2006

Installation of Flight Deck Manual Stowage Box, in accordance with Aero Consulting Services Modification Data Summary Number B78600, Revision H, dated November 9, 2006, or later TCCA approved revision.

Aircraft: DHC-8-101, DHC-8-102, DHC-8-103, DHC-8-106 +8 more

: Installation of the RDR-4000 Doppler Radar System in accordance with Master Drawing List 756-0174-001, Revision (E), dated August 20, 2006, or later FAA approved revisions.

Aircraft: 340

Installation of an Inlet Barrier Filter (IBF) System in accordance with Aerospace Filtration Systems, Inc. Installation- IBF System, Drawing 111001, Revision A, dated October 20, 2006, and Installation Procedures AFS-BH-210-IBF-IB, Revision B, dated October 20, 2006, or later FAA Approved revision.

Aircraft: 205A-1

Modifies the aircraft to change the material used for the construction of the floor panels in the forward and aft cargo compartments to MC Gill product Gillfab 4321B. The installation is in accordance with DAS-100219-NM United Air Lines Master Document List No.00937, Revision B, dated July 14, 2006, or later FAA approved revisions.

Aircraft: A319-131, A320-232

The modification changes the passenger seating capacity to forty-one passenger seats for the CRAF Aeromedical Evacuation Interior Configuration #1 and forty-five seats for Configuration #2. Modifies the aircraft interior through the removal of specific seats and monuments not required per the final configuration, and rearranges PSU's accordingly. The alteration will install system close outs and two electrical power provisions at the forward bulkhead of the forward cargo compartment. The installation is in accordance with DAS-100219-NM United Air Lines Master Document List No. 00936, Revision D, dated January 26, 2006 or later FAA approved revisions.

Aircraft: 767-300 Series

Installation of a Foreign Object Damage (FOD) Screen or an Inlet Barrier Filter (IBF) System in accordance with Aerospace Filtration Systems, Inc. Drawing 119000, Revision B, dated August 30, 2006, or later FAA approved revision.

Aircraft: A119, AW119 MKII

Reconfiguration from an eight (8) passenger interior to a 14 passenger interior, by installing a four (4) place Divan, a four (4) place Conference Group; and a 2 place conference group. Additionally updating the in flight entertainment systems, also a 20 and a 17 inch liquid crystal display monitors, the addition of a cockpit mounted camera and miscellaneous minor modifications, all installed in accordance with Master Drawing List MD-GIV-3947-01, Revision B, dated 2-1-2006, or later FAA approved revision and maintained per the Instructions for Continued Airworthiness ICA-GIV-3947-01, Revision IR, Dated 12-30-2005, or later FAA accepted revision and operated in accordance with Aircraft Flight Manual Supplement, Document No. FM-GIV-3947-01 dated 2-9-2006 is required.

Aircraft: G-IV

Installation of the Right or Left Passenger Sliding Door Kit in accordance with drawings listed on Aeronautical Accessories, Inc. Drawing List Report AA-01080, Revision H, dated March 8, 2006, or later FAA approved revision and Instillation Instructions Report No. AA-01039, Revision E, dated February 10, 2006 or later FAA approved revision.

Aircraft: 430

Manufacture of crew and passenger emergency push out windows in accordance with Aeronautical Accessories, Inc. Drawing List Report No. AA-97167, Revision E, dated December 22, 2006, and installation in accordance with Aeronautical Accessories, Inc. Report No. AA-97142, Revision D, dated December 22, 2006, or later FAA approved revisions.

Aircraft: 407

Installation of Cabin Interior Modifications and Aircell ST3100 Iridium satellite telephone system in accordance with BaySys Technologies, LLC, Master Data List 8027-MDL, Revision C, dated July 6, 2006.

Aircraft: 727 Series

Installation of Rockwell Collins Tailwind 550 Direct TV system in accordance with BaySys Technologies Master Data List No. 8050-ED-1067,Revision L, dated November 20, 2006, or later FAA approved revisions.

Aircraft: A319-115, A319-133

Installation of seating configurations on upper deck of B747-400 Boeing Converted Special Freighter in accordance with Clipper Aviation, Inc., Master Data List CLI-2006-003, Revision D, dated May 23, 2011.

Aircraft: 747-400 Series

Installation of Apical Industries, Inc. Liferaft Kit in accordance with Apical Industries, Inc., Master Document List MD76-2, Revision E, dated May 19, 2006, or later FAA approved revision, Rotorcraft Flight Manual Supplement, RFMS-76, Revision N/C, FAA approved on June 28, 2006, or later FAA approved revision is required as part of this modification.

Aircraft: S-76A, S-76B, S-76C

Replacement Low or High Skid Tubes and Lightweight Flotation Skid Tubes in accordance with Aeronautical Accessories, Inc. Drawing List Report AA-98007, Revision I, dated July 18, 2006, and installation per Report AA-98006, Revision D, dated March 31, 2003, or per Report AA-99024, Revision F, dated November 29, 2005, or later DAS approved revisions.

Aircraft: 407

Fabrication of Helipod II Slim Line (SL) external cargo pod in accordance with Helipod USA Master Data List No. NW007-HPSL-27-005, revision 2, February 5, 2008, or later FAA-approved revision; and installation of this system in accordance with Helipod USA Installation Drawing HPR44IISL25201, Revision NC, dated May 1, 2006, or later FAA-approved revision. This modification must be maintained in accordance with Helipod USA Instructions for Continued Airworthiness Document No. NW007-HPSL-27-007, revision IR, dated May 1, 2006, or later FAA-approved revision.

Aircraft: R44, R44 II