Non-Memory limitations Flashcards
AIRCRAFT STRUCTURAL
Maneuvering Load Limits(clean): ?
Maneuvering Load(slats/flaps ext.): ?
Max Pos. Differential Pressure: ?
Max Neg. Differential Pressure: ?
Safety Relief Valve Setting: ?
AIRCRAFT STRUCTURAL
Maneuvering Load Limits(clean): -1.0gto 2.5g
Maneuvering Load(slats/flaps ext.): 0gto 2g
Max Pos. Differential Pressure: 9.0psi
Max Neg. Differential Pressure: -1psi
Safety Relief Valve Setting: 8.6psi
ALTIMETER CHECK
GROUND CHECK
- ADR3/1OR3/2 ?
- STANDBYALT ?
- ISIS ?
ALTIMETER CHECK
GROUND CHECK
- ADR3/1OR3/2 20ʼ
- STANDBYALT 300ʼ
- ISIS 100ʼ
FL390/0.78M
- ADR1/2 ?
- ADR3/1OR3/2 ?
- STANDBYALT ?
- ISIS ?
FL390/0.78M
- ADR1/2 130ʼ
- ADR3/1OR3/2 195ʼ
- STANDBYALT 445ʼ
- ISIS 445ʼ
ALTITUDELIMITATIONS
MaxRunway Altitude ?
Flaps/Slats extended ?
MaxALTfor APU Elec & Start with A/CElec ?
Max ALTfor APU Start from A/CBatt ?
Max ALTfor 1 packw/ Electrical ?
Max ALTfor assisted ENG Start ?
Max ALTfor 2 packsw/ Electrical ?
ALTITUDELIMITATIONS
MaxRunway Altitude 9,200’
Flaps/Slats extended 20,000ʼ
MaxALTfor APU Elec & Start with A/CElec 39,000’
Max ALTfor APU Start from A/CBatt 25,000’
Max ALTfor 1 packw/ Electrical 22,500’
Max ALTfor assisted ENG Start 20,000’
Max ALTfor 2 packsw/ Electrical 15,000ʼ
APU LIMITATIONS APU Starter ? Maximum EGT ? Max EGT for Start (below 35,000') ? Max EGT for Start (above 35,000') ? Max RPM N (Auto Shutdown) ?
APU LIMITATIONS
APU Starter 3cycles separated by 1minutecool down,
then 60minutes off.
Maximum EGT 675°C
Max EGT for Start (below 35,000’) 1090°C
Max EGT for Start (above 35,000’) 1120°C
Max RPM N (Auto Shutdown) 107%
AUTOPILOT
• The use of AP or FD in OPEN DES or DES mode is?
AUTOPILOT
• Not permitted inside the FAF or below 1000ft
AGL on a visual approach.
• The use of auto thrust is approved with or
without AP/FD in selected or managed mode
AUTOLAND DEMONSTRATED CAPABILITY
A319/320: ?
A321: ?
AUTOLAND DEMONSTRATED CAPABILITY
A319/320: 9,200ʼ
A321: 5,750ʼ
AUTOLAND AUTO BRAKES REQUIREMENTS
Runway less than 8,000feet: ?
Runway8,000feet or longer: ?
AUTOLAND AUTO BRAKES REQUIREMENTS
Runway less than 8,000feet: MEDIUM
Runway8,000feet or longer: LOW or MEDIUM
AUTOLANDRESTRICTIONS 320/NEO/321 319
Headwind ? ?
Xwind ? ?
Tailwind ? ?
Min/Max wind ?
Braking Action ?
AUTOLANDRESTRICTIONS 320/NEO/321 319
Headwind 30kts 20kts
Xwind 15kts 15kts
Tailwind 10kts 5kts
Min/Max wind 5kts/15kts
Braking Action Fair or Better
AUTOLANDPERFORMANCE LIMITS (BELOW 500FT)
• Glideslope Deviation ?
• Localizer Deviation ?
• Airspeed ?
• Max Rate of Descent ?
• Airspeed ?
• Bank ?
• Pitch ?
AUTOLANDPERFORMANCE LIMITS (BELOW 500FT) • Glideslope Deviation
BRAKE LIMITATIONS
Max Brake Temp for Takeoff(Fans off): ?
Max Hydraulic Pressure: ?
BRAKE LIMITATIONS
Max Brake Temp for Takeoff(Fans off): 300°C
Max Hydraulic Pressure: 3200psi
ELECTRICAL
Max Cont. Load per Gen: (90 kVa) ?
Max Cont. Load per T/R: ?
ELECTRICAL
Max Cont. Load per Gen: (90 kVa) 100 percent
Max Cont. Load per T/R: 200A
ENGINE OIL TEMPERATURE
Maximum continuous: ?
Maximum transient: (15minutes) ?
Min Starting Temp: ?
Minimum temperature for takeoff: ?
Max N1RPM: (A320NEO) ?
(A319, A320& A321) ?
Max N2RPM: (A320NEO) ?
(A319,A320& A321) ?
ENGINE OIL TEMPERATURE
Maximum continuous: 140°C
Maximum transient: (15minutes) 155°C
Min Starting Temp: -40°C
Minimum temperature for takeoff: 19°C
Max N1RPM: (A320NEO) 101%
(A319, A320& A321) 104%
Max N2RPM: (A320NEO) 116.5%
(A319,A320& A321) 105%
EGT Limit
NEO
TOGA ?
MCP ?
Starting
Ground ?
Flight ?
CEO
TOGA
TOGA ?
MCP ?
Starting
Ground ?
Flight ?
EGT Limit
NEO
TOGA 1060c
MCP 1025c
Starting
Ground 750c
Flight 875c
CEO
TOGA
TOGA 950c
MCP 915c
Starting
Ground 725c
Flight 725c
ENGINE REVERSE THRUST
ENGINE REVERSE THRUST
- Selecting reverse thrust in flight is prohibited.
- Backing with reverse thrust is not permitted.
• Max reverse will not be used below 70knots
(Idle reverse is allowed down to aircraft stop).
• Except in an emergency, reverse thrust is not
authorized to reduce taxi speed.
ENGINE STARTERCYCLES
A320NEO:
?
319/320/321:
?
ENGINE STARTERCYCLES
A320NEO:
3 cycles of 2minutesmaxwith 60secs
in between, then 15minutesto allow
starter to cool before another 3cycles.
319/320/321:
4 cycles of 2minutes max with 20 secs
in between, then 15minutesto allow
starter to cool before another 4cycles.
FLAPS/SLATSSPEEDS – (A319/A320) (1 Slats) ? (1 Slats& Flaps) ? (2) ? (3) ? (FULL) ?
VFE: VFEnext-10knots,Unless EMER to avoid exceeding placarded speeds in case of unanticipated speed increases (e.g., wind change or turb).
FLAPS/SLATSSPEEDS – (A319/A320) (1 Slats) 230 (1 Slats& Flaps) 215 (2) 200 (3) 185 (FULL) 177
VFE: VFEnext-10knots,Unless EMER to avoid exceeding placarded speeds in case of unanticipated speed increases (e.g., wind change or turb).
FLIGHTMANEUVERING LOADACCELERATIONLIMITS
Clean configuration ?
Flaps retracted and slats extended ?
Flaps and slats extended ?
FLIGHTMANEUVERING LOADACCELERATIONLIMITS
Clean configuration -1.0gto +2.5g
Flaps retracted and slats extended 0.0gto +2.0g
Flaps and slats extended 0.0gto +2.0g
FUELLIMITS
Fuel Temp Good to Go: ?
(otherwise see VOL.II)
Minimum QTY for Takeoff: ?
?
FUELLIMITS
Fuel Temp Good to Go: -36°Cto 49°C
(otherwise see VOL.II)
Minimum QTY for Takeoff: 3300lbs
(ECAM WING TKLOLVL must not display)
FUEL IMBALANCE – MAX (TAKEOFF)
A319/320/320NEO
• Inner Tanks Fuel Qty (heaver tank) Max Imbalance
Full ?
6613lbs. ?
3196lbs. ?
• Outer Tanks Max Imbalance ?
A321 Fuel Qty (heaver tank) Max Imbalance
Full ?
6614lbs. ?
1543lbs. ?
FUEL IMBALANCE – MAX (TAKEOFF)
A319/320/320NEO
• Inner Tanks Fuel Qty (heaver tank) Max Imbalance
Full 1102lbs.
6613lbs. 2314lbs.
3196lbs. 3196lbs.
• Outer Tanks Max Imbalance 815lbs.
A321 Fuel Qty (heaver tank) Max Imbalance
Full 882lbs.
6614lbs. 882lbs.
1543lbs. 1543lbs.
FUEL IMBALANCE – MAX (IN FLTANDLANDING)
A319/320/320NEO
• Inner Tanks Fuel Qty (heaver tank) Max Imbalance
Full ?
9479lbs. ?
3196lbs. ?
• Outer Tanks Max Imbalance ?
A321 Fuel Qty (heaver tank) Max Imbalance
Full ?
8818lbs. ?
5180lbs. ?
WARNING -Takeoff with center tank fuel supplying the
engines is PROHIBITED
FUEL IMBALANCE – MAX (IN FLTANDLANDING)
A319/320/320NEO
• Inner Tanks Fuel Qty (heaver tank) Max Imbalance
Full 3306lbs.
9479lbs. 3527lbs.
3196lbs. 4960lbs.
• Outer Tanks Max Imbalance 1521lbs.
A321 Fuel Qty (heaver tank) Max Imbalance
Full 2910lbs.
8818lbs. 3196lbs.
5180lbs. 5180lbs.
WARNING -Takeoff with center tank fuel supplying the
engines is PROHIBITED
OIL PRESSURE/QUANTITY
Min Oil Pressure: ?
Min Oil Quantity:
CEO: ?
NEO: ?
OIL PRESSURE/QUANTITY
Min Oil Pressure: 17.4psi
Min Oil Quantity:
CEO: 9.5q plus 0.5qpr hr.
NEO: The minimum oil quantity is the highest of:
- 10.6 qts, or
- 9.0 qts + .5 qts per every hour of est flight time.
OXYGENREQUIREMENTS
For A/C201-216, 228-232 and 910-949:
2 Flight Crew ? psi
2 Flight Crew +1 Observer ? psi
2 Flight Crew +2 Observers ? psi
For A/C301-399:
CPT ? psi
CPT and Observer ? psi
FO ? psi
FO and 4th Observer ? psi
For A/C220-227, 223-238, and 701-799:
2 Flight Crew ? psi
2 Flight Crew +1 Observer ? psi
2 Flight Crew +2 Observers ? psi
OXYGENREQUIREMENTS
For A/C201-216, 228-232 and 910-949:
2 Flight Crew 600psi
2 Flight Crew +1 Observer 800psi
2 Flight Crew +2 Observers 1000psi
For A/C301-399:
CPT 600psi
CPT and Observer 800psi
FO 600psi
FO and 4th Observer 800psi
For A/C220-227, 223-238, and 701-799:
2 Flight Crew 900psi
2 Flight Crew +1 Observer 1100psi
2 Flight Crew +2 Observers 1400psi
REDUCED THRUST TAKEOFF
REDUCED THRUST TAKEOFF
• Takeoff at reduced thrust is permissible, only if the
airplane meets all applicable performance requirements
at the planned takeoff weight, with the operating
engines at the thrust available for the assumed
temperature.
• Thrust reduction must not exceed25% of the full
rated takeoff thrust. To meet this requirement, the
flexible temperature (T MAX FLEX) must not be higher
than ISA +60°Cfor A319,ISA +53°Cfor A320,ISA +55°C
for A320NEO and ISA +43°CforA321.
• The temperature must not be lower than actual OAT.
• Takeoff at reduced thrust is allowed with any
inoperative item affecting the performance, only if the
associated performance shortfall has been applied to
meet all performance requirements at the takeoff
weight, with the operating engines at the thrust
available for the flex temperature.
• Takeoff at reduced thrust is prohibited:
- On slippery or contaminated runways
- When suspected, reported, or known wind
shear is present
- When a Special Departure Procedure specifies
full thrust for takeoff.
RUNWAY LIMITS
Runway slope (maximum): ?
Maximum Runway altitude: ?
Minimum Runway Width: ?
A/C227,228, 229: ?
RUNWAY LIMITS
Runway slope (maximum): ±2 percent
Maximum Runway altitude: 9200 ft
Minimum Runway Width: 148 ft / 45m
A/C227,228, 229: 100 ft / 30m
RUNWAY OPERATIONS (NARROW)
Any runway less than ?
• Autoland is ?
• Diversion to normal width runway is recommended in
case of:
?
?
?
?
?
RUNWAY OPERATIONS (NARROW)
Any runway less than 148ft/45mwide.
• Autoland is not authorized
• Diversion to normal width runway is recommended in
case of:
– Rudder jam
– Rudder pedal jam
– Yaw damper fault
– No nose wheel steering
– Any wheel brake inoperative
SPEED BRAKE LIMITATION
• ALL NEO AIRCRAFT
For approach, use of speed brakes at or below ?
not permitted if:
?
?
SPEED BRAKE LIMITATION
• ALL NEO AIRCRAFT
For approach, use of speed brakes at or below 240kt
not permitted if:
-Gross Weight CG is above 35% or
-In overweight landing conditions
WEIGHT LIMITS
Maximum Taxi Weight:
A320 - ? NEO - ? A321 - ?
Maximum Takeoff Weight:
A320/NEO - ? A321 - ?
Maximum Landing Weight:
A320 - ? NEO - ? A321 - ?
WEIGHT LIMITS
Maximum Taxi Weight:
A320 - 170,637 NEO - 170,637 A321 - 207,014
Maximum Takeoff Weight:
A320/NEO - 169,755 A321 - 206,132
Maximum Landing Weight:
A320 - 142,198 NEO - 148,591 A321 - 171,519
