Limitations/Procedures

Question 1

Minimum hydraulic pressure required before engine start?

Answer 1

2800 psi

Question 2

Flap 1 VFE

Answer 2

250 kt CAS

Question 3

Flap 2 VFE

Answer 3

250 kt CAS

Question 4

Flap 5 VFE

Answer 4

250 kt CAS

Question 5

Flap 10 VFE

Answer 5

210 kt CAS

Question 6

Flap 15 VFE

Answer 6

200 kt CAS

Question 7

Flap 25 VFE

Answer 7

190 kt CAS

Question 8

Flap 30 VFE

Answer 8

175 kt CAS

Question 9

Flap 40 VFE

Answer 9

162 kt CAS

Question 10

Maximum Landing Gear Extension Speed

Answer 10

270 kt CAS / 0.82 M

Question 11

Maximum Landing Gear Retraction Speed

Answer 11

235 kt CAS

Question 12

Maximum Landing Gear Extended Speed

Answer 12

320 kt CAS / 0.82 M

Question 13

Turbulence Penetration Speed

Answer 13

280 kt IAS / 0.76 M

Question 14

Maximum Operating Altitude

Answer 14

41,000 ft

Question 15

Maximum Take-off and Landing Altitude

Answer 15

8,400 ft

Question 16

Maximum allowable in-flight difference between Capt & F/O altitude displays for RVSM operations

Answer 16

200 ft

Question 17

Maximum difference between Capt or F/O altimeter & field elevation

Answer 17

75 ft

Question 18

Maximum difference between Capt & F/O altimeter with field elevation from Sea Level to 5,000 ft

Answer 18

50 ft

Question 19

Maximum difference between Capt & F/O altimeter with field elevation from 5,001 to 10,000 ft

Answer 19

60 ft

Question 20

Minimum runway width?

Answer 20

30m

Question 21

Sideslip only (zero crab) landings not permitted with crosswinds above : (F15 / F30 / F40)

Answer 21

F15 - 15 kt / F30 - 18 kt / F40 - 21 kt

Increase these numbers by 2 knots for non-winglet aircraft

Question 22

Maximum tailwind component for take-off & landing

Answer 22

10 kt

Question 23

Runway slope limits

Answer 23

+/- 2%

Question 24

G-Load limits, flaps up

Answer 24

+2.5 g to -1.0 g

Question 25

G-Load limits, flaps down

Answer 25

+2.0 g to 0.0 g

Question 26

Maximum Dry snow depth for takeoff

Answer 26

4" / 101.6 mm

Question 27

Maximum Standing water, slush or wet snow depth for operation

Answer 27

0.5" / 12.7 mm

Question 28

Operation on contaminated / slippery runways with ATM

Answer 28

Prohibited

Question 29

Maximum Landing Weight

Answer 29

65,317 kg

Question 30

Maximum cabin differential pressure (relief valves)

Answer 30

9.1 psi

Question 31

Minimum autopilot engagement height on take-off

Answer 31

Jet2.com = 1,000ft Boeing = 400 ft

Question 32

Engine TAI must be on when...

Answer 32

Icing conditions exist or are anticipated, except during climb and cruise when SAT is below -40 degrees Celsius

Question 33

MUH for single channel autopilot operation

Answer 33

158 ft AGL

Question 34

Starter duty cycle maximum

Answer 34

2 minutes

Question 35

Minimum time between start attempts (starter duty cycle)

Answer 35

10 seconds

Question 36

Oil temperature operation between 140 & 155 degrees Celsius limited to...

Answer 36

45 minutes

Question 37

Engine Ignition required for (4 conditions)

Answer 37

* Take-off * Landing * Operation in heavy rain * Anti-Ice operation

Question 38

APU bleed + electrical load maximum altitude

Answer 38

10,000 ft

Question 39

APU bleed maximum altitude

Answer 39

17,000 ft

Question 40

APU electrical load maximum altitude

Answer 40

41,000 ft

Question 41

APU starter duty cycle

Answer 41

On ground maximum 3 start attempts followed by 15 minutes cool down

Question 42

Maximum flap extension altitude

Answer 42

20,000 ft

Question 43

Minimum speedbrake use height in flight

Answer 43

Less than 1,000 ft radio altitude

Question 44

Maximum fuel loading

Answer 44

20,896 kg

Question 45

Maximum fuel imbalance between main tanks 1 & 2

Answer 45

453 kg

Question 46

What call is required after flap retraction during an EFATO?

Answer 46

"LVL change, bug up, max continuous thrust"

Question 47

ATM prohibited for (4 situations)...

Answer 47

1) One or more anti-skid units inop 2) Runway contaminated with snow, slush, ice or standing water 3) Potential windshear conditions exist 4) When EEC is in ALTN mode

Question 48

Bank angle limit until reaching V2 + 15?

Answer 48

15º

Question 49

Bank angle must be limited to 15º until which speed?

Answer 49

V2 + 15

Question 50

What does the bottom of the amber bar on the PFD speed tape represent?

Answer 50

* When flaps are UP - 1.3g margin to high speed buffet * When flaps not UP - Placard speed for next normal flap setting | 1.3g occurs at approx 40º of bank in level flight (25º + 15º overshoot)

Question 51

What does the top of the lower amber bar on the PFD speed tape represent?

Answer 51

Below approx 20,000ft: 1.3g margin to stick shaker Above approx 20,000ft: 1.3g margin to low speed buffet | 1.3g occurs at approx 40º of bank in level flight (25º + 15º overshoot)

Question 52

When is the low speed amber bar displayed?

Answer 52

* After first flap retraction on take off Or * When a valid Vref is entered

Question 53

What conditions require ABORTED ENGINE START NNC?

Answer 53

* The N1 or N2 does not increase or increases very slowly after EGT increases * There is no oil pressure indication by the time the engine is at stable idle * The EGT does not increase by 15 seconds after the FUEL CONTROL lever is moved to IDLE detent * The EGT quickly nears or exceeds the start limit

Question 54

To what speed is the speed bug automatically driven on a G/A and what does it represent?

Answer 54

Target airspeed for current flaps at MTOW | 172 knots F15 / 202 knots F1

Question 55

How many spools does the CFM56 have?

Answer 55

2 spools

Question 56

What is the source of pressurised air on the 737?

Answer 56

* Engine bleed air (5th or 9th stages) * APU bleed air * External air

Question 57

Push and Park | Briefing / Calculation requirements

Answer 57

* Briefing should be re done * Calculation **must** be re done