POM Limitation Flashcards
Runway slope
+/– 2%
Gear Maximum speeds
Extend 270 / .82
Extended 320 / .82
Retract 235
Flap Maximum speeds
1 - 5 250kt 10 210kt 15 200kt 25 190kt 30 175kt 40 162kt
230kt for Alternate Flap Extend
Maximum Takeoff and
Landing Tailwind Component
15kts(10kts for HL8234)
Flight Deck Door Access System Test
once each flight day
HF radios during refueling operations
Do not operate
The maximum allowable in-flight difference between Captain and
First Officer altitude displays for RVSM operations is
200 feet.
The maximum
allowable on-the-ground altitude display differences for RVSM operations
are :
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
Wind Limitations Manual Flight (Takeoff and Landing)
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
Wind Limitations
Auto-landing(CAT I or Better)
25/20/15
25/20/10(HL8234)
Wind Limitations
Auto-landing(CAT II or CAT IIIa)
25/15/10
Contaminated Runway
Takeoffs and Landings are prohibited for following condition.
Standing water, slush
or wet snow
TO = 1/2inch
LD = 1inch
Dry snow
TO = 4inch
LD = 4inch
Maximum Takeoff Weight …
Maximum Landing Weight…
Maximum Zero Fuel Weight …
79,015 KG
65,317 KG
61,688 KG
The maximum cabin differential pressure (relief valves) is …
9.1 psi
With engine bleed air switches ON, do not operate the …
air conditioning packs
in HIGH for takeoff, approach or landing.
Engine TAI must be on when …
icing conditions exist or are anticipated,
except during climb and cruise below -40°C SAT
Do not engage the autopilot for takeoff below…
400 feet AGL.
For single channel operation during approach, the autopilot shall not be
engaged below…
FAA and JAA
50 feet AGL for FAA
158 feet AGL for JAA
Use of aileron trim with the autopilot engaged is …
prohibited.
Maximum and minimum glideslope angles for autoland are …
3.25° and 2.5°
respectively.
Autoland capability may only be used with flaps …
30 or 40 and both engines operative.
For circling approach, the autopilot can be used until intercepting a normal
landing profile, but it must be disengaged before
500 feet HAA.
Engine EGT
Takeoff/Go-Around…
Maximum Continuous…
Starting…
950°C 5 minutes* (6대 항공기 10 min)
925°C No Limit
725°C No Limit
Engine ignition must be on for :
- Takeoff
- Landing
- Operation in heavy rain
- Anti-ice operation
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
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
APU bleed valve may be open during engine start, but avoid engine power
above…
idle
After three consecutive aborted APU start attempts, a (……. Minute) cooling
period is required.
15 minute
Max flap extension altitude is…
20,000 feet.
Holding in icing conditions with flaps extended is…
prohibited.
Do not deploy the speedbrakes in flight at radio altitudes less than …
1,000 feet.
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
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
Avoid weather radar operation in …
a hanger
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.
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
Main tanks 1 and 2 must be full if center tank contains more than …
453kgs
Operation with (
? )takeoff thrust is not permitted
with anti-skid inoperative.
assumed temperature reduced
Do not apply brakes until…
after touchdown.
Maximum Operating Altitude
41,000 feet
Maximum Takeoff and Landing Altitude
8,400 feet
Vmo/Mmo
340KIAS / M.82
