TCDS H5NE

U.S. DEPARTMENT OF TRANSPORTATION TCDS NUMBER H5NE REVISION 20 DATE: October 16, 2023 SIKORSKY AIRCRAFT MODEL: S-70A, S-70M FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET H5NE This data sheet, which is part of Type Certificate Number H5NE, prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Si korsky Aircraft Corporation 6900 Main Street Stratford, CT 06615-9129 MODEL NUMBER: S-70A (Restrict ed Category) Approved: 10/22/88 (Derivative aircraft of U.S. Army Models UH-60A and UH-60L) ENGINES: 2 General Electric T700-GE-701A (See Notes 5, 13 and 14 for optional engines.) FUEL: JP-4, JP-5, JP-8, Je t A, Jet A1, or Jet B ENGINE LIMITS: SHAFT HP (S.L. STD) POWER TURBINE RPM/% GAS GEN RPM/% TURBINE GAS TEMP.oC Contingency Rated Power (CRP) (2 1/2 min. OEI) Maximum Rating (10 min. dual) Intermediate Rated Power (IRP) (30 min. dual) Maximum Continuous Power (MCP) 1,723 20,900/100 44,700/102 917 1,715 20,900/100 44,700/102 882 1,694 20,900/100 44,700/102 867 1,510 20,900/100 44,700/102 804 TRANSMISSION LIMITS: TORQUE 120% Single Engine 106% Dual Engine (no time limits) ROTOR LIMITS: POWER OFF: Maximum 110% Minimum 90% POWER ON: Maximum 107% Minimum 91% AIRSPEED LIMITS: Vne Power on: 193 knots IAS, (221 MPH). See appropriate Rotorcraft Flight Manual (Operators Manual) for variation of Vne with gross weight, pressure altitude and temperature. PAGE 1 2 3 4 5 6 7 8. 9 10 11 12 13 REV. 20 15 13 13 20 16 13 13 13 13 13 13 17 H5NE 2 of 13 INCHES AFT OF DATUM DATUM: 341.2 inches forward of the main rotor centroid. MAXIMUM WEIGHT: 22,000 lbs. MINIMUM CREW: 2 (pilot, copilot) NUMBER OF SEATS: a. 2 at Sta. 227.1; 2 at Sta. 264.6; 1 at Sta. 280.4; 2 at Sta. 282.5; 2 at Sta. (No Passengers Permitted) 300.5; 1 at Sta. 301.4; 4 at Sta. 334.3; 4 at Sta. 355.3; 4 at Sta. 387.2. b. OPTIONAL SEATING: 2 at Sta. 227.1; 1 at Sta. 262.0; 3 at Sta. 282.0; 3 at Sta. 320.7; 4 at Sta. 339.8; 4 at Sta.387.2 FUEL CAPACITY: 361.5 gallons; 2 tanks (LH & RH interchangeable). An additional 460 gallons (2x230 gallons) or 920 gallons (4x230 gallons) with external fuel tanks installed. OIL CAPACITY: 7 quarts each engine. OTHER OPERATING LIMITATIONS: TM 55-1520-237-10T S-70A Operator's Manual dated October 20, 1988, as revised. For aircraft Serial Numbers 701825, 701835 and 702127, TM 55-1520- 237-10HK Operator's Manual, dated October 29, 1992, as revised, is applicable. For aircraft Serial Numbers 701129 and 702029, TM55-1520-237-10B Operator’s Manual, dated June 22, 1992, as revised, is applicable. For aircraft Serial Numbers 700029, 702129 and 702929, TM 1-70-29-10 Operator’s Manual, dated October 6, 1997, as revised, is applicable. SERIAL NUMBERS 700029, 701129, 701322, 701325, 701327, 701329, 701331, 701333, 701592, ELIGIBLE: 701593, 70159 4, 701595, 701613, 701614, 701825, 701835, 702029, 702127, 702129, 702929. C.G. RANGE 347.7 360.2 22,000 A I R C R A F T W E I G H T L B S 15,900 345 .5 13,700 13,400 13,050 366 .3 11,500 342.6 358.1 H5NE 3 of 13 TYPE CERTIFICATION BASIS: FAR 21.25(a)(2), effective January 6, 1975, for the purpose of: (1) Agriculture, FAR 21.25(b)(1) (2) External Cargo, FAR 21.25(b)(7) (3) Forest and Wildlife Conservation FAR 21.25(b)(2) FAR 29, Amendments 29-1 through 29-17 for non-U.S. Army approved modifications. See Note 15 for Noise Requirements. PRODUCTION BASIS: Production Ce rtificate No. 105 and 8S0. EQUIPMENT: The following must be installed in each type helicopter for certification: (1) Sikorsky Rotorcraft Flight Manual (Oper ator's Manual) Publication TM 551520-237- 10T. (See Note 5.) For aircraft Serial Numbers 701825 and 701835, TM 55-1520-237- 10HK, dated October 29, 1992, as revised, is applicable. For aircraft Serial Number 701129, TM55-1520-237-10B, dated June 22, 1992, as revised, is applicable. (2) Removal and replacement of equipment in accordance with Sikorsky Aircraft Kit Drawing No. 70010-00003 (Dash number as applicable). (See Notes 5, 6, 7, 13 and 14) (3) Aircraft must be modified with Stabilato r Amplifier P/N 70902-02001-048; Pitot Static Probe Support, Assembly P/N 70219-02141-041 (left side), -042 (right side); and Pitot Static Probe Fairing, Assembly P/N 70219-02141-043 (left side), -44 (right side). II. MODEL NUMBER: S-70M (Restricted Cate gory) Approved: February 11, 2019 (Derivative aircraft of U.S. Army Model UH-60M) ENGINES: 2 General Electric T700-GE-701D FUEL: JP-4, JP-5, JP-8, Je t A, Jet A1, or Jet B ENGINE LIMITS: SHAFT HP (S.L. STD) POWER TURBINE GAS GEN RPM/% TURBINE GAS TEMP.oC RPM/% Contingency Rated Power (CRP) (2 1/2 min. OEI) Maximum Rating (10 min. dual) Intermediate Rated Power (IRP) (30 min. dual) Maximum Continuous Power (MCP) 2,000 20,900/100 46,935/105 903 1,994 20,900/100 46,935/105 879 1,902 20,900/100 46,935/105 846 1,716 20,900/100 46,935/105 793 TRANSMISSION LIMITS: TORQUE 135% Single Engine 120% Dual Engine ( < 80 KIAS) 100% Dual Engine ( > 80 KIAS) (no time limits) H5NE 4 of 13 ROTOR LIMITS: POWER OFF: Maximum 110% Minimum 90% POWER ON: Maximum 107% Minimum 91% AIRSPEED LIMITS: Vne Power on: 193 knots IAS, (221 MPH). See appropriate Rotorcraft Flight Manual (Operators Manual) for variation of Vne with gross weight, pressure altitude and temperature. S-70M Longitudinal Center of Gravity Envelope 25000 • 348.2 359.2 23500 - 23000 - 347.7 - Note 1 -360.2 22000 21000 WEIGHT - POUNDS 19000 17000 006ST 15000 342.6 345.5 13700 13400 13000 12000 12500=7 1305 366.3 11500 363.2 11000 348 _ 358.1, 360,8, 336 340 344 ZSE 356 360 364 368 Note 1 - Excursion into this region is permissible when performing external lift missions with a cargo hook load above 8000 pounds and up to 9000 pounds. EMPTY WEIGHT None. C.G. RANGE: DATUM: 341 inches forward of the main rotor centroid. LEVELING MEANS: Leveling plate at STA 309.62, BL 35 LH, and plumb line from top of LH forward cabin doorframe. MAXIMUM WEIGHT: INTERNAL: 22,000 Ibs. EXTERNAL: 23,500 Ibs. MINIMUM CREW: 2 (Pilot, Co-Pilot) H5NE 5 of 13 NUMBER OF SEATS: (No Passengers Permitted) a. 2 at St a. 227; 2 at Sta. 284; 3 at Sta. 321; 4 at Sta. 340; 4 at Sta. 387 b. OPTIONAL SEATING: 2 at Sta. 282; 1 at Sta. 282 MAXIMUM FLOOR LOADING: 300 lb./sq. ft. STORAGE COMPARTMENT 125 lb. MAXIMUM CAPACITY: FUEL CAPACITY: 360 gallons; 2 tanks. OIL CAPACITY: 7 quarts each engine. OTHER OPERATING LIMITATIONS: TM 1-S70M-280-10 S-70M Operator's Manual dated August 25, 2020, as revised. SERIAL NUMBERS 704091 ELIGIBLE: For modifications, the baseline certification basis (as defined in Policy Memo AIR-600- DM02), is 14 CFR 29 dated February 1, 1965, including Amendments 29-1 through 29- 17 (through 29-47 for main rotor blade and avionics systems modifications). See Note 20. In accordance with 14CFR Part 36.1(a)(4), compliance with the noise requirements was not shown. Therefore, aircraft certificated under this Type Certificate are only eligible for agricultural operations defined in 14CFR 137.3, aerial dispensing of liquids and forest conservation materi al as defined by 14CFR 137.3, or external loads as defined in 14CFR 133.1(b). Helicopter fuel system safety per FAA Reauthorization Act of 2018 Section 317, enacted October 05, 2018. Compliance has been established with 49 U.S.C. §44737 (2018) [29.952(a)(1), (2), (3), (5), (6), 29.952(c)(1)(ii), (iii), (iv), (v), (c)(2)(excluding fatigue), (f), (g), and 29.963(b) as amended by Amendment 29-35 and 29.975(a)(7) as amended by Amendment 29-42. Equivalent Level of Safety AT02311BO-R / P-1 for 29.952(c)(1)(i) and the fatigue requirements of 29.952(c)(2) as amended by Amendment 29-35]. PRODUCTION BASIS: Sikorsky Aircraft Corporation Production Certificate Number 105 EQUIPMENT: The following must be installed in each type helicopter for certification: (1) Sikorsky Rotorcraft Flight Manual (Operat or's Manual) Publication TM 1-S70M-280- 10 (see Note 16), as revised. (2) Removal and replacement of equipment in accordance with Sikorsky Aircraft Kit Drawing No. 70000-00120-046. TYPE CERTIFICATION BASIS: FAR 21.25(a)(2), effective January 6, 1975, for the purpose of: (1) Agriculture, FAR 21.25(b)(1) (2) External Cargo, FAR 21.25(b)(7) (3) Forest and Wildlife Conservation FAR 21.25(b)(2) H5NE 6 of 13 NOTES NOTE 1: Current weight and balance report, including li st of equipment 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." FAR 91.39 became FAR 91.313 in the recodification dated August 18, 1989. NOTE 3: For Model S-70A: Prior to Civil Airworthines s Certification, compliance with Sikorsky Aircraft document number IILS-L-88-006, dated October 5, 1988, as revised, must be accomplished. For Model S-70M: Prior to Civil Airworthiness Certification, compliance with Sikorsky Aircraft document number ASB/MAM-Armyint-PUB-001, dated August 18, 2017, as revised, must be accomplished. NOTE 4: For Model S-70A: Information essential to proper maintenance of the aircraft is contained in the following U.S. Army publications, as revised: TM 11-1520-237-1, -2, and -3, dated June 10, 1989; TM 55-1520-237- 23, Volumes 1 thru 8, dated August 29, 1989; TM 55-1520-237T, dated August 29, 1989; TM 55-1520-237- PMS-1, dated June 30, 1990; TM 55-1520-237-PMS-2, dated August 30, 1990; TM 55-1520-237-CL, dated June 10, 1989; TM 55-1520-237-MTF, dated November 13, 1990, and Sikorsky Supplement C-7 to these publications. Information essential to the proper maintenance of the T700-GE-701A engines is contained in General Electric Publications SEI 671 and 673, as revised and U.S. Army TM 1-2840-24823&P, as revised. Component overhaul and replacement times shall be in accordance with U.S. Army TM 55-1520-237-23, Volume 1, Chapter 1, Table I-II, dated August 29, 1989, as revised, and Sikorsky Supplement C-7, unless superseded by appropriate airworthiness directive. (See NOTE 10).Alternate information essential to the proper maintenance of the aircraft is contained in the following U.S. Army publications, as revised: TM 11- 1520-237-23-1, -2, and -3, dated April 30, 1979; TM 55-1520-23723-1, dated December 8, 1987; TM 55- 1520-237-2, through -10, dated December 29, 1978; TM 55-1520-237-PMS-1, dated July 14, 1988; TM 55- 1520-237-PMS-2, dated April 12, 1988; TM 55-1520-237-CL, dated August 15, 1987; TM 55-1520-237-MTF, dated January 8, 1988, and Sikorsky Supplement No. C-1 to these publications. Information essential to the proper maintenance of the T700-GE-701A engines is contained in General Electric Publications SEI 671 and 673, as revised, and U.S. Army TM 1-2840-24823&P, as revised. Component and overhaul and replacement times shall be in accordance with U.S. Army TM 55-1520-237-23-2, dated December 29, 1978; and Sikorsky Supplement C-1 to this publication, unless superseded by appropriate Airworthiness Directive. (See NOTE 10) The U.S. Army replaced TM 55-1520-237-23-1 through -10 with a single manual, TM 55-1520-237-23, composed of 18 chapters and 8 appendices divided into 8 volumes. Either set of TM's may be used. (See NOTE 10) Information on civil aircraft serial number correlation to U.S. Army serial numbers is contained in Sikorsky Letter TPL-W91-450, dated July 23, 1991, as revised or Sikorsky Engineering Report SER- 51010189 dated 7 June 2016, as revised. For Model S-70M: Information essential to proper maintenance of the aircraft is contained in the following publications, as revised: TM 1-S70M-280-23, volume 1 thru 11, dated July 1, 2021; TM 11- S70M-280-23, dated September 1, 2021; TM 1-S70M-280-PMD (Work Packages 0001 through 0007) dated July 1, 2021; TM 1-S70M-280-PMI (Work Packages 0001 through 0015) dated July 1, 2021; TM 1-S70M-280-PMS (Work Packages 0001 through 0008), dated July 1, 2021; TM 1-S70M- 280-23P dated September 1, 2021; TM 11-S70M-280-23P dated 1 September 2021. Information essential to the proper maintenance of the T700-GE-701D engines is contained in General Electric Publication SEI 671, as revised. Component overhaul and replacement times shall be in accordance with TM 1-S70M-280-AWL dated July 20, 2021. (See NOTE 16). NOTE 5: For Model S-70A: For aircraft equipped with optional engines: (UH-60L derivative) ENGINES: 2 General Electric T700-GE-701C FUEL: Aviation Kerosene JP-4, JP-5 , JP-8, Jet A, Jet A1, or Jet B H5NE 7 of 13 ENGINE LIMITS SHAFT HP POWER TURBINE GAS. GEN. TURBIN E GAS Contingency Rated 1,940 20,900/100 44,70 903 Power (CRP) 2 1/2 min. OEI) Maximum Rating 1,890 20,900/100 44,70 878 (10 min. dual Intermediate Rated 1,800 20,900/100 44,70 851 Power (IRP) (30 min. dual) Maximum Continuous 1,662 20,900/100 44,70 810 Power (MCP) TRANSMISSION LIMITS: TORQUE 135% Single Engine (No time limits) 120% Dual Engine (No time limits) Other Operating Limitations: U.S. Army TM 55-1520-237-10, UH-60A and EH-60A Operator's Manual, dated January 8, 1988, as revised, or U.S. Army TMI-1520-237-10, UH-60A, UH-60L, EH-60A Operator's Manual, dated August 31, 1994, as revised, and Sikorsky Supplements C-4 and C-5, dated October 26, 1990, as revised. For aircraft Serial Numbers 701825 and 701835, TM 55-1520-237-10HK, dated October 29, 1992, as revised, is applicable. Equipment: Each type certificated helicopter with T700-GE-701C engines installed must be equipped with U.S. Army TM 55-1520-237-10, UH-60A and EH-60A Operator's Manual, dated January 8, 1988 as revised, or U.S. Army TM-1-1520-237-10, UH-60A, UH-60L, EH-60A Operator's Manual, dated August 31,1994, as revised, and Sikorsky supplements No. C-4 and C-5, dated October 26, 1990, as revised. For aircraft serial numbers 701825 and 701835, TM 55-1520-237-10HK Operator's Manual dated October 29, 1992, as revised, is applicable. Removal and replacement of equipment is in accordance with Sikorsky Aircraft Kit Drawing No. 70010- 00003 (Dash number as applicable). Information essential to the proper maintenance of the aircraft is contained in the following U.S. Army publications, as revised: TM 11-1520-237-23-1, -2, and -3, dated June 10, 1989; TM 55-1520-237-23, Volumes 1 through 8, dated August 29, 1989; TM 55-1520-237T, dated August 29, 1989; TM 55-1520-237- PMS-1, dated June 30, 1990; TM 55-1520-237-PMS-2, dated August 30, 1990; TM 55-1520-237-CL, dated June 10, 1989; TM 55-1520-237-MTF, dated November 13, 1990; and Sikorsky supplement C-7 to these publications. Information essential to the proper maintenance of the T700-GE-701C engines is contained in U.S. Army TM 55-2840-248-23, dated December 31, 1981, as revised and General Electric Publication SEI- 671, as revised. Component overhaul and replacement times shall be in accordance with U.S. Army TM 55- 1520-237-23, Volume 1, Chapter 1, Table I-II, dated August 29, 1989, as revised, and Sikorsky supplement C-7 to this publication, unless superseded by appropriate airworthiness directive. (See NOTE 10) Alternate information essential to the proper maintenance of the aircraft is contained in the following U.S. Army publications, as revised: TM 11-1520-237-23-1, -2, and -3, dated April 30, 1979; TM 55-1520-23723-1, dated December 8, 1987; TM 55-1520-237-23-2 through -10, dated December 29, 1978; TM 55-1520-237- PMS-1, dated July 14, 1988; TM 55-1520-237-PMS-2, dated April 12, 1988; TM 55-1520-237-CL, dated August 15, 1987; TM 55-1520-237-MTF, dated January 8, 1988; and Sikorsky Supplement C-1 to these publications. Information essential to the proper maintenance of the T700-GE-701C engines is contained in U.S. Army TM 55-2840-248-23, dated December 31, 1981; as revised and General Electric Publication SEI- 671, as revised. Component overhaul and replacement times shall be in accordance with U.S. Army TM 55- 1520-237-23-2, dated December 29, 1978; and Sikorsky Supplement C-1 to this publication, unless superseded by appropriate Airworthiness Directive. (See NOTE 10) H5NE 8 of 13 The U.S. Army replaced TM 55-1520-237-23-1 through -10 with a single manual, TM 55-1520-237-23, composed of 18 chapters and 8 appendices divided into 8 volumes. Either set of TM's may be used. (See NOTE 10) Information on civil aircraft serial number correlation to U.S. Army serial numbers is contained in Sikorsky Letter TPL-W91-450, dated July 23, 1991, as revised, or Engineering Report SER-51010189 dated 7 June 2016, as revised. NOTE 6: For Model S-70A: For aircraft configured in accordance with Sikorsky Aircraft Kit Drawing No. 70010-00003-013. SERIAL NUMBERS ELIGIBLE: 701613 and 701614. Note 5 applies, except the only applicable TM 55-1520-237-10 Operator's Manual Sikorsky Supplement is C-7, dated May 24, 1991, as revised. Removal and replacement of equipment is in accordance with Sikorsky Aircraft Kit Drawing No. 70010-00003-013. NUMBER OF SEATS: 2 at Sta. 227.1; 2 at Sta. 283.5; 2 at Sta. 329.5; 4 at Sta. 384.3 Compliance with FAR 29.853 has been demonstrated. NOTE 7: For Model S-70A: For aircraft configured in accordance with Sikorsky Aircraft Kit Drawing No. 70010-00003-015. SERIAL NUMBER ELIGIBLE: 701129 For aircraft configured in accordance with Sikorsky Aircraft Kit Drawing No. 70080-95011-011. SERIAL NUMBER ELIGIBLE: 702029 Information essential to the proper maintenance of the aircraft is contained in the following publications: TM1-1520-237-10B Operators Manual TM1-1520-237-CLB Operators and Crewmembers Checklist TM1-1520-237-MTFB Maintenance Test Flight Manual TM1-70-29-23 Aircraft Maintenance Procedures Manual TM1-70-29-PMS-1 10 Hour/14Day (30 hour/42 day) Inspection Checklist TM1-70-29-PMS-2 Periodic Inspection Checklist TM1-70-29-23P Airframe Repair Parts and Special Tools List TM11-70-29-23 Avionics Maintenance Procedures Manual TM11-70-29-23P Avionics Configuration Repair Parts and Special Tools List NUMBER OF SEATS: 2 at Sta. 227.1; 2 at Sta. 283.5; 2 at Sta. 329.5; 3 at Sta. 384.3. Compliance with FAR 29.853 (a) only has been demonstrated. NOTE 8: For Model S-70A: For aircraft configured in accordance with Sikorsky Aircraft Kit Drawing Nos. 33770-51668, 70080-60031, 33770-81008. SERIAL NUMBER ELIGIBLE: 700029 For aircraft configured in accordance with Sikorsky Aircraft Kit Drawing Nos. 33770-51664, 33880-60013, 33770-81008. SERIAL NUMBER ELIGIBLE: 702129 For aircraft configured in accordance with Sikorsky Aircraft Kit Drawing Nos. 33770-51666, 70080-60031, 33770-81008. SERIAL NUMBER ELIGIBLE: 702929 Information essential to the proper maintenance of these aircraft is contained in the following publications: TM 1-70-29-10 Operator’s Manual TM 1-70-29-CL Operator’s and Crewmember’s Checklist TM 1-70-29-MTF Maintenance Test Flight Manual TM 1-70-29-23 Aircraft Maintenance Procedures Manual TM 1-70-29-PMS-1 10 hour/14 day(30 hour/42 day) Inspection Checklist H5NE 9 of 13 TM 1-70-29-PMS-2 Periodic Inspection Checklist TM 1-70-29-23P Airframe Repair Parts and Special Tools List TM 11-70-29-23 Avionics Maintenance Procedures Manual TM 11-70-29-23P Avionics Configuration Repair Parts and Special Tools List Number of seats: 2 at Sta. 227.1; 2 at Sta. 283.5; 2 at Sta. 329.5; 3 at Sta. 384.3 Compliance with FAR 29.853(a) only has been demonstrated. NOTE 9: For Model S-70A: S-70A derivatives of UH-60L ai rcraft may be operated at gross weights up to 23,500 pounds during external load operations, and hook loads up to 9,000 pounds in accordance with U.S. Army Aviation Safety Message 051326Z Jul 94, or appropriately revised FAA approved Operator's Manual. U.S. Army Safety Message 051325Z Jul 94, Serial Number 91-26354 is Sikorsky Serial Number 701656 and Serial Number 91- 26421 is Sikorsky Serial Number 701771. NOTE 10: For Model S-70A: The following table lists equivale nt sets of technical data approved for proper maintenance of the aircraft. U.S. Army Manuals Old New S-70A Commercial Manuals TM 55-1520-237-10 TM 1-1520-237-10 FAA Approved RFM TM55-1520-237-MTF TM 1-1520-237-MTF Not Applicable TM 55-1520-237-CL TM 1-1520-237-CL Not Applicable TM 55-1520-237-PMS-1 TM 1-1520-237-PMS-1 TM 1-70-PMS-1 TM 55-1520-237-PMS-2 TM 1-1520-237-PMS-2 TM 1-70-PMS-2 TM 55-1520-237-23 TM 1-1520-237-23 TM 1-70-23 and TM 1-70-23AW-2 TM 55-1520-237-T TM 1-1520-237-T TM 1-70-T TM 55-1520-237-23P TM 1-1520-237-23P TM 1-70-23P TM 11-1520-237-23 TM 11-1520-237-23 TM 11-70-23 TM 11-1520-237-23P TM 11-1520-237-23P TM 11-70-23P TM 11-1520-237-23P TM 11-1520-237-23P Not Applicable The initial publication date of the U.S. Army TM 1 series was 31 August 1994. The initial publication date of the Sikorsky TM-1 series was 31 August 1994. NOTE 11: Deleted by previous revision. NOTE 12: Deleted by revision 12. NOTE 13: For Model S-70A: For aircraft equipped with optional engines: (UH-60L derivative only) ENGINES: 2 General Electric T700-GE-701D/CC FUEL: Aviation Kerosene JP-4, JP-5 , JP-8, Jet A, Jet A1, or Jet B ENGINE LIMITS SHAFT HP (S.L. STD.) POWER TURBINE RPM/% GAS. GEN. RPM/% TURBINE GAS TEMP. oC Contingency Rated 1,940 20,900/100 44,700 /102 903 Power (CRP) 2 1/2 min. OEI) Maximum Rating 1,890 20,900/100 44,700/102 878 H5NE 10 of 13 (10 min. dual) Intermediate Rated 1,800 20,900/100 44,700/102 851 Power (IRP) (30 min. dual) Maximum Continuous 1,662 20,900/100 44,700/102 810 Power (MCP TRANSMISSION LIMITS: TORQUE 135% Single Engine (No time limits) 120% Dual Engine (No time limits) EQUIPMENT: Removal and repl acement of equipment in accordance with Sikorsky Aircraft Top Kit Drawing 70070-30258 (dash number as applicable). Other Operating Limitations: U.S. Army TMI-1520-237-10, UH-60A, UH-60L, EH-60A Operator's Manual, dated August 31, 1994, as revised, and Sikorsky Supplements C-4 and C-5, dated October 26, 1990, as revised. For aircraft Serial Numbers 701825 and 701835, TM 55-1520-237-10HK, dated October 29, 1992, as revised, is applicable. Equipment: Each type certificated helicopter with T700-GE-701D/CC engines installed must be equipped with U.S. Army TM-1-1520-237-10, UH-60A, UH-60L, EH-60A Operator's Manual, dated August 31,1994, as revised, and Sikorsky supplements No. C-4 and C-5, dated October 26, 1990, as revised. For aircraft serial numbers 701825 and 701835, TM 55-1520-237-10HK Operator's Manual dated October 29, 1992, as revised, is applicable. Removal and replacement of equipment is in accordance with Sikorsky Aircraft Kit Drawing No. 70010- 00003 (Dash number as applicable). Information essential to the proper maintenance of the aircraft is contained in the following U.S. Army publications, as revised: TM 11-1520-237-23-1, -2, and -3, dated June 10, 1989; TM 55-1520-237-23, Volumes 1 through 8, dated August 29, 1989; TM 55-1520-237T, dated August 29, 1989; TM 55-1520-237- PMS-1, dated June 30, 1990; TM 55-1520-237-PMS-2, dated August 30, 1990; TM 55-1520-237-CL, dated June 10, 1989; TM 55-1520-237-MTF, dated November 13, 1990; and Sikorsky supplement C-7 to these publications. Information essential to the proper maintenance of the T700-GE-701D/CC engines is contained in U.S. Army TM 55-2840-248-23, dated December 31, 1981, as revised and General Electric Publication SEI-671, as revised. Component overhaul and replacement times shall be in accordance with U.S. Army TM 55-1520-237-23, Volume 1, Chapter 1, Table I-II, dated August 29, 1989, as revised, and Sikorsky supplement C-7 to this publication, unless superseded by appropriate airworthiness directive. (See NOTE 10) Alternate information essential to the proper maintenance of the aircraft is contained in the following U.S. Army publications, as revised: TM 11-1520-237-23-1, -2, and -3, dated April 30, 1979; TM 55-1520-23723-1, dated December 8, 1987; TM 55-1520-237-23-2 through -10, dated December 29, 1978; TM 55-1520-237-PMS-1, dated July 14, 1988; TM 55-1520-237-PMS-2, dated April 12, 1988; TM 55-1520-237-CL, dated August 15, 1987; TM 55-1520-237-MTF, dated January 8, 1988; and Sikorsky Supplement C-1 to these publications. Information essential to the proper maintenance of the T700-GE-701D/CC engines is contained in U.S. Army TM 55-2840-248-23, dated December 31, 1981; as revised and General Electric Publication SEI-671, as