Limitations Flashcards

1
Q

Max operating Pressure Altitude

A

41,000 feet

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2
Q

Max TO/LDG Pressure Altitude

A

8400 feet

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3
Q

Flap Up flight maneuvering load

A

+2.5G / -1.0G

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4
Q

Flaps Extended flight maneuvering load

A

+2.0G / 0G

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5
Q

Mach Trim Inoperative Maximum speed

A

280 KIAS / .82 Mach

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6
Q

Turbulent Air penetration speed below 15,000 feet

A

250 kt

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7
Q

Turbulent Air penetration speed above 15,000 feet

A

280 KIAS / .76 Mach

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8
Q

Max tire speed for -700 and -800/MAX

A

NG: 195 / MAX: 205

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9
Q

Runway slope limit

A

+/- 2%

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10
Q

Braking Action NIL limitations for Takeoff/Landing

A

will not be attempted if ANY portion of the runway is reported NIL

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11
Q

Braking Action NIL limitations for Taxiing

A

will NOT be attempted on the portion of the taxiway reported as NIL

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12
Q

Takeoff/Landing not authorized if runway friction MU report includes a value of ________?

A

20 or Less

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13
Q

Dispatch to/from runways less than ____ is not allowed if _______ and ________are inoperative

A

45m (147.6ft)
-rudder pedal nose wheel steering inoperative
-one thrust reverser inoperative

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14
Q

if an alternate is available with runway at least 47m wide, Diversion to alternate shall be performed with

A

-jammed/resticted flight controls
-TE Flap asym
-LE flap/slat asym
-loss of A or B hydraulics

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15
Q

Takeoff Crosswind limits with RCC 6

A

35kts

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16
Q

Landing Crosswind limits with RCC 6

A

35kts unless runway is width limited under 47m (147 feet) then it is 25kts

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17
Q

Takeoff/Landing tailwind limits with RCC 6

A

10kts (15kts with RCC5 or greater at SJO/MROC

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18
Q

Bank angles greater than ____degrees will result in ventral strake strike

A

8.8 degrees

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19
Q

Do not use sideslip(wing low) crosswind landing technique alone when crosswinds exceed ____

A

15kts

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20
Q

In the MAX, limit thrust to setting normally used for taxi when crosswinds are greater than _____

A

43 kts

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21
Q

In the MAX, limit engine thrust to _______when winds greater than _______

A

idle, 58kts

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22
Q

Maximum headwind component for HGS AIII mode is

A

25 kts

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23
Q

Max wind velocity for takeoff and landing is _____steady and _____peak gusts

A

50 kts steady and 70 kts peak gust

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24
Q

Can a flight be dispatched on revenue flights if all Lavatories are inop

A

NO

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25
Safety relief differential pressure
9.1
26
Max cabin pressure differential pressure for takeoff/landing
.125
27
When engine bleed air switches on, do not operate the air-conditioning PACKs in
HIGH for takeoff, approach or landing
28
Can you use a PACK with a pre-conditioned air source
No
29
If aircraft must remain unpressurized, can the aircraft be dispatched on revenue flights
No
30
In flight, In the MAX, how many PACKS may be powered by one engine. bleed source
2 PACKS
31
Engine Ignition must be ON for
heavy RA in, anti-ice, Takeoff Landing (+RATL)
32
Engine Anti Ice must be on for
=ground and flight operations when icing cond exist, except during climb and cruise below -40deg SAT =before and during descent in all icing conditions below -40deg SAT
33
Can you hold in icing conditions with the flaps extended
No
34
Do not operate wing anti-ice when OAT is above
10deg C
35
Do not use wing anti-ice as substitute for
deicing/anti-icing
36
Window heat inoperative max speed speed
250kts below 10,000 feet
37
Do not operate weather radar when
during fueling, near fuel spills, or people,
38
Can you use wing anti-ice for takeoff
No
39
How long turning on engine bleed air or APU bleed air following deicing
1 minute
40
Can you use aileron trim with while Autopilot is on
No
41
Minimum altitude for Autopilot engagement
1000 feet
42
Minimum altitude for autopilot disengagement during approach
50ft below DA/DDA but no less than 50ft AGL
43
On the ground in the NG, limit one generator operation to a maximum of ----AMPs
215
44
In the MAX, on the ground or in the air, limit one generator operation to a maximum of ----AMPs
215
45
TR voltage range
22-30 volts
46
battery voltage range
22-30 volts
47
How long to wait before removing AC power from the aircraft after shutting down the IRS?
30 sec
48
Can you reset a CB inflight?
YES, when QRH directed.
49
How long must you wait before resetting a CB
2 min for cooling purposes
50
Resetting a CB, not directed by QRH, can be done if
CA deems critical to safety of flight, waiting. 2 minutes for cooling, and only reset once
51
If reseting a CB in-flight, what else needs to happen
Maintenance notified and logbook entry must be made
52
Can you reset a CB on the ground?
No, unless maintenance has deemed it safe to reset
53
If tripped CB is not reset is logbook entry required
Yes, the fault must be entered
54
If tripped CB is reset by Flight Deck crew member, does logbook entry need to be made?
Yes, Info Only entry is made in the logbook with Maintenance Controllers name
55
Can you cycle a CB?
Yes, when directed by -QRH -Procedure -Maintenace Control coordinated and approved and logbook Info Only entry is made
56
In the MAX, after engine starts, oil temp must rise to at least -----degs before setting takeoff thrust
31deg C
57
Maximum ground start EGT in NG
725deg C
58
In the MAX, with TakeOff Thrust set, can you takeoff with Oil Pressure in the yellow band
No
59
If EEC in Alternate Mode, can you takeoff
Yes - Max power only -reduced thrust is not allowed -both EECs must be selected in Alternate
60
What conditions must engine Ignition be on for?
+RA, Anti ice, Takeoff, Landing in FLT for mod/sever. turbulence
61
In the NG can oil pressure readouts be in yellow band?
No, only in the white band
62
On first flight of the day, operate engines at Idle, after rollback for a minimum of --- minutes prior to applying takeoff thrust
5 min (recommended)
63
Prior to applying takeoff thrust, operate engines at idle, after rollback for a minimum ---- NG and -----MAX
NG: 2min MAX: 3min
64
Prior to shutdown, operate engines at or near idle for a minimum of ----NG and -----Max
NG: 1min MAX: 3min
65
What is recommendation for engines idle time prior to shutting down engines
3 min
66
NG starter duty cycle
2min ON 10 sec OFF between start attempts
67
MAX starter duty cycle
3 min ON 10 sec OFF between start attempts
68
NG - Fuel Off Motoring time limit
15min
69
MAX - Fuel Off Motoring time limit
5min. and minimum of 5min between first two extended motorings
70
Min oil quantity to depart from Non-Maintenance Base
NG / MAX 60 / 66
71
Min oil quantity to depart from Maintenance base
NG / MAX 70 / 70
72
When terminating, arrange for oil servicing when oil quantity is
NG / MAX <65 / <70 may cause low oil qty alerts during initial takeoff and climb
73
Thrust reverser inoperative limitations for takeoff or landing
not authorized if runway is contaminated with clutter or braking action is less the RCC 5 -Good
74
Max altitude for APU operations, electric only
41,000 feet
75
Max altitude for APU operations, bleed air only
17,000 feet
76
Max altitude for bleed air and electric
10,000 feet
77
How long to wait before APU start attempts?
90 secs
78
How many consecutive APU start attempts are allowed
3, then must call Maintenance. Do not attempt 4 starts
79
After APU GEN OFF BUS light extinguishes, how long must you wait before turning Battery Switch OFF in the NG / MAX
NG / MAX 2min / 5 min
80
How long must you wait after APU start before operating as a bleed air source
2 min
81
Do not extend the flaps above what altitude
20,000
82
Limit associated with Alternate Flap Duty Cycle
-one cycle then 5 min off -cycle is 0 to 15, then back to 0
83
Alternate Flaps Position Switch must be in ----- position for ----- before reversing the direction of flap movement
OFF, 15 sec
84
Do not extent speedbrake lever beyond
FLIGHT DETENT
85
Do not use speedbrakes below
1000 feet AGL
86
In flight, do not use speedbrakes with flaps greater than
Flaps 10
87
With wing load alleviation system in operative, do not operate the aircraft at speeds in excess of ____kts at weights over ______ if
320kts at weights over 143,000 lbs
88
Maximum allowed inflight difference between CA and FO altimeters for RVSM is
200ft
89
From Sea Level to 5000' Maximum allowable on the ground altimeter difference for RVSM operations between CA and FO
50 feet
90
From 5001' to 10,000 feet Maximum allowable on the ground altimeter difference for RVSM operations between CA and FO
60 feet
91
From 5001' to 10,000 feet Maximum allowable on the ground altimeter difference for RVSM operations between CA or FO and field elevation
75 feet
92
From Sea Level to 5000 feet Maximum allowable on the ground altimeter difference for RVSM operations between CA or FO and field elevation
75 feet
93
If "UNABLE REQD NAV PERF-RNP" message is active, do not use
LNAV
94
What is required for RNAV operations with an RNP of 1.0nm or less
FD or Autopilot
95
What is required for RNAV approaches with RNP less than .3NM?
Autopilot is required
96
When can VNAV be engaged on GoAround or Missed approach?
once flaps are fully retracted
97
Max fuel tank temperature
+49deg
98
Min fuel tank temperature
-37deg
99
Fuel tanks must be full if center tank quantity is ----
greater than 1,000 lbs
100
center tank fuel pump switches must be on when center tanks have ----
more than 1,000 lbs
101
For ground operations, Center tanks fuel pump switches must not be positioned ON unless center tank fuel quantity exceeds
1000 lbs
102
Can you transfer fuel with passengers aboard.
Yes, provided 2000 is the minimum fuel in the tank being transferred from
103
If fuel in the tank being transferred from will drop below 2,000lbs , what needs to happen
passengers and non-essenential crew need to deplane
104
Center tanks must not be turned ON unless
crew is available to monitor for low pressure lights
105
Crew must not reset which CB
Fuel pump, Fuel pump control, Fuel quantity indicator circuit breakers
106
Landing gear extension airspeed limits
270kts
107
landing gear retraction airspeed limits
235kts
108
landing gear extended airspeed limit
320
109
Can you use auto brakes with anti-skid inop
No
110
Autobrakes must be used for landing when
-RCC is 5-Good or less -visibility less than 4000RVR or 3/4mile -if landing with less than Flaps 30
111
What auto brake setting is not allowed for use
1
112
-700 if discharge of fire suppression system, aircraft must land within ____
60min
113
-800/MAX: if discharge of fire suppression system, aircraft must land within ____
180min
114
Can a CB be reset in-flight?
Yes - when directed by QRH or CA deems necessary for safe conduct
115
Can CB be reset on the ground?
Yes - with Maintenance control coordination.
116
Logbook entry required with CB reset?
Yes. Info only. When coordinated with Maintenance Control, provide a name