Ops Limits Flashcards

(34 cards)

1
Q

Airplane / power plant maximum operating ambient temperature:

A

+50C or ISA +35C, whichever is lower

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2
Q

Airplane / power plant minimum operating temperature:

A

-54C

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3
Q

APU maximum operating ambient temperature:

A

+50C or ISA +35C, whichever is lower

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4
Q

APU minimum operating temperature:

A

-54C

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5
Q

Maximum operating altitude:

A

25,000 ASL

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6
Q

Maximum operating altitude for takeoff:

A

10,000 ASL

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7
Q

Max crosswind for takeoff and landing:

A

32 knots

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8
Q

Max ramp weight:

A

65,400 lbs

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9
Q

Max takeoff weight:

A

65,200 lbs

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10
Q

Max landing weight:

A

62,000 lbs

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11
Q

Severe turbulence speed:

A

210 Knots

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12
Q
Maneuvering Speed (vA): 
(Maximum speed with full application of rudder and aileron controls and maneuvers that involve angles of attack near the stall.)
A

204 Knots

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13
Q

Max Gear Extended Speed (vLE):

The maximum speed with landing gear extended.

A

215 Knots

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14
Q

Landing Gear Operating Speed (vLO):

The maximum speed it is safe to extend or retract landing gear.

A

195 Knots

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15
Q

Max Fuel Capacity:

A

11,724 lbs

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16
Q

Fuel: Max Imbalance (Inflight Only)

17
Q

Fuel: Tank 1 and 2 Auxiliary Pumps

A

On for takeoff and landing

18
Q

Engine Starter Cranking Limit:

A

70 seconds followed by 2 minutes off

19
Q

APU Starter Cranking Limit:

A
  • 60 seconds followed by 5 minutes off.

- Second attempt 60 seconds followed by 30 minutes off (MX Req’d after 2nd attempt).

20
Q

Battery Load Prior to Takeoff (Main, Aux, Standby):

21
Q

Min Battery Temperature Prior to Takeoff:

22
Q

Max Altitude Gear and Flaps Extended:

23
Q

Max Cabin Differential:

24
Q

Max Cabin Differential - Takeoff and Landing:

25
Bleed Air Must Be Off For Takeoff or Landing Whenever: (WTTL)
- Wind shear is suspected - Tailwind exceeds 10 knots - Takeoff with MTOP power selected - Landing only when OAT exceeds 39C (100F)
26
AHRS: Takeoff is prohibited in
BASIC mode | DG mode
27
Baggage Compartment Fire Extinguishing:
Unless the fwd and aft baggage compartments are empty, the airplane shall not be operated farther than one hour flying time from a suitable airport for landing.
28
Conditions Requiring a Takeoff Abort: (WHEETTFM)
- Windshear encounter - HGS failure, "TO WARN", or loss of HGS symbology during takeoff below 500 RVR when runway CL is not in sight - Engine fire or failure - Exceeding engine limitations - Takeoff warning horn - Takeoff torque not obtained on either engine - Failure of the A/F ARM message to illuminate on ED - MASTER WARNING
29
First Officer's Briefing:
Call out 80, V1 and rotate. Call any malfunctions, if before V1 it will be your decision to abort. After V1 I will continue the takeoff.
30
Flight Compartment Communication:
HOT MIC select switches on the Captain and FO ARCDU shall be OFF and the INT/RAD switch on the observer's audio control panel shall be centered when using the flight deck speakers.
31
APU Limitations:
- APU is approved for GROUND OPERATION ONLY - APU shall be shutdown prior to takeoff - APU shall not be operated unattended with passengers on board - APU shall not be operated during gravity refueling - (QX) To maintain steady electrical state, the APU shall not be started during refueling - (QX) The APU bleed air shall be selected OFF when the aircraft is being deices/anti-iced
32
Engine Limitations (3):
- Setting power for takeoff prior to brake release with winds over 8 knots more than 45 degrees off the nose is prohibited - Inflight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited - Engine Intake Bypass Doors must be open for operation in icing conditions
33
The use of VOR without associated DME is prohibited in _____ mode:
APP
34
Definition of icing conditions (Inflight):
SAT is 5 degrees or below and visible moisture is present in any form. Ice accretion on aerodynamic surfaces is not considered to exist at temperatures of -40dC or below.