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1
Q

What are the indications of an Engine Flameout

A
  1. Loss of Power
  2. ITT below 400deg
  3. NG decreasing below 80% with PMS in automatic mode and 70% with PMS in manual mode
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2
Q

ENGINE FLAMEOUT Boldface actions

A
  1. PCL …………….. IDLE
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3
Q

GEAR LOWERING FAILURE

A
  1. AIRSPEED ….. BELOW 180KIAS
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4
Q

CABIN OVERPRESSURE WARNING

A
  1. CABIN PRESS ….. PRESS DUMP
  2. PCL ……………………MINIMUM PRACTICAL
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5
Q

EMERGENCY LANDING CHECKS

A
  1. AIRSPEED …………………………….. BELOW 180KIAS
  2. LANDING GEAR HANDLE ….. DOWN
  3. EMER LDG GR HANDLE …….. PULL
  4. FLAPS ………………………………….. AS REQUIRED

When aircraft has stopped
5. BATT 1 AND BATT 2 …………… OFF

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6
Q

PMS FAILURE (PMS MANUAL)

NG Limit =
ITT Limit =
TQ Limit =

A
  1. PCL ….. CONTROL ENGINE LIMITS MANUALLY

NG 67.5% PMS Manual
ITT 860deg
TQ 2850ft-lb

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7
Q

OIL PRESSURE OUT OF LIMITS - IN THE AIR

A

If warning or caution remains indicated
1. PCL ….. MINIMUM PRACTICAL

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8
Q

PROPELLER SPEED

A

A. Overspeed - NP above 2200 RPM (warning):
1. PCL ……………… MINIMUM PRACTICAL
2. AIRSPEED ….. REDUCE

B. Overspeed - NP above 2080 RPM (caution)
C. Underspeed - NP below 1900 RPM (caution)

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9
Q

GEAR RETRACTION FAILURE

A
  1. AIRSPEED ….. BELOW 180KIAS
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10
Q

ENGINE FAILURE AFTER TAKE-OFF

A
  1. PCL ……………………………… FUEL OFF

If suitable runway exists
2. FUEL HYD CUTOFF ….. PULL
3. EMERGENCY LANDING CHECKS

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11
Q

AILERON CONTROL SYSTEM MALFUNCTION

A
  1. TRIM/AIL PWR ….. OFF
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12
Q

UNCOMMANDED POWER CHANGES

A
  1. PCL ……. IDLE
  2. PMS ….. MANUAL
  3. PCL …… AS REQUIRED
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13
Q

ABORTED TAKE-OFF

A
  1. PCL ….. IDLE
  2. BRAKES ….. AS REQUIRED

If aborting due to engine fire
3. ENGINE FIRE OR SMOKE AND FUMES - ON GROUND

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14
Q

METAL PARTICLES DETECTED IN GEARBOX

A
  1. PCL ….. MINIMUM PRACTICAL
  2. LAND AS SOON AS POSSIBLE
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15
Q

OIL TEMPERATURE HIGH - ON GROUND

A

A. OIL TEMP WARNING
1. PCL ….. FUEL OFF

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16
Q

ENGINE TEMPERATURE - ON GROUND

A

If ITT rapidly increases towards and exceeds 750deg in ground idle with warning displayed:
1. PCL ….. FUEL OFF

17
Q

EMERGENCY EGRESS ON THE GROUND

A
  1. SEAT PIN ………………………… IN
  2. LEG RESTRAINTS …………. RELEASE
  3. SEAT HARNESS ……………. RELEASE
  4. OXYGEN MASK HOSE …. DISCONNECT
  5. MIC-TEL ………………………… DISCONNECT
  6. PSP ……………………………….. DISCONNECT
  7. CANOPY ……………………….. OPEN
  8. EXIT THE COCKPIT
18
Q

What are the indications of an Engine Surge?

A
  1. Loss of Power
  2. ITT excessively high or fluctuating
  3. Unusual engine noise (popping or rumbling)
19
Q

ENGINE SURGE

A
  1. PCL ….. IDLE
20
Q

ITT High - IN FLIGHT

A

A. ITT above 860deg
1. PCL ….. MINIMUM PRACTICAL

B. ITT below 350deg

21
Q

MFD OXY WARNING

A

If above 10,000ft cabin altitude
1. EO2 …………. PULL
2. DESCEND BELOW 10000FT CABIN ALTITUDE

22
Q

OXY FLOW WARNING

A
  1. OXYGEN ….. ON, CHECK FLOW, CONNECTIONS, MASK
  2. INSTRUCTOR SELECTOR SWITCH ….. CHECK FOR CORRECTION SELECTION

If above 10,000ft cabin altitude and problem remains
3. EO2 ….. PULL (AFFECTED COCKPIT)
4. DESCEND BELOW 10000FT CABIN ALTITUDE

23
Q

OIL TEMPERATURE HIGH - IN FLIGHT

A

A. Oil Temp Warning
1. PCL ….. MINIMUM PRACTICAL

24
Q

ENGINE SPEED

A

A. NG below 50.7% (caution)
1. IGNITERS ….. ON
2. PCL ………….. SLOWLY INCREASE POWER

B. NG above 104% (caution for 2secs, then warning)
1. PCL …………… MINIMUM PRACTICAL

25
ENGINE TORQUE
1. PCL ..... MINIMUM PRACTICAL
26
FLAP FAILURE
1. AIRSPEED ..... BELOW 180KIAS
27
ENGINE FIRE OR SMOKE AND FUMES - ON GROUND
1. ACS SHUT OFF .............. PULL 2. PCL ................................... FUEL OFF 3. FUEL HYD CUTOFF ..... PULL 4. BATTS AND GENS ....... OFF 5. BRAKES .......................... AS REQUIRED 6. EMERGENCY EGRESS ON THE GROUND
28
OXYGEN SYSTEM OFF (BOTH COCKPITS)
If above 10,000ft cabin altitude 2. EO2 ..... PULL 3. DESCEND BELOW 10000FT CABIN ALTITUDE
29
ENGINE FIRE - IN FLIGHT
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. GEN1 and GEN2 ...... Off If fire continues 9. EJECT If fire not confirmed or FIRE Warning go out: 10. PMS ...... Manual
30
ENGINE MECHANICAL FAILURE
1. PCL .................................... FUEL OFF 2. FUEL HYD CUTOFF ..... PULL 3. EO2 .................................. PULL IF ABOVE 10000FT
31
PHYSIOLOGICAL EPISODE / HYPOXIA
1. EO2 ........................... PULL 2. DESCEND BELOW 10000 AIRCRAFT ALTITUDE 3. OXYGEN ................. OFF (BOTH COCKPITS) When at or below 10000ft aircraft altitude 4. ACS SHUTOFF ..... PULL 5. CABIN PRESS ....... RAM
32
OXYGEN OVERPRESSURE
If experiencing uncommanded oxygen oxygen system overpressure symptoms and unable to breathe. 1. OXYGEN ..... OFF (AFFECTED COCKPIT) If above 10000ft cabin altitude 2. EO2 ............. PULL 3. DESCEND BELOW 10000FT CABIN ALTITUDE
33
BRAKE FAILURE
If uncontrolled departure from hard surfrace will occur, consider PCL FUEL OFF, or ejection at high speed 1. BRAKES ...... Release Note Repeated application ("pumping") of the defective brake may restore braking pressure. 2. SERVICEABLE BRAKES ...... Gradually Reapply
34
FUEL PRESSURE LOW
1. FUEL PUMPS ..... ON 2. PCL ..... MINIMUM PRACTICAL If warning remains 3. LAND AS SOON AS POSSIBLE
35
SMOKE OR FUMES IN THE COCKPIT - IN FLIGHT
1. EO2 .............................. PULL 2. DESCEND BELOW 10000FT AIRCRAFT ALTITUDE 3. OXYGEN ...... Off (Both Cockpits) 4. ACS SHUT OFF ...... Pull 5. CABIN PRESSURE ...... Ram If fumes continue: 6. GEN1 AND GEN2 ...... Off
36
Ejection Checks
If Time Critical 1. Seat Firing Handling ...... Pull Otherwise Carry out as many of the following as time permits. 2. Seat Harness ...... Secured and Locked 3. PSP..... Connected 4. Helmet ...... Visors Down, Chin Strap Secured 5. Seat Pin ...... Removed 6. Location ...... Suitable 7. Height ...... Ideally 2000ft AGL 8. Airspeed ...... 150 - 250KIAS 9. Trim ...... 1/3 Aileron Trim 10. Attitude ...... Wings Level, climbing 11. PCL ...... IDLE Friction Tight (FUEL OFF if already selected) 12. Seat Firing Handle ..... Pull
37
Trim Runaway
TRIM/AIL PWR ...... Off

2FTS Basic Knowledge (3 decks)

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