PIPER CHEYENNE IIXL PA-31
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1 DEPARTAMENTO SEGURIDAD OPERACIONAL SUBDEPARTAMENTO LICENCIAS SECCIÓN EVALUACIONES PIPER CHEYENNE IIXL PA-31 A.- Operations Limitations 1.- Speed (Kias) Va 184 Vne 242 Vmo 242 Vfe Vle/Vlo (Extension) 153 Vlo (Retraction) 139 Vmca 91 Vs 86 Vso 77 Vx 95 Vy 116 Vsse 118 Vxse 113 Vyse 118 V 1 91 Vapp (flaps 40 ) Fuel (U.S. GAL) Tipo a Utilizar JET-A Capacidad Total 374 Capacidad Utilizable 366 Presión Combustible (PSI) Mínima 5 Máxima Weight (Lbs) Máximo TAKE Baggage FWD 300 Baggage AFT Start 30 Seconds On 1 Minute Off 30 Seconds On 1 Minute Off 30 Seconds On 30 Minutes Cooling 5.- C.G. PESOS FWD RWD or less (max takeoff) (max landing) (max Ramp)
2 B.- Emergencies Procedures 1.- ENGINE SECURING PROCEDURE Generator FEATHER 2.- ENGINE FIRE OR DAMAGE a.- In Flight: Firewall Shutoff Generator PULL FEATHER b.- On Ground: Firewall Shutoff (Af. Eng.) PULL 2
3 3.- ENGINE FAILURE DURING TAKE a.- BEFORE ROTATION (Below 91 Kias) s Brakes AS REQUIRED If Aircraft Departs Runway: Battery Master/Gen Trip Switches Firewall Shutoffs b.- AFTER ROTATION (After 91 Kias) Landing Gear Inoperative Engine VERIFY MCP RETRACT FEATHER & 4.- ENGINE FAILURE DURING FLIGHT a.- If Quick-Start Desired: Generator DO NOT FEATHER b.- If Quick-Start Unsuccessful or Not Desired: Engine Securing Procedure ACCOMPLISH 3
4 5.- ENGINE FLAMEOUT (2 ND ENGINE) DO NOT FEATHER 6.- PROPELLER UNDERSPEED REDUCE TORQUE 7.- ENGINE POWER RUNAWAY a.- If Flight: (Affected Engine) b.- If Power Continues Above Limits: Generator FEATHER c.- On Ground: s BOTH 8.- HIGH OIL TEMPERATURE Oil Cooler Door Power (if necessary) OPEN REDUCE 4
5 9.- LOW OIL PRESSURE a.- Less Than 40 PSI-Oil Pressure Annunciator ON: Power (below 40 PSI) Engine Securing Procedure ACCOMPLISH 10.- SINGLE ENGINE GO-AROUND Directional Control Flaps (If More Than 15 ) Landing Gear ANTICIPATE MCP 620 SHP AS REQUIRED APPROACH UP 11.- BATTERY OVERTEMPERATURE Electrical Load Battery Master CHECK 12.- SINGLE GENERATOR FAILURE Electrical Load Inoperative Generator Non-Essential Bus CHECK/REDUCE AS REQUIRED 5
6 13.- DUAL GENERATOR FAILURE Electrical Load Generator Switches Non-Essential Bus REDUCE TO MIN 14.- ELECTRICAL FIRE Battery Master & Gen Switches Reference for Flight Lighting (If Required) Oxygen PNEUMATIC TURN& SLIP FLASHLIGHT OR DOME AS REQUIRED 15.- AUTOPILOT HARDOVER Flight Control AP Disc/Trim Interrupt Switch MANUALLY OVERPOWER DEPRESS & HOLD 16.- ELECTRIC TRIM RUNAWAY AP Disc/Trim Interrupt Switch DEPRESS & HOLD a.- IF Trim does not stop immediately: AP FD/Avionics Master Switch Manual Trim RETRIM AS REQUIRED 6
7 17.- PRESSURIZATION SYSTEM MALFUNCTION a.- Differential Pressure Above 5.7 PSI or Continual Cabin 5.5 PSI: Press Controller Oxygen (if required) Cabin Pressure (if required) SET TO HIGHER ALT ON DON MASKS DUMP b.- Rapid Increase in Differential Pressure: Oxygen (if required) Cabin Pressure (if required) ON DON MASKS DUMP 18.- SMOKE OR FUMES IN THE CABIN a.- Determine Source if Possible Engines As Source: Oxygen Cabin Altitude Dump Switch (if required) AS REQUIRED SELECT HIGHER DUMP b.- Cabin Originated: Cabin Pressure Oxygen Cabin Air Handle DUMP ON DON MASKS OUTSIDE AIR 7
8 19.- EMERGENCY DESCENT a.- Gear And Flaps Retracted: Aircraft Attitude Airspeed FORWARD BANK Vmo/REDLINE b.- Gear And Flaps Extended: Aircraft Attitude Flaps (Below 181 Kias) Landing Gear (Below 153 Kias) Flaps (Below 148 Kias) Airspeed FORWARD BANK APPROACH EXTEND FULL 148 KIAS MAX RED LIGHT ILLUMINATED AFTER TAKE Airspeed LG handle Position REDUCE TO 130 KIAS MAX. VERIFY 8
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