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PSA New Hire Training > POH Chapter 3 > Flashcards

POH Chapter 3 Flashcards

1
Q

Minimum flight crew

A

One Captain and one First Officer

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2
Q

Maximum 90 degree crosswind for takeoff and landing

A

27 knots

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3
Q

Maximum 90 degree crosswind for landing from a Category II Approach

A

15 knots

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4
Q

Maximum headwind for landing from a Category II Approach

A

16 knots

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5
Q

Maximum direct tailwind for takeoff and landing

A

10 knots including gusts

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6
Q

Maximum runway slope approved for takeoff and landing

A

+2.0% (uphill) -2.0% (downhill)

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7
Q

Maximum operating altitude

A

41,000 ft

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8
Q

Maximum pressure altitude for takeoff and landing

A

8,000 ft

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9
Q

Maximum ambient temperature for takeoff and landing

A

ISA +35°C

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10
Q

Minimum ambient temperature approved for takeoff

A

-40°C

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11
Q

Maneuvering Limit Load Factors Flaps Retracted

A

-1.0 to +2.5G

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12
Q

Maneuvering Limit Load Factors Flaps Extended

A

0.0 to +2.0G

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13
Q

Except in an emergency, takeoff or landing will not be attempted whenever peak wind value ______.

A

exceeds 50 knots

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14
Q

Maximum Taxi and Ramp Weight

A

700: 75,250 lbs 900: 85,000 lbs

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15
Q

Maximum Takeoff Weight

A

700: 75,000 lbs 900: 84,500 lbs

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16
Q

Maximum Landing Weight

A

700: 67,000 lbs 900: 75,100 lbs

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17
Q

Maximum Zero Fuel Weight

A

700: 62,300 lbs 900: 70,750 lbs

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18
Q

Flight must be within ______ of a suitable airport, if cargo is carried in either cargo compartment.

A

60 minutes

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19
Q

Turbulence Penetration Speed

A

280 KIAS/.75M whichever is lower

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20
Q

Maximum gear extension speed

A

220 KIAS

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21
Q

Maximum gear extended speed

A

220 KIAS

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22
Q

Maximum gear retraction speed

A

200 KIAS

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23
Q

Maximum airspeed for windshield wiper operation

A

220 KIAS

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24
Q

Maximum airspeed for windshield wiper operation failed in the non-parked position

A

250 KIAS

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25
Q

Maximum Cruise Mach in RVSM Airspace

A

0.82M

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26
Q

Tire limit ground speed 700

A

182 knots

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27
Q

Tire limit ground speed 900

A

195 knots

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28
Q

Vfo/Vfe Flaps 1

A

Flaps 1 – 230 KIAS

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29
Q

The VFE and VFO speeds are ______.

A

equal

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30
Q

The Wing and Cowl Anti-Ice System(s) shall be operated in accordance with the following conditions:

A
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31
Q

Ground contamination definition

A

Runways, ramps or taxiways with surface snow, ice, slush or standing water

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32
Q

Visibile moisture definition

A
  • Visible moisture or precipitation in any form (such as fog with visibility of 1 mile or less, mist, rain, snow, sleet and ice crystals or clouds in flight)
  • If visible moisture is present below 400 feet AGL with OAT of 10°C or below activate cowl anti-ice for takeoff. If OAT 5°C or below activate both cowl and wing anti-ice for takeoff
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33
Q

Engine Indications (Red, Amber, Green)

A
  • Maximum and minimum limitations
  • Caution range
  • Normal operating range
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34
Q

During all starts, do not _______________________________________________.

A

exceed 75% N 1 for 2 minutes after start, or until all operating indications are in the normal range, whichever is longer.

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35
Q

Prior to shutdown _________________________.

A

Operate engines at or near idle for 2 minutes

36
Q

ITT limitations for ground start and airstart

A

Below 120°C before attempting to ground start and below 90°C before attempting to airstart

37
Q

Steady-state idle minimum oil pressure

A

25 psi

38
Q

Takeoff power minimum oil pressure

A

45 psi

39
Q

Continuous engine ignition must be used during the following:

A
  • Takeoff and landing on contaminated runways
  • Takeoff with high crosswind components (15 knots or greater)
  • Flight through moderate or heavier intensity rain
  • Flight through moderate or heavier intensity turbulence
  • Flight in the vicinity of thunderstorms
40
Q

Engine operating limits due to wind direction

A
41
Q

Engine Starter Cranking Limits (701 Ground only) (900 Ground Only)

A
42
Q

Engine Starter Cranking Limits (701 Flight only) (900 Flight Only)

A
43
Q

The starter must not be engaged if ________________.

A

indicated N2 RPM exceeds 45% (inflight or on the ground)

44
Q

At initiation of thrust lever movement from SHUT OFF to IDLE:

A
  • ITT must be 120°C or less for all ground starts
  • ITT must be 90°C or less for all air starts
45
Q

A dry-motoring cycle (with thrust levers at SHUT OFF) may be used for engine ground starts and engine air starts. Limitations:

A
46
Q

Oil pressure limitations

A
47
Q

Maximum permissible fuel imbalance between left and right tank

A
  • Takeoff: 300 lbs
  • All other phases of flight: 800 lbs
48
Q

Fuel remaining in a tank when the appropriate fuel quantity indicator reads zero is _________.

A

not usable

49
Q

Fuel quantities are based on _______.

A

6.75 lbs / per U.S. gallon

50
Q

Takeoff with a fuel load in excess of ______ in __________ is not permitted unless ___________________. __________________ must be OFF for takeoff.

A

500 lbs. in the center tank is not permitted unless each wing tank is above 4,400 lbs. Powered crossflow and gravity crossflow must be OFF for takeoff.

51
Q

The APU starter motor duty cycle is limited to not more than _____ starts/start attemps in ______ hour with a ______ minute delay between cranking attemps

A

3 starts/start attempts in 1 hour with a 2 minute delay between cranking attempts

52
Q

APU Bleed Air Limitations

A
53
Q

With the APU door not closed or the door position is unknown:

A
  • The airplane must be limited to: 220 KIAS
  • Or the APU must remain in operation
54
Q

Use of ______________ during approach is not permitted.

A

SPEED MODE (DES or IAS), flight director or autopilot coupled

55
Q

Use of ______________ during the climb and approach phases of flight is not permitted.

A

VNAV, flight director or autopilot coupled

56
Q

Operation with the autopilot engaged is prohibited at altitudes below 600 ft. AGL, except when performing the following:

A
  • For visual and non-precision approaches, the minimum height for autopilot use is 400 ft. AGL
  • For precision approaches (PAR/ILS), the minimum height for autopilot use is 80 ft. AGL unless:
    • The glide path angle is greater than 3.5° and less than or equal to 4.0° and the Airport elevation is less than or equal to 4000 feet the minimum height for autopilot use is 120 ft. AGL
    • ILS approaches with a glide path angle of greater than 4.0° is prohibited
  • For precision approaches (PAR/ILS) or approach procedures with vertical guidance, the minimum height for autopilot use with one engine operating is 110 ft. AGL
  • Category II Approach must be flown with the autopilot engaged.
57
Q
  • The ADC source coupled to the active FCC must be _________
  • In flight, prior to entering RVSM airspace __________
  • Maximum cruise speed in RVSM airspace is ________
A
  • the same as that coupled to the ATC transponder during flight in RVSM airspace.
  • all required equipment for operation in RVSM airspace must be operational.
  • 0.82M
58
Q

RVSM Required Equipment List

A
59
Q

To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DC power only is _______.

A

5 minutes

60
Q
  • Enroute use of slats/flaps is _________
  • Maximum slats and/or flaps extended altitude:
A
  • prohibited
  • 15,000 ft
61
Q

Minimum altitude for flight spoiler deployment:

A

1,000 ft AGL

62
Q

To ensure adequate maneuver margins, flight spoilers must not ____________________.

A

be extended inflight at airspeeds below the recommended reference speed plus 17 KIAS

63
Q

During landing, maximum reverse thrust is ________________________________.

A

prohibited below 75 KIAS, and reverse idle should be achieved by 60 KIAS

64
Q

The taxi lights must be switched OFF whenever _____________________________.

A

the airplane is stationary in excess of 10 minutes

65
Q

Minimum brake cooling time is __________, and all _____________ must be _________________________.

A

15 minutes; BTMS indicators must be green and are not increasing

66
Q

Maximum altitude for single pack operation

A

31,000 feet

67
Q

Vfo/Vfe Flaps 8

A

Flaps 8 – 230 KIAS

68
Q

Vfo/Vfe Flaps 20

A

Flaps 20 – 220 KIAS

69
Q

Vfo/Vfe Flaps 30

A

Flaps 30 – 185 KIAS

70
Q

Vfo/Vfe Flaps 45

A

Flaps 45 – 170 KIAS

71
Q

Maximum starting altitude for the APU

A

37,000 feet

72
Q

Maximum altitude for APU Bleed Air for Air Conditioning

A

25,000 feet

73
Q

Maximum time at TOGA power on 2 engines

A

5 minutes

74
Q

After cold start, engine must remain at ____ until oil pressure returns to normal range

A

idle

75
Q

If Static/Standing takeoff data is generated and wind limits prevent a Static/Standing takeoff Winds must be entered in ____ OR for aircraft with ACARS inoperative, Dispatch must _______ winds into TLR data

A

ACARS

manually insert

76
Q

Maximum fuel quantity for pressure refueling (total)

A

19,594 lbs

77
Q

Maximum fuel quantity for gravity refueling (total)

A

700 - 14,580 lbs

900 - 14,810 lbs

78
Q

Minimum fuel quantity for go-around per wing tank (with airplane level) and assuming a maximum airplane climb attitude of 10° nose up ____ lbs

A

600 lbs (CRJ700 & 900)

79
Q

Icing conditions in flight exist when visible moisture is present, and the TAT ____ except when the SAT is _____ or below

A

10°C or below, except when the SAT is -40*C or below

80
Q

Exterior Inspection to determine that the wing is free from forst, ice, snow, or slush when:

  • The OAT is ___ or less, or
  • The bulk fuel temperature is ____ or less or
  • __________________
  • Ice and frost may continue to adhere to wing surfaces for some time even at outside air temperatures above _____
A
  • 10*C
  • 0°C
  • The atmospheric conditions have been conducive to frost formation
  • 10°C
81
Q

Do not hold in icing conditions with ______ extended

A

slats and/or flaps

82
Q

Category II approaches are prohibited when the braking action is reported as less than _____.

A

Medium

83
Q

Cabin Alt/Emergency Descent

A

Oxygen masks……………..DON and 100%

Crew communication……………..ESTABLISH

Captain Assumes PF Duties

84
Q

Smoke/Fire/Fumes

A

Oxygen masks (if required)……………DON and 100%

Crew communication…………….ESTABLISH

85
Q

Stabilizer Trim Runaway

A

Control wheel…………………ASSUME manual control and OVERRIDE runaway

STAB TRIM DISC…………………….Push, hold and release

86
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

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