AIRCRAFT CRASH RECOVERY GUIDE CESSNA 335 & 340A CESSNA AIRCRAFT ‘A SANDPIPER PUBLICATIONAIRCRAFT CRASH RECOVERY GUIDE Fuel: 1001.1, Fuel Capacity: 100 US Gal. (3781) Optional Fuel: 203 US Gal. (768L) ‘Tire Pressure: Standard Air May Be Used Nose: 40 PSI Main: 60 PSI Ground Power: 24 VDC General Service 28 VDC Engine Start Cruise (max) - 264 mph (42Skmb) Ceiling = 12,800 ft (9,085m) Range = 1,586 mi (2,552km) Seating - 6 Empty - 3,911 Ibs (1,774ke) Take-Off | - 5,990 Ibs (2,717kg) Landing - §,750 Ibs (2,608kg) Span -38 ft OL in (11.61m) Length - 34 ft 04 in (10.46m) Height -12 ft 07 in (03.84m) CESSNA AIRCRAFT ‘A SANDPIPER PUBLICATIONAIRCRAFT CRASH RECOVERY GUIDE EMERGENCY RESCUE ACCESS CESSNA MODELS 335 AND 340A MAXIMUM SEATING CAPACITY 6 1. ewencency ext (NO EXTERNAL HANOLE, EXTERNAL RELEASE NOT rossiocs) 2. urns aaaaaae access 2008 stomieangente ap + scHoP OUT" AREA 2. casin D00R (SOP MARKED ON AIRPLANE) METAL CuTTiNG PORTABLE POWER EOuvent. 70 AvOw INuURY OUP WINDOW AND DETERMINE COcATION OF PERSONNEL WITHIN {TALCONE acCESS THROUGH + -cuor ours aned © CABIN Fite EXTINGUISHER (NOP MARKED ON AIRPLANE) Note 4 scHOP OUT" AREA. Je OxrGen Lines ARE LOCATED IN THE [MOT MARKED ON " SCuGr OUT" AREA AT TOP OF A PLANE, SHUT OFF OXYGEN BOTTLe(S) PRIOR TO START OF 4. EMERGENCY ExrT CUTTING OPERATION IF TIME PERMITS, fandielene Seana Feeaerr Sedetttaaeet ies a Rare Shani arta eathnentteae "2. caain 000R . CABIN DOR PULL RANDLE OUT ANO ROTATE HaNDLe CLOCKWISE UNTIL LOCKING PINS DISENGAGE UT UPRER BoOR UNTIL UbLocks Engage FANOLE Unie THE LOCKING Pins DISENGAGE FO0OR TS JAMMED = PRY OUT THESE PROCEDURES WERE SPECIFICALLY DESIGNED FOR AIRPLANE MODELS 995 AND Hom HOWEVER nist OF THe RFORMATION SHON WILL APRLY TO HE EARLER CESSNA AIRCRAFT ‘A SANDPIPER PUBLICATIONAIRCRAFT CRASH RECOVERY GUIDE FLAMMABLE MATERIAL / PRESSURE VESSEL LOCATIONS CESSNA 335 & 3404 OxvGEN BOTTLE - 1850 Ps! (neseune vessel) [Scare unoes aAcaace GOMPARTMENT FLOOR (COME AIRPLANES) OXYGEN BOTTLE - 1800 PS} (@nessune vessel) (Sone AIRPLANES) BRAKE HYDRAULIC RESERVOR, HYDRAULIC FLUID IS MICH S606 ENGINE FIRE EXTINGUISHER BOTTLE (PRESSUAE VESSEL) ALON 1501 600 Pe MAIN FUEL TANK auauiany’ POEL TANKS BATTERY (LEAD ACID)” FYASGAATOR MODULES etecrnodiie (SOME AIRPLANES) Barren ie BATTERY 1S CHARGED SYSTEM SEALED CONTAINER CABIN FIRE EXTINGUISHER’ VENTED OUTSIDE fPnESGURE VESSEL) YE AIRSLANE FIALON 1901200 PS (SOME AIRPLANES) EMERGENCY LOCATOR ‘TRANSMITTER (2 LOCATIONS) WHEELS CONTAIN MAGNESIUM COMPONENTS. WARNING: APPROAGH LANDING GEAR FROM FORWARD OR ‘APT WEN FIGHTING WHEEL FIRE FIRE AND SMOKE VISIBLE: Ccasiv Fine ExriNGUISHER (@nescune VeSsey) HALON 301200 PS (SOME AIRPLANES) ENGINE Fine EXTINGUISHER BOTTLE (PRESSURE VESSEL) ALON 1801 -c00 Pst MAIN FUEL TANK RUXIUARY Riou ony. CONDENSER MODULE Wii RvORAULIC ResenvoIn (SOME AIRPLANES) HYDRAULIC FLUID ISiuitensog Wie ACPRIGERANT CHARGED SYSTEM \WINDHIELD ALCOHOL RESERVOIR SSorngey. ALCOHOL mice (RH ONLY) MANO FRE EINGUISHER (PRESSURE VESSEL) EXTON 213-200 Pa WARNING: ALTHOUGH CABIN INTERIOR FURNISHINGS ARE FABRICATED FROM FAR APPROVED MATERIALS, THESE MATERIALS MAY GIVE OFF ‘Tome FUMES, MELT ANDO COMBUST DURING EXPOSURE TO EXTREME HEAT. USE OF PROTECTIVE CLOTHING AND BREATHING [APPARATUS ARE REQUIRED UNTIL VOU ARE SURE THE AREA IS SAFE. CESSNA AIRCRAFT ‘A SANDPIPER PUBLICATIONAIRCRAFT CRASH RECOVERY GUIDE FUEL AND ELECTRICAL SHUTDOWN CESSNA 335 & 3404 OF BATTERY. CESSNA AIRCRAFT ‘A SANDPIPER PUBLICATIONAIRCRAFT CRASH RECOVERY GUIDE CESSNA AIRCRAFT ‘A SANDPIPER PUBLICATION