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Boeing 737-800 Test

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1.
Under FAA Rules Maximum allowable wind speeds when landing weather minima are predicated on autoland operations:
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2.
Maximum Operating Altitude (-800)
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3.
Maximum and minimum limits color
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4.
Maximum allowable on the ground altitude display difference (-400)
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5.
Runway Slope
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6.
Both PMCs/EECs _______ be in the same mode for takeoff
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7.
Turbulent Penetration speeds
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8.
Maximum flight operating latitude (-800)
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9.
Maximum engine EGT for start on -400 aircraft
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10.
Maximum allowable on the ground altitude display differences (-800)
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11.
Thrust setting for engine out above max continuous can be maintained for _________
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12.
Maximum Takeoff and Landing Tailwind Component (-400)
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13.
Installation of ________________ on the overwing exits must be verified prior to departure whenever passengers are carried
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14.
Maximum Takeoff and Landing Altitude (pressure altitude)
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15.
Maximum flight operating latitude (-400)
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16.
Engine Ignition must be on for:
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17.
Verify that an operational check of the ________ _________ ________ _________ _________ has been accomplished according to the approved procedures in the supplementary section once each day.
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18.
On revenue flights, the ________ _________ _________ _________ ______ _____ must be installed during taxi, takeoff, and landing
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19.
Maximum and Minimum glideslope angles for autoland
A.
Flight deck door access system
B.
8,400 ft
C.
escape slide retention bar (girt bar)
D.
Takeoff, Landing, Operation in Heavy rain, anti-ice operation, turbulence
E.
+/- 2%
F.
41,000 Feet
G.
MUST
H.
3.25 degrees and 2.5 degrees respectively
I.
73 degrees North and 60 degrees South
J.
725 degrees C
K.
82 degrees north and 82 degrees south except for the region between 80 west and 130 west the maximum flight operating latitude is 70 north and the region between 120 east and 160 east longitude , the maximum flight operating latitude is 60 south
L.
10 knots
M.
Max difference between Cpt and F.O. SL to 5000ft: 50 FT 5001-10000ft: 60 FT Max difference between Cpt or F.O. & Field Elevation 75FT
N.
Max Difference between Cpt. and F.O. SL to 5000ft: 40ft @SL 45ft @5000' 5001-10000ft: 50 FT Max Difference Between Cpt or F.O. & Field Elevation 75FT
O.
Red
P.
10 Minutes (-800) 5 minutes (-400)
Q.
280 knots/.76M, whichever is lower (-800) 280 knots/.73M whichever is lower (-400)
R.
handle covers
S.
Headwind 25 knots - Crosswind 20 knots (15 for CAT II or CAT III conditions) - Tailwind 15 knots
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20.
Maximum demonstrated takeoff and landing crosswind (-400)
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21.
Maximum Operating Altitude (-400)
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22.
Standby altimeters _________ meet altimeter accuracy requirements of RVSM airspace
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23.
Autoland capability may only be used with flaps ____ or _____ and _____ engines running
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24.
Maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations.
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25.
Max differential pressure (relief valves) (-800)
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26.
Maximum demonstrated takeoff and landing crosswind (-800)
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27.
Max differential pressure (relief valves) (-400)
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28.
Runway Slope
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29.
Amber

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