Limitations Flashcards
B787 Limitations
MAXIMUM OPERATING PRESSURE ALTITUDE (787-8, 787-9)
43,100 feet
MAXIMUM OPERATING PRESSURE ALTITUDE
(787-10)
41,100 feet
MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT
15 knots
TURBULENT AIR PENETRATION SPEED (Severe turbulence at and above 25,000 feet)
310 knots/.84 Mach (whichever is lower)
TURBULENT AIR PENETRATION SPEED (Severe turbulence below 25,000 feet)
290 KIAS
Takeoff Crosswind Guidelines
40 knots Crosswind Component
Landing Crosswind Guidelines (Valid for all engine and one engine inoperative operations at any weight and CG)
40 knots Crosswind Component
ICING CONDITIONS DEFINITION
Icing conditions exist when OAT (ground) or TAT (flight) is 10°C or below.
Note: Use TAT to determine EAI selection during ground operations to avoid nuisance ANTI-ICE ON EICAS messages.
Autopilot minimum engagement altitude after takeoff (OpSpec C071)
200 feet AGL
Maximum Airfield Elevation for Autoland
8400 feet
Autopilot Disengagement Height, without LAND 2 or LAND 3 annunciated
“…the autopilot must be disengaged below 135 feet AGL.” (1.30.4)
Autopilot Disengagement Height with LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25° (OpSpec C071)
“…the autopilot must be disengaged below 100 feet AGL.” (1.30.4)
Do not use FLCH on final approach below 1000 feet AFE. (T/F)
TRUE
LOW VISIBILITY (HUD) TAKEOFF (RVR <500) Wind Components
25 knots headwind
15 knots tailwind
15 knots crosswind
SA CAT I APPROACHES
Maximum wind component speed
15 knots crosswind