# TCDS R00113SE: H-60 LLC - Type: Type certificate data sheet - Status: Current - Holder: H-60 LLC - Revision: 1 - Revised: May 4, 2026 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Registered aircraft: 1, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/39/af/39af9f7da1c538ade5cc40d8776e9d3c2ad4414423f89796342ea0c085898262 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185047887520260522151534.0001 - Page: https://openairdocs.org/tcds/R00113SE ## Models (5) As the data sheet lists them. - UH-60A - UH-60L - T700-GE-700 - T700-GE-701C - T700-GE-701D/CC ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. R00113SE This data sheet, which is a part of Type Certificate No. R00113SE prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of Title 14 of the Code of Federal Regulations (14 CFR). TYPE CERTIFICATE (TC) H-60, LLC HOLDER: 265 Durley Avenue Camarillo, CA 93010 I - MODEL: UH-60A (Restricted Category Military Surplus Rotorcraft) Approved 1/27/2025. ENGINES: (2) General Electric T700-GE-700 Original (2) General Electric T700-GE-701C (Alternate) (2) General Electric T700-GE-701D/CC (Alternate) FUEL: Aviation Kerosene JP-4, JP-5, JP-8, Jet A, Jet A-1 or Jet B. *See NOTE 8 for alternate and emergency fuels. ENGINE LIMITS: (T700-GE-700) SHAFT HP POWER TURBINE RPM GAS GEN RPM POWER TURBINE INLET (TGT) Military Power (30 min.) 1,561 20,900 44,700 850º C Normal Cont. Cruise 1,318 20,900 44,700 775º C ENGINE LIMITS: (T700-GE-701C) SHAFT HP POWER TURBINE RPM/% GAS GEN RPM/% POWER TURBINE INLET (TGT) Contingency Rated Power (CRP) (2 1/2 min. OEI) 1,940 20,900/100 44,700/102 903º C Maximum Rating (10 Min. dual) 1,890 20,900/100 44,700/102 878º C Intermediate Rated Power (IRP) (30 min dual) 1,800 20,900/100 44,700/102 851º C Maximum Continuous Power (MCP) 1,662 20,900/100 44,700/102 810º C Page No. 1 2 3 4 5 6 7 Rev. No. 0 0 0 0 0 0 1 R00113SE H-60, LLC UH-60A UH-60L Revision 1 March 4, 2025 Page 2 of 7 R00113SE ENGINE LIMITS: (T700-GE-701D/CC) SHAFT HP POWER TURBINE RPM/% GAS GEN RPM/% POWER TURBINE INLET (TGT) Contingency Rated Power (CRP) (2 1/2 min. OEI) 1,940 20,900/100 44,700/102 903º C Maximum Rating (10 Min. dual) 1,890 20,900/100 44,700/102 878º C Intermediate Rated Power (IRP) (30 min dual) 1,800 20,900/100 44,700/102 851º C Maximum Continuous Power (MCP) 1,662 20,900/100 44,700/102 810º C TRANSMISSION LIMITS: TORQUE: (UH-60A) 110% Single Engine (No time limit) 100% Dual Engine (No time limit) ROTOR LIMITS: Max. 258 RPM Min. 232 RPM AIRSPEED LIMITS: Vne Power on: 193 knots IAS, (221 MPH). See H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH-60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024, or later FAA-approved revision for variations of Vne with gross weight, pressure altitude, and temperature and for additional data. Page 3 of 7 R00113SE EMPTY WEIGHT C.G. RANGE: None DATUM: 341.2 inches forward of the main rotor centroid. LEVELING MEANS: Plumb bob in L/H cabin door frame to leveling plate on cabin floor. Ref. TM 1-1570-237-23. MAXIMUM WEIGHT: 22,000 lbs. MINIMUM CREW: 2 (pilot, copilot) NUMBER OF SEATS: 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. Refer to H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH-60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024, or later FAA- approved revision for seat configuration and loading information. FUEL CAPACITY: 361.5 gallons; 2 tanks (LH & RH interchangeable). 359.7 gallons; 2 tanks (LH &RH interchangeable) (with fuel boost pumps installed). OIL CAPACITY: 7 quarts each engine. OTHER LIMITS: Refer to H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH-60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024, or later FAA-approved revisions. Flight hours are counted from takeoff to landing. II – MODEL: UH-60L (Restricted Category Military Surplus Rotorcraft) Approved 1/27/2025. ENGINES: (2) General Electric T700-GE-701C (Original) (2) General Electric T700-GE-701D/CC (Alternate) FUEL: Aviation Kerosene JP-4, JP-5, JP-8, Jet A, Jet A-1 or Jet B. ENGINE LIMITS: (T700-GE-701C) SHAFT HP POWER TURBINE RPM/% GAS GEN RPM/% POWER TURBINE INLET (TGT) Contingency Rated Power (CRP) (2 1/2 min. OEI) 1,940 20,900/100 44,700/102 903º C Maximum Rating (10 Min. dual) 1,890 20,900/100 44,700/102 878º C Intermediate Rated Power (IRP) (30 min dual) 1,800 20,900/100 44,700/102 851º C Maximum Continuous Power (MCP) 1,662 20,900/100 44,700/102 810º C ENGINE LIMITS: (T700-GE-701D/CC) SHAFT HP POWER TURBINE RPM/% GAS GEN RPM/% POWER TURBINE INLET (TGT) Contingency Rated Power (CRP) (2 1/2 min. OEI) 1,940 20,900/100 44,700/102 903º C Maximum Rating (10 Min. dual) 1,890 20,900/100 44,700/102 878º C Intermediate Rated Power (IRP) (30 min dual) 1,800 20,900/100 44,700/102 851º C Maximum Continuous Power (MCP) 1,662 20,900/100 44,700/102 810º C TRANSMISSION LIMITS: TORQUE: (UH-60L) 135% Single Engine (No time limit) 120% Dual Engine (No time limit) ROTOR LIMITS: Max. 258 RPM Min. 232 RPM Page 4 of 7 R00113SE AIRSPEED LIMITS: Vne Power on 193 knots IAS, (221 MPH). See H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH-60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024, for variations of Vne with gross weight, pressure altitude, and temperature. OTHER LIMITS: Refer to H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH-60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024, or later FAA- approved revisions for additional limitation data. DATUM: 341.2 inches forward of the main rotor centroid. MAXIMUM WEIGHT: 22,000 lbs. MINIMUM CREW: 2 (pilot, copilot) NUMBER OF SEATS: 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). 359.7 gallons; 2 tanks (LH &RH interchangeable) (with fuel boost pumps installed). OIL CAPACITY: 7 quarts each engine. DATA PERTINENT TO ALL MODELS SERIAL NO. APPROVED: U.S. military surplus, UH-60A, and UH-60L Blackhawk helicopters as identified in H-60 LLC Approved Serial Number List Report Number SNL-H60, Rev. IR, Dated January 23, 2025, or later FAA-approved revision. Page 5 of 7 R00113SE CERTIFICATION BASIS: Part 21 § 21.25(a)(2) effective February 1, 1965, including Amendments 21-1 through 21-42 for the special purposes listed in FAR 21.25 (b)(1)(2)(7). § 21.25(b) (1) Agriculture Operations § 21.25(b) (2) Forest & Wildlife Conservation § 21.25(b) (7) External Loads Note: In accordance with § 36.1(a) (4), compliance with the noise requirements was not shown. Therefore, aircraft certificated under this type certificate are only eligible for aerial dispensing of liquids and forest conservation material excepted by § 36.1(a)(4) and defined under § 137.3 and 133.1(b). Page 6 of 7 R00113SE Any alteration to the aircraft for Special Purposes not identified above requires further FAA approval and in addition, may require noise and/or flight testing. This aircraft is approved for Day or Night VFR operations only. Flight into known icing conditions is prohibited. General Note: Any subsequent modifications to the helicopters type certified under this Type Certificate are to have the certification basis for that modification established under 14 CFR part 21 § 21.101 published June 7, 2000 which became effective June 10, 2003. Model UH-60A Non-significant modifications are to meet the requirements of 14 CFR part 29 airworthiness standards, transport category, Amendment 29-1 through 29-17, effective December 1, 1978, and 14 CFR part 29 § 29.1529, Instructions for Continued Airworthiness, Amendment 29-20, effective September 11, 1980. Model UH-60L Non-significant modifications are to meet the requirements of 14 CFR part 29 airworthiness standards, transport category, Amendment 29-1 through 29-24, effective December 6, 1984. DATE OF APPLICATION: March 9, 2021 PRODUCTION BASIS: None. No helicopters may be produced under this approval. No helicopter serial number may be added to this type certificate unless approved by the cognizant Certification Branch. EQUIPMENT: The basic required equipment necessary for the particular special purpose operation must be installed for certification. In addition, the following items of equipment must be on board the helicopter and available to the crew: Models UH-60A and UH-60L H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH- 60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024, or later FAA-approved revision. NOTE 1: A current weight and balance report including a list of equipment included in the certified empty weight, and loading instructions when necessary, must be provided for each helicopter at the time of original airworthiness certification. NOTE 2: All placards required by either the FAA-approved Rotorcraft Flight Manual, the applicable operating rules, or the Type Certification Data, must be installed on the helicopter. Required placards are contained in H-60, LLC. Decals, Placards & Markings Report No. DPM-H60, Revision IR, Dated July 24, 2023, or later FAA-approved revision, or any applied technical bulletins. NOTE 3: The helicopter(s) must be serviced, maintained, inspected, repaired and overhauled in accordance with the requirements specified in H-60, LLC. document ICA-H60 “Instructions for Continued Airworthiness”, Revision 2, Dated October 7, 2024, or later FAA-accepted revision, or inspected in accordance with other FAA-accepted inspection programs. The service life limited parts, overhaul and retirement intervals for these helicopters is specified in the FAA-Approved airworthiness limitation sections of document no. ICA-H60. An FAA-approved/accepted copy must accompany each helicopter on delivery. General Electric (GE) Aviation Unit and T700 Intermediate Maintenance Manual SEI 671 Change 4, dated July 16, 2021 and General Electric (GE) T700 Depot Maintenance Manual SEI 676 Change 14 dated February 17, 2023 or later FAA-accepted revision, are an acceptable alternate method for servicing, maintaining, inspecting, repairing and overhauling General Electric GE T700-GE-700, T700-GE-701C and T700-GE-701D engines. Revisions to the above listed manuals must be submitted to the FAA East Certification Branch, Boston, for review and concurrence before being submitted to the FAA Rotorcraft Aircraft Evaluation Division (AED) for FAA acceptance. Page 7 of 7 R00113SE NOTE 4: This helicopter must be operated in accordance with the Operator’s Manual comprised of the following: H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH- 60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024 or later FAA-approved revision. NOTE 5: This aircraft is prohibited from carrying cargo for compensation or hire. Carriage of cargo is limited to such cargo that is incidental to the helicopter owner/operator's business, which is other than air transportation. NOTE 6: A Restricted Category helicopter may not be operated in a foreign country without the express written approval of that country. NOTE 7: This helicopter has not been shown to meet the requirements of the applicable comprehensive and detailed airworthiness code as provided by Annex 8 to the Convention on International Civil Aviation. NOTE 8: Installation of T700-GE-701C or T700-701D/CC engines is approved when the aircraft is configured in accordance with US Army AWR no. 1682 R22, and when Auto- Relight and Transient Droop Improvement Installation have been incorporated via MWO 1-1520-237-30-3. UH-60A helicopters under this type certificate. Performance information and limitations with T700-GE-701C or T700-GE-701D/CC engines are contained in Chapter 7A of H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH-60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024, or later FAA-approved revision. NOTE 9: The US Army Safety Messages that must be complied with for the helicopter and engine prior to certification are contained in H-60, LLC Configuration Report Document No. Config-H60. A new report is generated for each initial certification project. Airworthiness Directives are contained in H-60, LLC Document No. AD-H60, Revision IR, Dated August 16, 2024 or later revision. NOTE 10: Alternative and emergency fuels are listed in document no.: H-60, LLC document no. RFM-H60 “Rotorcraft Flight Manual for H-60, LLC Model UH- 60A & UH-60L Helicopters”, Revision 0, Dated May 27, 2024 or later FAA-approved revision. NOTE 11: No person may be carried onboard this aircraft unless that person is a flight crewmember: is a flight crewmember trainee: performs an essential function in connection with a special purpose operation for which the aircraft is certificated: or is necessary to accomplish the work activity directly associated with that special purpose. Reference 14 CFR § 91.313(d). NOTE 12: Any alteration to the type design of this aircraft may require Instructions for Continued Airworthiness. Changes to the type design by means of a Supplemental Type Certificate requiring ICAs or changes to existing ICAs must be submitted and received by the Rotorcraft Aircraft Evaluation Division (AED). Type design changes by means or an FAA field approval that require ICAs must have those ICAs reviewed by the Flight Standards District Office managing the field approval or the Rotorcraft AED. NOTE 13: No helicopter may obtain a Restricted Category Airworthiness Certificate under this type certificate unless it is included in the "Approved Serial Number List", H-60, LLC Report Number SNL-H60, Revision IR, Dated January 23, 2025, or later FAA approved revision. NOTE 14: The builder's data plate must be installed in accordance with H-60, LLC. Decals, Placards, & Markings Report No. DPM-H60, Revision IR, Dated July 24, 2023, or later FAA-approved revision, or any applied technical bulletins. END ``` ## ADs None name its models. ## Registered aircraft by registry model (OpenAirDocs) - [H-60 UH-60L](https://openairdocs.org/model/h-60-uh-60l): 1 aircraft (registry code 8141843) ## STCs approved under this data sheet (16) - [STC SR02753LA](https://openairdocs.org/stc/SR02753LA): Installation of an engine Inlet Barrier Filter (IBF). Aerometals Inc. - [STC SR02597SE](https://openairdocs.org/stc/SR02597SE): Installation of Purge Fuel Collector System. Timberline Aerospace LLC - [STC SR02650SE](https://openairdocs.org/stc/SR02650SE): Installation of Station 34.5 Beam Modification. Timberline Aerospace LLC - [STC SR12058AK](https://openairdocs.org/stc/SR12058AK): Installation of Recoil Aerospace, Inc. T750-I Internal Fire Suppression Tank. Recoil Aerospace Inc. - [STC SR12471AT](https://openairdocs.org/stc/SR12471AT): Installation of RMCI Health Useage and Monitoring System (HUMS). RMCI Inc. - [STC SR00903DE](https://openairdocs.org/stc/SR00903DE): Installation of Left and Right, Hand Hold, Step and Step Fairing modification. Blackhawk Mission Equipment - [STC SR12380LA](https://openairdocs.org/stc/SR12380LA): Installation of Aerocraft's External Load Mount Kit (ARC-H60ELM). Aerocraft Incorporated - [STC SR04461CH](https://openairdocs.org/stc/SR04461CH): Installation of a Helitak FT4500 Black Hawk Fire Tank Liquid Dispensing System. Helitak USA, LLC - [STC SR02767LA](https://openairdocs.org/stc/SR02767LA): Installation of H-60 Electric APU Starter Modification to replace the original equipment hydraulic APU starter system on Restricted Category H-60 Firefighting and Utility Helicopters. Aerocraft Inc. - [STC SR02764LA](https://openairdocs.org/stc/SR02764LA): Installation of lift kit. Aerocraft Incorporated - [STC SR02544LA](https://openairdocs.org/stc/SR02544LA): Installation of a left side bubble window and a modified left side main landing gear fairing. Aerocraft Incorporated - [STC SR02744SE](https://openairdocs.org/stc/SR02744SE): Installation of BLR FastFin System. BLR Aerosapce LLC - [STC SR00919DE](https://openairdocs.org/stc/SR00919DE): Installation of Left and Right Pulse Light. Blackhawk Mission Equipment - [STC SR02584AK](https://openairdocs.org/stc/SR02584AK): Installation of Recoil Aerospace, Inc. T1000-E or T650-E Fire Suppression Tank. Recoil Aerospace Inc. - [STC SR02688SE](https://openairdocs.org/stc/SR02688SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc. - [STC SR00896DE](https://openairdocs.org/stc/SR00896DE) (historical): The installation of a bubble window with view port as a direct replacement for the existing window in the left hand side Cockpit door. Blackhawk Mission Equipment --- 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.