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POH 3 - Limitations Flashcards

1
Q

Max x wind component for takeoff and landing

A

27 knots

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2
Q

Max x wind for landing Cat II

A

15 knots

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3
Q

Max headwind for landing Cat II

A

16 knots

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4
Q

Max tailwind for takeoff and landing

A

10 knots

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5
Q

Max operating altitude

A

41,000 feet

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6
Q

Except in emergency, takeoff or landing will not be attempted whenever peak wind value exceeds

A

50 knots

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7
Q

Max altitude for single pack ops

A

31,000 feet

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8
Q

Max severe turbulence penetration speed

A

280 KIAS/.75M - whichever is lower

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9
Q

Max gear extension speed

A

220 knots

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10
Q

Max gear extended speed

A

220 knots

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11
Q

Max gear retraction speed

A

200 knots

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12
Q

Max airspeed for windshield wiper ops

A

250 knots

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13
Q

Flaps 1

A

230 KIAS

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14
Q

Flaps 8

A

230 KIAS

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15
Q

Flaps 20

A

220 KIAS

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16
Q

Flaps 30

A

185 KIAS

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17
Q

Flaps 45

A

170 KIAS

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18
Q

APU starter motor duty cycle

A

Not more than 3 starts/start attempts in 1 hour with 2 minute delay between cranking attempts

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19
Q

Bleed air extraction from APU is not permitted above

A

25,000 feet

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20
Q

Which engine can be started using APU as bleed air source

A

Either

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21
Q

With APU door not closed or position unknown

A

Aircraft is limited to 220 KIAS

Or

APU must remain in operation

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22
Q

Max permissible time for ground ops with DC power

A

5 minutes - to protect CRT displays

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23
Q

During all starts, do not exceed

A

75% N1 for 2 mins after start

Or

Until all operating indications are in normal range

Whichever is longer

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24
Q

Oil pressure with take off power

A

45 psi minimum

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25
After cold start, engine must
Remain at idle until oil pressure returns to normal range
26
When must use continuous ignition
Take off or landing on contaminated runway Take off with x wind 15 knots or greater Flight through mod or heavier intensity rain Flight through mod or heavier intensity turbulence Flight in vicinity of thunderstorm
27
Starter cranking limits
Start 1 - 90 seconds max time on - followed by 10 seconds off Start 2 - 90 - 10 Start 3 and subsequent- 90 seconds max time on - 5 minutes off
28
During landing, max reverse thrust is prohibited below
75 KIAS and reverse idle should be achieved by 60 KIAS
29
FLEX takeoff limitations
Anti skid must be operative No on contaminated runways No if aircraft has been deiced No if wing/cowl anti icing bleeds in use No if warnings of windshear or downdrafts forecast No with engine that cannot achieve full rated thrust No when special departure procedure requires full thrust for takeoff
30
Can you use slats/flaps en route?
No, prohibited
31
Max slats/flaps extended altitude
15,000 feet
32
Minimum altitude for flight spoiler deployment
1,000 feet AGL
33
To ensure adequate maneuver margins, flight spoilers must not be extended inflight at airspeeds below the recommended reference speed plus __.
10 KIAS
34
Max permissible fuel imbalance between left and right wing tanks
Takeoff: 300 lbs All other phases: 800 lbs
35
Takeoff with fuel load in excess of __ in center tank is not permitted unless each wing tank is above ___.
500 lbs 4,400 lbs
36
Powered crossflow and gravity crossflow must be __ for takeoff
Off
37
Cowls on temp range
Ground: OAT 10C or below Air: From TAT 10C to SAT -39c
38
Wing and cowls on temp range
Ground: Takeoff with OAT 5C or below and contamination/vis moisture Air: From TAT 10C to SAT -39C below 230 knots
39
Ground contamination definition
Rwys, ramps, or taxiways with surface snow, ice, slush, or standing water.
40
Visible moisture definition
Precipitation in any form (fog with vis of 1 mile or less, mist, rain, snow, sleet, and ice crystals or clouds in flight)
41
If visible moisture is present below 400 feet AGL with OAT 10C or below:
Cowls for takeoff
42
If OAT 5C or below and visible moisture present below 400 feet AGL:
Wing and cowl for takeoff
43
Do not hold in icing condition with
Slats or flaps extended
44
Taxi lights must be switched off when aircraft is
Stationary in excess of 10 minutes
45
Min brake cooling time is
15 minutes and all BTMS indicators must been green and not increasing
46
CAT II approaches are prohibited when braking action is reported as
Less than medium
47
Ops with autopilot engaged is prohibited below 600 feet AGL except:
For visual and non precision approaches (400 feet AGL) For precision approaches (80 feet AGL)
48
For precision approaches, the minimum height for autopilot use with one engine operating is
110 feet AGL
49
Max taxi and ramp weight
75,250 85,000
50
Max takeoff weight
75,000 84,500
51
Max landing weight
67,000 75,100
52
Max zero fuel weight
62,300 70,750
53
Max APU starting altitude
37,000 feet
54
Max APU operating altitude
41,000 feet
55
MEL Categories A
Varies
56
MEL Categories B
3 days
57
MEL Categories C
10 days
58
MEL Categories D
120 days
59
Differed MX Class 1
10 days max
60
Differed MX Class 2
30 days max
61
Max AC Electrical load on Engine or APU driven generator
40
62
Max DC Electrical load on each TRU
120
63
Max time at TOGA power on 2 engines
5 minutes
64
Max ITT for engine start on ground
120 C
65
Max ITT for engine start in flight
90 C
66
Min oil pressure at idle
25 PSI
67
Min oil pressure at TO power
45 PSI
68
Min fuel for go around per wing with airplane level and assuming max climb attitude of 10* nose up
600 lbs
69
Operation w autopilot engaged is prohibited below __ except with approaches
600 AGL
70
Min altitude for autopilot for visual and non-precision approaches
400 AGL
71
Min altitude for autopilot for precision approaches
80 AGL
72
Min altitude for autopilot on single engine precision approach or approaches with vertical guidance
110 AGL

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