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A-300 > Limitations > Flashcards

Limitations Flashcards

1
Q

All Turns: A300 over 360,520 lbs

A

15 knots

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2
Q

Taxi Straight Ahead Max Speed

A

30 Knots

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3
Q

Sharp Turns and all turns on contaminated surfaces

A

8-10 Knots

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4
Q

A300 Vmo/Mmo

A

335Kts/.82M

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5
Q

A300 Slats/Flaps 15/0

A

250Kts

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6
Q

A300 Slats/Flaps 15/15

A

215Kts

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7
Q

A300 Slats/Flaps 15/20

A

205Kts

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8
Q

A300 Slats/Flaps 30/40

A

175Kts

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9
Q

A300 Kruger Extended Speed

A

300Kts/.65M

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10
Q

Landing Gear Extended (Vle)

A

270Kts / .65M

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11
Q

Landing Gear Extension (Vlo/Vmo)

A

270Kts / .59M

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12
Q

Landing Gear Retraction (Vlo / Mlo)

A

240Kts / .53M

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13
Q

Tire Speed

A

195Kts

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14
Q

Cockpit Windows Open

A

225Kts

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15
Q

Maximum RAT Operating Speed

A

320Kts

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16
Q

Windshield Wiper Speed

A

230Kts

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17
Q

Pitch System Inop Speeds

A

285Kts / .78M

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18
Q

Tailwind Limitation (Manual/Autoland)

A

10Kts

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19
Q

Autoland Headwind

A

30Kts

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20
Q

Crosswind (Autoland not CAT II/III)

A

20

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21
Q

Crosswind (Autoland CAT II/III)

A

15Kts

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22
Q

Crosswind Using Rev Thrust Above Idle with the other inop

A

20Kts

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23
Q

Minimum Width for 180° Turn

A

148ft / 45m

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24
Q

Max Contamination for Takeoff and Landing

A

4” Dry Snow
1” Wet Snow (1 1/8” Landing)
1/2” Water or Slush

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25
Q

Max Operating Altitude

A

40,000ft

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26
Q

Max Operating Altitude with Center & Trim Tank Deactivated (Payload/Deact Mode)

A

35,000ft

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27
Q

Load Limits Slats & Flaps Retracted

A

+2.5 to -1.0

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28
Q

Load Limits Slats or Flaps Extended

A

+2.0 to 0.0

29
Q

Takeoff & Landing Temp Limits

A

55°C (135°F)
-60°C (-76F)

30
Q

Maximum Wind for Main Deck Cargo Door Operation

A

40Kts

31
Q

Maximum Wind for all other doors

A

60Kts

32
Q

Use Engine Anti-Ice when icing conditions exist or are anticipated except in _______ or ________ when SAT is ______°C or below.

A

Climb
Cruise
-40°C

33
Q

On the ground Icing Conditions exist when the OAT is ______°C or below and Visible Moisture is Present

A

10°C

34
Q

In Flight, icing conditions exist when the TAT is ______°C or below and visible moisture is present

A

10°C

35
Q

Engine Anti-Ice must be ON prior to and during ________ in icing conditions including temperatures below ______°C SAT

A

Descent
-40°C

36
Q

Select ENG ANTI ICE ON if takeoff in icing conditions or when icing conditions are expected below ______ft AGL

A

1,500ft

37
Q

Autopilot is not authorized below:

A

500ft AGL

38
Q

Min ALT for Autopilot use with least one autopilot engaged in CMD with LAND Mode (Without use of Autoland)

A

50ft above TDZE

39
Q

All other Approaches Min Autopilot Altitude Use:

A

DA/DDA

40
Q

Min Altitude for Autopilot after Go Around or Missed Approach:

A

500ft AGL

41
Q

Certified Autoland (Automatic Landing and Roll-Out) Configuration:

A

Slats/Flaps 30/40

42
Q

Do not use ROLLOUT mode on:

A

Snow covered or icy runway

43
Q

Light Off Times
Maximum Ground
Maximum Flight

A

CF6:
25 Sec Ground
45 Sec Flight

PW:
20 Sec Ground

44
Q

CF6 Continuous engagement: _______min
Before re-engaging, OFF for ______sec for each minute used.
After ______ start cycles, OFF for _____min

A

5 minutes
30 seconds
2 start cycles
10 minutes

45
Q

CF6 Under normal conditions do not engage starter above ______% N2.
Emergency conditions (engine fire) starter may be re-engaged with N2 as high as ______%

A

20%
30%

46
Q

Maximum N2 for starter engagement is _____%

A

30%

47
Q

PW N1 rotation must be obtained by _____% N2

A

40% N2

48
Q

PW Maximum N2 for starter engagement is _____%

A

30%

49
Q

PW ______ consecutive starts may be attempted

A

Two (2)

50
Q

PW Motor engine for ______ sec following aborted start

A

30 seconds

51
Q

PW After second start attempt, cool starter for ______ minutes before attempting subsequent starts

A

30 minutes

52
Q

CF6 Abort start if EGT remains in the 750° - 870° for more than ______ seconds or exceeds ______°

A

40 seconds
870°C

53
Q

PW Abort Start if EGT exceeds _____°C on the ground or ______° (PW4152) in flight

A

535°C
625°C

54
Q

Minimum Oil Qty Before Start

A

16 Qts

55
Q

APU Oil Qty Minimum for start

A

1/4

56
Q

APU Starter Maximum Altitude (BAT Only)

A

20,000ft

57
Q

APU Starter Maximum attempts per hour
Above FL370:
FL370 & Below:

A

5
3

58
Q

APU Bleed Air Max Altitudes
1 A/C Pack & Wing Anti-Ice:
2 A/C Packs:
Engine Start:

A

Up to 15,000ft
Up to 20,000ft
Up to 20,000ft

59
Q

Maximum altitude with Slats / Flaps extended:

A

20,000ft

60
Q

Do not use Speed Brakes with Slats/Flaps:

A

Greater than 15/20

61
Q

A300 Total Fuel Quantity

A

120,650

62
Q

Fuel must be burned from tanks in the following order:

A

CTR, Inner, Outer

63
Q

Fuel Imbalance
Wing to Wing:
Inner Tank to Inner Tank:
Outer Tank to Outer Tank:

A

Wing to Wing: 2,000lbs
Inner Tank to Inner Tank: 2,000lbs
Outer Tank to Outer Tank: 870lbs

64
Q

Maximum Brake Temps for Takeoff
Brake Fan Off:
Brake Fan On:
Do not takeoff with _____________ Caution Light Illuminated

A

Brake Fan Off: 300
Brake Fan On: 150
Brake Overheat

65
Q

Do not reposition the following controls during a non-normal procedure, until confirmed by the PF:

A

Throttle
ENG FUEL Lever
FUEL ISOL VALVES
FIRE Handle
FIRE AGENT Switch
IDG Disconnect Switch
Circuit Breakers while in-flight
IRS Mode Selector Switch

66
Q

Aircraft Dimensions
Wing Span:
Height:
Length:

A

Wing Span: 147’ 1”
Height: 54’ 3”
Length: 176’ 8”

67
Q

LAHSO Minimum Runway Length

A

6,700’

68
Q

Inbound Fuel Qty vs. Block A of FSF

A

1,500lbs

69
Q

FOB vs Release Tolerance

A

1,000lbs

A-300 (6 decks)

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