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My S-92 stuff with PHI > PHI GOM S92 ENGINE EPs > Flashcards

PHI GOM S92 ENGINE EPs Flashcards

0
Q

Single engine Notes

A

-Nr below 96% AC Generators may drop offline ondeck.
(80% inflight).
-may need to use crossfeed to prevent fuel imbalance

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1
Q

“Engine one failure”
Red X over engine pod
Torque, Np, Ng decreasing to zero

A

Fly…Set SE airspeed, torque. Land as soon as practical
ID- SINGLE ENGINE FAILURE number one engine
Throttle- Stop
Checklist- TAB 2

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2
Q

ENGINE RESTART IN FLIGHT

A

Fly..maintain SE profile
ID- ENGINE RESTART IN-FLIGHT
Checklist- TAB 2

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3
Q

FADEC 1A FAIL (or 1B)

A

Fly…Land as soon as practical (be ready for engine failure if both A & B fail)
ID - FADEC CHANNEL FAILURE
checklist- TAB 3

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4
Q

FADEC A FAIL- indications

A

FADEC 1A FAIL
ENGINE PWR LIM
Loss of Engine oil Temp and TGT

[“AT BP” FADEC A =loss of Temp B= Pressure.]

DISABLE CAUTIONS:
ENG OIL HOT
ENG OIL PRESS
FUEL BYPASS

(FADEC B
DISAlBLE CAUTIONS:
ENG OIL Bypass
ENG Chip
FUEL Pressure)
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5
Q

FADEC B FAIL- indications

A

FADEC 1B FAIL
ENGINE PWR LIM
Loss of Engine oil pressure @ TGT

DISAlBLE CAUTIONS:
ENG OIL Bypass
ENG Chip
FUEL Pressure

(FADEC A FAIL
DISABLE CAUTIONS:
ENG OIL HOT
ENG OIL PRESS
FUEL BYPASS)
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6
Q

ENG 1 FIXED PWR
Torque split
engine does not respond to collective input

A

Fly…set 80 knots, make small changes to confirm fixed pwr.
ID- ENGINE FIXED POWER on #1 engine
Throttle- (after going through checklist-
If unable to descend due to fixed at high power, throttle stop)
Checklist- TAB 3

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7
Q

Draw side view of engine

A

.

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8
Q

FADEC 1 XENG

30 sec power armed

A

Fly…avoid high power setting and rapid collective movements (Could inadvertently go into 30 range)
ID- FADEC CROSS ENG COM FAULT on #1 engine..
Checklist- TAB 4

30 Sec power armed in case the other engine has failed.
FADEC 1A cross engine A ARINC 429 data fault. #1 eng doesn’t know condition of #2

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9
Q

FADEC acronym for:

A

FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC)

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10
Q

ENG 1 RATE LIM
Possible Nr droop
Possible loss of Load sharing
Possible Slow engine acceleration

A

Fly….Minimize rate of collective input. Land as soon as PRACTICAL
ID- ENGINE RATE LIMIT on #1 engine
Checklist- TAB 4

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11
Q

Where are the FADECs located

A

.

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12
Q

ENG 1 POWER LIM
Full engine power may not be available
Power available is limited below maximum

A

FLY…avoid maneuvers that require high power, Land as soon as PRACTICAL
ID- ENGINE POWER LIM on #1 engine
Checklist- TAB 4

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13
Q

FADEC 1 OVRHEAT

A

Fly…Land as soon as PRACTICAL
ID- FADEC OVERHEAT #1 engine
Throttle-na
Checklist- TAB 4

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14
Q

ENG 1 OVERSPEED
Nr & Np cycle between 118 and 121%
Ng cycles above 108.5%

A

Fly…Adjust to OEI profile, Land as soon as PRACTICAL
ID- ENGINE OVERSPEED on #1 engine
Throttle- IDLE, then STOP.
Checklist- TAB 4

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15
Q

ENG 1 OVSP TEST

A

Fly…Continue flight (correct prior to next flight)
ID- ENGINE OVERSPEED TEST on #1 engine
Checklist- TAB 4

May not have overspeed protection

16
Q 
Bang or popping sounds
Yaw Kicks
Rapid increase in TGT
Decrease in torque
Fluctuations in Nr
A

Fly…reduce power, (adjust to OEI profile)
ID- ENGINE COMPRESSOR STALL
Throttle- Idle, back FLY if stall stops
Checklist- TAB 5

Flight through extreme air temp may cause compressor stalls

If stall continues go to EMERGENCY ENGINE SHUTDOWN

17
Q

Engine Start will be aborted for any of the following four reason:

A 
TGT will exceed 1000c
No oil pressure within 30 sec
No light off within 20 seconds (of initial Ng or Throttle to idle)
Starter drop out before 50% Ng
FCP 2.2
18
Q

FADEC 1 FAULT

A

Fly…Continue flight, correct prior to next flight
ID- FADEC FAULT on #1 engine
Checklist- TAB 5

Best Practice 7:

  • Check HEALTH, PROPULSION:
    1) . If ENGINE status is green then the FAULT will clear after shutdown. If more than half way to offshore location you may shutdown offshore to clear.
    2) . If ENGINE status is MAGENTA or less than half way to rig then RTB.
19
Q

ENG 1 OVERSPEED
Np above Nr then flameout
Loud high-speed rattle
Loud Bang

A

Fly…adjust to OEI flight profile
ID- ENGINE HIGH SPEED SHAFT FAILURE #1 engine
Throttle- STOP
Checklist- TAB 5

20
Q

ENG 1 CHIP

NO Secondary indications

A

Fly…Adjust to OEI flight profile, Land as soon as PRACTICAL
ID- ENGINE CHIP (No secondary)
Checklist- TAB 5

21
Q

ENG 1 OIL PRESS (Without Secondary indications) or

ENG 1 OIL HOT or ENG 1 OIL BYPASS

A

Fly…Adjust to OEI flight profile, Land as soon as PRACTICAL
ID- ENGINE OIL SYSTEM MALFUNCTION, #1 engine
Checklist- TAB 6

22
Q

ENG 1 A-ICE DGRD

A

FLY…Exit Icing Conditions, Land as soon as POSSIBLE
ID- ENGINE ANTI-ICE DEGRADED
Checklist- TAB 6

Indicates- Insufficient bleed air is being routed to the engine inlet for satisfactory ice protection

23
Q

INLET 1 A-ICE FAIL

(May have loss of power due to inlet blockage with ICE)

A

Fly…Exit Icing conditions
ID- ENGINE INLET ANTI-ICE FAIL #1 engine
Throttle-na
Checklist- TAB 6

Indicates an electrical failure of the inlet anti-ice. Note: Do not cycle the switch from OFF to ON more than once

24
Q

Any Engine Malfunction

A
  1. Fly….Maintain Aircraft control, adjust Airspeed, Power within limits.
  2. Identify……….Affected Engine/Problem, Confirm Secondary indications.

If Secondary Indications (including Engine Fire)

  1. Throttle……..Confirm (correct engine) then Idle
  2. Checklist……Complete (for the malfunction)
25
Q

During INLET 1 A-ICE FAIL how many times may you cycle the affected anti-ice switch OFF and then ON?

A

one time (RFM Part 1, Section III- 3.11)

26
Q

What is the minimum Ng speed of the donor engine for a cross bleed start?

A

90% Ng
(ensures the Anti-Ice start bleed valve is closed so full pressure is available. Otherwise, some air is vented to prevent compressor stalls at low Ng speed) PTM page 6-6

27
Q

With FADEC 1 FAIL and FADEC 2 FAIL what will happen to the engine and what unusual indications occur?

A
  • The engine will flame out
  • no red “X” over engine in EICAS
  • No Alt coupling available
  • No Engine failure audio

My S-92 stuff with PHI (46 decks)

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