Bold Face Flashcards
(34 cards)
BRAKE FAILURE
WARNING: If uncontrolled departure from hard surface will occur, consider PCL FUEL OFF, or ejection if at high speed.
- BRAKES……… RELEASE
- SERVICABLE BRAKES……… GRADUALLY RE-APPLY
EMERGENCY EGRESS ON THE GROUND
WARNING: Eject if circumstances dictate; however, do not attempt to eject if:
* Occupants are not correctly strapped in
* Canopy not closed and locked
* CFS and seat pins are not removed
- SEAT PIN……………………..IN
- LEG RESTRAINTS………….RELEASE
- SEAT HARNESS…………….RELEASE
- OXYGEN MASK HOSE……DISCONNECT
- MIC-TEL……………………….DISCONNECT
- PSP………………………………DISCONNECT
- CANOPY………………………OPEN
- EXIT THE COCKPIT
EMERGENCY LANDING CHECKS
CAUTION: Anti-skid is inoperative when the main hyd system is not operating. Apply the brakes carefully with anti-skid inoperative.
- AIRSPEED………………….BELOW 180 KIAS
- LANDING GEAR HANDLE………DOWN
- EMER LDG GR HANDLE………..PULL
- FLAPS………………………….AS REQUIRED
When aircraft has stopped:
- BATT 1 AND BATT 2……………..OFF
ENGINE FIRE OR SMOKE AND FUMES –
ON GROUND
MFD FIRE
DWP FIRE
WARNING: Activating the EO2 may lead to pure oxy flowing into the cockpit during egress. However, operate the EO2 if incapacitation is assessed to be a greater risk.
CAUTION: Anti-skid is inoperative when the main hyd system is not operating. Apply the brakes carefully with anti-skid inoperative.
Normal powered braking is not available when the main hyd system is not operating. Manual braking requires higher than normal pressure and travel.
- ACS SHUT OFF…………….…PULL
- PCL……………………………….FUEL OFF
- FUEL HYD CUTOFF…………PULL
- BATTS AND GENS………….OFF
- BRAKES…………………………AS REQUIRED
- EMERGENCY EGRESS ON THE GROUND
ENGINE FIRE – IN FLIGHT
MFD FIRE
DWP FIRE
WARNING: Monitor EO2 contents and descend to a safe altitude before EO2 is exhausted.
CAUTION: Observe eng limits manually and avoid rapid power changes with the PMS in manual mode.
1. PCL……………………MINIMUM PRACTICAL
2. EO2…………………………………..PULL
3. ACS SHUT OFF…………………..PULL
4. CHECK FOR FIRE
If fire confirmed:
5. PCL……………………………………FUEL OFF
6. FUEL HYD CUTOFF…………….PULL
7. BATT 1………………………………OFF
8. GEN 1 AND GEN 2……….…….OFF
If fire continues:
9. EJECT
If fire is not confirmed or FIRE warnings go out:
10. PMS……………………………….MANUAL
SMOKE OR FUMES IN THE COCKPIT – IN FLIGHT
MFD FIRE
DWP FIRE
WARNING: Monitor EO2 contents and descend to a safe altitude before EO2 is exhausted.
Land as soon as possible following smoke or fumes in the cockpit.
- EO2………………………………PULL
- DESCEND BELOW 10 000 FT AIRCRAFT ALTITUDE
- OXYGEN………………………..OFF (BOTH COCKPITS)
- ACS SHUT OFF………………PULL
- CABIN PRESS………………..RAM
If fumes continue:
- GEN 1 AND GEN 2………..OFF
ABORTED TAKE-OFF
WARNING: Eject if there is likely risk of collision.
If uncontrolled departure from the hard
surface will occur, consider PCL FUEL OFF, or ejection if at high speed.
CAUTION: Anti-skid is inoperative when the main hyd system is not operating. Apply the brakes carefully with anti-skid inoperative.
Normal powered braking is not available when the main hyd system is not operating. Manual braking requires higher than normal pressure and travel.
- PCL……………………………….IDLE
- BRAKES……………………..….AS REQUIRED
ENGINE FAILURE AFTER TAKE OFF
- PCL……………………………………….FUEL OFF
WARNING: Delaying ejection may place the aircraft in marginal conditions for safe ejection. Eject if unable to carry out a forced landing safely.
If a suitable runway is available:
- FUEL HYD CUTOFF…………………….PULL
- EMERENCY LANDING CHECKS
ENGINE MECHANICAL FAILURE
- PCL……………………….……..FUEL OFF
- FUEL HYD CUTOFF………..PULL
WARNING: Monitor EO2 contents and descend to a safe altitude before EO2 is exhausted.
- EO2……………..PULL IF ABOVE 10 000 FT
PMS FAILURE (PMS MANUAL)
MFD PMS MANUAL
DWP PMS
CAUTION: Observe eng limits manually and avoid rapid power changes with the PMS in manual mode.
- PCL…………………………CONTROL ENGINE LIMITS MANUALLY
When at safe height:
- PCL…………………………MID TO LOW POWER (PCL < 55◦)
ENGINE SURGE
CAUTION: Minimise power changes following engine surge.
NOTE
If an engine surge is identified, set aircraft
attitude for minimum sideslip and AOA as
soon as practicable. Achieve best glide
speed as soon as practicable.
- PCL……………………………..……….IDLE
Indications:
* Loss of power
* ITT excessively high or fluctuating
* Unusual engine noise (popping or rumbling)
ENGINE FLAMEOUT
CAUTION: Minimise power changes following engine flameout.
NOTE
If an engine flameout is identified, set
aircraft attitude for minimum sideslip and
AOA as soon as practicable. Achieve best
glide speed as soon as practicable.
- PCL………………….……………..IDLE
Indications:
* Loss of power
* ITT below 400°C
* NG decreasing:
* below 80% PMS auto
* below 70% PMS man
ENGINE TORQUE
MFD ENG TORQUE
DWP ——
- PCL………………….MINIMUM PRACTICAL
PROPELLER SPEED
OVERSPEED – NP ABOVE 2200 RPM (WARNING)
MFD PROP SPEED
DWP ——
CAUTION: Continue flight at low speed using minimum practical power.
Monitor the engine for indications of mechanical failure.
- PCL………………….MINIMUM PRACTICAL
- AIRSPEED………..REDUCE
ENGINE TEMPERATURE – ON GROUND
MFD ENG ITT
DWP ——
CAUTION: Ensure NP is not maintained between 1600 and 1900 RPM with tailwind.
NOTE: Above 63% NG the ITT limit is 860C
If ITT rapidly increases towards and exceeds 750°C in ground idle with warning displayed:
- PCL……………………………FUEL OFF
ENGINE TEMPERATURE – IN FLIGHT
(High or low?)
MFD ENG ITT (red)
or ENG ITT (yellow)
DWP ——
ITT ABOVE 860C
- PCL………………..MINIMUM PRACTICAL
ITT BELOW 350C:
CAUTION: Low ITT may indicate engine flameout.
ENGINE SPEED
(High or low?)
MFD ENG NG (red)
or ENG NG (yellow)
DWP ——
NG BELOW 50.7% (CAUTION)
CAUTION: Low ITT may indicate engine flameout.
- IGNITERS……………………ON
- PCL…………………………….SLOWLY INCREASE POWER
NG ABOVE 104% (CAUTION FOR 2 SECOND, THEN WARNING)
- PCL…………………MINIMUM PRACTICAL
OIL PRESSURE OUT OF LIMITS
MFD OIL PRESS
or OIL PRESS
DWP OIL
NOTE: Oil pressure may be as low as 40 psi during aerobatics if recovery is within 20 seconds.
Verify under positive G.
If warning or caution remains indicated:
- PCL……………..MINIMUM PRACTICAL
OIL TEMPERATURE HIGH – ON GROUND
MFD OIL TEMP
DWP ——
OIL TEMP WARNING
- PCL…………………………………….FUEL OFF
OIL TEMPERATURE HIGH - IN FLIGHT
MFD OIL TEMP
DWP ——
OIL TEMP WARNING
- PCL……………………MINIMUM PRACTICAL
UNCOMMANDED POWER CHANGES
CAUTION: Observe eng limits manually and avoid rapid power changes with the PMS in manual mode.
NOTE
The maximum approved torque is 2850 ft lb
(67.5%) with the PMS in manual mode.
- PCL…………………………IDLE
- PMS……………………….MANUAL
- PCL…………………………AS REQUIRED
METAL PARTICLES DETECTED IN GEARBOX
MFD CHIP PROP
or CHIP AGB
DWP CHIP
CAUTION: Minimise power changes with CHIP indicated.
Monitor the engine for signs of mechanical failure.
Shut down the engine as soon as possible after landing
- PCL……………………MINIMUM PRACTICAL
- LAND AS SOON AS POSSIBLE
OXYGEN SYSTEM OFF (BOTH COCKPITS)
MFD OXY OFF
DWP OXY
If above 10 000ft cabin altitude:
- EO2……………….…..PULL
- DESCEND BELOW 10 000 FT CABIN ALTITUDE
MFD OXY WARNING
MFD OXY
DWP OXY
If above 10 000ft cabin altitude:
- EO2……………….…..PULL
- DESCEND BELOW 10 000 FT CABIN ALTITUDE
