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330 limitations > deck_1247278 > Flashcards

deck_1247278 Flashcards

1
Q

What is the Center of Gravity referenced to?

A

CG position is given in percentage of the reference chord length (7.27m) aft of the leading edge (28.15 m aft of the aircraft nose)

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2
Q

Load acceleration limits ?

A

Clean configuration –1 g / + 2.5 g Other configuration 0 g / + 2 g

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3
Q

Maximum number of passenger seats ?

A

375 on B-HLL and older aircraft 440 on newer aircraft

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4
Q

Airport altitude and runway slope limitations ?

A

Runway slope. ±2 %Runway altitude. 12 500 ft

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5
Q

Crosswind limits ?

A
  • Take Off 32 kt (gust included) - Landing 40 kt (gust included)
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6
Q

Maximum wind for Passenger/Cargo door operation ?

A
  • Passenger door operation 40 kt (50 kt, if the nose of the aircraft is oriented into the wind)- Cargo door operation 40 kt (50 kt, if the nose of the aircraft is oriented into the wind, or the cargo door is on the leeward side)Passenger/Cargo doors must be closed before wind exceeds 60 kt.
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7
Q

On which Runway conditions it is not recommended to Take Off ?

A
  • Wet ice- Ice with Snow on top- Compacted Snow with Water on top
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8
Q

On which Runway conditions it is not recommended to Take Off ?

A

‐ Wet ice- Ice with Snow on top‐ Compacted Snow with Water on top

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9
Q

Maximum design maneuvering speed VA ?

A

VA is the maximum speed which permits full flight control deflection, it only applies in alternate or direct law:Above FL 280 VA is M 0.78Below FL 280 VA decreases from 305 kts at FL 280 to 250 kts at 0 ft

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10
Q

Maximum speed with Flaps / Slats extended ?

A

VFE 1 240 ktsVFE 1+F 215 ktsVFE 2 196 ktsVFE 3 186 ktsVFE Full 180 kts

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11
Q

Maximum speed to operate the Landing Gear and fly with the landing gear extended, normal operation ?

A

VLE, Flight with Gear Extended: 250 kt / M 0.55 VLO, Operation of Gear: 250 kt / M 0.55

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12
Q

Maximum tire speed ?

A

Ground speed of 204 kt

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13
Q

Maximum altitude to operate Flaps / Landing gear ?

A

Flaps: 20 000 ftLanding Gear: 21 000 ft

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14
Q

Maximum windshield wiper speed ?

A

230 kts

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15
Q

Maximum speed to open Cockpit windows ?

A

230 kts

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16
Q

Maximum pressure differential to allow the Ram inlet to open ?

A

1 PSI

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17
Q

Maximum pressure of air conditioning supply with LP ground units ?

A

2 ×1.6 kg/sec (2 × 3.53 lb/sec) using 2 ground carts

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18
Q

Maximum cabin differential pressure and safety valve settings ?

A

Max Positive/Negative: 9.25 /-1 PSISafety relief valve: 8.85 /-0.26 PSI

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19
Q

What are the minimum and maximum weight for use of autoland ?

A

Minimum: 123 000 kgMaximum: Demonstrated at Maximum Landing Weight, available up to 229 000 kg

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20
Q

Minimum height to use the autopilot on takeoff with SRS mode ?

A

100 ft AGLAn internal FMGES logic prevents the autopilot from engaging during the 5 s after liftoff

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21
Q

Minimum height to use the autopilot on approach ?

A

Straight-in non precision approach MDACircling approach MDA - 100 ftILS approach CAT1 160 ft AGLGo-around 100 ft AGLAll other phases 500 ft AGLAll above Ground Level and not Airport elevation

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22
Q

What RNP accuracy will FMGES provide with GPS Primary ?

A

NAV mode, AP ON :En route 1 NM / Terminal area 0.5 NM / Approach 0.3 NMNAV mode, AP OFF and FD ON :En route 1 NM / Terminal area 0.51 NM / Approach 0.3 NMHDG mode, AP OFF and FD OFF:En route 1,1 NM / Terminal area 0.51 NM / Approach Not authorized

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23
Q

What RNP accuracy will FMGES provide without GPS Primary ?

A

Without GPS Primary, Navigation accuracy is function of ground radio NAVAID infrastructure and elapsed time since the last radio update.

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24
Q

What is the lowest MDA to use FINAL APP mode ?

A

MDH/DH (barometric) 250 ft.

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25
Q

NAV/Final APP modes on NPA (VOR or NDB approach) what are the requirements on aircraft automation and Navaid availability ?

A

NPA may be performed in NAV or FINAL APP mode provided AP or FD is used and:- GPS PRIMARY: NAVAID/aircraft radio equipment can be inoperative- Without GPS PRIMARY: Accuracy is High and NAVAID serviceable tuned and monitored during the approach

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26
Q

What are the requirements to use NAV mode in the terminal area ?

A

NAV mode may be used in the terminal area, provided:‐ GPS PRIMARY is available, or‐ HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or‐ NAVAID raw data is monitored.

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27
Q

What is the minimum DH of an ILS CAT 2 ?

A

100 ft AGL

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28
Q

What is the minimum RVR for an ILS CAT 3 FAIL OPERATIONAL

A

75 m

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29
Q

What are the AP and A/THR Requirements for CAT 2 and CAT 3 approaches ?

A
  • CAT 2: 1 AP engaged in APPR mode and CAT 2 or higher capability displayed on the FMA.- CAT 3 FAIL PASSIVE: A/THR in selected or managed speed + 1 AP engaged in APPR mode and CAT 3 SINGLE or higher capability displayed on the FMA.- CAT 3 FAIL OPERATIONAL: A/THR in selected or managed speed + 2 AP engaged in APPR mode and CAT 3 DUAL displayed on the FMA.
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30
Q

What Flap setting can be used in CAT 2, CAT 3 approach with one engine out ?

A

CAT 2 and CAT 3 fail passive autoland with 1 engine out are only approved in Configuration 3. Procedures must be completed before 1 000 ft in approach

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31
Q

What are the maximum wind conditions for CAT 2 / CAT 3 approach or CAT 1 Automatic Landing and Roll Out ?

A

Tailwind: 10 ktCrosswind: 20 ktHeadwind: 35 ktWind limitation is based on surface wind reported by the tower.If wind is beyond limitations, a CAT 1 Automatic Approach without autoland can be performed.

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32
Q

AutolandWhat are the ILS G/S angle and airport, runway condition limitations ?

A

Autoland has been demonstrated on:- G/S angle between -2.5° and - 3.25°- Airfield elevation lower than 9 200 ft- Dry and wet runways (no contamination)

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33
Q

What is the minimum fuel temperatures values?

A

Inner tank, the highest of . Fuel Freezing point . -44 °C below 30 000 ft / -54 °C above 30 000 ftOuter and Trim tank, Fuel Freezing point Jet A1 Freezing point is -47 °C

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34
Q

What is the minimum fuel quantity for take off ?

A

5200 KG WING TK LO LVL warning must not be displayed on ECAM.

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35
Q

What is the maximum brake temperature for take off ?

A

Maximum brake temperature for takeoff (brake fans off): 300 °C

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36
Q

Can you taxi with damaged tires ?

A

No, If tire damage is suspected after landing, or after a rejected takeoff, inspection of the tires is required before taxi.

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37
Q

Can you use the ISIS bugs when you’ve lost both PFD ?

A

No, when both PFDs are lost, ISIS bugs function must not be used.

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38
Q

For what conditions the EGPWS enhanced functions should be inhibited (TERR pushbutton to OFF, on the GPWS panel) when the aircraft position is less than 15 nm from an airfield?

A
  • Runways not incorporated in EGPWS database- Approach procedures have previously been identified as potentially producing false terrain alerts
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39
Q

What are the limitations to taxi with one or more deflated tires ?

A
  • 1 tire deflated per gear (3 tires max total): Speed limited to 7 kt in turns.- 2 tires deflated on same main gear (tires not deflated on other one):Speed limited to 3 kt in turns and nose-wheel steering angle 30° max.
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40
Q

Can you start and operate an APU with the LOW OIL LEVEL ECAM advisory displayed ?

A

Yes, the APU may be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed.Maintenance action is required within next 15 h of APU operation.

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41
Q

What is the APU starter limitation ?

A

3 consecutive start attempts followed by a60 min cooling interval before the next start.

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42
Q

What is the maximum rotor speed of the APU ?

A

N= 107%

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43
Q

What is the maximum EGT of the APU during operation and for start ?

A

Maximum EGT:APU running: 650 °C APU start: 1250 °C

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44
Q

Up to what altitude can the APU supply both bleed air and Electrical power ?

A

22 500 ft with 1 pack, 17 500 ft with 2 packsAbove that altitude the APU can only provide electrical power

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45
Q

What does the minimum O2 bottle pressure covers ?

A
  • Preflight checks - Oxygen use with 1 pilot only in the cockpit- Unusable quantity- System leakage- Protection following a loss of pressure (regulator on NORMAL): ▪ Emergency descent, all crewmembers and observers for 15’ ▪ Cruise at FL 100, 2 crewmembers for 105’- Protection against smoke (regulator 100 %) for all crewmembers and observers during 15’ at 8 000 ft cabin altitude.
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46
Q

What are the minimum and maximum oil temperatures ?

A

Min Temp prior to takeoff 20°CMax Temp 190°C

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47
Q

What are the engines EGT limits ?

A

Start:On ground 700°CIn Flight 850°CMCT: 850 °CTAKE OFF:900°C for 5 mins both engines 900°C for 10 mins 1 Engine out920°C for 20s

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48
Q

What are the engines starter limitations ?

A

1 maximum continuous operation of 5 min or2 cycles of 3 min and a consecutive cycle of 1 min (run down to 0 N3 between each cycle)After 1 continuous operation, or the 3 cycles wait 30 min to allow the starter to cool.No running engagement of the starter (N3 above 10 % on ground, or 30 % in flight).

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49
Q

What is the minimum Engine oil pressure ?

A

25 PSI

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50
Q

What are the maximum RPM for N1, N2 and N3 ?

A

N1max………………………………………………….99 %N2 max…………………………………………….103.3 % N3 max……………………………………………….100 %

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51
Q

What is the minimum oil quantity ?

A

Before pushback, minimum oil quantity is 6qt+0.7qt/h with a minimum of 15qt

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52
Q

Can you use Wing anti ice on APU Bleed air ?

A

APU air bleed extraction for wing anti-ice is not permitted.

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53
Q

What is the maximum tailwind to operate at an airport ?

A

Maximum tailwind at or below 11 000 ft 15 kt Maximum tailwind above 11 000 ft 10 kt Maximum tailwind for automatic landing and rollout is 10 kt

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54
Q

what is the minimum weight to operate an A330 ?

A

121 000 kgExcept for LG, LI, LL and YB where it is 125 000 kg

55
Q

What is the Cabin pressure safety relief valve setting ?

A

-0.26 PSI / 8.85 PSI

56
Q

What is the altitude tolerance on Standby altimeter during the instruments check ?

A

+/- 300 ft

57
Q

What is the altitude tolerance between PFD altimeters and airport altitude during the instruments check ?

A

PFD 1 or PFD 2 at ground check : plus or minus 25 ft

58
Q

Can you open a cockpit window with the packs ON ?

A

No, It is not possible to open the cockpit windows, with the packs ON.

59
Q

What is the maximum taxi weight ?

A

205 900 kg

60
Q

What is maximum zero fuel weight ?

A

173 000 kg

61
Q

What restrictions apply to the use of reduced thrust ?

A
  • Meet performance requirements at planned takeoff weight with the thrust available at the assumed temperature. - maximum thrust reduction of 25 % from full rated takeoff thrust, Max flex temperature is ISA + 48 °C - Assumed temperature must not be lower than flat rating temperature, or actual OAT- Takeoff at reduced thrust is not permitted if:. Contaminated runways. Inoperative item affecting performance, unless the aircraft can meet performance requirements with the operating engines at the thrust available for the flex temperature.
62
Q

Can you land with fuel imbalance outside of the authorised asymmetry ?

A

Yes, in exceptional conditions (i.e fuel systems failure)

63
Q

What is maximum engine N3 Max ?

A

100 %

64
Q

Can the APU be started and operated if LOW OIL LEVEL on ECAM ?

A

Yes

65
Q

What is maximum altitude for gear extension ?

A

21 000 ft

66
Q

What is VLO ?

A

250 kts / .55

67
Q

Pressurization, the maximum negative differential pressure is?

A
  • 1 psi
68
Q

APU maximum altitude for Elec Power in flight ?

A

41 450 ft

69
Q

Minimum auto pilot disengage height during automatic approach without auto land ?

A

80 ft AGL

70
Q

APU maximum altitude for both Bleed Air (1 Pack) and Gen Load in flight ?

A

22 500 ft

71
Q

What is maximum certified crosswind for take off (gust included) ?

A

32 kts

72
Q

What is hydraulic normal operating pressure ?

A

3000 psi +/- 200

73
Q

Is APU air bleed extraction for wing anti ice permitted ?

A

No

74
Q

What is maximum landing weight ?

A

185 000 kg

75
Q

What is maximum engine N2 Max ?

A

103.3 %

76
Q

What is minimum height for autopilot on a go around ?

A

100 ft AGL

77
Q

What is maximum take off weight (brake release) ?

A

205 000 kg

78
Q

What is the maximum fuel temperature for JET A and JET A1 fuel ?

A

+55° c

79
Q

What is maximum engine N1 Max ?

A

99 %

80
Q

What is maximum wind for passenger door operation ?

A

40 kts or 50 kts if nose is into wind

81
Q

What is the maximum number of deflated tyres you can taxi with ?

A

3 tyres

82
Q

Nose wheel steering angle is limited to ___ ° and for towing or pushback is limited to ___ ° ?

A

72 ° / 65 °

83
Q

What is maximum wind for cargo door operation ?

A

40 kts or 50 kts if nose is into wind or cargo door on leeward side

84
Q

Alert height for Cat III approach ?

A

200 ft

85
Q

T Max Flex is ?

A

ISA + 48°

86
Q

Thrust reduction must not exceed ____ % of full take off thrust ?

A

25 %

87
Q

The APU can be consecutively started ____ times (without cool down), before a cooling down period of ____ mins is required ?

A

3 / 60 mins

88
Q

What is the maximum altitude for APU start ?

A

In Flight Start:- Normal configuration: 41 450 ft - Emergency Electrical configuration (APU bat only): 25 000 ftGround Start: 14 600 ft

89
Q

What is VLE ?

A

250 kts / .55

90
Q

Auto land wind limits are ?

A

Head Wind 35 kts / X-Wind 20 kts / Tail Wind 10 kts

91
Q

What are the restrictions on overwing fuelling ?

A

It is prohibited with passengers on board.

92
Q

The passenger / cargo door must be closed before the wind speed exceeds ?

A

60 kts

93
Q

What is maximum demonstrated crosswind for landing (gust included) ?

A

40 kts

94
Q

What is the maximum altitude difference between instruments on the ground ?

A

ALTITUDE TOLERANCES :‐ PFD 1 or PFD 2: plus or minus 25 ft / airport elevation- ADR1 / ADR2 / ADR3 on PFD : 20 ft- ISIS / ADRs : 60 ft‐ STBY ALTI: plus or minus 300 ft / airport elevationOn the ground, the vibrator is off, that is why the standby altimeter tolerance value is high. In flight, the vibrator is on and the value is lower.

95
Q

What is the maximum altitude for APU assisted Engine Start in flight ?

A

20 000 ft

96
Q

What is the maximum allowable wing fuel imbalance in inner tanks (outer tanks balanced), with heavier tank full, half full and 7500 kg left ?

A

2900 / 4800 / 7500 kgs

97
Q

What is maximum speed for gravity extension ?

A

200 kts

98
Q

Can you do LWMO and Autoland with 1 engine inoperative ?

A

Yes, Cat 2 and Cat 3 Single procedures are approved in conf 3 with 1 engine inoperative.

99
Q

What is the maximum engine EGT for Take off ?

A

920°

100
Q

If 2 tyres are deflated on same main gear (the other main gear tyres not being deflated) the speed should be limited to __ kts and nose wheel steering angle should be limited to ___ ° ?

A

3 kts / 30 °

101
Q

Maximum engine EGT of ___ °c is permitted up to ____ mins, in the case of engine failure ?

A

900°c / 10 mins

102
Q

Can you take off with WING TK LO LVL on ECAM ?

A

No, Take off not permitted

103
Q

What is VFE Config 3 ?

A

186 kts

104
Q

What is minimum weight for autoland ?

A

123 000 kgs

105
Q

What is maximum normal cabin altitude ?

A

8000 ft

106
Q

If 1 tyre is deflated on one or more gears (i.e. a maximum of three tyres) the speed should be limited to what speed during turns ?

A

7 kts

107
Q

What’s the maximum wind for landing?

A

55kts, Landings should not be made at airports where frequent gusts of 55 kt or greater are experienced. This reduces the potential damage to aircraft by wind-blown ground equipment.

108
Q

During Cold Soak procedure, no GPU available what should you do ?

A

Remove APU battery and store in warm place.

109
Q

In order to prevent inadvertent fuel aft transfer, in the case of a trim tank forward transfer pump failure, do not select the trim tank forward when the pitch attitude is above ?

A

3 °

110
Q

What is the maximum airport mean runway slope for a 330 ?

A

+/- 2 %

111
Q

At Take Off, SRS commands a maximum pitch of ____ ° increased at ____ ° in wind shear conditions?

A

17.5° / 22.5°

112
Q

Pressurization , the maximum positive differential pressure is ?

A

9.25 PSI

113
Q

The minimum flight crew oxygen pressure table can be found in…

A

FCOM LIM-35

114
Q

Can fuel types be mixed?

A

Yes.Determine the new minimum fuel temperature from FCOM LIM-28.

115
Q

What’s the Max steering angle taxiing with deflated tires?

A

30°

116
Q

After 3 APU start attempts without cooling down…

A

A 60 minute cooling period must be observed before the next start attempt.

117
Q

Maximum altitude for starting APU using APU battery only?(ELEC EMG CONFIG)

A

FL250

118
Q

If the first APU start attempt fails,what may help the second APU start attempt?

A

Wait 3 minutes after pushing the APU MASTER SW, before selecting APU START.

119
Q

Do not re-engage the engine starter unless the N3 is less than…

A

30% in flight10% on the ground

120
Q

Maximum continuous Engine starter operation ?

A

5 minutesFollowed by a 30 minute cool-down period.

121
Q

The assumed temperature at take-off (FLEX) must not be less than…

A

OATorThe flat rated temperature of the Engines

122
Q

Maximum speed in Config 2* ?(Transit to config 2)

A

205 KIAS

123
Q

Minimum TAT for the environmental envelope?

A

-53°C

124
Q

What is the minimum height for use of the autopilot on ILS approach with Cat2/3 not displayed?

A

160 ft AGL (not AAL)

125
Q

Internal FMGES logic prevents the autopilot from being engaged during ….

A

The first 5s after lift off

126
Q

Cat III Single Minimum Decision Height

A

50 ft AGL

127
Q

What is the minimum height for use of the autopilot during other phases than approach or departure?

A

500 ft AGL

128
Q

Minimum Decision Height for Cat II approach ?

A

100 ft AGL

129
Q

What is the maximum allowable wing fuel imbalance in outer tanks (inner tanks balanced), with heavier tank full, 2400 kg and 1730 kg left ?

A

1480 / 1580 / 1730 kgs

130
Q

Cat III Dual minimum RVR?

A

75m

131
Q

What is the maximum wind conditions for a Cat II approach and manual landing ?

A

Headwind 35Crosswind 20Tailwind 10

132
Q

What are the minimum and maximum OATs for take-off and landing?

A

-54°c to +55°c

133
Q

What is the maximum fuel temperature value ?

A

Maximum fuel temperature : JET A, JET A1, JP 5, JP 8, N°3 JET, RT, and TS-1: +55 °CJP 4, JET B : +49 °C

134
Q

Maximum speed for Landing Gear Gravity extension ?

A

VLE and VLO 200 ktIt’s because the doors stay open after extension

330 limitations (1 decks)

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