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Line Check 23 > Limitations > Flashcards

Limitations Flashcards

1
Q

Manoeuvering load factor limits - Clean

A

+2.5
-1.0

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2
Q

Manoeuvering load factor limits - Flap extended

A

+2.0
-0.0

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3
Q

Ramp 200

A

16556kg

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4
Q

Ramp 300

A

19595

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5
Q

Brakes Release Weight 200

A

16466kg

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6
Q

Brakes Release Weight 300

A

19505kg

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7
Q

Landing Weight 200

A

15650kg

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8
Q

Landing Weight 300

A

19051kg

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9
Q

Zero Fuel Weight 200

A

14696kg

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10
Q

Zero Fuel Weight 300

A

17917kg

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11
Q

Crosswind/Tailwind limit - Hard Runway

A

36/10

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12
Q

Crosswind/Tailwind limit - Compacted, Standng Water, Slush, Loose Snow

A

14 - Nil

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13
Q

Crosswind/Tailwind limit - Compacted Snow

A

20 - nil

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14
Q

Crosswind/Tailwind limit - Narrow Runway

A

20 - 10

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15
Q

Narrow Runway definition

A

14 - less than 30m

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16
Q

Narrow taxiway definition

A

15 - 18m

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17
Q

Maximum Engine Operating Ambient

A

48.9 or ISA +35 whichever is lower

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18
Q

Minimum Engine Operating Temperature

A

-54

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19
Q

Maximum Airstart Altitude

A

20,000ft

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20
Q

Automatic uptrim

A

10% Nominal

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21
Q

Max takeoff (MTOP) 200 Torque/ITT

A

111 / 800

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22
Q

Max takeoff (MTOP) 300 Torque/ITT

A

105.6 / 800

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23
Q

NTOP 200

A

99.5 or 97.5 (in flight) / 770 - Per graph

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24
Q

NTOP 300

A

92 or 90 (in flight) / 765 - Per graph

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25
Q

MCP 200

A

97.5 (1212) - 800
114.2 (1024 or less)

26
Q

MCP 300

A

90 (1212) - 800
96 (1125 or less)

27
Q

Starting ITT Limits

A

Transient 800 - 840 (20 Seconds)
840-900 (12 seconds)
900-950 (5 seconds)

28
Q

Transient 200

A

125 - 840

29
Q

Transient 300

A

115 - 840

30
Q

Transient Prop

A

1320

31
Q

Prop limit normal

A

1212

32
Q

Prop Transient Limit

A

1320

33
Q

Oil Pressure Normal

A

55 - 65

34
Q

Oil Pressure Transient / Starting

A

200 Max

35
Q

Oil Temp Normal

A

45 - 115

36
Q

Oil Temp Min - Starting

A

-40

37
Q

Oil Temp Max - Transient

A

125

38
Q

Min Idle NH

A

66%

39
Q

MTOP Time Limit

A

5 min

40
Q

Transient time Limits

A

5 min

41
Q

Oil Pressure Limit NH below 75%

A

40 - 55

42
Q

Minimum Prop Unfeather Oil Temp

A

0

43
Q

Max Torque on Ground

A

97.5% - 200
92.5% - 300

44
Q

Max Torque on Ground (Prop Feathered)

A

50% - 200
48% - 300

45
Q

Minimum NH on Ground

A

66%

46
Q

Propeller Prohibited Range

A

500 - 780

47
Q

Starter Cranking Limits

A

1 on 2 off
1 on 2 off
1 on 30 off

48
Q

Ice Definition

A

SAT 10 or below on the ground
SAT 5 or below inflight
and visible moisture is present in any form - 2km or less vis

49
Q

AFCS Limitations

A

Category 1 operations only.
During autopilot operation, the pilot flying must be seated at the controls with safety and shoulder harness fastened.
Autopilot must not be manually overpowered.
Autopilot & Flight Director only approaches are approved for glideslope angles of 2.5° - 4°.
Glideslope angles greater than 3.0° are approved for approach flap 15 only.
Autopilot must be disengaged at or above 200 ft. above runway
An autopilot approach must not be commenced or continued with an inoperative engine.
NOTE
(autopilot must be disengaged at or above 1,000)
ft AGL.
Glideslope (GS) flight director mode coupled with the autopilot is not permitted with:
Flap 35
Flap 5 below 1,500 ft AGL (300 Series Only)
Flap 0 below 500 ft AGL (300 Series Only)
Use of VOR without associated DME is not permitted in NAV and APP mode.
Autopilot backcourse approaches are not permitted.
After takeoff or go-around, the minimum height for autopilot engagement is 1000 feet AGL.
Autopilot must be disengaged in severe icing conditions.
Permissible use of the autopilot after a partial flight control failure is determined by QRH checklist.
Where a partial flight control failure occurs and the QRH checklist provides no autopilot advisory, re-engagement of the autopilot is permitted.

50
Q

What is the preference between electronic and visual slope
guidance?

A

When operating onto runways with both electronic and visual slope guidance, preference should be given to using the electronic slope guidance unless it is deemed to not enhance approach stability or is detrimental to safety.

51
Q

To what point do we follow the GS on an ILS approach?

A

When an ILS is selected to provide slope guidance, the glideslope indications must be followed until the published decision altitude is reached to avoid EGPWS glideslope warnings.

52
Q

What are some of the considerations in transitioning from
electronic to visual slope guidance?

A

Height over the threshold
Visual and electronic differences in indication

53
Q

What are the additional requirements for an APV BARO VNAV over
a standard RNP approach?

A

Flight director must be used;
Two altimeters must be operational and monitored;
Local QNH and temperature must be used;
Local temperature must be within the charted limits; and
EGPWS terrain alerting functions must be operative.

54
Q

What is the tolerance on the final approach segment?

A

+ or – 75ft

55
Q

When is a missed approach required in relation to the 75ft
tolerance?

A

A missed approach must be conducted if the vertical deviation after the FAF exceeds 75ft (momentary deviations above path are acceptable).

56
Q

What would trigger a ‘slope’ advisory call on the final approach
segment?

A

2D Approach: ± 1 dot vertical deviation 1
APV Baro-VNAV: ± ½ dot vertical deviation

57
Q

CTAF - Traffic separation plans – 10:10:1

A

10 Minutes
10NM
1000ft
If any of these it is likely a threat – determine the area of conflict – Develop a positive separation plan

58
Q

CTAF - Conformance with runway traffic directions.

A
59
Q

CTAF - How do we determine the active runway?

A
60
Q

CTAF - What are the risks with arriving or departing on the
opposite runway or with a tailwind?
Should we do it, and what, if any, mitigators can be
used?

A
61
Q

CTAF - How can we build SA as a crew?

A
62
Q

Taxi Speeds Normal/Narrow

A

25/15
15/10

Line Check 23 (1 decks)

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