1965

Installation of Turbocharged Lycoming G0-480-G1D6 engine (STC SE124SO) per FAA Sealed Roto-Master (Rajay/Riley) drawing List R0018. FAA approved Flight Manual Supplement, dated November 24, 1965 or later, FAA approved revision and Roto-Master (RAJAY/Riley) Turbo Owner s Manual required with this installation.

Aircraft: H-295 (USAF U10D)

Installation of Plane Booster Kit 101-C 1000 in accordance with Upper Valley Drawing 101-24250-6, dated January 10, 1965, and Installation Instructions, Revision 2, dated June 3, 1968.

Aircraft: 172, 172A, 172B, 172C +57 more

Installation of a Passenger Entertainment System per United Air Lines Report No. F-991 dated January 28, 1965, revision February 23, 1965.

Aircraft: 720 Series

Installation of cargo bins and seat track adaptors per United Air Lines Approved Drawing List No. COA T-2115 revised October 11, 1965, or later FAA approved revisions.

Aircraft: DC-8-12, DC-8-21, DC-8-51, DC-8-52

Installation of door-mounted inflatable evacuation slides in accordance with United Air Lines Approved Drawing List COA 6-3072/COA 6-3087. United Air Lines Supplemental Revision No. 1 dated August 25, 1965, to Douglas Airplane Flight Manual SM-19501, or Supplemental Revision No. 1 dated June 10, 1966, to Douglas AFM SM-19544 is required.

Aircraft: DC-6

Modification of R. H. forward lounge as described by United Air Lines Approved Drawing List No. COA 2-2450 dated March 4, 1965, or later FAA approved revisions.

Aircraft: DC-8-11, DC-8-12, DC-8-21, DC-8-51 +1 more

Installation control and annunciation circuitry to implement Flight Director "Go-Around" command modes in accordance with the UAL FAA approved drawing list dated August 11, 1965, revised August 16, 1965. UAL FAA approved Airplane Flight Manual Supplementary Log of pages as listed.\nType Manual Approved Dated Appendix\nDC-8-21, 31, 32, 33 SM 23889 1-19-60, 3-60, 2-1-60 and V\n 11-28-60 respectively\nDC-8-51, 52, 53 LB 30582 10-10-61, 4-28-61 and 4-28-61 resp. VII\nDC-8-51, 52, 53 LB 30757 1-26-62 IV\nDC-8F-54, 55 LB 31180 1-29-63, 6-19-64 respectively IV

Aircraft: DC-8-21, DC-8-31, DC-8-32, DC-8-33 +5 more

Installation of Cockpit Voice Recorder in accordance with United Airlines Engineering Report No. F-1021, dated June 9, 1965, revised November 9, 1965.

Aircraft: 720 Series

Installation of Cockpit Voice Recorder, United Data Controls, per United Air Lines Report F-1031 dated June 16, 1965, Revision, dated August 24, 1965, or later FAA approved revision.

Aircraft: Caravelle SE 210 Model VIR

Description of Type Design Change: Install Hoskins Twilighter MK III per Installation Manual and Specification Sheets as amended, dated September 20, 1965. Install Hoskins Twilighter MK IIIB Supplemental Lights per the following required data: Models 310 through 310F and 320 Specification Sheets P/N 65-0025-5 with drawings listed; Models 310G through N and 320-1 through F Specification Sheets P/N 65-0025-6 with drawings listed; Models 401, 401A and 402 Specification Sheets P/N 65-0025-9 with drawing listed; Models 411 and 411A Specification Sheets P/N 65-0025-7 with drawings listed; and Models 421 and 421A Specification Sheets P/N 65-0027-8 with drawings listed.

Aircraft: 310, 310A, 310B, 310C +28 more