LIMITATION B787 Flashcards
MAX RWY SLOPE?
+/- 2%
MAXIMUM TAKE OFF AND LANDING TAILWIND COMPONENT?
+/- 10 KTS
MAXIMUM OPERATING ALTITUDE?
43100 FT
MAXIMUM TAKE OFF AND LANDING ALTITUDE
14000FT
CNA YOU FLY RVSM WITH ISFD?
NO
WHEN NOT TO USE THE HF?
WHILE REFUELLING
SA-SB MAX CROSSIWINDS?
TAKE OFF 35KTS LANDING 33 KTS DEMOSTRATED
SC-SI MAX DEMOSTRATED TAKE OF AND LANDING CROSSWINDS?
TAKE OFF 29 KTS LANDING 35 KTS
SEVERE TURBULENCE SPEED?
290 KTS BELOW 25000FT
310kts or .84 M ABOVE 25000ft
WHAT IS THE MAX DIFFERENCE IN BETWEEN CPT AND FO ALTIMETERS AND FIELD ?
75 FEET
WHEN IS FORBIDDEN TO USE THE WEATHER RADAR?
IN HANGAR, OR WITHIN 15 MTRS FROM FUELING OPERATIONS,AVOID TO USE WHEN PERSONNEL ARE CLOSED TO THE PLANE
MAX TAXI WEIGHT 788
228,383 KG
MAX TAXI WEIGHT 789
251,743 KGS
MAX TO WEIGHT 788
227,930 KGS
MAX TAKE OFF WEIGHT 789
250,863 KGS
MAX LDG WEIGHT 788
172,365 KGS
MAX LDG WEIGHT 789
192.776 KGS
MAX ZFW 788
161.025 KGS
MAX ZFW 789
181.436 KGS
WHAT IS THE MINIMUM ALTITUDE TO ENGAGE THE A/P?
200FT
MAX AUTOLAND CAPABILITY ALTITUDE?
8400 FT
WITH OUT LAND 2/3 SHOWN A/P MUST BE DISENGAGED BY ?
100FT
WITHOUT LAND 2/3 ON B787-9 AT WHICH ALTITUDE THE A/P MUST BE DISENGAGED?
135 FT
WITH LAND 2 AND LAND 3 ANNUNCIATED WITH GS MORE THEN 3.25 DEGREES WHEN TO DISCONNECT THE A/P?
100 FT
WITH GS GRATER THE 3.77 DEGREES WHEN TO DISCONNECT THE A/P?
DISENGAGE NOT LATER THEN 50 FT BELOW MDA/DH
LOW VISIBILITY HUD TAKE OFF MAX WIND TAKE OFF
HEADWIND 25 KTS
TAIL 10 KTS
CROSS 20 KTS
MAX LDG WIND FOR AUTOLAND
HEAD 25 KTS
TAIL 10KTS
CROSS 25 KTS
MAX GS ANGLE?
3.25
MINIMUM GS ANGLE?
2,5
AUTOLAND FLAP CAPABILITY?
20/25/30 BOTH ENGINE OR ENGINE OUT
WHEN NOT TO USE FLCH?
IN FINAL APPROACH BELOW 1000 FT AFE
OIL TEMPERATURE LIMIT TO START?
GREATER THEN -40
CROSSWIND 40 KTS HOW MUCH U LIMIT THE TRUST TOO?
45 %
TAIL GREATER THE 5 KTS AND WIND GREATER THEN 35KTS TRUSTI LIMIT?
45 %
WIND GREATER THEN51 KTS TRUST LIMIT ON GRD?
IDLE
MAX ALTITUDE WITH FLAP EXTENDED?
20000FT
MAX FUEL TEMP AT TAKE OFF?
49 *c
In flight fuel temp limit?
-65*c
Tank fuel temperature prior takeoff not less then?
-29*c
Which temperature in flight to be maintained by the fuel?
At least 3 *c above freezing point
How much fuel can be loaded ion the center tank with main tanks not full?
Up to 10000 kgs provided that the center tank fuel weight plus actual zfw doesn ‘t exceed the maximum zfw and cg respected
When is prohibited to use LOOK AHEAD TERRAIN?
15 nm range in take off landing approach in airport not in the database
AIRSPEED UNRELIABLE MAX SPEED
ABOVE 40000FT 250 KTS
40000FT AND 38000FT 260KTS
38000FT TO 35000FT 270 KTS
BELOW 35000FT 290KTS
WHEN USING ALTN GEAR EXTENSION AND FLAPS ARE 20 WHAT IS THE SPEED LIMIT?
190 KTS
MAX CABIN PRESSURE POSITIVE RELIEF VALVE VALUE>?
9.9 PSI
MAX DIFF PRESS TO AND LDG?
0.11 PSI
FLAP LIMIT FOR JETTISON
DO NOT JETTISON WITH FLAP 30
MAX G
FLAP UP +2.5 AND -1.0
FLAP DOWN +2.0 AND 0.0
MAX IMBALANCE FUEL
WITH 30000KG OF FUEL MAX IS 680 KG
WITH 19000 KG FUEL MAX IMBALANCE 1100KGS
