2002

Installation of mounting hardware in accordance with Paravion Technology Master Drawing List DL-407LS-100, Revision N/C, dated April 01, 2002, FAA approved dated January 27, 2003 or later FAA approved revision, and approval for the aircraft to be operated by a single pilot from the left crew seat.

Aircraft: 407

Installation of OuterLink CP-2 SATCOM System in accordance with DECA Modification Summary MS01147-01, Revision 2, dated November 1, 2002.

Aircraft: 200, 200C, 200CT, 200T +20 more

Modification of main rotor blade part number 61170-20201 in accordance with Master Drawing List RR 9633-08, Revision A, dated September 17, 2002, or later FAA approved revision. Retirement life for the modified main rotor blade, part number RR-61170-20201 is 21,200 total time in service.

Aircraft: SH-3H, SH-3A, S-61L, S-61N +2 more

Installation of the Enhanced Ground Proximity Warning System in accordance with Honeywell, Master Drawing List 960-0524-001, Revision -, dated February 5, 2002, or later Federal Aviation Administration (FAA) approved revisions.

Aircraft: AS350BA

Installation of a third seat, removable cross member, and reinforced baggage compartment floor per Cub Crafters Master Document List 123600-1, Revision N/C, dated December 4, 2002, or later Federal Aviation Administration approved revision.

Aircraft: PA-18-135, PA-18-150, PA-18A-135, PA-18A-150

Install windows in accordance with Cub Crafters Master Drawing List CR102500-3, dated July 24, 2002, or later Federal Aviation Administration approved revisions. Since there are no special instructions for continued airworthiness required, Title 14 Code of Federal Regulation part 43 is considered adequate for the maintenance of the installation.

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

Metalize bottom of fuselage per Cub Crafters Master Drawing List (MDL) "Metal Fuselage Bottom for PA-18 Series Aircraft," Revision A, dated September 25, 2002, or later Federal Aviation Administration approved revision.

Aircraft: PA-18A

Installation of Goodyear Tundra 26 x 10.5 x 6 (6 ply), or 8:50 x 6 Tires and Tubes in accordance with Cub Crafters, Inc. Master Drawing List, MDL104200, Revision C, dated January 21, 2002, or later Federal Aviation Administration (FAA) approved revision.

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

Modifies the aircraft to incorporate the Honeywell Enhanced Ground Proximity Warning System. The original STC installation is for the 767-300 series model in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00551 dated November 6, 1998, or later FAA approved revisions. This amendment adds the 767-222 model in accordance with DAS-100219-NM approved Master Document List No. 00551, Revision D, approved September 25, 2002, or later FAA approved revisions. United Air Lines Airplane Flight Manual (AFM) Supplement dated November 9, 1998, or later approved revision to FAA Approved AFM No. D6T11320.322 is required for the 767-322 STC modification. United Air Lines AFM Supplement dated September 25, 2002, or later approved revisions to FAA approved Flight Manual No. D6T11320.222 is required for the 767-222 STC modification. This amendment also clarifies the model of the 767-300 series to specifically the 767-322.

Aircraft: 767-300 Series, 767-200 Series

Installation of main rotor blade grip with modified root radius and matching adapter in accordance with Helicopter Tech, Inc., Drawing List R47-120-252-1000, Revision IR, dated May 15, 2002, or later Federal Aviation Administration (FAA) approved revision.

Aircraft: 47J, 47J-2, 47J-2A, 47G-2A +9 more

Installation of a shutoff valve assembly in accordance with Kaiser ElectroPrecision Master Drawing List MDL 0094-0070, Revision A, dated August 22, 2002, or later FAA approved revisions.

Aircraft: A320-232, A319-131

Installation of MASS Systems fire extinguisher cartridges as replacements for W. Kidde Aerospace/L Hotellier/Dexaero fire extinguisher cartridges in fire extinguisher bottles installed in the rotorcraft models noted on the FAA Approved Model List SR01343LA dated June 28, 2002, or later FAA approved revisions. This cartridge is in accordance with MASS Systems Master Drawing List MDL-861345, Revision N/C, dated May 31, 2002, or later FAA approved revisions.

Aircraft: Falcon 900EX, Mystere-Falcon 50, Mystere-Falcon 900, FALCON 2000 +16 more

Installation of Dual Rockwell Collins VHF-422C (8.33 Khz) Capable VHF-AM Radio in accordance with Field Aviation East Limited Master Drawing and Data List DDL-1098 Revision IR approved December 20, 2002 or later Transport Canada approved revision.

Aircraft: CL-600-2B19 (Regional Jet Series 100)

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

Installation of Internal Load Attaching Means (ILAM) in accordance with Heli-Support, Inc. Master Document List (MDL) No. 123-000, Revision C, dated April 12, 2002, or later FAA approved revision. Rotorcraft Flight Manual Supplement No. 123-121, Revision A, dated April 12, 2002, or later FAA approved revisions required as part of these modifications.

Aircraft: AS-350D, AS-350D1, AS-350B2, AS-350C +4 more