1999

Installation of the Sigma Tek 1U619-( ) VHF COM/NAV/ATC Radio Control Panel with Collins VHF 22(C/D) radios to provide 25kHz and 8.33 kHz channel spacing in Cessna Airplanes listed on the attached FAA Approved Model List (AML) No. ST00831WI, dated November 4, 1999, in accordance with Cessna Aircraft Company, Master Document List No. CF90055, Revision B, dated October 21, 1999 or later FAA approved revision.

Aircraft: 500, 550, S550, 650

Install extended baggage compartment and baggage net in accordance with Cub Crafters, Inc., Master Drawing List, MDL105400, Revision D, dated November 2, 1999, or later Federal Aviation Administration (FAA) approved revision, and its listed data.

Aircraft: PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A), PA-18-135 +12 more

Install right side access door in accordance with Cub Crafters, Inc. Master Drawing List, MDL 105900, Revision B, dated May 25, 1999, and its listed data or later Federal Aviation Administration approved revision.

Aircraft: PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A), PA-18-135 +14 more

Installation of oil cooler, hoses, and baffles in accordance with Cub Crafters, Inc., Master Drawing List, MDL 103300, Revision A, dated July 2, 1999, and its listed data, or later Federal Aviation Administration approved revision.

Aircraft: PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A), PA-18-135 +14 more

Install engine baffles in accordance with Cub Crafters, Inc. Master Drawing List, MDL103800, Revision B dated August 30, 1999, and its listed data, or later Federal Aviation Administration approved revision.

Aircraft: PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A), PA-18-135 +14 more

Install boot cowling and firewall assembly in accordance with Cub Crafters, Inc. Master Drawing List, MDL105300, Revision A, dated October 26, 1999, and its listed data.

Aircraft: PA-18, PA-18-105 (Special), PA-18-125 (Army L-21A), PA-18-135 +14 more

Modifies the aircraft to remove seats in the economy class. The modification changes the passenger capacity to 12F/129Y. The installation is in accordance with DAS 1 WE Approved United Air Lines Master Document List No. 00558, dated October 12, 1999, or later FAA approved revisions.

Aircraft: 727-200 Series

Modifies the aircraft to remove RECARO seats in economy class. The modification changes the passenger capacity to 24F/158Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00556, dated August 24, 1999, or later FAA approved revisions.

Aircraft: 757-200 Series

Modifies the aircraft to remove RECARO seats in economy class. The modification changes the passenger capacity to 34F/210Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00559, dated November 19, 1999, or later FAA approved revisions.

Aircraft: 767-300 Series

Modifies the aircraft to install Primex Personal Computer (PC) Power System in the First Class Cabin. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00555 dated August 30, 1999, or later FAA approved revisions.

Aircraft: A320-211, A320-212, A320-214, A320-231 +2 more

Modifies the aircraft to remove B/E Aerospace seats in economy class. The modification changes the passenger capacity to 24F/158Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00557, dated August 25, 1999, or later FAA approved revisions.

Aircraft: 757-200 Series

Installation of ribbon heaters on potable water lines located in the lower fwd cargo compartment RH tunnel area to protect from freezing. The installation consists of individual ribbon heaters, thermal protection, circuit breaker and interface wire harness. This modification was accomplished in accordance with United Air Lines DAS-1-WE Approved Master Document List No. 00562 dated December 12, 1999 or later FAA approved revisions.

Aircraft: DC-10-30F (KC-10A)\nKDC-10)

Modifies the aircraft to install an AlliedSignal Flight Data Acquisition Unit, part number 965-0649-004, and status relay, installation of wiring from sensors and autopilot system to the FDAU, installation of wiring from the FDAU to the flight data recorder, installation of a circuit breaker for the new sensors, and re-routing of some existing wiring. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00553 dated August 17, 1999, or later FAA approved revisions.

Aircraft: 737-200 Series

Installation of Upper and Lower Red Anti-collision lighting in accordance with FAA Approved Master Drawing List, Drawing No. BFG-R-349-00, Revision "N/C" Dated November 12, 1999, or later FAA approved revision.

Aircraft: 737-500 Series, 737-400 Series, 737-300 Series, 737-200 Series +1 more

Installation of Instrument Panel in accordance with 1998-54 Installation Manual and Drawings 1998A200, 1998A300, 1998A400, and 1999 all dated July 1, 1977; Battery Box Kit per 1998-84 Installation Manual and Drawing 2000 dated July 1, 1977; Radio Cooling Kit per 1998-86 Installation Manual and Drawing 2002 each dated July 1, 1977.

Aircraft: 35-33, 35-A33, H35, J35 +12 more