T-6A BOLDFACE EMERGENCY PROCEDURES/OPERATING …



|T-6A BOLDFACE EMERGENCY PROCEDURES/OPERATING LIMITATIONS |

|1. BOLDFACE EMERGENCY PROCEDURES |

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|ABORT START PROCEDURE |

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|EMERGENCY ENGINE SHUTDOWN ON THE GROUND |

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|EMERGENCY GROUND EGRESS |

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|IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS: |

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|7. |

|8. |

|9. |

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|ABORT |

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|ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD) |

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|ENGINE FAILURE DURING FLIGHT |

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|IF CONDITIONS DO NOT WARRANT AN AIRSTART: |

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|IMMEDIATE AIRSTART (PMU NORM) |

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|IF AIRSTART IS UNSUCCESSFUL: |

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|IF AIRSTART IS SUCCESSFUL: |

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|8. |

|9. |

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|UNCOMMANDED POWER CHANGES / LOSS OF POWER/UNCOMMANED PROPELLER FEATHER |

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|IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT: |

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|IF POWER IS INSUFFICIENT TO COMPLETE PEL: |

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|COMPRESSOR STALLS |

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|IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT: |

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|IF POWER IS INSUFFICIENT TO COMPLETE PEL: |

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|INADVERTENT DEPARTURE FROM CONTROLLED FLIGHT |

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|FIRE IN FLIGHT (FIRE ANNUNCIATOR ILLUMINATED) |

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|IF FIRE IS CONFIRMED: |

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|IF FIRE IS EXTINGUISHED: |

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|IF FIRE DOES NOT EXTINGUISH OR FORCED LANDING IS IMPRACTICAL: |

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|IF FIRE IS NOT CONFIRMED: |

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|CHIP DETECTOR WARNING |

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|OIL SYSTEM MALFUNCTION OR LOW OIL PRESSURE |

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|IF ONLY AMBER OIL PX ANNUCIATOR ILLUMINATES |

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|1. |

|2. |

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|IF RED OIL PX ANNUNCIATOR ILLUMINATES AND/OR AMBER OIL PX ANNUNCIATOR REMAINS ILLUMINATED FOR 5 SECONDS: |

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|3. |

|4. |

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|LOW FUEL PRESSURE |

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|1. |

|2. |

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|OBOGS FAIL ANNUNCIATOR |

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|IF PCL IS ABOVE IDLE |

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|1. |

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|IF PCL IS AT IDLE |

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|2. |

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|OBOGS FAILURE / PHYSIOLOGICAL SYMPTOMS |

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|1. |

|2. |

|3. |

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|EJECT |

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|FORCED LANDING |

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|PRECAUTIONARY EMERGENCY LANDING (PEL) |

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|1. |

|2. |

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|SMOKE AND FUME ELIMINATION/ELECTRICAL FIRE |

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|1. |

|a. |

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|c. |

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|ENGINE OPERATING LIMITS TABLE |

|POWER SETTING |TORQUE % |ITT (C |N1 % (1) |NP % (4) |OIL PRESSURE psi |OIL TEMP (C |

|TAKEOFF/MAX | (MAX) | | (MAX) | (MAX) (2) | to (6) | to |

|IDLE | | | to (ground) | to | Min | to |

| |_____to_____(9) | | |(GROUND) | |(Grnd) |

| |(GROUND) | |Min (flight) | | |to (Flt) |

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| | | | | | |to (7) |

|NOTES |

|N1 values presented for PMU ON. With PMU OFF, N1 may vary from these values. |

|With PMU OFF, permissible maximum NP is +/- %. |

|Permissible at all powers for completion of flight in emergency. |

|Avoid stabilized ground operation from to % NP. |

|Operation in this range permitted only during aerobatics or spins, and to psi for seconds with PCL at IDLE. |

|Normal oil pressure during steady state conditions is to psi. Operation at oil pressure less than psi at flight idle or above is |

|indicative of oil system malfunction. |

|Acceptable for ground operation at and below 20% torque. |

|Torque at 132% is a materials limit above which damage to the engine may occur. Torque above is indicative of a system malfunction. |

|Allowable torque range with Np stabilized and PCL at IDLE. |

|AIRSPEED LIMITATIONS |STARTER CYCLE LIMITATIONS |

|MAXIMUM AIRSPEED GEAR DOWN (VLE) & FLAP DOWN (VFE) KIAS |STARTER DUTY CYCLE IS LIMITED TO FOUR CYCLES |

| |COOLING PERIOD AFTER FIRST STARTER CYCLE |

|MAX OPERATING (VMO) KIAS / MAX MACH (MMO) MACH |COOLING PERIOD AFTER SECOND STARTER CYCLE |

| |COOLING PERIOD AFTER THIRD STARTER CYCLE |

|TURBULENT AIR PENETRATION SPEED (VG), MAXIMUM: KIAS |COOLING PERIOD AFTER FOURTH STARTER CYCLE |

|MAX OPERATING MANEUVERING (VO) ________ KIAS |FLIGHT MANUEVERING LIMITATIONS |

|MAX WITH FULL RUDDER DEFLECTION ________ KIAS | |

|PROHIBITED MANEUVERS |INVERTED/NEGATIVE G FLIGHT sec |

| |INTENTIONAL ZERO G FLIGHT sec |

| |ACCELERATION LIMITATIONS |

| |SYMMETRIC CLEAN TO Gs |

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| |SYMMETRIC GEAR & OR FLAPS EXTENDED TO Gs |

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| |ASYMMETRIC CLEAN TO Gs |

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| |ASYMMETRIC GEAR & OR FLAPS EXTENDED TO Gs |

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| |FOR UNCOORDINATED ROLLING MANEUVERS INITIATED AT ___G, THE MAXIMUM |

| |BANK ANGLE CHANGE IS DEGREES |

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| |OTHER LIMITATIONS |

| |MIN VOLTAGE FOR BATTERY START VOLTS |

| |MAX CROSSWIND FOR DRY RUNWAY ____ KNOTS |

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| |MAX CROSSWIND FOR WET RUNWAY KNOTS |

|THE AIRCRAFT HAS BEEN APPROVED ONLY FOR TRANSIT THROUGH |MAX CROSSWIND FOR ICY RUNWAY KNOTS |

|FEET OF ICE. | |

|MINIMUM BATTERY VOLTAGE: VOLTS | |

|HYDRAULIC CAUTION: < PSI, > PSI | |

|FUEL CAUTION LIGHT: < POUNDS IN RESPECTIVE WING TANK | |

|COCKPIT PRESSURIZATION SCHEDULE LIMIT: +/- PSI | |

| |MAX TAILWIND COMPONENT FOR TAKEOFF KNOTS |

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