Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

PSA -k > Limits and immediate action items test > Flashcards

Limits and immediate action items test Flashcards

0
Q

Max takeoff weight

A

53000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
1
Q

maximum taxi and ramp weight

A

53250

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Max landing weight

A

47000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Max zero fuel weight

A

44000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Max pressure alt for takeoff and landing

A

8,000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Max operating altitude

A

36000

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Min ambient temp for takeoff

A

-40c

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Definition of icing conditions for COWL

A

cowl icing conditions exist when:
OAT on the ground and for takeoff or the TAT inflight is 10C or below and visible moisture is present in flight
below 400 feet AGL for ground ops
when operating on surface that are wet or contaminated

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Cowl A\I must be on when

A

Cowl A/I Must be on for:
all ground and flight ops when icing conditions exist
when ice is annunciated by the ICE detect system
except when the inflight SAT is -40 or below

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Wing Anti Ice conditions

A

wing Icing conditions exist when:
OAT is 5C or less or tat in flight is 10 C or below and visible moisture is preset
in flight or below 400ft AGL for takeoff
the runway is wet or contaminated

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Wing A/I must be on:

A

Wing anti-ice must be on:
>takeoff and flight operations when ice is annunciated
>when icing conditions exist at less than 230 kias unless inflight SAT is >-40c or below.
>Must be ON during final 2 mins before takeoff unless type 4 anti ice fluid has been applied.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Tactile Check when why and how

A

Tactile check is needed when
OAT is 5c or less or wing fuel temp is 0C or less
atmospheric conditions have been conducive to frost formation.
Ice and frost may continue to adhere to wing surfaces for some time even at air temps above 5c
Check leading edge, wing forward upper surface, and wing rear/upper surface during external walk around inspection

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Do not hold in icing conditions with ____ and or ____ extended

A

slats /flaps

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Continued operation in areas where SLD icing conditions exist is _____

A

Prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

All contaminated performance data will be for ______ takeoffs

A

Static

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Maximum tailwind for takeoff and landing ___

A

10kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Maximum crosswind for takeoff and landing___

A

27kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Max 90 degree xwind for landing from a cat II approach ___

A

15 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Max headwind for cat II approach ___

A

17kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Max weight in cargo compartment ___

A

3500

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

flights must be within__minutes of a suitable airport with cargo in the cargo compartment

A

45 minutes

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

Eicas limit markings

A

RED- min and max limits
Amber- Caution range
Green- normal operating range

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Max itt for start

A

900C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Max n2 split at idle

A

2%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Max itt allowed to advance the thrust levers to idle for all ground starts

A

120

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Oil pressure steady state idle

A

25 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Oil pressure takeoff power

A

45 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

Min oil temp for engine starting

A

-40C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

during all starts do not exceed ___N1 for ___minutes after start or until all operating indications are in the normal range whichever is ___

A

75% 2min Longer

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

operate engines at or near idle for ____ minutes prior to shutdown

A

2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

Airplane cold soak Defined

A

Before first flight of the day has set out in -30C or below for more than 8 hours

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

Cold soak operation requirements

A

Motor engines for 60 seconds and fan rotation must be verified thrust reversers must be actuated until the deploy and stow cycles are 5 seconds or less

32
Q

Continuous ignition must be used during: (5 things)

A

1- takeoff and landing on contaminated runways
2- takeoff with high crosswind components 15kts or greater
3- flight through moderate or heavier intensity rain
4- flight through moderate or heavier intensity turbulence
5- flight in the vicinity of thunderstorms

33
Q

Starter Cranking limits

A

Start Max time on time off
1 1 min 10s
2 1 min 10s
3+ 1 min 5min off

34
Q

Dry motoring cycle for engines

A

Start Max time on followed by
1 90 seconds 5 min off
2+ 30 seconds 5 min off

35
Q

Max fuel imbalance between the left and right wing tank ______

A

450

36
Q

Max total fuel for Pressure refueling

A

14518 lbs

37
Q

Takeoff with fuel load in excess of _____ in the center tank is not permitted unless each wing tank is above ____

A

500lbs, 4400 lbs

38
Q

Powered crossflow and gravity crossflow must be____ _____ for takeoff

A

selected off

39
Q

Takeoff with the engine fuel temperature indications below ____ is prohibited

A

5C

40
Q

Minimum fuel quantity for a go around per wing tank assuming 10 degrees pitch up

A

450

41
Q

APU start on battery

A

Start Max time on Off
1 30s 2 min
2 30s 20 min
3 30s 2 min
4 30s 40 min

42
Q

APU start on DC ground power

A

Start Max time on followed by
1 15s 2 min
2 15s 20 min
3 15s 2 min
4 15s 40 min

43
Q

APU max starting altitude

A

30,000

44
Q

APU Max operating altitude

A

36,000

45
Q

Max apu RPM

A

107%

46
Q

With the APU door not closed or the door position unknown, the airplane must be limited to _______ or _______

A

300 kias or apu remain operational

47
Q

Max bleed air extraction for air conditioning from the APU is ____

A

15,000ft

48
Q

Max engine start altitude with APU bleed air

A

13,000 ft

49
Q

Min engine oil pressure for takeoff

A

45PSI

50
Q

Flaps 8 VFE/VFO

A

230/200

51
Q

Flaps 20 VFE/VFO

A

220/200

52
Q

Flaps 30

A

185

53
Q

Flaps 45

A

170

54
Q

VLE

A

220

55
Q

landing gear down and locked

A

220

56
Q

Gear Up

A

200

57
Q

Max tire speed

A

182

58
Q

Max airspeed for windshield wiper operation failed in the non parked position

A

220

59
Q

Max turbulence penetration speed

A

280/.75

60
Q

Max cruise mach in RVSM airspace

A

.82M

61
Q

RVSM equipment List

A

Autopilot- must be operational
Altitude alerting system- must be operational
Altitude reporting transponder (2) -one must be operational
Air data computers (2) - two must be operational

62
Q

Minimum autopilot engagement altitude_____ except when performing non precision approach_______ or precision approach

A

600/400/80 AGL

63
Q

Max slats/ flaps extension altitude _____

A

15,000

64
Q

Max permissible time on the ground with only DC power

A

5Min

65
Q

Min alt for flight spoiler deployment

A

1000ft

66
Q

Min airspeed for flight spoiler use

A

Reft +17kts

67
Q

Min brake cooling time

A

15 min and all BTMS green and not increasing

68
Q

During landing application of thrust reverse above_____ is not permitted at airspeeds below _____. Below _____ reverse thrust must be reduced to idle not above____.

A

60%N1
75kts
60kts
30%N1

69
Q

use of the EMER DEPRESS switch above ______ is prohibited

A

15000

70
Q

Max altitude for singe pack ops

A

25000

71
Q

Max differential pressure for taxi takeoff and landing

A

0.1

72
Q

Max relief diff pressure

A

8.7

73
Q

Braking loss/asymmetry

A

Wheel brakes….. release momentarily
PM will select anti-skid to off
Wheel brakes…. re-apply as required
Reverse thrust…. apply maximum until stopping assured

74
Q

Cabin alt

A

oxygen masks…… Don and 100%
Crew communication…… establish
Captain assumes PF duties

75
Q

Double Engine Failure

A

Cont ignition …. on

Airspeed 240 kias minimum

76
Q

Smoke/fumes

A

oxygen masks Don and 100%

Crew Communication Establish

77
Q

Stab Trim Runaway

A

Control wheel assume manual control and override runaway
Both stab trim discs… push hold and release
Captain assumes pf duties
Stab ch1 cb 2f5 … open
stab ch2 cb 4a1… open

PSA -k (1 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions