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Latitude Study Guide > (RKA) AOM RED [& RKA] Limitations (AOM 1.3.0) > Flashcards

(RKA) AOM RED [& RKA] Limitations (AOM 1.3.0) Flashcards

1
Q

Crosswind Limit Dry or Wet Runway
(AOM 12.1.3)

A

30 kts for both Takeoff and Landing

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2
Q

Contaminated Runway Crosswind Limitation ≥ 150 ft
(AOM 12.1.3)

A

15 kts

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3
Q

Contaminated Runway Crosswind Limitation < 150 ft
(AOM 12.1.3)

A

10 kts

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4
Q

Tailwind for Takeoff & Landing
(AOM 12.1.4)

A

10 kts

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5
Q

Maximum Ramp & Taxi Weight
(AOM 12.2.3)

A

31,050 lbs.

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6
Q

Maximum Takeoff Weight
(AOM 12.2.3)

A

30,800 lbs.

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7
Q

Maximum Landing Weight
(AOM 12.2.3)

A

27,575 lbs.

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8
Q

Maximum Operating Altitude
(AOM 12.3)

A

45,000 ft.

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9
Q

Minimum Altitude for Speed Brake extension
(AOM 12.3)

A

500 ft AGL

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10
Q

Turbulent Air Penetration Speed
(AOM 12.5)

A

225 kts or .73 M

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11
Q

Maximum Landing Gear Operating Speed
(AOM 12.5)

A

210 kts

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12
Q

Maximum Airspeed Flaps 1
(AOM 12.5)

A

250 kts

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13
Q

Maximum Airspeed Flaps 2
(AOM 12.5)

A

200 kts

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14
Q

Maximum Airspeed Flaps FULL
(AOM 12.5)

A

175 kts

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15
Q

Minimum Holding in icing speed
(AOM 12.5)

A

180 kts

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16
Q

Pressurization Above FL410
(AOM 12.6)

A

L & R ENG BLD AIR to NORM or HP and select PRESS SOURCE to NORM.

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17
Q

Pressurization On Ground
(AOM 12.6)

A

Cabin must be depressurized prior to operating the cabin door.

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18
Q

APU Starter Operation Limits
(AOM 12.8.1)

A
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19
Q

Maximum airspeed for APU start
(AOM 12.8.1)

A

305 kts

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20
Q

Maximum altitude for APU start
(AOM 12.8.1)

A

20,000 ft

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21
Q

Maximum operating APU airspeed
(AOM 12.8.2)

A

305 kts .80M

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22
Q

Maximum APU operating altitude

A

30,000

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23
Q

Autopilot use enroute or descent
(AOM 12.9.1)

A

1000 ft AGL

24
Q

Autopilot use ILS or LPV approach
(AOM 12.9.1)

A

160 ft AGL

25
Q

Autopilot use all other approach types
(AOM 12.9.1)

A

200 ft AGL

26
Q

Autopilot use takeoff, climb, and missed approach
(AOM 12.9.1)

A

400 ft AGL

27
Q

Autothrottle HOLD
(AOM 12.9.2)

A

Must be displayed prior to 65 kts during takeoff

28
Q

Autothrottle engagement
(AOM 12.9.2)

A

If not already engaged during takeoff, do not engage autothrottle above 65 kts on the ground, and not until at or above 400 ft AGL.

29
Q

Autothrottle disengagement
(AOM 12.9.2)

A

Prior to landing with other than FULL flaps.

30
Q

Sufficient voltage for battery start
(AOM 12.10)

A

Displayed green.

31
Q

Maximum GPU voltage
(AOM 12.10)

32
Q

Maximum Fuel Imbalance
(AOM 12.12)

33
Q

Ground operation of Pitot Static Heat
(AOM 12.15.1)

A

Two minutes.

34
Q

Approach Category
(AOM 12.18.4)

A

Category B

35
Q

Maximum tailwind component for engine start
(AOM 12.19.2)

36
Q

Takeoff Thrust All Engines Operating
(AOM 12.19.2)

A

5 minutes.

37
Q

Takeoff Thrust One Engine Inoperative
(AOM 12.19.2)

A

10 minutes.

38
Q

Use of Reverse Thrust
(AOM 12.19.2)

39
Q

Transient N1 (%)
(AOM 12.19.2)

A

106% for 20 seconds.

40
Q

Transient N2 (%)
(AOM 12.19.2)

A

106% for 20 seconds.

41
Q

Maximum ITT Transient (Deg C)
(AOM 12.19.2)

A

950 Degrees C. for 20 seconds

42
Q

Oil Pressure (psi) Transient
(AOM 12.19.3)

A

0-20 psi for 20 seconds.

43
Q

Cool-Down Period Between Engine Start Attempts
(AOM 12.19.4)

A

Limitation is independent of power source and applies to dry or wet motoring.

44
Q

Engine Motoring Time Limits
(AOM 12.19.4)

A

To only motor the engine (no start)

45
Q

Refueling pressure range

A

10 - 55 PSI

46
Q

Defueling pressure range

A

0 to -10 PSI

47
Q

Maximum Operating Speed Mmo

A

Mach 0.80 (indicated)

48
Q

Maximum Operating Speed Vmo
(Below 8,000 feet)

A

305 KIAS
(270 KIAS)

49
Q

VFTO

50
Q

Minimum Speedbrake Extended Speed?

A

Vref + 15 KIAS

51
Q

Maximum landing sink rate

52
Q

Maximum baggage compartment weight

A

1,000 lbs.
[Max floor loading distribution: 150 pounds per square foot]

53
Q

Engine Generator Limits
Ground
Air
>FL350

A

Ground: 300 amps
Air: 300 amps
>FL350: 275 amps

54
Q

APU Generator Limits
Ground
Air
>FL350

A

Ground: 275 amps
Air: 275 amps*
>FL350: N/A

*The maximum altitude for operating the APU is FL300.

55
Q

Thrust reverser limitations:

A
  • Must be at idle by 65 kias
  • Deployment for more than 30 seconds with APU operating is prohibited
  • Static ground operations is limited to IDLE with reversers deployed.
  • Prohibited during touch-and-go landings.
  • Using to back the airplane is prohibited.

Latitude Study Guide (33 decks)

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