Engine fire on deck
Request FF assistance / inform crew T-handle - pull Fire button - Push T- handle (other engine) - pull GRD AND FLT BATT SWITCHES- Off
Start valve open light on after 62%
CL - ground stop
Bleed air switches - off
Fail to feather procedure
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
Brake failure
Reverse thrust - a/r
Brake selector valve - Aux
Parking / emergency brake - a/r
Aborted takeoff
Power levers - flight idle Flaps - up Power levers - ground idle Brakes - a/r Arresting hook - a/r
Beta lights failure
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
Decoupling of engine and propeller
If recouple fails:
Perform Engine Fire failure shutdown in flight procedure
Prop pump light(s) steady
Power lever - max
Maintain at least 135 KCAS
if normal governing
Perform engine fire/failure/shutdown in flight procedure.
Smoke and fumes from personal air conditioning system
Personal air cond switch -off
Don oxygen - 100%
Bailout
Inform crew Don oxygen/emergency oxygen - a/r Depressurize cabin MEH -jettison E-2D - EMIRS CABLE - SEVER IF EXTENDED.
HYD system complete failure
Level aircraft and reduce airspeed
Dual engine failure during flight
Maintain 150 KIAS CLEAN power levers - slightly above flight idle Condition lever (l or r) - ground stop then air start
Tow link unsafe indication
Check nose gear visually before raising gear
Explosive decompression
oxygen - don a/r
Smoke and fume elimination
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
Fire smoke fumes
1) Don oxygen - as required
2) Isolate affected equipment
If source cannot be immediately isolated
3) Gen switches - Off
Ditching checklist
Landing gear - up Flaps - A/r Max rudder - a/r Ditching hatches - open / remove Harness - locked
Engine fire / failure / shutdown inflight
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
Bleed air overheat light(s) in flight / cabin bleed air leak
1) bleed air switches - Off
2) Don Oxygen
Start Limits
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
Stabilized Start Limit - E-2D
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)
Max Reverse
TMT - 360-560 IHP - 680-2000 RPM - 96.5 - 105.5 G/B - 150-250 P/S - 50-60 Oil temp 50-90
Flight idle limits
TMT - 300-540
IHP - 1100 nominal
RPM - 94.5-99.0
LSGI LIMITS
TMT - 400-600
RPM - 71.0-72.1 %
RGB - 25 psi (100 normal)
P/S - 25 psi
