TCDS R00054SE

Page No. 1 2 3 4 Rev. No. - - - - DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET R00054SE This data sheet, which is a part of Type Certificate (TC) No. R00054SE, 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 High Performance Helicopters Corp. HOLDER: 17819 Airport Road Lakeview, OR 97630 Mailing Address: P.O. Box 390 Crestline, CA 92325 TYPE CERTIFICATE HOLDER RECORD: N/A I - MODEL: UH-60A (Restricted Category Military Surplus Rotorcraft) Approved October 5, 2017 ENGINES: (2) General Electric T700-GE-700 Original (2) General Electric T700-GE-701D/CC (Alternate) *See NOTE 8 for alternate engine information. FUEL: Aviation Kerosene JP-4, JP-5, JP-8, Jet A, Jet A-1 or Jet B. *See NOTE 10 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 Maximum Continuous Power (MCP) 1,318 20,900 44,700 775º 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: 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%) R00054SE Revision 0 High Performance Helicopters Corp. UH-60A October 5, 2017 Page 2 of 4 R00054SE AIRSPEED LIMITS: Vne Power on: 193 knots IAS, (221 MPH). See HPH 1-1520-237-10, “Rotorcraft Flight Manual for High Performance Helicopters Corp. UH-60A,” Revision 0, dated August 15, 2017, or later FAA-approved revision for variations of Vne with gross weight, pressure altitude, and temperature and for additional limitation data. C.G. RANGE 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. Work Package 1727 contained in TM 1-1520-237-23. MAXIMUM WEIGHT: 22,000 lbs. *See NOTE 14 for configuration requirements. MINIMUM CREW: 2 (pilot, copilot) at Sta. 227.1 NO. OF PASSENGERS None. *See NOTE 11 for information on personnel carrying restrictions. 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 HPH 1-1520-237-10, “Rotorcraft Flight Manual for High Performance Helicopters Corp. UH-60A,” Revision 0, dated August 15, 2017, or later FAA-approved revision for approved seat configurations and loading information. OTHER LIMITS: Refer to HPH 1-1520-237-10, “Rotorcraft Flight Manual for High Performance Helicopters Corp. UH-60A,” Revision 0, dated August 15, 2017, or later FAA-approved revision. Flight hours are counted from takeoff to landing. FUEL CAPACITY: 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 OIL CAPACITY: 7 quarts each engine at Sta. 375.0 SERIAL NO. APPROVED: U.S. military surplus UH-60A helicopters as identified in High Performance Helicopters Corp. report no. HPH-UH60A-SNL-1 “Approved Serial Number Report,” Revision 0, dated September 20, 2017, or later FAA-approved revision. AIRCRAFT WEIGHT - LBS Page 3 of 4 R00054SE 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: March 2, 2017 PRODUCTION BASIS: None. No helicopters or parts 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: “Rotorcraft Flight Manual for High Performance Helicopters Corp. UH-60A,” No. HPH 1-1520-237-10, Revision 0, dated August 15, 2017, 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 High Performance Helicopters Corp. document # HPH-UH60A-DPM-1, Revision NEW, dated August 23, 2017, 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 High Performance Helicopters Corp. document no. HPH-UH60A-ICA-1, “High Performance Helicopters UH-60A ICA Manual,” Revision NEW, dated June 5, 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 HPH-UH60A-ICA-1. An FAA-approved/accepted copy must accompany each helicopter on delivery. NOTE 4: This helicopter must be operated in accordance with the Operator Manual “Rotorcraft Flight Manual for High Performance Helicopters Corp. UH-60A,” Document No. HPH 1-1520-237-10, Revision 0, dated August 15, 2017, 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. Page 4 of 4 R00054SE 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 High Performance Helicopters Corp. Technical Bulletin HPH-UH60A-TB-001 “Installation of T700-GE- 701D/CC Engines,” Revision 0, dated September 20, 2017, or later FAA-approved revision, is approved for the model UH-60A helicopters under this type certificate. Performance information and limitations with T700-GE-701D engines is contained in Chapter 7A of RFM HPH 1-1520-237-10, Revision 0, dated August 15, 2017, 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 High Performance Helicopters Corp. Model UH-60A Configuration Report document no. HPH-UH60A-CR-1, Revision 0, dated September 19, 2017, or later FAA-accepted revision. NOTE 10: Alternative and emergency fuels are listed in “Rotorcraft Flight Manual for High Performance Helicopters Corp. UH-60A” document no. HPH 1-1520-237-10, Revision 0, dated August 15, 2017, 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 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 13: 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 14: Aircraft must be equipped with 14-lug wheels for ground operations in excess of 20,500 lbs. - END -