General Limitations Flashcards
(68 cards)
1
Q
Ground Clearance - Tailstrike Pitch Attitude
A
A319….13.9 degrees
A320….11.7 degrees
A320 Neo…..11.7 degrees
A321…..9.7 degrees
2
Q
Wingspans
A
A319, A320…….111 feet, 10 inches
A320 Sharklet, A321 Sharklet…….117 feet, 5 inches
3
Q
Maximum Certified Altitude
A
FL398
4
Q
Runway Slope
A
+/- 2%
5
Q
Runway Altitude
A
9,200 ft
6
Q
Nominal Runway Width
A
148 ft
7
Q
Maximum Demonstrated Crosswind
A
38 knots
8
Q
Maximum Tailwind for Takeoff
A
15 knots
9
Q
Maximum Tailwind for Landing
A
10 knots
10
Q
Maximum Wind for Passenger Door Operation
A
65 knots
11
Q
Max Crosswind on Wet & Contaminated Runways
A
Good...38 knots Good to Medium...29 knots Medium...25 knots Medium to Poor...20 knots Poor...15 knots
12
Q
Cockpit Window Open Maximum Speed
A
200 knots
13
Q
Flap Speeds A319, A320
A
Flap 1...230 knots Flap 1 + F...215 knots Flap 2...200 knots Flap 3...185 knots Full...177 knots
14
Q
Flap Speeds A321
A
Flap 1...235 knots Flap 1 + F...225 knots Flap 2...215 knots Flap 3...195 knots Full...190 knots
15
Q
Maximum Operating Speeds
A
VMO…350 knots
MMO…Mach 0.82
16
Q
Maximum Speeds with Landing Gear Extended
A
VLE…280 knots
VLO Extension…250 knots
VLO Retraction…220 knots
17
Q
Maximum Altitude to extend Landing Gear
A
25,000 feet
18
Q
Maximum Tire Speed
A
195 knots
19
Q
Maximum Wiper Speed
A
230 knots
20
Q
V MCL - -Maximum Control Speed for Landing
A319 N502NK thru N536NK
A
109 knots
21
Q
V MCL - -Maximum Control Speed for Landing
A320 N601NK thru N656NK, N690NK thru N698NK
A
109 knots
22
Q
V MCL - -Maximum Control Speed for Landing
A320 N901NK thru N937NK
A
116 knots
23
Q
V MCL - -Maximum Control Speed for Landing
A321 N657NK thru N687NK
A
114 knots
24
Q
Max Taxi Speed in a turn (N601NK thru N656NK, N690NK thru N698NK)
A
When the weight is greater than 167,550 lbs, do not exceed 20 knots in a turn.
25
Max Landing Weight - A319 Classic (N502NK thru N536NK)
137,788
26
Max Landing Weight - A320 Classic (N601NK thru N617NK, N697NK, N698NK)
145,505
27
Max Landing Weight - A320 Sharklet (N618NK thru N656NK, N690NK thru N696NK)
145,505
28
Max Landing Weight - A320 Neo (N901NK thru N937NK)
148,951
29
Max Landing Weight - A321 Sharklet (N657NK thru N687NK)
171,519
30
APU Bleed with Air Start Unit
The crew must not use air from the APU BLEED and from the HP Air Start Unit at the same time.
31
Cabin Pressure Limits
Maximum Positive Differential + 9.0 psi
| Maximum Negative Differential - 1.0 psi
32
Packs with LP Air Conditioning Unit
The crew must not use conditioned air from the packs and the LP air conditioning at the same time.
33
Minimum Height for use of autopilot takeoff with SRS Mode
100' AGL
34
Minimum Height for use of the autopilot straight-in non-precision approach
Applicable Minimum
35
Minimum Height for use of the autopilot circling approach
Applicable Circling Minimums - 100'
36
Minimum Height for use of the autopilot ILS Approach when CAT2 or CAT3 is not displayed on the FMA
160' AGL
37
Minimum Height for use of the autopilot go-around (AP or FD engagement)
100' AGL
38
Minimum Height for use of the autopilot in all other phases
A319/A320 - - 500' AGL
| A321 - - 900' AGL
39
Use of the AP or FD in OPEN DES or DES mode is not permitted in approach, unless the FCU altitude is set at or above:
The highest of:
A319/A320 - - 500' AGL or minimums
A321 - - 900' AGL or minimums
40
Note on Takeoff with SRS Mode
Internal FMGS logic prevents the AP from engaging during the 5 seconds after liftoff
41
Limitations on NAV mode usage in the terminal area
Nav mode may be used in the terminal area provided:
- - GPS PRIMARY is available
- - Appropriate RNP is checked or entered on the MCDU, and HIGH accuracy is displayed, or
- - FMS Navigation is crosschecked with NAVAID raw data
42
Non-precision approaches with engine-out limitation.
| N502NK thru N536NK, N657NK thru N668NK, N670NK, N671NK
If one engine is inoperative, it is not permitted to use the autopilot to perform NPA's in the following modes:
- - FINAL APP
- - NAV V/S
- - NAV/FPA
Only FD use is permitted
43
Limitation on APU Starter
After 3 attempts, the Crew must wait 60 minutes before another attempt
44
Max altitude for bleed air extraction (N901NK thru N905NK)
One Pack - - 20,000'
| Two Pack's - - 15,000'
45
Maximum Engine EGT in TOGA (N502NK thru N656NK, N690NK thru N698NK)
635C
46
Maximum Engine EGT during Engine Start on ground or air (N502NK thru N656NK, N690NK thru N698NK)
635C
47
Maximum Engine EGT in TOGA (N657NK thru N687NK)
650C
48
Maximum engine EGT in MCT (N657NK thru N687NK)
610C
49
Maximum engine EGT during engine start on ground or air (N657NK thru N687NK)
635C
50
Maximum engine EGT in TOGA (N901NK thru N937NK)
1,083C
51
Maximuum engine EGT in MCT (N901NK thru N937NK)
1,043C
52
Maximum engine EGT during engine start on ground or air (N901NK thru N937NK)
1,083C
53
Engine Time Limit in TOGA
5 minutes (10 minutes in case of engine failure)
54
Minimum Oil Temperature for Start (M503NK thru N687NK)
-40C
55
Minimum Oil Temperature prior to exceeding idle
-10C
56
Minimum Oil Pressure (N901NK thru N905NK)
65 psi
57
Engine Starter Limitation (N502NK thru N698NK)
- - Cycle is one attempt
- - ground start, 15 second pause between cycles
- - 30 minutes cooling after 3 failed cycles or 5 minutes of continuous cranking
- - Manual starts, 2 minute maximum cycle time
- - For crank, maximum 5 minute cycle time
- - Starter must not be run when N2 is above 10% on ground and 18% in flight
58
Engine Starter Limitation (N901NK thru N937NK)
- - Standard automatic start includes up to 2 attempts is considered one cycle
- - on ground, 35 second pause between cycles
- - 15 minute cooling period subsequent to three failed cycles or 15 minutes of continuous crank
- - Starter must not be run when N2 is above 20%
59
Reverse Thrust Limitation
Maximum reverse should not be used below 70 kts. Idle reverse permitted to aircraft stop.
60
Reduced Thrust Takeoff Limitation
FLEX takeoff is not permitted on contaminated runways
61
Crosswind Operation on ground during engine start
up to 35 kts crosswind
62
Max Altitude with Slats/Flaps extended
20,000'
63
Minimum Fuel Temp Jet A
TAT -34C, monitor FUEL SD Page, fuel must remain above -36C
64
Maximum wing fuel imbalance at takeoff (A319/A320)
1,102 lbs
65
Maximum wing fuel imbalance at landing (A319/A320)
3,306 lbs
66
Maximum wing fuel imbalance at takeoff (N657NK thru N687NK)
882 lbs
67
Maximum brake Temperature for Takeoff (brake fans, if installed - Off)
300C
68
CWT Usable Fuel N697NK, N698NK
Reduce the usable fuel capacity of the Center Wing Tank by up to 42.9 gallons
