Memory Items Flashcards
To assist with learning and assess knowledge of QRH memory items.
Aborted Engine Start L, R
Aborted Engine Start L, R
Condition:
On the ground, an aborted engine start is needed.
- FUEL CONTROL switch (affected side) …. CUTOFF
Airspeed Unreliable
Airspeed Unreliable
Condition:
Airspeed or Mach indications are suspected to be unreliable. (Items which can indicate unreliable airspeed are listed in the Additional Information section in QRH NNC10)
Objective:
To identify a reliable airspeed indication, if possible, or to continue the flight using the Flight With Unreliable Airspeed table in the Performance Inflight chapter.
- Autopilot disengage switch …. Push
- A/T ARM switches (both) …. OFF
- F/D switches (both) …. OFF
- Set the following gear up pitch attitude and thrust:
Flaps extended …. 10 degrees and 85% N1
Flaps up ……………… 4 degrees and 70% N1
[ ] CABIN ALTITUDE
[ ] CABIN ALTITUDE
Condition:
Cabin altitude is excessive.
- Don the oxygen masks.
- Establish crew communications.
- Check the cabin altitude and rate.
- If the cabin altitude is uncontrollable:
PASS OXYGEN switch …. Push to ON and
hold for 1 second
Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
To descend:
- Move the thrust levers to idle
- Extend the speedbrakes
- If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads.
- Descend at Vmo/Mmo
Dual Eng Fail/Stall
Dual Eng Fail/Stall
Condition:
Engine speed for both engines is below idle.
- FUEL CONTROL switches (both) …. CUTOFF, then RUN
- RAM AIR TURBINE switch …. Push and hold for 1 second
[ ] ENG AUTOSTART L, R
[ ] ENG AUTOSTART L, R
Condition:
During a ground start, one of these occurs:
- Autostart did not start the engine
- Fuel control switch is in RUN at low engine RPM with the autostart switch OFF
- FUEL CONTROL switch (affected side) …. CUTOFF
Eng Lim/Surge/Stall L, R
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
- A/T ARM switch (affected side) …. Confirm .. OFF
- 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
Eng Svr Damage/Sep L, R
Condition:
One or more of these occur:
- Airframe vibrations with abnormal engine indications
- Engine separation
- A/T ARM switch (affected side) … Confirm .. OFF
- Thrust lever (affected side) …. Confirm .. Idle
- FUEL CONTROL switch (affected side) …. Confirm .. CUTOFF
- Engine fire switch (affected side) …. Confirm .. Pull
[ ] FIRE ENG L, R
[ ] FIRE ENG L, R
Condition:
Fire is detected in the affected engine.
- A/T ARM switch (affected side) …. Confirm … OFF
- Thrust lever (affected side) …. Confirm … Idle
- FUEL CONTROL switch (affected side) …. Confirm … CUTOFF
- Engine fire switch (affected side) …. Confirm … Pull
- If the FIRE ENG message shows:
Engine fire switch (affected side) … Rotate to the stop
and hold for 1 second
[ ] STABILIZER
[ ] STABILIZER
Condition:
One of these occurs:
- Stabilizer movement without a signal to trim
- The stabilizer is failed
- STAB cutout switches (both) …. CUTOUT
- Do not exceed the current airspeed.