Limitations

Question 1

Fail passive x wind
fail operational x wind

Answer 1

20 kts
25 kus

Question 2

• When GA during autoland
• CAT III [DH<50 or no DH] LAND 3 changes to LAND 2 or ANTISKID INOP
• ENG failure
• autothrottle disengage

Answer 2

-A/P disengage, A/P steady red, ILS/GLS failure or deviation alert, FLARE not armed or NO AUTOLAND
- Revert to DH > 50’ or GA above 200’ AGL [fail operational
- GA above 200’ AGL [fail operational], or manual GA [fail passive]
- continue manual thrust

Question 3

Approach discontinue 1000’ AGL

Answer 3

When RVR is below required for approach being flown

Question 4

runway slope
minimum runway width and taxi width
max operating altitude
maximum take off and landing altitude

Answer 4

2.0%
30m (down to 26m after careful judgement of commander) and 13m
41.000 feet
8.400 feet pressure altitude

Question 5

maximum precipitation depth on runway for takeoff and landing
- dry snow
- standing water, wet snow, slush

Answer 5

102mm
13mm

Question 6

turbulence air penetration speed

Answer 6

280 KIAS, .76M WHICHEVER LOWER

Question 7

reducing crosswind limitation

Answer 7

reduce crosswind limit by 1kts per 1 meter to a minimum of 10 knots when runway width < 40m

Question 8

Dry/Wet runway
- for landing reduce crosswind on wet or contaminated runway whenever asymmetrical thrust used
- manual landings sideslip only landing not permitted when:

Answer 8

• reduce by 5 kts
• crosswind components in excess of 15 kts

Question 9

max allowable in-flight difference altitude captain and FO for RVSM

Answer 9

200 feet

Question 10

max allowable on ground altitude difference captain and FO

MAX difference between captain or FO and Field elevation

Answer 10

Sea level: 50 feet,
5000’: 60 feet
MAX difference: 75 feet

Question 11

max cabin pressure differential
either one or both eng bleed on:

Answer 11

9.1 psi
Do NOT operate air conditioning packs in HIGH for takeoff, approach or landing

Question 12

aileron trim ap on
min altitude AP

Answer 12

prohibited
do NOT engage below 400’ AGL,
737-700 single channel AP OPS: 140 feet
737-800 single channel AP OPS: 158 feet
737-8 single channel AP OPS: 111 feet

Question 13

LVL CHG prohibited

Answer 13

on final approach below 1000 feet AFE

Question 14

auto land
- glide slope
- flaps

Answer 14

between 2.5 and 3.25
flaps 30 and 40, 40 recommended

Question 15

coms
- operate hf
- frequencies prohibited during flights

Answer 15

• NOT during refueling ops
• 29.489 and 29.490 MHZ

Question 16

Use of Flight Deck Auxiliary Power Outlets

Answer 16

Only for approved EFB devices

Question 17

Eng ignition

Answer 17

TO, LDG, operation in heavy rain and anti-ice operation

Question 18

Assumed temperature reduced TO thrust not permitted

Answer 18

when antiskid is iNOP

Question 19

Reverse thrust prohibited

Answer 19

intentionally in flight, for backing up the airplane, do not attempt GA after thrust reverser deployment upon landing

Question 20

APU
- after 3 attempted starts
- when ready for bleed air source
- when APU bleed valve must be closed

Answer 20

• cool for 15 minutes
• when APU is running for 2 min
  when:
• ground air connected and isolation valve open
• engine no 1 bleed valve open
• engine no 2 and isolation valve open

Question 21

APU
- APU bleed valve at ENG start
- max altitude

Answer 21

• APU bleed valve may be opened, but NO thrust above IDLE
• electrical load + APU bleed: 10.000 feet
• only APU bleed: max 17.000 feet
• only electrical load: max 41.000 feet

Question 22

Flight Controls
- max alt with flaps extended
- holding in ice condition
- speed brake in flight
- Speed brake MAX

Answer 22

• 20.000 feet
• prohibited with flaps
• MAX flight detent, do not deploy in flight at radio altitude less than 1000 feet
• do not extend in flight beyond ARMED detent with Flaps 40 selected

Question 23

Flight Controls
- rapid and large alternating control inputs
- flap 15 landing

Answer 23

• prohibited
• flap 15 only when required by non normal

Question 24

Alternate flap duty
- after using alternate flap position switch
- after complete extend/retract

Answer 24

• allow 15 seconds to avoid damage to alternate flap motor clutch
• allow 5 min cooling

Question 25

ADIRU allignment

Answer 25

at latitudes above 78 degrees 15 minutes must NOT be attempted

Question 26

QFE selection

Answer 26

prohibited

Question 27

• intentional dry running center tank
• in flight, tripped fuel pump or fuel pump control circuit breaker

Answer 27

• prohibited
• do NOT reset

Question 28

FUEL Temp
- max temperature
- min fuel temp

Answer 28

• max 49 DEG
• min -43 Deg or 3 Deg above the fuel freezing point (-47) whichever is higher

Question 29

random fuel imbalance
- when center tank fueling

Answer 29

must NOT exceed 453 KG for taxi, takeoff, flight or landing
- main tanks must be full

Question 30

GPWS - Look-ahead terrain alerting
- not to use for navigation
- when NOT use look-ahead terrain alerting and terrain display function

Answer 30

• terrain display
• within 15nm of takeoff, approach or landing at an airport or runway not contained in GPWS database

Question 31

Engine warm up time/ cool down time

Answer 31

2 min and increase in oil temp (3 min for MAX at 31 DEG oil temp or above) or 5 min when ENG has been off for more than 4 hours
3 min cool down

Question 32

Speedbrake with F40 (MAX)

Answer 32

Prohibited!

Question 33

MAX
crosswind greater than 43 KIAS
- when wind greater than 58 KIAS

Answer 33

Limit thrust to normal thrust setting for taxi
- except t/o thrust on runway, limit thrust to IDLE