DAFCS Flashcards
What DAFCS functions are provided under the core features?
- Damping of angular rates
- Control response augmentation
- Bank Angle Hold
- Heading Hold
- Directional Static Stability
- Automatic Turn Coordination above 40 KCAS
- Limited Automatic Turn Coordination below 40 KCAS
- Roll Axis Attitude Command/Attitude Hold (ACAH) response below 40 KCAS
- Longitudinal Static Stability
- Airspeed Stability above 40 KCAS
- Pitch Attitude Stability below 40 KCAS
- LCT scheduling (WHEN IN AUTO)
Core features enhance stability and control of the aircraft
What DAFCS functions are provided under the native (pilot selectable) features?
- DECEL to hover
- Position Hold (PSN)
- Inertial Altitude Hold (ALT-INRT)
- Radar Altitude Hold (ALT-RAD)
- Descent
- Roll Wings Level Mode (LEVEL or RWL)
- Velocity Hold
Native features allow pilots to manually select control modes
Where are Native features selected by the pilot?
The TCL
TCL stands for Thrust Control Lever
When do the Core features become active?
When DAFCS selector switch is placed in 1, 2 or both positions
What programs the LCTs based on airspeed and WOW condition when in AUTO?
LCTs are programmed by the DAFCS
When the LCT switch is in MANUAL, how are the LCTs controlled?
Manually by the pilot
Which components are controlled by DAFCS to make inputs into the pitch, roll, yaw and thrust axes?
- Extensible link portion
- Differential Airspeed Hold Actuator (DASH)
- Thrust Cockpit Control Driver Actuator (CCDA)
- Pitch Cockpit Control Driver Actuator (CCDA)
- Longitudinal Cyclic Trim Actuators (LCTs)
- Control Position Transducers (CPTs)
These components work together to manage flight control inputs
What are the different DAFCS regimes?
- Ground
- Low Speed
- FWD Flight
When accelerating from a hover, what is the max airspeed that can be flown to remain within the Low-Speed Regime?
45 KCAS
What is Rate Damping?
The Resistance to a rate motion not caused by the pilot in the pitch, roll and yaw axes
What is Control Response Augmentation/ Quickening?
Amplification of the pitch, roll and yaw control inputs
What does the acronym CPT stand for?
Control Position Transducers
What does the acronym LVDT stand for?
Linear Variable Differential Transducer
What information does each LVDT inside the CPTs send to each FCC?
Position and rate of motion (if in motion) to each FCC
If the aircraft moves without CPT movement, the FCCs know the movement was caused by what?
Outside force (wind, turbulence etc.)
What information do the EGIs provide to the FCCs?
Pitch, roll and yaw information
What should you do if the LCT actuators fail to position to GND during taxi or slope operations?
Select manual Adjust manually
Will the Longitudinal Cyclic Trim Actuators (LCT’s) function with the DAFCS switch in the off position?
Yes
Do not manually extend the LCT actuators beyond the GND position on the cyclic trim indicators at airspeeds below ______ KCAS.
60 KCAS
When does the Ground Regime become active?
When the L and R GND CONT light is active
Which CPT input is cancelled when both WOW switches are engaged?
Pitch CPT
When the landing gear proximity switches/WOW switches are activated, the DAFCS input into the pitch ILCA is reduced by what percent?
50%
How does this reduction help the pilot control the aircraft?
Reduces porpoising while 2-wheel taxiing
When does Low-Speed Turn coordination become active?
When accelerating above 45 KCAS
What is the maximum back angle for Low-Speed Turn Coordination?
45 Degrees
When does Turn Coordination become active?
Above 40 Knots
VEL can be armed at any speed but will activate only below ___ knots forward groundspeed.
35 knots
It will remain active up to ___ knots forward groundspeed.
45 knots
Below ____ knots total groundspeed, the aircraft will automatically be slowed to a zero-velocity hover.
3 knots
Deceleration/Position Hold (DECEL/PSN) can be armed at any speed but will activate only below ___ knots forward GS.
65 knots
It will remain active at up to ___ knots GS.
70 knots
At what groundspeed does the PSN feature become captured?
Less than 1 knot
In DECEL, the AFCS TRIM switch biases the speed by ___ knot/sec in the direction of actuation.
1 knot/sec