Other Limitations [B767] Flashcards

1
Q

Runway Slope

A

+/- 2%

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2
Q

Max Operating Altitude

A

43,100’ PA

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3
Q

Max T/O & LDG Altitude

A

8,400’ PA

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4
Q

Nav & dislay systems do not support operations at latitudes greater than __ degrees North or South

A

87

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5
Q

Standby Altimeters do not meet the accuracy requirements of

A

RVSM

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6
Q

Max allowable IN-FLIGHT difference between Captain & First Officer altitude displays for RVSM operation

A

200 feet

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7
Q

Max allowable ON-GROUND difference between Captain & First Officer altitude displays for RVSM operation

A
Field Elevation - max diff CP & FO
Sea Level - 40' 
5,000' - 45'
10,000' - 50'
max diff (pilot & field) any alt. - 75'
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8
Q

Crew & Supernumerary Evacuation

A

1 operable inertia reel AND 1 escape harness for each occupant

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9
Q

Smoke Barrier door must be closed during:

A

Taxi, takeoff, flight, and landing

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10
Q

Engine ignitions system must be on for

A

Takeoff and landing

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11
Q

Minimum INFLIGHT Fuel Temp

A

3 deg. C (5 deg. F) > freezing point of fuel

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12
Q

Max Fuel Temp

A

49 deg. C (120 deg. F)

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13
Q

JET-B, JP-4, NATO F-40, T-2, RP-4, No. 4 jet fuel

A

PROHIBITED

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14
Q

The Center Fuel Tank may contain up to _____ lbs of Fuel with less than full main tanks provided the center tank Fuel weight plus actual zero fuel weight, and CG limits are observed.

A

22,050 LBS

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15
Q

GE Engine Starter Limits (Normal Duty Cycle)

A

Five(5) minutes
1) Five (5) minutesON, followed by ON, followed by
one and one half one and one half (1 (1 1/2) minutes
OFF.

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16
Q

GE Engine Starter Limits (Extended Duty Cycle)

A

Five 5 mins ON, followed by 1 1/2 mins OFF

Two consecutive cycles require a 10 minute cooling period before additional cycles can be attempted.

17
Q

GE Engine Starter Re-Engagement

A

Recommended starter Re-engagement: 0% N2
Permissible Starter Re-engagement: 0-20% N2
Permissible for purging or to clear a fire: 21-30% N2

Notes: A logbook entry is required whenever the starter is re-engaged above 20% N2.

Re-engagement above 30% N2 may result in starter or gearbox damage.

18
Q

GE Engines

Minimum Oil Quantity for dispatch

A

17 QTS

19
Q

During dual engine failure disregard ________ Start Limit and use _______ ________ ___ ___ Limit for Inflight Start EGT Limit.

A

Inflight

Standby Engine Indicator Max EGT

20
Q

GE Engines
Min Oil Press
Max Oil Temp

A

10 psi

160 deg. C (continuous ops)

21
Q

Minimum crew Oxygen Pressure

A

1300 psi

22
Q

APU Starter Duty Limitations

A

3 start attempts in 60 min