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.