T-6B EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS & OPERATING LIMITATIONS EMERGENCY PROCEDURE CRITICAL ACTION MEMORY ITEMS ABORT START PROCEDURE EMERGENCY ENGINE SHUTDOWN ON THE GROUND EMERGENCY GROUND EGRESS IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS: ABORT ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF (SUFFICIENT RUNWAY REMAINING STRAIGHT AHEAD) ENGINE FAILURE DURING FLIGHT IF CONDITIONS DO NOT WARRANT AN AIRSTART: 1 01 DECEMBER 2017 (Change 1)
IMMEDIATE AIRSTART (PMU NORM) IF AIRSTART IS UNSUCCESSFUL: IF AIRSTART IS SUCCESSFUL: UNCOMMANDED POWER CHANGES / LOSS OF POWER/ UNCOMMANDED PROPELLER FEATHER IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT: IF POWER IS INSUFFICIENT TO COMPLETE PEL: COMPRESSOR STALLS IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT: IF POWER IS INSUFFICIENT TO COMPLETE PEL: INADVERTENT DEPARTURE FROM CONTROLLED FLIGHT 2 01 DECEMBER 2017 (Change 1)
FIRE IN FLIGHT IF FIRE IS CONFIRMED: IF FIRE IS EXTINGUISHED: IF FIRE DOES NOT EXTINGUISH OR FORCED LANDING IS IMPRACTICAL: IF FIRE IS NOT CONFIRMED: SMOKE AND FUME ELIMINATION/ELECTRICAL FIRE CHIP DETECTOR WARNING *1 a. b. c. OIL SYSTEM MALFUNCTION OR LOW OIL PRESSURE IF ONLY AMBER OIL PX caution ILLUMINATES: IF RED OIL PX WARNING ILLUMINATES AND/OR AMBER OIL PX CAUTION REMAINS ILLUMINATED FOR 5 SECONDS, OIL PRESSURE FLUCTUATIONS, OR OIL TEMPERATURE OUT OF LIMITS: LOW FUEL PRESSURE OBOGS FAIL MESSAGE OBOGS FAILURE / PHYSIOLOGIAL SYMPTONS EJECT 3 01 DECEMBER 2017 (Change 1)
DDD FORCED LANDING PRECAUTIONARY EMERGENCY LANDING (PEL) 4 01 DECEMBER 2017 (Change 1)
ENGINE OPERATING LIMITS TABLE POWER SETTING TORQUE % ITT C N 1 % (1) N P % (4) OIL PRESSURE psi OIL TEMP C TAKEOFF/MAX IDLE START TRANSIENT % (9) - - - (2) (6) ( sec) ( sec)(8) ( sec) Min (flight) Min (Grnd) (Flt) (7) - - - - - - Min (3) ( sec) (5) ( minutes) NOTES 1. N 1 values presented for PMU ON. With PMU OFF, N 1 may vary from these values. 2. With PMU OFF, permissible maximum N P is +/- %. 3. Permissible at all powers for completion of flight in emergency. 4. Avoid stabilized ground operation from % N P. 5. Operation in this range permitted only during aerobatics or spins, and psi for seconds with PCL at IDLE. 6. Normal oil pressure during steady state conditions is psi. Operation at oil pressure less than psi at flight idle or above is indicative of oil system malfunction. 7. Acceptable for ground operation at and below % rque. 8. Torque at % is a materials limit above which damage the engine may occur. Torque above % is indicative of a system malfunction. 9. Allowable rque range with Np stabilized and PCL at IDLE. AIRSPEED LIMITATIONS MAXIMUM AIRSPEED GEAR DOWN (V LE) & FLAP DOWN (V FE) KIAS STARTER CYCLE LIMITATIONS STARTER DUTY CYCLE IS LIMITED TO FOUR COOLING PERIOD AFTER FIRST STARTER CYCLE CYCLES MAX OPERATING (V MO) KIAS / MAX MACH (M MO) MACH COOLING PERIOD AFTER SECOND STARTER CYCLE COOLING PERIOD AFTER THIRD STARTER CYCLE TURBULENT AIR PENETRATION SPEED, MAXIMUM: PROHIBITED MANEUVERS KIAS COOLING PERIOD AFTER FOURTH STARTER CYCLE INVERTED FLIGHT FLIGHT MANUEVERING LIMITATIONS sec 1. 2. 3. 4. 5. 6. 7. INTENTIONAL ZERO G FLIGHT sec NEGATIVE G FLIGHT Negative G Operations sec Do not exceed -2.5 G for longer than sec Min. pos. Gs upright before additional neg. Gs sec ACCELERATION LIMITATIONS SYMMETRIC CLEAN TO Gs SYMMETRIC GEAR & FLAPS EXTENDED TO Gs ASYMMETRIC CLEAN TO Gs 8. 9. 10. ASYMMETRIC GEAR & FLAPS EXTENDED TO Gs FOR UNCOORDINATED ROLLING MANEUVERS INITIATED AT G, THE MAXIMUM BANK ANGLE CHANGE IS DEGREES OTHER LIMITATIONS 11. THE AIRCRAFT HAS BEEN APPROVED ONLY FOR TRANSIT THROUGH FEET OF ICE. MINIMUM BATTERY VOLTAGE: HYDRAULIC CAUTION: < FUEL CAUTION LIGHT: < PSI, > VOLTS PSI POUNDS IN RESPECTIVE WING TANK COCKPIT PRESSURIZATION SCHEDULE LIMIT: +/- PSI MIN VOLTAGE FOR BATTERY START MAX CROSSWIND FOR DRY RUNWAY MAX CROSSWIND FOR WET RUNWAY MAX CROSSWIND FOR ICY RUNWAY MAX TAILWIND COMPONENT FOR TAKEOFF VOLTS 5 01 DECEMBER 2017 (Change 1)