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Flashcards in B-737Aircraft Limitations: Deck (114)
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1

Runway Slope

+/-2%

2

Maximum Takeoff Tailwind Component

10 or 15 knots (Depending on ship number)

3

Maximum Landing Tailwind Component

10 knots

4

Maximum Autoland Headwind Component

25 knots

5

Maximum Takeoff and Landing X-wind Component

34 knots [w/ Winglets] / 36 knots [w/o Winglets]

6

Maximum Autoland Crosswind Component

15 knots

7

With the exception of flights between 80°W and 130°W ando/or flights between 120°E and 160°E, the operational limitation for the maximum flight operating latitude is:

82°N or 82°S

8

Maximum Operating Altitude

41,000 ft

9

Maximum Takeoff and Landing Altitude

8,400 ft pressure altitude

10

The maximum allowable in-flight difference between CA & FO alt displays for RVSM ops

200 feet

11

The max alt display dif on-the-ground for RVSM ops are: Max Dif between CA & FO

50 feet

12

The max alt display dif on-the-ground for RVSM ops are: Max Dif between (CA or FO) & Field Elevation

75 feet

13

Max Allowable Load Factor: Flaps Up

+2.5g to -1.0g

14

Max Allowable Load Factor: Flaps DOWN

+2.0g to 0.0g

15

Largest Dimensions: Nose to tail

129’6”

16

Largest Dimensions: Wingtip to wingtip

117’10”

17

Largest Dimensions: Main Gear width (L to R)

18’8”

18

Largest Dimensions: Tail Height

41’2”

19

Largest Dimensions: (1) Wingtip turn radius (2) Minimum width of pavement for 180° turn

(1) 77.9’ (2) 79.6’

20

Maximum Zero Fuel Weight

138,300 lbs. (138,276 lbs.)

21

Maximum Ramp Weight

174,700 lbs. (174,670 lbs.)

22

Maximum Taxi Weight

174,700 lbs.

23

Maximum Takeoff Weight

174,200 lbs. (174,170 lbs.)

24

Maximum Landing Weight

146,300 lbs. (146,275 lbs.)

25

VFE: 1

250

26

VFE: 2

250

27

VFE: 5

250

28

VFE: 10

210

29

VFE: 15

200

30

VFE: 25

190