Emergency Procedures+ Flashcards
ENGINE FIRE SHUTDOWN
- Power Lever (affected engine) - FLT IDLE
- FIRE Handle (affected engine) - PULL
- Agent (affected engine) - Discharge, as required
APU FIRE
- APU Fire handle - PULL
- AGENT - Discharge, as required
ABORTED TAKE OFF
- State - “ABORT, ___”
- Power Levers (All) - FLT IDLE
- Maximum Braking - As required
———————————————— - Nosewheel steering - As Required
- Power Levers (all) - GND Idle
- State - All Four/Inboards/Outboards
- Power Levers - MAX REV
- ACAWS Crew Action - Accomplish
INADVERTENT IMC
- Announce - “Inadvertent IMC”
- Transition - Establish Instrument Scan
- Maneuver - As required
FIRE/SMOKE/FUMES ELIMINATION
- OXYGEN - ON, 100%
If at any time during the execution of this checklist the fire, smoke, or fumes decrease in intensity, stop and ascertain what systems are affected and isolate the component(s) (if able) and restore aircraft power
RAPID DECOMPRESSION
- OXYGEN - ON, 100%
Windshear Recognition
o +/- 20 KCAS
o +/- 500 fpm Alt Changes
o +/- 6* Pitch Attitude Changes
o +/- 1.5 dot G/S Deviation
o Unusually steep/shallow pitch attitudes
o Unusually high/low Pwr Settings
Recommended:
o Use 50% Flaps for LDG
Windshear Recovery
- T/O Power and Level Wings
- Pitch to 15* Nose up to
- Maintain 10 kts > Stall Caret
- PM Calls RA, A/S, Sink Rate
- Do not change config until out of alert and stable
- Do not use G/A F/D – Does not optimize Perf
Abort Start With FIRE handle When:
- Engine Fire
- Engine MGT High
- Start Valve Open
- MGT rapidly approaches/exceeds 807* C
- Visible fluid leak/smoke or flames
FIRE Handle Secures:
HBOFFA
H: HYDRAULIC
B: BLEED AIR
O: OIL
F: FUEL
F: FEATHERS PROP
A: ARMS/ROUTES FIRE EXT AGENT
Go-Around
- Announce Go-Around
- Go-Around Button - Press
- Power Levers - set TAKEOFF as req
- Pitch - Follow FD
- Flaps - Check/Set 50%
- Gear - Up
- Rudder Trim - As Req
- Flaps - Up (Passing FUSS)
Three Engine Go-Around
- Announce Go- Around
- Go-Around Button - Press
- Power Levers - set TAKEOFF as req
- Bank - 2-5* into operating engines
- Pitch - Follow FD
- Flaps - Check/Set 50%
- Gear - Up
- Rudder Trim - As Req
- Flaps - Up (Passing FUSS)
Four Engine Flameout
- Pitch Attitude - Adjust for airspeed control (NG between 15-28%)
- Power Levers (all) - FLT IDLE
- Fuel X Feed Switches - Close
- Inboard (No. 2 and No. 3) ENGINE START switches - STOP, START, release
- Outboard (No. 1 and No. 4) ENGINE START switches - STOP, START, release
Loss of Normal Brake Pressure
- AUX PUMP switch - ON
- BRAKES - EMER
Engine Surge Identification
Characterized by several ACAWS in succession
- ENG 1 (2, 3, or 4) MGT HI (W)
- ENG 1 (2, 3, or 4) MGT HI (C)
- HOT START 1 (2, 3, or 4) (C)
- ENG 1 (2, 3, or 4) FAIL (C)
- ENG 1 (2, 3, or 4) A/I VLV FAIL (C)
- ENG 1 (2, 3, or 4) FLAMEOUT (C)
Clear Air Icing Procedure
Ice Protection Panel
1. ENG Switch - Off (at or above FL210) or AUTO (below FL210)
2. WING/EMP - AUTO (Verify DE-ICE Selected)
When ICE DETED (A) or LEVEL 2 ICE (A) or crew detects indication of clear air icing
3. Autothrottle - Disengaged
4. Power Levers (all) - Immediately retard approx two knob widths, no lower than FLT IDLE
5. WING/EMP switch - ON (Verify DE-ICE selected)
6. After WING/EMP A/I has been ON approx 5 seconds - ENG Switch - ON
After NG stablized (approx 15 seconds)
7. Power Levers (all) - Slowly advance, as requried, while monitoring MGT
8. If at or above FL210 and conditions permit descend below FL210 and maintain cruise airspeed
After 6 minutes since ICE DETECTED (A) or LVL 2 ICE (A) has cleared:
ICE PROTECTION panel, in this order:
9. ENG switch - OFF (at or above FL210)
10. WING/EMP switch - AUTO
Engine Surge Recovery
- Autothrottle - Disengage
- Power Levers (all) - Immediately retard approx two knob widths, no lower than FLT IDLE
- Power Lever (affected engine) - retard to FLT Idle
After NG has stabilized on nonaffected engines (approx 15 sceonds)
4. Power Levers (nonaffected engines) - Slowly advance as required while monitoring MGT
5. Descend below FL210, if conditions permit
If affected engine has decresaed to <100 HP and is not responsive to power lever movement:
6. FIRE handle - Pull
7. ENGINE START Switch - Stop
8. Airstart - As required
9. Land as soon as practicable
Engine Failure Above Refusal Speed
- Takeoff - continue
- Directional Control - Maintain
- Rotate - to target pitch attitude
- Speed - capture VOBS
- Bank Angle - 2 to 5 degrees into operating engine
- Rudder Trim - Set, as required
- GEAR - Up
- Flaps - Up
- Power Levers - Max Cont
- ACAWS Crew Action - Accomplish
- Climb Speed - Maintain
ACAWS Logic
The aural alert and the MASTER WARNING and MASTER CAUTION lights for some ACAWS alerts are inhibited for takeoff between 70 to 140 kt or 0 to 400 ft AGL. Aural alerts remain active during touch and go landings unless airspeed decreases to ≤60 KIAS on the runway with the power levers below FLT IDLE.
Place ENGINE START switch to STOP for:
- Flameout (C)
- No Lightoff (A)
- Stagnated Start (A)
- No NG within 10 seconds
- No oil px within 15 seconds of NG or ENG 1/2/3/4 NO OIL PRESS (c)
- No oil px within 15 second of NP rotation or GBOX 1/2/3/4 NO OIL PRESS (C)
- Torching
Hydraulic System Leak
- Hydraulic Engine Pump Switches (affected system) - Off
- Suction Boost Pump Switches (affected engine) - Off
- Reservoir Fluid Level - Check
— continue checklist in red book
Drift Down Procedures
1) Engine failure.
2) Set maximum continuous power (decelerate).
3) At drift down speed descend at DD speed to the lower service ceiling (3/2ENG SVC).
4) At the service ceiling accelerate to cruise speed.
Basic Assumptions for Landing Distance
o 1 Second allowance for distance traveled during transition from TD to taxi attitude
o Maximum anti-skid braking and power selection upon reaching taxi attitude
Land Immediately
Land without delay; primary consideration is to assure survival of occupants