737 Flash cards April 12 2024

1
Q

Flight Maneuvering Load Acceleration Limits

A

Flaps Up +2.5gto -1.0g Flaps Down +2.0g to 0.0g

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2
Q

Max Operating Pressure Altitude *

A

41,000 feet

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3
Q

Max Takeoff/Landing Pressure Altitude

A

10,000 feet

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4
Q

Max Flight Operating Latitude

A

82N 82S exceptions for certain East and west longitudes

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5
Q

Runway Slope

A

2% + or -

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6
Q

Max Takeoff/Landing Tailwind *

A

15 KTS

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7
Q

Max Airspeed MMO

A

.82 Mach

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8
Q

Max gear retraction speed

A

235 KTS

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9
Q

Max gear extension speed

A

270 KTS/ .82M

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10
Q

Max gear extended speed

A

320 KTS/ .82M

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11
Q

Severe Turbulence Penetration Speed Cruise *

A

Turb N1 setting from cruise pg

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12
Q

Severe Turbulence Penetration Speed Climb and Descent *

A

280 KTS /.76Mach

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13
Q

Over wing Exits

A

Handle covers must be installed when ever pax are carried

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14
Q

On revenue flights the Girt bar must-

A

Be installed for Taxi, Takeoff, and Landing

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15
Q

Quick turn around weight limit exceeds chart value wait at least

A

67 Min. 48 Min with Carbon brakes

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16
Q

Crosswind Guidlines Takeoff and Landing Dry - code 6

A

Takeoff - 33 Landing - 37

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17
Q

Crosswind Guidlines Takeoff and Landing Wet - code 5

A

Takeoff - 25 Landing - 37

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18
Q

Gross Weight 737-800

A

Taxi-174,700 lbs. Takeoff - 174,200 lbs. Landing - 146,300 lbs. ZFW - 138,300 lbs.

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19
Q

Max Cabin Diff.

A

9.10 psi

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20
Q

Max Cabin Diff. for Takeoff and Landing

A

0.125

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21
Q

Duct pressure for Max cooling

A

20 - 25 psi

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22
Q

Min Duct Pressure for Two Pack Operation From Single Bleed Source

A

20 - 25 psi

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23
Q

Iceing conditions exist on the ground and for takeoff when… *

A

10c or below - visible moisture and orvisibility 1 mile or less in clouds or fog. - anytime on the ground when standing water rain slush or snow may be ingested.

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24
Q

Takeoff in Moderate/ Heavy Freezing Rain or Hail is..

A

Prohibited

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25
Q

Engine Anti Ice Must Be On Durring All flight Ops when…

A
  • Icing conditions exist or are anticipated. - When Temp is below -40SAT Except during climb and cruise. - Ignition must be set to CONT. prior to using Engine Anti Ice.
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26
Q

Wing Anti Ice

A

Must be used during all ground ops from engine start to takeoff when icing conditions exist. Unless Type II or Type IV fluid is used. Do not use Wing Anti Ice above 10C / 50F. Do Not use Wing Anti Ice During Takeoff until After the First Power Reduction.

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27
Q

Windsheild wipers

A

Do not use on DRY Windshield

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28
Q

Widow Heat

A

Must be ON 10 Min. before takeoff.

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29
Q

Autopilot Engagemet *

A

400AGL

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30
Q

Autoland Max Winds

A

Headwind - 25 X-wind -15 Tailwind -10 (for flaps 30 or 40)

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31
Q

Aileron trim with Autopilot engaged

A

Is Prohibited

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32
Q

Autopilot use prohibited below 100’ RA at Airports above…

A

AT Airports with a Pressure Altitude above 8400’

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33
Q

Min. Altitude for Autopilot use on Approach *

A

ILS/GLS (not autoland) 50’AGL - Non Precision App 50’ below MDA/DA - Auto Lnd to Touchdown

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34
Q

Auto land can only be used when..

A

Runway is at or below 8400’ pressure Alt. - Flaps 30 or 40 used with two operating engines. - Max and Min Glideslope angle 3.25 and 2.5

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35
Q

Autoland should not be used for

A

Overweight landings

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36
Q

Do Not use the autopilot or autothrottle if

A

The associated radio altimeter is inoperative.

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37
Q

APU Bleed and Electrc Max Alt.

A

10000

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38
Q

APU Bleed Max Alt.

A

17000

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39
Q

APU Electric Load Max Alt.

A

41000

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40
Q

APU Starter duty cycle

A

15 Min cooling required after 3Rd start attempt on the ground or in the air

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41
Q

APU Warm up cool down

A

Operate APU “1” Min before using Bleed air. - Wait 120 Sec for APU shutdown then turn Batt sw OFF.

42
Q

APU Bleed valve must be closed when…

A

Ground Pneumatic air on and ISOLATION valve OPEN. - Engine 1 Bleed vave open (engine1 running). - ISOLATION valve OPEN and Engine2 Bleed valve Open( engine2 running).

43
Q

Max single Engine Generator load

A

75KVA - 215 Amps (ground ops)

44
Q

Min Batt Volts for APU start

A

23V

45
Q

Engine Ignition must be “ON” for..

A

-Takeoff - Landing - Engine Anti Ice Operation. - Heavy Rain

46
Q

Min Oil Pressure

A

13psi

47
Q

Max oil temp

A

155C

48
Q

Max Continuous oil temp

A

140C

49
Q

Max Allowable for 45min. Oil Temps

A

140C-155C

50
Q

MAX EGT Takeoff 5min.

A

950C

51
Q

MAX EGT Continuous

A

925C

52
Q

MAX EGT Starting

A

725C

53
Q

Engine Starter Duty Cycles

A

Do Not exceed 2 min for each start attempt. - A Min. of 10 sec. between starts.

54
Q

MAX N1

A

104%

55
Q

MAX N2

A

105%

56
Q

Reduced Thrust Takeoffs are not permitted when…

A

Antiskid inop. - Runway is contaminated with standing water, ice, slush or snow.

57
Q

EEC

A

both must be “ON” or “ALT” for takeoff. - Reduced thrust Takeoff not permitted in “ALT”mode.

58
Q

Min Oil Quantity

A

70%

59
Q

Starter Engagement

A

Do not engage starter above 20% N2

60
Q

Engine starts in temp below -35C

A

Idle for 2 min before changing thrust lever position.

61
Q

Lavatory fire extinguishing

A

Black dots or discharge nozzle tip turns an aluminium color. Maint. req.

62
Q

Engine Fire Extinguishing bottles

A

800psi@70F

63
Q

Flaps Altitude limitation

A

20,000

64
Q

Holding in Icing conditions …

A

is prohibited

65
Q

Speed brake lever limitations

A

Do not extend beyond the Flight detent. - Do not use RA less than 1,000’- Not used beyond Flaps 15

66
Q

Alternate Flap duty cycle

A

Allow 15 sec.off after releasing Alt flap position switch. After a complete 0-15-0 cycle allow 5 Min. cooling.

67
Q

Max Airspeed with Alternate Flap System

A

230 KTS

68
Q

Mach trim fail (both channels) Max speed

A

280 KTS / .82 Mach

69
Q

RVSM Max diff. between Captain and FO Altimeters in flight

A

200’

70
Q

RVSM Max diff. between Captain and FO Altimeters on ground 0-5,000’

A

50’

71
Q

RVSM Max diff between either pilot and field elevation

A

75’

72
Q

JET A Min. Max temp

A

Min -37C Max +49C

73
Q

The use of JP4 and JetB is..

A

Prohibited

74
Q

Tank fuel must be……temperature

A

3C above Fuel Freezing point

75
Q

7/8/9/ Wing Tank Qantity

A

8630 lbs

76
Q

7/8/9/ Center Tank Quantity

A

28,803 lbs

77
Q

Fuel Density

A

6.7 lbs/gal

78
Q

Random Fuel Imbalance must not exceed

A

1,000lbs

79
Q

The Center Tank “CONFIG” light will illuminate..

A

When Center tank fuel exceeds 1,600lbs with center tank fuel pumps off

80
Q

Min. Wing tank fuel for cooling electric Hydraulic pumps on the ground..

A

1,675 lbs each

81
Q

Min Hydraulic QTY

A

Above RF

82
Q

Max Tire Speed

A

195 KTS

83
Q

Engine Failure (V1 Cut) Take off profile LNAV/VNAV

A

“ROTATE” 7-11 degrees “POSATIVE RATE” “GEAR UP” climb V2 - 15 degree bank to 1500AGL ( unless special EO) fly runway centerline. At 400’ “Heading select” or “LNAV”, At 800’ or charted Alt retract flaps on schedule. At VM0 “Set Max Continuos Thrust” Engine Failure or Sever Damage or Engine Fire Checklist.

84
Q

Engine Failure (V1 Cut) Take off profile HDG SEL and TOGA

A

“ROTATE” 7-11 degrees “POSATIVE RATE” “GEAR UP” climb V2 - 15 degree bank to 1500AGL (unless spcial EO) fly runway centerline. At 400’ “Heading select” , At 800’ or charted Alt. ‘Set Clean Mauvering Speed” retract flaps on schedule. At VM0 “Set Max Continuos Thrust” Engine Failure or Sever Damage or Engine Fire Checklist.

85
Q

2 Engine ILS Profile Cat 1

A

“2500” “ In or Hpa”. At glideslope intercept “Set TDZE”. “1000” “Set missed approach altitude” Cleared to land” or “no landing clearance”. “500” “Stable” or “Unstable going around”. “minimums” “Landing” or “Going Around” (note) 1 1/2 dot gear down flaps15

86
Q

1 Engine ILS Profile

A

Intercept Loc with Flaps 5. At 1 dot GS deviation “ Gear down flaps 15 “.

87
Q

RNAV / Non-Precision Approach profile

A

4 Miles FAF “Gear down Flaps 15t” 2 Miles “Flaps__”

88
Q

1 Engine missed approach.

A

“GOING AROUND”, “FLAPS 1”, “Check Thrust”, “Posative Rate, Gear Up”, “Set Missed Approach Altitude”at 400’ “Heading Select/LNAV”, at 800’ or higher if published “SET CLEAN MANEUVERING SPEED” Clean up on schedule. “SET MAX CONTINUOUS THRUST” accomplish “Abbreviated After Takeoff Checklist

89
Q

2 Engine missed approach

A

“GOING AROUND”, “FLAPS 15” “ CHECK THRUST” “POSATIVE RATE GEAR UP” “SET MISSED APPROACH ALTITUDE” @ 400’ “HEADING SELECT or LNAV”, at 800’ or higher if published “LEVEL CHANGE SET CLEAN MANUEVERING SPEED” Clean up on schedule. “After Takeoff Checklist”.

90
Q

Immediate Action APU FIRE

A

APU Fire Switch….Confirm….Pull….Rotate and Hold 1 Sec. APU SWITCH…OFF

91
Q

Immediate Action LOSS OF THRUST BOTH ENGINES

A

ENGINE START SWITCHES (both)….FLT ENGINE START LEVERS (both)…CUTOFF ENGINE START LEVERS (both)….IDLE

92
Q

Immediate Action ENGINE FIRE or SEVERE DAMAGE

A

Autothrottle (if engaged)….Disengage Thrust Lever (affected engine)…. Confirm….Close

93
Q

Immediate Action ENGINE OVERHEAT

A

Autothrottle (if engaged)….Disengage Thrust Lever (affected engine)…. Confirm….Close

94
Q

Immediate Action ENGINE LIMIT SURGE or STALL

A

Autothrottle (if engaged)….Disengage Thrust Lever (affected engine)…. Confirm…RETARD (until within limits)

95
Q

Immediate Action AIRSPEED UNRELIABLE

A

Autopilot (if engaged)….Disengage Autothrottle (if engaged)….Disengage FLIGHT DIRECTOR switches (both)….OFF / Set following gear up pitch attitude and thrust….Flaps Extended…….10deg and 80% N1 Flaps Up…4deg and 75% N1

96
Q

Immediate Action SMOKE FIRE FUMES

A

Oxygen Masks and Regulators….ON(as needed), 100% CREW COMM…..Establish

97
Q

Immediate Action CABIN WARNING / RAPID DECOMP

A

Oxygen Masks and Regulators….ON, 100% CREW COMM…..Establish Seatbelt Sign…..ON

98
Q

Immediate Action Flight Deck Door

A

JAMCO…..Hardlock switch…..PUSH Boeing…..FLT Deck Door selector…..ROTATE to DENY

99
Q

Immediate Action RUNAWAY STABILIZER

A

1.Control Column..Hold Firmly - 2.Autopilot (if engaged)…Disengage - 3.Autothrottle (if engaged)…Disengage
4.Controll Column and Thrust Levers -controll airplane pitch attitude and airspeed
5.Main Electric Stab Trim - Reduce controll collumn forces.

If runaway stops do not reengage autopilot or auto throttle.
If Runaway continues… STAB TRIM CUTOUT
if runaway continues…
Grasp and Hold

100
Q

T.E.S.T

A

TYPE of nonnormal EVACUATION prep required or not SPECIAL instructions TIME remaining

101
Q

Do Not use LVL CHG below…

A

1000 feet AFE

102
Q

Engine Start Aborted Start*

A

Engine Start Lever effected engine…CUTOFF