Piper Aircraft Corporation Chieftain PA31-350 Specifications/Performance

shielded ignition harness Dynafocal engine mounts Propellers - 2 Hartzell, 3 blade extended hub, constant speed, full feathering, with propeller spinners Propeller governors, two Geared starters, 24 volt, two Air filters, two Oil coolers with thermostatic control, two Oil filters, two Alternate air sources - automatic, with manual controls, two Electric cowl flaps, two Dry pneumatic pumps, two Engine driven hydaulic pumps, two FLIGHT INSTRUMENTS AND INDICATORS Piper Truspeed Indicator Magnetic compass (illuminated) I Sensitive altimeter (In. and Mb.) Piper pictorial turn rate indicator Rate of climb indicator 8-day clock 3" pictorial gyro horizon (Air Driven) TSO'd 3" directional gyro (Air Driven) TSO'd Gyro air filter Outside air temperature gauge Ammeter Annunciator panel: Alternator inoperative L/R Pneumatic source inoperative L/R Low fuel flow L/R Fuel boost pump inoperative L/R Heater over temperature Flap Cabin door ajar Nose baggagedoor ajar Dual manifold pressure gauge Pneumatic gauge Dual tachometer Flight bour recorder Fuel quantity gauges, two Dual fuel flow gauge Dual fuel pressure gauge Combination oil pressiJre, oil temperature and cylinder head temperature gauges, two Dual exhaust gas temperature gauge Aileron trim position indicator (illuminated) Elevator trim position indicator (illuminated) Rudder trim position indicator (illuminated) Wing flap position indicator (illuminated) Cowl flap position indicator (illuminated) AVIONICS PROVISIONS Cabin speaker Cockpit speakers, two Headphone and microphone jacks - dual External avionics racks and cabling provisions Provisions for automatic locator beacon Wide choice of optional avionics available Circuit breaker panel, copilot - avionics ICE PROTECTION PROVISIONS Heated pitot head - pilot's Elevator horn anti icing boots Deicing group available for flight in icing conditions EXTERNAL FEATURES Three tone exterior paint design, in a wide choice of color combinations Polyurethane paint - exterior finish Corrosion proofing - internal and external Main wheels - 6:50 x 10 with disc brakes; tires with tubes - 6:50 x 10, 8 ply rating Nose wheel- 6:00 x 6, tire with tube - 6:00 x 6,6 ply rating Aircraft brakes Stowable towbar Tie down rings, three Jack pads Bonding straps across all control surfaces and fiberglass parts for lightning strike protection Nose gear safety mirror Cabin entrance door with built-in steps and pneumatic extender Meets FAR Part 36 noise requirements Cabin, nose and nacelle luggage door locks with keys and carpeting COCKPIT AND CABIN APPOINTMENTS AND PROVISIONS Choice of eleven interior color themes, which incl udes: fabric and vinyl seats, fabric Side panels, wall to wall carpeting, vinyl headliner and color keyed curtains Continued on back page Standard Equipment Continued Pilot/copilot seats - fabric and vinyl with headrests, folding armrests and oxygen mask storage underneath each seat. Seats adjust fore and aft, vertically and tilting with shoulder and safety belts and inertia reels." Flashlight that stows under pilot's seat Ash trays, two in crew area Storm windows - pilot and copilot No smoking/seat belt lighted signs with cockpit control switches Forward cabin divider curtain Cirgarette lighter, cockpit Scuff plates, pilot and copilot Shock mounted instrument panels Removable instrument panels, three Two-piece windshield Sun visors, two Four reclining and adjustable passenger seats - fabric and vinyl in Club arrangement with headrests, folding armrests, seat belts, oxygen mask storage underneath each seat, and magazine storage pockets on the back of each seat Provisions for up to eight adjustable passenger seats Ash trays, four located in each seat outboard armrest Emergency exit window Double glazed windows Quietized soundproofing Window curtains Coat hanger support bar Coat hangers, six Luggage compartments with security straps: Cabin walk-in, 22 cu. ft. - 200 Ibs. Fuselage nose, 14 cu. ft. - 200 Ibs. Nacelle, 13.25 cu. ft. - 150 Ibs. each side Removable floorboards Provision for oxygen installation Compass card Compass card holder Weight and balance plotter Pilot's Operating Handbook - Jepp size Passenger briefing cards Aircraft logbook Engine logbooks Certificate of Airworthiness PRODUCT SUPPORT Piper Warranty Form Piper Service Center Directory Inspection Forms The performance information is based on an airplane flown at gross weight under standard sea level atmospheric conditions except as noted and based on the latest data available at the time of publication approval. Take-off and landing performance is optimum. Actual performance depends on pilot techniques, operating surfaces and other factors. It is the responsibility of the pilot to determine that all operations are conducted within approved limits of design gross weight, center of gravity, and in accordance with the FAA-approved Airplane Flight Manual which is the only official source of operating parameters and performance information. In accordance with GAMA format, range provides for taxi, take-off, climb at MCP, cruise at stated mixture and descent with 45-minute reserve at maximum range power. Empty weight in- cludes unusable fuel, full operating fluids and full oil. Piper Aircraft Corporation reserves the right to make changes in specifications, materials, equipment or prices at any time without prior notice or to discontinue models as required. Your Piper Dealer has listings of a wide variety of optional equipment and avionics. Items most frequently chosen by owners are packaged for factory installation at substantial price savings. '!!II PIPER AIRCRAFT CORPORATION LOCK HAVEN. PENNSYLVANIA 17745 995-3-002 10/1/82 Printed in USA @ a BANGOR PUNTA Company f) MEMBER OF GAMA