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B737 > LIM > Flashcards

LIM Flashcards

1
Q

Runway Slope

A

+-2%

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2
Q

Max Tail Wind

A

15kts or 10 kts

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3
Q

Max speeds

A

RED

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4
Q

Max operating altitude

A

FL410

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5
Q

Max Take off and landing altitude

A

8400 or 12000 with High altitude landing system

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6
Q

30 meter runway cross wind limit

A

27 kts runway centerline must be clearly visible

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7
Q

Revenue flight must have what installed

A

Girt Bar

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8
Q

Cross wind limits Winglets

A

33kts

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9
Q

Cross wind limits No winglets

A

36kts

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10
Q

Max RVSM difference between inflight CAP and FO altimiter

A

200ft

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11
Q

On ground Max difference CAP and FO below 5000ft

A

50ft CAP and FO, 75ft with field

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12
Q

On ground max difference CAP and FO up to 10000ft

A

60ft, 75ft with field

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13
Q

Max taxi weight

A

70.76T

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14
Q

Max differential pressure

A

9.1 PSI

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15
Q

Engine Bleed air limit for packs during Take off approach and landing

A

Do not use HIGH flow for packs

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16
Q

Engine TAI used when

A

Icing condition 10* or below OAT/TAT down to SAT/OAT -40*

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17
Q

Without stiffened elevator tabs, speed limit after deicing or anti ice on horizontal stabilizer

A

270kts until maintenance procedure

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18
Q

Auto pilot engage limit

A

400ft AGL

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19
Q

With High altitude landing system, auto pilot used down to what altitude above 8400ft

A

100ft RA

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20
Q

JAA rules When must AP be disconnected during approach

A

50ft below MDA unless ILS or in go around

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21
Q

AUTO land max wind limits

A

25kts head, 20kts cross, 15kts tail

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22
Q

Engine limits

A

RED

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23
Q

Ignition must be on when

A

Take off
landing
Heavy rain
anti ice operation

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24
Q

APU bleed+ elec max alt in air

A

FL100

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25
Q

APU bleed+ elec max alt in ground

A

FL150

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26
Q

APU bleed only

A

FL170

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27
Q

APU elec only

A

FL410

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28
Q

Dont use when APU bleed

A

Ground air connected

ENG1 bleed in use

Isolation valve and ENG2 valve open

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29
Q

After engine start with APU bleed, precaution

A

Don’t go above IDLE

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30
Q

Look ahead terrain alerting and terrain display prohibited

A

Within 15nm of airport thats not in database

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31
Q

Max fuel temp

A

49*C

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32
Q

Min fuel temp

A

-43*C

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33
Q

Max fuel imbalance during taxi, take off, flight and landing

A

453kg

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34
Q

Fuel cross feed position during take off and landing

A

closed

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35
Q

If main tanks full, center tank fuel amount

A

453kg

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36
Q

if anti skid inoperative

A

Temperature reduced thrust not permitted

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37
Q

initial climb speed

A

V2＋15 to 25kts if light weight

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38
Q

When to engage VNAV after take off

A

3000 fr AGL

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39
Q

Angle of bank limit during take off

A

15* until V2＋15

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40
Q

Maximum continuous thrust time

A

5 minutes or 10

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41
Q

Minimum flap retraction altitude

A

400 ft but Boeing recommend 1000ft

42
Q

when will stall warning test horn work

A

AC busses powered for up to 4 minutes

43
Q

How will stall warning test not work

A

Asymmetrical flaps, use HYD B electrical pump to retract and test again

44
Q

when is PSEU light inhibited

A

thrust from take off until 30 seconds after landing

45
Q

HYD normal pressure, max, min

A

3000PSI normal
3500PSI max
2800PSI minimum

46
Q

HYD max quantity and min

A

106%

76%

47
Q

Minimum fuel for ground operation of HYD ELEC pump

A

760kgs for cooling of HYD fluid

48
Q

PTU purpose

A

back up of HYD B ENG PUMP failure, to retract leading edge devices

49
Q

Landing gear transfer unit

A

Back up for HYD A ENG PUMP to help retract landing gear

50
Q

standby HYD automatically operates when

A

HYD A or B loss + flaps extend + airborne or wheels faster than 60kts

or

main PCU FORCE FIGHT MONITOR trips, starts standby ELEC HYD motor pump, starts standby rudder allow rudder and reverser

51
Q

Max cabin altitude selectable

A

8000ft at FL410

52
Q

Window heat time before take off

A

10 minutes

53
Q

wing anti ice area and source of hot air

A

3 inboard leading edge slats using bleed air

54
Q

ENG anti ice air source

A

heats the cowl by 5th stage or 9th if not enough

55
Q

what does ALT nose wheel steering do

A

Supply HYD from B rather than A

56
Q

when does PASS OXYGEN automatically activate

A

FL140 cabin altitude

57
Q

Flight crew oxygen highest pressure

A

1850 PSI

58
Q

PBE time

A

15 to 20 minutes

59
Q

Passenger oxygen time

A

12 minutes

60
Q

passenger portable oxygen time

A

30minutes

61
Q

Coating frost on lower wing permitted up to

A

3mm

62
Q

Crew ozygen pressure and time

A

8000ft and 15minutes

63
Q

Tail strike clearance attitude

A

11*

64
Q

how is wheel well fire detection powered

A

AC BUS TRANSFWR 1

has no fire extinguishment

65
Q

APU check during walk around

A

APU fire control handle up
Yellow discharge disc in place
Red over pressure

66
Q

Minimum brake pressure

A

2800 PSI

67
Q

Engine start sequence

A

2 then 1

68
Q

ENG start sequence, things to check

A

2 then 1

GRD
Oil pressure increase
N1 rotation
N2 increase to around 25% or 20% stable for 5 seconds

start lever IDLE

FUEL FLOW AND EGT

56% N2 back to auto or off

average indication
N1 20%
N2 59%
EGT 320 - 520, 410 average
fuel flow 272KGPH
69
Q

Starter limit

A

2 minutes, wait 10 seconds for next start attempt

70
Q

Take off procedure

A

40% N1

forward pressure till 80kts

84kts confirm THR HLD

V1
ROTATE

POSITIVE RATE GEAR UP

71
Q

after take off procedure

A

V2 +15 UP TO 25

400FT call roll mode + AP on

1000ft acceleration flaps up

after take off climb checklist

3000ft VNAV

72
Q

CLB FL100 and cruise

A

landing lights off

set standard

level off fuel pumps off CENTER tank if LOW PRESSURE LIGHT illuminates must be on in cruise if more than 453kg

confirm FMC for arrival

73
Q

Descent a d approach

A

VREF CHECK

ANTI ICE

PRESSURIZATION FOR DESTINATION

AUTO BRAKE

Transition set QNH

Radio BARO for approach

NAV tune identify

FL100 LANDING LIGHT ON

CHECKLIST

FLAPS

74
Q

landing procedure

A

INTERCEPT ILS

APP + set TCAS

GLIDE SLOPE ALIVE + GEAR DOWN + FLAPS 15 + SPEED BRAKE

START SWITCH CONT

CHECKLIST

at GS, check N1 set for go around + set go around altitude

set remaining flaps

altitude check

CHECKLIST

500FT FLARE ARMED

50FT FLARE

75
Q

Go around

A

Push TO/GA switch

FLAPS 15

PUSH TOGA AGAIN IF REQUIRE MORE THRUST

POSTIVIE RATE GEAR UP

TUNE RADIOS FOR MISSED APPROACH

400FT SET ROLL MODE

RETRACT FLAPS

AFTER TAKE OFF XLB CHECKLIST

76
Q

landing procedure

A

disengage auto throttle

SPEED BRAKES UP

AUTO BRAKE

REVERSE

idle reverse at 60kts

taxi speed stow

disarm auto brake before taxi speed

77
Q

Max vs on the wheel

A

+6000

-7900

78
Q

lowest altitude for VNAV

A

400ft

79
Q

when is LNAV active in go around

A

50ft AGL

light does not appear until 400ft

80
Q

When does Mach trim activate

A

above 0.615M

Information from ADIRU

Counter pitch down moment

81
Q

Aileron control CAP AND FO

A

cap direct link to aileron

FO direct link to spoilers

82
Q

Speed trim system

A

uses stab trim to maintain CG

83
Q

Stall identification controlled by which 3 systems

how does it work

A

yaw damper
elevator feel shift
speed trim system

trims stabilizer nose down

inhibit from ground to 100ft RA during take off

84
Q

Yaw damper controlled by

A

Stall Management Yaw damper

85
Q

Flaps 1-15 usage

15 to 40

Flaps altitude max

A

1 to 15 for increased lift

15 to 40 increased lift and drag

FL200

86
Q

flaps and slats are operated normally by which HYD

A

B

87
Q

Which fluid system has most fluid

A

B, has more fluid for system B and standby sytem

88
Q

HYD for STBY leak reduces from B amount to

A

72%

89
Q

When does low pressure light standby hyd appear?

A

STANDBY HYD PUMP ON AND LOW PRESSURE

will go off once standby pump off

90
Q

STANDBY HYD LOW QUANTITY

A

will appear when standby fluid reaches half, regardless if pump is working or not

91
Q

when will STANDBY HYD automatically operate

A

if A or B fail during takeoff or landing

92
Q

how to view HYD QUANTITY

A

SYS button on MFD SYS

93
Q

Ground spoilers and flight spoilers powered by which systems?

A

ground just B

FLIGHT A and B

94
Q

Why not speed brake pass flight detent in flight

A

Will cause buffering, but can still go to max UP

95
Q

when will auto spoiler activate during takeoff

A

Above 60kts with reverse thrust on

96
Q

When will auto spoiler activate during landing

A

when wheel spin up

97
Q

how many leading edge flaps and slats

A

2 flaps inner wing

4 slats sealed or slotted depending on position

98
Q

Can you retract leading edge devices with only standby HYD Alternate flaps

A

no, unless there is HYD B

99
Q

which part responsible for sensing asymmetric trailing edge flaps

A

FLAP SLAT ELECTRONIC UNIT FSEU, senses rate by twist

100
Q

VMO MMO

A

340/0.82

B737 (2 decks)

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