Emergency Procedures Flashcards
Unusual attitude recovery
- Level wings
- Nose on horizon
- Center the ball
- Stop rate of climb/descent
- Control airspeed
Electrical power failure/dual generator failure
- Safe altitude and airspeed establish
- Stab - check position, slew as required
- APU emergency start procedure - perform
- Computer power, SAS 1, SAS 2, TRIM, autopilot, and STAB auto PB - ON
Warning: ensure airspeed vs stab angle limits are not exceeded. Stab auto mode is inop.
Note: the stab position indicator will be inop with no power to the AC essential bus. Attempt to check visually.
The capability of slewing the stab is retained by the DC essentially bus. Travel is limited to 35 degrees if full down and 30 if full up when a power failure occurs.
A loss of electrical power to the engine will result in activation of the engine anti ice system regardless of the position of the engine anti ice switch or the de ice master switch, reducing max torque available by up to 18%. A malfunction inlet anti ice valve can reduce torque available by up to 49%.
Unusual vibrations on deck
- Collective lower
- PCLs - OFF
- Rotor brake - apply as required
Application of the rotor brake and aggravate lead/lag tendencies and cause a mechanical failure.
Warning
Explanatory information about an operating procedure, practice, or condition, etc that may result in injury, death, or loss of aircraft if not carefully observed or followed.
Caution
Explanatory information about an operating procedure, practice, or condition that may result in damage to equipment if not carefully observed or followed.
Note
Explanatory information about an operating procedure, practice, or condition that needs to be emphasized.
Shall
Application of a procedure is mandatory
Requirements for compliance
Should
Application of a procedure is recommended
Requirements for compliance
May/need not
Application of a procedure is recommended
Requirements for compliance
Will
Indicates futurity and never indicates any degree of requirement for application of a procedure
Requirements for compliance
Land immediately
Execute a landing without delay
Land as soon as possible
Execute a landing at the first site at which a safe landing can be made
Land as soon as practicable
Further flight is not recommended. Landing site and duration of flight are at the discretion of the PIC
Actions taken for all emergencies
- Maintain control of the aircraft
- Alert the crew
- Determine the precise nature of the problem
- Complete the appropriate EP or take action appropriate to the problem
- Determine landing criteria and land as required
CB handling terms
Check: visually observe condition, do not change
Pull: if CB is in, pull CB out. If CB is out, do not change condition
Reset: if CB is out, push CB in. If CB is in, do not change condition
Cycle: if CB