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NATOPS EMERGENCY PROCDURES > E-2D EP > Flashcards

E-2D EP Flashcards

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0
Q

Engine fire on deck

A 
Request FF assistance / inform crew
T-handle - pull
Fire button - Push
T- handle (other engine) - pull
GRD AND FLT BATT SWITCHES- Off
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1
Q

Start valve open light on after 62%

A

CL - ground stop

Bleed air switches - off

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2
Q

Fail to feather procedure

A

1) Condition lever feather
2)FEA oride switch - Toggle and hold to complete feather
If prop does not feather
3)Power lever - (operating engine) - a/r
4)Configuration - gear up, flaps 10, max rudder 20
5) Airspeed - a/r

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3
Q

Brake failure

A

Reverse thrust - a/r
Brake selector valve - Aux
Parking / emergency brake - a/r

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4
Q

Aborted takeoff

A 
Power levers - flight idle
Flaps - up
Power levers - ground idle
Brakes - a/r
Arresting hook - a/r
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5
Q

Beta lights failure

A 
Flaps -set for takeoff
Execute go around - a/r
If go around not executed, takeoff aborted or arresting gear not available
Power levers -flight idle
Flaps - up
Condition lever (one affected engine) - ground stop 
Power levers - ground idle (a/r)
Brakes -a/r
Arresting hook - a/r
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6
Q

Decoupling of engine and propeller

A

If recouple fails:

Perform Engine Fire failure shutdown in flight procedure

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7
Q

Prop pump light(s) steady

A

Power lever - max
Maintain at least 135 KCAS
if normal governing
Perform engine fire/failure/shutdown in flight procedure.

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8
Q

Smoke and fumes from personal air conditioning system

A

Personal air cond switch -off

Don oxygen - 100%

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9
Q

Bailout

A 
Inform crew
Don oxygen/emergency oxygen - a/r
Depressurize cabin
MEH -jettison
E-2D - EMIRS CABLE - SEVER IF EXTENDED.
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10
Q

HYD system complete failure

A

Level aircraft and reduce airspeed

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11
Q

Dual engine failure during flight

A 
Maintain 150 KIAS CLEAN
power levers - slightly above flight idle
Condition lever (l or r) - ground stop then air start
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12
Q

Tow link unsafe indication

A

Check nose gear visually before raising gear

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13
Q

Explosive decompression

A

oxygen - don a/r

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14
Q

Smoke and fume elimination

A

If bleed air switches were secured for bleed air duct failure or bleed air leak go to step 3

1) Person air cond switch - On
2) Side window. Defog - max

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15
Q

Fire smoke fumes

A

1) Don oxygen - as required
2) Isolate affected equipment
If source cannot be immediately isolated
3) Gen switches - Off

16
Q

Ditching checklist

A 
Landing gear - up
Flaps - A/r
Max rudder - a/r
Ditching hatches - open / remove
Harness - locked
17
Q

Engine fire / failure / shutdown inflight

A 
Power levers - a/r
Landing gear -a/r
T-handle - pull
Fire button - a/r
Flaps - a/r
Max rudder - a/r
Fuel dump - a/r
APR - a/r
If prop doesn't feather:
Execute Fail to feather procedure
18
Q

Bleed air overheat light(s) in flight / cabin bleed air leak

A

1) bleed air switches - Off

2) Don Oxygen

19
Q

Start Limits

A

TMT - 830
G/B and P/S - indication by 35%
Oil temp - -40 for Mil-l-23699 and -54 for Mil-l-7808

Same for D

20
Q

Stabilized Start Limit - E-2D

A

TMT - 300 to 500
IHP - min until oil temp is above 0 C and 1000 max at oil temp 0-40 C
RPM - 96.7-99.0
G/B - 150-250
P/S - 50-60 (100 permitted during start and warm up)
Engine oil temp - 50-90 (100 permitted for 30 minutes)

21
Q

Max Reverse

A 
TMT - 360-560
IHP - 680-2000
RPM - 96.5 - 105.5
G/B - 150-250
P/S - 50-60
Oil temp 50-90
22
Q

Flight idle limits

A

TMT - 300-540
IHP - 1100 nominal
RPM - 94.5-99.0

23
Q

LSGI LIMITS

A

TMT - 400-600
RPM - 71.0-72.1 %
RGB - 25 psi (100 normal)
P/S - 25 psi

24
Q

PCMU FAIL FLIGHT ILLUMINATED ON DECK

A

If the resulting thrust or RPM is unacceptable for ground operations

T-Handle - Pull

25
Q

PCMU FAILURE / PCMU POWER LEVER FAILURE ON TAKEOFF

A

1) Continue takeoff
2) PMCU Fail Caution Light - Execute

If take off not continued-

3) T-handle (affected engine) - Pull
4) power lever- flight idle
5) Flaps - Up
6) power levers - Grd Idle
7) Brakes - a/r
8) Arresting Hook - a/r

26
Q

Autopilot Malfunction

A

A-button - PUSH AND RELEASE
If control returns and malfunction was in pitch or roll, leave the AFCS MODE DISENGAGED and continue normally

If control returns and malfunction caused the aircraft to yaw:
AFCS POWER - off

If malfunction still exists:
A-button - push and hold
Configuration- 150-170, clean, max rudder 6 degrees

27
Q

EMIRS LATCH PREMATURE CLOSURE ON RETRACTION

A

EDS OVERRIDE AND EMIRS DEPLOYMENT STOP SWITCHES - simultaneously toggle and hold EDS OVERRIDE to OVRD and press and hold stop.

28
Q

MAX / MIL / Transitory IHP

A

MAX - 5350 (875) (10 min)
MIL - 5350 (845) (30 min)
Trans IHP - 5350 up 5999

APR - 5450 @ 103 5 mins max

29
Q

Trim runaway longitudinal

A

T-button - Push

NATOPS EMERGENCY PROCDURES (4 decks)

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