TCDS HR-35

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION HR-35 Revision 3 VERTOL H21A Revised January 24, 2005 TYPE CERTIFICATE DATA SHEET NO. HR-35 This data sheet which is a part of ty pe certificate No. HR -35 prescribes conditions and lim itations under which the product for which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. Type Certificate Holder: This Type Certificate (TC) has been designated as ABANDONED (See Note 5) Type Certificate Holder Record: Heli-Crane Corporation Van Nuys Airport 7646 Hayvenhurst Avenue Van Nuys, California I - Model H21A (Restricated Category), approved July 21, 1961 Engine Wright R-1820-103 Fuel 115/145 or 100/130 minimum grade aviation gasoline Engine limits Maximum r.p.m. 2600 Maximum manifold pressure 50 in. Hg. Rotor limits and Power Off (Rotor Tach) Power On (Engine Tach.) engine operating speeds Maximum 260 r.p.m. Maximum 2500 r.p.m. Minimum 235 r.p.m. Minimum 2300 r.p.m. Airspeed limits Vne (Never exceed) 110 knots. (See NOTE 2 for required placards) C.G. range 31 in. fwd. to 6.5 in. aft Datum Point midway between rotors Maximum weight 14,500 lb. Minimum crew 1 (Pilot) Fuel capacity Main fuel tank and three auxiliary tanks 600 gal. (3600 lb) Oil capacity 21.5 gal. Other operating USAF T.O. 1H-21-1 and Heli-Crane Corporation FAA Approved Flight limitations Manual Supplement Revision dated November 18, 1963. Serial Nos. eligible All USAF serial Nos Certification basis CAR 8 effective October 11, 1950. Type Certificate No. HR-35 issued July 21, 1961, for the purposes of: (1) Dumping fire retardants. (2) Aerial placement of power and telephone poles, air conditioning units, wet concrete and other similar items conducted in furtherance of operator's or lessee's own business only. Date of application for Type Certificate April 4, 1961. Page No. 1 2 Rev. No. 3 3 HR-35 Page 2 of 2 Revision 2 Production basis None. No helicopter may be produced under this approval. Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations (see certification basis) must be installed in the helicopter for certification. In addition, equipment necessary for the particular special purpose must be installed. 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 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 pilot: "Airspeed Limits" Never exceed speed, Vne 110 KIAS With external stores in place 65 KIAS Maximum dumping speed 40 KIAS With empty bag hanging free 40 KIAS NOTE 3. Prior to civil airworthiness certif ication, the following must be accomplished: (a) Modification in accordance with Heli-Crane Dwg . No. H.C.C. -001 or other FAA-approved special purpose modification. (b) The provisions of AD 51-12-1, AD 58-20-4, AD 60-7-8, AD 60-23-5, AD 64-19-6 and AD 64-27-4. (c) The provisions of USAF T.O. 1H-21-526, -531, -541, -582, -587, -588, -589, -592, -593, -593B, -600A, -601, -602, -604, -610, -614B, -616, -618, -620, -621, -622 and -623. NOTE 4. This model helicopter must be serviced and ma intained in compliance with T.O. 1H-21-6 including Heli-Crane Special Inspections on Pages 4-2 and 4-7; and AD 51-12-1, AD 60-23-5 and AD 64-27-4. NOTE 5. This Type Certificate (TC) has been designated "ABANDONED". A “Notice of Intent To Designate as Abandoned Certain Type Certificates Issued in the Restricted Category,” was published by the Federal Aviation Administration (FAA) in the Federal Register on August 8, 2003 (68 FR 47379). That Notice listed this TC. The FAA received no comments on the published Notice. The FAA has been unable to contact this TC holder. Hence, the FAA has determined that this TC holder is not complying with its Continued Operational Safety (COS) responsibilities. Therefore, no additional aircraft will be added to this TC and no additional original airworthiness certificates will be issued based on this TC. The effectiveness of this TC is limited to those aircraft that received original airworthiness certification prior to the incorporation of this note (Date of Incorporation, January 24, 2005). Subsequently, if the TC holder is located and assumes their COS responsibilities, the restriction(s) imposed by this note may be lifted. .....END.....