Limitations Flashcards
Max Landing Weight
502NK-536NK
137,788 lbs
Max Landing Weight
601NK-650NK
145,505 lbs
Max Landing Weight
901NK-905NK
148,591 lbs
Max Landing Weight
587NK, 588NK, 657NK-683NK
171,519 lbs
Max Altitude
FL 398
Runway Slope (mean)
+/-2%
Runway Altitude
All except 535NK, 536NK
9,200 ft
Nominal Runway Width
45m (148ft)
Max X-wind Landing
38 kt (gust included)
Max Tailwind for Takeoff
15 kt
Max Tailwind for Landing
10 kt
Max Wind for Passenger Door Operation
65 kt
Max Crosswind for Takeoff
901NK-905NK
35 kt (gust included)
Vle
280kt/M.67
Vlo Extension
250kt/M.60
Vlo Retraction
220kt/M.54
Max Altitude Landing Gear May Be Extended
25,000ft
Windshield Wipers Max Speed
230kt
When Taxi Weight Higher than 167,550 lb, taxi speed in a turn
587NK, 588NK, 601NK-905NK
20kt
Do not use conditioned air simultaneously from…(to avoid any adverse effects on the air conditioning system)
PACKS and LP ground unit
Do not use….when the APU supplies bleed air to avoid any adverse effects to the bleed system
HP ground unit
Max positive differential pressure
9.0 psi
Max negative differential pressure
-1.0 psi
Minimum Height for use of Autopilot
Takeoff with SRS mode
100 ft AGL
Minimum Height for use of Autopilot
Straight-in non-precision approach
Applicable Minimum
Minimum Height for use of Autopilot
Circling Approach
Applicable Circling Minimums -100 ft
Minimum Height for use of Autopilot
ILS Approach when CAT 2 or CAT 3 is not displayed on the FMA
160ft AGL
Minimum Height for use of Autopilot
Go-Around (AP or FD engagement)
100ft AGL
Minimum Height for Use of Autopilot
All Other Phases
500ft AGL (A319/A320) 900ft AGL (A321)
Minimum Height for use of Autopilot
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:
Highest of:
Minimum or 500ft (A319/A320)
Minimum or 900ft (A321)
NAV mode may be used in the terminal area, provided:
- GPS PRIMARY is available
- HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or
- FMS navigation is cross-checked with NAVAID raw data
If one engine is inoperative, it is not permitted to use the Autopilot to perform NPAs in the following modes:
FINAL APP, NAV V/S, NAV/FPA
Only FD use is permitted
Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out All Engines Operative(AEO) And One Engine Inoperative (OEI) N502NK-N536NK
(AEO)
Headwind - 20kt
Tailwind - 5kt
Crosswind - 15kt
(OEI)
Headwind - 15kt
Tailwind - 5kt
Crosswind - 10kt
Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out
All Engines Operative(AEO)
N601NK-N683NK, N587NK, N588NK
Headwind - 30kt
Tailwind - 10kt
Crosswind - 15kt
Max Wind Conditions for CAT II or CAT III Automatic Approach, Landing and Roll Out
All Engines Operative(AEO)
N901NK-N905NK
Headwind - 20kt
Tailwind - 5kt
Crosswind - 15kt
Max operating Altitude with slats and/or flaps extended
20,000ft
Max Fuel Imbalance at Takeoff, Inner Tanks
502NK-536NK, 601NK-650NK, 901NK-905NK
1,102 lb
Max Fuel Imbalance In Flight and At Landing, Inner Tanks
502NK-536NK, 601NK-650NK, 901NK-905NK
3,306 lb
Max Fuel Imbalance in Flight and At Landing
587NK, 588NK, 657NK-683NK
2,910 lb
Max Fuel Imbalance at Takeoff
657NK-683NK
882 lb
Max brake temperature for Takeoff (brake fans off)
300 C
APU Starter duty cycles
After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles
EGT limits
Takeoff and Go Around
502NK-536NK, 601NK-650NK
5 min, 635 C
10 min, 635 C only in case of engine failure
EGT limits
MCT
502NK-536NK, 601NK-650NK
587NK, 588NK, 657NK-683NK
Unlimited 610 C
EGT limits
Starting
502NK-536NK, 601NK-650NK
587NK, 588NK, 657NK-683NK
635 C
EGT limits
Takeoff and Go Around
901NK-905NK
5 min, 1,083 C
10 min, 1,083 C only in case of engine failure
EGT limits
MCT
901NK-905NK
Unlimited, 1,043 C
EGT limits
Starting
901NK-905NK
1,083 C
EGT limits
Takeoff and Go Around
587NK, 588NK, 657NK-683NK
5 min, 650 C
10 min, 650 C only in case of engine failure
Minimum Oil Temperature prior to exceeding idle
502NK-683NK
-10 C
Minimum Oil Temperature for Starting
502NK-683NK
-40 C
Minimum Oil Pressure
901NK-905NK
65 psi
Stater Cycles
502NK-683NK
3 consecutive cycles, for manual start, observe a 2 min max start cycle time
Pause 15s between starts
Cooling period, following 3 start attempts or 5 min of continuous cranking wait 30 min
No running engagement if the starter, when N2 is above 10% on ground, or 18% in Flight
Starter Cycles
901NK-905NK
3 consecutive start attempts, 35s in between each cycle
After 3 cycles, or 15 min of continuous or cumulative cranking: 15 min cooling period
No running engagement of the starter, when N2 is above 20%
Maximum reverse should not be used below
70 kt (Idle reverse is permitted down to aircraft stop)
Takeoff on contaminated runway
Reduced thrust takeoff is not permitted on contaminated runways
Max Crosswind for engine start
35kt
Vmo/Mmo
350kts/M.82
Max Tire Ground Speed
195 kts
Cockpit Window Open Max Speed
200 kt
Max Continuous Load per Generator
100%
90KVA
Max Continuous Load per TR
200 A
For JET A only, if TAT reaches…,monitor the FUEL SD page that the fuel temp remains higher than…
-34C, -36C
Minimum Fuel Quantity for Takeoff
3,307 lb and the WING TK LO LVL warning must not be displayed on the ECAM
Fuel Management, tanks must be emptied in the following order:
N502NK-N536NK, N601NK-N628NK
Center tank then wing tanks
Takeoff on center tank is prohibited
Hydraulic normal operating pressure
3,000psi +/- 200
Taxi with deflated Tires
If one tire is deflated on one or more gears( maximum of 3 tires) Speed should be limited to
7kts
Taxi with deflated Tires
If two tires are deflated in the same main gear(the other main gear tires not being deflated) Speed should be limited to…and nose wheel steering angle limited to…
3kt and 30*
Nosewheel steering limits with hand wheels and for towing and pushback
75* when using hand wheels
95* for towing and pushback
Tail Strike Pitch Attitude
A319
(Struts Compressed)
13.9*
Tail Strike Pitch Attitude
A320
(Struts Compressed)
11.7*
Tail Strike Pitch Attitude
A321
(Struts Compressed)
9.7*