TCDS R00025LA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET R00025LA This data sheet, which is a part of Type Certificate No. R00025LA 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) SIXTYHAWK TC, LLC HOLDER: 2015 McKinley Ave. Suite F4 La Verne, CA 91750 I – MODEL: SIXTYHAWK TC, LLC EH-60A/UH-60A (Restricted Category Rotorcraft) Approved 04/27/2020. ENGINES: (2) General Electric T700-GE-700 Original (2) General Electric T700-GE-701C Alternate (2) General Electric T700-GE-701D Alternate FUEL: Aviation Kerosene JP-4, JP-5, JP-8, Jet A, Jet A-1 or Jet B. 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 ENGINE LIMITS: (T700-GE-701D) 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. 1 - - 1 1 1 - R00025LA Revision 1 SIXTYHAWK TC, LLC EH-60A HH-60L UH-60A April 27, 2020 Page 2 of 7 R00025LA 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 document BD-RFM-001 “Rotorcraft Flight Manual Restricted Category Utility Helicopter, UH-60A” for variations of Vne with gross weight, pressure altitude, and temperature. Refer to SixtyHawk TC, LLC document no. RFM-BD-001 “Rotorcraft Flight Manual for UH-60A, UH-60L, & EH-60A Blackhawk Helicopter”, Rev. IR, Dated May 31, 2019 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) Page 3 of 7 R00025LA 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. OTHER LIMITS: Refer to SixtyHawk TC, LLC document no. RFM-BD-001 “Rotorcraft Flight Manual for UH-60A, UH-60L, & EH-60A Blackhawk Helicopter:”, Rev. IR, Dated May 31, 2019 or later FAA approved revisions. Flight hours are counted from takeoff to landing II – MODEL: SIXTYHAWK TC, LLC HH-60L (Restricted Category Rotorcraft) Approved 06/07/2019. ENGINES: (2) General Electric T700-GE-701C Alternate (2) General Electric T700-GE-701D 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) 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 document RFM-BD-002 “Rotorcraft Flight Manual Restricted Category Utility Helicopter, HH-60L Blackhawk Helicopter:” for variations of Vne with gross weight, pressure altitude, and temperature. Refer to SixtyHawk TC, LLC document no. RFM-BD-002 “Rotorcraft Flight Manual Restricted Category Utility Helicopter, HH-60L Blackhawk Helicopter:”, Rev. IR, Dated May 31, 2019 or later FAA approved revisions for additional limitation data. Page 4 of 7 R00025LA 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. OTHER LIMITS: Refer to SixtyHawk TC, LLC document no. RFM-BD-002 “Rotorcraft Flight Manual Restricted Category Utility Helicopter, HH-60L Blackhawk Helicopter”, Rev. IR, Dated May 31, 2019 or later FAA approved revisions. Flight hours are counted from takeoff to landing DATA PERTINANT TO ALL MODELS SERIAL NO. APPROVED: U.S. military surplus, EH-60A, UH-60A and HH-60L Blackhawk helicopters as identified in SixtyHawk TC, LLC Serial Number Approved Report Number RPT-BD-102, Rev. NC dated June 6, 2019, or later FAA approved revision. 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. Page 5 of 7 R00025LA 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). Any alteration to the aircraft for Special Purposes not identified above require further FAA approval and in addition, may require noise and/or flight testing. 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. 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: AUG. 27, 2018 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. In addition, the following items of equipment must be on board the helicopter and available to the crew: Model EH-60A/UH-60A “Rotorcraft Flight Manual for UH-60A, UH-60L, & EH-60A Blackhawk Helicopter:”, Document number RFM-BD-001, Rev. IR, Dated May 31, 2019, or later FAA-approved revision Model HH-60L “Rotorcraft Flight Manual for HH-60L Blackhawk Helicopter:”, Document number RFM- BD-002, Rev. IR, Dated May 31, 2019, 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 SixtyHawk TC, LLC Engineering Configuration Drawing number BD-001-100, Revision NC dated January 8, 2019, 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 SixtyHawk TC, LLC. document no. ICA- BD-001 “Instructions for Continued Airworthiness” Rev. NC dated January 8, 2019, 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 the ICA-BD-001. An FAA approved/accepted copy must accompany each helicopter on delivery. General Electric (GE) Aviation Unit and T700 Intermediate Maintenance Manual SEI 671 Change 1, dated March 1, 2014 and General Electric (GE) T700 Depot Maintenance Manual SEI 676 Change 7 dated September 1, 2013 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 Boston Aircraft Certification Office for review and concurrence before being submitted to the FAA Fort Worth Aircraft Evaluation Group for FAA-acceptance Page 6 of 7 R00025LA NOTE 4: This helicopter must be operated in accordance with the Operator Manual comprised of the following: Model EH-60A/UH-60A “Rotorcraft Flight Manual for UH-60A, UH-60L, & EH-60A Blackhawk Helicopter”, Document number RFM-BD-001, Rev. IR, Dated May 31, 2019, or later FAA-approved revision Model HH-60L “Rotorcraft Flight Manual for HH-60L:”, Document number RFM-BD-002, Rev. IR, Dated May 31, 2019, 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 T-700-GE-701D engines in accordance with SixtyHawk TC, LLC. Technical Bulletins TB-BD-101, "T700-GE-701D/CC Engine Installation, Revision NC dated January 17, 2019, or later FAA-approved revision, and TB-BD-102, "T700- GE-701D/CC Auto Relight and Transient Droop Improvement Installation, Revision NC dated January 17, 2019, or later FAA-approved revision, is approved for the helicopter models: EH-60A/UH-60A helicopters under this type certificate. Performance information and limitations with T700-GE-701D/CC engines are contained in Chapter 7A of RFM-SKY- 500 “Rotorcraft Flight Manual for UH-60A, UH-60L, & EH-60A Blackhawk Helicopter”, Document number RFM-BD-001, Rev. IR, Dated May 31, 2019, or later FAA-approved revision HH-60L helicopters under this type certificate. Performance information and limitations with T700-GE-701D/CC engines are contained in Chapter 7A of Rotorcraft Flight Manual for HH-60L:”, Document number RFM-BD-002, Rev. IR, Dated May 31, 2019, 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 SixtyHawk TC, LLC. Engineering Configuration Report document RPT-BD-100, Revision NC, dated January 18, 2019, or later FAA- approved revision. NOTE 10: Alternative and emergency fuels are listed in document no: Model EH-60A/UH-60A “Rotorcraft Flight Manual for UH-60A, UH-60L, & EH-60A Blackhawk Helicopter”, Document number RFM-BD-001, Rev. IR, Dated May 31, 2019, or later FAA-approved revision Model HH-60L “Rotorcraft Flight Manual for HH-60L:”, Document number RFM-BD-002, Rev. IR, Dated May 31, 2019, 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 .3I 3(d). Page 7 of 7 R00025LA 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 Fort Worth Aircraft Evaluation Group (FTW-AEG). 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 FTW-AEG. 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 ", SixtyHawk TC, LLC. Report Number RPT-BD-102, Revision NC, Dated June 7, 2019 or later FAA approved revision. NOTE 14: The builder's data plate must be installed in accordance with SixtyHawk TC, LLC. Drawing BD-001-101, Rev. NC dated January 8, 2019, or later FAA approved revisions. END