Memory Limitations Flashcards
Max Operating Pressure Altitude
(787-8, 787-9)
43,100 feet
Max Operating Pressure Altitude
(787-10)
41,100 feet
Max Takeoff and Landing Tailwind Component
15 knots
Turbulent Air Penetration Speed
Severe Turbulence at and above 25,000 feet
310 knots/ .84 mach which is lower
Turbulent Air Penetration Speed
Severe turbulence below 25,000 feet
290 knots
Takeoff Crosswind Component
>430,000 lbs Dry Rwy, CG < 20
40 knots
Takeoff Crosswind Component
350,000 lbs Dry Rwy, CG < 20
40 knots
Takeoff Crosswind Component
< 270,000 lbs Dry Rwy, CG < 20
40 knots
Landing Crosswind Component
RWY Dry
40 knots
AUTOFLIGHT LIMITATIONS
Autopilot/ Flight Director System
(5)
- Do not engage the autopilot below a minimum altitude of 200 feet AGL after takeoff
- Autoflight capability may only be used for operations to runways at or below 8,400 AFE
- Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below 135feet AGL
- With LAND 2 or LAND 3 annunciated and glidepath angles greater than 3.25, the autopilot
must be disengaged below 100 feet AGL - Do not use FLCH on final approach below 1000 feet AFE
Max wind component Low Vis HUD Takeoff
Headwind 25 knots
Tailwind 15 knots
Crosswind 15 knots
SA CAT I Approach Max Crosswind
15 knots
ILS Automatic Landing Max Glideslope Angle
3.25
ILS Automatic Landing Min Glidepath Angle
2.5
Communication/Fueling Limitation
Do not operate the HF radio during fueling operations