Limitations Flashcards
757 Max Landing Weight
198,000 lbs
757 Max T/O Weight
230,000 lbs
Normal Taxi Speed
20 knots
Long Straight Taxi Speed
30 knots
Approaching a turn taxi speed
Slow
Turns on a dry surface
10 knots
Max Crosswind T/O & Land dry/damp
30 knots
Max Crosswind T/O & Land braking action fair/medium
15 knots
Max Crosswind T/O & Land braking action poor
10 knots
Max Crosswind Landing single engine
30 knots
Max Crosswind Autoland
25 knots
Max Crosswind Autoland Cat II or III
15 knots
B757 Max tail wind T/O & Landing
10 knots
B757 Max tail wind Autoland
10 knots
B767 Max tail wind Autoland
15 knots
Max headwind for Autoland 757 and 767
25 knots
Minimum runway width for 180 degree turn (B757)
120 feet or 36.6 meters
B757 Max ceiling
42,000 feet
Icing conditions exist when…
OAT on the ground and for T/O or TAT in-flight is 10 degrees C or below and visible moisture in any form is present.
Visibility 1 mile or less!
Do not use engine anti-ice if;
- Temp is below -40 C
2. Temp exceeds 10 C / 50 F
RVSM Captain’s altitude vs. F/O’s on the ground at sea level max difference.
+/- 35 ft
RVSM Captain’s altitude vs. F/O’s in flight max difference.
+/- 200 ft
RVSM Captain’s altitude or F/ O’s for a known elevation max difference.
+/- 75 ft.
Minimum altitude for autopilot engagement
1000 feet agl
Max imbalance between fuel tanks
B757 1950 lbs
B767 2500 lbs with main tank fuel less than 48,000 lbs
B767 1500 lbs with main tank fuel greater than 48,000 lbs
Do not use the A/P below 100 feet radio altimeter with airport pressure altitudes above
B757: 8400 Feet
B767: 8500 Feet
RVSM Captain’s altitude vs. F/O’s on the ground at sea level max difference.
+/- 35 ft
RVSM Captain’s altitude vs. F/O’s in flight max difference.
+/- 200 ft
RVSM Captain’s altitude or F/ O’s for a known elevation max difference.
+/- 75 ft.
Authorized Flaps for Autoland
25 or 30 only
B757 fuel tank quantity
Main tanks: 15,450 x 2 = 30,900
Center tank: 48,997
Total: 79,897
