Procedures

Question 1

PREFLIGHT

Answer 1

1) Exterior Safety Inspection (FO or first arriving crew member)
2) Preliminary Flight Deck Procedure (CA or FO)
3) CDU Preflight Procedure (CA or FO)
4) Exterior Inspection (FO)
5) Flight Deck Procedure (CA)
6) Security Inspection (FO)
7) Upper Deck/Cockpit Procedure, Main Deck Procedure (FO)

Question 2

Max break away thrust

Answer 2

45% N1

Question 3

Taxi Speed recommendations

Answer 3

Normal taxi: 20 knts
Long straight routes: up to 30 knts
Turns: 10 knts

Question 4

CABIN ALTITUDE (Rapid Depressurization)

Answer 4

• Don O2 Maks
• Crew Communication Establish
• check cabin altitude and rate (packs on and outflow valves closed)
• IF cabin altitude is uncontrollable:
  
  • SUPRNMRY (PASS) OXY switch…. Push to ON … hold for 1 sec
• MAIN DECK SIGNALING switch (if installed) ……… Push
• descent to lowest safe altitude or 14,000’ (whichever is higher)
• TO DESCEND:
  
  • thrust lever idle
  • extend Speedbrakes
  • speed Vmo/Mmo
  • limit airspeed and avoid high loads if structural integrity in doubt

Question 5

ENG 1, 2, 3,4 AUTOSTART (Aborted Engine Start)

Answer 5

FUEL CONTROL switch (affected engine) ………..CUTOFF

Question 6

Switches requiring confirmation from both crew members

Answer 6

• ENG FIRE Switch
• IDG Disconnect
• Thrust Lever
• FUEL CONTROL Switch
• IRS Selector
• APU FIRE Switch
• CARGO FIRE Switch

Question 7

Engine Limit or Surge or Stall

Answer 7

Thrust Lever (affected engine)………Confirm…..Retard until engine indication stay within limits, or thrust lever is at idle

Question 8

IAS DISAGREE (Airspeed Unreliable)

Answer 8

Autopilot disengage switch………Push
A/T ARM switch…………………………OFF
F/D switches (both) ………………….OFF
Set gear up pitch altitude and thrust:
Flaps extended……………………10º and 90% N1
Flaps Up……………………………….4º and 80% N1

Question 9

FIRE ENG 1,2, 3, 4 (Engine Severe Damage or Separation)

Answer 9

Thrust Lever (affected engine)…………………………..Confirm ……….Idle
FUEL CONTROL switch (affected engine) ……….Confirm………..CUTOFF
Engine Fire Switch (affected engine)…………………Confirm………..Pull
IF the FIRE ENG message is shown:
Engine fire switch …………… Rotate to the stop and hold for 1 sec
IF after 30 seconds the FIRE ENG messages stays shown:
Engine fire switch………..Rotate to the other stop and hold for 1 sec

Question 10

Procedure “Immediate Action Items” on Quick Reference Checklist

Answer 10

• CABIN ALTITUDE (Rapid Depressurization)
• ENG 1, 2, 3, 4 AUTOSTART (Aborted Engine Start)
• Engine Limit or Surge or Stall
• IAS DISAGREE (Airspeed Unreliable)
• FIRE 1, 2, 3, 4 Engine Severe Damage or Separation
• Multiple Engine Flameout or Stall
• Evacuation

Question 11

When is a consequential checklist not required to be referenced

Answer 11

When there is a statement “Do not accomplish the following checklists”

Question 12

Noise Abatement Procedures

Answer 12

NAP1:
Thrust Reduction: 1,500’
Acceleration Height: 3,000’

NAP2:
Thrust Reduction: Flaps 5
Acceleration Height: 1,000’

Question 13

Flaps 30 approach speed (VREF 30 + wind) is above 167 knts

Answer 13

Use flaps 25 and VREF25

Question 14

What conditions void a TLR?

Answer 14

• performance related DDG item is missing
• OAT is greater than MT
• OAT is more than 10° below POAT
• actual TOW is great than MFPTW
• actual ZFW is great than OFP ZFW + 10,000 kg
• located in FCOM 1 Supp

Question 15

Guidelines for approach speed corrections

Answer 15

With auto-throttles disconnected:

• Add 1/2 steady state headwind + full gust factor
• max additive 20 knts

*plan to touchdown at Vref + gust factor

Non-normal checklist adjustment:
- non-normal Vref per checklist + wind correction (min 5 knts, max 20 knts)

Question 16

Engine Run up procedures

Answer 16

When OAT is 3ºC or below and anti-ice required

GE - run-up to min 60% N1 for 30 sec (interval no greater than 30 mins)

Question 17

Two Engine Inoperative

Answer 17

• Auto-throttle is inop
• consider fuel jettison
• No Autoland

LANDING GEAR DOWN IS COMMIT POINT

During Go-Around:

• Do not use TO/GA
• set flaps 20
• retract gear without delay
• Retract flaps to 1 (may require descent)
• climb at Vref 30+60 (approx 217 knts @ 300.0 kg)

For Landing:

• Flaps 10 @ glide slope alive
• Flaps 20 and Gear Down at G/S intercept
• Flaps 25 approaching 1,000’ and center rudder trim

Question 18

When complete “RECALL REVIEW”

Answer 18

• prior to accomplishing the approach briefing - PF
• completion of any NNC (Non-normal checklist) - PF
• request during checklist procedure flow - CA

Question 19

When to select APP

Answer 19

After:

• ILS tunes and identified
• on inbound intercept heading
• loc and g/s pointer appear
• clearance received

Question 20

Stabilized Approach Criteria

Answer 20

Prior to 1000’ AGL:

1) On Flight Path:
- sink rate no greater that 1000 fpm
- For ILS within 1-dot of LOC or GS
- For Non-ILS on VNAV Glide Path or VTK +/- 75’; within 1-dot lateral deviation or 1/2 RNP

2) Configured for Landing
- aircraft configured
- landing checklist complete

3) On Speed
- speed target
- thrust stabilized

Question 21

Engine Warm Up Requirements

Answer 21

GE, GEnx:

• Oil temp above bottom of temp scale
• 3 mins

PW:

• Oil temp above lower amber band
• 5 mins