Other AOM Ch 3 limitations

Question 1

Mach Trim Inoperative Max Speed

Answer 1

NG: 280 KIAS/.82M
CL: .74M

Question 2

VB (at and below 15000)

Answer 2

250 kt

Question 3

VB (above 15000)

Answer 3

NG: 280/.76M
CL: 280/.73M

Question 4

Max tire speed

Answer 4

195 kt

Question 5

Min recommended plowed or usable runway width

Answer 5

100 ft

Question 6

Takeoff or landing is not authorized if the most current friction Mu report includes a value of xx or less for any section of the runway.

Answer 6

Takeoff or landing is not authorized if the most current friction Mu report includes a value of 20 or less for any section of the runway.

Question 7

RCC 6/Dry; Max Steady xWind
Takeoff
Landing

Answer 7

Takeoff: 35(25 if narrow runway)
Landing: 35(25 if narrow runway)

Question 8

RCC 5/Good; Max Steady xWind
Takeoff
Landing

Answer 8

Takeoff: 25
Landing: 35(25 if narrow runway)

Question 9

RCC 1/Poor; Max Steady xWind
Takeoff
Landing

Answer 9

Takeoff: 10 (Medium-Poor CL:7)
Landing: 10

Question 10

RCC 0/Nil; Max Steady xWind
Takeoff
Landing

Answer 10

Not Authorized

Question 11

Sideslip only landings (no crab) are not recommended when crosswind component exceeds xx kt.

Answer 11

Sideslip only landings (no crab) are not recommended when crosswind component exceeds 15 kt.

Question 12

(split scimitar winglet aircraft) bank angles greater than x.x deg will strike the ground

Answer 12

(split scimitar winglet aircraft) bank angles greater than 8.8 deg will strike the ground

Question 13

Max headwind component for HGS AIII mode is xx kt.

Answer 13

Max headwind component for HGS AIII mode is 25 kt.

Question 14

Use peak gust wind velocity for xx component computations.

Answer 14

Use peak gust wind velocity for TW component computations.

Question 15

Max wind for TO/Landing is xx kt steady and xx kt peak gusts.

Answer 15

Max wind for TO/Landing is 50 kt steady and 70 kt peak gusts.

Question 16

Max external air pressure xx psi.

Answer 16

Max external air pressure 60 psi.

Question 17

The xxxxxx fan must be off when operating at or above xx000 ft.

Answer 17

The gasper fan must be off when operating at or above 10000 ft. (unless QRH procedure directs otherwise)

Question 18

FLT ignition required?

Answer 18

In or in the vicinity of: Moderate or Greater Precipitation

Question 19

Min altitude for autopilot/autothrottle disengagement during approach:
xx ft below DA/DDA,
but no less than xx ft AGL.

Answer 19

Min altitude for autopilot/autothrottle disengagement during approach:
50 ft below DA/DDA,
but no less than 50 ft AGL.

Question 20

Battery voltage range xx-xx volts

Answer 20

Battery voltage range 22-30 volts

Question 21

FFOD, operate the engines at or near idle, after rollback, for a minimum of xxxx minutes prior to applying takeoff thrust.

Answer 21

FFOD, operate the engines at or near idle, after rollback, for a minimum of five minutes prior to applying takeoff thrust.

Question 22

Starter Duty Cycle
NG: x minutes ON, xx seconds OFF
CL: x minutes ON, xx seconds OFF
x minutes ON, x minutes OFF next and subsequent attempts

Answer 22

Starter Duty Cycle
NG: 2 minutes ON, 10 seconds OFF
CL: 2 minutes ON, 20 seconds OFF
2 minutes ON, 3 minutes OFF next and subsequent attempts

Question 23

Starter Motoring: xx minutes

Answer 23

Starter Motoring: 15 minutes

Question 24

Takeoff and landing are not authorized if either thrust reverser is inoperative and the runway is contaminated with clutter or the braking action is less than x-xxxx.

Answer 24

Takeoff and landing are not authorized if either thrust reverser is inoperative and the runway is contaminated with clutter or the braking action is less than 5-GOOD.

Question 25

Wait xx seconds between APU start attempts except: (CL: after xxx aborted start attempts, a xxxx-minute cooling period is required prior to a xxxxx start attempt.) If the APU fails to start after the xxxxx attempt, call Dx/Mx. Do not attempt a xxxxxx start.

Answer 25

Wait 90 seconds between APU start attempts except: (CL: after two aborted start attempts, a five-minute cooling period is required prior to a third start attempt.) If the APU fails to start after the third attempt, call Dx/Mx. Do not attempt a fourth start.

Question 26

NG: Wait at least x minutes after the APU GEN OFF BUS light extinguishes prior to positioning the battery switch OFF. CL: Wait at least xx seconds after APU shutdown prior to positioning the battery switch OFF.

Answer 26

NG: Wait at least 2 minutes after the APU GEN OFF BUS light extinguishes prior to positioning the battery switch OFF. CL: Wait at least 20 seconds after APU shutdown prior to positioning the battery switch OFF.

Question 27

CL: The APU bleed air switch should be OFF for at least xxx minutes before the APU is shut down.

Answer 27

CL: The APU bleed air switch should be OFF for at least two minutes before the APU is shut down.

Question 28

Authorized TO flap settings NG: x,x,x,x,x CL: x,x,x

Answer 28

Authorized TO flap settings NG: 1,5,10,15,25 CL: 1,5,15

Question 29

Do not operate the aircraft at speeds in excess of xxx kt at weights over xxx,000 lb if the speedbrake wing load alleviation system is inoperative [7W]

Answer 29

Do not operate the aircraft at speeds in excess of 320 kt at weights over 143,000 lb if the speedbrake wing load alleviation system is inoperative [7W]

Question 30

Max allowable on-the-ground altimeter differences for RVSM operations NG: Field Elevation; CA/FO diff; CA or FO ; field diff 0-5000; xx ft; xx ft 5001-10000; xx ft; xx ft

Answer 30

Max allowable on-the-ground altimeter differences for RVSM operations NG: Field Elevation; CA/FO diff; CA or FO ; field diff 0-5000; 50 ft; 75 ft 5001-10000; 60 ft; 75 ft

Question 31

FD or AP is required for RNAV approaches with RNP less than x.x NM.

Answer 31

FD or AP is required for RNAV approaches with RNP less than 1.0 NM.

Question 32

AP is required for RNAV approaches with RNP less than x.x NM.

Answer 32

AP is required for RNAV approaches with RNP less than 0.3 NM.

Question 33

Allowed fuel types: x,x,x,x,x

Answer 33

Allowed fuel types: Jet A, A1, JP-5, JP-8, F-24

Question 34

Max fuel imbalance (taxi, takeoff, flight, landing) xxxx lb

Answer 34

Max fuel imbalance (taxi, takeoff, flight, landing) 1000 lb

Question 35

What is done before an aircraft is towed forward?

Answer 35

Both engines will be shut down and hydraulic system A depressurized before the aircraft is towed forward.

Question 36

Takeoff with anti-skid inoperative is only allowed xx xxx xxxxxxx.

Answer 36

Takeoff with anti-skid inoperative is only allowed on dry runways.

Question 37

[800] Carbon brakes are limited to a fixed time of xx minutes for ground turnaround if the maximum quick turnaround weight is exceeded.

Answer 37

[800] Carbon brakes are limited to a fixed time of 48 minutes for ground turnaround if the maximum quick turnaround weight is exceeded.

Question 38

Autobrakes, if operable, must be used: Any runway RCC x-xxxx or less, or Reported visibility less than xxxx RVR (or x/x mile), or Landing with less than flaps xx. Or landing in xxxxxx/xxxxx xxxxxxxxx or when xxxxxxx brake application due to rudder input may be affected.

Answer 38

Autobrakes, if operable, must be used: Any runway RCC 5-GOOD or less, or Reported visibility less than 4000 RVR (or 3/4 mile), or Landing with less than flaps 30. Or landing in strong/gusty crosswinds or when uniform brake application due to rudder input may be affected.

Question 39

iPad is to be recharged when the battery displays xx% or less. Any flight over x hours requires a minimum of xx % battery.

Answer 39

iPad is to be recharged when the battery displays 20% or less. Any flight over 6 hours requires a minimum of 80 % battery.