Tabletop GK Flashcards
CAP
EMERGENCY GROUND EGRESS
- ISS mode selector - SOLO
- Seat safety pin - Install (BOTH)
- PARKING BRAKE - As required
- Canopy - Open
**IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS: ** - CFS handle safety pin - Remove (BOTH)
- CFS handle - Rotate and pull (BOTH)
- Shoulder straps, lap belt or lap straps, SSK fittings, and leg restraint garters - Release (BOTH)
- BAT, GEN, and AUX BAT switches - OFF
- Evacuate aircraft
SOLO PIN PARK POP
CAP
EMERGENCY ENGINE SHUTDOWN ON THE GROUND
**1. PCL - OFF
2. FIREWALL SHUTOFF HANDLE - PULL **
3. Emergency ground egress - As required
CAP
ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
**1. AIRSPEED - 110 KNOTS (MINIMUM)
2. PCL - AS REQUIRED
3. EMER LDG GR HANDLE - PULL (AS REQUIRED) **
4. Flaps - As required
CAP
ENGINE FAILURE DURING FLIGHT
**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
CAP
IMMEDIATE AIRSTART (PMU NORM)
**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
CAP
UNCOMMANDED POWER CHANGES/LOSS OF POWER/PROP FEATHER
**1. PCL - MID RANGE
2. PMU SWITCH - OFF
3. PROP SYS CIRCUIT BREAKER (left front console) - 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
CAP
COMPRESSOR STALLS
- PCL - Slowly retard below stall threshold
- DEFOG switch - ON
- 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
CAP
INADVERTENT DEPARTURE FROM CONTROLLED FLIGHT
**1. PCL - IDLE
2. CONTROLS - NEUTRAL
3. ALTITUDE - CHECK **
4. Recover from unusual attitude
CAP
FIRE IN FLIGHT
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
CAP
SMOKE AND FUME ELIMINATION/ELECTRICAL FIRE
- OBOGS - Check (BOTH)
a.OBOGS supply lever - ON
b.OBOGS concentration lever - MAX
c.OBOGS pressure lever - EMERGENCY
CAP
CHIP DETECTOR WARNING
- PCL - Minimum necessary to intercept ELP; avoid unnecessary PCL movements
- PEL - Execute
CAP
OILS SYSTEM MALFUNCTION OR LOW OIL PRESSURE
IF ONLY AMBER OIL PX ANNUCIATOR 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
4. PEL - Execute
CAP
LOW FUEL PRESSURE
- PEL - Execute
- BOOST PUMP - ON
CAP
HIGH FUEL FLOW
- PEL - Execute
CAP
FORCED LANDING
- Airspeed - 125 KIAS prior to extending landing gear
- EMER LDG GR handle - Pull (as required)
- Airspeed - 120 KIAS minimum until intercepting final; 110 KIAS minimum on final
- Flaps - As required
CAP
PRECAUTIONARY EMERGENCY LANDING
- Turn to nearest suitable field
- Climb or accelerate to intercept ELP
- Gear, flaps, speed brake - UP
FL Ejection Criteria
ORM 321
Below 2000 feet you MUST be:
On Profile
Runway in sight
can safely Maneuver to landing
300 feet you make a go/no-go decision
200 feet confirm gear
100 feet maintain centerline
If you lose any of this criteria below 2000 AGL immediate ejection
CWS Annunciatior
Red CKPT PX
cockpit pressure exceeds 3.9-4.0 PSI
Checklist: Cockpit Overpressurization
CWS Annunciator
Red FUEL PX
Less the 10 PSI in the motive flow line
Checklist: Low Fuel Pressure
CWS Annunciator
Red OIL PX
below 15 PSI
15-40 for 5 secs @ IDLE
below 40 PSI above IDLE
Checklist: Oil Sys Malf or Low Oil Pressure
CWS Annunciator
Amber CKPT ALT
Cabin Altitude above 19000
CWS Annunciator
Amber DUCT TEMP
Duct Temp above 300 deg F
Checklist: ECS Duct Overtemp
CWS Annunciator
Amber HYDR FL LO
Resevoiur below 1 QT
Checklist: Hydraulic Systems Malfunction
CWS Annunciator
Amber FUEL BAL
Fuel Imbalance exceeds 30 pounds for 2 mins
FP Fail
EDM Fail
Checklist: Fuel Imbalance
CWS Annunciator
Amber EHYD PX LO
2400 +/- 150 PSI
Checklist: Hydraulic System Malfunctions
CWS Annunciator
Amber OBOGS TEMP
200 deg F
Boldface
CWS Annunciator
Amber L FUEL LO
Left tank below 110 pounds
Leaking Fuel Checklist
CWS Annunciator
Amber R FUEL LO
Right tank below 110 pounds
Leaking Fuel Chechlist
CWS Annunciator
Amber OIL PX
15-40 @ IDLE
40-90 for 10 secs above IDLE
Checklist: Oil System Malf or Low Oil Pressure
FDR Annunciator
Amber FDR Fail
IDARS has failed
FDR Annunciator
Green Maintenance
IDARS is 80% Full
Possible Over-G
Max Abort Speed
3 seconds to recognize
3 seconds to react
20 KTS of airspeed gained
Chairfly a TCCC
I will use coordinated stick and rudder to perform a 2G pull up to 20 degrees NH with up to 45 deg of bank towards the nearest available key approaching 145 KIAS I will do a 1/2 G buntover to capture 125 KIAS
expect 100 feet of alt gain for every 10 kts above 140.
MATL
I will maintain aircraft control, analyze the situation, take proper action, and land as soon as conditions permit.
