TCDS TC 760

P a g e N o . 123 R e v . N o . 100 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 760 Revision 1 FS 2000 Corp L-14 March 30, 2001 AIRCRAFT SPECIFICATION NO. 760 Type Certificate Holder FS 2000 Corp 709 Dupont Street, P.O. Box 1678 Bellingham, WA 98227-1678 Type Certificate Ownership Record The New Piper Aircraft, Inc 2926 Piper Drive Vero Beach, Florida 32960 TC-760 transferred 9-25-00; reissued 3-30-01 Model L-14: 3 PCLM (Normal Category, See Note 1(b)); 3 PCLM (Utility Category, See Note 1(a)); Approved July 31, 1945 Engine Lycoming O-290-C Fuel 73 minimum octane aviation gasoline Engine Limits Take-off--2800 rpm (130 hp) All other operations – 2600 rpm (125 hp) Airspeed Limits Level Flight or Climb 125 mph (109 knots) (True Indicated) Glide or dive 169 mph (147 knots) Flaps Extended 81 mph ( 70 knots) Propeller limits Not more or less than 2350 rpm (Static rpm at maximum permissible throttle setting) Diameter Not more than 76 inches Not less than 74 inches C. G. Range (+11.0) to (+20.0) Datum Wing leading edge Leveling Means Plumb bob from lug on fuselage member between wing hinge fittings to fixed point on floorboard at door. Maximum Weight 1800 lbs. Number of Seats 3 (two ( +38), pilot (+9)) (See NOTE 1 for alternate arrangement with copilot or attendant (+15), patient (+55)) Baggage None Fuel Capacity 30 gallons (two wing tanks at 14 gallons (+23); fuselage header tank at 2 gallons (-16)) Oil Capacity 2 gallons (-39) TC-760 2 Control Surface Elevator 22° Up 30° Down Movements Rudder 16° right 17° Left (relative to airplane ref. axis) Ailerons 28° Up 23° Down Stabilizer -2° -12° Down Flaps 40° Down (maximum) Serial Numbers Eligible 5-3000 and up Required Equipment Items 1, 101, 201, 202, and 406 SPECIFICATIONS PERTINENT TO ALL MODELS Certification Basis Type Certificate No. 760 (CAR 4a) Production Basis None (See NOTE A) Export Eligibility Eligible for export to all countries except Great Britain, Australia, Canada, and New Zealand EQUIPMENT: (Plus sign (+) indicates net increase) Propellers and Propeller Accessories 1. Propeller - Sensenich 76JB44, or any other fixed pitch wood propeller which is eligible for the engine speed and power and which meets the static RPM and diameter specified on page 1 14 lbs. (-57) Engines and Engine Accessories - Fuel and Oil Systems 101. Carburetor air heater and control 2 lbs. (-30) 102. Carburetor air scoop and filter ( Skinner or equivalent) 3 lbs (-45) 103. Cabin Heater 3 lbs (-32) 104. Starter, Eclipse Model 56C, Type 756 (24V) 19 lbs (-27) 105. Generator, Eclipse Model 2, Type 1235 17 lbs (-27) Landing Gear and Floats 201. 6.00-6 wheels (Hayes 601M) with expander tube brakes and 7.00-6, 4 ply tires 33 lbs (-2) 202. 6x2.00 steerable tail wheel and tire (Scott3-24E) 6 lbs (+197) Electrical Equipment 301. Voltage Regulator, Eclipse Model I, Type 1524 2 lbs (-16) 302. Battery, 24 volt, 12AC7D and solenoid 35 lbs (+72) 303. Landing light (AN3095-2A) 6 lbs (+14) 304. Position lights (must be of approved type – see NOTE 2) 3 lbs (+65) 305. Dome Lights (Piper) No weight change Interior Equipment 401. Litter 30 lbs (+61) 402. Attendant and co-pilot seat 5 lbs (+15) 403. Litter tie down equipment 2 lbs (+65) 406. Instruments (required) (airspeed indicator, tachometer, oil pressure and temperature gage, altimeter, compass) 6 lbs (-9) 407. Instruments (optional) (clock, turn and bank indicator, rate of climb indicator, ammeter) 4 lbs (-9) 3 TC-760 NOTE A. Prior to original certification, each aircraft must satisfactorily pass: (a) An inspection for workmanship, materials and conformity before any covering, metal priming or final finish is applied. All woodwork may be varnished. (b) A final inspection of the completed aircraft. (c) A check of the flight characteristics. NOTE 1. The following alternate seating arrangement is authorized: (a) When the aircraft is used as an ambulance: (1) The litter installation (item 401) replaces the rear seat. (2) The attendant’s seat (item 402) is installed adjacent to the pilot’s seat. (3) With this seating arrangement the total number of occupants is limited to three. (b) When the aircraft is used for observation: (1) Co-pilot’s seat (item 402) is installed adjacent to pilot’s seat. (2) With this seating arrangement, pilot and co-pilot occupy the two forward seats with one person seated on the rear seat. (3) With this seating arrangement the total number of occupants is limited to three. NOTE 2 The following apply to position lights and tail lights: (a) If Army Type A-9 position lights are installed, the sand blasted area on the inside of the streamlined glass cover should be painted black. As an alternative, the streamlined glass cover may be replaced by a glass globe and a streamlined metal cover obtained from a Grimes Model E light. (b) If an approved AN3092-2 tail light is installed, it should be repl aced with an approved tail light. ....END....