767 memory items/Limitations Flashcards

1
Q

Max operating Alt.?

A

43,100’

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2
Q

Max TO and Ldg alt.?

A

8,400’

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3
Q

Max. TO and LDG tailwind comp.?

A

15kts.

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4
Q

Turbulent air penetration speed?

A

290 kts/.78 mach

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5
Q

At what latitudes are the navigation and display systems operation not supported?

A

87 degrees N and S

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6
Q

Do not operate the HF radios during?

A

Refueling operations.

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7
Q

Do the standby altimeters meet the RVSM accuracy requirements?

A

No.

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8
Q

Max inflight difference between the Cpts. and FO’s altitude displays?

A

200’

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9
Q

Max allowable on the ground differences between the Cpts. and FO’s altitude displays?

A

SL - 40’
5,000’ - 45’
10,000’ - 50’

75’ is the max diff. between Cpt/FO and field elevation.

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10
Q

Max wind gust with main cargo door open?

A

60 kts.

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11
Q

Max wind for operating the main cargo door?

A

40 kts.

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12
Q

Supernumery and Crew evacuation requirements?

A

Must have available for use, 1 operable inertial-reel and 1 operable escape harness for each occupant of the airplane.

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13
Q

Weather radar limitations?

A

Do not operate the wx radar in a hanger or within 50’ of any personnel or fuel spill.
The hanger and personnel restrictions do not apply to the test mode.

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14
Q

Flight deck security door requirements?

A

Verify that an operational check of the Flight Deck Access System has been accomplished according to approved procedures once each flight day.

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15
Q

During takeoff the autopilot must not be engaged below what alt.?

A

200’

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16
Q

When is the aileron trim use is prohibited?

A

when the autopilot is engaged.

17
Q

Max allowable wind speeds for wx minima CAT 1 or greater for autoland ops?

A

Headwind 25 kts
Crosswind 25 kts
Tailwind 15 kts

18
Q

Max allowable crosswind when wx minima are predicated on CAT 2 or 3 autoland ops?

A

15 kts

19
Q

The flight crew shall not blank the engine vibration display?

A

During Takeoff

20
Q

Minimum inflight fuel tank temp.?

A

3 degrees c above the freeze point of the fuel being used.

21
Q

Max fuel temp?

A

49 degrees C

22
Q

How much fuel may the center tank contain with less than full main tanks?

A

22,050 lbs. provided that the center tank fuel weight plus the actual ZFW does not exceed the MZFW and the CG limits are observed.

23
Q

Reverse thrust limits?

A

Are for ground use only.

24
Q

Max alt. for flap extension?

A

20,000’

25
Q

why should you avoid rapid and large alternating control inputs?

A

They may result on structural failure at any speed, including speeds below Va.

26
Q

What latitudes should you not operate into airports during IFR or at night, whose navigation aids are referenced to magnetic north?

A

73 degrees N or 60 degrees S

27
Q

On 312AA, 763CX if an approach is predicated on the use of DME data with an ILS or LOC what is the correct tuning procedure?

A

By aural station identification or DME data cross comparison between left and right DME’s prior to executing the approach.

28
Q

GPWS look-ahead-alerting limitations?

A
  • Do not use the terrain display for navigation.
  • the terrain display and functions are prohibited w/in 15 nm of takeoff, approach or landing if the airport is not contained in the database.
29
Q

When must the terrain display and functions be inhibited by selecting the Grd Prox switch to override?

A
  • when operating outside the US and the database is not referenced to WGS-84 unless the FMS has been found suitable for ops in that airspace.
  • FMS is operating in IRS NAV only
  • Prior to TO, FMS position updating is not accomplished or actual aircraft/runway position is not verified.
30
Q

767-200 Dimensions

A

156.1’ wingspan
159.2’ length
52’ height

31
Q

767-300 Dimensions

A

156.1’ wingspan
180.3’ length
52’ Height

32
Q

767 Turning Radius

A

767-200 129’

767-300 146’

33
Q

What are the Main Cargo Door wind limits?

A

40kts while operating

60kts in open position

34
Q

What are the Lower Cargo Door wind limits?

A

40kts while operating

65kts in open position

35
Q

How is the Main Cargo Door operated and from what bus?

A

Electrically controlled and operated off the ground handling bus.

36
Q

Thrust Ratings for CF6-80A, CF6-80A2 and CF6 80C2B6?

A

80A - 46,900lbs
80A2 - 48,000lbs
80C2B6 - 60,200lbs