NEW Emergency Procedures Flashcards
Partial power loss in flight:
CAUSE check: move PCL, fuel pumps, ignition
- PCL —————————- IDLE
- MOR ————————– ADVANCE SLOWLY
if a compressor stall occurs and/or ITT exceeded: - MOR ————————– RETARD
if engine falls below 50% Ng: - STARTER ——————– 2 SECONDS
(when starter is pressed, A/P disengages and EFIS goes dark) - MOR ————————– ADVANCE TO >80% Ng
- LAND ————————- ASAP
Do not permit anything less than 65% Ng, maintain 75% until touchdown
NOTE: Go-around may not be an option, total landing distance increased by a factor of 2, do NOT use MOR on ground for taxi
CONFIRM CHECKLIST WITH FO!
Engine failure before rotation:
- PCL —————————— IDLE
- BRAKING ———————- MAX
If runway overrun imminent: - CONDITION LEVER ——– IDLE/CUTOFF
- FUEL EMERG. —————- OUT AND UP
- GANGBAR ——————– OFF
EVACUATE
Engine failure after rotation (gear down):
if altitude is not sufficient to land straight ahead, turn only to avoid obstacles
- FLAPS —————————- 40
- FINAL REF ———————- 84KTS
- PCL ——————————- IDLE
- CONDIITON LEVER ——— IDLE/CUTOFF
- FUEL EMERG. —————– OUT AND UP
after touchdown: - GANGBAR ——————— OFF
EVACUATE
Engine failure after rotation (gear up):
- LANDING GEAR ———————– DOWN
- N ESNTL BUS OVRD —————– OVRD ON
- FLAPS ———————————— 40
- FINAL REF —————————— 84KTS OR 98 FLAPS 15
- PCL —————————————- IDLE
- CONDITION LEVER —————— IDLE/CUTOFF
- FUEL EMERG. ————————- OUT AND UP
After touchdown:
8. GANGBAR —————————– OFF
Be sure to abide by your takeoff brief; FO to get gear, flaps, N ESNTL for you and advice ATC!
Total power loss:
Initially, check fuel amount, fuel flow, select fuel pumps and ignition to ON
- PCL ———————————- IDLE
- CONDITION LEVER ————- IDLE/CUTOFF
- REMAINING FUEL ————— CHECK
- AIR START ————————– CONDUCT
transfer controls to FO, 114kts, carry out air start checks - IF >13,500’ ————————- EMERGENCY DESCENT
- IF AIR START UNSUCESSFUL, FORCED LANDING
AIR START:
1. PCL ———————————IDLE
2. CONDITION LEVER ———— IDLE/CUTOFF
3. FUEL EMERG. ——————- FULL IN
4. ELECTRICAL LOAD ———— REDUCE/SHED
(lights, cabin heat, recircs, anti-ice IF WEATHER PERMITS)
5. ECS ——————————— OFF
6. GEN 2, GEN 1 ——————- OFF
7. BAT 1(and 2) ——————– ON
8. AIR START ENVELOPE ——- CHECK
(not possible above 20,000ft, make emergency descent)
9. STARTER ————————- ON
10. IGNITION ———————- ON
11. CONIDITON LEVER ——— GI ABOVE 13% Ng
12. ITT & NG ———————– MONITOR
When stable above 60% Ng:
13. IGNITON ———————– AUTO
14. CONDITION LEVER ——— FI
15. GEN2, GEN 1 —————– ON
16. ELECTRICAL ——————- AS REQ’D
17. ECS —————————— AUTO
1:15
Multiply altitude by 2.5 to get distance
Air start:
Do NOT attempt more than 1 air start, it discharges battery to a critical endurance
- PCL ———————————IDLE
- CONDITION LEVER ———— IDLE/CUTOFF
- FUEL EMERG. ——————- FULL IN
- ELECTRICAL LOAD ———— REDUCE/SHED
(lights, cabin heat, recircs, probes IF WEATHER PERMITS) - ECS ——————————— OFF
- GEN 2, GEN 1 ——————- OFF
- BAT 1(and 2) ——————– ON
- AIR START ENVELOPE ——- CHECK
(not possible above 20,000ft, make emergency descent) - STARTER ————————- ON
- IGNITION ———————- ON
- CONIDITON LEVER ——— GI ABOVE 13% Ng
- ITT & NG ———————– MONITOR
When stable above 60% Ng: - IGNITON ———————– AUTO
- CONDITION LEVER ——— FI
- GEN2, GEN 1 —————– ON
- ELECTRICAL ——————- AS REQ’D
- ECS —————————— AUTO
NOTE: with single battery, an air start causes a transient DC BAT voltage drop causing A/P and EFIS/AHRS to go offline. Aircraft should be straight and level during this phase.
Engine fire on ground:
- PCL ———————————— IDLE
- CONDITION LEVER ————– IDLE/CUTOFF
- ECS EMERG. ———————— OUT AND UP
- FUEL EMERG. ———————- OUT AND UP
- RADIO ——————————– EMERG. CALL
- GANGBAR ————————— OFF
- PARKING BRAKE —————— ON
EVACUATE, FIRE EXTINGUISHER
Engine fire in flight:
After identifying fire and carrying out final checks, ask FO to plug in nearest, advise ATC to descend, and read aloud checklist
- PCL ——————————– REDUCE TO MINIMUM
(reduce to minimum to maintain level flight) - ECS EMERG. ——————– OUT AND UP
- OXYGEN MASKS ————– ON,
- CREW OXYGEN ————— ON
only if cabin pressure is lost: - PAX OXYGEN —————— ON
- FIRE ——————————- CONFIRM IT EXISTS
- FUEL EMERG. —————– OUT AND UP
- CONDITON LEVER ——— IDLE/CUTOFF
- EMERGENCY DESCENT/ FORCED LANDING
Cockpit/cabin fire, smoke or fumes:
After doing initial steps, give FO control to proceed direct nearest, a descent below 10,000’, and prepare checklist
- OXYGEN MASKS ——————— ON
- CREW OXYGEN ———————– ON
- PAX OXYGEN ————————– ON
- PASSENGERS ————————– INSTRUCT TO DON MASKS
- AIRCRAFT —————————— DESCEND BELOW 10,000’
- GPS ————————————— PROCEED DCT AIRPORT
if a smoke evacuation is required: - ECS EMERG. —————————- OUT AND UP
- ECS —————————————- DUMP
- DV PORT ——————————– OPEN
- FANS ———————————– ON HIGH
- FIRE EXTINGUISHER ————— USE
if source is known, pull respective CCB. if not: - BUS TIE CB ————————— OUT (overhead)
- GEN 2 TIE CB ———————— OUT (overhead)
- GEN 1(BAT 2) ———————– OFF
if smoke persists: - GEN 1 ——————————— ON
- GEN 2 ——————————— OFF
if smoke STILL persists: - GEN 2 ————————————– ON
- BAT 1 ————————————— OFF
if smoke STILL AGAIN persists: - All electrical equipment off.
NOTE: in any case, do NOT pull CABIN FAN or U/F FAN associated with the aux. cabin heating system
Oil pressure 60 - 90 PSI:
EIS master caution blinking!
- Ng ————- Above 72%
- Torque —— Reduce below 23.9
- Aircraft —— Land as soon as practical
Oil pressure below 60 PSI or above 135 PSI:
Land as son as possible using minimum torque.
Retain glide capability, i.e. follow donut
Oil temp above 105:
- PCL ———————– REDUCE POWER
if oil temperature does not reduce to normal: - LANDING GEAR ——- LOWER
- LAND AS SOON AS PRACTICAL
CHIP CAWS on ground/in flight:
Before engine start on ground:
DO NOT START
After engine start on ground:
- RETURN TO PARKING
- SHUT DOWN ENGINE
- INSPECT CHIP DETECTOR AND ENGINE IF REQ’D
In flight:
MONITOR ENGINE PARAMITERS
REDUCE POWER TO MINIMUM FOR SAFE FLIGHT
LAND AS SOON AS PRACTICAL
After landing:
INSPECT CHIP DETECTOR AND ENGINE IS REQ’D
When does OIL QTY CAWS light illuminate?
1 minute after shutdown or 1 minute before start with battery running
Propeller overspeed:
- PCL —————– REDUCE
- SPEED ————- REDUCE
if Np remains between 1760 and 1870: - PCL —————– REDUCE TO IDLE IF NEEDED
- SPEED ————- REDUCE TO BELOW 120kts
- LAND ASAP
NOTE: retain best glide just in case engine fails. In the event of heavy vibration or speed runaway, be prepared to shut engine down
Propeller low pitch (PROP LOW P):
PROP LOW P CAWS light!
- PCL ————— ENSURE FORWARD OF IDLE
if not able to maintain speed and altitude: - CONDITION LEVER ————– IDLE/CUTOFF
- EMERGENCY LANDING ——– CARRY OUT
Propeller underspeed:
When prop is indicating below 1640 RPM, EIS will blink
In flight:
1. PCL —————— INCREASE POWER
2. SPEED ————– INCREASE
On ground:
1. Retard PCL aft of idle OR increase power until above 950 RPM
Minimum GI RPM range is 650-950 RPM. EIS will blink for this
What are the two types of emergency descents?
Engine failure, flown for max range
and
Engine running, flown for max descent rate
Maximum range descent (single battery):
1.PCL ———————————— IDLE
2. CONDITION LEVER ————– IDLE/CUTOFF
3. A/C CONFIG. ———————– GEAR UP, FLAPS 0
4. SPEED ——————————– 114kts (or ride donut)
5. OXYGEN MASKS —————— ON if cab. alt. >10,000’
6. PAX OXYGEN ———————- ON if cab. alt. >10,000’
7. PAX ———————————– BRIEFED
(Seats upright, seatbelts on, stow objects)
8. ELECTRICAL LOAD ————— SHED LOAD
9. AIR START ————————– CONDUCT
if air start unsuccessful:
10. DESCENT RATE —————— INCREASE to below 10,000’
11. WINDSHIELD HEAT ———— HEAVY, draws less!
12. ECS EMERG. ———————- OUT AND UP
NOTE: When retracting flaps and/or gear, AHRS and EFIS could go offline and severe battery draw will occur. However, when in clean, it significantly increases gliding distance. OIL QTY CAWS may appear while in a long extended glide with no power. Disregard this for engine air start.
When time permits, what CBs can we pull to reduce the electrical load?
AHRS 2 —————— on AV1 BUS and AV2 BUS
EFIS 2 ——————– on AV1 BUS
RMI 1 ——————– on AV1 BUS
RMI 2 ——————– on AV2 BUS
EFIS EADI ————— on AV2 BUS
LH PITOT DE ICE —– on GEN 1 BUS
What are switches we can turn off in the cockpit (excluding CCBs) to reduce electrical loads?
- External lights
- Internal lights
- De-icing systems, ALL besides probe heat
- Nav/Comm2
- ADF
- Transponder
- WX Radar
Maximum range descent (dual battery):
- PCL ——————————- IDLE
- CONDITION LEVER ———- IDLE/CUTOFF
- A/C CONFIG. ——————- GEAR UP/ FLAPS UP
- SPEED —————————- 114kts (or ride donut)
- AUTOPILOT ——————– ENGAGE IAS, and NAV when direct nearest airport
- OXYGEN MASKS ————– ON if cab. alt. >10,000’
- PAX OXYGEN —————— ON if cab. alt. >10,000’
- PAX ——————————- BRIEFED
- ELECTRICAL LOAD ———- SHED LOAD
as follows: external lights, de-ice systems, internal lights, LH PITOT DEICE on GEN 1 BUS out
CAUTION:
Monitor BAT 1 & BAT 2 AMPS. If one is positive, switch off that battery (its feeding the other one, possible overcharge). After 5 minutes the battery can be switched on again. if it happens again shut that battery off.
NOTE: When retracting flaps and/or gear, AHRS and EFIS could go offline and severe battery draw will occur. However, when in clean, it significantly increases gliding distance.
Maximum rate descent:
- PCL ————————- IDLE
- LDG GEAR —————- EXTEND BELOW 177KTS
- SPEED ———————- Mmo/Vmo
- OXYGEN MASKS ——– PREPARE
- PAX OXGYEN ————- ON and calculate oxygen duration and check flow to pax
- WINDSHIELD HEAT —- AS REQ’D
CAUTION: In turbulence reduce speed to 170kts
A fully charged battery will last as follows:
60 AMPS = 20mins
50 AMPS = 30mins