Memory Items 737 Flashcards

(97 cards)

1
Q

Cabin altitude warning or rapid depressurisation

A

3 step procedure.
Emer descent starts from step 2.
(ie you may do a non cabin alt emer descent with masks off.)

PF decides and calls:
‘Cabin Altitude Warning - don masks regulators 100%’
estab comms. ‘Capt on 100% O2, cancel horn’

Note: a cabin altitude warning above 10,000’ is always the result of a cabin altitude exceedance (except in the very unlikely case of an air-ground logic system failure). The IDENTIFY & CONFIRM process may be omitted.
Checklist is also called cabin altitude warning…imho that covers you.

Memory items “Cabin altitude warning”

1
PM:
“Pressurisation mode selector manual” (announce)
Outflow valve switch, Hold in close” outflow valve indicating closed. (announce)
- outflow valve can take 20s
PM says ‘Cabin alt uncontrollable’… DON’T RUSH
- see below for cabin assessment
PAUSE here, make sure you don’t rush off with a controllable cabin!!
- note if cabin controllable supp procedure manual mode..
- you can value add here - door light - my window is missing etc
- look at bleeds, packs, isol valve - maybe try trip reset!
PF ‘continue’
PM:
Pax signs on
Pass oxy switch push.
- PAX OXY light may be ON already – still un-guard and move the switch.
PF just watches.
THEN (that’s mem items Cabin alt warning complete)
Pause again, recheck that cabin - is it controllable….?
“Memory items Emergency Descent”
2
PM: PAN ‘emergency descent’ & Area QNH (7700)
PM ESS both CONT
PM all lights
Pax signs on (if not already)
3
PF PF PA ‘Attention Cabin Crew Emergency Descent.’
“Descending to 10T or LSALT”
alt down and lvl chg, window to IAS
- -5 degrees manual flight
- use AP/AT, cws if other modes not avail
AoB 15º and hdg sel off course 30-45º
TL’s idle
- See note below dispatch with MEL
SB flt detent
Assess damage
- Accelerate to MMO VMO unless damage.
- doors, uncommanded yaw/roll/buffet explosion
- If structural integrity is in doubt, limit speed as much as possible and avoid high Manoeuvring loads: consider slowing to buffet stop etc
Early Level Off?
- Did you load DPD buildup preflight
- were you CPE critical preflight?
- Obs is terrain a factor..
If level off at 14000’ intermediate level off PA is required
- this is not the 737 profile so you’ll most probably head straight down to 10T…

We were not taught to exactly split it up into a 3 stage, but as the auto PA is blaring it’s easy for PF to wait and watch PM do his shit then get into his, I reckon it worked well, no rush.

Anti ice as required
Conf lights on
Conf 7700
RATS, radar, aids for diversion, terrain, tcas, signs

Nice and calm NNCL
At PA requirement hold, don’t forget to read it all, above 14 and below 14 - it’s easy for PM to miss this…
- you should be at 10 cos u are in the maggot.

Set QNH early! If you change qnh during alt cap it will cause problems, same with speed if u r at VMO.

Call 2000 and 1000 to go
Wind speed back 300kts or LRC if required, 250 with damage.
LEVEL OFF recommendation – ALT AQC then ALT HOLD
Don’t reduce speed until nearing level off as the reduced rate of descent to slow down lengthens the time to reach 10,000’. Unconscious passengers need supplementary oxygen ASAP.

Stop checklists for level off, two heads up.
Direct remove mask, reset O2
Hand over remove and reset you mask
Continue Checklist - don’t forget deferred items - don’t land pressurised!

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2
Q

Emergency descent

A

3 step procedure.
Emer descent starts from step 2.
(ie you may do a non cabin alt emer descent with masks off.)

PF decides and calls:
‘Cabin Altitude Warning - don masks regulators 100%’
estab comms. ‘Capt on 100% O2, cancel horn’

Note: a cabin altitude warning above 10,000’ is always the result of a cabin altitude exceedance (except in the very unlikely case of an air-ground logic system failure). The IDENTIFY & CONFIRM process may be omitted.
Checklist is also called cabin altitude warning…imho that covers you.

Memory items “Cabin altitude warning”

1
PM:
“Pressurisation mode selector manual” (announce)
Outflow valve switch, Hold in close” outflow valve indicating closed. (announce)
- outflow valve can take 20s
PM says ‘Cabin alt uncontrollable’… DON’T RUSH
- see below for cabin assessment
PAUSE here, make sure you don’t rush off with a controllable cabin!!
- note if cabin controllable supp procedure manual mode..
- you can value add here - door light - my window is missing etc
- look at bleeds, packs, isol valve - maybe try trip reset!
PF ‘continue’
PM:
Pax signs on
Pass oxy switch push.
- PAX OXY light may be ON already – still un-guard and move the switch.
PF just watches.
THEN (that’s mem items Cabin alt warning complete)
Pause again, recheck that cabin - is it controllable….?
“Memory items Emergency Descent”
2
PM: PAN ‘emergency descent’ & Area QNH (7700)
PM ESS both CONT
PM all lights
Pax signs on (if not already)
3
PF PF PA ‘Attention Cabin Crew Emergency Descent.’
“Descending to 10T or LSALT”
alt down and lvl chg, window to IAS
- -5 degrees manual flight
- use AP/AT, cws if other modes not avail
AoB 15º and hdg sel off course 30-45º
TL’s idle
- See note below dispatch with MEL
SB flt detent
Assess damage
- Accelerate to MMO VMO unless damage.
- doors, uncommanded yaw/roll/buffet explosion
- If structural integrity is in doubt, limit speed as much as possible and avoid high Manoeuvring loads: consider slowing to buffet stop etc
Early Level Off?
- Did you load DPD buildup preflight
- were you CPE critical preflight?
- Obs is terrain a factor..
If level off at 14000’ intermediate level off PA is required
- this is not the 737 profile so you’ll most probably head straight down to 10T…

We were not taught to exactly split it up into a 3 stage, but as the auto PA is blaring it’s easy for PF to wait and watch PM do his shit then get into his, I reckon it worked well, no rush.

Anti ice as required
Conf lights on
Conf 7700
RATS, radar, aids for diversion, terrain, tcas, signs

Nice and calm NNCL
At PA requirement hold, don’t forget to read it all, above 14 and below 14 - it’s easy for PM to miss this…
- you should be at 10 cos u are in the maggot.

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3
Q

Automatic Unlock

A
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4
Q

Aborted Engine Start.
PROCEDURE
Reasons to abort?

Limitations

A

ESL cutoff

Non memory has you motor engine in GND for 60s, if ESS already in auto wait till N2 blw 20% and switch to GND for 60s.

Abort for:
*​ N1 or N2 doesn’t inc or inc v slowly after the ​EGT​ increases​
*​ no​ oil pressure indication by the time that the engine is ​stable at idle​
​EGT​ does​ not increase by 15 seconds​ after the engine start lever ​is moved to IDLE detent
​ the​ EGT​ quickly nears or exceeds the start limit.
hot,hung,wet,oil.

2min starter duty time with 10s off between.

stable at idle is when EGT start limit redline not shown.

Remember after 3 aborted starts you require 15 min cooling.

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5
Q

Engine limit or surge or stall

A

May lead to engine shutdown.

Below the line you have:
- Engine indications are abnormal or EGT continues to increase then:
- Eng start lever..confirm..cutoff

Consider APU, descent etc.
But remember FCTM:

Many engine surge or stall events are recoverable and permit continued​ engine ​operation. Stabilized​ engine indications​ and decreasing EGT​ indicate the surge/​stall has cleared. In these cases, the engine may be operated normally, or at a ​reduced thrust level​ which is surge and​ stall free.
Only shutdown if you really need to.

Also
Loss of parameter:
Flight Crew should be advised​ that the loss of an engine parameter indication ​while inflight does not necessarily constitute a situation that​ would require the ​engine to be shutdown. As long​ as there are no​ other accompanying indications of ​an engine malfunction, the engine can be operated normally​ for the remainder of ​the flight.

Vibration:
However, high AVM indications combined​ with other abnormal ​engine indications, extreme vibrations, severe damage, and/or engine limit ​exceedances should be addressed in accordance with the appropriate Non-Normal ​Checklist.
B flight ops review 737-33

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6
Q

What checklist do you access if there is no response or abnormal response to TL movement?
Consider phase of flight in answer.

When might you consider a quick engine shutdown.

A

Engine Limit or surge or stall.
Any phase of flight.

From FCTM:
All​ turbo fan engines are susceptible to this malfunction whether engine control is ​hydro-mechanical, hydro-mechanical with supervisory​ electronics (e.g. PMC) or ​Full Authority​ Digital Engine Control (FADEC).
Engine response to a loss of ​control varies from engine to engine. Malfunctions have occurred​ in-flight​ and on ​the ground.
The major challenge​ the Flight Crew faces when responding to this ​malfunction is recognizing​ the condition and determining which engine has ​malfunctioned.
The Engine Limit​ or Surge or Stall NNC​ is written​ to include this ​malfunction.This condition​ can occur during​ any phase of flight.​
Failure of engine or fuel control system​ components or loss of thrust lever position ​feedback has caused​ loss of engine thrust​ control. Control​ loss may not be ​immediately evident since many engines fail to some fixed RPM or thrust lever ​condition. This fixed​ RPM or thrust​ lever condition may​ be very near the ​commanded thrust level and therefore difficult to recognize until the Flight Crew ​attempts to change thrust with the thrust lever.
Other engine responses include:​ ​shutdown, operation at​ low RPM, or thrust at the last valid thrust​ lever setting (in ​the case of a thrust lever feedback fault)​ depending on altitude or air/ground logic. ​In all cases, the affected engine does not respond to thrust​ lever movement or the ​response is​ abnormal.​

Since recognition may be​ difficult, if a loss of engine control is suspected, the ​Flight Crew should continue the takeoff or remain airborne until the NNC can​ be ​accomplished. This helps with directional control and may preclude an ​inadvertent shutdown of the wrong engine.
In some conditions, such as during low​ ​speed ground​ operations, immediate engine shutdown may​ be necessary​ to ​maintain directional control.
So on the ground veering off the runway or unable to stop taxiing…

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7
Q

What checklist do you run if flames are reported in engine inlet or exhaust in flight?

A

Engine Limit or surge or stall.

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8
Q

Dual engine failure.

What are your initial target speeds?

A

“AP off - Manual flight - Capt PF”
Identify the problem
Loss of thrust on both engines
‘have fuel, fuel pumps are on,
and no severe damage so relight possible’ Try anyway obs…
Turn toward nearest airport/ off airport landing spot.

Restart attempt as soon as possible to take advantage of higher engine RPM at point of flame out - gives best windmill relight chances.

Memory items…

At monitor EGT on start:
Capt Mayday call/ 7700/ area qnh if req. and wind up speed as required.
At/Abv FL270 = 275kts
Blw Fl270 = 300 kts - ie get in windmill window.
These are the QRH speeds to get a relight, but some consideration to min drag speed is due if terrain a serious factor. Do you have any fuel?

During start attempt use lower of EGT redline or EGT start limit line if displayed. Hung start is STAGNANT rpm and INCREASING EGT, don’t abort too early.

Restart attempt as soon as possible to take advantage of higher engine RPM at point of flame out - gives best windmill relight chances.
Consider turn off track for traffic and consider diversion/terrain/weather.
Requesting area QNH - maybe maybe not depends on alt, could be a bit distracting high alt.
Traffic position report all stations PAN call.
You maintain transponder 1 so 7700, not sure if tcas or adsb still works.
AP lost - revert to basic modes, I’m pretty sure you’ll have lost VNAV/LNAV
Only Capt screens so LHS flying.

LHS will be hand flying - area of responsibility..
Engine start lever PM domain, on ground it is the captain during engine start.
This is reverse of normal - will need CRM.
You have capt screens and compact eng displays.

Get start attempt going ASAP to take advantage of high post flameout rpm - do not delay till you are in envelope!
Get speed up and lower altitude quickly to get in windmill envelope.
Windmill envelope is AFM demonstrated - doesn’t mean a windmill might not work outside.
Only after a start attempt get APU on, but don’t delay this too much.
Although Elec sys fcom pages only recommend starting apu below F250…

Inflight start:
During​ in-flight restart attempts use the lower of the EGT​ redline and the EGT​ ​start​ limit redline, if displayed. A​ hung​ or stalled​ in-flight start is​ normally​ ​indicated by stagnant RPM and increasing​ EGT. During start, engines may ​accelerate to idle slowly but action should​ not be taken if RPM is increasing and ​EGT​ is not near or rapidly approaching the limit.

Don’t confuse APU start gen trip on with engine return.

Oil qty indication as low as zero is normal if windmilling N2 RPM is below approximately 8%.

The checklist doesn’t talk about closing thrust levers but I’d guess this is a good idea. You do in an engine inflight start.

What do you lose?
Elecs obs but what?
AP AT?
lights? internal/external?
Tcas?
Anti ice, capt probe heated FO and stby not - IAS disag/URAS.

1 Engine relights?
Stop checklist,
Eng out on CDU,
Consider LO @ single eng ceiling - are you damaged?
Consider EO speed if terrain - OTW stay @ 275kts for second eng relight.
Remember set CON

2 Eng restored?
All eng on CDU
AT avail
ATC notify
APU off if required for fuel burn.
GPWS ovrd back to norm.

Multiple CL’s…. Prioritise

Use power on descent if you are worried about fuel contamination.

Leave inop engine in idle
consider continuing to get a restart.

Boeings checklist is basically designed for volcanic ash, fuel mismanagement or rain hail ingestion. If you have severe damage, ie serious low level bird strike hit the APU straight away.

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9
Q

APU fire

A

On ground before start consider impending battery power and some blackness…

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10
Q

Engine fire, or severe damage or separation.

A

Start time once you’ve blown first bottle.
AT …off
TL, affected side…conf…close
ESL, affected side….conf… cutoff
Eng Fire switch, affected side…conf…pull
IF:
Engine fire switch or
Engine Overheat
remains illuminated :
“Fire message remains”
Eng fire sw, affected side…. Rotate to stop and hold for 1 second.
“Fire indication remains, or extinguished”

PF calls “mem items complete, time check, fire eng X NNCL”
I thinks, on the 73…?

With an N1 sudden seizure, SPD LIM amber flag is annunciated, yellow and red bands are removed from the speed tape and same side AFDS pitch modes LVL CHG, V/S and VNAV are not available.

Place the failed engine’s Start Switch to CONT to remove the SPD LIM flag and to restore AFDS pitch modes, or use the opposite A/P.
Refer to SPEED TRIM FAIL for additional background information.

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11
Q

Engine overheat
Mem items… what if light stays illuminated?

A

Leads to remainder Eng fire:
ESL, affected side….conf… cutoff
Eng Fire switch, affected side…conf…pull
IF:
Engine fire switch or Engine Overheat
remains illuminated :
“Fire message remains”
Eng fire sw, affected side…. Rotate to stop and hold for 1 second.
“Fire indication remains, or extinguished”

PF calls “mem items complete, time check, fire eng X NNCL”
Remember you open CL and check mem items straight away before cessna.

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12
Q

Engine Tailpipe fire - ie no engine fire warning on the ground:

A

This it’s not a memory item… But used to be…
But ESL to cutoff (ie shutoff fuel)
alert PA
notify ATC…
a good start…

Engine Fire CL is inappropriate.
You would probably get this during an engine start.

Worst case scenario would be after shutdown with no APU available.

From FCTM:
An engine tailpipe fire can occur while on the ground, during engine start or ​shutdown.
Since a tailpipe fire develops in an area of the engine without fire ​detection capability, the engine fire warning will not show.​
Communication with a trained ground​ crew member via the flight​ interphone or ​hand signals can provide​ awareness of a tailpipe fire. Reports of a tailpipe fire may​ ​also be received from ATC,​ Cabin Crew, or Flight Crew members of nearby ​airplanes.​
Engine tailpipe fires can​ occur due to​ the following:​
*​ engine control malfunction​
*​ excess fuel in the combustor,​ turbine or exhaust nozzle​
*​ oil accumulation in the hot section flow path or exhaust system.​
If a tailpipe fire is reported, the Flight Crew should accomplish the NNC without ​delay. Flight Crews should consider the following when​ dealing​ with this ​situation:​
*​ motoring the engine is​ the primary​ means of extinguishing the fire​.
*​ to prevent​ an​ inappropriate evacuation,​ flight attendants should be ​notified without​ significant​ delay.
*​ communications with ramp personnel and ATC​ are important to ​determine the status of the tailpipe fire and to request​ fire extinguishing ​assistance​
*​ the engine fire checklist is inappropriate because the engine fire ​extinguishing agent is not​ effective against a fire inside the tailpipe.

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13
Q

Runaway Stabilizer.

A

Reducing airspeed reduces air loads to help control. AP and AT are out for remainder of flight.
You may conduct mem items simultaneously.

Did trim stop when you disconnected AP - consider jammed FC’s

Cutout switches do not require confirmation

1 unit trim is 15 turns of wheel

Consider seatbelts cabin management.

FCTM:
​A​ runaway stabilizer condition can be recognized by continuous uncommanded ​movement of stabilizer trim, or​ if​ stabilizer trim is occurring in a manner that​ is​ ​not​ appropriate for current flight conditions. During manual flight​ or flight​ with ​the autopilot engaged, automatic stabilizer​ trim can be commanded by the Speed ​Trim System or autopilot​ trim. Since commanded stabilizer trim can occur ​automatically, the pilot needs to consider the existing flight conditions to ​determine if a runaway stabilizer condition exists. For example, some stabilizer ​trim movement can be expected to occur during speed, altitude, or configuration​ ​changes.​During​ a runaway​ stabilizer condition the crew should maintain airplane pitch ​control through​ the use of the control​ column, main electric stabilizer trim, and ​thrust levers. The control​ column must​ be held firmly before the autopilot (if ​engaged) is disengaged​ to maintain airplane pitch control and retain any elevator ​commands from the autopilot. After the autopilot and autothrottle are disengaged, ​use the control column and thrust levers to​ establish​ appropriate pitch attitude and ​airspeed. If uncommanded​ trim​ motion​ continues, it​ may stop​ when the control​ ​column is displaced in the opposite direction and the control column cutout is ​activated. Use main electric stabilizer trim​ to reverse any​ stabilizer trim movement ​and to reduce control column​ forces. Sustained use of main electric stabilizer trim ​may​ be needed. It is important​ to note that even though the steps in the Runaway ​Stabilizer checklist are sequential,​ these steps can be​ accomplished ​simultaneously. If uncommanded stabilizer trim movement continues, place both ​STAB TRIM cutout switches to the CUTOUT​ position. Manual stabilizer trim​ ​should then​ be used for the remainder of the flight.

Manual Stabilizer​ Trim​
During​ some non-normal conditions, manual stabilizer trim​ may​ be​ needed. The ​Flight Crew should use main electric stabilizer trim, if available, to ensure the ​airplane is in-trim​ prior to relying on the use of manual stabilizer​ trim. Manual ​stabilizer trim is intended for small corrections from an​ in-trim​ condition. If ​manual stabilizer​ trim​ is needed, make sure both STAB TRIM cutout switches are ​in the CUTOUT​ position prior​ to extending​ the manual trim wheel​ handles. ​Anytime manual stabilizer trim​ is in​ use, keep the manual trim wheel handles ​extended. This allows easy access for the pilots to make required trim​ changes.​Note:​ Moving the STAB​ TRIM cutout switches to the CUTOUT​ position can ​result in illumination of the SPEED​ TRIM​ FAIL​ light. This can occur ​during​ manual​ flight if the Speed Trim​ System determines a need to trim ​but​ the system is disabled

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14
Q

Airspeed Unreliable.

A

After flight path safe…
Configuration will be:
with gear up
flap xxx so limited to gear speed/flap speed/alt.
Anti ice is/is not required.
Turning to hdg and climbing, this will keep us safe.

Identify the problem
xxx non normal checklist
important items complete,
ok hold CL lets get vectors to hold here and consider position, plan, return etc.
Continue CL.

If you are in icing conditions remember AI!!

May get SS, overspeed, airspeed low warnings. FPV and PLI may be unreliable.

FCTM:
Once flight path is under control​ and the airplane is not ​in a critical phase of flight, accomplish the Airspeed Unreliable NNC

Low level consider GS readout with Pan call.

Level is 280/0.76

Consider Ref GS for app below 1000’
Vref subtract HW or add TW to get ref gs, this will keep you safe - consider for keeping you safe.
+1kt for isa+5, +1kt for 1000’ elevation

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15
Q

Airspeed unreliable TO

A

+ve rate GU
“AP/AT off”
“FD off”
‘Maintaining TO thrust and AETA to accn height, flaps to remain set.
@accn verify mem items and set 10/80 (or leave thrust as is if heavy)
Pitch, don’t look at FPV AND DON’T do 10 and 80 on rotation.
OPT will have given us a target att and target N1, eo and all eng. know these b4 TO.
FCTM references 15° if you don’t know.
Gear up Maint current flap.
(URAS during rotate u need a plan.)

Mem items @ accn height - ie set 10/80
Consider safe altitude, climb to MSA for checklist.
‘We’ll climb above MSA for CL’
Pan call, request block to 10T and GS readout.
@/abv MSA checklist.

GS probably a good indicator or reliable speed unless winds very high.

FCTM:
​​If an unreliable airspeed event occurs during​ takeoff at or after V1, maintain​ ​takeoff thrust, smoothly​ rotate towards 15° pitch attitude and establish the normal ​takeoff​ pitch attitude target, retract the landing gear, and maintain flap ​configuration. Climb at the normal takeoff pitch attitude target​ until reaching a ​safe altitude (acceleration height) and do the Airspeed Unreliable NNC.​See discussion regarding normal​ takeoff pitch attitude target in Chapter 3, ​Takeoff, Rotation​ and Liftoff and​ Typical​ Rotation.​

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16
Q

Approach and Landing Airspeed Unreliable

A

Approach:
If available, accomplish an​ ILS or GLS approach. Establish landing configuration ​early​ on final​ approach. At glideslope intercept or beginning​ of descent, set​ thrust ​and attitude per the QRH​ tables and control​ the rate of descent with​ thrust.

Landing:
Control the final approach so as to​ touchdown​ approximately​ 1,000ft​ to 1,500ft ​beyond the threshold. Fly the airplane​ on to the runway, do not hold​ it off or let it ​“float” to touchdown.​Use autobrakes if available.​ If manual braking is used, maintain adequate brake ​pedal​ pressure until a safe stop is assured. Immediately​ after touchdown, ​expeditiously accomplish the landing roll procedure.

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17
Q

Go Around Airspeed Unreliable

A

You may lose both side FD pitch guidance on GA.
You get pitch back with new pitch mode and lose roll guidance on dud side.
You can use TOGA (to exit APP mode) on GA.
Don’t use TOGA ISFD only.

From FCTM
Prior to Approach​
In the event that either the Captain’s or​ First Officer’s​ airspeed indication is ​reliable, the flight directors on​ the reliable PFD can be used during an approach. ​
When TO/GA​ is pushed in the event of​ a go-around​ or missed approach, pitch ​guidance may automatically be removed from​ view on both PFDs as a result​ of a ​disagreement between​ PFD flight director pitch guidance.
Flight director roll ​guidance remains available.​
Flight director pitch guidance returns to view on the reliable PFD when​ a pitch ​mode change is made or automatically occurs.
Simultaneously, flight director roll ​guidance is automatically removed on the unreliable PFD.​
Refer to​ the Flight With Unreliable Airspeed, go-around​ table prior to starting the ​approach.
This provides a target​ pitch setting in the event that​ flight director​ pitch​ ​guidance is removed.​
Note:​ If the APP​ mode is used during the approach, it is important to exit​ the APP​ ​mode in the event of a go-around.
This can​ be done by pushing TO/GA.​
Note:​ If only​ the standby​ airspeed indication is reliable, do not use TO/GA.​
On Approach​
If an airspeed​ unreliable event occurs during approach, and a go-around or missed ​approach is necessary, execute a go-around using go-around thrust and smoothly ​increase pitch towards​ a normal takeoff pitch attitude. Upon reaching a safe ​altitude set the target pitch attitude and thrust settings from the Airspeed ​Unreliable NNC and accomplish the checklist.

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18
Q

AofA disagree
What indication might help?

A

Go to Unreliable Airspeed checklist.
ISFD speed.

FCTM:
If the Flight Crew suspects that the unreliable airspeed condition may be caused ​by erroneous AOA, in addition​ to the above flight deck indications, the AOA​ ​DISAGREE alert is shown on​ both PFDs​ and​ erroneous minimum​ and maximum ​speed bars are shown on one side. In this​ situation, comparing indicated airspeed ​on the PFDs with the ISFD can​ help the Flight Crew​ determine a reliable airspeed ​indication

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19
Q

IAS disagree

A

Go to unreliable airspeed checklist

Capt FO IAS different more than 5kts for 5 seconds

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20
Q

Landing configuration
TO configuration

A

Sounds if:
Trim out of green band
PB set
SB not down
TE Flaps (5-15)
LE Flaps

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21
Q

Wind shear escape, Manual

A

Manual Wind Shear Escape
AP disc
Press TOGA (verify FMA)
TL’s firewall
AT disc
SB retracted
Both hands on controls level winds and 15° NU
Follow FD TOGA commands if avail (do not exceed PLI - not in 737 fcom but good idea?)
“set alt 10T, notify atc windshear escape”
May need to intervene if you capture LNAV….
Turn only for obstacle clearance.
Config remains till clear of WS - beware secondary WS - what is a safe ALT?
Monitor VS and alt
Do not attempt to regain lost airspeed till clear of WS

PM
Verify max thr (and AT off)
Verify all actions and call omissions
Monitor VS and alt
Call out any trends towards terr an and sig changes
ATC ‘Qantas windshear escape’

Watch FMA’s - avoid alt capture!
Config remains till clear of WS - beware secondary WS - what is a safe ALT?
Monitor VS and alt
Do not attempt to regain lost airspeed till clear of WS

So recovery recovery:
‘winds check’ no cray wind esp tailwind.
Set 10deg and 80-85%
ignore FD if in alt cap - fix it alt abv push toga.
watch flap speed if applicable ie GA.

set xx alt( well above),
cycle fds
level change set speed xxx
say In the GA F 15
Flap 15
positive rate and GU
AP engage,
AT on
fair hdg hdg sel.
call FMA’s - normal ga from here…
What’s your new track - recapture LNAV - talk to ATC
Above accn alt, remain at F5 for return,
holding - how much fuel.
This would avoid unintended capture of LNAV…

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22
Q

Windshear Escape Auto

A

Auto Wind Shear escape
Push Toga switch
Verify TOGA annunciation
Verify GA thrust
Verify SB retracted
Monitor system perf
PM
verify GA thr
verify all actions complete
ATC ‘Qantascunt windshear escape’

Watch FMA’s - may need to set higher alt to avoid alt capture!
Config remains till clear of WS - beware secondary WS - what is a safe ALT?
Monitor VS and alt
Do not attempt ton regain lost airspeed till clear of WS

So recovery recovery:
‘winds check’ no cray wind esp tailwind.
Set 10deg and 80%
ignore FD if in alt cap
watch flap speed if applicable ie GA.

set xx alt( well above),
Push Flch
say In the GA F 15
Flap 15
positive rate and GU
AP engage, verify AT and thrust mode.
call FMA’s and do normal GA
What’s your new track - recapture LNAV - talk to ATC
Above accn alt, remain at F5 for return,
holding - how much fuel.
This would avoid unintended capture of LNAV…

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23
Q

Wind shear unacceptable deviations

A
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24
Q

Wind shear Caution vs Warning
TO
Approach
What aural do you get with each?
When inhibited?

A

Caution:
MONITOR RADAR DISPLAY
Manoeuvre as required to avoid WS

Warning:
WINDSHEAR AHEAD
TO:
prior V1: reject
after V1: WS escape manoeuvre

GO-AROUND WINDSHEAR AHEAD
WS escape manoeuvre OR
Normal GA at pilot discretion.

Note:
WINDSHEAR WINDSHEAR WINDSHEAR means you are IN a windshear.

Note Inhibits:
NEW cautions 80kt-400’
NEW Warnings 100kts-50’

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25
Accomplish the following if a RAAS callout or alert differs from the Flight ​Crew's​ expectation
26
GPWS Warning​ “PULL​ UP” “TERRAIN TERRAIN PULL​ UP” ​warning.​ “PULL​ UP” “OBSTACLE OBSTACLE PULL​ ​UP” warning.​ *Other situations resulting in unacceptable flight toward terrain...
AP off AT off aggressively apply max thrust SB retracted 2 hands on controls 20° NU wings level. Terrain threat - pitch to PLI or initial buffet Config remains the same Rad alt for sustained or increasing terr separation. When clear slowly decrease pitch and accelerate. PM Assure max thr and verify PF actions Monitor vertical speed and altitude Rad alt = terrain clearance a Baro alt = min safe Call trends towards terrain Low RNP ops If warning occurs during low RNP ops re-establish required gnd track while executing the procedure.
27
GPWS warning during low RNP operations?
If the warning occurs​ during​ low RNP​ operations, re-establish ​or maintain the required ground track while executing the terrain ​avoidance manoeuvre.
28
When can you ignore a GPWS activation?
GPWS CAUTION If a Terrain CAUTION occurs under DAY VMC and positive visual verification is made that no obstacle or terrain hazard exists, the alert may be regarded as cautionary and approach may be continued. GPWS WARNING If positive visual verification is made that no obstacle or terrain hazard exists when under DAY VMC *PRIOR TO* a terrain or obstacle warning the alert may be regarded as cautionary and approach may be continued. The intent​ of​ the​ referenced notes​ in the​ GPWS​ Caution​ and​ GPWS​ Warning Maneuvers​ is to​ allow​ ​crews to continue an approach when flying under​ daylight​ VMC and​ a positive visual verification is made​ ​that​ no obstacle or​ terrain hazard exists.​ The notes​ also assume that​ this continuation occurs only *during ​a stabilized approach* as​ described in the FCTM​. ​ The ​notes​ address​ nuisance​ alerts which occur​ due​ to​ a lack​ of​ runway data in the database,​ terrain database​ ​errors, an out-of-date database or​ a system sensor​ issue.​ *It is​ not the​ intent of​ the notes​ to allow​ ​the​ continuation​ of an​ approach​ when the​ aural​ PULL UP warning​ caused​ by​ excessive rate​ of​ closure​ ​to terrain occurs.​* In​ that​ event, the crew should take immediate​ action​ as​ described in​ the​ QRH​ GPWS​ ​Warning Maneuver. ​ ​An important​ difference​ between the​ GPWS Caution note and the GPWS Warning note is that ​continuation of​ the approach may​ be​ made during a GPWS Warning only if​ there is visual verification ​that​ no obstacle or​ terrain hazard exists BEFORE the warning alert occurs.​ In the case of​ a GPWS​ ​Caution,​ visual verification that​ no​ obstacle or terrain hazard​ exists​ can​ be​ made​ when the​ caution​ alert​ ​occurs.
29
TA
Ok we have standard or xxxxHpa set and crosschecked, get onto atc and confirm our altitude and what is this joker doing? In climb descent - reduce rate.
30
RA CLIMB RA in landing config Does GPWS take priority How about stick shaker? What is some good support calls?
TCAS I have control, airbus call but maybe a good one. Disconnecting’ If manoeuvring is required, disengage ​the autopilot and disconnect the ​autothrottle. Smoothly​ adjust pitch​ and ​thrust to satisfy​ the RA​ command. ​Follow​ the planned lateral flight​ path​ ​unless visual contact with the ​conflicting traffic requires other ​action. You have 5 seconds to complete 0.25g move, 2.5 for an increaser When you are PM include support on climb rate from hud. Post TCAS. ATC Call. Confirm altitude you are cleared to (it might have been your mistake) Do you need to climb - what excess energy do you have? Good support call you are where regarding optimum. Level change AP on AT on confirm modes or Cycle fd's etc. Windshear, GPWS, and stall warnings take precedence over TCAS advisories. ​Stick shaker must take​ priority at all times. Complying​ with​ RAs may result in ​brief exceedance of altitude and/or placard limits. However, even at the limits of ​the operating envelope, in most cases sufficient​ performance is available to​ safely ​manoeuvre the airplane.
31
On the ground, the EGT digital readout flashes white for an:
32
What engine parameters are monitored by EEC for start, ie what bad starts are monitored?
GROUND START ONLY! Hot, wet, stall, egt limit.
33
Abort inflight start when (x4) Under what conditions would you see low acceleration - and what would you do?
An in-flight engine start must be aborted for the following: No EGT increase within 30 seconds; N1 or N2 does not increase or increases very slowly after EGT increase; No OIL PRESS indication by the time the engine is stable at idle; EGT rapidly approaches or exceeds the start limit. If any of the above occur, move the engine start lever to CUTOFF and select the ENGINE START switch AUTO. Hung, wet, hot, oil… From QRH inflight start: Engines can accelerate to idle very​ slowly, ​especially at high altitudes or in​ heavy ​precipitation. If​ N2 is steadily increasing and EGT ​stays within limits, do not interrupt the start. A hung start in flight is usually accompanied by an unacceptable egt climb I thinks…
34
Aborted engine start Engine start selector: Not a memory item the checklist directs you to do this.
After MI ESL to cutoff checklist directs you to: If the ENGINE START switch remains in GRD, continue to motor the engine for 60 seconds, then position the switch AUTO. If the ENGINE START switch has already released to AUTO, wait until the N2 RPM has decreased below 20% and then select the GRD position. After motoring the engine for 60 seconds position the ENGINE START switch AUTO.
35
Abort engine start for: Starter duty time?
Abort for: - N1 or N2 doesn't inc or inc v slowly after the ​EGT​ increases​. - no​ oil pressure indication by the time that the engine is ​stable at idle​ - EGT​ does​ not increase by 15 seconds​ after the engine start lever ​is moved to IDLE detent ​- the​ EGT​ quickly nears or exceeds the start limit 2min starter duty time with 10s off between. See FCOM for extended motoring. stable at idle is when EGT start limit redline not shown.
36
Eng Fail short final Normal weight? How about heavy, or otherwise performance limited? wind additives?
GA if unstable... Continue: Sufficient thrust available? - continue with landing flaps, you’ll need 20% more thrust on good engine. Sufficient thrust not available (prob heavy)? -bug up 20kts to current set command speed (was set to F30 or F40) -increase thrust -Retract flap to F15 -Remember to Add wind additives as required (This sets command speed at least Vref for F15 - it's a white coloured bug on tape.) Go Around: Use F15 for GA if flaps were set to F30 or F40 Use F1 if you bugged up. From FCTM Failure On Final Approach​ If an​ engine failure should​ occur on​ final approach with the flaps in the landing ​position,​ the decision to continue the approach​ or execute a go-around should be ​made immediately.​ If the approach is​ continued​ and sufficient thrust is available, ​continue​ the approach with landing flaps. If the approach is continued​ and ​sufficient thrust is not available for landing​ flaps, retract the flaps to 15 and adjust ​thrust on the operating engine. Command speed should be increased to 20kt over ​the previously set flaps 30 or 40 VREF. This sets​ a command speed that is equal ​to at least VREF for flaps 15 and is represented by the white colored bug on the ​airspeed tape. Wind​ additives should be added as needed, if time and conditions ​permit. If a go-around is required, follow the Go-Around and Missed Approach​ ​procedures except use flaps 15 initially if trailing​ edge flaps are at 30​ or 40. ​Subsequent flap retraction should be made at​ a safe​ altitude and in level flight or​ ​a shallow climb.
37
What is an Upset?
An upset condition is [now] considered​ any time an airplane is *diverting ​from the intended​ airplane​ state.* An airplane upset can involve pitch or​ roll​ ​angle deviations as well as inappropriate airspeeds for the conditions
38
What are some stall identification items?
Indications of low speed event 737 - Higher than normal pitch, AofA in hud. (outside +5º to -2.5º) - Unusual auto trimming - PLI's - Amber band and zipper - BUFFET ALERT in scratchpad (Only appears if flaps are retracted) Current conditions result in a manoeuvre margin less than specified. - Airspeed Low - When current airspeed decreases into the minimum manoeuvre speed amber bar: - airspeed readout box turns amber and flashes for 10 seconds. - voice alert annunciate ‘Airspeed Low, Airspeed Low’ once - box returns to white when airspeed is above minimum manoeuvre speed. - Stick shaker And other stall indicators: buffet pitch roll descent: 1. Buffet of a magnitude and severity that is a strong deterrent; BUFFET 2. Uncommanded nose down pitch that cannot be arrested; or, PITCH 3. No further increase in pitch when the pitch control is held at the after stop for two seconds; 4. Uncommanded rolling motion; ROLL 5. Inability to arrest the descent rate. DESCENT
39
Upset recovery Nose Low
Recognise and confirm. Confirm and announce “Not stalled” Disc AP/AT Recover recover from stall if needed - call ‘not stalled’ roll in shortest direction to wings level (if BA more than 90deg unload and roll) complete apply nose up elevator apply nose up trim if required adjust thrust and drag as needed. Estab correct pitch: Set pitch 2.5/thr XXX After you find your happy place, FD's cycle alt hold AP on AT on Fair HDG HDG Sel CALL MODES
40
Upset recovery Nose High
Recognise and confirm Disc AP/AT Recover Apply ND elevator, as much as needed to obtain nose down pitch rate. Apply ND trim - use caution Reduce thrust Roll to obtain nose down pitch rate Complete When app horizon roll wings level check as and adjust thr establish correct pitch PM call attitude, as, alti throughout. Verify all actions of PF Estab correct pitch: Set pitch 2.5/thr XXX After you find your happy place, FD's cycle alt hold AP on AT on Fair HDG HDG Sel CALL MODES
41
Approach to stall. Indications and recovery Post recovery?
Amber band and speed dec, blue below wheels if not turning, pitch increasing, buffet, inability to stop desc, Lack of pitch authority​, Lack of roll control​... Recognise confirm breath... Do not use FD, Hold column firmly Disco AP/AT INITIATE Smoothly apply ND elevator to reduce AofA until buffet or SS stops. Trim may be needed. PM monitor Altitude and airspeed, verify actions and call trend toward terr CONTINUE Verify SB retracted Roll wings in shortest dir to wings level if needed COMPLETE Check AS and adjust thr as needed Advance thr half way up amber band speed increasing 2°/s pitch out, beware sec stall. Establish pitch happy place 2.5deg set thrust xxxx FD's off/on then re-establish auto's PM monitor Alt&A/s, verify actions and call trend toward terr. Estab correct pitch: Set pitch 2.5/thr XXX After you find your happy place, FD's cycle alt hold AP on AT on Fair HDG HDG Sel CALL MODES
42
Inflight RVSM requirments with AP failure (specifically the 'height lock') How about class A oceanic?
Evaluate capability to maint alt through man control Assess situation with conflicting traffic turn on all exterior lights if not in contact with ATC on VHF broadcast on 121.5 Notify ATC 'negative RVSM' Class A If you can maintain current level then maintain that otw leave track by 90deg and desc below F290
43
What are the RVSM requirments if one primary alti fails? How about both? How about oceanic Class A? When do you get Alt Disagree?
AP must be engaged 'Increased   vigilance" Notify ATC: "for information operating on one primary alti only" Both: use stby alti all ext lights on notify ATC "negative RVSM" and the intended course of action. Class A without clearance: leave track by 45deg and descend below F290 IF operationally feasible.. If not feasible continue to alert nearby aircraft and attemt contact with ATC.
44
RTO
Capt. Without delay: Simultaneously close the thrust levers, disengage the autothrottles, and apply maximum manual wheel brakes or verify operation of RTO autobrake. If RTO AB is selected, monitor system performance and apply manual wheel brakes if the AUTOBRAKE disarm light illuminates or deceleration is not adequate. Raise the speedbrakes are extended. Apply reverse thrust up to the maximum amount consistent with conditions. Continue maximum braking until certain the airplane will stop on the runway. PM Verify actions as follows: Thrust levers closed. Autothrottles disengaged. Maximum brakes applied. Reverse thrust applied. Verify speedbrake lever UP and call “SPEEDBRAKES UP.” If speedbrake lever not UP call “SPEEDBRAKES NOT UP.” When both REV indications are green, call “REVERSERS NORMAL.” If there is no REV indication(s) or the indication(s) stays amber, call “NO REVERSER LEFT ENGINE,” or “NO REVERSER RIGHT ENGINE,” or “NO REVERSERS.” When AUTOBRAKE​ DISARM light ​illuminates, call “AUTOBRAKE ​DISARM”.​ Call​ out omitted action​ items. When stopping assured: Capt Start movement of the reverse thrust levers to reach the reverse idle detent before taxi speed. After the engines are at reverse idle, move the reverse thrust levers to full down. PM Call out “60 KNOTS”. Communicate the reject decision to the control tower and cabin as soon as practical. When the airplane is stopped, perform procedures as required. Review Brake Cooling Schedule for brake cooling time and precautions (refer to the Performance Inflight chapter). Consider the following: * the possibility of wheel fuse plugs melting * the need to clear the runway * the requirement for remote parking * wind direction in case of fire * alerting fire equipment * not setting the parking brake unless passenger evacuation is necessary * advising the ground crew of the hot brake hazard * advising passengers of the need to remain seated or evacuate * completion of Non-Normal checklist (if appropriate) for conditions which caused the RTO
45
Ditch Drill
Captain 1. Complete checklist. 2. Fit lifejacket and take torch. 3. Proceed to cabin and oversee evacuation. 4. When all assistance rendered, evacuate. First Officer 1. Complete checklist. 2. Fit lifejacket and take torch. 3. Proceed to cabin or as directed by Captain. 4. When all assistance rendered, evacuate.
46
IMPACT drill
Captain 1. Complete checklist. 2. Take torch. 3. Monitor and oversee evacuation. 4. When all assistance rendered, evacuate. First Officer 1. Complete checklist. 2. Take torch, NOTOC and loadsheet. 3. Proceed to cabin and relay evacuation command. 4. Evacuate first available exit. 5. Report to Emergency Services if available. Additional Actions BOTH. Supervise welfare of passengers until relieved by rescue personnel.
47
Jammed Flight Controls? Not memory item but...
- Auto’s off - Big block (atc), - Belts on (look after cabin), - Consider Icing and performance 1: AP/AT disengage DO NOT TURN OFF flight control switches. Limit manoeuvres and plan to land at nearest AVAILABLE. Seat belts on You may be here from a stab trim runaway ATC, block, consider negative g for jam clearing. Descent to warm air if ice jam suspected. Call for non normal CL 2: Try to clear Jam - overpower, both pilots full force OK Wheel and column both have overrides. Cleared jam then ok 3: ICE? Go warmer - descend. Cleared jam then ok 4: If jam doesn't clear overpower controls one at a time, pilot with the most controls has unjammed controls howvere will be 23kg heavier than normal. 5: Use trim -If elec stab trim needed then use stab trim override in OVERRIDE. Long Runway with Minimum Crosswind. You can use SB - but gentle with everything Don't change anything after fence crossing Thrust idle after touchdown recommended @MLW stab trim may be needed in flare. Asymmetric reverse and braking for directional control on roll. Go Around with Elevator Jam not recommended! Remember Stab trim override switch, this allows you to use trim even if there is opposite direction force on the column… Advance thrust and control pitch with Stabilizer and any Elevator you have...
48
Driftdown Above SE max alt. This is driftdown, obs consider different profile considering situation.
1. Rudder keep her straight 1. It doesn't require must BUT must be done - centre skid brick!! Onside Eng fail AP disco, get it back in immediately 2. AT disco & Thrust up to amber band on N1 gauge 3. Set alt F240, set speed (open window ) 240kts, LVL CHG 4. HDG off track, 15° aob and HDG SEL... Now you are safe. 6. N1 page, set CON 7. VNAV eng out get speed and alt 1. fine tune MCP Identify the problem and go from there. If you have a fire you can even delay 5,6 or ID problem before 5,6 and triage. Mem items complete Terrain Fuel Time ATC. NNCL
49
Fuel Spill
Spill within 15m of aircraft likely to cause fire? Probably reverse boarding back to terminal, pax must remain 15m from spill. power units shutdown Maintenance stop fuelling stop no eng start notify ATC 22.8 When a fuel spill of any quantity likely to create a fire hazard occurs within 15 m of the aircraft, the regulations require that the Pilot In Command must ensure that any passengers on board or in the process of embarking or disembarking the aircraft, are moved to a point at least 15 m from the fuel spill. Practically, this may mean ceasing passenger embarkation and/or requiring all passengers and crew to disembark the aircraft to the safety of the terminal. Until the fuel spill is removed, the Pilot In Command, as far as possible, will ensure that: -all power units, vehicles and power loading devices within 15 m of the fuel spill, are shut down; -any maintenance being performed on the aircraft is ceased; -refuelling of the aircraft is ceased. -The aircraft engines must not be started within 15 m of a fuel spill. Fuel spills should be reported to air traffic control and/or the ARFFS. A Pilot Report may be required.
50
Thrust reverser remains unlocked on Ground.
FAM 22.16.4 Thrust Reverser(s) Remain Unlocked If a thrust reverser remains unlocked on the ground, shut down the affected engine(s) prior to approaching the gate or stand-off parking area. This prevents jet blast damage to property and/or personnel, or the ingestion of foreign objects into the engine(s).
51
Overweight landings FAM and 737
How do we Plan? Longest runway, into wind. Contamination and Downslope avoided. Burn off fuel if required for landing distance. OPT required for F15 or less flap, brake energy can be exceeded in this case. - use maximum runway length in these non normal situations F30,F40 landings will not exceed brake energy. How do we fly: Turn at normal manoeuvre speed. Configure long final wings level up to man speed - 20kts - this gives manoeuvre margin but no 15º overshoot (caution LNAV) How do we approach? Don't carry excess speed. Therefore limit ROD. F30 recommended for placard speeds. Final app speeds may be limited by placards Limit descent rate How do we flare? Don't hold off GA if float. How do we Land? Max reverse, ensure SB up. Use full runway How do Taxi? Hot brakes Possible brake fires Standoff bay preferable How do we GA? Min 90% N1 Possibly need tracking via CDP Care on placard speeds 22.16.3.1 As guidance, for the purposes of an Overweight Landing, the following situations are typical of those under which the Captain may elect to land overweight: - Any malfunction that would render the aircraft non-airworthy. - Any condition or combination of conditions (mechanical or otherwise), in which an expeditious landing would reduce the exposure to potential additional problems which may result in a derogation or compromise of safety. - Serious illness of crew or passengers which would require immediate medical attention. 737 Configuring: Turns @ manoeuvre speed. Flap extend level up to Man-20kts for placards. Consider early Gear extension for extra cooling Autoland NOT recommended - in an emergency though it will work Stopping on runway in doubt? - Burn fuel, hold GD burns ~ extra 1000kg hr Longest runway, consider slope, Tailwind. F30/F40 return ok if you took off DRY, for landing distance F30 preferred for return, for increased flap placard margin. Use as low an AB as possible. - use an autobrake setting, consistent with reported runway conditions, that will result in the use of all available runway length. A stopping distance safety margin should be used in accordance with Company policy. Although the autobrakes initially increase brake temperature, the brake contribution is minimized after reverser deployment Don't carry excess airspeed on final. Don't Float Ensure SB on TD Max Reverse asap after TD + SB Use maximum amount of runway. Stopping assured AB disco and use revers
52
Counter Threat Response Model levels
1 Verbal abuse 2 Physical Assault 3 Life Threatening 4 Attack on Flight Deck
53
Flight Deck Lockdown
Flight deck door is to remain closed and locked till on ground. You may allow opening only to allow the minimum crew complement to be on the flight deck - must be risk assessed. When determining the risk, Flight Crew in conjunction with the IOC (where possible) must be sure that the scenario that caused the lockdown is under control. Crew must ensure that unauthorised persons cannot reach the flight deck door during the time it is being opened and closed. This may be achieved by the following: Use of catering carts and other hand held equipment to barricade the aisle(s); Cabin Crew positioned between the passengers and the flight deck door; The first 5 rows cleared of all passengers. Before the flight deck door is opened, the Pilot Flying will apply standard flight deck access protocols and ensure that the door is opened only when satisfied that the security of the flight deck is assured. This should involve verification that no unauthorised persons are in the vicinity of the flight deck door. The Flight Crew will make an interphone call to inform all crew that a flight deck lockdown is in effect.
54
Crew Action Level 1/2 Threat
Pilots: - Consider Lockdown Cabin Crew: - Verbal defuse - Use all resources ABPs etc - Use necessary force to manage threat - Consider collusion - Evasion and Separation Lockdown remains till on Ground if invoked
55
Crew Action 3/4
Pilots: - Lockdown Cabin Crew: - Use all resources ABPs etc - Use necessary force to manage threat - Evasion and Separation - Hostage Survival techniques, delay tactics Lockdown remains till on Ground
56
Hijack Inflight
Lockdown use all resources use all necessary force to 'repel and subdue' ATC. Squawk appropriate code. Datalink send Emergency Report > ‘PAN’ message. If armed intervention is required send Emergency Report > ‘MAYDAY’ message. Consider BOMB ON BOARD and activate the Suspicious Article Action Plan. If possible maintain contact with Cabin Crew members by any appropriate means. Land as soon as practicable at the nearest available airport. Contact Qantas Security and Investigation Services with relevant threat information via Satcom/VHF/HF radio.
57
Birdstrike short Final
If the landing is assured, continuing the approach​ to landing is the preferred ​option.​ If more birds are encountered, fly through the bird​ flock and​ land. - Maintain as low a thrust setting as possible. ​- If engine​ ingestion is suspected, limit reverse thrust on landing to​ the amount ​needed​ to​ stop on the runway. - Reverse thrust may increase engine damage, ​especially when engine vibration or high​ EGT​ is indicated.
58
Items requiring confirmation:
The word “Confirm” is added to checklist items when both Flight Crew members ​must​ verbally agree before action is taken. During an inflight non-normal ​situation, verbal confirmation is required for:​ •​ an engine thrust lever​ •​ an engine start lever​ •​ an engine, APU or cargo fire switch​ •​ a generator drive disconnect switch​ •​ an IRS mode selector, when only one IRS is failed​ •​ a​ flight control switch​ This does not apply to the Loss of Thrust on Both Engines checklist.​ Confirmation is not​ needed for completion​ of non-normal​ checklist items when on ​the ground.​ There is no requirement for specific words to say during​ a confirm step or for ​physical actions such​ as touching​ or pointing to a control.
59
Land at nearest available and Immediate landing
22.1.7 Available Airport An Available airport is an airport which in the judgment of the Captain is appropriate for landing in terms of weather, airport conditions and runway length, at the time of the intended landing.
60
Circuit Breaker reset rules What ones can never be reset?
Flight crew reset of tripped *fuel pump and fuel pump control​* circuit breakers in flight is prohibited. In flight, reset​ of a tripped circuit ​breaker is​ not​ recommended. However,​ a tripped circuit​ breaker may be ​reset once, after a short cooling​ period (approximately 2 minutes), if in ​the judgement of the captain, the situation resulting from the circuit​ ​breaker trip has a significant adverse effect on safety. On the ground, ​flight crew reset of a tripped circuit breaker should only be done after ​maintenance has determined that it is safe to reset the circuit​ breaker.
61
onside FMC Fail RNP app
"Nav problem" "Switching FCC" - engage offside AP, or select offside FD Push LNAV "LNAV" Wind alt to mins Push VNAV - "VNAV" Wind alt to MAP Call FMA's, missed alt set... After failure and LNAV/VNAV re-engaged: - "remaining within NPS limits" Better instruments on XXX side - handing over if required. Identify the problem: (AP remained eng in CWS) VTK flags X side CDU either L&R for Lfmc or R for Rfmc "L/R FMC failure" ... Switching is available TOGA to LNAV not available, select Lnav @ 400' We have: - 1 navigation sys display - No integrity problems - within NPS limits Are you happy to continue? Switching is available. - Visual day ok - above 2000' ok otw imho fuck that if everything is tickety boo...
62
FMC disagree RNP app What other messages mean the same?
FMC disagree is a go around IMC. Verify Pos, and unable required NAV perf rnp. All mean a loss of integrity. FMC Disagree: - During approach or on the ground, monitored parameters required for dual FMC operation are in disagreement. Verify Pos: - Position information is contradictory Unable reqd nav perf RNP: - Actual nav performance is not sufficient. If you meet visual approach requirements and have RIS then you can continue. At night are you in the circling area? 5.28nm,4.2nm…. 10nm on final/14 if ILS runway not below onslope papi tvasis 14… well with that one why aren’t you flying an ILS in that case….?
63
Dual FMC Failure RNP app
DUAL FMC fail You have 30s of nav info, try to memorise mud map. Immediate GA max thrust GPWS climb to MSA if in terrain rich environment.
64
onside IRS Fault RNP app
"Nav problem" "Switching FCC" - engage offside AP, or select offside FD Push LNAV "LNAV" Wind alt to mins Push VNAV - "VNAV" Wind alt to MAP Call FMA's, missed alt set... After failure and LNAV/VNAV re-engaged: - "remaining within NPS limits" Better instruments on XXX side - handing over if required. Identify the problem: (AP kicks out - stays out) Master Caution IRS L/R IRS fault light ATT, HDG, VERT, FPV flags (lost horizon) Autobrake disarm light "L/R IRS fault" At some point disco AT... ... Switching is available TOGA not available on missed approach. - Manual flight, use level change do not descent. TOGA to LNAV not available, select LNAV at 400' Set AB to off We have: - 1 navigation sys display - No integrity problems - within NPS limits Are you happy to continue? Switching is available. - Visual day ok - above 2000' ok otw imho fuck that if everything is tickety boo...
65
DEU Failure RNP app Indications?
"Nav problem" "Switching FCC" - engage offside AP, or select offside FD Push LNAV "LNAV" Wind alt to mins Push VNAV - "VNAV" Wind alt to MAP Call FMA's, missed alt set... After failure and LNAV/VNAV re-engaged: - "remaining within NPS limits" Better instruments on XXX side - handing over if required. Identify the problem: (AP remains CWS) Master caution Eng - EEC's in alternate Display source flag Speed lim flag lost low speed bricks Hyd pressure A/B side blank "DEU 1/2 Fail" ... No switching available. TOGA not available in GA (from videos...) We have: - 1 navigation sys display - No integrity problems - within NPS limits Are you happy to continue? Switching is available. - Visual day ok - above 2000' ok otw imho fuck that if everything is tickety boo...
66
Fuel imbalance, maybe leak
Check nothing funky set on fuel panel - are your pumps on? Note each main tank QTY and start time. Check 3 things if you are not going to do checklist. Fuel flow abnormal? Fuel used + FOB = Departure fuel +- 600kg. Amount of fuel left compared to what you should have planned on OFP. then... Call CSM and ask if there is anything unusual streaming from engine. Change of fuel imbalance of 230kg in 30 mins or less is bad news.
67
EEC alternate mode cautions? N1 N2 limits, EGT limits, Thrust lever position? Can you use AT?
If in Alternate mode you can reach max thrust before full forward - only use full forward in emergency. N1 and N2 protection always supplied by EEC Norm and Both Alt EGT protection never supplied by EEC, Norm and both Alt. AT good for all modes. But recommend both in same mode to prevent lever split. Why would you op in different modes I aint sure…
68
Hyd Systems
Both AREEFAT Ailerons, Rudder, elevator, elev feel, flt spoilers, AP onside, TR onside. A GPLAN Ground spoilers, PTU, Landing gear, alt brakes, NWS You lose autoland, req manual gear ext, no retraction, consider icing and perf B FLAABY Flaps, LGTU, Autoslats, alt NWS, Brakes Normal, YD You lose autoland, autobrake, slow manual flaps and LE will remain ext, consider icing amd perf Stby LYRR LE Flap slat (ext only), Yaw Damper (stby), Reversers, Rudder
69
Engine limit exceedance on TO, Take off continued.
If an engine exceedance occurs after thrust is set and the decision is made to continue the takeoff, do not retard the thrust lever in an attempt to control the exceedance. Retarding the thrust levers after thrust is set invalidates takeoff performance. When the PF judges that altitude (minimum 400ft AGL) and airspeed are acceptable, the thrust lever should be retarded until the exceedance is within limits and the appropriate NNC accomplished.
70
Thrust setting on TO, N1 tolerances.
+4 /+-2/-0+1 The PM should verify that takeoff thrust has been set and the throttle hold mode (THR HLD) is engaged. A momentary autothrottle overshoot of 4% N1 may occur but thrust should stabilize at +/- 2% N1, after THR HLD. Thrust should be adjusted by the PM, if required, to - 0% + 1% target N1. Once THR HLD annunciates, the autothrottle cannot change thrust lever position, but thrust levers can be positioned manually. The THR HLD mode remains engaged until another thrust mode is selected.
71
Inbound ctaf area call, 80nm out
Area Call, on centre freq. _____centre and_____traffic B737 Q______ xxx dist segment/radial ib passing FL____ ______@______z _______tfc.
72
8min, 35nm ctaf inbound.
Inbound call @ 35nm/ 8mins (rms) _____traffic B737 Q_____ seg,radial,dist/alt intentions landing ______@______z be ready for tfc
73
pre taxi call ground ctaf departure.
Taxi call ATS ________Traffic B737 IFR taxi QF_______ For Dest Runway_____
74
Airborne from ctaf call
Traffic departure call ctaf _______ traffic B737 Q_____ segment,radial,dist tracking_______radial passing_____for_____ ____@_____z (first rep point) location Expect ID: OB segment dme from _______ Passing__________for___________ _____@_________z (first reporting point)
75
Holding Procedure Oz speeds
Up to and including 140 = 230 abv 140 up to including 200 = 240 abv 200 = 265
76
Single and double GPS failures on PBN app
If you get a gps L or R invalid WITHOUT a master caution it’s all good, you can COMMENCE approach (this is not a receiver failure) MC and GPS light comes on with recall = single gps fail MC and GPS comes on and stays on after MC cancel = dual GPS failure.
77
GPWS inop or Terr fail on PBN Approach
78
RA fail on PBN app? Single and double
79
Wind shear PA from GA
Hey Folks from the flight deck this is your Captain speaking. There was a change in wind conditions on the ground in XXX that resulted in us having to discontinue our approach. [And while they might feel unusual from the cabin] These are standard and safe manoeuvres that we train for regularly. We’re now returning for another approach and expect to land shortly. Qantas ground staff have been informed of the delay and are currently working on your onwards travel plans. As always thank you for you continued patience, Once again we'll be landing in XXX in approximately xxx mins..
80
GA from ATC
G’day from the flight deck folks your Captain speaking. Air Traffic Control asked us to discontinue our last approach so we now require to manoeuvre for approximately another 20 minutes before we land in XXX Qantas ground staff have been informed of the delay and are currently working on your onwards travel plans. As always, Thank You for you continued patience, Once again we'll be landing in XXX in approximately xxx mins..
81
Return to land Unruly Pax
Hey Folks from the flight deck this is your Captain speaking. We’ve encountered a situation on board that requires us to return to our departure airport. This decision is being made with your safety and comfort as our top priority. We ask that you remain calm, remain seated with your seatbelt fastened, and follow all your crew members instructions. We expect to be on the ground shortly and appreciate your cooperation and understanding.” Qantas ground staff have been informed of the delay and are currently working on your onwards travel plans. As always thank you for you continued patience, Once again we'll be landing in XXX in approximately xxx mins..
82
Diversion/return smoke in cabin PA
Hey Folks from the flight deck this is your Captain speaking. We’re experiencing some smoke in the cabin and, as a precaution, we’ll be returning to our departure airport. [Diverting to XXX airport] This is just a standard safety precaution because, as always, your safety is our top priority. Our crew is fully trained to manage this type of situation, and we’re working closely with air traffic control to get us back on the ground quickly and safely. "Please remain seated with your seatbelt fastened, and follow all your crew members instructions.' Qantas ground staff have been informed of the delay and are currently working on your onwards travel plans. As always thank you for you continued patience, Once again we'll be landing in XXX in approximately xxx mins..
83
Standard Malfunction PA
Hey Folks from the flight deck this is your Captain speaking. We've experienced a technical difficulty that require us to return/divert to land in XXX. This is just a standard safety precaution because as you know at Qantas your safety is our top priority. ”Qantas ground staff have been informed of the delay and are currently working on your onwards travel plans.” "So we ask you now to remain seated with your seatbelt fastened, and follow all your crew members instructions” As always thank you for you continued patience, Once again we'll be landing in XXX in approximately xxx mins..
84
Volcanic Ash
Turn, descend and don, thrust off with ign on - Exit the volcanic ash as quickly as possible. - Consider a 180° turn. Consider a descending turn. 1 Don oxygen masks and smoke goggles, as needed. 2 Establish crew comms. 3 Autothrottle (ie) . . . . . . . . . . . Disengage If conditions allow, run the engines at idle thrust. 4 Thrust levers (both) . . . . . . . . . . . . . . . . . . . . . Close This reduces possible engine damage or flameout, or both, by decreasing EGT. 5 ENGINE START switches (both) . . . . . . . . . . FLT 6 PACK switches . . . . . . . . . . . . . . . . . . . . . . . . . HIGH 7 ENG ANTI–ICE switches (both) . . . . . . . . . . . . ON 8 WING ANTI–ICE switch . . . . . . . . . . . . . . . . . . . ON 9 APU start Consider Loss of thrust on both engines speeds At or above FL270, set airspeed to 275kt. Below FL270, set airspeed to 300kt.
85
PRM breakout
Brief the procedure TCAS, follow RA AND breakout heading. "Auto wailer volume" Autopilot: - Use AP for approach. Wailer - Don't disco AP till atc has topped jabbering otw wailer will drown him out Volume - Both VHF on same volume Breakout the 3 and 3: PF: 1. Disco AP (keep AT) (wait till ATC tx finished) 2. turn to heading - consider 15º 3. Init climb or descent as req... - 1000fpm max descent... PM: 1. FD's, 2. set hdg, 3. set alt... - Ack atc - PM FD on, basic modes (hdg sel, v/s)...all good? - PF FD on PF AP on... Transition to GA if required. - I guess if you are going to do this do it before you re-engage AP! It works quite well two engine just setting up a 1000fpm climb and @ 1000' bugging up and saying we are in the GA F15, +ive rate GU etc... worked well in sim... The instinct is to reset both FD's is this is what you do with uprt etc, just reset PM's first.
86
Landing Gear Lever Will Not Move Up After Takeoff
LANDING GEAR lever​ ​ . . . . . . . . . . . . . . . . . .​ DN​ ​ Retract the flaps on schedule….. Then:
87
Considerations for Wing body overheat. Bleed Trip Off, Or Pack failure
Drive up cabin temps to let remaining pack have a chance. Consider getting out of icing conditions for bleed or wing body overheat. If you get a Pack because you made remaining pack work too hard, wind up temps and attempt trip reset by memory…
88
Low speed in a hold, ie a turn
Low Speed event in hold etc: - 'Low speed' 'Confirmed" - Fair heading and hdg sel - ie wings level reduce load. - Consider disconnecting AT to keep thrust up - Ie disconnect AT and push thrust to amber bands - Call for continuous thrust - just set it to your amber bands... - Alt below you and level change - Fine tune thrust at mct once N1 bugged. - Notify ATC Disconnect and normal stall recovery if severe...
89
Spd lim flag and speed trim fail light after engine severe damage?
With an N1 sudden seizure, SPD LIM amber flag is annunciated, yellow and red bands are removed from the speed tape and same side AFDS pitch modes LVL CHG, V/S and VNAV are not available. Place the failed engine’s Start Switch to CONT to remove the SPD LIM flag and to restore AFDS pitch modes, or use the opposite A/P.
90
Oceanic contingency non weather
91
Smoke smell in the cabin - what do you ask?
ANY report of fumes don masks immediately. Tell csm to switch off ife, and notify lights may go off. turn off ife, shed galleys? Source not Immediately obvious accessible extinguishable CSM questions is it: Immediately obvious accessible extinguishable where is it located? Oven, chiller, coffee pot, lav? Forward or aft of wing - doors? (Overhead risers @ doors 3 Visible? Colour? Smells like? Anyone coughing? Eyes stinging? Shortness of breath? Feel panels, floor - any heat Can you hear anything? Tell the csm that there may be some light switching, reading lights should still work.
92
Fan Ice removal supp pro
Most of the time read and do? Engine start switches continuous… Engine High Vibration leads you here too.
93
Missed approach requirements PBN approach.
Go-around/missed approach​ is required for any of the following:​ •​ Outside NPS limits​ •​ Loss of integrity (UNABLE REQD​ NAV​ PERF-RNP, FMC​ ​DISAGREE​ or VERIFY​ POS message)​ •​ Less than one Navigation System Display. NSD = one FMC​ one MCDU​ one PFD one​ ND​ one F/D
94
Display Control Failure RNP approach
"Nav problem" "Switching FCC" - engage offside AP, or select offside FD Push LNAV "LNAV" Wind alt to mins Push VNAV - "VNAV" Wind alt to MAP Call FMA's, missed alt set... After failure and LNAV/VNAV re-engaged: - "remaining within NPS limits" Better instruments on XXX side - handing over if required. Identify the problem: (AP kicks out - can re-engage) Display control panel flag Alt flag and lost Alt tape "DCP 1/2 Fail" ... Switching is available We have: - 1 navigation sys display - No integrity problems - within NPS limits Are you happy to continue? Switching is available. - Visual day ok - above 2000' ok otw imho fuck that if everything is tickety boo...
95
FMC DISAGREE –VERTICAL
Condition: One of the following has occurred: • Left FMC and right FMC target airspeeds disagree during descent • Left FMC and Right FMC vertical paths disagree during descent The vertical disagree will most likely be corrected when crossing a waypoint with an altitude constraint. If the disagreement remains when entering the ‘ON APPROACH’ phase, the FMC DISAGREE-VERTICAL will be replaced with the FMC DISAGREE messaging. This message will only appear when the FMC has transitioned to ‘On Approach logic’.
96
Vdev event
non saftey, fmc flattens out path passing a at or above waypoint into a coded descent angle and you have a trigger event fmac can do this recalc. trigger = config change, ai on, rf leg calc - ie fmc thinking :) recommendation to leave isa dev page blank
97
Moderate to heavy rain
ICATA Ign Continuous AT off Thrust move slowly Slow down APU - consider starting.