Limitation 737

Question 1

Runway slope

Answer 1

-/+ 2

Question 2

HF radios

Answer 2

Dont operate refueling

Question 3

Altitude Display Limits for RVSM Operations

Answer 3

Max Difference Between Captain & F/O

Sea level to 5000 feet : 50 feet
5001 to 10.000 feet :60 feet

Question 4

Altitude Display Limits for RVSM Operations 2

Max Difference Between Captain or F/O & Field Elevation

Answer 4

Sea level to 5000 feet : 75 feet
5001 to 10.000 feet :75 feet

Question 5

The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is

Answer 5

200 feet

Question 6

The maximum cabin differential pressure (relief valves) is

Answer 6

9,1 psi

Question 7

Airplanes operating with EASA Certification: The Minimum Use Height (MUH) for single channel autopilot operation is defined as—— AGL.

Answer 7

158 feet AGL

Question 8

Airplanes operating with EASA Certification – Maximum allowable wind speeds, when conducting a dual channel Cat II or Cat III landing predicated on autoland operations, are: headwind
Cross, tailwind

Answer 8

Headwind 25 knots
Crosswind 20 knots
Tailwind 10 knots

Question 9

Maximum and minimum glideslope angles for autoland are ___degrees and ___ degrees respectively.

Answer 9

3.25

2.5

Question 10

Autoland capability may only be used with flaps

Answer 10

30 or 40 and both engines operative.

Question 11

Airplanes operating with EASA Certification: Autoland capability may only be used with flaps 30 with one engine operative and

Answer 11

only for DH at or above 50 feet.

Question 12

Do not use LVL CHG on final approach below

Answer 12

1000 feet AGL

Question 13

Engine ignition must be on for:

Answer 13

• takeoff • landing • operation in heavy rain • anti-ice operation.

Question 14

Operation with assumed temperature reduced takeoff thrust is not permitted with

Answer 14

Antiskid inoperative

Question 15

APU bleed valve must be closed when:

Answer 15

• ground air connected and isolation valve open
• engine no. 1 bleed valve open
• isolation and engine no. 2 bleed valves open.

Question 16

After three consecutive aborted start attempts,________ minute cooling period is required.

Answer 16

a fifteen

Question 17

When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow________ after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch

Answer 17

15 seconds

Question 18

Maximum tank fuel temperature is

Answer 18

49°C

Question 19

Minimum tank fuel temperature prior to takeoff and inflight is___, or 3°C above the fuel freezing point temperature, whichever is higher.

Answer 19

–43°C

Question 20

Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero. Random fuel imbalance must not exceed ______ for taxi, takeoff, flight or landing.

Answer 20

453 kg

Question 21

Main tanks 1 and 2 must be full if center tank contains more than…

Answer 21

453 kgs

Question 22

What is the maximum altitude with flaps extended?

Answer 22

20000 feet

Question 23

Flap 1 Speed Limit

Answer 23

250 kt

Question 24

Flap 2 Speed Limit

Answer 24

250 Kt

Question 25

Flap 5 Speed Limit

Answer 25

250 Kt

Question 26

Flap 10 Speed Limit

Answer 26

210 kt

Question 27

Flap 15 Speed Limit

Answer 27

200 Kt

Question 28

Flap 25 Speed Limit

Answer 28

190 kt

Question 29

Flap 30 Speed Limit

Answer 29

175 kt

Question 30

Flap 40 Speed Limit

Answer 30

162 Kt

Question 31

Landing Gear Extend Speed Limit

Answer 31

270 kt- 0,82m

Question 32

Landing Gear Retract Speed Limit-
Extended Limit-

Answer 32

235 kt
320 kt - 0,82m.