Summary: B777 Trc

Read the summary and the most important questions on B777 TRC

• 1 Preliminary Procedure

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• Pushback/ENG start

  • Captain:
    
  • "Ground, ready for pushback"
  • When starting pushback, before engine start: PA: "Cabin crew arm slides"
  • Captain: "Start L/R ENG"
  • FO: START/IGNITION selector START
  • Captain: Fuel control switch run
  • Verify oil pressure increases

• 2 QRH Memory Items

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• Aborted Engine Start L,R

  Condition: On the ground, an aborted engine start is needed.
  

  1. FUEL CONTROL switch  (affected side)  CUTOFF

• Dual Eng Fail/Stall

  1. FUEL CONTROL switches:  (both) CUTOFF, then RUN.
     
  2. RAM AIR TURBINE switch:  Push and hold for 1 second.

• ENG AUTOSTART L, R

  Condition: During a start, one of these occurs:
  

  • Autostart did not start the engine.
  • Fuel control switch in RUN at low engine RPM with the autostart switch in OFF.

  1. FUEL CONTROL switch:  (affected side)  Confirm  CUTOFF

• Eng Lim/Surge/Stall L, R

  Condition: One or more of these occur:
  

  • Engine indications are abnormal.
  • Engine indications are quickly nearing or show an exceedance.
  • Abnormal engine noises are heard, possibly with airframe vibration.
  • There is no response to thrust lever movement or the response is abnormal.
  • Flames in the engine inlet or exhaust are reported.

  1. A/T ARM switch  (affected side)  Confirm  OFF
  2. Thrust lever  (affected side)  Confirm  Retard until engine indications stay within limits or the thrust lever is at idle.

• Eng Svr Damage/Sep L, R

  Condition: One or more of these occur:
  

  • Airframe vibrations with abnormal engine indications.
  • Engine separation.

  1. A/T ARM switch:  (affected side)  Confirm  OFF
  2. Thrust lever:  (affected side)  Confirm  Idle
  3. FUEL CONTROL switch:  (affected side)  Confirm  CUTOFF
  4. Engine fire switch:  (affected side)  Confirm  Pull

• FIRE ENG L, R

  Condition: Fire is detected in the engine.
  

  1. A/T ARM switch:  (affected side)  Confirm  OFF
  2. Thrust lever:  (affected side)  Confirm  Idle
  3. FUEL CONTROL switch:  (affected side)  Confirm  CUTOFF
  4. Engine fire switch:  (affected side)  Confirm  Pull
  5. IF the FIRE ENG message stays shown:

  • Engine fire switch:  (affected side)  Rotate to the stop and hold for 1 second.
  • IF after 30 seconds, the FIRE ENG message stays shown: Engine fire switch:  (affected side)  Rotate to the other stop and hold for 1 second.

• 3 FCOM Memory Items

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• Severe turbulent air penetration speed (in severe turbulence)

  270 knots below 25,000 feet.
  280 knots or 0.82 Mach whichever is lower at 25,000 feet and above.
  Maintain a minimum speed of 15 knots above the minimum maneuvering speed at all altitudes when airspeed is below 0.82 Mach.

• Max. Allowable difference between altimeters and field elevation

  75 feet.
  The standby altimeter does not meet altimeter accuracy requirements of RVSM airspace.

• Required oxygen pressure from Schiphol

  Flight crew: 1000 psi
  Pax: 1400 psi