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737 POM/QRH > POM Limitation > Flashcards

POM Limitation Flashcards

1
Q

Runway slope

A

+/– 2%

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2
Q

Gear Maximum speeds

A

Extend 270 / .82
Extended 320 / .82
Retract 235

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3
Q

Flap Maximum speeds

A 
1 - 5     250kt
10         210kt
15         200kt
25        190kt
30        175kt
40        162kt

230kt for Alternate Flap Extend

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4
Q

Maximum Takeoff and

Landing Tailwind Component

A

15kts(10kts for HL8234)

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5
Q

Flight Deck Door Access System Test

A

once each flight day

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6
Q

HF radios during refueling operations

A

Do not operate

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7
Q

The maximum allowable in-flight difference between Captain and
First Officer altitude displays for RVSM operations is

A

200 feet.

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8
Q

The maximum
allowable on-the-ground altitude display differences for RVSM operations
are :

A

Sea Level - 5,000 feet
CAPT & F/O : 50 feet
CAPT or F/O & Field Elevation : 75 feet

5,001 to 10,000 feet
CAPT & F/O : 60 feet
CAPT or F/O & Field Elevation : 75 feet

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9
Q 
Wind Limitations
Manual Flight (Takeoff and Landing)
A

Braking Action
(Cross wind / Tail wind)

Good - 30 / 10
Medium(or Fair) - 20 / 5
Poor - Takeoff: 8 / NA
         -  Landing: 10 / NA
NIL - NA

Note : The NA means Not Authorized

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10
Q

Wind Limitations

Auto-landing(CAT I or Better)

A

25/20/15

25/20/10(HL8234)

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11
Q

Wind Limitations

Auto-landing(CAT II or CAT IIIa)

A

25/15/10

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12
Q

Contaminated Runway

Takeoffs and Landings are prohibited for following condition.

A

Standing water, slush
or wet snow
TO = 1/2inch
LD = 1inch

Dry snow
TO = 4inch
LD = 4inch

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13
Q

Maximum Takeoff Weight …
Maximum Landing Weight…
Maximum Zero Fuel Weight …

A

79,015 KG
65,317 KG
61,688 KG

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14
Q

The maximum cabin differential pressure (relief valves) is …

A

9.1 psi

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15
Q

With engine bleed air switches ON, do not operate the …

A

air conditioning packs

in HIGH for takeoff, approach or landing.

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16
Q

Engine TAI must be on when …

A

icing conditions exist or are anticipated,

except during climb and cruise below -40°C SAT

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17
Q

Do not engage the autopilot for takeoff below…

A

400 feet AGL.

18
Q

For single channel operation during approach, the autopilot shall not be
engaged below…
FAA and JAA

A

50 feet AGL for FAA

158 feet AGL for JAA

19
Q

Use of aileron trim with the autopilot engaged is …

A

prohibited.

20
Q

Maximum and minimum glideslope angles for autoland are …

A

3.25° and 2.5°

respectively.

21
Q

Autoland capability may only be used with flaps …

A

30 or 40 and both engines operative.

22
Q

For circling approach, the autopilot can be used until intercepting a normal
landing profile, but it must be disengaged before

A

500 feet HAA.

23
Q

Engine EGT
Takeoff/Go-Around…
Maximum Continuous…
Starting…

A

950°C 5 minutes* (6대 항공기 10 min)
925°C No Limit
725°C No Limit

24
Q

Engine ignition must be on for :

A
  • Takeoff
  • Landing
  • Operation in heavy rain
  • Anti-ice operation
25
Q

In flight - APU bleed + electrical load :
Ground only - APU bleed + electrical load :
APU bleed :
APU electrical load :

A

max alt 10,000 feet
max alt 15,000 feet
max alt 17,000 feet
max alt 41,000 feet

26
Q

APU bleed valve must be closed when :

A
  • Ground air connected and isolation valve open
  • Engine no. 1 bleed valve open
  • Isolation and engine no. 2 bleed valves open
27
Q

APU bleed valve may be open during engine start, but avoid engine power
above…

A

idle

28
Q

After three consecutive aborted APU start attempts, a (……. Minute) cooling
period is required.

A

15 minute

29
Q

Max flap extension altitude is…

A

20,000 feet.

30
Q

Holding in icing conditions with flaps extended is…

A

prohibited.

31
Q

Do not deploy the speedbrakes in flight at radio altitudes less than …

A

1,000 feet.

32
Q

Alternate flap duty cycle :
• When extending or retracting flaps with the ALTERNATE FLAPS position
switch, allow ( ? ) seconds after releasing the ALTERNATE FLAPS position
switch before moving the switch again to avoid damage to the alternate
flap motor clutch.
• After a complete extend/retract cycle, i.e., 0 to 15 and back to 0, allow ( ? )
minutes cooling before attempting another extension.

A

15 seconds

5 minutes

33
Q

Do not use the terrain display for ( ? )
Do not use the look-ahead terrain alerting and terrain display functions :
Within( ? ) of takeoff, approach or landing at an airport not contained in
the GPWS terrain database

A

navigation.

15nm

34
Q

Avoid weather radar operation in …

A

a hanger

35
Q

Maximum tank fuel temperature:

Minimum tank fuel temperature prior to takeoff and inflight is :

A

49°C

-43°C, or 3°C
above the freezing point temperature, whichever is higher.

36
Q

Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero.
Random fuel imbalance must not exceed ( ? ) for taxi, takeoff, flight or
landing

A

453kgs

37
Q

Main tanks 1 and 2 must be full if center tank contains more than …

A

453kgs

38
Q

Operation with (
? )takeoff thrust is not permitted
with anti-skid inoperative.

A

assumed temperature reduced

39
Q

Do not apply brakes until…

A

after touchdown.

40
Q

Maximum Operating Altitude

A

41,000 feet

41
Q

Maximum Takeoff and Landing Altitude

A

8,400 feet

42
Q

Vmo/Mmo

A

340KIAS / M.82

737 POM/QRH (2 decks)

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