Certificado Tipo

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION H4EU Revision 15 SA330F SA330G SA330J AS332C AS332L AS332L1 AS332L2 EC225LP October 21, 2010 TYPE CERTIFICATE DATA SHEET NO. H4EU This data sheet which is part of Type Certificate No. H4EU prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of theFederal Aviation Regulations. Type Certificate Holder EUROCOPTER FRANCE Aeroport International Marseille Provence 13725 - Marignane - Cedex France

I.

Model SA330F (Transport Helicopter, Categories A and B), approved 23 June 1971. Engine Engine Limits 2 Turbomeca TURMO IV A Sea level static - standard day conditions (59F 29.92 in. hg.) Shaft HP Max. Duration minutes 5 2 1/2 30 No Limit 1/21/2 1/2 Gas Generator RPM 33,300 33,950 33,300 32,800 34,100 Power Turbine Inlet Temperature C 780 790 780 750 800 750 150 (max.)

Takeoff One engine inoperative (2 1/2 mn power rating) One engine inoperative (30 mn power rating) Maximum Continuous Maximum Transient Starting (During (Before 100% = 33,500 r.p.m.

1274 1415 1274 1170

Nominal Free Turbine Speed is: 22,840 r.p.m. Maximum Weight14,800 lb. (Category A and Category B)

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H4EU, Rev 15

II. Model SA330G (Transport Helicopter, Categories A and B), approved 15 May 1974. (Same as Model SA 330F except for more powerful engines andincrease in weight). Engines Engine Limits 2 Turbomeca TURMO IV C See level static - standard day conditions (59F 29.92 in. hg.) Shaft HP Max. Duration minutes 5 2 1/2 30 No Limit 1/2 1/2 Gas Generator RPM 33,450 33,800 32,900 32,400 34,100 Power Turbine Inlet Temperature C 780 790 740 705 790 750 150 (max.)

Takeoff One engine inoperative (2 1/2 mn power rating) One engine inoperative (30 mn powerrating) Maximum Continuous Maximum Transient Starting (During (Before 100% = 33,500 r.p.m.

1495 1555 1380 1260

Nominal Free Turbine Speed is: 22,840 r.p.m. Maximum Weights 15,400 lb. (Category A and Category B)

III. Model SA330J (Transport Helicopter, Categories A and B), approved 9 June, 1976. (Same as Model SA330G except for maximum weight) Maximum Weight 16,300 lb. (Category A and B)INFORMATION PERTINENT TO ALL SA330 MODELS ONLY M.G.B. Limits Nominal Free Turbine Speed: 22,840 r.p.m. Maximum Torque (Takeoff) Maximum Continuous Torque Maximum Torque (One Engine Inoperative) 2 x 108,5 mdaN (2427 hp.) 2 x 78 mdaN (1742 hp.) 156 mdaN (1742 hp.)

(Torques based on torquemeter shaft r.p.m. of 7960) Rotor Limits Maximum: Minimum: 310 r.p.m. 220 r.p.m. when IAS is below 108 knots.240 r.p.m. when IAS is above 108 knots.

See Rotorcraft Flight Manual for other limits. Airspeed Limits C.G. Range Never exceed 167 knots CAS at minimum weight. Variation of VNE with weight and altitude is in the Rotorcraft Flight Manual. Longitudinal: + 177 inches to + 194.7 inches Lateral: Right 3.55 inches Left 3.15 See Rotorcraft Flight Manual for external load C.G. range.

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H4EU,Rev 14

INFORMATION PERTINENT TO ALL SA330 MODELS ONLY (cont'd) Datum 185 inches forward of center reference on the cabin floor (main rotor centroid). Leveling Means Minimum Crew Leveling plates on each side of fuselage. The minimum crew required for IFR operation consists of 2 pilots. For Category A consists of 2 pilots. (For VFR operation). For Category B consists of 1 pilot. (For VFRoperation). 19 (Limited by emergency exits available). 414 U.S. Gallons LH Group = 240 U.S. Gal. at 217.3 inches RH Group = 174 U.S. Gal. at 155.1 inches (See NOTE 1 for data on system fuel and oil). SPECIFICATION (Latest Amendment) NATO U.S.A. U.K. F.34 D. eng. RD 2453 AVTUR/FS.11 AIR 3405 ASTM Jet A TRO F.35 ASTM Jet A-1 D. eng. RD 2494 AVTUR F.40 MIL-T.5624 D. eng. RD2454 AIR 3407 (JP.4) AVTAG FS II...