TCDS E00054EN

1 I I I I I I I I I I I I I I U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. E00054EN TCDS NUMBER E00054EN REVISION: 11 DATE: November 23, 2021 Safran Helicopter Engines, S.A. MODELS: ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 ARRIEL 2C ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2D ARRIEL 2E Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E00054EN) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations, provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. TYPE CERTIFICATE (TC) HOLDER Safran Helicopter Engines, S.A. (formerly Turbomeca, S.A.) 64511 Bordes - Cedex France I. MODELS ARRIEL 2S1, 2S2, 2B, 2B1, 2C, 2C1, 2C2, 2D, 2E TYPE: Turboshaft engine consisting of an axial air intake, an axial compressor and a centrifugal compressor driven by a single stage turbine, a combustion chamber, and a single stage power turbine driving a reduction gearbox located at the rear. An accessory drive gearbox, driven by the gas generator, is located at the front. RATINGS: SHP (KW) (See Note 8) ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 30 second OEI 985 (735) 1048 (771) --- --- 2 minute OEI 889 (663) 950 (699) --- --- Continuous OEI 857 (639) 896 (659) --- --- Takeoff (5 minutes) 817 (601) - - 747 (557) - - Maximum continuous 794 (592) 817 (601) 728 (543) - - 30-minute (See NOTE 23) 817 (601) - - --- --- ARRIEL 2C ARRIEL 2C1 ARRIEL ARRIEL 2D ARRIEL 2E 2C2 30 second OEI 944 (704) 962 (718) 1006 (750) --- 800 (753) 2 minute OEI 851 (635) 865 (646) 956 (713) --- 775 (630) Continuous OEI 818 (610) 838 (616) 858 (640) --- 710 (490) Takeoff (5 minutes) 722 (531) 790 (581) 821 (612) 802 ( 598) 667 (445) Maximum continuous 722 (531) - - 821 (612) 802 ( 598) 575 (360) 30-minute (See NOTE 23) --- --- 821 (612) 802 (598) 667 (445) FUEL/OIL/ADDITIVES: REFER TO INSTALLATION MANUAL PRINCIPAL DIMENSIONS: INCHES (M) Length Width Height ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 60.6 (1.539) 19.8 (0.504) 28.1 (0.715) 60.6 (1.539) 19.6 (0.497) 28.1 (0.715) 46.5 (1.181) 19.6 (0.498) 24.3 (0.616) 44.88 (1.140) 19.33 (0.491) 24.25 (0.616) * PAGE 1 2 3 4 5 6 7 8 9 10 11 12 REV. 11 11 11 9 11 9 11 9 9 9 9 11 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" INDICATES "DOES NOT APPLY" NOTICE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN TCDS E00054EN Page 2 of 12 PRINCIPAL DIMENSIONS: (continued) INCHES (M) ARRIEL 2C Length 46.5 (1.181) Width 19.6 (0.498) Height 24.25 (0.616) ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2D ARRIEL 2E 39.9 (1.015) 19.6 (0.498) 22.6 (0.576) 39.9 (1.015) 19.6 (0.498) 22.6 (0.576) 46.34 (1.177) 19.68 (0.500) 24.25 (0.616) 46.54 (1.182) 19.99 (0.508) 24.25 (0.616) CENTER OF GRAVITY: REFER TO INSTALLATION MANUAL MAXIMUM DRY WEIGHT: Refer to engine manual for definition of dry weight LBS. (KG) ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 289 (131.2) 289 (131) 295 (134.0) 291.5 (132.2) ARRIEL 2C ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2D ARRIEL 2E 289 (131.0) 285 (129.2) 290 (131.5) 293 (132.9) 307 (139.2) DRIVE SHAFT TYPE: REFER TO INSTALLATION MANUAL IGNITION: Low tension, high energy system, including: 1 high-energy (H.E.) ignition unit 2 ignition cables 2 igniter plugs STARTING: CERTIFICATION BASIS: The automatic starting sequence is ensured by the Engine Electronic Control Unit. For detail, see Installation Manual. Title 14 of the Code of Federal Regulations Section 21.29 and Part 33, Amendments 33-1 through 33- 14; and for Arriel 2S1 and Arriel 2C Special Condition No. SC-33-ANE-05 published on April 15, 1996. For Arriel 2C2 and Arriel 2S2, Part 33, Amendments 1 through 14, § 33.28, Amendment 15, Special Conditions 33-ANE-05 and 33-001-SC published June 19, 1998. For Arriel 2D and 2E , Part 33, Amendments 33-1 through 33-15 and Special Condition No. 33-009-SC, published May 27, 2011. MODEL APPLICATION TYPE CERTIFICATE TYPE CERTIFICATE DATE ISSUED / AMENDED CANCELLED ARRIEL 2S1 02/25/94 06/10/96 ARRIEL 2B 04/28/97 05/06/98 ARRIEL 2C 04/28/97 05/06/98 ARRIEL 2C1 11/27/97 09/24/99 ARRIEL 2B1 12/13/98 12/1/00 ARRIEL 2C2 09/12/99 01/10/03 ARRIEL 2S2 03/9/04 12/13/05 ARRIEL 2D 8/26/10 07/12/11 ARRIEL 2E 03/04/13 05/14/14 The aviation authority for France, the Direction Generale de L'Aviation Civile (DGAC), originally type certificated this engine. The FAA validated this product under U.S. Type Certificate Number E00054EN. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of France. PRODUCTION BASIS: ARRIEL 2S1, 2S2 and 2E: Production Certificate Number 5SW. Produced by Safran Helicopter Engines USA (formerly Turbomeca USA) in the United States under license agreement from Safran Helicopter Engines S.A., France. ARRIEL 2S1, 2S2 and 2E: Engine modules, and parts thereof, produced by Safran Helicopter Engines S.A., France, conforming to this type certificate are fully interchangeable with ARRIEL 2S1, 2S2 and 2E engine modules, and parts thereof, produced under Production Certificate Number 5SW. Engines manufactured under Production Certificate Number 5SW shall have the suffix "TEC" added to the engine serial number and shall be included in the required identification data as specified by 14CFR Section 45. TCDS E00054EN Page 3 of 12 IMPORT To be considered eligible for installation on U.S. registered aircraft, each new engine to be exported REQUIREMENTS: to the United States with the DGAC or EASA airworthiness approval shall have a Joint Aviation Authorities (JAA) or EASA Form 1, Authorized Release Certificate. The JAA or EASA Form 1 should state that the engine conforms to the type design approved under the U.S. Type Certificate E00054EN is in a condition for safe operation and has undergone a final operational check. Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the agreement, to identify any required statements by the exporting authority on the export certificate of airworthiness (or equivalent document) , and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for imported aircraft. TCDS E00054EN Page 4 of 12 NOTES NOTE 1. MAXIMUM PERMISSIBLE ENGINE SPEEDS / RPM 30 second OEI rating 2 minute OEI rating Continuous OEI rating Takeoff rating Maximum continuous rating 30-minute rating Maximum inadvertent over speed (<20 sec) ** all engines operating 30 second OEI rating 2 minute OEI rating Continuous OEI rating Takeoff rating Maximum continuous rating 30-minute rating Maximum inadvertent over speed (<20 sec) ** all engines operating Minimum stabilized power on Minimum stabilized power off Minimum transient (<20 sec) Maximum inadvertent overspeed (<20 sec) power on Maximum inadvertent overspeed (<20 sec) power off Maximum stabilized Minimum stabilized power on Minimum stabilized power off Minimum transient (<20 sec) Maximum inadvertent overspeed (<20 sec) power on Maximum inadvertent overspeed (<20 sec) power off Maximum stabilized A. GAS GENERATOR SPEED (N1) ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 55156 53386 52756 52756 51616 52756 53312 ** 55178 53348 52776 53089 51959 53089 53661 ** --- --- --- 52756 50672 --- 53312 --- --- --- - - - - --- - - ARRIEL 2C ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2D ARRIEL 2E 55051 53192 52571 52660 51520 --- 53312 54986 53126 52506 52776 51637 --- - - 55265 53275 52764 53079 51922 53079 - - --- --- --- 53086 52050 53086 53568 55186 54480 53102 52518 51572 52518 53102 ** For variation of these limits with outside air temperature (OAT), refer to Installation Manual. For required action if limits are exceeded, refer to Maintenance Manual. 100% = 52,110 rpm B. POWER SHAFT SPEED (N2) ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 35381 35381 26584 42613 47305 42418 - - - - - - 43719 - - - - - - 33230 - - 42613 - - - - - - - - - - - - - - - - ARRIEL 2C ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2D ARRIEL 2E 35381 33230 26584 42613 47305 42418 - - - - - - - - - - - - - - - - - - - - - - - - 35437 33284 26627 - - 46598 42477 - - - - - - 46598 - - 42418 If limits are exceeded, refer to Maintenance Manual. 100% N2 = 39,095 rpm for all Models except Arriel 2D and 2E 100% N2 = 39,158 rpm for Arriel 2D and 2E TCDS E00054EN Page 5 of 12 NOTE 2. MAXIMUM PERMISSIBLE TEMPERATURE 30 second OEI rating 2 minute OEI rating Continuous OEI rating Takeoff rating 30 minute rating Max. continuous rating Starting (<10 seconds) Starting (unlimited) Maximum inadvertent Overtemperature (<20 sec) A. EXHAUST GAS T45, Measured with 8 thermocouples on gas generator turbine diffuser (Degrees °C) ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 1000 941 912 912 912 877 865 750 --- 996 944 926 930 930 893 840 - - --- --- --- --- 915 --- 849 865 - - 941 --- --- --- - - --- - - - - - - - - 30 second OEI rating 2 minute OEI rating Continuous OEI rating Takeoff rating 30 minute rating Max. continuous rating Starting (<10 seconds) Starting (unlimited) Maximum inadvertent overtemperature (<20 sec) **All engines operating A. EXHAUST GAS T45, Measured with 8 thermocouples on gas generator turbine diffuser (Degrees °C) ARRIEL 2C ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2D ARRIEL 2E 1000 941 912 912 --- 877 865 750 --- - - - - - - - - --- - - - - - - --- 996 944 926 929 929 891 840 - - --- --- --- --- 962 962 918 - - - - 994 1035 1016 974 947 947 930 840 760 974** If limits are exceeded, refer to Maintenance Manual for required action. TCDS E00054EN Page 6 of 12 NOTE 2. (continued) B. OIL, Measured at engine inlet Minimum oil temperature -30oC for oil with a kinematic viscosity for engine starting: of 5.4 x 10-5 ft2/sec. -45 oC for oil with a kinematic viscosity of 3.2 to 4.2 x 10-5 ft2/sec for 2B and 2B1. -50oC for oil with a kinematic viscosity of 3.2 to 4.2 x 10-5 ft2/sec for all other models. Minimum oil temperature for power-up: 0oC for oil with a kinematic viscosity of 5.4 x 10-5 ft2/sec. -10oC for oil with a kinematic viscosity of 3.2 to 4.2 x 10 -5 ft2/sec. Maximum oil temperature for all Models except Arriel 2D and 2E: 115oC Maximum oil temperature for Arriel 2D and 2E (measured at a different location from other Models) 117 oC C. FUEL, Measured at engine inlet 1. Maximum temperature: REFER TO INSTALLATION MANUAL 2. Minimum temperature: REFER TO INSTALLATION MANUAL 3. For 2S1, 2B, 2B1, 2C , 2C1, 2D and 2E: Use of anti-icing additive for fuel temperature <-20°C For 2C2 and 2S2: Use of anti -icing additive for fuel temperature <-30°C 4. Starting: REFER TO INSTALLATION MANUAL TCDS E00054EN Page 7 of 12 NOTE 3 POWER TURBINE UNIT TORQUE LIMITS / FOOT - POUND (daNm) 30 second OEI rating 2 minute OEI rating Continuous OEI rating Takeoff Maximum continuous Max. inadvertent over-torque ( < 20 sec) 30-minute rating 30 second OEI rating 2 minute OEI rating Continuous OEI rating Takeoff Maximum continuous Max. inadvertent over-torque (< 20 sec) 30-minute rating ARRIEL 2S1 ARRIEL 2S2 ARRIEL 2B ARRIEL 2B1 887 (120.3) - - --- --- 835 (113.2) - - --- --- 756 (102.5) - - --- --- 682 (92.5) - - 673 (91.3) - - 682 (92.5) - - - - 673 (91.3) 975 (132.2) - - - - 1055 (143) 682 (92.5) - - --- --- ARRIEL 2C ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2D ARRIEL 2E 861 (116.8) 875 (118.7) 880 (119.3) --- 883(119.8) 791 (107.3) 796 (107.9) 856 (116.0) --- 740(100.3) 760 (103) 749 (101.55) 751 (101.8) --- 575(78.0) 682 (92.5) - - 718 (97.3) 708 (96.0) 522(70.8) 682 (92.5) - - 718 (97.3) 708 (96.0) 423(57.3) - - - - 975 (132.2) 989 (134.2) 856(116) 718 (97.3) 708 (96.0) 522(70.8) NOTE 4. FUEL AND OIL PRESSURE LIMITS A. FUEL PRESSURE, at engine inlet A. Minimum fuel pressure 1. Normal operation, excluding starting phase, the minimum (absolute) pressure is defined for all models except Arriel2D and 2E, by the highest of the following conditions: 2.9 PSIA (20kPa) 35% of atmospheric pressure, 1 PSI (7 kPa) above the vapor pressure of the fuel used, Fuel pressure corresponding to a vapor volume over Liquid volume ratio of 0.30 For Arriel 2D and 2E: Refer to Installation / Operating Manual 2. During the starting phase or at relight, fuel pressure (relative) must not be less than: +3.6 PSIG (25 kPa) for the 2S1 +2.9 PSIG (20 kPa) for the 2S2 +3.6 PSIG (25 kPa) for the 2B, 2B1, 2C, 2C1, 2C2, 2D and 2E. B. Maximum fuel pressure: Less than or equal to 21.8 PSIG (150 kPa) (relative pressure) in all operating phases, for all Models except Arriel 2D and 2E. Less than or equal to 26.1 PSIG (180kPa) (relative pressure), in all operating phases, for Arriel 2D and 2E. B. OIL PRESSURE, 1. Minimum Oil Pressure (relative): For 2S1, 2B, 2B1, 2C and 2C1: 16.0 PSIG (110 kPa) For 2C2 and 2S2: 24.7 PSIG (170 kPa) For 2D and 2E: Refer to Installation / Operating Manual 2. Maximum Oil Pressure (relative): For 2S1, 2S2, 2B, 2B1, 2C, 2C1 and 2C2: 87.0 PSIG (600 kPa) For 2D and 2E: Refer to Installation / Operating Manual TCDS E00054EN Page 8 of 12 NOTE 5. MAXIMUM PERMISSIBLE AIR BLEED FROM CENTRIFUGAL COMPRESSOR PLENUM Maximum air mass flow at Takeoff and Max. Continuous: 0.22 lb/sec for all Models except Arriel 2D and 2E Maximum air mass flow at Takeoff, Max. Continuous and 30-minutes rating: 0.33 lb/sec for Arriel 2D and 2E Power loss due to air bleed: For further details, see Installation and Operating Manual. NOTE 6. AIR INTAKE REQUIREMENTS The ARRIEL engines have not been tested to evaluate the effects of foreign object ingestion other than rain water. Foreign object ingestion characteristics of airframe air inlet and engine combination are to be evaluated prior to approval of the engine installation, for all remaining foreign objects. The ARRIEL engines do not have anti-icing provisions and have not been tested to evaluate the effects of icing conditions. Anti -icing characteristics of airframe, air inlet, and engine combination are to be evaluated prior to approval of the engine installation. The ARRIEL 2S1 engine meets the requirements of § 33.68(a) and (b) when installed with Sikorsky S76C+ helicopter air intake assembly Part Number (P/N) 76300-07761-101. The helicopter air intake design shall be such as to prevent instantaneous ingestion of ice, snow and water in excess of maximum quantities defined in the Installation and Operating Manual. A protective grid, as defined in the Installation and Operating Manual shall be installed to limit the ingestion of foreign matter in the engine. The Arriel 2B, 2B1 and 2D are not approved for operation in icing conditions with Eurocopter AS 350 B3 / EC 130 sand filter P/N 704 A 41 650 010. The ARRIEL 2S2 engine meets the requirements of § 33.68(a) and (b) when installed with Sikorsky S76C++ helicopter air intake assembly P/N 041277880, barrier filter P/N 76302- 07800, inlet bellmouth P/N 76304-07009-049 and heated duct P/N 0401277880. The Arriel 2B and 2D engines meet the requirements of § 33.68(a) and (b) when installed with Eurocopter AS 350 B3 helicopter air intake P/N 350.A.54.1080.04 and protection screen P/N 350.A.58.1607.03. The engines are not approved for operation in icing conditions with Eurocopter AS 350 B3 sand filter P/N 704.A.41.650.010. The Arriel 2B1 and 2D engines meet the requirements of § 33.68(a) and (b) when installed with Eurocopter EC 130 helicopter air intake P/N 350.A.54.1080.04 and protection screen 350.A.58.1607.03. The engines are not approved for operation in icing conditions with Eurocopter EC 130 sand filter P/N 704.A.41.650.010. The Arriel 2C and 2C1 engines meet the requirements of § 33.68(a)(b) when installed with Eurocopter AS 365 N3 helicopter air intake ducts consisting of P/N 365.A.24.0110.04/05 (MGB section, left/right sides respectively) and P/N 365.A.54.5022.01 (engine compartment section, both sides), along with protection screen P/N 365.A.24.1067.02/03 (left/right sides respectively). The Arriel 2E engines meet the requirements of § 33.68(a) and (b) when installed with the following Aircraft air intake and inlet Part Numbers (P/N): - Intake protection outer LH assy P/N 117-602351 - Intake protection inside RH assy P/N 117-602401 - Intake protection inside LH assy P/N 117-602371 - Intake protection outer RH assy P/N 117-602421 - Air inlet LH P/N D710M1010801 - Air inlet RH P/N D710M2010801 For further details, see Installation and Operating Manual. The 2B, 2B1, and 2D installation are approved for single-engine application only. The 2C, 2C1, 2C2, 2S1, 2S2, and 2E engine models are restricted to multi-engine helicopter applications. TCDS E00054EN Page 9 of 12 NOTE 7. ACCESSORY DRIVE PROVISIONS Designation Direction* Of Rotation Rotation Speed rpm Maximum Torque in Overload (in-lb) Maximum Static Overhang (in-lb) Fuse Shaft Breakaway Torque (in-lb) Maximum Permanent Shaft Power(SHP) Twin engine OEI situation Starter-generator 2S1 2S2 2C/2C1 2C2 2E 2B/2B1 2D CW 11330 443 456 221 841 10.1 4.7 4.7 6.7 16.1 (1) 10.1 10.1 6.7 6.7 16.1 (1) 10.1 (single engine) 12.1 (single engine) Oil cooling fan output drive: 2S1/2S2 2C2 CCW CCW 12253 11452 89 89 133 133 885 885 2.0 2.0 2.0 2.0 For Accessories: Oil pump pack HP fuel pump LP fuel pump Control system Alternator CW CCW CCW 11883 11883 12180 *CW: clockwise; CCW: counterclockwise. The rotation direction of the power drives for the accessories is indicated conside ring the power drive seen from the outside. The rotation direction of the engine rotors is indicated with respect to viewing the engine from its rear end. For further details see Installation Manual. (1) For Arriel 2E, refer to the Installation and Operating Manual for detailed power shaft extraction in case of failure Oil cooling fan output drive is available on 2S1 and 2C2 only. NOTE 8. ENGINE RATINGS Engine ratings are based on calibrated test rig with performance under the following conditions: Static, sea level standard conditions (59 o F, 29.92” Hg) No airbleed, no accessory power extraction 6,409 RPM output shaft drive speed for 2S1 and 2S2 6,000 RPM output shaft drive speed for 2B/2B1, 2C, 2C2, 2D, and 2E Fuel load heat value = 18,545 BTU/lb The ratings given above are minimum final test performance of production and overhaul engines in accordance with engine acceptance test specification: No. 0.292.02.941.0 for 2S1 No. 0.292.02.945.0 for 2B No. 0.292.02.949.0 for 2B1 No. 0.292.02.944.0 for 2C No. 0.292.02.948.0 for 2C1 No. 0.292.02952.0 for 2C2 No. 0.292.02953.0 for 2S2 No. AA049722 for 2D No. AA043433 for 2E Use the exhaust pipe specified below with calibrated test bed air intake No. 6.528.12.500.0 for 2S1, 2B, 2B1, 2C, and 2C1and No. 6.528.12.501.0 for 2C2, 2S2, 2D and 2E. Exhaust pipe No. 0.292.81.500.0 is part of the engine definition (primary exhaust pipe), and is common to the 2S1, 2B, 2B1, 2C, and 2C1. Exhaust pipe No. 0.292.81.502.0 is part of the engine definition (primary exhaust pipe), and is common to the 2S2 and 2C2. Exhaust pipe No. 0.292.81.047.0 is part of the Arriel 2D engine definition (primary exhaust pipe) Exhaust pipe No. 0.292.81.053.0 is part of the Arriel 2E engine definition (primary exhaust pipe) TCDS E00054EN Page 10 of 12 NOTE 9. FUEL SUPPLY REQUIREMENTS The ARRIEL 2S1, 2S2, 2B, 2B1, 2C, 2C1, 2C2, 2D and 2E have a fuel filter supplied with the engine. Use of anti-icing additive for fuel temperature: < -20 oC for Arriel 2B, 2B1, 2C, 2D, 2E, 2C1, and 2S1. < 30 oC for Arriel 2C2 and 2S2 NOTE 10. OIL SYSTEM: Refer to Installation Manual. NOTE 11. ENGINE MONITORING TRANSMITTERS: Refer to Installation Manual. NOTE 12. CONTROL SYSTEM: Single channel electronic engine control system with manual backup for 2S1, 2B, and 2C. Dual channel electronic engine control system with optional auxiliary backup control for 2B1, 2C1, 2C2 and 2S2. Dual channel electronic engine control system with auxiliary back-up control for 2D. Dual channel electronic engine control system for 2E. NOTE 13. ENGINE FIRE DETECTOR The ARRIEL 2S1 and 2S2 have no fire detectors installed on the engine. The Arriel 2B, 2B1, 2C, 2C1 and 2C2 feature mounting and wiring for installation of three fire detectors. Fire detectors are not part of the engine definition. The Arriel 2D feature mounting and wiring for installation of three fire detectors. Fire detectors are part of the engine definition. The Arriel 2E feature mounting and wiring for installation of one fire detector. Fire detector is part of the engine definition. NOTE 14. Refer to Installation Manual for approved oil specifications. NOTE 15. Refer to Installation Manual for approved fuel and additive specification. NOTE 16. Life-limited components are listed in EASA-approved Airworthiness Limitations Section (Chapter 5) of the engine Maintenance Manual. NOTE 17. Permissible overhaul and inspection intervals are listed in EASA- approved Airworthiness Limitations Section (Chapter 5) of the engine Maintenance Manual. NOTE 18. MANUALS REQUIRED BY § 33.5 ARRIEL 2S1 ARRIEL 2B ARRIEL 2B1 ARRIEL 2C ARRIEL 2C1 ARRIEL 2C2 ARRIEL 2S2 ARRIEL 2D ARRIEL 2E Performance Manual No. Installation Manual No. Operation Manual No. Maintenance Manual No. Repair Manual No. X 292 L0 001 9 X 292 M5 001 9 X 292 N5 002 9 X 292 M1 001 9 X 292 N4 002 9 X 292 N6 002 9 X 292 P5 001 9 AA049088 AA056554 X 292 L0 001 1 X 292 M0 001 2 X 292 N5 001 9 X 292 M1 001 2 X 292 N4 001 2 X 292 N6 404 1 X 292 P5 001 2 X 292 R1 001 2 X 292 R2 001 2 See Note 19 See Note 19 See Note 19 See Note 19 See Note 19 See Note 19 See Note 19 See Note 19 See Note 19 X 292 L0 301 2 X 292 M5 450 2 X 292 N5 450 2 X 292 M1 450 2 X 292 N4 450 2 X 292 N6 450 2 X 292 P5 451 2 X 292 R1 450 2 X 292 R2 300 2 X 292 L0 500 2 --- --- --- --- X 292 P5 550 2 X 292 R1 500 2 X 292 R2 500 2 NOTE 19. The Operation Manual is contained within Chapter 15 of the Installation Manual. NOTE 20. DELETED. TCDS E00054EN Page 11 of 12 NOTE 21. Each of the documents listed below must state that it is approved by the European Aviation Safety Agency (EASA) or, for approvals made before September 28, 2003 by the Direction Generale de L'Aviation Civile (DGAC). Any such documents including those approved under a delegated authority, are accepted by the FAA and are considered FAA accepted. • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. These approvals pertain to the type design only. NOTE 22. The Models shown on this TCDS have the following general characteristics: MODELS CHARACTERISTICS ARRIEL 2S1 Base Model ARRIEL 2B Similar to ARRIEL 2S1. The rating structure is simplified for single eng ine application: Takeoff and Maximum Continuous ratings only. The main differences are the mounts, provision for the tail rotor drive, and the deletion of the oil cooler fan drive on the reduction gearbox. ARRIEL 2B1 Similar to ARRIEL 2B. The main diff erence is the dual channel electronic engine control system. ARRIEL 2C Similar to ARRIEL 2S1. The main differences are the mounts and the deletion of the oil cooler fan drive on the reduction gearbox. ARRIEL 2C1 Similar to ARRIEL 2C. The main differ ence is the dual channel electronic engine control system. ARRIEL 2C2 Similar to engine ARRIEL 2C1, main differences being the increased power ratings, (thermal and torque) the HIP/SARM rating (similar to 2S1), new HPT material and new axial compressor wheel. ARRIEL 2S2 Similar to the ARRIEL 2S1. The main differences are a control system with a dual channel FADEC with mechanical back-up, increased power ratings and new HPT blade material and new axial compressor wheel (similar to 2C2). ARRIEL 2D Similar to the ARRIEL 2C2. The main differences are: it is a single-engine application that has a 30-minute Take-off Power Rating, new dual channel electronic control system, new power turbine rear bearing support with new containment ring, new power turbine blade profile, and engine mounts identical to those of the Arriel 2B/2B1. ARRIEL 2E Similar to the ARRIEL 2D. The main difference s are: it is a dual-engine