Memory EPs Dash 1

Question 1

Emergency Index

Answer 1

• Hydraulics = EA
• Electrical = EB
• Fuel = EC
• Oxygen = ED
• Engine = EE
• Takeoff = EF
• General = EG

Question 2

Abort Start Procedure*

Answer 2

(EE-3)
*1. PCL - OFF; or STARTER switch - AUTO/RESET
2. Perform Motoring Run Procedure

Question 3

Emergency Ground Egress*

Answer 3

(EG-19)
*1. ISS mode selector - SOLO
*2. Seat Safety Pin - Install (BOTH)
*3. PARKING BRAKE - As Required
*4. Canopy - Open
IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS:
5. CFS handle safety pin - Removed (Both)
*6. CFS handle - Rotate and pull (BOTH)
*7. Shoulder straps, lap belt, SSK fittings, and leg restraint garters - Release (BOTH)
*8. BAT, GEN, and AUX BAT switches - OFF
*9. Evacuate aircraft

Question 4

Abort

Answer 4

*1. PCL - IDLE
*2. BRAKES - AS REQUIRED

Question 5

Engine Failure Immediately After Takeoff (Sufficient Runway Remaining Straight Ahead)

Answer 5

(EF-7)
*1. AIRSPEED - 110 KNOTS (MINIMUM)
*2. PCL - AS REQUIRED
*3. EMER LDG GR HANDLE - PULL (AS REQUIRED)
4. Flaps - As Required

Question 6

Engine Failure During Flight

Answer 6

(EE-25)
*1. ZOOM/GLIDE - 125 KNOTS (MINIMUM)
*2. PCL - OFF
*3. INTERCEPT ELP
*4. Airstart - Attempt if warranted
IF CONDITIONS DO NOT WARRANT AN AIRSTART:
*5. FIREWALL SHUTOFF handle - Pull
*6. Execute Forced Landing or Eject

Question 7

Immediate Airstart (PMU NORM)

Answer 7

(EE-21)
(As long as not Fire, Fod, Frozen, Final, or Fuel Starvation)
*1. PCL - OFF
*2. STARTER SWITCH - AUTO/RESET
*3. PCL - IDLE, ABOVE 13% N1
*4. Engine instruments - Monitor ITT, N1, and oil pressure
IF AIRSTART IS UNSUCCESSFUL:
*5. PCL - OFF
*6. FIREWALL SHUTOFF handle - PULL
*7. Execute Forced Landing or Eject
IF AIRSTART IS SUCCESSFUL
*8. PCL - As Required after N1 reaches IDLE RPM (approximately 67% N1)
*9. PEL - Execute
10. Confirm the position of the following
a. BOOST PUMP switch - ON
b. IGNITION SWITCH - ON
11. STARTER SWITCH - NORM
12. BLEED AIR INFLOW switch - NORM
13. GEN switch - VERIFY ON; RESET IF NECESSARY
14. OBOGS - AS REQUIRED

Question 8

Uncommanded Power Changes/Loss of Power/Uncommanded Propeller Feather

Answer 8

(EE-7)
*1. PCL - MID RANGE
*2. PMU SWITCH - OFF
*3. PROP SYS CIRCUIT BREAKER - PULL, IF NP STABLE BELOW 40%
*4. PCL - As required
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
*5. PEL - Execute
IF POWER IS INSUFFICIENT TO COMPLETE PEL:
*6. PROP SYS circuit breaker - Reset, as required
*7. PCL - OFF
*8. FIREWALL SHUTOFF handle - PULL
*9. Execute Forced Landing or Eject

Question 9

Compressor Stalls*

Answer 9

(EE-9)
*1. PCL - Slowly retard below stall threshold
*2. DEFOG switch - ON
*3. PCL - Slowly advance (as required)
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
*4. PEL - Execute
IF POWER IS INSUFFICIENT TO COMPLETE PEL:
*5. PCL - OFF
*6. FIREWALL SHUTOFF handle - PULL
*7. Execute Forced Landing or Eject

Question 10

Inadvertent Departure From Controlled Flight

Answer 10

(EG-3)
*1. PCL - IDLE
*2. CONTROLS - NEUTRAL
*3. ALTITUDE - CHECK
*4. Recover from unusual attitude

Question 11

Fire In Flight

Answer 11

(EE-11)
IF FIRE IS CONFIRMED:
*1. PCL - OFF
*2. FIREWALL SHUTOFF HANDLE - PULL
IF FIRE IS EXTINGUISHED
*3. Forced Landing - Execute
IF FIRE DOES NOT EXTINGUISH OR FORCED LANDING IS IMPRACTICAL:
*4. Eject (Both)
IF FIRE IS NOT CONFIRMED
*5. PEL - Execute

Question 12

Chip Detector Warning*

Answer 12

(EE-17)
*1. PCL - Minimum necessary to intercept ELP; avoid unnecessary PCL movements
*2. PEL - Execute

Question 13

Oil System Malfunction or Low Oil Pressure*

Answer 13

(EE-19)
IF ONLY AMBER OIL PX ANNUNCIATOR ILLUMINATES
*1. Terminate Maneuver
*2. Check oil pressure; if oil pressure is normal, continue operations
IF RED OIL PX ANNUNCIATOR ILLUMINATES AND/OR AMBER OIL PX ANNUNCIATOR REMAINS ILLUMINATED FOR 5 SECONDS
*3. PCL - Minimum necessary to intercept ELP; avoid unnecessary PCL movements
84. PEL - Execute

Question 14

Low Fuel Pressure*

Answer 14

(EC-3)
*1. PEL - Execute
2. BOOST PUMP switch - ON

Question 15

OBOGS System Malfunction*

Answer 15

(ED-3)
*1. PCL - Advance
2. OBOGS - CHECK (BOTH) - ON, MAX, EMERGENCY
If OBOGS FAIL annunciator remains illuminated:
3. OBOGS Inoperative procedure - Execute

Question 16

OBOGS Inoperative

Answer 16

(ED-5)
*1. GREEN RING - PULL (AS REQUIRED)
2. Descent below cabin altitude of 10,000 feet - Initiate
3. Disconnect main oxygen supply hose from CRU-60/P
4. OBOGS - OFF (BOTH)
5. Land as soon as practical

Question 17

Eject

Answer 17

*1. EJECTION HANDLE - PULL

Question 18

Forced Landing*

Answer 18

(EE-33)
*1. Airspeed - 125 KIAS prior to extending landing gear
*2. EMER LDG GR handle - Pull (as required)
*3. Airspeed - 120 KIAS minimum until intercepting final; 110 KIAS minimum on final
*4. Flaps - As required
Accomplish the following as conditions permit:
5. Distress call - TRANSMIT
6. ELT switch - AS REQUIRED
7. Transponder - 7700 (AS REQUIRED)
8. Harness - LOCKED (BOTH)
9. Emergency Ground Egress procedure - EXECUTE (AS REQUIRED)

Question 19

Precautionary Emergency Landing (PEL)*

Answer 19

(EE-23)
*1. Turn to nearest suitable airfield
*2. Climb or accelerate to intercept ELP
*3. Gear, flaps, speed brake - UP
4. Conduct a systematic check of the aircraft and instruments for additional signs of impending engine failure
5. BOOST PUMP switch - AS REQUIRED
6. IGNITION switch - AS REQUIRED
7. Plan to intercept the emergency landing pattern at or below high key in the appropriate configuration and a minimum airspeed of 120 KIAS