Stablization Flashcards

1
Q

At what Alt should you be stabilized ?

A

Planned landing configuration by 1500 ft. AAL

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2
Q

When is an app considered stable @ 1k AAL (L F S R P C)

A

A. Landing configuration (L/G dwn, F flap SPB Arm.

B. Final approach path, lat & vert

C. Command speed -5 to +10 KIAS.

D. Rate of des (NOP)

E. Power setting is appropriate for the aircraft’s configuration.

F. Lnd C/L

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3
Q

Wt Are Stabilized app Add guidance:

“Prevailing conditions: Wind Change & turb altitudes shall be based on the LANDING ALTITUDE At 1,000 ft AAL PM shall call “

A

“STABLE/NOT STABLE”

” below 1,000ft AAL G/A announces a Go-around”

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4
Q

What are the Stabilized Approach Criteria Exceptions ?

A

Complying wt ATC Speed Planned target approach speed by 500 ft. AAL
< 4NM

Turn required for lateral alignment Wings LvL by 400 AAL or OMC

Arm Spd Brk < 1K max 500 AAL + ASR (Exceptional)

Lnding C/L < 1k max of 500 AAL (Exceptional)

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5
Q

When Manv below 1k be aware of:

A

Des Rate
Left/ R center Line (displacement)
Tail wind Xwind component
RWy lenght available

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6
Q

As the Airplane crosses Rwy threshold it should be:

A

App spd within +10 until arresting Stab Flt path

Make landing within 3k or 1st 3rd of Rwy

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7
Q

Landing Procedure - G/S from Above

A
Arm APP 
Set the MCP altitude 1000 feet AGL above touchdown
Loc cap B4 des
 Select V/S mode (0)
LND config (Grdn FPs 20)

Spb Brk control spd
V/S 2000 >2000
G/S capture set the missed approach altitude in the MCP

If G/S is not captured by 1,000 feet above touchdown or ALT engages at anytime, execute go-around

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8
Q

At 1000 feet AAL PM Calls?

A

“1000 STABLE” or “1000 NOT STABLE”

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9
Q

IAS Deviations - Below 1500’ AAL

A

“+10/-5 kts from bug speed “SPEED”

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10
Q

Rate of Descent >1000 ft.min Below 1K PM Call

A

“SINK RATE”

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11
Q

Pitch Attitude Deviation below 1500 AGL

A

+7.5 Nose Up

-2.5 Nose Down

-0.0 Nose Down below 1000 ft
“PITCH”

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12
Q

Bank Angle > 7° PM Call:

A

“BANK”

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13
Q

Localiser Excess Deviation Warning or 1 Doton the PFD

A

“LOCALIZER”

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14
Q

Glideslope Excess Deviation Warning or 1/2Dot on the PFD

A

“GLIDESLOPE”

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15
Q

Max rate of Descent to 5k

A

5000 fpm

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16
Q

Max rate of Descent to 5k-3k

A

3000 fpm

17
Q

Max rate of Descent to 3k-1000

A

2000 fpm

18
Q

Max rate of Descent From 1K- landing

A

1000 fpm