2008

Installation of Pratt & Whitney Canada PT6C-67D, engine in accordance with DynCorp International Master Drawing List Report Number D1H-MDL-100, Revision IR, dated \nApril 17, 2007, or later FAA approved revision. DynCorp International Rotorcraft Flight Manual Supplement (RFMS) Report Number DIER-0012, Revision 0, dated \nJanuary 17, 2008, or later FAA approved revision, is required. Instructions for Continued Airworthiness (ICAs) DIER-0003, Revision 1, dated August 30, 2007, or later revision is required. Airworthiness Limitations section of ICA DIER-0003, approved on August 30, 2007 or later approved revision is required.

Aircraft: UH-1H

Installation of the ELDEC Battery Charger Part number 81-025-01 per Master Data List MDLST 81-025-01, Revision C, Release Date September 10, 2008 or later Federal Aviation Administration Approved Revisions.

Aircraft: CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701) +3 more

Installation of a Honeywell HD-710 High Speed Data Receiver, EMS AMT-50 High Gain Antenna System, and EMS CNX-200 Cabin Network Router in accordance with Pro Star Aviation Master Document List 20674-MDL-02, Revision D, dated March 17, 2008, or later FAA-approved revision.

Aircraft: BD-100-1A10

Installation of Structural and Electrical provisions for a Panasonic in-flight entertainment (IFE) television (TV) monitor into a B747-400 crew rest compartment in accordance with TAECO GA Aviation Services LLC Master Drawing List MDL251BC0001, Revision P, dated June 26, 2008, or later Federal Aviation Administration (FAA) approved revision.

Aircraft: 747-400 Series

Installation of an Executive Interior in accordance with Associated Air Center (AAC) Master Document List, Document Number R137-000, Revision H, dated December 3, 2010, or later FAA/ODA approved revision. Airplane Flight Manual Supplement, Document Number R137-011, Rev. A, dated August 14, 2008, or later FAA/ODA approved revision is required.

Aircraft: 737-700 Series

Installation of a Honeywell FMZ-2000 Flight Management System Upgrade with 6.1 Software in accordance with STC Required Document List (RDL) No. 230-2008 Revision 2 dated May 19, 2011, or later FAA approved revision. Use of FAA approved Airplane Flight Manual Supplement, No. 230-3008 Revision 1, dated May 20, 2011, or later FAA approved revision is required.

Aircraft: BAe.125 Series 800A, BAe.125 Series 800A (C-29A), BAe.125 Series 800A (U-125), Hawker 800 +1 more

Installation of the MECHANICAL SPECIALTIES, Model # UH606 in accordance with document # UH606-100-ICAW paragraph 6, Revision A, dated November 09, 2008, or later FAA approved revision. Manufactured in accordance with Master Document list MDL-205-60-111, Revision A, dated April 9, 2009, or later FAA approved revision. Maintained in accordance with document # UH606-100-ICAW Revision A, dated November 09, 2008, or later FAA approved revision.

Aircraft: 204B, 205A-1, 212, 412 +1 more

Installation of a galley per Indianapolis Jet Center Drawing List DL5008-01, Rev. IR, dated October 17, 2008 or later FAA approved revision.

Aircraft: CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R), CL-600-2B16 (CL-604)

Installation of Powertech Electronic Powered Window Shades in accordance with Aerospace Technologies Group (ATG) Engineering Drawing List LIEDL30001, Revision A, Dated October 20, 2008, or later FAA approved revision.

Aircraft: 757-200 Series, 757-200CB Series, 757-200PF Series, 757-300 Series

Interior Modifications in accordance with BaySys Technologies, LLC Master Data List 8119-MDL, Revision D, dated June 19, 2008, or later FAA approved revision.

Aircraft: 737-700 Series

1. Installation of Cabin Systems Upgrades in accordance with BaySys Technologies, LLC, Master Data List Number 8165-MDL, Revision C, dated April 29, 2008.\n2. BaySys Technologies Airplane Flight Manual Supplement Document Number 8165-AFMS, Revision IR, dated May 16, 2008, is required for this installation.\n3. The following BaySys Technologies Maintenance Instructions are required for this installation:\na. Instructions for Continued Airworthiness Document Number 8165-ICAW, Revision A, dated March 20, 2008.\nb. Maintenance Manual Supplement Document Number 8165-MMS, Revision IR, dated March 5, 2008.

Aircraft: 747SP Series

Installation of a Tail Boom Antenna Mount Kit in accordance with FAA approved Meeker Aviation MDL for VHF Communication Antenna Mount Kit, AA-TBA-010, Revision IR, dated January 15, 2008 or later FAA approved revision.

Aircraft: 407

Installation of a Dual SAGEM Attitude and Heading Reference System, in accordance with Gulfstream Index List CE211138005, Rev. , dated October 17, 2008 or later FAA approved revision. FAA approved Flight Manual Supplement CE21113M000, Rev. None, dated October 17, 2008 or later FAA approved revision is required.

Aircraft: G-1159, G-1159B

Installation of the Cessna 182D cowling (upper cowling P/N 0752031-27, lower cowling P/N 0752031-28) with cowl flaps and cowl flap mechanism in accordance with Tom P. O Reilly s Installation Manual, Rev. Orig., Dated 11/7/2008, FAA approved on 2/25/2011 or later FAA approved revision.

Aircraft: 182A

Installation of reduced-weight skid tubes for high skid landing gear in accordance with Master Drawing List AA-07045 Rev. A dated October 2, 2008, or later FAA approved revision.

Aircraft: 206L, 206L-1, 206L-3, 206L-4