A320/319 Lims & Mem Rev. 17

1) 38kts x-wind (gust included)

2) 10kts max. tailwind T/O & Landing?

1) 65kts max. wind for passenger door operations.

1) 40kts (50kts if aircraft is positioned into the  wind or the cargo door is on the leeward side of the aircraft) to Open Cargo Door.

2) 65kts max. to Close Cargo Door.

280kts/M.67

VLO 250kts Extension

VLO 220kts Retraction

25,000 ft.

195kts

300ºC  (If brake fans are in use: 150C)

75% N1 on both engines.

230kts

200kts

Do not use the ISIS bug function - it inhibits (peanut) attitude indicator.

1) No - Do not use LP ground conditioned air while the packs are operating to avoid valve chatter.

2) No - Do not use HP ground pneumatic air while APU bleed air is on (avoids damaging bleed air system).

100' agl

*(Internal FMGS logic prevents sys from engaging the first 5 seconds after liftoff.)

1) Applicable MDA (DA)

**All aircraft have the NO AP DISCONNECT function for non-precision approaches installed.  Currently, N200VA series, N300VA series, N639-N642VA, N837VA and N839VA-N855VA aircraft have the amber DISCONNECT AP FOR LDG PFD message on the installed.

2) Applicable MDA (DA) minus 100'

160 ft. AGL

80 ft. AGL

• Min Height for AP Engagement on G/A
• 100 ft. AGL

• Min Height for AP Use in all other phases?
• 500 ft. AGL

500 ft. AGL

1) Yes - FD use with S.E. operations IS authorized. BUT AP is not in the FINAL APP, NAV V/S, NAV FPA modes.

2) OEI FD use is permitted but no AP use in modes Final App, Nav V/S or Nav FPA.

No Single-Engine appr. AP use during the following modes (only applicable to 319 N521VA-N530VA a/c): 

• FINAL APPR
• NAV V/S
• NAV FPA

FD use is authorized.

Yes - AT use in selected or managed modes is approved with or without AP/FD.

20,000 ft.

• Max. Fuel Imbalance for takeoff:
• Outer tank 800 lbs.  
• Inner tank 1,100 lbs.

• Max Fuel Imbalance inflight and landing:
• Outer tank 1,500 lbs. 
• Inner tank 3,300 lbs.

Do not Takeoff using center tank fuel - center tanks must be emptied first, then wing tanks.

1) 15,000' max. APU bleed dual pack ops.

2)  22,500' max APU bleed air single pack ops.

20,000' max. for apu bleed assisted engine start.

Do not use APU bleed air for wing anti-icing.

After 3 APU starter motor cycles, wait 60 minutes before attempting another start.

When below FL250, APU START (if available).

9.5 Quarts + 0.5 Quarts per Hour of Flight

-40ºC min. for engine starting

-10ºC for takeoff

4 consecutive engine start cycles maximum

15 minutes cooling period required after 4 engine start cycles.

1) 2 minutes duration max for engine start cycle.

2) Pause 20 seconds between engine start attempts.

3) 20% N2 maximum for starter re-engagement.

1) 70 knots

2) No inflight reverse.

3) Do not push-back the aircraft utilizing reverse thrust.

EMERGENCY DESCENT

• Crew O2 Masks: ON
• CREW COMMUNICATIONS: ESTABLISH
• SIGNS: ON
• (EMER DESCENT INITIATE)
• ALT: SET & PULL (descend to 10k' or MEA)
• HDG: SET & PULL (if ETOPS turn 45 degrees rt. or lt. to establish lateral track offset of 15nm from assigned track, turn towards anticipated alt if on a random route, or if on a track that is bracketed on both sides. If on an outside tract turn away from existing tracks.) (IF NOT ETOPS: Turn to avoid traffic)
• SPD/MACH: ADJUST
• Thrust Levers (if A/T off): IDLE
• Spd Brk: FULL (Respecting VLS)

• If Autobrake Is Selected 
• Brake Pedals: PRESS
• If No Braking Available 
• REV: MAX
• Brake Pedals: RELEASE
• A/Skid & N/W STRG: OFF
• Brake Pedals: PRESS (max brake pres. 1k psi)

• If Still No Braking 
• Parking Brake: SHORT SUCCESSIVE APPS

• AP/FD:  OFF
• A/THR:  OFF
• PITCH/THRUST
• Below THRUST RED ALT:  15˚ANU/TOGA

Above THRUST RED ALT & below 10,000':  10˚ANU/CLB

• Above THRUST RED ALT & Above 10,000':  5˚ANU/CLB
• FLAPS (if CONF 0,1,2,3:  MAINTAIN CURRENT CONFIG
• FLAPS (if CONF FULL) Select CONF 3 & MAINTAIN 
• SPEEDBRAKES:  CHECK RETRACTED
• Landing Gear:  UP
• When at or above MSA or Circuit Altitude:  Level off for trouble shooting

• THR LEVERS - MCT
• A/THR - OFF
• SPD/MACH - SET M.78 & PULL (If ETOPS & turn back is req'd, consider green dot to minimize the turn radius)
• HDG - SET & PULL (if ETOPS turn 45 degrees L or R from present track to est. 15 nm offset. If not ETOPS: Turn to avoid traffic.)
• ALT - SET & PULL FL200

WINDSHEAR

• At TAKEOFF
• IF BEFORE V1:  REJECT
• IF AFTER V1 THRUST LEVERS: TOGA
• REACHING VR: ROTATE
• SRS ORDERS: FOLLOW

• AIRBORNE, INITIAL CLIMB OR LANDING:
• THR LEVERS AT TOGA: SET OR CONFIRM
• AP (if engaged): KEEP ON
• SRS ORDERS: FOLLOW
• Maintain CONFIGURATION until out of shear. 
• Closely monitor flight path and speed.
• Recover smoothly to normal climb out of shear.

• WINDSHEAR AHEAD (RED):
• DURING the TAKEOFF Run: REJECT
• WHEN AIRBORNE:
• THR LEVERS: TOGA
• AP (if engaged): KEEP ON
• SRS ORDERS: FOLLOW
• APPROACH LANDING -
• GO AROUND: PERFORM
• AP (if engaged): KEEP ON

• TCAS:
• AP (if engaged): OFF
• Both FDs: OFF
• V/S: ADJ PITCH, MAINTAIN GREEN, AVOID RED
• ATC: NOTIFY

• Simultaneously:
• AP: OFF
• PITCH: PULL UP (pull & maintain full backstick)
• THR LEVERS: TOGA
• SPEED BRAKES LEVER: CHECK RETRACTED
• BANK: WINGS LEVEL or ADJUST

• STALL RECOVERY
• Any Stall Indication, Immediately:
• NOSE DOWN PITCH CONTROL:  APPLY
• (if lack of pitch authority thrust reduction may be necessary)
• BANK:  WINGS LEVEL
• When out of stall (no longer stall indications):
• THRUST:  INCREASE SMOOTHLY AS NEEDED
• SPEED BRAKES:  CHK RETRACTED
• FLIGHT PATH:  RECOVER SMOOTHLY

• If in clean configuration & below FL200:
• FLAP1:  SELECT

STALL RECOVERY AT LIFTOFF:

• THRUST:  TOGA
• (Simultaneously)PITCH ATTITUDE:  15˚ANU
• BANK:  WINGS LEVEL