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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

A

-1.0 psi

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27
Q

Max positive cabin differential pressure

A

9.0 psi

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28
Q

Cabin differential pressure safety relief valve setting

A

8.6 psi

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

When visibility is less than _______, the approach must be flown with the autopilot engaged if operable

A

4000 RVR or 3/4

35
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

36
Q

When do we use a DDA

A

Anytime there is an MDA

37
Q

When is autoland required?

A

Below CAT 1 minimums

38
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.

39
Q

Max demonstrated altitude for autoland?

A

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

40
Q

Max generator load

A

100% (90 kVA)

41
Q

Max TR Load

A

200 amps

42
Q

Max time for engine to be in TOGA or FLEX

A

all engines - 5 minutes
One engine inop - 10 minutes

43
Q

Max engine EGT during start on the ground

A

A/c 301-399 NEO - 750 C
CEO - 725 C
A/c 601-699 NEO - 1083

44
Q

Max engine EGT during start in flight

A

NEO - 875 C
CEO - 725

45
Q

Min oil pressure

A

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

46
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

47
Q

max continuous oil temp

A
  • 205-299, 301-399, 701-799
    140
  • 601-699
    151
48
Q

Min starting engine oil temp

A

-40 C All aircraft

49
Q

Min engine oil temp before takeoff

A

A320, A320NEO, A321 - 19C
A321NEO - 52C

50
Q

How many automatic start attempts are considered 1 start cycle?

A

A320, A320NEO, A321-
Up to 3 start attempts are considered one start cycle

A321NEO -
Up to 2 start attempts are considered one start cycle

51
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
52
Q

Min fuel for takeoff

A

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

53
Q

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

A

NO

54
Q

Max hydraulic pressure

A

3,200 psi

55
Q

Max brake temp for takeoff

A

300 C

56
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

57
Q

Max speed the flaps will be extended

A

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

58
Q

Is a cross bleed engine start authorized during push back?

A

NO

59
Q

Speed brake limitation

A

For approach in all NEO aircraft, Prohibited at or below 240 knots if:

-GWCG is above 35%
-In an overweight Landing condition

60
Q

VOR, VOR/DME approach procedures may be performed in NAV, NAV and APP NAV, or FINAL APP mode provided what?

A
  • The autopilot or FD is used
  • GPS primary or NAV accuracy high
  • The applicable navaid and corresponding airborne equipment is serviceable, tuned, and monitored during the approach. The VOR is the primary navaid.
61
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
62
Q

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

A
  • GPS PRIMARY
63
Q

If one engine is inoperative, it is not permitted to use​ the autopilot to​ perform non precision approaches in the​ ​following modes for the following aircraft:

A
  • A/C 701-712
  • FINAL APP, NAV​ V/S, NAV/FPA.​
  • Only FD use is authorized.​
64
Q

For all NEO aircraft, during approach the use of speed brakes is prohibited when?

A
  • at or below 240 kts if:
    • GWCG is above 35% or
    • In overweight landing conditions
65
Q

Crosswind limitation for engine start

A

A320NEO - 45 kt.
A321NEO - 35 kt.

66
Q

Which aircraft have ROW/ROP

A

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

67
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.

68
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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