TCDS R00023LA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET R00023LA This data sheet, which is a part of Type Certificate (TC) No. R00023LA, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Title 14 Code of Federal Aviation Regulations (14 CFR). TYPE CERTIFICATE HOLDER Unical Air Inc. 1240 Oakhaven Lane Arcadia, California 91006 TYPE CERTIFICATE HOLDER RECORD: Unical Aviation, Inc .transferred to Unical Air Inc. on August 13, 2021 I - MODEL: UH-60A (Restricted Category Military Surplus Rotorcraft) Approved Aug 28, 2018 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. *See NOTE 9 for alternate and emergency fuels. 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%) ENGINE LIMITS: (T700-GE-700) POWER TURBINE GAS GEN POWER TURBINE SHAFT HP RPM RPM INLET (TGT) Military Power (30 min.) 1,561 20,900 44,700 850° C Maximum Continuous Power (MCP) 1,318 20,900 44,700 775° C ENGINE LIMITS: (T700-GE-701D/CC) POWER TURBINE GAS GEN POWER TURBINE SHAFT HP RPM/% RPM/% INLET (TGT) Contingency Rated Power (CRP) (2 1/2 min. OEI) 1,940 20,900/100 44,700/102 903° C Maximum Rating (10 Min. dual) 1,890 20,900/100 44,700/102 878° C Intermediate Rated Power (IRP) (30 min dual) 1,800 20,900/100 44,700/102 851° C Maximum Continuous Power (MCP) 1,662 20,900/100 44,700/102 810° C Page No. 1 2 3 4 Rev. No. 1 - - - R00023LA Revision 1 Unical Aviation, Inc. UH-60A August 13, 2021 Page 2 of 4 R00023LA AIRSPEED LIMITS: Vne Power on: 193 knots IAS, (221 MPH). See UAI 1-1520-237-10, Rotorcraft Flight Manual for Unical Aviation UH-60A, Revision A, dated April 18, 2018, or later FAA-approved revision for variations of Vne with gross weight, pressure altitude, and temperature and for additional limitation data. EMPTY WEIGHT C.G. RANGE: DATUM: LEVELING MEANS: MAXIMUM WEIGHT: MINIMUM CREW: NO. OF PASSENGERS NUMBER OF SEATS: OTHER LIMITS: FUEL CAPACITY: OIL CAPACITY: SERIAL NO. APPROVED: None 341.2 inches forward of the main rotor centroid. Plumb bob in L/H cabin door frame to leveling plate on cabin floor. Ref. Work Package 1727 contained in TM 1-1520-237-23. 22,000 lbs. *See NOTE 13 for configuration requirements. 2 (pilot, copilot) at Sta. 227.1 None. *See NOTE 10 for information on personnel carrying restrictions. 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 UAI 1-1520-237-10, Rotorcraft Flight Manual for Unical Aviation UH-60A, Revision A, dated April 18, 2018, or later FAA-approved revision for approved seat configurations and loading information. Refer to UAI 1-1520-237-10, Rotorcraft Flight Manual for Unical Aviation UH-60A, Revision A, dated April 18, 2018, or later FAA-approved revision. Flight hours are counted from takeoff to landing. 361.5 gallons; 2 tanks (LH & RH interchangeable) 359.7 gallons; 2 tanks (LH &RH interchangeable) (with fuel boost pumps installed). at Sta. 420.75 7 quarts each engine at Sta. 375.0 U.S. military surplus UH-60A helicopters as identified in Unical Aviation report no. UAI UH60A-SNL, Military Document Supplement, Revision -, dated April 05, 2018, or later FAA-approved revision. Page 3 of 4 R00023LA CERTIFICATION BASIS: 14 CFR Part 21 § 21.25(a)(2) for the special purposes listed in 14CFR Part 21.25 (b)(1)(2)(7) as defined below: (1) § 21.25(b)(1) Agriculture Operations (2) § 21.25(b)(2) Forest & Wildlife Conservation (3) § 21.25(b)(7) External Loads Note: 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 as defined in § 137.3, aerial dispensing of liquids and forest conservation material as defined in § 137.3, or external loads as defined in § 133.1(b). Any alterations to the aircraft for Special Purposes 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. 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 § 21.101. Non-significant modifications shall have a certification basis of 14 CFR § 29 dated February 1, 1965, including Amendments 29-1 through 29-17 (amendment effective as of 12/1/1978) and 29.1529, Instructions for Continued Airworthiness, Amendment 29-20, effective September 11, 1980. DATE OF APPLICATION: July 25, 2017 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 item of equipment must be on board the helicopter and available to the flight crew: UAI 1-1520-237-10, Rotorcraft Flight Manual for Unical Aviation UH-60A, Revision A, dated April 18, 2018, or later FAA-approved revision. NOTE 1: A current weight and balance report, including a list of equipment included in the certificated 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 Unical Aviation document UH60A-RPD, Revision -, dated April 06, 2018, 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 Unical Aviation document no. UA-UH60A-ICA-1, Instructions for Continued Airworthiness, Revision - , dated December 08, 2017, or later FAA-accepted revision, or in accordance with any other FAA-accepted maintenance program. The service life limited parts retirement intervals for these helicopters is specified in the FAA-approved airworthiness limitations sections of UA-UH60A-ICA-1. An FAA-approved/accepted copy must accompany each helicopter on delivery. Page 4 of 4 R00023LA - END - NOTE 4: This helicopter must be operated in accordance with the UAI 1-1520-237-10, Rotorcraft Flight Manual for Unical Aviation UH-60A, Revision A, dated April 18, 2018, 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: The US Army Safety Messages that must be complied with for the helicopter and engine prior to certification are contained in Unical Aviation, Configuration Report document no. UAI-UH60A- CR-1, Revision - , dated July 18, 2018, or later FAA-accepted revision. NOTE 9: Alternative and emergency fuels are listed in UAI 1-1520-237-10, Rotorcraft Flight Manual for Unical Aviation UH-60A, Revision A, dated April 18, 2018, or later FAA-approved revision. NOTE 10: 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 11: 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 of 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 12: No helicopter may obtain a Restricted Category Airworthiness Certificate under this type certificate unless it is included in the “Serial No. Approved” list above. NOTE 13: All aircraft under this TC must be equipped with 14-lug wheels for ground operations in excess of 20,500 lbs. NOTE 14: The builder’s data plate must be installed in accordance with Unical Aviation document UH60A- RPD, Revision -, dated April 06, 2018, or later FAA-approved revision.