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F9 Study > Operating Limitations (VOL II, Section 2) > Flashcards

Operating Limitations (VOL II, Section 2) Flashcards

1
Q

Max crosswind for takeoff

A

35 knots - All aircraft

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2
Q

Max crosswind for landing

A

38 knots - All aircraft

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3
Q

Max tailwind for takeoff

A

A319, A320, and A321NEO - 15 kts
A321CEO- 10 kts

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4
Q

Max tailwind for landing

A

10 kts - All aircraft

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5
Q

Max wind for pax door operation

A

65 kts

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6
Q

Max wind for cargo door operation

A

40 kts / 50 kts*
*If the nose is into the wind, or if the door is on the leeward side.

If the wind begins to exceed these limitations, the door must be closed before the wind exceeds 65 knots.

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7
Q

Vmo / Mmo

A

350 kias / .82 Mach

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8
Q

Approach Category

A
  • A319, A320, A321NEO category C
  • A321 category D
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9
Q

Stabilized Approach Policy

A

1000 AFE
- Lateral path (1 dot for Loc, 1/2 dot for VOR, .3 NM for RNAV)
- Vertical path (1 dot)
- Final Landing configuration
- Absent any GPWS warnings or cautions
- Max 1200 ft/min descent rate

500 AFE
- Landing checklist completed
- Max 1000p ft/min descent rate
- Speed -5 to +15 knots
- Thrust stabilized

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10
Q

Normal runway width

A

148 feet (45 meters)

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11
Q

Minimum runway width

A

100 feet (30 meters)

A/C - 227, 228, 229, and 601-600

All other aircraft 148 feet (45 meters)

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12
Q

Max landing gear retraction speed (VLO)

A

220 kts/0.54 Mach

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13
Q

Max landing gear extension speed (VLO)

A

250 kts/0.60 Mach

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14
Q

Max landing gear extended speed (VLE)

A

280 kts / .67 mach

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15
Q

Max tire speed

A

195 kts ground speed

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16
Q

Max speed for windshield wiper opeartion

A

230 kias

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17
Q

Max speed for cockpit window open

A

200 kias

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18
Q

Max taxi speed

A

A/C 213-299
Weight greater than 167,550 lbs, don’t exceed 20 kts during a turn

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19
Q

Max altitude with flaps or slats extended

A

20,000 feet MSL

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20
Q

Flight Maneuvering Load Acceleration Limits

A

Clean configuration = -1.0g - +2.5g
Other configurations = 0.0g - +2.0g

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21
Q

Max Operational Pressure Altitude

A

39,800 ft

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22
Q

Max pressure altitude for takeoff and landing

A

9,200 ft

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23
Q

Minimum pressure altitude for takeoff and landing

A

-2,000 ft

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24
Q

Runway slop (mean)

A

+/- 2%

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25
Q

Max runway altitude

A

9,200 ft

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26
Q

Max negative cabin differential pressure

27
Q

Max positive cabin differential pressure

28
Q

Cabin differential pressure safety relief valve setting

29
Q

Ram air inlet limitation

A

If differential pressure is greater than 1 psi, the check valve located downstream will not open

30
Q

APU bleed use limitation with LP ground unit

A

Do not use both at the same time to avoid chattering of the non return valves

31
Q

Is the us of external high pressure (HP) air cart authorized to be used for air conditioning?

A

No. It is prohibited at all times

32
Q

Avionics ventilation limitation

A

The aircraft electrical system should not be powered for more than 2 hours without a cooling system when the outside air temperature is above 49 C.

33
Q

Autopilot Minimum Engagement Height
- After Takeoff (if SRS is indicated)
- Enroute
- RNAV visual approach
- Non-presicion approach
- Non-Autoland ILS with CAT 1 FMA
- Non-autoland ILS with CAT 2/3 FMA
- Go-Around (if SRS is indicated)
- Autoland Approach

A
  • After Takeoff (if SRS is indicated) - 100 ft AGL and at least 5 seconds
  • Enroute - 900 ft AGL
  • RNAV visual approach - 500 ft AGL
  • Non-presicion approach - DDA/DA
  • Non-Autoland ILS with CAT 1 FMA - 160 ft AGL
  • Non-autoland ILS with CAT 2/3 FMA - 80 ft AGL
  • Go-Around (if SRS is indicated) - 100 ft AGL
  • Autoland Approach - Rollout/Taxi speed
34
Q

The use of AP or FD in OPEN DES or DES mode is not permitted when?

A

Inside the FAF or below 1000 ft AGL on a visual approach

35
Q

When do we use a DDA

A

Anytime there is an MDA

36
Q

When is autoland required?

A

Below CAT 1 minimums

37
Q

When are we required to setup and brief an autoland?

A

Anytime the report visibility is at or below 1/2 mile or 2400 RVR.

38
Q

Max demonstrated altitude for autoland?

A

A320, A320NEO, A321NEO - 9,200 ft
A321CEO- 5,750 ft MSL

39
Q

Max generator load

A

100% (90 kVA)

40
Q

Max TR Load

41
Q

Max time for engine to be in TOGA or FLEX

A

all engines - 5 minutes
One engine inop - 10 minutes

42
Q

Max engine EGT during start on the ground

A

CEO - 725 C
NEO (Leap engine) - 750 C
NEO (Pratt engine) - 1083

43
Q

Max engine EGT during start in flight

A

CEO - 725 C
NEO (Leap engine) - 875 C
NEO (Pratt engine) - 1083 C

44
Q

Min oil pressure

A

A320, A321 - 13 psi
A320NEO - 17.4 psi
A321NEO - 65 psi

45
Q

Min engine oil quantity

A

A320, A321
9.5 qt + .5 qt per hour

A320NEO
9.0 qt + .5 qt per hour and not below 10.6 qt

A321NEO
At or above -30C - 14 qt
Below -30C - 16.5 qt

46
Q

max continuous oil temp

A
  • 205-299, 301-399, 701-799
    140
  • 601-699
    151
47
Q

Min starting engine oil temp

A

-40 C All aircraft

48
Q

Min engine oil temp before takeoff

A

A320, A320NEO (Leap engine), A321 - 19C
A321NEO (Pratt engine) - 52C

49
Q

How many automatic start attempts are considered 1 start cycle?

A

A320, A320NEO (Leap engine) A321-
Up to 3 start attempts are considered one start cycle

A321NEO (Pratt engine)-
Up to 2 start attempts are considered one start cycle

50
Q

When is takeoff with reduced thrust prohibited?

A
  • On slippery or contaminated runways
  • Suspected, reported, or known windshear
  • When a special departure procedure specifies full thrust
51
Q

Min fuel for takeoff

A

3,300 lbs. The WING TK LO LVL warning must not be displayed.

52
Q

Is takeoff with center tank fuel supplying the engines authorized? (A/c 216-229)

53
Q

Max hydraulic pressure

54
Q

Max brake temp for takeoff

55
Q

Landing on narrow runways
(227-229, A321NEO)

A

-Autoland is not authorized
-Dispatch to/from not allowed in case of:
-nose wheel steering into
-one brake or more inop
-Diversion to normal runway recommended in case of:
-rudder jam
-rudder pedal jam
-yaw damper fault
-rudder travel limit fault
-all failures leading to loss of nose wheel steering

56
Q

Max speed the flaps will be extended

A

VFE -10 knots unless an abnormal or emergency procedure dictates otherwise.

57
Q

Is a cross bleed engine start authorized during push back?

58
Q

Approach procedures based on radio NAVAIDS may be performed in NAV, NAV and APP NAV, or FINAL APP mode provided what?

A
  • The autopilot or FD is used
  • If GPS PRIMARY, then the reference NAVAID may be unserviceable, or the airborne radio equipment may be inoperative or not installed.
  • If NOT GPS PRIMARY, then the applicable navaid and corresponding airborne equipment is serviceable, tuned, and monitored during the approach.
59
Q

RNAV (GPS) approach procedures may be performed in NAV, NAV and APP NAV, or FINAL APP mode provided what?

A
  • GPS PRIMARY or NAV ACC HIGH
60
Q

RNAV (RNP) approach procedures may be performed in NAV, NAV and APP NAV, or FINAL APP mode provided what?

A
  • GPS PRIMARY
61
Q

Crosswind limitation for engine start

A

A320NEO (Leap engines) - 45 kt.
A321NEO (Pratt engines) - 35 kt.

62
Q

Which aircraft have ROW/ROP

A

389-393 (No ROW/ROP pb)
394-399, 601-699 (Has ROW/ROP pb)

63
Q

How can the ROPS function be inhibited? (A/C 394-399, 601-699)

A

ROW/ROP pb-sw set to OFF on SURV panel.

64
Q

For A/C 389-393
When a runway is identified as incompatible with ROPS by CBI or AIP, the ROPS may be inhabited (TERR pb set to off on GPWS panel) when the aircraft is less than 15 NM miles from the airport when:

A
  • approach procedures have been previously identified as producing undue ROW alerts
  • If a NOTAM displaces the threshold

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