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72-600 > Limitations > Flashcards

Limitations Flashcards

1
Q

Length and width …

A

27m x 27m

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2
Q

Flaps position …

A

0, 15, 30

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3
Q

FLAPS UNLK

A

4 deg

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4
Q

VMO clacker operates when VFE exceeds …

A
  • 15 deg - 185 kt

- 30 deg - 150 kt

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5
Q

Max fuel quantity

A

5000 kg

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6
Q

Max fuel quantity per wing

A

2500 kg

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7
Q

Electric pump off and on, when ?

A

over 8.5 PSI - off

under 5 PSI - on

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8
Q

Fuel LO LVL …

A

160 kg

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9
Q

HYD normal level …

A

9.35 L / max 9.6 L - min 8.5 L

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10
Q

HYD low level …

A

under 2.5 L

!!! In case of LO LEVEL alert the cross feed valve is inhibited or closes automatically if it was open !!!

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11
Q

HYD level for each system (blue/green)

A

4 L

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12
Q

Take off rating

A

2475 SHP

!!! 0.9 x max take off rating !!!

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13
Q

Reserve take off rating (RTO)

A

2750 SHP

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14
Q

Blade angle operating range

A
  • 14 deg (reverse) and + 78.5 deg (feather
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15
Q

Power corresponding to the mode selected (PWR MGT)

A 
TO = 2475 SHP
MCT = 2500 SHP
RTO = 2750 SHP
CLB = 2192 SHP
CRZ = 2132 SHP
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16
Q

PAX

A

72

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17
Q

Weight

A 
RAMP = 23170 KG
TAKE-OFF = 23000 KG
LANDING = 22350 KG
ZFW = 21000 KG
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18
Q

VMO/MMO

A

250 KT/ 0.55M

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19
Q

VA

A

175 KT

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20
Q

VFE

A

15 deg - 185 KT

30 deg - 150 KT

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21
Q

VLE

A

VLO - 185 KT
VLO RET - 160 KT
VLO LOW - 170 KT

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22
Q

VRA

A

180 KT

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23
Q

VWO

A

160 KT

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24
Q

Max tyre speed

A

165 KT GS

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25
Q

RTO TQ

A

100%

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26
Q

TO TQ

A

90%

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27
Q

MCT TQ

A

90.9%

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28
Q

Max fuel unbalance

A

730 kg

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29
Q

Max speed CRZ

A

275 kt

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30
Q

Trim green band

A

+2.5 to 0

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31
Q

Refueling

A

LG bay, right side

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32
Q

Brakes

A

Carbon

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33
Q

Wind limitations …

A

15 kt tail, 30 kt cross (ops)

15 kt / 30 kt (AFM)

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34
Q

Wind limitations (LVO) landing

A

10 kt tail/ 17 kt cross/ 29 kt head

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35
Q

ATPCS conditions

A
  • PWR MGT TO
  • PL > 49 deg
  • TQ > 46%
  • ATPCS pb ON
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36
Q

Climb speed

A

170 kt

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37
Q

TQ =…

A

P/NP

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38
Q

ATPCS triggering condition

A

One TQ under 18%

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39
Q

Fuel tank temperature. Where is the probe located?

A

Left feeder tank

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40
Q

TLU

A

180/185kt

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41
Q

High speed climb speed

A

190kt

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42
Q

GND HNDLG BUS is disconnected when …

A

Airborne

43
Q

DC UNDV

A

STBY BUS under 19.5V

44
Q

BAT OVRD toggle switch

A

Overrides all protection, ensuring the busses are supplied from their respective battery

45
Q

OVRD P/B

A

Transfers DC STBY BUS and AC STBY BUS from HOT MAIN BAT BUS to HOT EMER BAT BUS

46
Q

O2 PAX supply on. How many PAX

A

25%

47
Q

If cockpit O2 bottle is under …PSI use table

A

1400 PSI

48
Q

PITCH TRIM ASYM

A

Pitch tabs desynchronization greater than 0.7 deg

49
Q

VAPP = …

A

VREF + wind factor

Wind factor = 1/3 headwind or the gust in full (maximum 15 KT)

50
Q

Which are the only doors monitored through the MFC?

A

FWD COMPT, CARGO and EMER

51
Q

NAV lights coverage

A

Wings 110 deg, tail 140 deg

52
Q

EMER EXIT LIGHTS…

A
  • ON when DC STBY BUS under 18v or both generators lost

- OFF when DC STBY BUS above 20v and at least one generator is running

53
Q

The packs supply…

A

Lef pack - cabin and cockpit
Right pack - cabin only
! If one pack is inoperative, the other one supplies both compartments through the mixing chamber !

54
Q

Landing elevation on AUTO PRESS is

A

-1500ft to 10000ft

55
Q

AUTO PRESS DESCENT RATE…

A

Normal - 400ft/min

Fast - 500ft/min

56
Q

Batteries

A

Main Ni-Cd 24V and 43Ah

Emer Ni-Cd 24V and 15Ah

57
Q

O2 cylinder capacity…

A

2182 l

58
Q

Complete refueling in about…

A

16 min

59
Q

RMI

A

CAPT - DC BUS 2

FO - DC STBY BUS

60
Q

The LP VALVE is controlled by the associated….

A

Fire handle

61
Q

ICING AOA LT illuminates as soon as …

A

One horn is activated

62
Q

Wipers speed …

A
  • slow 80/min

- fast 130/min

63
Q

Exciters

A
  • 2, A and B for each engine powered by the DC ESS BUS

- each has two spark igniters (first 25s 5-6 sparks/s, then 1 spark/s)

64
Q

Maximum runway slope and minimum width

A
  • +/-2 deg

- 30 m

65
Q

In ICING conditions NP must not go below…

A

82 %

66
Q

Starter limitations

A

3 starts in 1min and 30 sec, total combined time, followed by 4 min off

67
Q

Maximum value for TQ, time limit and when …

A

120%, for 20s, in transient

68
Q

BRK TEMP

A

150 deg

69
Q

NAC OVHT

A

Over 170 deg

70
Q

DUMP function is only available in …

A

AUTO MODE

71
Q

Temperature limitations …

A
  • 715 Hotel Mode ENG 2
  • 765 Take Off (5 MIN)
  • 800 MCT, RTO (10 MIN) - UPTRIM CONDITION
  • 800 - 840 (MAX 20 SEC)
  • 840 - 950 (START, MAX 5 SEC)
72
Q

When putting the battery sw ON, MFC 1A and 2A will flash if ….

A

The cargo door is closed, otherwise, only MFC 1B and 2B will flash

73
Q

Gust lock on when speed is ….

A

40KT

74
Q

Engine fire handle pulled, activates the following:

A
  • propeller on feather
  • fuel: LP valve closed
  • air: BLEED and HP VALVE closed
  • electric: DC and ACW GEN OFF
  • deice: deice and shut off valve closed
  • SQUIBS armed, light illuminates
    + HUD PROP BRAKE closed on ENG NO 2
75
Q

PROP BREAK READY light conditions:

A
  • A/C on ground
  • fire handle not pulled
  • gust lock engaged
  • CL on FTR or FUEL S/O
  • BLUE HYD pressure over 2100 PSI
76
Q

“DISCHARGE” will light up when …

A

The fire extinguisher bottle is empty

77
Q

The fire is considered extinguished when

A

The FIRE HANDLE turns off

78
Q

“SQUIB” appears and are armed when …

A

The FIRE HANDLE is pulled

79
Q

DRIFT DOWN procedure, in case of SE OPS …

A
  • descend till the SE GROSS CEILING (normal or icing conditions)
  • OBSTACLE: descend with white bug + flaps 15 deg
  • NO OBSTACLE: descend with 200 kt until we reach a VS of 500 FT/MIN and stop the descent at approximately FL 80
80
Q

Use of a weak GPU

A

If we have a voltage under 28 V we verify if it’s above 26 V. If it’s not above 26 V, we must SHED the consumers, if it’s still under 26 V, we remove the GPU and start the engine on BATTERIES.

81
Q

GREEN HYD FAULT “LO PR”

A
  • LG
  • normal braking
  • after take off, T/O INHI won’t cancel by itself, we must press RCL pushbutton
82
Q

RAPID and EXPLOSIVE DECOMPRESSION descent speeds:

A
  • RAPID: VMO - 10 kt

- EXPLOSIVE: our current speed

83
Q

Emergency battery duration …

A

30 min

84
Q

AUX HYD PUMP activation

A
  • one engine running
  • PROP BRAKE OFF
  • BLUE HYD SYSTEM pressure under 1500 PSI
  • LDG down
85
Q

VLO (185 kt/ 180 kt) is larger than V retraction (160 kt) and V lowering (170 kt) because …

A

After the LDG is down, the doors will close, which means we can fly at a higher speed compared to V retraction and V lowering

86
Q

The buttons on the overhead panel that have a yellow contour are used in case of ….

A

SMOKE

87
Q

PROP DE-ICE, mode of operation …

A

The blades are heated in sequence:
- 1-3-5
- 2-4-6
!!! “FAULT” sign will alternate ON and OFF only if one of the series doesn’t work, if “FAULT” stays ON it means that the heating isn’t working on any of the blades !!!

88
Q

TCAS RA …

A
  • CLIMB: MCT, CL 100% OVRD

- RADIO: “TCAS RA” and when it’s the case, “CLEAR OF CONFLICT”

89
Q

APM

  • “CRUISE SPEED”
  • “DEGRADED PERFORMANCE”
  • “INCREASE SPEED”
A
  • No action
  • Checklist
  • Severe icing
90
Q

Minimum height for AP engagement after take off is …

A

100 FT

91
Q

Minimum height for use of either AP or FD:

  • except during take off or executing an approach …
  • VS or IAS mode during approach …
  • CAT I approach …
  • CAT II approach …
A
  • 1000 FT
  • 160 FT
  • 160 FT
  • 80 FT
92
Q

Avoid PROP BRAKE immobilization when the temperature is below … for a prolonged period of time.

A
  • 20 deg
93
Q

Avoid PARKING BRAKE engagement in wet conditions, when the temperature is below …

A
  • 5 deg
94
Q

Maximum fuel unbalance during single engine operation is …

A

200 kg

95
Q

EXCESSIVE ITT DURING STARTALERTA hot start may be recognized by :

A
    • Rapid ITT increase,
    • NH slow increase,
    • Exhaust flames may be reported by ground crew.
96
Q

An engine flame out may be recognized by:

A
    • sudden dissymmetry
    • TQ decrease
    • rapid ITT decrease
97
Q

ENG OIL LO PR ALERT

A

Oil pressure drops below 40 PSI

98
Q

Some alerts are not processed by the MFCs, they are processed locally. These systems are …

A
  • ENG FIRE
  • EXCESS CABIN DIFFERENTIAL PRESSURE
  • EXCESS CABIN ALTITUDE
  • NACELLE OVERHEAT (2)
  • SMOKE
99
Q

TAT/SAT information are valid only when …

A

the engine (propeller unfeathered) corresponding to the selected ADC is running.

100
Q

A standing takeoff shall be performed under any of the following conditions:

A
  • TOW is near limiting RTOW for RWY length or obstacle;
  • Visibility / RVR at or close to takeoff minimum;
  • Contaminated RWY.
    The aircraft must be lined up and brought to a stop. Before releasing the brakes, the engines must be accelerated by setting the PL’s just above FI detent.
101
Q

PROP BRAKE unlock/ lock time …

A
  • 5 sec. to unlock

- 10 sec. to lock

102
Q

GND HDLG BUS is active and the battery discharges, even if it’s not selected on, when …

A
  • Cargo control panel door is open
  • Refueling door is open
  • Passenger door is open
103
Q

Vmcl …

A

98 kt

72-600 (17 decks)

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