# TCDS H4EA: Erickson Air-Crane Incorporated DBA Erickson Air-Crane - Type: Type certificate data sheet - Status: Current - Holder: Erickson Air-Crane Incorporated DBA Erickson Air-Crane - Revision: 4 - Revised: March 28, 2007 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheet PDF: https://openairdocs.org/files/sha256/fd/91/fd91714e73d9dbc233a6831b0412a1476bf9fcda90fe324d479619f6175699ed - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8D3AF9BC48F9CD21862585CB0058F460.0001 - Page: https://openairdocs.org/tcds/H4EA ## Models (1) As the data sheet lists them. - S-64E ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No 1 2 3 4 Rev No 4 4 4 4 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION H4EA Revision 4 ERICKSON AIR-CRANE INCORPORATED S-64E March 28, 2007 TYPE CERTIFICATE DATA SHEET NO. H4EA This data sheet, which is part of Type Certificate Number H4EA, prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate (TC) Holder Erickson Air-C rane Incorporated, DBA Erickson Air-Crane 3100 Willow Springs Road P. O. Box 3247 Central Point, Oregon 97502 Type Certificate Holder Record Sikorsk y Aircraft transferred TC H4EA to Erickson Air-Crane on February 13, 1992. I - Model Number: S-64E (Restricted Category) Approved March 18, 1969 Engines 2 Pratt & Whitney JFTD12A-4A (T73-P-1) Fuel Aviation Kerosene JP4 or JP5 Engine limits (See NOTE 6) Shaft Power Turbine Gas Gen. Power Turbine H.P. Speed (N 2) Speed (N 1) Inlet (T 5) Military Power 4500 105% 104% 688°C (30 min.) Normal Continuous 4000 105% 104% 655°C Cruise Rotor limits Max 110% N r (204 r.p.m.) Min 90% N r (167 r.p.m.) Airspeed limits Never exceed: 99 knots betw een 38,000 lb. and 42,000 lb. gross weight 115 knots up to 38,000 lb. gross weight C.G. range 328.0 to 357.0 at 23,000 lb. 324.0 to 357.0 at 30,000 lb. 328.0 to 357.0 at 38,000 lb. 328.0 to 346.0 at 38,000 lb. 328.0 to 346.0 at 42,000 lb. 324 328 23,000 30,000 38,000 357 Station--Inches Gross Weight (Pounds) 42,000 346 H4EA 2 Datum 336 inches forward of main rotor centroid. Leveling means Plumb line from top level plate inside cockpit aft door. Maximum weight 42,000 lb. Minimum crew 2 (pilot and co-pilot). Number of seats 5: 2 at (+94.0), 1 at (+108.5), 1 at (+127.0), 1 at (+130.0). Maximum cargo See NOTE 5. Fuel capacity 1356 gal. 454 gal. at (+280.0), 454 gal. at (+397.3), 448.5 gal. at (+461.3). Oil capacity 2.8 gal. at (+234.0) (2 tanks 1.4 gal. each). Rotor blade and control movements For riggi ng infomation, see NOTE 8. Other operating See NOTE 4. Serial numbers eligible There are no e ligible serial numbers at this time. Certification basis FAR 21.25(a)(2) effective February 1, 1965, including Amendments 21-1 thru 21-4. Type Certificate No. H4EA issued March 18, 1969, for the Special Purpose of carriage of external loads. Date of applicati on for Type Certificate: February 26, 1969. Equipment Equipment necessary for the particular special-purpose operation must be installed (see NOTE 5). Production basis None. Prior to certification of each aircraft, an FAA representative must perform a detailed inspection for workmanship, material s, and conformity with approved technical data and a check of the flight characteristics. 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 in each helicopter at the time of original airworthiness certification and at all times thereafter. NOTE 2. The following placard must be prominently disp layed in the cockpit in full view of the pilots: "THIS ROTORCRAFT MUST BE OPERATED IN ACCORDANCE WITH THE RESTRICTED CATEGORY OPERATING LIMITATIONS OF FAR 91.39" NOTE 3. Service Life-Limited parts must be re tired in accordance with the following schedule: Component Part No . Service Life (Hours) Upper plate S6410-23011-101 4615 Lower plate S6410-23009-101 4615 Spacer S6410-23006-012 4175 Hub S1510-23001-4 5275 Sleeve S1510-23351 7300 Vertical hinge S1510-23022 2800 Horizontal hinge pin S1510-23099-1 1550 Scissors bracket, rotating S6410-24069-011 4950 Upper link, rotating S6410-24056-101 17,000 Lower link, rotating S6410-24052-101 17,000 Damper assembly S6410-26200-042 500 Damper upper bracket S6410-26106-041 500 Damper lower bracket S6410-26106-042 500 Main rotor blade S6415-20101-043 5000 Main rotor shaft S6435-20078-014 1100 3 H4EA NOTE 4. These helicopters must be operated in accordan ce with a Flight Manual comprised of the following: (1) Department of the Army Technical Manual No . TM 55-1520-217-10, "Operator's Manual, Army Model CH-54A Helicopters,” dated Janua ry 1967; revised Septermber 1968. (2) Sikorsky Aircraft "S-64E Commercial Helicopter Supplement to TM 55-1520-217-10, Operator's Manual, CH-54A Helicopt er,” dated March 3, 1969. (3) Department of the Army Technical Manual No. TM 55-1520-217-CL, "Operator's & Crewmember's Checklist, Army Model CH-54A Helicopter s, Pilot's Checklist,” dated October 1968. (4) Sikorsky Aircraft "S-64E Co mmercial Helicopter Supplement to TM 55-1520-217-CL, Operator's and Crewmember's Checklist, CH-54A Helicopter,” dated March 18, 1968. (5) Winterization Program Supplement to TM-55- 1520-217-10, Operator's Manual, CH-54A Helicopter. NOTE 5. Provisions for the carriage of external loads are av ailable in the form of structural hard points on the fuselage and main landing gear; single and four-point hoists; and a four-point load-leveler suspension system. Information concerning the operating limitations with this equipment is contained in the Flight Manual. NOTE 6. Deleted February 1, 1970. NOTE 7. Prior to civil airworthiness certification, compliance with the following must be accomplished: Department of the Army Technical Bulletins: TB55-1520-217-20/1 dated June 26, 1967. TB55-1520-217-20/2 dated April 25, 1963. TB55-1520-217-20/4 dated May 24, 1968. TB55-1520-217-30/1 dated September 4, 1968. TB55-1520-217-30/2 dated July 12, 1968. TB55-1520-217-30/3 dated August 26, 1968. NOTE 8. These helicopters must be serviced and maintained in compliance with the following: (1) Department of the Army Technical Manual No. TM 55-1520-217-20, "Organizational Maintenance Manual, CH-54A Helicopter,” da ted July 1967; revised January 1969. (2) Sikorsky Aircraft "Maintenance Manual (Part I of II), Sikorsky Models S-64E Helicopter,” dated December 1968. (3) Sikorsky Aircraft "Maintenance Manual (Par t I of II) (Appendix VI), Sikorsky Model S-64E Helicopter,” dated December 1968. (4) Department of the Army Technical Manua l No. TM 55-1520-217-20 PMD, "CH-54A Helicopter, Preventive Maintenance Daily Inspection Ch ecklist,” dated August 1968; revised October 1968. (5) Department of the Army Technical Manua l No. TM 55-1520-217-20 PMI, "CH-54A Helicopter, Preventive Maintenance Intermediate Inspecti on Checklist,” dated August 1968; revised November 1968. (6) Department of the Army Technical Manua l-No. TM 55-1520-127-20 PMP, "CH-54A Helicopter, Preventive Maintenance Periodic Inspection Ch ecklist,” dated August 1968; revised October 1968. (7) Sikorsky Aircraft "S-64E Maintenance Manual, Commercial Aircraft Supplement to TM 55-1520-217- 20 PMD, TM 55-1520-20 PMI, TM 55-1520-217-20 PMP, Preventive Maintenance Checklist, S-64E Helicopter." (8) Department of the Army Technical Ma nual No. TM 55-1520-217-35, "DS, GS, and Depot Maintenance Manual, CH-54 Helicopter,” dated July 1967; revised October 1968. (9) Sikorsky Aircraft "Maintenance Manual (Part II of II), Sikorsky Model S-64E Helicopter,” dated December 1968. H4EA 4 (10) Department of the Army Technical Bulletin No. TM 11-1520-217-20, "Organizational Maintenance Manual, Electronic Equipment Configuration, Ar my Model CH-54A Helicopter,” dated March 1967; revised November 1968. (11) Department of the Army Technical Ma nual No. TM 11-1520-217-35, "DS, GS, and Depot Maintenance Manual, CH-54A Helicopter,” dated March 1967. ...END... ``` ## ADs None name its models. ## STCs approved under this data sheet (5) - [STC SR02807SE](https://openairdocs.org/stc/SR02807SE): Installation of a Fly Away Tool box. Helicopter Transport Services LLC - [STC SR02777SE](https://openairdocs.org/stc/SR02777SE): Installation of a Load Beam. Helicopter Transport Services LLC - [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc - [STC SR02754SE](https://openairdocs.org/stc/SR02754SE): Installation of External Cargo Container. Helicopter Transport Services, LLC - [STC SR01956NY-D](https://openairdocs.org/stc/SR01956NY-D): Installation of a Keystone Helicopter Anti-Rotational Restraint System.. Erickson Air Crane Inc. dba Erickson Air-Crane --- 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.