PILATUS PC-12 SERIES EMERGENCY AND RESCUE CHART OPENING MECHANISM OF PASSENGER/CREW DOOR ENTRY DANGER HOT ZONES! (MSN 101 - 1575) (MSN 1576 - Present) - AOA PROBES x2 - ENGINE EXHAUST x2 1 PULL OUTWARDS TO 1 1 PUSH BUTTON DISENGAGE PIN - ENGINE INTAKE DEICE LIP 2 PULL OUT HANDLE - STATIC PORT x2 2 TURN HANDLE 1 CLOCKWISE - PITOT PROBE x2 3 ENSURE DOOR IS 2 FULLY PULLED OUT MATERIALS 3 ENSURE DOOR IS FULLY 2 PULLED OUT - CARBON FIBER EPOXY - GLASS FIBER EPOXY OPENING MECHANISM OF CARGO DOOR SYSTEMS AND PARTS MATERIALS REFRIGERANT ENGINE OIL TANK 1 PUSH BUTTON 1 14.5 QUART(13.7 US GAL) AOA PROBE COOLING UNIT (R134) FUEL (JET A1 KEROSINE): 2 PUSH BACK PLATE, LIFT HANDLE PITOT PROBE ELT TRANSMITTER PER WING: 757 LITERS (200 US GAL) SYSTEMS AND PARTS 3 PULL CARGO DOOR OUTWARDS 2 RIGHT FUEL TANK REFUELLING POINTS 200 US GAL EMERGENCY EXIT (OPENS OUTWARDS) OXYGEN BOTTLES: 2 OPTIONAL LARGER MAIN OXYGEN BOTTLE 1850 PSI / 22 FT3 3 OXYGEN CYLINDER 1 or 2 LARGE OXYGEN BOTTLES (OPTION) NiCd or LEAD 1850 PSI / 77 FT3 BATTERIES NiCd or LEAD ACID BATTERIES HAND FIRE EXTINGUISHER DOOR ACTUATOR GAS STRUT (BEHIND SEAT) CARGO DOOR NITROGEN HYDRAULIC/TANK 56 PSI OXYGEN CYLINDER 1850 PSI (OPENS UPWARDS) (STANDARD SYSTEM) OIL AND GAS STRUTS FOR THE DOORS OVER-WING EMERGENCY EXIT OPENING PROCEDURE LEFT FUEL TANK 200 US GAL HYDRO PNEUMATIC SHOCK ABSORBER 1 PUSH BUTTON IN PRESSURE 1668 PSI PITOT PROBE HYDRAULIC PUMP/ ACCUMULATOR 2 PUSH EMERGENCY EXIT IN 3000 PSI 3 REMOVE EMERGENCY EXIT AND DISCARD OUTSIDE PASSENGER/CREW DOOR (OPENS DOWNWARDS) 4 BLADE OR 5 BLADE PIPELINES HYDRO PNEUMATIC 2 PROPELLER AOA PROBE FUEL (JET A1 KEROSENE) DANGER AREA SHOCK ABSORBER PRESSURE 834 PSI FUEL MAINTENANCE SHUT-OFF LEVER HYDRAULIC FLUID (AEROSHELL FLUID 41) & FUEL/AIR SEP TANK FUEL FILTER OCCUPANTS 3 2 COCKPIT SEATS AND UP TO 9 CABIN SEATS 1 © Pilatus Aircraft Ltd 6371 Stans, Switzerland. Issue 2.0 Mar 2018 FLIGHT DECK EMERGENCY PROCEDURES ACCESS TO THE FUEL MAINTENANCE SHUT-OFF LEVER 1 PRESS LATCH DOWN, PULL EMERGENCY 1 LOCATE ACCESS PANEL FOR FUEL MAINTENANCE SHUT-OFF LEVER UP 2 a b c SHUT-OFF LEVER (MSN 101 - 400) (MSN 401 - 888) (MSN 1001 - Present) 2 CUT THE ELECTRICAL POWER 2 PRESS 3 LATCHES DOWN TO OPEN QUICK ON MASTER POWER MASTER POWER RELEASE FASTENER a TURN RED BAR TO SET 4 SWITCHES OFF OFF OPEN SAFETY COVER, SET SWITCH TO b c 3 OPEN THE SERVICE DOOR 4 “EMERGENCY OFF” 3 4 PULL RED ROD TO CLOSE FUEL MAINTENANCE PULL OUT EMERGENCY ACS SHUT-OFF VALVE SHUT-OFF HANDLE FUEL EMER SOV HANDLE ACS EMER SOV HANDLE 1 3 1 PRESS TO RELEASE FUEL ACS EMERGENCY EMERGENCY SHUT-OFF SHUT-OFF 4 PULL PULL 2 x3 ACCESS TO THE BATTERY COMPARTMENT 1 LOCATE BATTERY COMPARTMENT 3 2 PRESS 4 LATCHES TO RELEASE 3 ALL 4 LATCHES MUST BE OPEN 4 OPEN SERVICE DOOR 1 DISCLAIMER THIS AIRCRAFT RESCUE AND FIRE FIGHTING INFORMATION SUMMARISES SELECTED DATA AND INFORMATION RELATING TO PC-12 AIRCRAFT CONTAINED IN THE FOCA APPROVED AIRPLANE FLIGHT MANUAL (AFM). IT HAS BEEN PREPARED TO THE ATTENTION OF 2 3 RESCUE AND FIRE FIGHTING PERSONAL WHO MIGHT BE INVOLVED IN A RESCUE OPERATION OF A PC-12. NO UPDATE SERVICE OF THIS DOCUMENT WILL BE PROVIDED. x4 ELT PILATUS REJECTS ALL AND ANY LIABILITY WITH RESPECT TO ANY HANDLING, MAINTENANCE AND/OR OPERATION OF THE PC-12 BATTERY COMPARTMENT BATTERY AIRCRAFT WHICH IS NOT IN FULL AND STRICT COMPLIANCE WITH THE PROVISIONS OF THE PILOT OPERATING HANDBOOK (POH). THE PRESENT DOCUMENT DOES NOT CONTAIN AND SHALL NOT BE DEEMED TO CONTAIN ANY REPRESENTATIONS, WARRANTIES AND/OR COVENANTS REGARDING THE SPECIFICATIONS AND/OR OPERATIONS OF THE PC-12. IN PARTICULAR THE PRESENT DOCUMENT DOES NOT CONTAIN ANY REPRESENTATIONS OR WARRANTIES AS TO THE COMPLETENESS TO THE DESCRIPTION OF POTENTIAL FIRE HAZARDS. IF YOU NEED MORE INFORMATION, PLEASE DOWNLOAD THE PILOTS INFORMATION MANUAL AVAILABLE ON WEBSITE: 4 WWW.PILATUS-AIRCRAFT.COM ➜ CUSTOMER SUPPORT ➜ TECHNICAL PUBLICATION ➜ PC-12 ➜ FLIGHT MANUALS OR CLICK HERE © PILATUS AIRCRAFT LTD MAR 2018, PC-12 © Pilatus Aircraft Ltd 6371 Stans, Switzerland. Issue 2.0 Mar 2018.