POM Limitation Flashcards

(42 cards)

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 …

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
In flight - APU bleed + electrical load : Ground only - APU bleed + electrical load : APU bleed : APU electrical load :
max alt 10,000 feet max alt 15,000 feet max alt 17,000 feet max alt 41,000 feet
26
APU bleed valve must be closed when :
* Ground air connected and isolation valve open * Engine no. 1 bleed valve open * Isolation and engine no. 2 bleed valves open
27
APU bleed valve may be open during engine start, but avoid engine power above...
idle
28
After three consecutive aborted APU start attempts, a (....... Minute) cooling period is required.
15 minute
29
Max flap extension altitude is...
20,000 feet.
30
Holding in icing conditions with flaps extended is...
prohibited.
31
Do not deploy the speedbrakes in flight at radio altitudes less than ...
1,000 feet.
32
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.
15 seconds | 5 minutes
33
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
navigation. | 15nm
34
Avoid weather radar operation in ...
a hanger
35
Maximum tank fuel temperature: Minimum tank fuel temperature prior to takeoff and inflight is :
49°C -43°C, or 3°C above the freezing point temperature, whichever is higher.
36
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
453kgs
37
Main tanks 1 and 2 must be full if center tank contains more than ...
453kgs
38
Operation with ( ? )takeoff thrust is not permitted with anti-skid inoperative.
assumed temperature reduced
39
Do not apply brakes until...
after touchdown.
40
Maximum Operating Altitude
41,000 feet
41
Maximum Takeoff and Landing Altitude
8,400 feet
42
Vmo/Mmo
340KIAS / M.82