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Delta 737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max T/O and Landing Tailwind Component

A

10 kts, or as permitted by company pages

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2
Q

Max Operating Altitude

A

41,000 feet

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3
Q

Max T/O and Landing Altitude

A

8,400 feet

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4
Q

True or False
Do not operate HF radios during refueling operations

A

True

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5
Q

Max Crosswind

A

33 kts for T/O and Landing, including gusts

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6
Q

Severe turbulent air penetration speed

A

280 KIAS/.76M

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7
Q

Max Taxi Weight (MTW) - 737-800

A

174,900 lbs

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8
Q

Max Taxi Weight (MTW) - 737-900ER

A

188,200 lbs

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9
Q

Max Takeoff Weight (MTOW) - 737-800

A

174,200 lbs

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10
Q

Max Takeoff Weight (MTOW) - 737-900ER

A

187,700

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11
Q

Max Landing Weight (MLW) - 737-800

A

146,300 lbs

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12
Q

Max Landing Weight (MLW) - 737-900ER

A

157,300 lbs

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13
Q

Max Zero Fuel Weight (MZFW) - 737-800

A

138,300 lbs

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14
Q

Max Zero Fuel Weight (MZFW) - 737-900ER

A

149,300 lbs

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15
Q

Max Cabin Differential Pressure

A

9.1 PSI

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16
Q

Max Differential Pressure for T/O and Landing

A

0.125 PSI

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17
Q

With either one or both engine bleed switches ON, do not operate the air conditioning packs in ______ for T/O, approach, or landing

A

HIGH

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18
Q

When must Engine TAI be on

A

Icing conditions exist/anticipated, except during climb and cruise below -40 C SAT

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19
Q

Do not operate wing anti ice on the ground when the OAT is above ____

A

10 C (50 F)

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20
Q

Max and Min glideslope angle for autoland

A

3.25 and 2.5 degrees

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21
Q

Max headwind for autoland

A

25 kts

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22
Q

Max crosswind for autoland

A

20 kts

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23
Q

Max tailwind for autoland

A

10 kts

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24
Q

Autoland may only be used with flaps ____ or ____ and both engines operating

A

30 or 40

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25
Q

Do not use LVL CHG on finall approach below _____

A

1000 ft AFE

26
Q

On the ground limit one generator (engine driven) operation to a max of _____

A

75 KVA (215 amps)

27
Q

EGT limit for takeoff

A

Top of Amber Arc (5 minutes)

28
Q

EGT limit max continuous

A

Top of White Arc

29
Q

EGT limit starting (ground/flight)

A

EGT start limit line

30
Q

Engine ignition must be on for…

A

takeoff
landing
operation in heavy rain
anti ice operation

31
Q

Limit each start attempt to _____

A

2 minutes

32
Q

A min of ____ is required between start attempts

A

10 seconds

33
Q

Max APU operating altitude inflight - Bleed + Electrical load

A

10,000 ft

34
Q

Max APU operating altitude inflight - Bleed

A

17,000 ft

35
Q

APU start duty cycle

A

3 starts per 15 minute interval
Wait time after 3 starts - 15 min

36
Q

Run the APU for ____ minutes before using as a bleed source

A

2 minutes

37
Q

Max alittude with flaps extended

A

20,000 ft

38
Q

Holding in icing conditions with flaps extended is

A

Prohibited

39
Q

Do not use the speedbrakes in flight below

A

1000 ft

40
Q

In flight do not extend speedbrakes beyond

A

FLIGHT DETENT

41
Q

When extending or retracting flaps with ALTERNATE FLAPS position switch, allow ____ seconds after releasing position switch

A

15

42
Q

Max crosswind for HUD guided takeoffs

A

10 kts

43
Q

Max headwind for HUD AIII

A

25 kts

44
Q

Max crosswind for HUD AIII

A

15 kts

45
Q

Max tailwind for HUD AIII

A

10 kts

46
Q

Max fuel tank temperature

A

49 C

47
Q

Min inflight fuel tank temperature

A

3 C above freezing point of fuel being used or -43 C, whichever is higher

48
Q

Fuel imbalance must not exceed

A

1000 lbs

49
Q

Ensure the center tank fuel pump switches are OFF before _________

A

any planned power transfer

50
Q
A
51
Q

Landing Gear Extension Speed

A

270 KIAS .82M

52
Q

Landing Gear Retraction Speed

A

235 KIAS

53
Q

Landing Gear Extended Operating Speed

A

320 KIAS .82M

54
Q

Flaps 1

A

250 KIAS

55
Q

Flaps 2

A

250 KIAS

56
Q

Flaps 5

A

250 KIAS

57
Q

Flaps 10

A

210 KIAS

58
Q

Flaps 15

A

200 KIAS

59
Q

Flaps 25

A

190 KIAS

60
Q

Flaps 30

A

175 KIAS

61
Q

Flaps 40

A

162 KIAS

Delta 737 (2 decks)

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