2025 RTS-Even Flashcards

(22 cards)

1
Q

TCAS RA

A

Remember to disengage A/P and A/T, then report the RA to ATC. Mention you will need to do a CERS report

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2
Q

Low visibility TAKEOFF

A

*verify “ground roll”
*”centerline” if deviating

Use of these procedures is required with less than 500 RVR (150 m) on runways
supported by 300 RVR (75 m) takeoff (refer to Jeppesen 10-9A page). Requires any
two of following three transmissometers. All reporting transmissometers are
controlling.
— Touchdown: 300 RVR (75 m)
— Mid-field: 300 RVR (75 m)
— Roll-out: 300 RVR (75 m)

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3
Q

GUSTY CROSSWIND TAKEOFF

A
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4
Q

REJECTED TAKEOFF

A
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5
Q

V1 CUT

A
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6
Q

HOLDING

A

Request relief from holding speed since you’re above the 200 knot limit and reset the
cruise altitude on the VNAV page if you get an altitude conflict.

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7
Q

2-Engine CAT I approach

A
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8
Q

SINGLE ENGINE CAT I APPROACH

A

SPOT 5: CA Flies. Non-HUD SE CAT I ILS Approach, autopilot off. Landing with gusting crosswind.
After landing, call “single reverse”

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9
Q

CAT III APPROACH

A

Vectors to ILS 16L CAT III. WX ¼SM, 6/6/INOP.

Review AOM CAT III pages (10.5.2) and as a technique, mention the SMGS 1200-500 RVR
taxi page when you do the approach brief. Landing full stop.

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10
Q

RNAV (RNP) AR Approach setup

KSEA RNAV (RNP) Z 16R

A

Run all RNAV/RNP checks (20-7 pages, confirm RAIM prediction, 0.15 and 125, VOR updates off, coded GP, etc.). If you are in a non-NPS sim, it does not allow you to enter the 125 VERT RNP, so the PM must monitor PROG page 4.

Make sure you comply with the 210 knot restriction at VASHN. After cleared the approach at 4K with
LNAV/VNAV/VNAV PATH and minimums set, we were vectored off the approach and told to
maintain 4K. Make sure you reset the MCP altitude back to 4K or the VNAV path will start your
descent. As soon as we caught the altitude, we were re-cleared the approach – make sure you set
the minimums back in the MCP (if on LNAV/VNAV/VNAV PATH). Make sure you’re below 180 KIAS
on the final approach section (RNAV/RNP limit).

Missed approach with very little time to hit the 2000 missed approach altitude, so your VNAV will go into altitude capture mode which opens up the speed window - call for PM to roll speed to 220 if you don’t want to get fast. After level off, AUTOTHROTTLE DISENGAGE. (Wind additive)

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11
Q

LOC Approach

A

Spot 2: FO Flies. Low visibility (1600 RVR) takeoff. Similar to spot 1, TCAS RA and vectored off SID to
nose high upset recovery.

Vectors to 16R LOC (set DDA) to a go-around – remember again the quick
level off.

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12
Q

Landing with Gusting Crosswind

A
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13
Q

Single Engine Landing

A
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14
Q

EET Upset Recoveries (Maneuver-based, CA)

A

Avoid rudder at high altitudes

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15
Q

Fire/Overheat Non-Normal (FO and CA)

A

Spot 2- FO Flies. Low visibility (1600 RVR) takeoff. Similar to spot 1, TCAS RA and vectored off SID to
nose high upset recovery. Vectors to 16R LOC (set DDA) to a go-around – remember again the quick
level off. After level, expect ENGINE FIRE/OVERHEAT DETECTOR FAULT (there are no checklist items,
just a condition note). Vectors to RNAV (RNP) Z 16R to a landing.

Spot 3: 16L KSEA departure. CARGO FIRE below V1. CA: “REJECT, my aircraft”, throttles,
speed brakes, reversers in that order (habit pattern is to do throttles, then reversers – don’t!). FO
calls “Deployed”, “80” and “60”, then “Mayday mayday mayday” to tower and get flaps 40 once
stopped. Once stopped, CA calls, “This is the Captain, Remain Seated, Remain Seated, Remain
Seated,” and FO call for Mayday and ARFF. Run the checklist – the fire will not go out, so call for
evacuation and run the evacuation checklist.

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16
Q

Hydraulic Non-Normal
(Look up in debrief)

17
Q

TCAS RA

Climb RA in Landing Configuration

18
Q

AUTOTHROTTLE DISENGAGE. (Wind additive)

A

If the autothrottle is disengaged, or is planned to be disengaged prior to landing, the recommended method for approach speed correction is to add ½ of the reported steady headwind component plus the full gust increment above the steady wind to the reference speed.

19
Q

No HUD V1 cut (Engine Fire)

A

HUD-Off takeoff with ENGINE FIRE/FAILURE after V1. Select HDG to continue
straight (<14.2 miles). Engine failure is not on the QRC (straight to the QRH), but most Sim-Ps/CKP
want you to reference the QRC.

Practice the litany for running the QRH; PM reads entire checklist
step (ex: “Thrust lever, affected engine, confirm, close”) then PF will touch, but not move, affected
thrust lever and say, “Thrust lever #1/2, confirm”. Then PM confirms PF touches the correct thrust
lever and says, “Confirmed” and PF closes the thrust lever and say, “Closed”. In each step,
“confirmed” is said three times. PF accomplishes the first two steps (autothrottles off, thrust lever
closed) and PM accomplishes the rest (engine cutoff, etc.).

This spot is long because there are a lot
of checklists to go through. After all engine checklists are run, CA gives PF duties to FO to run non-
routine landing consideration checklist.

HUD-Off SE Cat I ILS 16L approach to a go-around or missed
approach.

20
Q

Single Engine Go Around

21
Q

Wind shear- landing

A

Spot 8: CA Flies. 16L ILS SEA. Windshear on short final. You may start to get indications (airspeed
deviations) around 400-500’. Gusty winds may mask initial indications, but if the airspeed drops
considerably or you get audible warning, call “Escape”, TOGA, max power. PM should call out RA
altitude and whether we are climbing / descending. If you Go-Around early (prior to windshear
warning), you can start to deconfigure, otherwise don’t deconfigure until clear of windshear.

22
Q

Wind shear- takeoff

A

-If there is insufficient runway left to stop, initiate a
normal rotation at least 2000 feet before the end of the runway even if airspeed
is low
-Consider increasing VR speed to the performance limited gross weight rotation
speed, not to exceed actual gross weight VR + 20 knots. Set V-speeds for the actual
takeoff weight. Determine VR based on the TPS MTOW for the runway and flap
configuration from the value in 6p.7 Takeoff Data. Delay rotation to the adjusted
(higher) rotation speed. This increased rotation speed results in an increased stall
margin and meets takeoff performance requirements. If windshear is encountered at
or beyond the actual takeoff weight VR, do not attempt to accelerate to the
increased VR but rotate without hesitation.