Limits

Question 1

Runway slope

Not Required

Answer 1

+/- 2%

Question 2

Maximum Takeoff and Landing Tailwind Component (including gusts)

Answer 2

15 knots

Question 3

Maximum Operating Pressure Altitude

Not required

Answer 3

(B757) 42,000 feet

(B767) 43,100 feet

Question 4

Maximum Takeoff and Landing Pressure Altitude

Not required

Answer 4

8400 feet
(B767: N335UP through N361UP) 9500 feet
(B757: N451UP through N470UP) 14,000 feet

Question 5

Maximum demonstrated crosswind Takeoff and Landing (including gusts)

Answer 5

(B757) 30 knots
(B767) 33 knots

Question 6

(B767) A 180 degree turns on runways with widths less than 148 ft (45m)

Answer 6

Are prohibited.

Permitted if Runway turn pad or taxiway is available.

Question 7

Avoid weather radar operation

Answer 7

in a hangar, or within 50 feet of fueling operations or a fuel spill.

Question 8

Turbulent air speed

Answer 8

290 kts/.78M, whichever is lower

Question 9

Maximum Taxi Weight

Not required

Answer 9

(B757) 251,000 lbs.

(B767: N301UP through N361UP and N362UP through N364UP) 409,000 lbs.

Question 10

Maximum Takeoff Weight

Not required

Answer 10

(B757) 250,000 lbs.

(B767: N301UP through N361UP and N362UP through N364UP) 408,000 lbs.

Question 11

Maximum Landing Weight

Not required

Answer 11

(B757) 210,000 lbs.

(B767) 326,000 lbs.

Question 12

Maximum Zero Fuel Weight

Not required

Answer 12

(B757) 200,000 lbs.
(B767 N301UP through N361UP) 312,300 lbs.
(B767 N362UP through N364UP) 309,000 lbs.

Question 13

On takeoff, do not engage autopilot below….

Answer 13

200 AGL.

Question 14

Reverse thrust is restricted to….

Answer 14

Ground use only.

Question 15

Backing the aircraft with use of reverse thrust……..

Answer 15

Is not permitted.

Question 16

(PW) Minimum oil temperature for takeoff is…..

Answer 16

50 degrees C.

Question 17

(RR) Minimum oil temp for advancing thrust lever is…

Answer 17

0 degrees C.

Question 18

The Maximum altitude with flaps extended….

Answer 18

20,000 ft.

Question 19

Maximum temperature for JET A…..

Answer 19

49 degrees C.

Question 20

Minimum Fuel Tank Temperatures…

Answer 20

(B757) Minus 45C or 3C above the freezing point of the fuel being used (whichever is higher).

(B767) 3C above the freezing point of the fuel being used.

Question 21

(B757) The maximum fuel imbalance between left and right main tanks for all operations….

Not required

Answer 21

1800 lbs.

Question 22

(B767) The maximum fuel imbalance between left and right main tanks for all operations….

Not required

Answer 22

Main tank fuel load
48,000 lbs or less…………2500 lbs.
48,000 to 79,800 lbs…….linear reduction to 1500 lbs.
79,800 lbs or greater…….1500 lbs.

Question 23

The center tank fuel pumps must be off for takeoff……………………..(AD 2002-19-52)

Answer 23

if center tank fuel is less than 5000 pounds with the aircraft readied for initial taxi.

Question 24

Both Center Tank Fuel Pump switches must be selected OFF when….. (AD 2002-19-52)

Answer 24

center tank fuel quantity reaches approximately 1000 pounds during climb, cruise or descent.

Question 25

Flaps 30 - 757

Answer 25

Not approved below 140.0
Required below 160.0