# TCDS H4NE: Sikorsky Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Sikorsky Aircraft Corporation - Revision: 6 - Revised: February 27, 2017 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 91 - Data sheet PDF: https://openairdocs.org/files/sha256/f8/e3/f8e3317f60e2daad72be716918831aa8bb2d602b09af96a7182983105fb9a119 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/38935D1796D6B9F8862580D4007B1868.0001 - Page: https://openairdocs.org/tcds/H4NE ## Models (2) As the data sheet lists them. - S-70C(M1) - S-70C(M) ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text TCDS NUMBER: H4NE U.S. DEPARTMENT OF TRANSPORTATION REVISION NUMBER: 6 FEDERAL AVIATION ADMINISTRATION SIKORSKY AIRCRAFT MODELS: TYPE CERTIFICATE DATA SHEET H4NE S-70C(M1) S-70C(M) REVISION DATE: February 27, 2017 This data sheet, which is part of Type Certificate Number H4NE, prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate (TC) Holder: Sikorsky Aircraft Corporation 6900 Main Street Stratford, Connecticut 06615-9129 I. - Model Number: S-70C(M1) (Restricted Category) Approved: 2/21/90 (See Note 3) ENGINES: 2 General Electric CT7-2D 2 General Electric T700-GE-401 FUEL: Aviation Kerosene, JP4, JP5, Jet A, Jet A-1, Jet B or JP 8. ENGINE LIMITS: FOR GENERAL ELECTRIC MODEL CT7-2D SHAFT HP (S.L. STD) POWER TURBINE RPM / % GAS GEN. RPM / % TURBINE GAS TEMP/ °C 2 1/2 min. Power 1,725 20,900 / 100 46,070 / 103 911 (Contingency Power) 30 min. Power 1,625 20,900 / 100 45,430 / 102 873 Maximum Continuous 1,595 20,900 / 100 45,240 / 101 858 Power (MCP) ENGINE LIMITS FOR GENERAL ELECTRIC MODEL T700-GE-401 SHAFT HP (S.L. STD) POWER TURBINE RPM / % GAS GEN. RPM / % TURBINE GAS TEMP/ °C 2 1/2 min. Power 1,723 20,900 / 100 45,600 / 102 917 (Contingency Power) 30 min. Power 1,690 20,900 / 100 45,600 / 102 867 Maximum Continuous 1,437 20,900 / 100 43,800 / 98 801 Power (MCP) Page No. 1 2 3 4 5 6 7 Rev. No. 6 5 6 5 5 5 5 H4NE 2 TRANSMISSION LIMITS: Torque / % 2 Minute 120 OEI 115 Dual 30 Minute 120 OEI 106 Dual Continuous 120 OEI 106 Dual ROTOR LIMITS: Power On: Max. 101% (100% = 258 RPM) Min. 96% Power Off: Max. 121% Min. 90% AIRSPEED LIMITS: Maximum (red line) airspeed 180 KIAS C.G. RANGE 352.5 361.0 21,700 19,462 20,700 10,000 346.8 364.0 DATUM: 341.2 inches forward of the main rotor centroid MAXIMUM WEIGHT: 21,700 lbs. MINIMUM CREW: 2 (pilot, copilot) NUMBER OF SEATS: 1 at Sta. 329; 1 at Sta. 366. FUEL CAPACITY: 590 gallons; 2 tanks (LH & RH interchangeable) OIL CAPACITY: 7.3 quarts each engine OTHER OPERATING Sikorsky Publication Operator's Manual S-70C(M1) Helicopter RFM SA4047-70CM1- LIMITATIONS: NFM-000. SERIAL NUMBERS None ELIGIBLE: 3 H4NE TYPE CERTIFICATION FAR 21.25(a)(2), effective January 6, 1975. BASIS: Type Certification No. H4NE issued April 25, 1986, revised February 21, 1990, (See Note 3), for the purpose of: (1) Agricultural (2) External Cargo (3) Forest and wildlife conservation PRODUCTION BASIS: Production Certificate No. 105. EQUIPMENT: The following must be installed in each type helicopter for certification: (1) Sikorsky Publication Operator's Manual S-70C(M1) Helicopter RFM SA4047- 70CM1-NFM-000. (2) Removal of military equipment in accordance with the latest FAA approved Revision of Sikorsky Aircraft Kit Drawing No. 70080-00102, and replace with commercial equipment. Remove T700-GE-401 engines and replace with GE CT7-2D engines. II. Model Number: S-70C(M) (Restricted Category) Approved: 2/21/90. (See Note 3) ENGINES: 2 General Electric CT7-2D1 2 General Electric T700-GE-401 2 General Electric T700-GE-401C FUEL: Aviation Kerosene JP4, JP5, Jet A, Jet A-1, Jet B, or JP 8. ENGINE LIMITS: FOR GENERAL ELECTRIC MODELS CT7-2D1 SHAFT HP (S.L. STD) POWER TURBINE RPM / % GAS GEN. RPM / % TURBINE GAS TEMP/°C 2 1/2 min. Power 1,725 20,900 / 100 46,070 / 103 858 (Contingency Power) 30 min. Power 1,625 20,900 / 100 45,430 / 102 858 Maximum Continuous 1,595 20,900 / 100 45,240 / 101 841 Power (MCP) ENGINE LIMITS: FOR GENERAL ELECTRIC MODEL T700-GE-401 SHAFT HP (S.L. STD) POWER TURBINE RPM / % GAS GEN. RPM / % TURBINE GAS TEMP/°C 2 1/2 min. Power 1,723 20,900 / 100 45,600 / 102 917 (Contingency Power) 30 min. Power 1,690 20,900 / 100 45,600 / 102 867 Maximum Continuous 1,437 20,900 / 100 43,800 / 98 801 Power (MCP) H4NE 4 FOR GENERAL ELECTRIC MODEL T700-GE-401C SHAFT HP (S.L. STD) POWER TURBINE RPM / % GAS GEN. RPM / % TURBINE GAS TEMP/°C 2 1/2 min. Power 1,940 20,900 / 100 44,700 / 100 917 (Contingency Power) 30 min. Power 1,690 20,900 / 100 44,700 / 102 839 Maximum Continuous 1,662 20,900 / 100 43,800 / 98 810 Power (MCP) Absolute torque limitations, regardless of atmospheric conditions for the T700-GE-401C. DUAL ENGINE DA (FT) TORQUE MAX. CONT. TORQUE (10 SEC. TRANSIENT) 0-4000 106% 127% 4000-5000 103% 127% 5000-6000 100% 127% 6000-8000 94% 127% 8000-10,000 88% 127% Single Engine Continuous 0-120% 10 min. max. 121-135% 10 sec. max. 136-144% 5 H4NE TRANSMISSION LIMITS: TORQUE / % 10 Minute 135 OEI 106 Dual Continuous 120 OEI 106 Dual ROTOR LIMITS: Power On: Max. 120% (100% = 258 RPM) Min. 91% Power Off: Max. 120% Min. 90% AIRSPEED LIMITS: Maximum (red line) airspeed 180 KIAS C.G. RANGE: 353.0 361.0 21,884 19,462 20,800 12,000 346.8 364.0 DATUM: 341.2 inches forward of main rotor centroid. LEVELING MEANS: Leveling plate on cabin floor, right side, BL 14.90 and plumb line from upper frame at station 346.65. MAXIMUM WEIGHT: 21,884 lbs. MINIMUM CREW: 2 (pilot, copilot) NUMBER OF SEATS: 1 at Sta. 311; 1 at Sta. 329; 1 at Sta. 366. FUEL CAPACITY: With General Electric T700-GE-401 engines: 695 gallons; 2 tanks (LH & RH interchangeable), 590 gallons and 1 auxiliary tank LBL 41, sta. 295, 105 gallons. With General Electric CT7-2D1 and T700-GE-401 engines: 695 gallons; 2 tanks (LH & RH interchangeable) 590 gallons and 1 auxiliary tank LBL 41, sta. 295, 105 gallons. OIL CAPACITY: 7.3 quarts each engine. OTHER OPERATING With General Electric CT7-2D1 engines: Sikorsky Publication Flight Manual LIMITATIONS: S70C(M) SA4047-H60FB-NFM-000(1). H4NE 6 With General Electric T700-GE-401engines: Sikorsky Publication Flight Manual S70C(M) SA4047-H60FB-NFM-000. With General Electric T700-GE-401C engines: Sikorsky Publication Flight Manual S70C(M) SA4047-H60CA-NFM-000. SERIAL NUMBERS Serial number will be assigned in conjunction with individual FAA airworthiness ELIGIBLE: certificate for the aircraft. TYPE CERTIFICATION FAR 21.25(a)(2), effective January 6, 1975. BASIS: Type Certification No. H4NE issued April 25, 1986, revised February 21, 1990, (See Note 5) for the purpose of: (1) Agricultural (2) External Cargo (3) Firefighting PRODUCTION BASIS: Production Certificate No. 105 EQUIPMENT: The following must be installed in each type helicopter for certification: With General Electric CT7-2D1 Engines: (1) Sikorsky Publication Flight Manual S70C(M) SA4047-H60FB-NFM-000(1). (2) Removal of military equipment and replacement with commercial equipment (if required) in accordance with the latest FAA approved revision of Sikorsky Aircraft Kit Drawing No. 70080-00112-012. With General Electric T700-GE-401 Engines: (1) Sikorsky Publication Flight Manual S70C(M) SA4047-H60FB-NFM-000. (2) Removal of military equipment and replacement with commercial equipment (if required) in accordance with the latest FAA approved revision of Sikorsky Aircraft Kit Drawing No. 70080-00112-011. With General Electric T700-GE-401C Engines: (1) Sikorsky Publication Flight Manual S70C(M) SA4047-H60CA-NFM-000. (2) Removal of military equipment and replacement with commercial equipment (if required) in accordance with the latest FAA approved revision of Sikorsky Aircraft Kit Drawing No. 70080-00112-013. NOTES NOTE 1: Current weight and balance report including list of equipment included in certificated empty weight, and loading instructions must be in each type helicopter at time of original airworthiness certification and at all times thereafter. NOTE 2: The following placard must be prominently displayed in the cockpit in full view of the pilots: "THIS ROTORCRAFT MUST BE OPERATED IN ACCORDANCE WITH THE RESTRICTED CATEGORY OPERATING LIMITATIONS OF FAR 91.39." 7 H4NE NOTE 3: Model S-70C(M1) originally approved as Model S-70C(M) on April 25, 1986, and is the civil equivalent of U.S. Navy Model SH-60B. Revision 1 to TCDS H4NE, February 21, 1990 established Model S -70C(M) as the civil equivalent of U.S. Navy Model SH -60F, and established Model S-70C(M1) as the civil equivalent of U.S. Navy Model SH-60B. NOTE 4: For Model S-70C(M1): Prior to the Civil Airworthiness Certification, compliance with the following must be accomplished: (a) Comply with U.S. Navy Airframe Bulletin No. AFB 017, Main Transmission Support Beam Inspection. (b) Comply with U.S. Navy Message No. 291913Z (January 86) Special Spindle Inspection. (c) Comply with U.S. Navy Message No. 291623Z (January 86) Main Rotor Damper/Maintenance procedure. (d) Comply with U.S. Navy Avionics Bulletin No. 399, Inspection of Stabilator Amplifier. (e) Comply with U.S. Navy Interim Airframe Change No. 004, Airframe and Landing Gear System, Tail Landing Gear Assembly. (f) Comply with U.S. Navy Interim Airframe Change No. 014, Installation of Cargo Hook Keeper and External Spring. Copies of the U.S. Navy Messages, Bulletins and Interim Changes may be obtained from Sikorsky Aircraft, Division of United Technologies, Attention Civil Aviation Requirements Office, North Main Street, Stratford Connecticut 06601. Information essential to the proper maintenance of the Model S-70C(M1) is contained in Sikorsky Publications: SA4047-S70CM1-110-300 SA4047-S70CM1-140-300 SA4047-S70CM1-150-300 SA4047-S70CM1-220-300 SA4047-S70CM1-240-300 SA4047-S70CM1-260-300 SA4047-S70CM1-410-300 SA4047-S70CM1-420-300 SA4047-S70CM1-450-300 SA4047-S70CM1-460-300 SA4047-S70CM1-490-300 SA4047-S70CM1-510-300 SA4047-S70CM1-560-300 SA4047-S70CM1-690-300 SA4047-S70CM1-710-300 SA4047-S70CM1-720-300 SA4047-S70CM1-740-300 SA4047-S70CM1-750-300 SA4047-S70CM1-GAI-000 SA4047-S70CM1-GAI-010 SA4047-S70CM1-MRC-100 SA4047-S70CM1-MRC-200 SA4047-S70CM1-MRC-000 SA4047-S70CM1-MRC-300 SA4047-S70CM1-SRM-000 SA4047-S70CM1-WDM-000 Information essential to the proper maintenance of the General Electric CT7-2D engines is contained in General Electric Publications SEI 569, 570 and 690. “Lines deleted here” H4NE 8 NOTE 5: For model S-70C(M) with General Electric CT7-2D1 engines installed: Information essential to the proper maintenance is contained in Sikorsky Publications: SA4047-S70CM-110-300 SA4047-S70CM-140-300 SA4047-S70CM-150-300 SA4047-S70CM-220-300 SA4047-S70CM-240-300 SA4047-S70CM-260-300 SA4047-S70CM-410-300 SA4047-S70CM-420-300 SA4047-S70CM-450-300 SA4047-S70CM-460-300 SA4047-S70CM-490-300 SA4047-S70CM-510-300 SA4047-S70CM-560-300 SA4047-S70CM-690-300 SA4047-S70CM-710-300 SA4047-S70CM-720-300 SA4047-S70CM-740-300 SA4047-S70CM-750-300 SA4047-S70CM-GAI-000 SA4047-S70CM-GAI-010 SA4047-S70CM-MRC-100 SA4047-S70CM-MRC-350 SA4047-S70CM-MRC-400 SA4047-S70CM-MRC-300 SA4047-S70CM-SRM-000 SA4047-S70CM-SRM-300 SA4047-S70CM-WDM-000 SA4047-S70CM-MRC-000 Information essential to the proper maintenance of the General Electric CT7-2D1 engines is contained in General Electric Publications SEI 569, 570 and 690. “Lines deleted here” NOTE 6: For model S-70C(M) with General Electric T700-GE-401C engines installed Information essential to the proper maintenance is contained in Sikorsky Publications: SA4047-S70CM-110-300 SA4047-S70CM-140-300 SA4047-S70CM-140-300 SA4047-S70CM-220-300 SA4047-S70CM-240-300 SA4047-S70CM-260-300 SA4047-S70CM-410-300 SA4047-S70CM-420-300 SA4047-S70CM-450-300 SA4047-S70CM-460-300 SA4047-S70CM-490-300 SA4047-S70CM-510-300 SA4047-S70CM-560-300 SA4047-S70CM-690-300 SA4047-S70CM-710-300 SA4047-S70CM-720-300 SA4047-S70CM-740-300 SA4047-S70CM-750-300 SA4047-S70CM-GAI-000 SA4047-S70CM-GAI-010 SA4047-S70CM-MRC-100 SA4047-S70CM-MRC-000 Information essential to the proper maintenance of the General Electric T700-GE-401C engine is contacted in General Electric publication SEI-698. ...END... ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [Sikorsky S-70C(M)-1](https://openairdocs.org/model/sikorsky-s-70c-m-1): 0 aircraft (registry code 8143016) ## STCs approved under this data sheet (4) - [STC SR12058AK](https://openairdocs.org/stc/SR12058AK): Installation of Recoil Aerospace, Inc. T750-I Internal Fire Suppression Tank. Recoil Aerospace Inc. - [STC SR02584AK](https://openairdocs.org/stc/SR02584AK): Installation of Recoil Aerospace, Inc. T1000-E or T650-E Fire Suppression Tank. Recoil Aerospace Inc. - [STC SR02617SE](https://openairdocs.org/stc/SR02617SE): Installation of a Mechanical Specialties Model 909 Cargo Hook. Mechanical Specialties Inc - [STC SR04422CH](https://openairdocs.org/stc/SR04422CH): Installation of NASI NTEC36TM Cooling System in accordance with Master Data List (MDL) as listed on AML No. SR04422CH, or later FAA approved revision.. National Aircraft Service Inc --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.