LIMITATIONS Flashcards
(47 cards)
Wingspans NON SHARKLET
111’ 10”
Wingspans SHARKLET 320/321
117’ 5”
Max Landing Weight 319 N502NK THRU N534NK
137,788
Max Certified Altitude
FL398
Max Landing Weight 320 N601NK THRU N617NK
145,505
Max Landing Weight 321
171,519
Applicable to N502NK THRU N672NK
- Runway Slope
- Max Runway Altitude
- Normal Runway Width
- Max demonstrated crosswind
Applicable to N502NK THRU N672NK
- Runway Slope ……………………… +/- 2%
- Max Runway Altitude ……………. 9200
- Normal Runway Width ………….. 148 (see note)
- 38 kt (gust included)
NOTE: Narrow runway ops procedures up to 98 ft
Applicable to N502NK THRU N672NK
Wind for takeoff and landing
Max demonstrated cross wind …..
Max Tailwind - Takeoff ………………
Max Tailwind - Landing ……………..
Applicable to N502NK THRU N672NK
Max demonstrated cross wind ……………..38 knots
Max Tailwind - Takeoff …………………………15 knots
Max Tailwind - Landing ……………………….. 10 knots
Landing Gear Speed Limitations Max Extended Max Extension Max Retraction Max Altitude to Extend
Max Extended (VLE) ............................. 280 kts/M.67 Max Extension (VLO Extension) ........... 250 kts Max Retraction (VLO Retraction) ......... 220 kts Max Altitude to Extend ......................... FL250
Max Speed - Windshield Wipers
230 kts
Landing Gear Speed Limitations Max Extended Max Extension Max Retraction Max Altitude to Extend Brakes maximum temperature for takeoff
Max Extended (VLE) ............................. 280 kts/M.67 Max Extension (VLO Extension) ........... 250 kts Max Retraction (VLO Retraction) ......... 220 kts Max Altitude to Extend ......................... FL250 Brake fans (if installed) off...............300° C
Max Taxi Speed in a Turn (320/321)
Taxi Weight higher than 167,550, do not exceed 20 kts
Air Conditioning with LP Ground Unit
Do not use A/C from Ground Unit and PACKS simultaneously to avoid chattering of non-return valves
A/C with HP Ground Unit
Do not use HP Ground Unit when the APU is supplying bleed air. This avoids bleed system damage
AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot
Takeoff with SRS mode
100 ft AGL
Cabin Pressure
Max positive
Max negative
Safety relief valve setting
Max positive ………………. 9.0 psi
Max negative ……………… -1.0 psi
8.6 psi
AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot
Straight-in non-precision approach
Applicable Minimum
AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot
Circling Approach
Applicable Circling Minimums - 100 ft
AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot
ILS approach when CAT2 or CAT3 is not displayed on the FMA
160 ft AGL
AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot
Go-Around (AP or FD engagement)
100 ft AGL
AUTO PILOT FUNCTION
Minimum Height For Use of Autopilot
All other phases
500 ft AGL (A319/A320)
900 ft AGL (A321)
AUTO PILOT FUNCTION
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 500 ft (A319/A320)
Minimum or 900 ft (A321)
NAV mode may be used in the terminal area, provided:
- GPS PRIMARY is available, or
- HIGH accuracy is displayed, and the appropriate
RNP is checked or entered on the MCDU, or - NAVAID raw data is monitored.
Non-Precision Approaches with Engine-Out
A319/A321
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
