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B737 > B737 Limitation Memory Items & Good To Know > Flashcards

B737 Limitation Memory Items & Good To Know Flashcards

1
Q

Maximum Takeoff and Landing Tailwind Component

A

15 knots

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2
Q

Vmo/Mmo

A

340KIAS / .82M

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3
Q

TURB Penetration Speed

A

280KIAS / .76M

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4
Q

USE OF AIL TRIM IS PROHIBITED WHEN AP IS ENGAGED

A
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5
Q

WHAT IS MIN ALTITUDE FOR AP ENGAGEMENT ?

A

400 FT

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6
Q

WHAT IS THE MIN HEIGHT SINGLE CHANEL AP CAN BE ENGAGED UNTIL?

A

50 FT

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7
Q

AUTOLAND MAX WIND SPEEDS?
- HW
- X-WIND
- TW

A

HW - 25 KTS
X-WIND - 20KTS (723-852)
TW - 15 KTS

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8
Q

MAX GLIDESLOPE ANGLE FOR AUTOLAND ?

A

3.25 AND 2.5 DEGREES RESPECTIVELY??

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9
Q

WHAT FLAP SETTINGS CAN YOU USE AUTOLAND WITH?

A

AEO - FLAP 30 & 40
OEI - FLAP 30 only

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10
Q

WHEN CAN YOU NOT USE LEVEL CHANGE ?

A

ON FINAL APPROACH BELOW 1000FT AFE

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11
Q

MAX ALT WITH FLAPS EXTENDED ?

A

20,000FT

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12
Q

CAN YOU HOLD IN ICING CONDITIONS WITH FLAPS EXTENDED ?

A

NO

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13
Q

WHEN CAN YOU NOT DEPLOY SPEEDBRAKES ?

A

WHEN RADIO ALT IS LESS THAN 1000 FT

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14
Q

APU USGAE:
- GROUND
- APU BLEED
- APU ELEC

A

GROUND - APU BLEED + ELEC LOAD UP TO 15,000’
- APU BLEED - MAX ALT 17,000’
- APU ELEC LOAD - MAX 41,000’

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15
Q

At 14nm ?

A

Flaps 1

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16
Q

At 12nm ?

A

Flaps 5

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17
Q

At 2000’ AFE ?

A

Gear Down
Flap 15

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18
Q

At 1500’ AFE

A

Flaps 30/40
“Landing checklist”

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19
Q

How long after engine start until take off power can be applied ?

A

2 minutes

3 mins for MAX (31 degrees) 3 min @ 0degrees will reach above 31 degrees

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20
Q

Max EGT engine start ?

A

725 degrees

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21
Q

4 conditions to abort engine start ?

A

No EGT rise within 15 seconds or 725 degrees exceed

No n1

No Oil Pressure rise

No n2

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22
Q

High speed reject reasons >80kts

A

Engine failure and or fire
Predicted wind shear
Aircraft unsafe to fly (jammed controls usually)

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23
Q

Max time windshield heat ON during ground ops ?

A

45 mins

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24
Q

Length

A

39.5

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25
Q

Wingspan

A

35.9

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26
Q

Height

A

12.5

Top tail - 14.3

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27
Q

GSR per nm

A

6kg
8kg OEI
10kg Depress

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28
Q

VA speed limit below 3000’

A

210kts

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29
Q

Severe turbulence actions

A
  1. Yaw damper ——- ON
  2. AT ——- disengage
  3. AP ——- CWS
  4. Start switches ——— FLT
  5. Thrust ——- Cruise Turb N1 speed (FMC) or 280kts/0.76
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30
Q

Min cruise speed

A

Vref40 + 70

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31
Q

Standard descent speed

A

280kts

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32
Q

Max speed window heat inop below 10,000’

A

250kts

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33
Q

APU failure and Drive failure. Should be a mayday as only 1 electric source now available

A

Land at nearest sweetable airport

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34
Q

Max speed gear extension

A

270kts

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35
Q

Max speed extended

A

320kts

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36
Q

Max speed retraction

A

235kts

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37
Q

Max wind speed doors opened on ground ?

A

40 knots

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38
Q

Fuel total capacity

A

20896kg

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39
Q

Centre tank capacity

A

13066kg

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40
Q

Tank 1 and 2

A

3915kg each

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41
Q
  1. Max operating EGT APU
  2. Max Continuous EGT APU
A
  1. 760
  2. 710
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42
Q

Max EGT on engines ?

A

925 degrees

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43
Q

EGT for
- Max Cont Thrust
-Engine restart in flight

A

950

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44
Q

What altitude is APU not recommended to be started above ?

A

25,000’

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45
Q

What should be be done above FL300?

A

Bank to 10 degrees
And
Speed maintained +10kts above bottom of amber speed band

46
Q

Visual Circuit technique

A

1500’ AGL

Enter circuit @ 180KIAS and Flaps 5

Abeam Threshold - Timing (45 secs) and Gear Down Flap 15
(If higher than 1500’AGL add additional 3 secs per 100’)

Descent rate GS / 2 = FPM (eg: 160kts GS = 800fpm

47
Q

Take off Briefing

A
  1. MEL, DEFECT, NOTAMS
  2. Non normal briefing
    - LH or RH seat takeoff
    - Flap setting, assumed method, V speeds.
    - Prior to 80kts (Reject or Continue)
    - Above 80kts (4 reasons why)
    - Actions for REJECT
    - Actions if CONTINUE - Single engine procedure (also put in relevant FIX’s into FMC)
    Suitable alternate for return
  3. Normal Brief - TAXI, SID, any other operational points
48
Q

WHAT FLAP SETTING IS USED FOR OEI LANDING ?

A

FLAPS 15

49
Q

WHAT FLAP SETTING IS CALLED FOR DURING OEI GO AROUND ?

A

FLAPS 1
CHECK THRUST

50
Q

Phraseology for calling memory items

A

“Memory items, ————— checklist”

Eg: “Memory items, engine fire or severe damage or separation checklist”

51
Q

2D APPROACH USING VNAV PROCEDURE

Note be Flaps 5 prior to Intercept of Final App CRS

A

2nm from FAF -

Set DA or MDA
Select or verify VNAV
Speed intervention ??
Gear Down
Flaps 15
ARM SPD BRAKE

@ FAF -

Landing Flap

300’ BELOW MAP ALTITUDE -

Set the missed approach altitude

52
Q

2D Approach Procedure using V/S

Note be Flaps 5 prior to Intercept of Final App CRS

A

2nm prior to FAF -

Set MDA
Gear down
Flaps 15
Arm SPD BRAKE

@ FAF
Landing FLAP
Select V/S (if profile starts here)

Approx 300’ below MAP alt set it -

Set MAP altitude on MCP

53
Q

5000’ clean pitch and power target

A

5 degrees NU
58% N1

54
Q

10,000’ clean pitch and power

A

4 degrees NU
65% N1

55
Q

OEI at 5000’ pitch and power

A

5 degrees NU
75% N1

56
Q

For every 10kts IAS you need to reduce, how many nm per 10kts should you anticipate?

A

1 nm per 10kts of speed

57
Q

Will a higher airspeed result in a faster or slower descent rate ?

A

Faster descent rate. High speed descent plus drag eg: gear, flap, speed brake will provide for best altitude loss

58
Q

At what flap setting can speed brake no longer be used?

A

Anything above flaps 10

59
Q

Circle to Land configuration from MDA

A

Enter the circling area with Gear Down and Flaps 15

When at MDA and within the circling area, Turn 45 degrees for 45 seconds

Abeam threshold
- Timing (for 3 x alt to loose eg: 700’ to loose is 7x3= 21 sec. Adjust for Half wind component in seconds)
- Landing Flap

On base start a shallow vertical speed maybe 300fpm and intercept FAC

(OEI enter circuit with gear up flaps 10. Abeam threshold - Gear down Flaps 15)

60
Q

Balked landing TOGA actions

A

TOGA must be selected on the ground to initiate PWR up if AT is engaged and must be again clicked once airborne to activate the GA/TOGA function

61
Q

Loss of Hydraulic System A - what is major system lost ?

A

Gear

62
Q

Loss of Hydraulic System B - what is major system lost ?

A

Flaps

63
Q

If APU GEN BUS is switched on following OEI operation, What will happen to the AP on affected side of engine failure if engaged ?

A

This bus transfer will disconnect the AP is the respective AP side emerged is the same as the failed engine Side

64
Q

What Speed does auto brake system activate for an RTO condition ?

A

88kts (basically 90kts)

65
Q

Engine Severe Damage indications ?

A

Seizure of possibly N1 and or N2 (max may show no n2 normal)

Also an increase in EGT

66
Q

Engine Separation indications ?

A

All figures will be dashed as nothing can be read

FAULT light on affected engine fire panel will also illuminate as lined as basically cut

67
Q

Be cautious about Tracking modes on Takeoff especially when LNAV can’t be engaged on the Ground. At 400’ verify LNAV

A

As Above

68
Q

During OEI checklist when APU is available for start. During the 1 min delay before putting ELEC load on. Maybe get an ATIS update for alternate,

Then always return to the checklist and finish it in full.

A

As Above

69
Q

OEI GO AROUND

A

Going Around
Flaps 1 check thrust
Positive rate, gear up
400ft - LNAV
MSA OR MAP ALT - Bug Up
Flaps on Schedule
LVL Change
Max CONT thrust
AP on
After TO checklist

70
Q

Hot Start - FF indications

A

During normal start FF ≈ 326kg
Hot start FF can be ≈ 450-500kg

71
Q

Hot or Hung Start. No further start attempt. Call Maintenance

A

As above

72
Q

Engine smoke reported no cockpit indications

A

Engine limit, surge or Stall checklist

73
Q

If you have an ENG Stall and are operating on reduced power.

Treat the landing and go around as OEI. Reference OEI checklist and plan Flaps 15 landing

A
74
Q

Taxi speeds

A

20 knots mostly used
30 knots acceptable on a long straight
10 knots for turns that require greater steering than a rapid exit
Low vis operations - 10 knots

75
Q

There is Bank angle protection when operating in the confines of LNAV. However if in HDG select you must have selected the limited bank.

Eg - above FL300 Bank 10 deg

A

As above

76
Q

How is the Max altitude calculated ? Lowest of ?

A

Max structural
Max thrust limited
Buffet Margin

77
Q

MCP speed window. What does it mean if it shows an ‘A’ or an ‘8’ before the speed ?

A

A - underspeed
8 - overspeed

78
Q

What % N2 will the start switch move to OFF/AUTO?

NG and MAX

A

NG - 56%
MAX - 63%

79
Q

Min oil qty at start for NG and MAX ?

A

NG - 12

MAX - 14

80
Q

What position does RCAS say on runway during ground operations ?

A

When within 30 degrees of RWY HDG

81
Q

What happens to Bank with dual FMC Failure ?

A

Limited to 8 degrees.

Must conduct MAP on RNP AR

82
Q

What is the noodle on ND display ?

A

Vector showing position in next 30 seconds

83
Q

Green arrow on speed tape indicate ?

A

Speed trend that shows where you will be in the next 10 seconds

84
Q

B737 rough fuel burn per hour ?

A

2.4 T (1.2T) per side

15 min = 600kg
20 min = 800kg

Fixed Res (30 min) = 1.2 T

85
Q

What is difference between 350nm ring and 418nm ring ?

A

350nm ring is alternate for TO alternate

418nm ring is for suitable alternates enroute for non EDTO flights

86
Q

When can you use the “Commit to destination” philosophy?

A

When flight time is greater than 2hours and you are within 2 hours of destination.

Required to have a TAF 3 for domestic ops valid until 30 minutes post landing
Can use METAR/SPECI/TAF for international ops (as these include 2hr trends)

Captain just deem the wx conditions suitable to be able to land, even though may be below listed minima but still allows any approach of some kind.

Low vis approaches can’t be planned

87
Q

What is a typical engine oil burn per hour ?

A

0.4-0.6 per hour

(Be aware of this on long sectors, make sure enough oil for the return eg: 12 flying hours = 5, so you’d want to have 17 before first sector to ensure min 12 for return)

88
Q

What needs to be included in a PDC readback ?

A

SID
SQUAWK
BAY

(FOR YSSY OPS, ALSO RUNWAY AND TRANSITION)

89
Q

What is a rough figure for LDR?

MAX WEIGHT, FLAPS 30, VREF+5

A

2000m LDR - this includes 455m air distance

*each blue airport on ND represents a runway 1526m available and is suitable for landing if needed eg: on fire)

90
Q

Latest point of touchdown example - (150m to 900m or first third of the runway whichever is less)

LDR YPPH RWY 24 - 2070m

LDA - 2163m

For the above where would you nominate latest point of touchdown ?

A

5 x 150m markers RWY24 = 750m total zone

LDA - 2163 / 3 = 721 m (earliest point = 150m markers, latest point = 721m)

So at Perth you would use the end of the 4th markers as a defined latest point of touchdown. Which equals - 4 x 150 = 600m

91
Q

How would you confirm refuelling is complete ?

A
  1. required fuel shown on gauges
  2. If DC selector is on BATT, during fuel panel operation this takes power and would show around 28V, once refuelling is complete and fuel panel closed the voltage goes to 30-31V as the APU now recharges the respective battery.
92
Q

800 NG MTOW

A

79015kg

93
Q

800NG MLW

A

66360kg

94
Q

What does the white bug represent ?

A

V2 + 15

95
Q

Max take off crosswind DRY / WET?
45m
30m

A

40m -
34kts (DRY) / 25kts (WET)

30m -
25kts (DRY & WET)

96
Q

Max landing crosswind ? DRY / WET
45m
30m
Split Scimitar winglet

A

45m -
40kts (DRY / WET)

30m -
25kts (DRY / WET)

Split scimitar winglet -
37kts (DRY / WET)

97
Q

Fuel IMBL

A

453kg

98
Q

Where is torch located in flight deck ?

A

Behind LHS

99
Q

Evacuation duties FO?

A

Take torch, first available exit, check condition of exits and slides.

Assist pax upwind aircraft

100
Q

What is TAT?

A

Temp of airflow taken into account kinetic heat of the aircraft.

101
Q

Explain 737 Max Cross FCC system -

A

On NG FCC flip flops between each flight.

Due MCAS on the max, cross FCC was introduced so the standby FCC always does a reliability check to the operating FCC for trim commands.
If the reasonableness is out of tolerance the FCC will be cut off from making inputs to the STS

102
Q

Give 15 seconds for CM to be seated from cabin ready signal

A

As above

103
Q

Takeoff into a HW of 20kts or more may result in THR HLD earlier than target n1

A

As above

104
Q

Scavenge pump centre tank

A

Transfers fuel from centre tank automatically when FWD pump in tank 1 is on and main tank 1 is half full (float valve opens)

105
Q

What is initial AEO climb speed ?

A

v2+15 - v2+25

106
Q

-700 MTOW & MLW

A

70,080

58,604

107
Q

Why is an AFT CG beneficial?

A

Increases the lift available at a given AOA due to the reduced nose up trim required.

Improving aircraft climb perf
Allows a reduced vR & v2 therefore reducing field length required for TO

108
Q

When is a rolling start recommend?

A

When XWIND exceeds 20kts or TW exceeds 10kts

109
Q

When using ATM the takeoff speeds are still calculated as a full rates thrust take off.

A

Therefore you can apply max thrust anytime and be covered in regards to VMCG/VMCA

110
Q

If V speeds are lost and no pilot recalls the Vr speed. When should the crew rotate the aeroplane ?

A

5 to 10kts prior to v2 speed

B737 (5 decks)

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