Limitations Flashcards
Flap operation limits
1 1+f 2 3 Full
1- 230 (slat only, least limiting. Flap will auto extend at 100kts)
1+f- 215 (slat and flap, more limiting. Flap auto retracts at 210kts)
2- 200
3- 185
Full- 177
Wind speed limit for:
Wiper operation
Door operation
Cockpit Window open
230
65
200
Load limitations
Clean
Slats only
Slats and flaps
-1 to 2.5
0 to 2
0 to 2
Max weights, A319, A320
MTOW*
MLW
MZFW
*this varies by aircraft, see placard
A319
66,000*
61,000
57,000
A320
77,000*
66,000
62,500
Landing gear limitations:
Extend
Retract
Keep out
Vtyre
250
220
280
195
Rwy limitations
Width
Slope
Altitude
Taxi speed
45m -/+2 degrees 9200ft Taxi speed Straight: 30kt Straight 77,600kg: 20kt Corners: 10kt
Crosswinds for takeoff and landing
Wet and dry
Wet contaminated (3mm+)
Snow (inc slush, wet snow, dry snow)
Snow contaminated (3mm+)
Ice cold and dry, and slush 3mm+
38
20
29
25
15
Min fuel quantity for takeoff
1500kg,
WING TK LO LVL must not be displayed
Stable Approach Criteria
All approaches should be stable by 1,000 feet above TDZE and MUST be stable by 500 feet RA with the exception of bank angle for a circling procedure.
- Aircraft in landing configuration.
- Target final approach speed + 10/- 5 kt.
- Rate of descent less than 1,000 ft per minute for a 3 degree or nominal 3 degree approach (visual approach). The rate of descent limit may be increased by 150 fpm per 0.5 degree that the published approach path exceeds 3 degrees, e.g. approach path between 3.0 and 3.5 degrees the limit is 1,150 fpm.
- Aircraft on correct lateral and vertical flight path. In the case of ILS or LOC approaches, this means that the aircraft must be with ± 1 dot of the LOC/Glideslope.
- Bank angle less than 15º.
Cross wind limits for FOs, and tail wind limit
FI Xwind limit 20kts
Tailwind limit (all ranks) 10kts.
Brakes temperatures
Max 300 degrees for takeoff
If 150+, fans on. If arc appears over wheel, brake fans on.
Fans on max temp 150 before entering Rwy.
Max flaps extended altitude
20,000 ft
Max APU operating altitudes?
Eng start 20,000’
One pack up to 22,500’
Two packs up to 15,000’
Air bleed extraction for wing anti ice is not permitted.
If in flight it becomes necessary to start the APU, we should consult the FCOM or QRH for limiting factors, rather than rely on memory.