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Boeing 757/767 > 757/767 Limitations > Flashcards

757/767 Limitations Flashcards

1
Q

Category for Circling Approaches

A

Category D

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2
Q

757-200 Category for Straight-in-Approaches

A

Category C

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3
Q

757-300-767 Category for Straight-in-Approaches

A

Category D

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4
Q

Maximum Operating Pressure Altitude - 757

A

42,000 feet

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5
Q

Maximum Operating Pressure Altitude - 767

A

43,100 feet

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6
Q

Maximum Takeoff/Landing Tailwind Component

A

757/767 15 knots

767-400 10 Knots

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7
Q

Maximum gear operating/extended speed

A

270/.82

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8
Q

Maximum alternate gear extension speed

A

250/.75

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9
Q

Severe Turbulence Penetration Airspeeds

A

10,000 feet and above 290/.78

Below 10,000 feet 250

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10
Q

Maximum Runway Slope

A

+/- 2%

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11
Q

What is a normal runway width?

A

148’ (45 meters) or greater

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12
Q

What is the minimum runway width for the 757?

A

100’ (30 meters)

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13
Q

What is the minimum runway width for the 767?

A

115’ (35 meters)

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14
Q

Takeoff from narrow runways (5)

A
  1. Nose wheel steering must be operative
  2. All Brakes must be operative
  3. Crosswind capability is diminished with thrust
    reverser or flight control deferrals.
  4. Reference crosswind guidelines
  5. Ensure V1 is greater than or equal to narrow
    runway calculated VMCG
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15
Q

Windshear Alert Prohibition

A

Takeoff with forward looking windshear warning alert annunciated is not approved.

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16
Q

Flaps 1 Takeoffs 757-300

A

Prohibited

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17
Q

To minimize wear on flap assembly, when extending flaps to positions 1 through 20, use placard speed minus 10 knots. Use placard limit speeds during flap retraction or when operating flaps in accordance with a non-normal procedure.

A

N/A

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18
Q

Crosswind Guidlines for takeoff and landing.

Runway condition code 6 “Dry”

A

Takeoff 40

Landing 40

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19
Q

Crosswind Guidlines for takeoff and landing.

Runway condition code 5 “Good”

A

Takeoff 25

Landing 40

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20
Q

Icing conditions exist on the ground and for takeoff when:

A

Outside air temperature is 10C or below

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21
Q

Icing conditions exist in flight when:

A

Total Air Temperature is 10C or below

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22
Q

Wing anti-ice use during takeoff

A

During takeoff don not use wing anti0ice until after the first power reduction.

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23
Q

On takeoff or missed approach, do not engage autopilot below

A

800 feet AGL

24
Q

Do not use FLCH

A

Do not use FLCH on final approach below 1000’ AFE

25
Q

Autopilot use prohibited below 100 feet RA at airpots pressure altitudes above

A

8400’

26
Q

Do not use aileron trim

A

With the auto pilot engaged.

27
Q

767-400 When coupled to an ILS without land 2 or Land 3 annunciated the autopilot must be disengaged prior to

A

descending below 100 feet RA

28
Q

Autolanding maximum allowable headwind

A

25 knots

29
Q

Autolanding maximum allowable tailwind

A

757-200 15 knots / 10 knots for CAT II/III

767 15 knots / 10 knots for CAT II/III

757-300 12 knots flaps 30
15 knots flaps 25
10 knots for CAT II/III

30
Q

Autolanding maximum crosswind

A

25 knots / 15 knots for CAT II/III

31
Q

Maximum / Minimum Glideslope Angle

A

Maximum 3.25 degrees

Minimum 2.50 degrees

32
Q

Minimum altitude for use of autopilot on approach:

A

ILS coupled approaches (No Autoland) 50’ AGL

Non-ILS approaches 50’ below MDA/DA

Autolanding Touchdown and Rollout

33
Q

Autolanding Notes:

Not authorized on runways with offset localizer.

A

N/A

34
Q

Autolanding Notes:

Autopilot control wheel and throttle mounted autothrottle disconnect switches must be fully operative.

A

N/A

35
Q

Autolanding Notes:

At 100’ AGL, autoland tolerances are:
+/- 5 knots of target
Zero to one dot high on glideslope
1/3 dot of localizer center

A

N/A

36
Q

Autolanding Notes:

Autoland Status Annunciator (ASA) Land 3
The autopilot system meets the applicable airworthiness and performance reliability requirements for a fail operational system for approach, landing, and rollout.

A

N/A

37
Q

Autolanding Notes:

Autoland Status Annunciator (ASA) Land 2
The autopilot system meets the applicable airworthiness and performance reliability requirements for a fail passive system for approach, landing, and rollout.

A

N/A

38
Q

Autolanding must be made using what flap settings

A

Flaps 25 or 30

39
Q

Autolanding Notes:

Two engines must be operating until 200’ RA. Below 200’ RA the ASA can only change to NO AUTOLAND. The approach may continue for engine failures that occur below 200’ RA.

A

N/A

40
Q

Autolanding Notes:

Autoland is not authorized if the maximum structural landing weight is exceeded.

A

N/A

41
Q

Autolanding Notes:

Autoland must be used when below CAT I weather conditions.

A

N/A

42
Q

In all cases other than autoland, The autothrottle must be disconnected not lower than:

A

50’ AGL

43
Q

Circuit breaker resets that are prohibited:

A

Fuel Boost Pump

Fuel Control

44
Q

Engine Start Selector to CONT

A

Severe Turbulence

Takeoff and Landings

45
Q

APU Starts

A

Three start attempts may be made followed by a 1 hour cooling period.

46
Q

APU Bleed Air

A

Do not use APU bleed air above 17,000’ MSL

47
Q

Minimum Oil Quantity for engine start

A

757-200 RR; 757-300; 767-400 18 quarts - ETOPS
16 quarts - NON ETOPS

757-200 PW; 767-300 15 quarts

48
Q

Inflight engine start may be accomplished with zero oil quantity as long as all other indications are normal.

A

N/A

49
Q

A significant drop in oil quantity is normal after engine start.

A

N/A

50
Q

Do not start APU during fueling operations following an APU automatic shutdown or failed start.

A

N/A

51
Q

APU starts: 757-200 RR; 757-300; 767-400

A

Allow 5 minutes cooling between start attempts

52
Q

APU starts: 767-300

A

Allow 1 minute cooling between start attempts

53
Q

Maximum Flap Extension Altitude

A

20,000 feet MSL

54
Q

Speed brake restriction

A

Do not use speed brakes in flight below 1,000’ AGL

55
Q

Max Tire Groundspeed

A

757; 767-300 195 knots

767-400 205 knots

56
Q

Brake Wear

A

Brake assembly must be replaced when brake wear indicator pins indicate flush or below flush with the parking brake set.

Boeing 757/767 (5 decks)

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