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P-8 > Limits > Flashcards

Limits Flashcards

1
Q

Runway Slope

A

+- 2%

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2
Q

Vmo

A

340

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3
Q

Mmo

A

0.82

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4
Q

Maximum Operating Altitude

A

41,000

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5
Q

Maximum Takeoff and Landing Altitude

A

8,400

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6
Q

Maximum Takeoff Crosswinds (flaps 1,5 dry)

A

35 knots

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7
Q

Maximum Takeoff Crosswinds (flaps > 5, dry)

A

30 knots

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8
Q

Maximum Takeoff Crosswind (all flaps, wet)

A

25 knots

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9
Q

Maximum Landing Crosswind (All flaps, dry)

A

35 knots

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10
Q

Maximum Landing Crosswind (All flaps, wet)

A

30 knots

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11
Q

Maximum Takeoff and Landing Crosswind (all flaps, contaminated)

A

15 knots

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12
Q

Maximum Takeoff and Landing Tailwind Componet

A

15 Knots

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13
Q

Maximum Total Air Temperature (TAT)

A

55°C

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14
Q

Maximum Touch and Go Crosswind Reccomendation

A

25 knots

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15
Q

Maximum Landing Crosswind Recommendation Flaps 40

A

30 knots

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16
Q

RVSM Maximum In-Flight Altitude Difference

A

200 ft

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17
Q

Maximum RVSM On-The-Ground Altitude Display Difference

A

50 ft (sea level - 5,000)
60 ft (5,001 - 10,000)

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18
Q

Maximum RVSM On-The-Ground Altitude Between Display and Field Elevation

A

75 ft

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19
Q

IDG Load Limit During Ground Operations

A

41% Load requires 32% N1

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20
Q

Engine Oil Minimum

A

Overland: 60% (12 Quarts)
Overwater: 60% (12 Quarts) or 7 Quarts plus 1 Quart per Total Flight Hour (whichever is higher)

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21
Q

Minimum Oil to Arrive at Destination or Alternate

A

7 Quarts

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22
Q

Maximum Takeoff EGT

A

950-965°C (3 minutes)
950°C (5 minutes) (Increases to 10 min if Engine Failure Occurs)

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23
Q

Maximum Continuous EGT

A

925°C

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24
Q

Maximum Start EGT

A

725°C

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25
Q

Maximum N1 RPM

A

104.7% (20 seconds)
104.0% (continuous)

26
Q

Maximum N2 RPM

27
Q

Minimum Oil Pressure

28
Q

Maximum Oil Temperature

A

155°C (maximum)
140-155°C (45 minutes)
140°C (continuous)

29
Q

Engine Idle Time Prior to Shutdown

30
Q

Maximum Start Time

31
Q

Time Required Between Starts

A

10 seconds

32
Q

Maximum N2 to Engage Starter

33
Q

Engine Ignition for Moderate or Heavy Rain, Hail or Sleet

34
Q

Engine Ignition for Severe Turbulance

35
Q

Assumed Temperature Method Limits

A

Shall not be amused for EEC in Alternate Mode, Contaminated With Slush, Snow, Standing Water or Ice, or when Antiskid is Inoperative

Not Recommended for Potential Windshear

36
Q

Reduced Thrust Takeoff Limits

A

Not Recommended for Potential Windshear
Shall Not Be Used for Takeoff With EEC in Alternate

37
Q

EEC in Alternate for Takeoff Limits

A

1) Both in Alternate
2) No Fixed Derate or ATM
3) Do Not Use FMC Takeoff N1
4) Use of Autothrottle is Prohibited

38
Q

AAR Airspeed Envelope

A

250-300 Knots

39
Q

AAIR Altitude Envelope

A

8,000-28,000 ft

40
Q

Minimum On-Station Altitude

A

200 ft AGL

41
Q

Minimum Altitude for Seat Swaps

A

1,000 ft AGL

42
Q

Maximum Taxi Weight

A

189,700 lbs

43
Q

Maximum Takeoff Weight

A

189,200 lbs

44
Q

Maximum Landing Weight

A

149,800 lbs

45
Q

Maximum Zero Fuel Weight

A

141,800 lbs

46
Q

Maximum Fuel Temperature

A

Active Feeding: 59°C
Not Feeding: 62°C

47
Q

Maximum Fuel Imbalance

48
Q

Minimum Fuel for Landing

A

6,000 lbs or 10% of Total Fuel Required (Transit+Onstation+Alternate)

49
Q

Minimum Temperature for Hot Fuel Mins

50
Q

Emergency On Deck Fuel

51
Q

Minimum Fuel for Electric Hyd Pumps

A

1,675 lbs in Related Tank

52
Q

APU Bleed Air and Electrical Load Maximum Altitude

53
Q

APU Bleed Air Maximum Altitude

54
Q

APU Electrical Load Maximum Altitude

55
Q

APU Altitude and Load Limit

A

32,000 ft, load must be below 68%

56
Q

Icing Conditions

A

10°C and Visible Moisture

57
Q

Minimum Altitude for Autopilot on Takeoff

58
Q

CWS Bank Angle Limit

A

Above 1,500 ft: 45° AOB
Below 1,500 ft: 30° AOB

59
Q

Autopilot Minimum Altitude

A

Non-Terminal: 500ft
Approach: Minimums (50ft below DH or 50+MDA) or 100ft AGL

60
Q

Turbulent Air Penetration Speed

A

280 knots
0.76 Mach

61
Q

Maximum Hydraulic Pressure

62
Q

Hydraulic Quantity Limits

A

Minimum: 76%
Maximum: 106%

P-8 (2 decks)

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