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84 Cards in this Set
- Front
- Back
- 3rd side (hint)
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Aircraft length |
37,57 m |
3 times Boeing 7,57 |
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Wingspan |
34,10 m |
NIL |
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Aircraft height |
12,14 m |
NIL |
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Flight Instrument Tolerances on Ground |
Altitude PFD 1+2 - 25ft (to pupl. Alt) ADR's - 20ft ISIS + any ADR - 100ft
Speed any ADR/ISIS - 6kts
Heading ND 1+2 - 4° |
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Max. App. Parameter Exeedance and associated callouts |
IAS +10 / -5 kts. "speed" Pitch +10°/-2.5° "pitch" v/s 1000ft/min "sinkrate" Bank 7° "bank" LOC 1/2 dot "localizer" G/S 1/2 dot "glideslope" NPA's XTK>0.1NM "crosstrack" V/Dev.>1/2 Dot "vertical deviation" VOR Course>2.5° or 1/2 dot "course" NDB Course>5° "coures" Alt.-Distance Check "__ft high/low" |
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Actions after Eng. Failure in flight |
1. Thrust Levers MCT 2. A/THR Disconnect 3. Select Speed acc. Strategy 4. if appropriate select a heading 5. Select Eng. out altitude acc. strategy 6. ECAM Actions
standard strategy: .78M/300kts / eng. out max. altitude on MCDU PROG Page
obstacle strategy: green dot speed / drift down ceiling on MCDU PERF CRZ Page
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Discription of CAT III Approach |
1000 ft ECAM actions must be completed 700 ft FMS Data frozen (e.g. ILS tune inhibited) 400 ft FCU frozen 350 ft FMA: LAND 200 ft Auto Land Warning Light is armed 100 ft Alert Height 40 ft FMA: FLARE 30 ft Thrust IDLE 10 ft autocall "Retard" Touch Down FMA: ROLL OUT |
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GPWS Basic Modes |
Mode 1 Excessive descent rate Mode 2 Excessive terrain closure rate Mode 3 Altitude loss after T/O or G/A Mode 4 Unsafe terrain clearance Mode 5 Excessive deviation below G/S |
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APU max. EGT's |
max. continuous: 675°C
start EGT below 35.000ft: 1090°C
start EGT above 35.000ft: 1120°C |
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min. pavement width for a 180° turn |
22,9 m |
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Limitations for non precision approach (NPA) with managed guidance (FINAL APP) |
Managed guidance (FMA: FINAL APP) only if: - App. is defined in NAV data base - App. is xchecked with published procedure - final App. is not modified by crew
FINAL APP, NAV - V/S, NAV - FPA is not permitted with one engine out
=> use TRK - FPA or HDG - V/S |
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Holding Speeds |
<=14.000ft 230kts >14.000ft - 20.000ft 240kts >20.000ft - 34.000ft 265kts >34.0000ft 0.83M |
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Load Factor Limitation |
Clean: +2.5g / -1g
other config.: +2g / 0g |
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APU - max. altitude for engine start |
20.000 ft |
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APU - max. altitude with 2 packs |
15.000 ft |
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APU - max. altitude 1 pack |
22.500 ft |
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APU - max. altitude bleed and electric |
22.500 ft |
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APU - max. altitude electric |
41.000 ft |
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APU - max. altitude for APU start on battery power |
25.000 ft |
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max. APU speed |
107% indicateted on ECAM
(equals 106% actual APU speed. APU shuts off at 107% automatically) |
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APU starter limitations |
after 3 cycles wait 60 minutes |
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Turbulence Penetration Speed |
app. 260KIAS / M .76
(QRH-Abn/Emer procdr.-MISC-Severe Turbulence) |
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EGPWS - additional functions to GPWS |
TAD - Terrain Awareness Display
60 sec. • Caution: "terrain ahead"/ "obstacle ahead"
30 sec. • Warning: "terr. ahead-pull up" / "obstacle ahead-pull up"
TCA - Terrain Clearance Floor
RFCF - Rwy Field Clearance Floor |
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Limitations for NAV mode in terminal area
(Ref.: FCOM-UM-22-10-USE OF NAV) |
• GPS Primary or
• High accuracy and appropriate RNP is checked or entered in MCDU
• FMS navigation is x-checked with NAV aid raw data. |
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Requirements for RNAV and RNP RNAV Approach
(Ref.: FCOM-UM-22-10-USE OF NAV...) |
• GPS Primary
• Autopilot and/or F/D engaged
• WGS 84 coordinate system |
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Bank Angle Protection |
. |
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Total Fuel Quantity |
18.700 kg
(app. - depends in S/N) |
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Max. Zero Fuel Weight |
61.000 kg |
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RCAM - Runway Condition Assessment Matrix Max. X-Wind for T/O and Ldg.
BA medium |
15 kts |
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Center Tank Fuel Quantity |
6480 kg |
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Definition Optimum FL |
Altitude with best specific range (NM per kg of Fuel) for a given weight and flight proceedure (e.g. LRC, ECON) |
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Noise Abatement Departure Climb - NADP 1 |
T/O thrust to min. 800ft AGL with V2+10
Climb Thrust at min. 800ft AGL with V2+10
Flap retraction at 3000ft AGL and accelleration to final climb speed |
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Noise Abatement Departure Climb - NADP 2 |
T/O thrust with V2+10 to min. 800ft AGL.
At min. 800ft AGL retract flaps and accellerate to clean speed.
Thrust reduction during flap retraction to ensure good accelleration.
At 3000ft AGL accellerate to final climb speed. |
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Wake turbulence categories |
Light < 7000kg
7000kg < Medium < 136000kg
136000kg < Heavy
Super = A380 |
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Distance at green dot speed and rate of descent all engines out |
2.5 NM / 1000 ft
1600 ft / min |
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Standard EASA minima for precision approaches |
CAT I DH 200ft / RVR 550m
CAT II DH 100ft / RVR 300m
CAT IIIA DH<100ft / RVR 200m
CAT IIIB DH<100ft / RVR 150m DH<50ft / RVR 125m no DH - RVR 75m |
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Max. wind for door operation |
Pax Door - 65 kts
Cargo Doors - 40 kts • 50 kts if A/C nose into wind or doors at lee side >65 kts => close cargo doors |
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Max. Ldg. Gear speeds |
Vlo retr. - 220 kts / M 0.54
Vlo ext. - 250 kts / M 0.60
Vle - 280 kts / M 0.67 |
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Pitch attitude protection |
• Conf. 0 - 3: 30° Nose up progressively reduced to 25° at low speed.
• Conf. Full: 25° Nose up progressively reduced to 20° at low speed.
• 15° Nose down
• FD's disappear >25°NU; <13° ND
• FD's return <22°NU; >10°ND |
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Starter cycle CFM Engine |
• 4 cycles of max. 2 min.
• Pause in between 20 sec.
• after 4 cycles 15 min. pause
• no engagement if N2 > 20% |
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CFM engine max. EGT's |
• Start - 725°C
• TOGA 5 min. - 950°C OEI 10 min. - 950°C
• MCT - 915°C |
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When is windsheer detection provided and by which computer? |
• 3 sec. after lift off up to 1300 ft AGL
• for LDG. 1300 ft AGL down to 50 ft
• with at least conf. 1 selected
• provided by FAC |
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When is windsheer detection provided and by which computer? |
• 3 sec. after lift off up to 1300 ft AGL
• for LDG. 1300 ft AGL down to 50 ft
• with at least conf. 1 selected
• provided by FAC |
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max. radius of wingtip with a 180° turn |
21,99 m |
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max. differential pressure |
• positive 9,0 psi
• negative - 1,0 psi
• safety valve opens at 8,6 psi |
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High speed protection |
• activated at or above Vmo / Mmo
• AP disengages
• ECAM "O/SPEED" at Vmo + 4 / Mmo + 0.006
• if sidestick released => 0° bank
• max. bank 40°
• if Vmo/Mmo exceeded: - sidestick nose down authority reduced - nose up order applied |
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Rate of descent awareness |
Height above terrain / ROD
>10.000ft / no limit >5.000ft / 5.000 fpm >4.000ft / 4.000 fpm >3.000ft / 3.000 fpm >2.000ft / 2.000 fpm >1.000ft / 1.500 fpm <1.000ft / 1.000 fpm
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max. number if UM's |
4 |
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max. number of deportees |
• DEPA - 2
• DEPU - 4 + own children
Exeptions by NPFO / security department |
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- max. number PETC
- max. weight
- what kind of animals |
• max. 5
• max. 8kg incl. container
• cats, dogs |
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All engines out distance on final - conf. 3, ldg gear down |
1,2NM / 1000ft |
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LMC limitation |
• A319/320/321 - 500 kg
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When is maintanance action required regarding brake temperature? |
• Temp. diff. on the same gear >150°C and either brake temp. >600°C
• Temp. diff. on the same gear >150°C and one brake temp. <\= 60°C
• Diff. of average LH + RH brake >200°C
• one brake >900°C
• a fuse plug has melted |
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Approximate one engine inop. ceilling at ISA +15°C |
76t - FL 210
72t - FL230
68t - FL240
64t - FL250 |
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High AOA protection |
If AOA > alpha prot - AP disengages
- AOA is proportional to side stick deflection => side stick controls: alpha prot. - alpha max
- release of side stick: AOA = alpha prot
alpha protmax |
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Fire fighting category A319 bis A321 |
A319 - CFR 6 A320 - CFR 6 A321 - CFR 7 |
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Normal Law Protections |
• Load factor limitation
• Pitch attitude protection
• High AOA Protection
• Bank Angle protection
• High speed protection |
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Max. RWY elevation |
9200 ft |
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Outer tank fuel quantity |
Each tank 690 kg |
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A/C length wingspann height |
37,57 m
34,10 m
12,14 m |
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RCAM - Runway Condition Assessment Matrix Max. X-wind for T/O and Ldg. BA medium to poor |
10 kts |
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Inner fuel tank qty. |
5420 kg |
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All engines out significant remainig systems |
(Fly) PFD1, alternate law
(Navigate) RMP1, VOR1
(Communicate) VHF1, HF1, ATC1 |
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Max. brake temperature for T/O |
150°C - brake fan on
300°C - brake fan off |
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Max. Whiper speed |
230 kts |
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Max. tire speed |
195 kts |
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RCAM - Runway Condition Assessment Matrix Max. X-Wind for T/O and Ldg. BA good to medium |
20 kts |
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Main Ldg gear width |
7,59 m |
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RCAM - Runway Condition Assessment Matrix Max. X-wind for T/O and Ldg. BA good |
30 kts Gust 38 |
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CFM Engine
Normal idle parameters |
N1 - 19,5%
EGT - 390°C
N2 - 58,5%
FF - 275 kg/h
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Vmo / Mmo |
350 kts / .82 M
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Wake turbulence separation |
Medium behind Medium 5 NM
Medium behind Heavy 5 NM / 2 min. int.section T/O 3 min.
Medium behind Super 7 NM / 3 min. int. Setion T/O 4 min.
Heavy behind Heavy 4 NM
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Max. Brake Temperature for Parking |
500° C with Brake fan off
350° C with Beake fan on
Avoid applying parking brake
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Automatic Landing (CAT I/II/III)
Glide slope angle range |
-2.5° to -3.15° |
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Automatic Landing (CAT I/II/III)
Max. airport elevation |
2500 ft |
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Max. Ldg. parameters and asociated callouts |
"Pitch Pitch" at tailstrike pitchlimit indicator or 10° pitch
"Bank Bank" when reaching 7° |
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Max. Go Around parameters and asociated callouts |
"Bank" when greater 7°
"Pitch" when greater 20° or less than 10°
"Sink Rate" if there is no climbrate |
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Formula for max. Fuel difference after refueling |
1% Tank Capacity + 1% FOB (before uplift) + 0,45% Uplift |
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A320 Min Oil qty before engine start |
9.5 qts + 0.5 qts/FH |
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A319 Min oil qty before engine start |
11 qts + 0.3 qts/FH |
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A319 Starter Limitation |
- 3 consecutive cycles - each cycle max 2 min - 15 s between each cycle - 30 min cooling after 3 start attempts or 5 min of continous cranking - no starter engagement if N2>10% on ground or N2>18% in flight |
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A319 Max X-wind OEI or one Thrust Reverser inop. |
10 kt |
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RCAM - Runway Condition Assessment Matrix Max. X-wind for T/O and Ldg. Slush / Dry snow / Wet snow / Frost BA good |
25 kts |
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Formular for TAS effect at Flex Temp. Take Off |
Per 10° Temp. difference Flex - OAT: +3% ASD Flex - OAT = 35° -> 3.5 x 3° = 10.5% If e.g. ASD = 2000m -> 10.5% x 2000m = 210m TAS effect |
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