Start - Taxi - Takeoff - Climb

Question 1

Preflight

Prior to APU start, wait ______________?

Answer 1

Prior to APU start, wait 15 seconds after the left CCR is online.

Question 2

Preflight

Left CCR online is indicated by

Answer 2

the Captain’s inboard and lower display unit

showing the default formats

Question 3

Both pilots will use the HUD (if operative) during all approaches when the visibility is less than

Answer 3

4000 RVR (1200m) or 3/4 mile visibility. The HUD is
recommended for all takeoffs and landings.

Question 4

One pilot must have VSD displayed when

Answer 4

for takeoff, landing and all other flight operations below 10,000 AFL. Use of VSD is recommended for all flight
operations.

Question 5

Autothrottle Use

Answer 5

Autothrottle use is recommended during all phases of flight. When in manual flight,
autothrottle use is also recommended, however manual thrust control may be used
to maintain pilot proficiency.

Question 6

Preflight

IRS selectors If already ON,

Answer 6

OFF 30 seconds, then ON.

Verify that the ON BAT Light is extinguished.

Question 7

Verify that the following are sufficient for flight:
• Oxygen Pressure
- ETOPS-
- Non-ETOPS-
• Hydraulic quantity
• Engine oil quantity

Answer 7

• Oxygen Pressure
- ETOPS-Minimum bottle pressure is 1250 psi at 70°F
- Non-ETOPS-Minimum pressure is 800psi at 70°F
• Hydraulic quantity
- RF or OF not displayed
• Engine oil quantity
- 20 quarts (min)

Question 8

The MAIN BATTERY LOW message

Answer 8

The MAIN BATTERY LOW message can show when power is established.
The main battery is charging and when the battery charge is sufficient for
takeoff, the message blanks.

Question 9

Simultaneous engine start is only allowed when

Answer 9

the APU is running and both

APU starter generators are operational.

Question 10

Autostart monitors for:

Answer 10

• Loss of both starters
• No N1 Rotation
• No oil pressure rise
If any of these occur, the EEC aborts the autostart and the message ENG AUTOSTART L, R displays.

Question 11

Autostart corrects for:

Answer 11

• High residual EGT
• Hot start
• No EGT rise
• Loss of one starter
• Start duty cycle exceedance
• Compressor stall
• Hung start

Question 12

If the EEC is unable to correct for a hung start or compressor stall,

Answer 12

EEC cancels the autostart and the EICAS message ENG AUTOSTART L, R displays.

Question 13

There is a limit of ___ start attempts on the ground.

Answer 13

3

Question 14

Accommodating “Last Minute” Baggage / Cargo

Answer 14

late loading of baggage / cargo will be accomplished with both engines shut down.

Question 15

Accommodating “Last Minute” Passengers after Engines Start

Answer 15

Shut down both engines prior to boarding passengers.

Question 16

Authorized flap settings for takeoff are

Answer 16

(-8) 5, 15 or 20.

(-9) 5, 10, 15, 17 or 20.

Question 17

Before Takeoff
Engine warm up requirements
Engine warm up recommendations:

Answer 17

Engine warm up requirements:
• Engine oil temperature must be above the bottom of the temperature scale.
Engine warm up recommendations:
• Run the engines for at least 3 minutes.
• Use a thrust setting normally used for taxi operations.

Question 18

Taxi Wind Limits

Answer 18

For taxi with crosswinds greater than 35 knots, limit thrust to 45% N1.

Question 19

Single Engine Taxi

Answer 19

Single engine taxi prior to takeoff is not authorized except in an emergency.

Question 20

Normal taxi speed is

Answer 20

approximately 20 knots, adjusted for conditions. On long straight taxi routes, up to 30 knots are acceptable, On a dry surface, approximately 10 knots for turn angles greater than typically required for high speed runway turnoffs.

Question 21

Carbon Brake Life

Answer 21

Brake wear is primarily dependent upon the number of brake applications. For example, one firm brake application causes less wear than several light
applications.

Question 22

Takeoff Terrain Display

Answer 22

One pilot shall have Terrain Display selected, unless weather conditions require
both pilots to display weather.

Question 23

Prior to Low Visibility Takeoffs

Answer 23

Prior to low visibility takeoffs with the HUD (RVR < 500), the Captain will make a
PA in conjunction with the Prepare for Takeoff PA.

Question 24

HUD Low Visibility Takeoff
General
Lighting

Answer 24

The runway must be CAT III operations.
Use of these procedures is required with less than 500 RVR (150m) on runways supported by 300 RVR (75m) takeoff (see Jepp 10-9A page). Requires any two of
following three transmissometers. All reporting transmissometers are controlling.
• Touchdown: 300 RVR (75m)
• Mid-field: 300 RVR (75m)
• Roll-out: 300 RVR (75m)
• Access to runway requires use of taxiway centerline lighting that meets US orICAO CAT III criteria.
• Operative HIRL.
• Operative runway CL lights.

Question 25

HUD Low Visibility Takeoff Wind Minimum Aircraft Equipment

Answer 25

Headwind. 25 kts Tailwind. 15 kts Crosswind. 15kts • HUD system • 2 windshield wipers • 2 ILS receivers

Question 26

LNAV may be armed ____________and will become active _______.

Answer 26

LNAV may be armed on the ground and will become active at 50 feet AGL.

Question 27

the FMC automatically selects the EO SID as a route modification:

Answer 27

During Takeoff: | If an engine failure occurs prior to flap retraction

Question 28

The APU battery is designed to support _____ start attempts.

Answer 28

two consecutive start attempts.

Question 29

If the APU fails to start after the second attempt

Answer 29

a 5 minute cooling period must be observed before a third attempt is made.

Question 30

• Oxygen Pressure - ETOPS- - Non-ETOPS-

Answer 30

- ETOPS-Minimum bottle pressure is 1250 psi at 70°F (bottle temp). - Non-ETOPS-Minimum bottle pressure is 800psi at 70°F (bottle temp.)

Question 31

Flight deck door access system “CHECK”

Answer 31

Flight deck door- Open Flight deck door access selector - AUTO Flight deck door power switch - OFF At least 20 seconds after the switch is selected to OFF, verify FD DOOR LOCK FAIL EICAS advisory message shows. Flight deck door power switch - ON Verify FD DOOR LOCK FAIL EICAS advisory message blanks. Emergency access code - Enter Digits ENT key - Push Verify FD DOOR AUTO UNLOCK EICAS warning message shows, master WARNING lights are on, and aural alert sounds. Flight deck door access selector - DENY Verify FD DOOR AUTO UNLOCK EICAS warning message blanks. Flight deck door access selector - UNLKD Flight deck door power switch - OFF

Question 32

FMC: | • ENGINES [ 1R ]

Answer 32

– Check Displays GENX-1B70 @ 69,800 lbs thrust | 787-9 GEnx-1B70/75 @ 74,100 lbs thrust

Question 33

Before connecting ground air conditioning cart:

Answer 33

• PACK switches (both) – Off (*Packs can be damaged if running w/PCA) Allows maximum efficiency. • LOWER RECIRC FAN switch – Off Allows maximum efficiency and protects lower recirculation fan.

Question 34

Ensure the “________________” EICAS is displayed beforepressurizing hydraulics.

Answer 34

“STEERING LOCKED OUT” EICAS

Question 35

When both of the following exist, do an engine run-up to minimize ice build-up:

Answer 35

* OAT is 3°C or below * visible moisture (clouds, fog with visibility of one statute mile [1600 m] or less, rain, snow, sleet, ice crystals, and so on)

Question 36

Icing conditions engine run up is

Answer 36

• Run-up to a minimum of 40% N1 for at least 5 seconds duration at intervals no greater than 60 minutes. • If high engine vibration indications occur, a run-up to 50% N1 may be done.

Question 37

If takeoff is not completed within __________, manually de-ice the engines before takeoff.

Answer 37

120 minutes total taxi time

Question 38

If a change in HUD TAKEOFF runway is needed,

Answer 38

select both flight director switches OFF. After the new runway is executed on the CDU, select the flight director switches back to ON.

Question 39

For takeoff, set stabilizer trim to

Answer 39

FMC computed value.

Question 40

When engine anti-ice is required and the OAT is 3°C or below, the takeoff must be preceded by a static engine run-up. Use the following procedure:

Answer 40

Increase thrust to a minimum of 40% N1 up to 55% N1 maximum. Maintain that thrust level for 5 seconds minimum. If high fan vibrations persist, increase thrust to a minimum of 50% N1 up to 55% N1 maximum and maintain that thrust until vibration decreases to below 4 units before proceeding with the takeoff. Confirm stable engine operation prior to final advance to takeoff thrust.

Question 41

The autopilot must not be engaged below a minimum engage altitude of _____ after takeoff.

Answer 41

200 feet AGL

Question 42

Maximum Takeoff and Landing Tailwind Component - Maximum Crosswind

Answer 42

15 knots. 787-8 - 40 kts. 787-9 - 33 kts

Question 43

If Economy Climb Schedule - FMC Data Unavailable:

Answer 43

* 250 knots/VREF 30 + 80 knots, whichever is higher- Below 10,000 feet * 320 knots/0.85M - Above 10,000 feet

Question 44

APP mode should not be selected until:

Answer 44

* the ILS is tuned and identified * the airplane is on an inbound intercept heading * both localizer and glide slope pointers appear on the attitude display in the proper position * clearance for the approach has been received

Question 45

FAA Holding Speeds

Answer 45

To 6,000 200kts to 14,000 230kts, may be restricted to 210 above 14,000 265 kts and 1-1/2 mins

Question 46

ICAO Holding Speeds

Answer 46

Thru 14,000 230 kts to 20,000 240 kts to 34,000 265 kts above FL340 .83 M

Question 47

Events Requiring Maintenance Inspection

Answer 47

* hard landing (identify if the hard landing is suspected on the main gear, the nose gear, or both) * severe turbulence * overspeed - flap/slat, MMO/VMO, landing gear, landing gear tires * rejected takeoff * lightning strike * extreme dust * tail strike * overweight landing * any event that the pilot feels a maintenance inspection could be needed.

Question 48

787-8 Fuel Capacity

Answer 48

Left Main 37,319 Right Main 37,319 Center 148,740 Total 223,378

Question 49

787-9 Fuel Capacity

Answer 49

Left Main 36,984 Right Main 36,984 Center 149,678 Total 223,646