Limitations Flashcards

(69 cards)

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
Max Operating Altitude
40,000ft
26
Max Operating Altitude with Center & Trim Tank Deactivated (Payload/Deact Mode)
35,000ft
27
Load Limits Slats & Flaps Retracted
+2.5 to -1.0
28
Load Limits Slats or Flaps Extended
+2.0 to 0.0
29
Takeoff & Landing Temp Limits
55°C (135°F) -60°C (-76F)
30
Maximum Wind for Main Deck Cargo Door Operation
40Kts
31
Maximum Wind for all other doors
60Kts
32
Use Engine Anti-Ice when icing conditions exist or are anticipated except in _______ or ________ when SAT is ______°C or below.
Climb Cruise -40°C
33
On the ground Icing Conditions exist when the OAT is ______°C or below and Visible Moisture is Present
10°C
34
In Flight, icing conditions exist when the TAT is ______°C or below and visible moisture is present
10°C
35
Engine Anti-Ice must be ON prior to and during ________ in icing conditions including temperatures below ______°C SAT
Descent -40°C
36
Select ENG ANTI ICE ON if takeoff in icing conditions or when icing conditions are expected below ______ft AGL
1,500ft
37
Autopilot is not authorized below:
500ft AGL
38
Min ALT for Autopilot use with least one autopilot engaged in CMD with LAND Mode (Without use of Autoland)
50ft above TDZE
39
All other Approaches Min Autopilot Altitude Use:
DA/DDA
40
Min Altitude for Autopilot after Go Around or Missed Approach:
500ft AGL
41
Certified Autoland (Automatic Landing and Roll-Out) Configuration:
Slats/Flaps 30/40
42
Do not use ROLLOUT mode on:
Snow covered or icy runway
43
Light Off Times Maximum Ground Maximum Flight
CF6: 25 Sec Ground 45 Sec Flight PW: 20 Sec Ground
44
CF6 Continuous engagement: _______min Before re-engaging, OFF for ______sec for each minute used. After ______ start cycles, OFF for _____min
5 minutes 30 seconds 2 start cycles 10 minutes
45
CF6 Under normal conditions do not engage starter above ______% N2. Emergency conditions (engine fire) starter may be re-engaged with N2 as high as ______%
20% 30%
46
Maximum N2 for starter engagement is _____%
30%
47
PW N1 rotation must be obtained by _____% N2
40% N2
48
PW Maximum N2 for starter engagement is _____%
30%
49
PW ______ consecutive starts may be attempted
Two (2)
50
PW Motor engine for ______ sec following aborted start
30 seconds
51
PW After second start attempt, cool starter for ______ minutes before attempting subsequent starts
30 minutes
52
CF6 Abort start if EGT remains in the 750° - 870° for more than ______ seconds or exceeds ______°
40 seconds 870°C
53
PW Abort Start if EGT exceeds _____°C on the ground or ______° (PW4152) in flight
535°C 625°C
54
Minimum Oil Qty Before Start
16 Qts
55
APU Oil Qty Minimum for start
1/4
56
APU Starter Maximum Altitude (BAT Only)
20,000ft
57
APU Starter Maximum attempts per hour Above FL370: FL370 & Below:
5 3
58
APU Bleed Air Max Altitudes 1 A/C Pack & Wing Anti-Ice: 2 A/C Packs: Engine Start:
Up to 15,000ft Up to 20,000ft Up to 20,000ft
59
Maximum altitude with Slats / Flaps extended:
20,000ft
60
Do not use Speed Brakes with Slats/Flaps:
Greater than 15/20
61
A300 Total Fuel Quantity
120,650
62
Fuel must be burned from tanks in the following order:
CTR, Inner, Outer
63
Fuel Imbalance Wing to Wing: Inner Tank to Inner Tank: Outer Tank to Outer Tank:
Wing to Wing: 2,000lbs Inner Tank to Inner Tank: 2,000lbs Outer Tank to Outer Tank: 870lbs
64
Maximum Brake Temps for Takeoff Brake Fan Off: Brake Fan On: Do not takeoff with _____________ Caution Light Illuminated
Brake Fan Off: 300 Brake Fan On: 150 Brake Overheat
65
Do not reposition the following controls during a non-normal procedure, until confirmed by the PF:
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
Aircraft Dimensions Wing Span: Height: Length:
Wing Span: 147’ 1” Height: 54’ 3” Length: 176’ 8”
67
LAHSO Minimum Runway Length
6,700’
68
Inbound Fuel Qty vs. Block A of FSF
1,500lbs
69
FOB vs Release Tolerance
1,000lbs