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FedEx 767 Limits & Phase Ones > FedEx 767 Limitations > Flashcards

FedEx 767 Limitations Flashcards

1
Q

767 Flt Man - Rev 3: Limitations

Max Takeoff Weight:

A

408,000

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2
Q

767 Flt Man - Rev 3: Limitations

Max Landing Weight:

A

326,000

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3
Q

767 Flt Man - Rev 3: Limitations *

Normal Taxi Speed

A

20 kts

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4
Q

767 Flt Man - Rev 3: Limitations *

Taxi - Long straight:

A

30 kts

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5
Q

767 Flt Man - Rev 3: Limitations *

Taxi - Turns, dry surface

A

10 kts

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6
Q

767 Flt Man - Rev 3: Limitations *

Severe Turbulent Air Penetration Speeds:

A

290 kts / 0.78 Mach - whichever is lower

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7
Q

767 Flt Man - Rev 3: Limitations

Max Landing Gear Speed - Operating and Extended:

A

270 / 0.82 Mach

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8
Q

767 Flt Man - Rev 3: Limitations

Max Tailwind - Takeoff, Landing, and Autoland

A

15 kts

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9
Q

767 Flt Man - Rev 3: Limitations

Max Headwind - Autoland

A

25 kts

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10
Q

767 Flt Man - Rev 3: Limitations

Max Crosswind - Takeoff and Landing
– Runway CC = 6:

A

Takeoff: 30 kts
Landing: 30 kts

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11
Q

767 Flt Man - Rev 3: Limitations

Max Crosswind - Takeoff and Landing
– Runway CC = 5 / Braking Action = “GOOD”

A

Takeoff: 25 kts
Landing: 30 kts

** NOTE: Sideslip only (zero crab) landings are not
recommended with crosswind components
in excess of 26 knots.

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12
Q

767 Flt Man - Rev 3: Limitations

Maximum runway slope:

A

+/- 2%

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13
Q

767 Flt Man - Rev 3: Limitations

Minimum runway width for 180° turn:

A

146 feet/ 44.6 meters

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14
Q

767 Flt Man - Rev 3: Limitations

Maximum depth of slush, wet snow, or standing water for takeoff:

A

1/2 inch (13 mm)

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15
Q

767 Flt Man - Rev 3: Limitations

Maximum depth of dry snow for takeoff:

A

4 inches (102 mm)

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16
Q

767 Flt Man - Rev 3: Limitations

Max Operating altitude:

A

43,100 feet

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17
Q

767 Flt Man - Rev 3: Limitations

Maximum takeoff/landing altitude:

A

9,500 feet pressure altitude

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18
Q

767 Flt Man - Rev 3: Limitations

(T/F): The head-up display (HUD), if installed, must be stowed prior to deployment of the Emergency Vision Assurance System (EVAS).

A

True

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19
Q

767 Flt Man - Rev 3: Limitations

(T/F): Front windshield sunshields, if installed, may remain installed during deployment of EVAS.

A

False

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20
Q

767 Flt Man - Rev 3: Limitations

Door wind limits - any cargo door operation:

A

40 kts

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21
Q

767 Flt Man - Rev 3: Limitations

Door wind limits - any cargo door open:

A

60 kts

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22
Q

767 Flt Man - Rev 3: Limitations *

Icing conditions exist when:

A

OAT (ground and takeoff) or TAT (in-flight) = 10° C and visible moisture present.

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23
Q

767 Flt Man - Rev 3: Limitations

(T/F): Engine anti-ice must be ON during flight when icing conditions exist or are anticipated, except during “climb and cruise “ when the temperature is below -40°C SAT:

A

True

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24
Q

767 Flt Man - Rev 3: Limitations

(T/F): Engine anti-ice must be ON “prior to and during descent” in icing conditions, except when temperatures are below -40°C SAT.

A

False (should be “including” temperatures below -40 degrees SAT.)

“Except” below -40 SAT on climb and cruise.
“Including” below -40 SAT on descent.

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25
Q

767 Flt Man - Rev 3: Limitations

(T/F): Do not use anti-ice if OAT or TAT exceeds 10°C.

A

True

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26
Q

767 Flt Man - Rev 3: Limitations

How much should TAT normally increase for every 1,000’ descent.

A

Approximately 2° C

27
Q

767 Flt Man - Rev 3: Limitations

What conditions must exist for ice crystals to form?

A

Visible moisture and one of the following:

  • Amber or red WX radar returns below the airplane.
  • Liquid water on the windshield at temperatures too
    cold for rain.
  • Autothrottle unable to maintain airspeed.
  • TAT indication on EICAS stays near 0°C.
28
Q

767 Flt Man - Rev 3: Limitations *

(T/F): Use of aileron trim with the autopilot engaged is prohibited.

29
Q

767 Flt Man - Rev 3: Limitations *

(T/F): Do not use FLCH on final approach below 1,000’ AFE.

30
Q

767 Flt Man - Rev 3: Limitations *

Do not use the autopilot below 100’ radio altitude at airport field elevations above what altitude?

31
Q

767 Flt Man - Rev 3: Limitations

Minimum altitude for autopilot engagement after takeoff:

A

1000’ AFE

32
Q

767 Flt Man - Rev 3: Limitations

Autopilot Minimum Altitude - Coupled ILS without autoland:

33
Q

767 Flt Man - Rev 3: Limitations

Autopilot Minimum Altitude - Non-precision with VNAV:

A

50’ below DA

100’ below DDA

34
Q

767 Flt Man - Rev 3: Limitations

Autopilot Minimum Altitude - Non-precision with V/S:

A

50 below MDA

100 below DDA

35
Q

767 Flt Man - Rev 3: Limitations

At what flap settings is autoland authorized?

A

Flaps 25 or 30 (Both engines or single engine)

36
Q

767 Flt Man - Rev 3: Limitations

(T/F): : Do not operate HF radios during refueling operations.

37
Q

767 Flt Man - Rev 3: Limitations

Takeoff Power EGT time limit:

38
Q

767 Flt Man - Rev 3: Limitations

Max Continuous Power time limit:

A

Continuous

39
Q

767 Flt Man - Rev 3: Limitations

(T/F): Reverse Thrust for back taxi is limited to 30 seconds.

A

False - Reverse Thrust is not authorized for reverse taxi.

40
Q

767 Flt Man - Rev 3: Limitations

Normal Starter duty cycle:

A

Five minutes on, followed by one-half minute off per minute on.

41
Q

767 Flt Man - Rev 3: Limitations

Starter Re-engagement speed (N2)

  • Recommended:
  • Normal:
A
  • Recommended: 0% N2

- Normal: 0-20% N2

42
Q

767 Flt Man - Rev 3: Limitations

What is the one exception for Starter Re-engagement above 20% N2?

A

Engine Fire (other engine)

43
Q

767 Flt Man - Rev 3: Limitations

The APU starter duty cycle:

A

Three consecutive starts or attempts within

a sixty-minute period.

44
Q

767 Flt Man - Rev 3: Limitations *

(T/F): Avoid rapid and large alternating control inputs,
especially in combination with large changes in
pitch, roll, or yaw (e.g., large side slip angles) as
they may result in structural failure at any speed,
including below VA.

45
Q

767 Flt Man - Rev 3: Limitations *

Maximum altitude for flap extension:

46
Q

767 Flt Man - Rev 3: Limitations

(T/F): The standby altimeter is sufficient to meet altimeter accuracy requirements of RVSM.

47
Q

767 Flt Man - Rev 3: Limitations

Max allowable “in-flight” difference between Capt and FO altitude displays for RVSM:

48
Q

767 Flt Man - Rev 3: Limitations

Max allowable “on-the-ground” difference between Capt and FO altitude displays for RVSM:

FIELD ELEVATION
at Sea Level
at 5000’
at 10000’

A

FIELD ELEVATION: Max: Capt/FO Max: Capt/FO/FE**

  • at Sea Level 40’ 75’
  • at 5000’ 45’ 75’
  • at 10000’ 50’ 75’

**FE = Field Elevation

49
Q

767 Flt Man - Rev 3: Limitations

(T/F): HUD takeoff guidance is valid only when
conducted on low visibility facility runways
(CAT III) with ILS critical area procedures in
operation.

50
Q

767 Flt Man - Rev 3: Limitations

For HUD Takeoffs, at what RVR must the Flight Path Vector (FPV) be caged?

A

During TOs < 500’ / 150m RVR (actual or reported visibility),

51
Q

767 Flt Man - Rev 3: Limitations

For takeoff requiring the use of the HUD takeoff guidance mode, the maximum crosswind
is?

52
Q

767 Flt Man - Rev 3: Limitations

For approach requiring the use of the EFVS to continue beyond the final approach fix,
the maximum crosswind is?

53
Q

767 Flt Man - Rev 3: Limitations

For approach requiring the use of EFVS to continue beyond the final approach fix, the maximum final course offset from the runway is?

54
Q

767 Flt Man - Rev 3: Limitations

For approach requiring the use of EFVS to continue beyond the final approach fix, what vertical modes are authorized?

A

Only VNAV or Glideslope Track is authorized.

Note: (V/S or FPA vertical navigation modes
are not authorized.)

55
Q

767 Flt Man - Rev 3: Limitations

Max Fuel Capacity - either main tank:

A

40,267 lbs (approx 40,000 lbs)

56
Q

767 Flt Man - Rev 3: Limitations

Max Fuel Capacity - Center fuel tank:

A

79,730 lbs (approx 80,000 lbs)

57
Q

767 Flt Man - Rev 3: Limitations

Max Total Fuel Capacity for the 767:

A

160,264 lbs (approx 160,000 lbs)

58
Q

767 Flt Man - Rev 3: Limitations

(T/F): Do not reset a tripped fuel pump or fuel pump control circuit breaker.

59
Q

767 Flt Man - Rev 3: Limitations

What is the Standard “Fuel Usage I” (No center tank fuel) procedure?

A

“Fuel Usage I” procedure:

  • Tank-to-engine fuel feed for takeoff and landing.
  • All operable main tank boost pumps on.
  • Crossfeed valve(s) closed**.

**NOTE: Crossfeeds are only opened for Min-Fuel Ops
and for fuel balancing.

60
Q

767 Flt Man - Rev 3: Limitations

What is the Standard “Fuel Usage II” (Fuel in center tank) procedure?

A

“Fuel Usage II” procedure:

  • Center tank fuel for all operations.
  • All operable boost pumps on.
  • Crossfeed valve(s) closed**
  • When Center tank fuel is depleted, use
    “FUEL USAGE I” procedure.

**NOTE: Crossfeeds are only opened for Min-Fuel Ops
and for fuel balancing.

61
Q

767 Flt Man - Rev 3: Limitations *

Define “Fuel Imbalance” in the 767:

A

Fuel Imbalance in the 767:

> 2,500 lb - when total main tank fuel is < 48,000 lb.
1,500 lb - when total main tank fuel is > 48,000 lb.

62
Q

767 Flt Man - Rev 3: Limitations

The center tank may contain up to 22,050 pounds of fuel with less than full main tanks provided:

A
  • Center tank fuel plus actual ZFW < Max ZFW.

* CG limits are observed.

63
Q

767 Flt Man - Rev 3: Limitations *

Avoid WX radar operation in _____, or within ______ of any personnel, fueling operations, or a fuel spill.

A
  • A hangar
  • 50 feet (15.25 meters)

**NOTE: The hangar restriction does not apply to
the weather radar test mode.

64
Q

767 Flt Man - Rev 3: Limitations

(T/F): Pilots are authorized to deviate fromtheir current ATC clearance to the extent necessary to comply with a TCAS resolution advisory (RA).

FedEx 767 Limits & Phase Ones (2 decks)

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