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EMB-505S Study Cards > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

45-Minute IFR Reserve (lbs.)

A

1121 lbs. (FL300, .74, 16800 lbs)

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2
Q

Minimum Fuel for Release

A

1880 lbs.

DO or ADO on duty may authorize reduction of this quantity

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3
Q

Minimum Fuel for Hot Spare

A

3600 lbs.

DO or ADO on duty may authorize reduction of this quantity

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4
Q

Emergency Fuel

A

759 lbs.

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5
Q

Minimum Runway Length for Release.

A

3500 feet DRY.

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6
Q

Minimum Runway Width

A

60 feet

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7
Q

Max Slope

A

+/- 2%

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8
Q

(Runway Requiremets) Ops Review Required if…

A
  1. Dry: Less Than 4000ft.
  2. Wet/Contaminated: Less than 5500ft.
  3. DAAP Less than 4500

Chief pilot must approve release from or to, or landing on runways with poor braking action.

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9
Q

Exceptions to Runway Requirements…

A

Beaufort, SC (KARW), 3434ft x 75ft, Day and Dry Only.

Port Aransas, TX (KRAS), 3482ft x 70ft. Day Only, Dry Only, Max crosswind 15KTS.

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10
Q

Maximum crosswind for takeoff (STATIC)

A

18 KTS

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11
Q

Maximum crosswind for takeoff (Rolling)

A

25 KTS.

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12
Q

Maximum Crosswind for Landing

A

28 KTS

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13
Q

Maximum Crosswind on a Contaminated Runway

A

Runway = or > 150’…………….. 15KTS

Runway = or < 149’…………….. 10 KTS

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14
Q

Maximum Tailwind for takeoff and landing:

A

10 KTS

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15
Q

The Following Equipment must be operational in RVSM Airspace:

A

Autopilot (1)

Altitude Alerting Device (1)

ATC altitude reporting transponder (1)

Air Data Computers (2)

Pitot Heaters (2) on the probes linked to the ADC in use.

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16
Q

Maximum Ramp/Taxi Weight

A

18,497 lbs.

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17
Q

Maximum Takeoff Weight

A

18,387 lbs

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18
Q

Maximum Landing Weight

A

17042

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19
Q

Maximum Zero Fuel Weight

A

14,220 Lbs

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20
Q

Maximum Operating Altitude

A

45,000 ft.

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21
Q

Maximum Flaps Extended Altitude

A

18,000 ft.

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22
Q

Maximum Altitude OEI in Icing

A

15,000 ft.

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23
Q

Maximum Altitude for TAKEOFF and LANDING

A

14,000 ft

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24
Q

Maximum Altitude for TAKEOFF and LANDING in Icing

A

10,000 ft.

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25
Q

Maximum Operating Speed Vmo

A

320 KTS.

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26
Q

Maximum Operating Mach Number Mmo

A

.78 mach

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27
Q

Turbulent Air Penetration Speed

A

232 kts/.65 mach

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28
Q

Maneuvering Speed

A

205 Kts

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29
Q

Maximum Landing Gear Operating Speed

A

250 KTS

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30
Q

Maximum Tire Ground Airspeed

A

182 KTS

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31
Q

Vfe Flaps 1

A

180 KTS

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32
Q

Vfe Flaps 2 and 3

A

170 KTS

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33
Q

Vfe Flaps Full

34
Q

Minimum Airspeed in Icing - WING STAB anti-ice system INHIBITED (flaps and gear up)

35
Q

Minimum Airspeed in Icing - WING STAB anti-ice system UN-INHIBITED (flaps and gear up)

36
Q

Maximum Airspeed in Icing - YAW DAMPER OFF

37
Q

Vmc TAKEOFF

38
Q

Vmc LANDING

39
Q

Vmc LANDING in Icing

40
Q

Max Differential Pressure (psi)

41
Q

Max Differential OVERPRESSURE

42
Q

Max NEGATIVE Differential

43
Q

Max Differential for TAKEOFF and LANDING

44
Q

Do Not use Autopilot or Yaw Damper for….

A

TAKEOFF and LANDING

** DO NOT MANUALLY OVERRIDE AUTOPILOT DURING NORMAL FLIGHT.

45
Q

Autopilot or Yaw Damper MINIMUM engagement height TWO ENGINES

A

600 ft AGL

46
Q

Autopilot or Yaw Damper MINIMUM engagement height OEI

A

1000 ft AGL

47
Q

Autopilot or Yaw Damper MINIMUM USE height TWO ENGINES

A

195 ft. AGL

48
Q

Autopilot or Yaw Damper MINIMUM USE height OEI (ONE ENGING INOP)

A

220 ft AGL

49
Q

Minimum Voltage for Battery Start

50
Q

Minimum GPU voltage for Battery Charging

51
Q

Maximum generator load in flight

52
Q

Maximum generator load on the ground

53
Q

Total Fuel Quantity

54
Q

Maximum Fuel Imbalance

55
Q

Operate the Engines and Airframe anti-icing systems in accordance with:

A

4.5.2 Operation of Anti-Ice Systems

56
Q

Minimum Temperature for Landing

57
Q

Automated operating (Temperature) Envelope for wing stab heating (Below 16,000ft)

A

-40 C

Amber A-I WINGSTB INHB CAS message is displayed if WING STAB is selected ON outside the operating envelope. Refer to QRH for additional information.

58
Q

Automated operating Envelope for wing stab heating (at or above 16000ft)

A

-45C

Amber A-I WINGSTB INHB CAS message is displayed if WING STAB is selected ON outside the operating envelope. Refer to QRH for additional information.

59
Q

Do Not use the Autopilot in icing conditions when:

A
  • there is ice accumulation on the wing, aft of the protected area.
  • encountering unusual lateral trim inputs or autopilot trim warnings
60
Q

Aircraft is certificated in Approach Category:

A

Category B

** however, if operational requirements dictate and approach speed faster than 120Kts, use Category C minima.

61
Q

Time Limitation at Maximum Thrust

A

10 minutes

62
Q

Time limit at Takeoff Thrust

63
Q

Maximum Continuous Thrust time limit and condition

A

5 Minutes when in level flight.

64
Q

Climb Thrust time limit and condition

A

5 minutes in level flight.

65
Q

Max TRANSIENT N1

66
Q

Max TRANSIENT N2

67
Q

Max TRANSIENT ITT

68
Q

Max TRANSIENT time limit

A

20 seconds

69
Q

Max ITT for Engine Start

70
Q

Max Continuous/Climb Thrust ITT

71
Q

Max ITT at Takeoff Thrust

72
Q

Max ITT at Maximum Thrust

73
Q

Ground Idle N2

74
Q

Flight Idle N2

75
Q

Max N1/N2 (maximum Thrust, takeoff thrust, Max cont thrust, climb thrust)

A

N1 - 100%

N2 - 101%

76
Q

One Engine Inoperative (OEI) ground Idle N2

77
Q

Min-Max TRANSIENT oil Pressure (20 Seconds)

78
Q

Min-Max TRANSIENT oil Pressure (400 Seconds)

A

20-270 psi

79
Q

Starter Limitations…. How many attempts? Cool Down?

A

Four Attempts:

1st attempt, 1 minute cool down
2nd attempt, 1 minute cold down
3rd attempt, 15 minutes cool down
4th attempt, 30 minutes cool down

80
Q

Unless the batteries are warmed prior to start, GPU assisted engine start must be accomplished when OAT is at or below?

A

-18 C (AOM 4.5.1 Cold Soaked Airplane)

EMB-505S Study Cards (15 decks)

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