0.82 Mach or minimum maneuver speed plus 15 knots, whichever is lower.
280 KCAS /.82M above 10000 feet.
280 KIAS below FL 250 and 270 KIAS /.80 at or above FL250
270 KIAS /.80M above 10000 feet
25 knots
38 knots
36 knots
33 knots
11.1 psi
7.3 psi
9.1 psi
8.5 psi
49 degrees Celsius
3 degrees above the EICAS limit for ‘Jet B’
3 degrees above the EICAS limit for ‘Jet A’
40 degrees Celsius
A wet runway
Inoperative RTO mode
Inoperative anti-skid on two wheels
Contaminated runways
There are no opening limitations on speedbrake operatrion.
400 feet
1500 feet
700 feet
38 knots while opening or closing, 45 knots while open
15 knots while opening or closing, 25 while open
40 knots while opening or closing, 65 while open
There are no ground wind Limits for doors
Headwind 30 knots
Tailwind 5 knots
Crosswind 38 knots
Crosswind 25 kts
There is no airspeed limit with unserviceable window heat.
280 knots
250 knots below 10000 feet
280 knots below 10000 feet
25,000 feet
15,000 feet
20,000 feet
30,000 feet
30 knots
25 knots
38 knots
10 knots
0 feet
100 feet
75 feet
50 feet
1000 feet
400 feet
250 feet
200 feet
199 feet 11 inches (60.9 meters)
205 feet 10 inches (62.7 meters)
209 feet 1 inch (63.7 meters)
70 feet 7.5 inches (21.5 meters)
239 feet 9 inches (73.1 meters)
199 feet 11 inches (60.9 meters)
206 feet 6 inches (63 meters)
209 feet 1 inch (63.7 meters)
45, 100 feet
41,100 feet
47,100 feet
43,100 feet
50 feet AGL
200 feel AGL
200 feet RA
500 feet AGL
The maximum glideslope angle is 3.25 degrees and flap 30 must be used
The minimum glideslope angle is 2.5 degrees and autoland status must display LAND 3
Automatic landings can be made using flaps 20 or 30, with both engines operative or one engine inoperative.
Contact flight dispatch for the landing climbout performance dictated flap setting.
239 feet 9 inches (73.1 meters)
206 feet 6 inches (63 meters)
199 feet 11 inches (60.9 meters)
102 feet 5 inches (31.2 meters)
129 feet (39.3 meters)
149 feet (45.4 meters)
182 feet (55.4 meters)
154 feet (46.8 meters)
15 feet (4.6 meters) of the wingtip or 51 feet (15.7 meters) of the nose
15 feet (4.6 meters) of the wingtip of 40 feet (12.2 meters) of the nose
40 feet (12.2 meters) of the wingtip or 15 feet (4.6 meters) of the nose
51 feet (15.7 meters) of the wingtip or 15 feet (4.6 meters) of the nose
156 feet (47.5 meters)
182 feet (55.4 meters)
145 feet (44.2 meters)
154 feet (46.8 meters)
10,000 feet
14,000 feet
9,800 feet
8,400 feet
None, autoland is always allowed.
Before the airplane descends more than 50 feet below the MDA unless it is coupled to an ILS glideslope and localizer or in the go-around mode.
200 feet AGL
None, autoland is always allowed.
Before the airplane descends more than 50 feet below the MDA unless it is coupled to an ILS glideslope and localizer or in the go-around mode.
50 feet RA
200 feet AGL
3.0 degrees
2.5 degrees
2.25 degrees
2.75 degrees
3.25 degrees
3.0 degrees
3.5 degrees
3.75 degrees
Automatic landings may be accomplished using flaps 20, 25 or 30.
Automatic landings may be accomplished using flaps 20 or 30 when LAND 2 or LAND 3 is annunciated.
Automatic landings may be accomplished using flaps 20, 25 or 30 when LAND 2 or LAND 3 is annunciated.
Automatic landings may be accomplished using flaps 20 or 30.
Jet A
Jet B
JP-4
JET B and JP-4
Reverse thrust use below 60 knots is prohibited.
Intentional selection of reverse thrust below 10 feet radio altitude is allowed.
Backing the airplane with the use of reverse thrust is prohibited.
Backing the airplane with the use of reverse thrust and intentional use of reverse thrust in flight are prohibited.
Main tanks must be maintained full on the ground if center tank fuel is loaded
Main tanks must be scheduled to be full if center tank fuel is loaded.
Fuel crossfeed valves must be close for landing.
Fuel imbalance must not exceed 1000 pounds (500 kilograms)
10,000 feet
14,000 feet
9,800 feet
3,400 feet
Up 2% and down 2%
Up 3.25% and down 2.5%
Up 2.5% and down 2.5 %
There is no slope limitation.
0.11 psi
11.1 psi
9.1 psi
8.5 psi
Pilots are authorized to deviate from their current ATC clearance to the next extent necessary to comply with TCAS II resolution advisory
Pilots are not authorized to deviate from their current ATC clearance to the extent necessary to comply with TCAS II resolution.
TCAS information and advisories can not be used when not in radar controlled airspace.
Pilots are authorized to comply with a TCAS II resolution advisory when the airplane transponder is in OFF or STBY.
10 NM
5 NM 1 5 NM 115 NM
20 NM
18 NM
A QFE altitude reference for the primary flight display must be selected in the flight management system whenever QFE is used instead of QNH. The use of VNAV wit QFE selected is prohibited.
A QFE altitude reference for the primary flight displays must be selected in the flight management system whenever QFE is used instead of QNH.
The use of look-ahead terrain alerting and terrain display functions are permissible during QFE operations.
A QFE altitude reference for the primary flight display automatic selects QFE reference in the flight management system.
10 knots
15 knots
18 knots
20 knots
212 feet 7 inches (64.8 meters)
206 feet 6 inches (63 meters)
119 feet 11 inch (60.9 meters)
239 feet 9 inch (73.1 meters)
152 feet (46.3 meters)
149 feet (45.4 meters)
182 feet (55.4 meters)
160 feet (48.8 meters)
15 feet (4.6 meters) of the wingtip or 44 feet (13.4 meters) of the nose
15 feet (4.6 meters) of the wingtip or 40 feet (12.2 meters) of the nose
40 feet (12.2meters) of the wingtip or 15 feet (4.6 meters) of the nose
51 feet (15.7 meters) of the wingtip or 15 feet (4.6 meters) of the nose
156 feet (47.5 meters)
182 feet (55.4 meters)
186 feet (56.5 meters)
154 feet (46.8 meters)
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