Limitations Flashcards

1
Q

What operations is aircraft certified for?

A

Day and Night VFR
IFR
Icing Conditions (note - severe icing may result from environmental conditions outside of those for which the airplane was certificated)
Unpaved Runway Operations

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2
Q

Maximum number of passenger seats

A

Refer to Weight and Balance manual

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3
Q

Minimum Flight Crew

A

Captain and First Officer

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4
Q

Minimum Cabin Crew

A

Two for passenger carrying operations

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5
Q

Maximum Weights
Ramp Weight (almost evil)
Brakes Release Wt /Take Off Wt (on the floor)
Landing Weight (easy as 123 - 1t)
Zero Fuel Weight (26yo with a 308)

A

RW : 29,665kg
BRW / TOW : 29,574kg
LDW : 28,123kg
ZFW : 26,308

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6
Q

MAC certified limits are?
up to 24,020kg
up to 27,987kg
up to 28,998kg
up to 29,257kg
up to 29,574kg

A

13.8% - 36%
16.6% - 36%
17.3% - 36%
17.4% - 36%
17.7% - 36%

(safe bet is 17.3 - 36%)

Note - If CoG limits are met with LDG gear down, safe limits of flight are automatically achieved

Note - The maximum aft limit is 20%MAC for operations with one inoperative stall warning and / or stick pusher system.

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7
Q

Vmcg
Flaps 15, 10, 5, 0

A

89, 89, 89, 101 KCAS

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8
Q

Vmca
Flaps 15, 10, 5, 0

A

91, 95, 98, 113 KCAS

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9
Q

Vmcl
Flaps 35, 15, 10, 5,

A

92, 96, 99, 100 KCAS

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10
Q

Vmo
8, 10, 18, 20, 25,000*

A

245, 282, 286, 275, 248 KIAS

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11
Q

Vfe
5, 10, 15, 35

A

200, 181, 172, 158 KIAS

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12
Q

Vlo, Vle, Alternate

A

200, 215, 185 KIAS

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13
Q

Vb - Turbulence penetration

Vmax tire

A

210 KIAS

182 knots ground speed

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14
Q

Va

A

204 KIAS

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15
Q

Vaquaplaning - T/O
Vaquaplaning - LDG

A

107 kts G/S
92 kts G/S

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16
Q

Manoueuvering Limit Load Factors
Flaps Retracted
Flaps Extended

A

+2.5 / -1.0g
+2.0 / 0.0g

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17
Q

Max Crosswind - T/O, LDG, CAT II Landing Coupled
Dry / Wet
WED 3mm <0.125in contaminated
WED 3mm >0.125in contaminated
Compacted Snow
Wet ice, poor braking action

A

32kt Dry and wet for T/O and LDG
18kt Dry and Wet for CAT II Landing coupled

14kt for both WED 3mm for T/O, LDG and Coupled

20kt T/O and LDG for Compacted Snow
18kt Compacted Snow for Coupled

0kt for all on Wet Ice with poor braking action

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18
Q

Maximum Tailwind - T/O, LDG, CAT II, Steep Approach
Dry / Wet
Contaminated
Ice and Wet Ice Braking action poor

A

T/O Flap 5, 10, 15 on wet / dry / contaminated = 10kt
LDG Flap 10, 15, 35, CAT II on wet / dry / contaminated = 10kt
T/O & LDG, CAT II and Steep approach on Ice and wet ice braking action poor = 0kt
Steep APPR Landing (Flap 35) - Dry / Wet / Contaminated - 5kt

(Note - limits may be increased when AFM supplement 3 is applicable)

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19
Q

Maximum headwind for CAT II coupled landing

A

CAT II coupled - 24kt

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20
Q

Minimum and Maximum temperatures

A

MAX - +50c or ISA + 35c
MIN - -54*c

(Note cold weather procedures apply after 3hrs in -15*c or lower on ground)

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21
Q

Take off power setting limitation (wind)

A

Setting take-off power prior to brake release, with nose of the airplane more than 45* out of wind, is prohibited for wind speeds greater than 8kt (measured at a 10m height)

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22
Q

Maximum operating altitude &

for T/O and LDG

A

FL 250

10,000’

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23
Q

Maximum slope for T/O and LDG

A

+/-2%

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24
Q

Maximum glide slope angle for CAT II approaches

A

< 3.25*

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25
Q

Eye / ILS to Wheel path distances.

A

3*
Flap 10 4.662 / 4.446m
Flap 15 4.339 / 3.927m
Flap 35 3.928 / 3.273m
4.5*
Flap 35 3.934 / 3.278m

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26
Q

Limitations for operations on contaminated runways

A

Take off with reduced power is prohibited

Operations from runways contaminated with water, slush or loose snow:
- Max altitude for T/O & LDG is 6000’
- Max permitted WED of contaminant is 15mm
- Max depth of contaminant is 6cm
- For WED greater than 3mm, selection of power lever to DISC is prohibited
- Max crosswind component for T/O & LDG is 14kt

Operation from runways contaminated with compacted snow
- Max crosswind for T/O & LDG is 20kt

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27
Q

Airframe Contamination

A

See FOM for procedures on de-icing and anit-icing

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28
Q

Baggage Compartment Classifications

A

Class C with the following restrictions

  • A separate approved smoke detector or fire detector system to give warning to pilot station
  • An approved built in fire extinguishing system controllable from the pilot station
  • Any means to exclude hazardous quantities of smoke, flames or extinguishing agent, from any compartment occupied by the crew or passengers
  • Any means to control ventilation and draughts within the compartment so that the extinguishing agent used can control the fire that may start within the compartment.
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29
Q

Baggage compartment fire extinguishing time limitation

A

Unless the forward and aft baggage compartments are empty, the airplane must not be operated further than 1 hr flying time from a suitable airport for landing.

30
Q

Cargo Compartment fire extinguising time limitation

A

Unless the cargo compartment is empty, the airplane must not be operated further than 1 hr flying time from a suitable airport for landing.

31
Q

Minimum turning radius

A

26m

32
Q

Nose wheel steering angle required for minimum turning radius

A

70*

33
Q

Line up losses

A

See table in limitations

34
Q

Static Eye to Ground and ILS to ground distances

A

Eye - 3.029m
ILS - 1.864m

35
Q

Minimum Runway width

A

30m

36
Q

ACN classification with 34” tires - Values at MTOW (Rigid pavement subgrade)

A

High - 17.6
Medium - 18
Low - 19.1
Ultra Low - 19.9

Recommendation to use 20 for planning purposes

37
Q

ACN classification with 34” tires - Values at MTOW (Flexible pavement subgrade)

A

High - 15.2
Medium - 16.0
Low - 18.3
Ultra Low - 20.2

Recommendation to use 20 for planning purposes

38
Q

LCN values with 34” tires

A

Rigid - LCN 39
Flexible - LCN 43

39
Q

Approved Approach flap settings

A

5, 10, 15 degrees

40
Q

Approved Landing flap settings

A

10, 15, 35 degrees

41
Q

Approved cruise flap setting

A

0 degrees

42
Q

Operating with gear extended and doors closed

A

Subject to local airworthiness authorities

43
Q

Operating limitations for non - normal ops

A

See Limitations sections

44
Q

Max difference between L & R ASI at approach and cruise speeds.

A

2kts

45
Q

Max difference between ASI and STBY ASI at approach and cruise speeds

A

10kts

46
Q

When altitude mismatch appears on PFD apply corrections to the Integrated Standby Instrument

A

See table in limitations chapter

47
Q

Min and Max temp for operation of engine

A

Min - -54c
Max - +50
c or ISA +35*c (whichever is lower)

48
Q

Max temp for operation with engine intake bypass doors open

A

ISA + 25*c

49
Q

Maximum Airstart altitude

A

20,000’

50
Q

Roughly how much torque will Automatic Take off Power Uptrim provide?

A

10% torque (nominal)

51
Q

Max taxi speeds straight and turning
- Normal Taxiway
- Narrow (15-18m) Taxiway

A

25kt straight
15kt turning

15kt straight
10kt turning

52
Q

Maximum Torque Settings

A

MTOP - 106%
NTOP - 90.3% (indication of 90% or 91%)
MCP - 100%
Transient - 135%
Reverse - 35%

53
Q

Maximum ITT settings (*C)

A

MTOP - 880
NTOP - 822
MCP - 880
Transient - 920
Starting - 920
Reverse - 880

54
Q

Maximum NL% RPM across power ranges

A

MTOP - 100
NTOP - 95.3
MCP - 100
Transient - 102.3
Reverse - 100

55
Q

Maximum NH% RPM

A

MTOP - 100%
NTOP - 97.6%
MCP - 100%
Transient - 101.2%
Reverse - 100%

56
Q

Maximum NP RPM

A

MTOP - 1020
NTOP - 1020
MCP - 1020
Transient - 1173
Reverse - 1020

57
Q

Oil Pressure PSID

A

MTOP - 61 - 72
NTOP - 61 - 72
MCP - 61 - 72
Starting - 100 Max (165 Discing < 0* OAT)
Transient - 44 to 61 & 72 - 100 (20sec max)
Reverse - 61 to 72

58
Q

Oil Temp (*C)

A

MTOP / NTOP / MCP - 0 to 107 (115 permitted for continuation of flight with 20% reduction in power. Maint action reqd)
Starting - -40
Transient - 125 for 5 sec above FLT IDLE & < 55%
Reverse - 0 to 107

59
Q

Engine and Propellor Ground limitations
Wind Speed
- 9 to 20kts
- 21 to 35kts
- 36 to 50kts (55kt gusts)

A

Max TQ is 100%
Minimum NH is 64.2%
Nose of aeroplane > 30* out of wind - 50kts
Wind > 8kts and nose > 30* out of wind (see below)

  • FLT IDLE (momentary above is ok)
  • FLT IDLE
  • FLT IDLE (PWR levers must be at DISC when stationary)
60
Q

Starter Cranking limits

A

1) 70 sec on 2 min off
2) 70 sec on 2 min off
3) 70 sec on 30 min off

61
Q

Maximum Fuel

A

5318kg

62
Q

What position must the fuel pumps be at for TO and LDG

A

ON

63
Q

Hydraulic system minimum QTY’s

A

1) 40%
2) 40%
3) 45%

64
Q

Rejected Landing Considerations

A

Brake cooling times (AFM)

65
Q

APU starter Limitations

A

1min on 5 mins off
1 min on Maintenance action required (&30mins)

66
Q

In regard to Airframe contamination, what must be the condition of the aircraft before departure?

A

Must be free of Frost, Ice and snow before takeoff

67
Q

PEC?

A

20 foot addition

68
Q

Battery max load for departure

Battery min Temp

A

0.1

-20*C

69
Q

When must AP be disconnected?

A

Flaps 0 < 1000’ AGL
Severe Icing
Pilot at control seat
on landing <200’ AGL
OEI approach < 1000’ AGL
AP / FD approach 2.5* to 4* only

70
Q

Minimum speed gates
flaps: 0
5
10
15 & 15 with 35 selected for landing
35
Holding

A

0 - 180
5 - 165
10 - 155
15 - Vref or Vref ICE
15 with 35 for landing - Vref ICE Flap 35 + 10kts
35 - Vref or Vref ICE
Holding - 190kts

71
Q

What is the minimum speed in the climb

A

Vbg or Vbg ice