T-6B

Card Set Information

Author:
Maximus
ID:
105459
Filename:
T-6B
Updated:
2011-10-25 22:31:49
Tags:
Emergency Procedures EP
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Description:
T_6B Bold Face EPs 30 SEP 2011
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  1. Abort Start Procedure
    *1. PCL - OFF; or STARTER switch - AUTO/RESET
  2. Emergency Engine Shutdown on the Ground
    *1. PCL-Off

    *2. Firewall Shutoff Handle- Pull

    *3. Emergency Ground Egress- As Required
  3. Emergency Ground Egress
    *1. ISS mode selector - SOLO

    *2. Ejection seat 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 - Rotate and pull (BOTH)

    • *6. Upper fittings, lower fittings, and leg restraint garters - Release
    • (BOTH)

    *7. BAT, GEN, and AUX BAT switches - OFF

    *8. Evacuate aircraft
  4. Abort
    *1. PCL - IDLE

    *2. BRAKES - AS REQUIRED
  5. Engine Failure Immediately After Takeoff
    (Sufficient Runway Remaining Straight Ahead)
    *1. AIRSPEED - 110 KNOTS (MINIMUM)

    *2. PCL - AS REQUIRED

    *3. EMER LDG GR HANDLE - PULL (AS REQUIRED)

    *4. Flaps - As required
  6. 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
  7. Immediate Airstart (PMU NORM)
    *1. PCL - OFF

    *2. STARTER SWITCH - AUTO/RESET

    *3. PCL - IDLE, ABOVE 13% N1

    *4. Engine instruments - Monitors ITT, N1, and oil pressure

    IF AIRSTART IS UNSUCCESSFUL:

    *5. PCL - OFF

    *6. FIREWALL SHUTOFF handle - Pull

    *7. Execute Forced Landing or Eject
  8. Uncommanded Power Changes/Loss of Power/ Uncommanded Propeller 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
  9. Compressor Stalls
    *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
  10. Inadvertent Departure From Controlled Flight
    *1. PCL - IDLE

    *2. CONTROLS - NEUTRAL

    *3. ALTITUDE - CHECK

    *4. Recover from unusual attitude
  11. 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
  12. Chip Detector Warning
    *1. PCL - Minimum necessary to intercept ELP; avoid unnecessary PCL movements

    *2. PEL - Execute
  13. Oil System Malfunction or Low Oil Pressure
    IF ONLY AMBER OIL PX CAUTION ILLUMINATES:

    *1. Terminate maneuver

    *2. Check oil pressure; if oil pressure is normal, continue operations

    • IF RED OIL PX WARNING ILLUMINATES AND/OR AMBER OIL
    • PX CAUTION REMAINS ILLUMINATED FOR 5 SECONDS:

    • *3. PCL - Minimum necessary to intercept ELP; avoid unnecessary
    • PCL movements

    *4. PEL - Execute
  14. Low Fuel Pressure
    *1. PEL - Execute
  15. OBOGS System Malfunction
    *1. PCL - Advance
  16. OBOGS Inoperative
    *1. GREEN RING - PULL (AS REQUIRED)
  17. Eject
    *1. EJECTION HANDLE - PULL (BOTH)
  18. Forced Landing
    *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
  19. Precautionary Emergency Landing (PEL)
    *1. Turn to nearest suitable field

    *2. Climb or accelerate to intercept ELP

    *3. Gear, flaps, speed brake - UP
  20. OPERATIONS CHECK
    1. Hydraulic pressure – Check

    2. Electrical systems – Check

    3. Fuel quantity/balance – Check

    4. OBOGS – Check flow indicator for normal operation (BOTH)

    5. Engine instruments – Check

    6. Pressurization – Check
  21. PRE-STALLING, SPINNING, AND AEROBATIC CHECKS
    1. Loose items – Stowed (BOTH)

    • 2. Engine instruments – Check
    • (Verify caution and warning messages are extinguished)

    3. Fuel balance – Check less than 50 pounds
  22. BEFORE LANDING
    1. DEFOG switch – OFF

    2. Engine instruments – Check

    3. Gear – DOWN (press down firmly) (BOTH) (Check three green annunciators illuminated)

    • 4. Brakes – Check, as required
    • (Verify positive pressure by actuating toe brakes.)

    5. Flaps – As required (BOTH)

    6. Speed brake – Verify retracted
  23. Land As Soon As Possible
    An emergency shall be declared and a landing accomplished at the nearest suitable landing area considering the severity of the emergency, weather conditions, field facilities, ambient lighting, and command guidance.
  24. Land As Soon As Practical
    Emergency conditions are less urgent and, although the mission is to be terminated, the degree of the emergency is such that an immediate landing may not be necessary.
  25. PROHIBITED MANEUVERS
    Inverted stalls

    Inverted spins

    Aggravated spins past two turns

    Spins with PCL above idle

    Spins with landing gear, flaps, or speed brake extended

    Spins with PMU off

    Spins below 10,000 feet pressure altitude

    Spins above 22,000 feet pressure altitude

    Abrupt cross-controlled (snap) maneuvers

    Aerobatic maneuvers, spins, or stalls with a fuel imbalance greater than 50 pounds between wings

    Tail slides
  26. ACCELERATION LIMITATIONS Symetric
    Clean +7.0 to -3.5 G's

    Gear and flaps extended +2.5 to 0.0 G's
  27. ACCELERATION LIMITATIONS
    ASYMMETRIC (ROLLING G’S)
    • Clean +4.7 to -1.0 G's
    • Gear and flaps extended +2.0 to 0.0 G’s
    • For uncoordinated rolling maneuvers initiated at -1 G, the maximum bank angle change is 180 degrees.
  28. WEIGHT LIMITATIONS
    Maximum ramp weight - 6950 pounds


    • Maximum takeoff weight - 6900 pounds
    • Maximum landing weight - 6900 pounds

    Maximum zero fuel weight - 5850 pounds

    Maximum weight in baggage compartment - 80 pounds
  29. WIND LIMITATIONS
    Maximum crosswind component for dry runway - 25 knots.

    Maximum crosswind component for wet runway - 10 knots.

    Maximum crosswind component for icy runway - 5 knots.

    Maximum tailwind component for takeoff - 10 knots.
  30. Starter Limitations
    Starter duty cycle (start attempts and/or engine motoring) is limited to four 20-second cycles as follows:

    First - Motor 20 seconds then, 30-second cooling period.

    Second - Motor 20 seconds then, 2-minute cooling period.

    Third - Motor 20 seconds then, 5-minute cooling period.

    Fourth - Motor 20 seconds then, 30-minute cooling period.
  31. PROPELLER GROUND OPERATION LIMITATIONS
    Sustained propeller operation on the ground between 62 and 80% NP is prohibited to prevent damage from ground resonance.
  32. DESCENT
    • 1. PFD – Check (BOTH)
    • 2. Altimeters – Set (BOTH)
    • 3. DEFOG switch – As required
    • 4. MASTER ARM switch – As required
    • 5. Vent control lever – As required
  33. CLIMB (PASSING 10,000 FEET)
    • 1. OBOGS – Check flow indicator for normal operation
    • (BOTH)
    • 2. DEFOG switch – As required
    • 3. Vent control lever – As required
    • 4. Pressurization system – Check
    • NOTE
    • If readings other than 3.6±0.2 psi are
    • encountered at or above 18,069 feet MSL,
    • notify maintenance after landing.

    With canopy defog ON, expect an increase inITT of up to 40 °C for a given PCL setting.Cockpit noise will also increase. Performancewill decrease with defog on. A DUCTTEMP indication is likely at climb or cruisepower with canopy defog ON and cockpittemperature controller set to AUTO orMANUAL HOT. Refer to EnvironmentalSystems Duct Overtemp procedure in SectionIII.
  34. LINEUP CHECK
    • 1. EICAS display – Check (BOTH)
    • 2. PROBES ANTI-ICE switch – ON
    • 3. Transponder – Mode to ALT
    • 4. Landing/taxi light – ON
    • 5. Nose wheel steering – Off
  35. Torque Max Transient
    • 131 (20 sec) (8)
    • 8. Torque at 131% is a materials limit above which damage to the engine may occur. Torque above 102% is indicative of a system malfunction
  36. ITT Limits
    Max/TO
    IDLE
    Start
    Transient
    • Max/TO 820
    • IDLE 750
    • Start 1000 (5 sec)
    • Transient 870 (20 sec)
  37. N1% Max
    Max/TO
    IDLE
    Transient
    • Max/ TO 104
    • IDLE: 60 Min (ground)/ 67 Min (flight)
    • Transient 104
  38. NP% Max
    • TO/MAX 100
    • Transient 102 (20 sec) 110 (3)
    • 3. Permissible at any power setting for completion of in-flight emergency.
  39. Oil Pressure psi
    TO/Max
    Idle
    Start
    Transient
    • TO/MAX 90-120
    • IDLE 90 minimum
    • START 200
    • Transient 40-130(5)
    • 5. Operation in this range permitted only during aerobatics or spins, and 15 to 40 psi for 5 seconds with PCL at IDLE.
  40. Oil Temp °C
    TO/Max
    Idle
    Start
    Transient
    • TO/Max 10 to105
    • Idle 10 to 105 (flight), -40 to 105 (ground)
    • Start -40 minimum
    • Transient 106-110 (10 minutes, ground ops only below 20% torque)
  41. Zoom capability
    Zoom capability at 200 knots will vary from 603 to 915 feet of altitude gained. Zoom capability at 250 knots will vary from 1180 to 1576 feet of altitude gained.

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