• Maximum glideslope deviation is 1/2 of a dot
• No sustained oscillations about the localizer or the glideslope are allowed

Question 5

Max Ramp weight

Answer 5

768,000LBS

Question 6

Max T/O weight

Answer 6

766,000LBS

Question 7

Max Landing weight

Answer 7

575,000LBS

Question 8

Zero Fuel weight

Answer 8

547,000LBS

Question 9

What is an acceptable CG range at any weight?

Answer 9

21.9% to 29.2%

With a max range of 14% to 44%

Question 10

Taxi Speeds:
Normal____
Long/straight____
Turns/dry surface____

Answer 10

20kts
30kts
10kts

Question 11

Turbulent Air Penetration Speed
Below 25,000ft____
25,000ft and above____*

Answer 11

270kts
280kts or .82 whichever is lower
*maintain a minimum of 15kts above min maneuver speed at all altitudes when airspeed is below .82 Mach

Question 12

Normal Crosswind Limits:
T/O & Landing____
Autoland____
Autoland Cat II/Cat III____

Answer 12

38kts
25kts
15kts

Question 13

Crosswind limits with braking action reports:
Good to medium braking____
Medium to poor braking____
Poor braking____

Answer 13

35kts
20kts
17kts

Question 14

Max tailwind limit for:

T/O, Landing, or Autoland____

Answer 14

10kts

Question 15

Max Headwind for an Autoland____

Answer 15

25kts

Question 16

Rwy slope ____%

Answer 16

+/- 2%

Question 17

Max T/O & Landing altitude____

Max field elevation____

Answer 17

9,800ft

9,650ft

Question 18

Max operating altitude____

Answer 18

43,100ft

Question 19

Icing Conditions are considered to exist when:

Answer 19

OAT on the ground, for takeoff, or TAT in flight is 10°C or below and visible moisture in any form is present.

Question 20

Visible moisture is defined as:

Answer 20

A form of precipitation such as clouds or fog with visibility of 1 mile or less rain, snow, sleet, or ice crystals.
OAT is 10°C or below when operating on ramps taxiways or runways where surface snow, ice, standing water, or slush maybe ingested.

Question 21

Autopilot must be disengaged below____ft AGL without LAND2 or LAND3 Annunciated

Answer 21

200ft

Question 22

Cat II/III approaches are not authorized with any of the following EICAS msgs displayed:

Answer 22

SGL Source Displays
SGL Source RAD ALT
Single Source ILS

Question 23

To Autoland you must see _____

And what msg can not be present on EICAS

Answer 23

Land2 or Land3

SLATS DRIVE

Question 24

Ground OPS require an engine run up to a minimum of ____% N1at intervals not to exceed ____ minutes when OAT is ____°C or below in icing conditions.

Answer 24

50%N1 60 minutes 3°C

Question 25

Do not extend flaps above ____ft

Answer 25

20,000ft

Question 26

Max Dif between Captain or First Officer Altimeter Display and Field Elevation is ____ft

Answer 26

75ft

Question 27

Fuel Capacity for Left or Right tank____LBS Center tank Capacity____LBS Total aircraft Fuel Capacity____LBS

Answer 27

73,130LBS each wing tank 193,759LBS Center tank 340,019LBS total capacity

Question 28

Use main tanks until in cruise flight if there's less than ____LBS in the Center tank

Answer 28

10,500LBS

Question 29

Fuel Balance Limits: When total in main tanks is greater than ___LBS ____LBS max between tanks When total in main tanks is equal to or less than ___LBS ____LBS max between tanks

Answer 29

``` 123,000LBS = 3,000LBS 90,000LBS = 4,500LBS ```

Question 30

Do not operate weather radar in a ____ or within ____ft of a fuel spill

Answer 30

Hangar | 50ft

Question 31

ABORTED ENGINE START L,R

Answer 31

Fuel Control Switch(Affected Side)....Cutoff

Question 32

CABIN ALTITUDE

Answer 32

Oxygen Masks.....On 100%

Question 33

DUAL ENGINE FAIL/STALL

Answer 33

Fuel Control Switches......Cutoff, then RUN | Ram Air Turbine Switch....Push and Hold for One Second

Question 34

ENG LIM/SURGE/STALL L,R

Answer 34

A/T ARM Switch(Affected Side)....Confirm Off Thrust Lever(Affected Side)..........Confirm -Retard until engine indications remain within appropriate limits or the thrust lever is at idle.

Question 35

STABILIZER

Answer 35

STAB CUTOUT Switches(Both).....Cutout | Do not exceed current airspeed

Question 36

SMOKE, FIRE, OR FUMES

Answer 36

Oxygen Masks.....On 100%

Question 37

WNDSHEAR ESCAPE MANEUVER AUTOMATIC FLIGHT Pilot Flying: 5 Items Pilot Monitoring: 2 Items

Answer 37

``` PF - press either TOGA switch - verify TO/GA mode annunciation - verify thrust advances to GA thrust - retract speedbrakes - monitor system performance Be prepared to disconnect autopilot and autothrottles PM - assure GA thrust - verify all required actions have been accomplished and call out any omissions ```

Question 38

WNDSHEAR ESCAPE MANEUVER MANUAL FLIGHT Pilot Flying: 6 Items Pilot Monitoring: 2 Items

Answer 38

PF - push either TO/GA switch - aggressively advanced throttles full forward (to mechanical stops) - disconnect autothrottles - simultaneously roll wings level and rotate toward initial pitch attitude of 15° - retract speedbrakes - follow flight director TO/GA guidance (if available) PM - assure throttles are full forward (to mechanical stops) -verify all required actions have been completed and call out any omissions

Question 39

Any excess of the following indicates the airplane is in windshear: 5 items

Answer 39

- 15 knots indicated airspeed - 500 FPM vertical speed - 5° pitch attitude - one dot displacement from the glideslope - unusual thrust lever position for a significant period of time