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Limitations Flashcards

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1
Q

What are the load factor limits:
1. Clean configuration?
2. Other configurations?

General

A
  1. -1G to +2.5G
  2. 0G to +2G
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2
Q

What is the min/max operating altitudes?

General

A

Min: -1000’
or -2000’ PA
Max: 39,100’
or 39,800’ PA

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3
Q

What are the min/max altitudes for takeoff and landing?

General

A

Min: -1000’
or -2000’ PA
Max: 9200’
or 8000’ PA

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4
Q

Nominal Runway Width?

General

A

147’/45m
A runway of 147’/45m or greater where the outer portion is contaminated is acceptable for use provided that a minimum of 100’/30.5m width is cleared within the allowable limits.

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5
Q

Minimum Runway Width?

General

A

98’/30M
A runway of 147’/45m or greater where the outer portion is contaminated is acceptable for use provided that a minimum of 100’/30.5m width is cleared within the allowable limits.

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6
Q

Max Runway Slope?

A

+/- 2%

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7
Q

Max Demonstrated Crosswind (takeoff and landing)

General

A

38 kt (gust included)

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8
Q

Max Tailwind for Takeoff?

General

A

15 kts or
10 kts

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9
Q

Max Tailwind for landing?

General

A

10 kts or
15 kts

(For tailwinds greater than 10kts, FLAPS FULL recommended)

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10
Q

Max Wind Speed for doors operations?

General

A
  • Pax door - 65 kts
  • FWD/AFT Cargo operation - 40 kts (50kts if into wind or on leeward side)
  • FWD/AFT Cargo doors must be closed before wind exceeds 65 kts.
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11
Q

Max Cockpit Window Open Speed?

General

A

200 kts

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12
Q

Max Flaps/Slats Speeds

319/320

A
  • 1 = 230 kts
  • 1 + F = 215 kts
  • 2 = 200 kts
  • 3 = 185 kts
  • Full = 177 kts

319/320

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13
Q

Max Flaps/Slats Speeds

321

A
  • 1 = 235 kts
  • 1 + F = 225 kts
  • 2 = 215 kts
  • 3 = 195 kts
  • FULL = 190 kts

321

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14
Q

Max Operating Speed (Vmo/Mmo)?

General

A

350 kts / M .82

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15
Q

Max speed with landing gear extended (Vle)?

General

A

280 kts / M 0.67

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16
Q

Max Speed at which the gear may be extened (Vlo extension)?

General

A

250 kts / M 0.60

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17
Q

Max speed at which the gear may be retracted (Vlo retraction)?

General

A

220 kts / M 0.54

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18
Q

Maximum Tire Speed

General

A

195 kts

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19
Q

Minimum control speed for landing (Vmcl)?

General

A

116 kts / 113 kts /110 kts / 108 kts

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20
Q

Taxi Speed limit in a turn at a hight gross weight?

General

A

20 kts above 76 000 kg.

225-226, 232, 235-242, 401-402, 415-422

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21
Q

Max Wiper Operating Speed

General

A

230

This limitation is applicable when the wipers are sweeping. It is not applicable if the wipers are not sweeping for any reasons.

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22
Q

Max Landing Wieght?

General

A

319 - 61,000KG
320 - 64,500 KG (or 66,000KG)
321 - 77,800KG

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23
Q

Max Positive Diff. Pressure

Air Bleed/Cond/Press/Vent

A

9.0 PSI

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24
Q

Max Negative Diff. Pressure

Air Bleed/Cond/Press/Vent

A

-1.0 PSI

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25
Safety Relief valve setting (PSI) ## Footnote Air Bleed/Cond/Press/Vent
8.6 PSI
26
At what temperature should you start to be concerned about avionics ventalation on ground? | Air Bleed/Cond/Press/Vent
49º OAT
27
What Altitude does the Outfllow Valve Close? | Air Bleed/Cond/Press/Vent
15,000'
28
What altitude do you get a Cab Alt Warning? | Air Bleed/Cond/Press/Vent
9,550' +/- 350'
29
Max Cab Alt Selection? Min Cab Alt Selection? | Air Bleed/Cond/Press/Vent
14,000' 2,000'
30
Max Norm Cab Alt | Air Bleed/Cond/Press/Vent
8,000'
31
Minimum height for AP use on Takeoff ## Footnote Autoflight
100' AGL (and atleast 5 s after takeoff)
32
Min AP Use In Approach with F-G/S Mode ## Footnote Autoflight
200' AGL
33
Min AP Use In Approach with FINAL APP, V/S or FPA mode ## Footnote Autoflight
250' AGL
34
Min AP Use In circling approach ## Footnote Autoflight
500' AGL for aircraft CAT C (600' AGL for aircraft CAT D)
35
Min AP Use ILS/MLS approach when CAT 1 is displayed on the FMA ## Footnote Autoflight
160' AGL
36
Min AP Use ILS/MLS approach when CAT 2 or CAT 3 SINGLE or CAT3 DUAL is displayed on the FMA ## Footnote Autoflight
0' AGL if Autoland
37
Min AP Use GLS approach when CAT1 is displayed on the FMA ## Footnote Autoflight
160' AGL
38
Min AP Use GLS approach when AUTOLAND is displayed on the FMA ## Footnote Autoflight
0' AGL if autoland
39
Min AP Use After a Go-Around ## Footnote Autoflight
100' AGL
40
Min AP Use In all other phases of flight ## Footnote Autoflight
500' AGL (900' AGL in some A321's) ## Footnote OP DES/DES may only be used if FCU altitude is set to, or above the higher of the two: MDA/MDH or 500/900'
41
What limitations are there for Engine-out NPA Approaches? ## Footnote Autoflight
It is not permitted to use the autopilot to perfrom NPA in the following modes: FINAL APP, NAV V/S, NAV/FPA. Only FD use is permitted. *Note: One Engine inoperative RNP APCH approaches must be hand flown in FINAL APP or NAV/FPA mode. To reduce pilot workload, and if conditions permit, it is recommended to fly an RNP APCH approach in FINAL APP using the FD.*
42
ILS CAT II Min Decision Height ## Footnote Autoflight
100' *At leaste one autopilot must be engaged in APPR mode, and CAT 2 or CAT 3 SINGLE or DUAL must be displayed on FMA. For manual landing AP should be disconnected no later than 80' AGL.*
43
RNP Accuracy with GPS Primary
* AP // AP off and FD on // Off * Enroute - 1nm/1nm/1.1nm * Terminal - .5/.51/.51 * Approach - .3/.3/ Not auth ## Footnote AP / AP off and FD on both require to be in NAV or LOC (for approach phase)
44
What limitations are there to a SA ILS CAT II approach? ## Footnote Autoflight
Same as normal CAT II AND Crew must perform an automatic landing.
45
ILS CAT III (Single) Limitations ## Footnote Autoflight
* Min decision height - 50 AGL * A/THR must be used in selected or managed speed. * At least one autopilot must be engaged in APPR mode, and CAT 3 SINGLE or DUAL must be displayed on the FMA.
46
ILS CAT III (DUAL) Limitations ## Footnote Autoflight
* Alert Height - 100' * A/THR must be used in selected or managed speed. * Both AP's must be engaged in APPR mode, and CAT III DUAL must be displayed on the FMA.
47
ILS CAT III DUAL with DH Minimum Decision Height ## Footnote Autoflight
20' AGL (AC) 18' AGL (Airbus)
48
ILS CAT III DUAL Minimum RVR ## Footnote Autoflight
250'
49
What limitations are there to Engine Out Precision Approaches? ## Footnote Autoflight
CAT II and CAT III fail passive autoland are only approved in configuration FULL, and if engine out procedures are completed before reaching 1000' in approach. *Air Canada Limitation. Airbus allows CONF 3.*
50
Autoland Glideslope Limitations? ## Footnote Autoflight
Glideslope angle between 2.5º and 3.15º
51
Autoland Weight Limitation? ## Footnote Autoflight
Below maximum landing weight. *A319: Depending on the situation (eg. emergency or other) and provided that the runway is approved for automatic alnding, the flight crew can perform an autoland up to 69t.*
52
Autoland max/min elevation? ## Footnote Autoflight
-1000' to 9200' (A319/A320) -1000' to 2500' (some A320) -1000' to 5750' (A321)
53
Autoland Configuration Limitations? ## Footnote Autoflight
AC is CONF FULL only. *Airbus allows CONF 3 and CONF FULL*
54
What are the APU Start Limitations? ## Footnote APU
After 3 attempts, wait 60 minutes before next attempt.
55
APU Start/Shutdown During Refueling Limitations? ## Footnote APU
APU Starts/Shutdowns are permitted with the following restrictions: * If the APU failed to start or following an automatic APU shutdown, do not start the APU * If a fuel spill occurs, perform an APU shutdown.
56
Above what Altitude can the APU only provide Electrical output? ## Footnote APU
22,500' PA or 20,000 PA
57
What is the APU Battery Restart Atltitude Limit? | APU
25,000' PA
58
Up to what altitude can the APU provide Bleed Air output? | (Single Pack) ## Footnote APU
22,500' PA or 20,000 PA | (Single Pack)
59
Up to what altitude can the APU provide Bleed Air Output? | (Dual Pack) ## Footnote APU
15,000' PA | (Dual Pack)
60
Max Altitude for APU assisted engine start? ## Footnote APU
20,000'
61
Max Altitude for air conditioning and pressurization (single pack operation?) ## Footnote APU
22,500' PA or 20,000' PA
62
Max altitude for air conditioning and pressurization (dual pack operation?) ## Footnote APU
15,000'
63
Can you use APU bleed air for wing anti-ice? ## Footnote APU
Not permitted.
64
Max Continuous Load per generator | Electrical
90 KVA
65
Max Continuous Load per TRU | Electrical
200 A
66
How long can you use TOGA? | Engines
All Engines - 5 mins One engine - 10 Mins
67
Max start EGT Limit? | Engines
725º C
68
Oil Min start Temp? | Engines
-40º C
69
Oil Min temp before Takeoff | Engines
-10º C
70
Min oil quantity? | Engines
9.5 qt + est consumption | 0.5qt/h
71
What is considered one start cycle? | Engines
- A standard automatic start that includes up to three start attempts is considered one cycle.
72
How long of a pause is requried between start cycles? | Engines
20 seconds
73
How long of a cooling period is required and when (during start?) | Engines
- A 15 minute cooling period is required, subsequent to 4 failed cycles.
74
Starter N2 limitation | Engines
Starter must not be run when N2 is above 20%
75
When is Flex Thrust Prohibited? ## Footnote Engine
* The assumed temp for Flex Thrust is less than the actual OAT. * Windshear or known temperature inversion exists below 1500 AGL. * Runway is contaminated. * Reduced thrust takeoff is prohibited by the Route Manual. * Prohibited by MEL Manual. The flex takeoff thrust must bever be below the MCT at ISA + 40ºC (320/321) TFLEX cannot be: * Higher than TMAXFLEX, equal to ISA +53º or +40º (320) / +44º (319) / +43ºC (321). * Lower than the flat temperature (TREF). * Lower than actual OAT.
76
At what altitude are TCAS RA's inhibited below? ## Footnote MT #2 Slide (Maybe double check)
1000' AGL
77
What are the syptoms of windshear? | MT #2 Slide (Maybe double check)
1. IAS variations excess of +/- 15kts. 2. Ground speed variations 3. Wind indications variations in direction and speed on the ND. 4. Vertical speed excursions of 500 fpm. 5. Pitch attitude excursions of 5º. 6. Glide slope deviations of 1 dot. 7. Heading variations of 10º. 8. Unusaly A/THR activity.
78
What is the normal maximum taxi speed in a straight line and sharp turn?
* 30 kts * 10 kts | FCOM-Taxi
79
What is the min/max fuel temps JA/A-1? | Fuel
* JET A - 36ºc (Moniter if -34ºc) * JET A1 - 43ºc Max 54ºc
80
What are the altitude limits for high fuel temperatures? | Fuel
If wing fuel temp exceeds 30ºC at engine start, the altitude must be limited to FL350, until the center tank is empty. ## Footnote Pressure supplied by center tank pumps becomes lower than the pressure supplied by the wing tank pumps.
81
Fuel Imbalance Limits at Takeoff | Fuel (319/320)
* Inner Tanks - 500kgs * Outer Tanks - 370kgs | (319/320)
82
Fuel Imbalance Limits in flight | Fuel (319/320)
* Inner Tanks - 1500kgs * Outer Tanks - 690kgs | (319/320)
83
Fuel Imbalance at Takeoff | Fuel (321)
600kgs 400kgs (483) | (321)
84
Fuel Imbalance in flight | Fuel (321)
1320kgs | (321)
85
Min Fuel for Takeoff | Fuel
1500kgs (ECAM alerts must not appear)
86
Max Operating Pressure | Hydraulics
3000 PSI +/- 200 PSI (At zero Delivery)
87
Definition of Icing Conditions | Ice and Rain Protection
* OAT or TAT is at or below 10ºc and visible moisture is present (clouds, fog, of 1sm or less, rain, snow, sleet or ice crystals * OAT is at or below 10ºc and operating on ramps, taxiways or runways where surface snow, standing water, or slush may be ingested
88
Severe Ice Definition | Ice and Rain Protection
5mm or 0.2 in
89
Max brake temps for takeoff | Landing Gear
150ºc Fans on 300ºc Fans off
90
Max speed during turn if max one tire per gear is deflated (up to 3) | Landing Gear
7kts
91
Max speed with two tires deflated on same gear | Landing Gear
3 kts
92
Max nosewheel steering angle with deflated tires | Landing Gear
30º
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