Limitations & Memory Items Flashcards
(18 cards)
Unreliable Speed Indication
- LAND AS SOON AS POSSIBLE
*2. Autopilot and Autothrust……..off
*3. Flight Directors…………………….off
*4. If below safe altitude, pitch and thrust:
Below THR RED altitude…..15 degree and TOGA
Above THR RED &
below 10,000 feet MSL…..10 deg and CLB
Above 10,000 feet MSL…..5 degrees and CLB
SMOKE/FUMES
- LAND AS SOON AS POSSIBLE
- If smoke/fumes are perceptible
*Oxygen masks and
regulators (if required)…..On, 100%
*Crew communications….. Establish
Emergency Descent
- Oxygen masks and regulators…..As required
- Crew communications…..Establish
Flight Deck Emergency Access Alarm
COCKPIT DOOR…..LOCK
Loss of Braking
- Brake pedals…..Release
- A/SKID & N/W STRG…..OFF
- Brake pedals…..Press, 1000 PSI max
- if still no braking:
PARKING BRK…..Successive applications
Reverse…..As required
CROSSWIND GUIDELINES – TAKEOFF AND LANDING
Runway Condition Code 6
Control/Braking Action Dry
Surface Condition (Smooth, Grooved, or
PFC) Dry
Normal Runway Width (≥ 148 Feet)?
Narrow Runway Width (< 148 Feet)?
★38
★38
OPERATING SPEEDS
VMO/MMO (1)
(319) (320) (NEO)
★350 knots/.82 Mach
(1) This limit must not be intentionally exceeded in any flight regime.
If anticipating severe turbulence, the PF should target _____ while the __________
.76 Mach
PM references this table for the best penetration speed
TAILWIND – MAXIMUM SPEEDS
(319)
★10 knots takeoff
10 knots landing
(320)
★15 knots takeoff (1)
10 knots landing
(NEO)
★15 knots takeoff
15 knots landing (2)
(1) (320 N4901U and N1902U) ★ Takeoff tailwind limit is 10 knots.
(2) For landing with a tailwind greater than 10 knots, FLAPS FULL is recommended.
ENVIRONMENTAL AND OPERATING ENVELOPE
Maximum altitude
★39,100 feet from -70°C to -30°C
OXYGEN (FLIGHT DECK) REQUIREMENTS – MINIMUM PSI
★If oxygen pressure is below _____, reference the aircraft-specific table.
1350 PSI
WEIGHT LIMITATIONS (1000 LBS)
(319) 1 (320) 1 (NEO) 1
Maximum landing weight (MLW)
319 (1)…..137.7
320 (1)…..142.2
NEO (1)…..174.6
(1) The maximum weight limits may be further restricted due to factors such as MELs,
climb performance, obstacle clearance, brake energy limit, and tire speed.
ENGINE ANTI-ICE
Weather conditions requiring engine anti-ce
1. Ground operations?
2. Climb/cruise?
3. Descent/approach?
★ ≤ 10°C OAT and icing conditions exist
★ ≤ 10°C TAT and ≥ -40°C SAT and icing conditions exist
★ ≤ 10°C TAT and icing conditions exist
AUTOPILOT – MINIMUM ENGAGEMENT HEIGHT
- After takeoff or a manual go-around
- (NEO) Approach with F-G/S mode
- Approach with FINAL APP or FPA
- Circling approach
- ILS non-autoland with CAT 1 FMA
- ILS non-autoland with CAT 2 FMA or CAT 3 FMA
- AP or FD in OPEN DES or DES
1..★100 feet AGL and at least
5 seconds after liftoff
2. ★200 feet AGL
3. ★◘ 250 feet AGL (2)
4. ◘ 600 feet AGL
5. ★160 feet AGL
6. ★80 feet AGL
7. ★◘Higher of 1000 feet or
MDA/MDH
(2) On non-ILS/GLS approaches, the autopilot must be disconnected no later than the
higher of the mode reversion point or the AGL limitation. When charted, the mode
reversion point is represented by the “M” in the chart profile. When not charted, the
mode reversion is 50 feet AGL.
(319) (320) ENGINE OIL
Minimum quantity (before start)
11 quarts (1)
★14 quarts (2)
(1) The limitation is 11 quarts plus estimated consumption. Average estimated
consumption is 0.3 quarts per hour.
(2) This is a memory item, not a limitation.
(NEO) ENGINE OIL
Minimum quantity at or above -30°C (before start)
★14 quarts (1)
(1) This is a memory item and the limitation.
OPERATING ALTITUDE – MAXIMUM
Slats and/or flaps extended?
★20,000 feet
