# TCDS R00031LA: Hagglund Helicopters LLC - Type: Type certificate data sheet - Status: Current - Holder: Hagglund Helicopters LLC - Revision: 0 - Revised: April 28, 2026 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 29 - Data sheet PDF: https://openairdocs.org/files/sha256/a9/0e/a90ea2de9d1be41d8e9658234eaf208924265e2835b2d85c6c0249a3dc997279 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129301591020260429222051.0001 - Page: https://openairdocs.org/tcds/R00031LA ## Models (2) As the data sheet lists them. - UH-60A - 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 R00031LA This data sheet, which is a part of Type Certificate No. R00031LA prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the 14 Code of Federal Aviation Regulations (14 CFR). TYPE CERTIFICATE (TC) HOLDER: Hagglund Helicopters LLC 5101 NW A Ave Pendleton OR 97801 I – MODEL NUMBER: UH-60A (Restricted Category Military Rotorcraft) Approved April 28, 2026 ENGINES: (2) General Electric T700-GE-701D/CC Alternate *See NOTE 9 for alternate engine information. FUEL: Aviation Kerosene JP-4, JP-5, JP-8, Jet A, Jet A-1 or Jet B *See NOTE 18 for alternate and emergency fuels. 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: 110% Single Engine (No Time Limit) 100% Dual Engine (No Time Limit) ROTOR LIMITS: POWER OFF: POWER ON: Max. 265 RPM (110%) Max. 258 RPM (107%) Min. 217 RPM (90%) Min. 232 RPM (96%) AIRSPEED LIMITS: Vne POWER ON: 193 knots IAS, (221 MPH). Refer to HH-1-1520-237-10, Operator’s Manual for the Restricted Category Aircraft Model UH-60A Helicopter, Revision Original, Dated April 25, 2023, or later FAA approved revision(s), for variations of Vne with gross weight, pressure altitude, and temperature. Page No. 1 2 3 4 Rev. No. - - - - R00031LA REVISION 0 HAGGLUND HELICOPTERS LLC UH-60A APRIL28, 2026 Page 2 of 4 TC No. R00031LA 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 or electronic leveling means Ref. Work Package 1727 contained in TM 1-1520-237-23. MAXIMUM WEIGHT: 22,000 lbs. *See NOTE 15 MINIMUM CREW: 2 (Pilot in Command and Second in Command) both located at aircraft station 227. *See NOTE 14 NUMBER OF SEATS: OEM established locations: 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. No Passengers permitted. *See NOTE 11 MAX COMPARTMENT WEIGHT: Compartment C Compartment D Compartment E Sta. 247 to Sta. 288 6460 lbs. Sta. 288 to Sta. 343 8370 lbs. Sta. 343 to Sta. 398 8370 lbs. FUEL CAPACITY: 361.5 gallons; 2 tanks (LH & RH interchangeable) 359.7 gallons; 2 tanks (LH &RH interchangeable) (with fuel boost pumps installed) STA. 420.75 356.0 gallons closed circuit, 2 tanks (LH & RH interchangeable) STA. 420.75 OIL CAPACITY: 7 quarts each engine at STA. 375.0 OTHER LIMITS: Refer to HH-1-1520-237-10, Operator’s Manual for the Restricted Category Aircraft Model, UH-60A Helicopter, Revision Original, Dated April 25, 2023, or later FAA approved revision(s). Page 3 of 4 TC No. R00031LA DATA PERTINENT TO ALL MODELS SERIAL NO. APPROVED: Refer to the latest FAA approved revision(s) of Hagglund Helicopters LLC Document No. HH-2000, Revision 1, Dated October 20, 2022 Approved Serial Numbers List for the listing of all and UH-60A serial numbers that are approved by the FAA to be conformed under this Restricted Category Type Certificate. CERTIFICATION BASIS: Title 14 CFR part 21 §21.25(a)(2) effective February 1, 1965, including Amendments 21-1 through 21-42 for the special purposes listed in 14 CFR §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 In accordance with § 36.1(a) (4), compliance with the noise requirements was not shown. Therefore, aircraft certificated under this type certificate are limited to dispensing of firefighting materials when performing the special purpose listed in FAR 21.25(b)(2) Forest & Wildlife Conservation. Any alteration to the aircraft for Special Purpose operations not identified above require further FAA approval and in addition, may require noise and/or flight testing. This aircraft approved for Day or Night VFR operations only. Flight into known icing conditions is prohibited. 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 §21.101. Otherwise, non-significant modifications are to meet the requirements of 14 CFR 29 airworthiness standards, transport category, Amendment 1, effective August 12, 1965 and 14 CFR part 29 § 29.1529, Instructions for Continued Airworthiness, Amendment 20, effective September 11, 1980. DATE OF APPLICATION: August 7, 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 Aircraft Certification Office. EQUIPMENT: The basic required equipment necessary for the particular special purpose operation must be installed for certification. The following item of equipment must be on board the helicopter and available to the flight crew. “Rotorcraft Flight Manual” No. HH -1-1520-237-10 Rev. Original Dated April 25, 2023, or Later FAA approved revision(s). 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 Hagglund Helicopters LLC Engineering Configuration Report HH- 1000, Revision 2, Dated September 25, 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 Hagglund Helicopters LLC Document No. HH- 3000 Instructions for Continued Airworthiness , Revision 6, Dated September 30 th, 2024, or later FAA accepted revision(s), or inspected in accordance with other FAA accepted inspection programs. The service life limited parts overhaul and retirement intervals for these helicopters are specified in the FAA-Approved airworthiness limitation sections of Document No. HH-3000. The latest FAA approved/accepted copy of the ICA must be provided with each helicopter at delivery and all later FAA approved revision(s) must be provided to the helicopter owner and operator. NOTE 4: The helicopter(s) must be operated in accordance with the Operator Manual comprised of the following: Page 4 of 4 TC No. R00031LA HH-1-1520-237-10, Operator’s Manual for Restricted Category Aircraft Model, UH- 60A Helicopter, Revision Original, Dated April 25th, 2023, including Supplements, or later FAA approved revision(s). NOTE 5: This aircraft is prohibited from carrying cargo for compensation or hire. Carriage of cargo is limited to such cargo that is required to support the approved special purpose. NOTE 6: Restricted Category helicopter may not be operated in a foreign country without the express written approval of that country’s Civil Air Authority. 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 the approved alternate engines must be in accordance with MWO 1-1520-237- 20-3. T700-GE-701C and T700- GE-701D/CC performance information and limitations are contained in Chapter 7A of HH-1 -1520-237-10, Operator’s Manual for Restricted Category Aircraft Model UH-60A Helicopter, Revision Original, Dated April 25th, 2023, or later FAA approved revision(s). Military engine changes are allowed provided the replacement engine is conformed to Hagglund Helicopters LLC Document N o. HH- 3000, Revision 6, dated September 30th, 2024, or later FAA approved revision(s). NOTE 9: All applicable FAA ADs and Military Safety Messages listed in Hagglund Helicopters LLC . Document No. HH-4000 Airworthiness Directives & Military Safety Messages Report, Revision 2, Dated May 25th, 2023, or later FAA-approved revision(s), must be complied with prior to original airworthiness certification. NOTE 10: Alternative and emergency fuels are listed in HH -1-1520-237-10, Operator’s Manual for Restricted Category Aircraft Model UH-60A Helicopter, Revision Original, Dated April 25th, 2023, or later FAA approved revision(s). 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 FAA Aircraft Evaluation Division (AED). Type design changes by means or an FAA field approval that requi re ICAs must have those ICAs reviewed by the Flight Standards District Office managing the field approval or 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”, Hagglund Helicopters LLC Report HH-2000, Revision 1, Dated October 20, 2022, or later FAA approved revision. NOTE 14: The TC Holder’s data plate required by 14 CFR §45.13 must be installed in accordance with Hagglund Helicopters LLC Data Plate Drawing No. HH -1-001, Revision NC, dated November 9, 2022, as approved by the Engineering Configuration Report HH-1000, Revision 2, Dated September 25, 2023, or later FAA-approved revision. - END – ``` ## ADs None name its models. ## STCs approved under this data sheet (1) - [STC SR02753LA](https://openairdocs.org/stc/SR02753LA): Installation of an engine Inlet Barrier Filter (IBF). 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