# TCDS H7NM: Rotary Rocket Company - Type: Type certificate data sheet - Status: Current - Holder: Rotary Rocket Company - Revision: 3 - Revised: May 7, 2003 - Product: Aircraft, Rotorcraft - Certification basis: Part 21 - Data sheet PDF: https://openairdocs.org/files/sha256/96/81/968171b543f3555659915fd513b195e33b0a8693045dfe1f61882ee9c8510292 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5D3B4BC553E0CFFD86257A3200591D98.0001 - Page: https://openairdocs.org/tcds/H7NM ## Models (2) As the data sheet lists them. - UH-34D (HUS-1) - UH-34E (HUS-1A) ## What the data sheet says This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION H7NM Revision 3 Rotary Rocket Company UH-34E UH-34D May 7, 2003 TYPE CERTIFICATE DATA SHEET NO. H7NM which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. This data sheet, which is a part of Type Certificate No. H7NM, prescribes conditions and limitations under which the product for Type Certificate Holder Rotary Rocket Company 1475 Terminal. Way, #E Reno, NV 89502 Type Certificate Holder Record: Federico Helicopters, Inc. 2291 Airways Drive, Bldg. 420-A Fresno, CA 93727 ... Model U.S. Marines UH-34E (HUS-1A), UH-34-D (HUS-1) (Restricted Category) approved February 4. 1985 Engine Wright Cyclone R-1820-84A 2. Wright Cyclone R-1820-84C/989C9HE2 3. Wright Cyclone R-1820-84D/998C9HE2 (same limitations as for Wright 989C9HE2) Fuel 115/145, 100/130 minimum grade aviation gasoline Engine Limits Fuel Grade 115/145 M.P. Maximum continuous in. Hg Alt. Maximum continuous 47.5 S.L. Takeoff (5 minutes) Takeoff (5 minutes) 46.0 56.5 3500 ft. S.L. (Straight line manifold pressure variation with altitudes shown.) 55.5 700 A. Fuel Grade 100/130 (Item (1) required) Maximum continuous Maximum continuous akeoff (5 minutes) Takeoff (5 minutes) (Straight line manifold pressure variation with altitudes shown. Rotor Limits aximum 258 rpm Minimum 170 rpm. See Note 3 for required placard. Airspeed Limits Maximum never exceed, Vne: 120 knots CAS (117 knots IAS) See Note 3 for required Placard. C.G. Range (+129.6) to +146.7) Empty weight C.G. Range None Page No. 3 Rev. No. 3 3 H7NM NOTE 1. Current weight and balance report, including list of equipment included in 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. When changes are made to the helicopter which affect weight and balance, refer to the Flight Manual for instructions. NOTE 2. time of critical components is contained in the Sikorsky S-68 Maintenance Manual Information essential to the proper maintenance of the helicopter including retirement provided with each helicopter. Volume II of SA-4045-15 & Sikorsky Equalized Inspection & Maintenance Program, or service life cannot be increased without FAA engineering approval. Component overhaul intervals shall be in accordance with Sikorsky Maintenance Manual, Section IV, Sikorsky Publications No. SA4045-15, Part IV, S-58 Maintenance Manual and Sikorsky Equalized Inspection and Maintenance Program, SA-4047-20. The values of retirement NOTE 3. pilot. The following placards must be displayed on the instrument panel in full view of the 1. ¿This helicopter must be operated in compliance with the operating limitations specified in the FAA approved rotorcraft flight manual SA-4045-12." 2. "Avoid fast turns, 15 sec. minimum for 360 degrees." 4. "During extending hovering, sideward and rearward flight, close windows and doors "During extended hovering, close windows and doors and turn vent system on. and turn vent system on." Close left window during starting and taxiing." "Avoid taxi turns below 2400 engine rpm." "Never exceed speeds. Variation of Vne with altitude, engine rpm and manifold ALTITUDE SEA LEVEL 10,000 FT. 5,000 FT. JAS Кл. 72 2200 RPM M.P 35.5 "Hg" 60 IAS " | M.P. Kn &7 2300 RPM 37.0 "Hg" 38.7 IAS 103 K.л. 76 2400 RPM | M.P. 41.0 "Hg" 42-3 117 JAS Kn. 90 2500 RPM M.P 47.5 F.T. "H¿" 63 F.T 7. "Maximum baggage permitted 1000 Ibs." "See loading information in flight manual." (On baggage compartment door) NOTE 4. Prior to civil airworthiness certification, the following must be accomplished: 1. Sikorsky S-58 series ADs must be reviewed for applicability pertinent to model to be certificated and complied with if required. Any follow-on ADs to be complied 2. Sikorsky S-58 Service Bulletin must be reviewed for applicability pertinent to model 3. Deactivate Automatic Flight Control System if installed. to be certificated and complied with if required by Sikorsky aircraft. Any follow-on service bulletin required by Sikorsky Aircraft to be complied with. NOTE 5. The transmission oil cooler blower may be removed in accordance with Sikorsky Drawing 58080-35001. 1956, reissued June 28, 1957, revised August 13, 1972, (RFM 4045-12) required when revised April 23, 1959, (1): Item 1 Flight Manual Supplement No. 5 dated October 9, 1957, reissued June 10, 1958, grade 100/130 fuel is used. to FAA approved Rotorcraft Flight Manual dated August 2; ...END... ``` ## ADs (1, in force first) - [AD 95-26-09](https://openairdocs.org/ad/95-26-09): Main Rotor Shaft · Consolidated Air Crane CH34A, CH34C, HSS-1N/UH-34J and 12 more. Effective Jan 4, 1996 ## Registered aircraft by registry model (OpenAirDocs) - [Sikorsky UH-34E](https://openairdocs.org/model/sikorsky-uh-34e): 0 aircraft (registry code 8141819) --- 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.