E-2D EP Flashcards
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
PCMU FAIL FLIGHT ILLUMINATED ON DECK
If the resulting thrust or RPM is unacceptable for ground operations
T-Handle - Pull
PCMU FAILURE / PCMU POWER LEVER FAILURE ON TAKEOFF
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
Autopilot Malfunction
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
EMIRS LATCH PREMATURE CLOSURE ON RETRACTION
EDS OVERRIDE AND EMIRS DEPLOYMENT STOP SWITCHES - simultaneously toggle and hold EDS OVERRIDE to OVRD and press and hold stop.
MAX / MIL / Transitory IHP
MAX - 5350 (875) (10 min)
MIL - 5350 (845) (30 min)
Trans IHP - 5350 up 5999
APR - 5450 @ 103 5 mins max
Trim runaway longitudinal
T-button - Push
