1983

Installation of Duke Solid Chemical Dispersal System in accordance with Duke Drawing Number 10102, dated September 21, 1983, or later FAA approved revisions.

Aircraft: G-164A, G-164B

Installation of DC-10-10 yaw damper computers on DC-10-30 aircraft per COA 3-2958. This change order will replace Bendix yaw computers P/N 3757082-7 with Bendix yaw computers P/N 3757091-9 with mod "H" accomplished. The installation will be in accordance with United Air Lines, DAS-1-WE, Approved Drawing List No. 1936 dated June 7, 1983 or later FAA approved revisions.

Aircraft: DC-10-30

Three video projectors and their associated wiring and controls are installed throughout the cabin. Video installation was done according to United Air Lines, DAS-1-WE, Approved Drawing List No.1933 dated May 25, 1983, or later FAA approved revisions.

Aircraft: DC-8-71

Installation of an engine power trim system in accordance with FAA Approved United Airlines Report F-1953, Revision B, dated July 15, 1983, or later FAA approved revisions. United Air Lines FAA Approved Airplane Flight Manual Supplement B727-200 dated September 13, 1983, or later FAA approved revisions is required for this installation.

Aircraft: 727-200 Series

Cabin configuration changed to 24 F/C/72 business/141 coach seats. Installed two double closets, one single closet and the foldable crew rest berth in the door 2 area. Installed video in zones A, B & C. Removed centerline overhead storage compartments in zone A. Relocated lights and emergency oxygen supply to suit new cabin configuration. Replaced emergency evacuation alarm system with one similar to 747 system. This reconfiguration is accomplished according to United Air Lines, DAS-1-WE, Approved Drawing List No. 1935 dated June 16, 1983, or later approved revisions.

Aircraft: DC-10-30

Installation of 40:1 gear ratio wing flap transmissions and related changes in accordance with Colemill Enterprises, Inc., Installation Instructions dated February 16, 1983, or later FAA approved revision. This modification provides and equivalent means of compliance with paragraphs (a)1, (a)2, and (a)4 of AD 82-27-13 and restores the 40 (full) flap travel.

Aircraft: PA-31, PA-31-300, PA-31-325, PA-31-350 +1 more

Installation of one or two 90 US gallons fuselage auxiliary fuel tank(s), in accordance with Branson List of Drawings and Documents, No. 61A000, Revision B, FAA approved May 16, 1983, or later FAA approved revision.

Aircraft: Learjet 55C, Learjet 55B, Learjet 55

Modification in accordance with Delta Engineering Corporation Master Drawing List No. 93-8, Revision D, dated March 26, 1983 which removes the “Daylight Operations Only” limitation from Supplemental Type Certificates (STC’s) SA1048NE, SA1049NE, and SA1082NE.

Aircraft: DHC-7-102, DHC-7-103

Cockpit Sun Visor installation in accordance with FAA approved ROSEN Drawing List Number R500S-00DL, dated August 29, 1983, or later FAA approved revisions.

Aircraft: 525, 525A, 525B, 500 +5 more

Installation of Simuflight, Seattle Part No. SP-4000-1 and SP-4000-2 Fiberglass Camber Wing Tips in accordance with Simuflight, Seattle Installation Instructions SP-400. Simuflight, Seattle FAA Approved Airplane Flight Manual Supplement dated September 12, 1983 is required.

Aircraft: RC-3

Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

Aircraft: 210-5 (205), 210-5A (205A), 210B, 210C +18 more

Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

Aircraft: 337, 337A, 337B, 337C +8 more

Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

Aircraft: T207A, 207, 207A, T207

Installation of Lompoc Aero Specialties inner Plexiglass pane in swing out window frames presently employing a single window in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacture of the windows is controlled by Lompoc Aero Specialties Drawing LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

Aircraft: 172M, 172A, 172N, 172L +10 more

Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window, in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4, 1983, together with their FAA sealed Installation Instructions dated September 20, 1982, or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6, 1982, LAS 1013 dated October 5, 1982, and LAS 1014 dated October 6, 1982, or later FAA approved sealed revisions.

Aircraft: 206, P206, P206A, P206B +23 more