Memory Limitations Flashcards
(19 cards)
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
Minimum Oil Quantity Prior to Start
18 quarts
Minimum Oil temp prior to start
The oil temp must be greater than -40C for engine start
Reverse Thrust Limitations
- Intentional selection of reverse thrust in flight is prohibited
- Backing the plane with use of reverse thrust is prohibited
Control Inputs
Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA
