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B737 FLOWS & PROFILES > Flows & Profiles > Flashcards

Flows & Profiles Flashcards

1
Q

Before Push

A
  • KA GND TX ENABLE switch…………Override
  • Hydraulic Pumps……Checked/On
  • Doors……………………Closed
  • Transponder/Push Clearance……..XPNDR/Request
  • Beacon………On(Push Clear. Received)
  • Sterile Light…………..On
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2
Q

After Start Flow

A

Set Flaps, then:

  • Probe Heat………….On
  • Anti-ice………………As required
  • Trim Air (-800)……On(or off)
  • Air Cond and Press…….Set
  • APU switch………….Off (or on)
  • Recall……………Check A
  • Autobrakes………….RTO
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3
Q

Delayed Engine Start

A

If starting engine No. 1:

  • [F] L PACK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
  • [F] ISOLATION VALVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE

Operation of the right pack during start is permissible. No. 2 engine
may be operated above idle thrust.

  • [F] APU BLEED air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
  • [F] No. 1 engine BLEED air. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
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4
Q

Before Takeoff Flow

A
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5
Q

Takeoff

NADP-2

LNAV/VNAV

A
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6
Q

Takeoff

NAPD-2

HDG SEL/LVL CHG

A
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7
Q

Takeoff

NAPD-1

LNAV/VNAV

A
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8
Q

After Takeoff Flow

A
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9
Q

Descent Flow

A
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10
Q

ILS

A

After cleared for the approach, below the transition level, and no later than immediately following the 2500-foot callout:

  • [PF] “____ (approach), (
    runway) ____, (final approach course) ______,

minimums ____ BARO/RADIO” . . . Announce

  • [PM]“___ in/hPa”. . . . . . . Announce
  • [Auto] “2500” . . . . . . . . Announce

At glide slope capture:

  • [PF]SetTDZE…………………Announce
  • [PM]MCP altitude…………SetTDZE

By 1500 feet or the FAF/FAP/GP Intcpt,

which ever occurs later

  • [PF]Gear down………………….Announce
  • [PM]Landing gear lever……Down

At 1000feetRA:

  • [PM] “1000”…………………Announce
  • [PF]“Set missed approach altitude.

Cleared to land.” or

“Set missed approach altitude.

No landing clearance.”………….Announce

  • [PM]Missed approach altitude……….Set

At 500feet RA:

  • [Auto]“500”………………………………Announce
  • [PF]“Stable”or

“Unstable, going around”……………Announce

At 100 feet above minimums:

  • [Auto]“Approaching minimums”……Announce

At DA:

  • [Auto] “Minimums”………………. Announce

If the runway environment is in sight

and continuing the approach:

  • [PF] “Landing” . . . . . . . . . . . .. Announce
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11
Q

ILS

Autoland

A
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12
Q

NON-ILS APPROACH

A
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13
Q

Visual Approach

A
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14
Q

Go-Around

A
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15
Q

Landing Flow

A
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16
Q

After Landing Flow

A
17
Q

Parking Flow

A
18
Q

V1 Cut

A
19
Q

Engine Failure after V1

A
20
Q

More info V1

A
21
Q

Engine Failure on Final

A
  • Disconnect the autothrottle and the autopilot.
  • Increase thrust.
  • Select flaps 15.
  • PFincrease indicated speed to VREF 30 / 40 plus (-700) 15 knots / (-800/-900) 20 knots.
  • Inhibit the GROUND PROXIMITY FLAP INHIBIT SWITCH
22
Q

S.E. ILS

A
  • Intercept the localizer with flaps 5 at flaps 5 maneuvering speed. When the glideslope deviation is approximately 1½ dots,
  • lower the landing gear,
  • extend f laps to 15,
  • and arm the speed brakes.
  • Fly the approach at flaps 15 target speed
23
Q

S.E. Go-Around

A
24
Q

NON-PRECISION APPROACH (ONE ENGINE INOPERATIVE)

A
  • intercept the final approach course with flaps 5 at flaps 5 maneuvering speed.
  • At approximately 1.0 -1.5 miles from the FAF, extend the landing gear, select flaps 15, reduce speed to flaps 15 target speed and call for the Landing Checklist.
25
Q

UPSET RECOGNITION AND RECOVERY PROCEDURE

A
26
Q

GPWS Terrain/obstacle warning

(Night or IMC)

A

At night or in instrument conditions:

  • [PF] Call “Max thrust, stow speed brakes.”
  • [PF] Disconnect autopilot and autothrottles.
  • [PF] Apply maximum thrust. Move thrust levers aggressively to forward stops.
  • [PF]Simultaneously roll wings level and rotate to an initial pitch attitude of 20°. Do not follow flight director commands.
  • [PF, PM] Retract speed brakes.
  • [PM] Verify all required actions have been completed. Call out any omissions.
  • [PF] Maintain configuration. Do not change flap, gear, or trim position until terrain separation is assured. Only vertical maneuvers are recommended unless the pilot determines, based on all available information, that turning in addition to the vertical escape maneuver is the safest course of action.
  • [PF, PM] Monitor for sustained or increasing terrain separation. Monitor vertical speed and altitude (radio altitude for terrain clearance and barometric altitude for a minimum safe altitude). PMcalls out any trend toward terrain contact.
  • [PF] When clear of terrain, slowly decrease pitch attitude and accelerate.
27
Q
A
28
Q

TCAS “RA”

A

WARNING: A“descend” (fly down) RA issued below 1000 feet AGL should not be followed.

For a CLIMB RA in a landing configuration:

  • [PF] Disengage autopilot and autothrottles.
  • [PF] Accomplish a normal go-around using maximum thrust.
  • [PM] Verify maximum thrust is selected while accomplishing normal PM go-around duties.
  • [PF, PM] Visually acquire intruder, if able. For all other RAs:
  • [PF] Disengage autopilot and autothrottles.
  • [PF] Adjust pitch attitude. Establish or maintain a pitch outside of all RPAAs. Adjust thrust manually to keep airspeed in an acceptable range. Maintain pitch attitude that complies with the RA (outside all RPAAs) and deviates least from ATC clearance.
  • [PF, PM] Visually acquire intruder, if able.
  • [PM] Advise ATC. Use the phraseology, “TCAS RA.”
  • [PF, PM] Maintain a pitch attitude clear of RPAAs. If needed, strengthened RA guidance (e.g., “Climb, climb now”) will be issued if the miss distance does not increase after the initial RA. When “Clear of conflict” message is heard:
  • [PF] Return aircraft flight path to ATC clearance. PM notifies ATC of the return to clearance if a TCAS RA or TCAS descent was initially reported.
  • [PF] Set autopilot and autothrottles as desired.
29
Q
A
30
Q

Rejected Takeoff

A
31
Q

Windshear Recovery

A

B737 FLOWS & PROFILES (2 decks)

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