1005

ONE ONLY STC, S/N 1005: Installation of a single pilot IFR configuration.

Aircraft: AS-350D

Installation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later.

Aircraft: E35, C35, F35, G35 +1 more

Installation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005, stamped FAA Approved on April 15, 1980, or later.

Aircraft: M35, N35, P35, J35 +2 more

Installation of elevator tail cone fairing per Smith Speed Conversions, Inc. Drawing List No. 1005 stamped FAA Approved on February 5, 1979, or later.

Aircraft: 95-C55, D55A, 95-A55, 95-B55 +9 more

Install 170 hp Lycoming O-340-A1A engine and Hartzell HC-82XL-1DB/8433-12 propeller according to Doyn data listed on Engineering Releases 100 (3/22/58), 1010 (3/16/57), 1011 (8/28/57), 1012 (7/15/57), 1014 (3/30/57), 1050 (7/13/57), 1051 (& DCN 1, 12/10/57), 1052 (7/19/57), 1053 (7/19/57), 1099 (3/22/58), and Instructions (2 sheets, undated) Data required for parts manufacture: As listed on Engineering Releases 1001 (1/18/57), 1002 (12/21/57), 1003 (5/1/57), 1004 (7/13/57), 1005 (7/12/57), 1006 (3/30/57), 1007 (4/12/57), 1008 (2/27/57), 1009 (10/23/57), 1015 (2/25/56).

Aircraft: 170B, 170A

Installation of Lycoming O-360-A1A, A1D, or B1B engine with McCauley 2D36C14-X/78KM-4 propeller or Lycoming O-360-A1A and A1D engines with Hartzell HC-C2YK-1A/7666A-2 propeller. Data required: Doyn Aircraft, Inc. Drawings: 1000, 1005 Rev. C, 1006 Rev. C, 1009, 1010 Rev. A, 1011, 1012 Rev. A, 1013, 1014, 1015, 1016, 1099, 1100 Rev. B, 1101 Rev. A, 1102, 1103 Rev. A, 1104, 1107, 1150. Drawing Changes Notices: 1005-5A, 1006-8A, 1006-6, 1009-2A, 1199-1A, 1199-2A, and 1199-3A.

Aircraft: 170A, 170B

Replacement of the original forward and aft left-hand cabin door wedge windows with Garlick window part numbers OH58W-1004-43 and OH58W-1005-43, respectively. Garlick parts are fabricated and installed in accordance with Garlick Master Drawing List (MDL) No. 990115, dated May 13, 1999, or later Federal Aviation Administration (FAA) approved revision. These replacement parts must be maintained in accordance with U.S. Army Aviation Unit and Intermediate Maintenance Manual No. TM-1520-228-23-1 for OH-58A and OH-58C Helicopters, Paragraphs 2-123 through 2-128, dated May 25, 1984, or later FAA approved revision.

Aircraft: OH-58A, OH-58A+, OH-58C

Installation of Lycoming TIO-540- J2B(d) engine, Hartzell HC-C3YR-2UF/FC8468D-6R, or HC-C4YR-2/ FC6660 propeller and optional Merlyn Products MPI 98-1005-519 turbocharger.

Aircraft: 500-U, 500-B, 500-S

Fiberglass nose bowl assemblies 1005-01-100 through -800.

Aircraft: 18 Series, C-45 Series