1001

The above boeing model which has incorporated Raisbeck Commercial Air Group Inc Master Drawing List 96B-1001, Revision D, dated September 2, 1997, or later FAA approved revision, complies iwth FAR Part 36, Stage 3 noise limits.

Aircraft: 727-200 Series

Installation of Butterfield Industries Flow Through Anti-Ice Kit Part Number BI 1001-1

Aircraft: 200, 200C, 200CT, 200T +18 more

Installation of Honeywell MK VIII EGPWS Terrain Awareness and Warning System (TAWS) in accordance with Pro Star Aviation Master Document List No. 1001-MDL-01, Rev IR, dated 10/15/01, or later FAA-approved revisions.

Aircraft: 550, 560

Installation of SDI CFS-1000, -1001, or FT-100 fuel flow indicating system system and facet P/N 480543 auxiliary fuel pump.

Aircraft: PA-28-180, PA-28-140, PA-28-150

Installation of SDI CFS-1000, -1001, or FT-100 fuel flow indicating system and facet P/N 480543 auxiliary fuel pump. (172H (USAFT-41A) LANDPLANE ONLY)

Aircraft: 172, 172A, 172B, 172C +10 more

Installation of SDI CFS-1000, CFS-1001, or FT-100 fuel flow indicating system and facet P/N 480543 auxiliary fuel pump. (175C LANDPLANE ONLY)

Aircraft: 175B, 175A, 175, 175C

Installation of SDI CFS-1000, CFS-1001, or FT-100 fuel flow indicating system and facet P/N 480543 auxiliary fuel pump. (170B LANDPLANE ONLY NORMAL CATEGORY)

Aircraft: 170A, 170B

Installation of Dual UNS-1( )w FMS, SCN 1001.X/1101.X/1101.XM

Aircraft: F90

Upgrade of triple Flight Management System (FMS) UNS-1Fw system software to SCN 1001.X

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

Installation of elevator tail cone fairings per Smith Speed Conversions Drawing List No. 1001 stamped FAA Approved on May 17, 1978, or later.

Aircraft: S35, V35, V35A, V35B

Install 170 hp Lycoming O-340-A1A engine and Hartzell HC-82XL-1DB/8433-12 propeller according to Doyn data listed on Engineering Releases 100 (3/22/58), 1010 (3/16/57), 1011 (8/28/57), 1012 (7/15/57), 1014 (3/30/57), 1050 (7/13/57), 1051 (& DCN 1, 12/10/57), 1052 (7/19/57), 1053 (7/19/57), 1099 (3/22/58), and Instructions (2 sheets, undated) Data required for parts manufacture: As listed on Engineering Releases 1001 (1/18/57), 1002 (12/21/57), 1003 (5/1/57), 1004 (7/13/57), 1005 (7/12/57), 1006 (3/30/57), 1007 (4/12/57), 1008 (2/27/57), 1009 (10/23/57), 1015 (2/25/56).

Aircraft: 170B, 170A

Installation of Aero Twin, Inc. CASA 212 Exhaust Deflector, part number AT-CASA-EXDF-1001

Aircraft: C-212-CB, C-212-CC, C-212-CD, C-212-CE +2 more

ONE ONLY STC, SN 1373: Installed two Lycoming GO-480B1D model engines (with dual impulse coupling magnetos both engines and 24 volt alternator charging system) and two Hartzell HC-A3V20-2C/V9333C-3 model propellers. Modified airplane electrical system to a 24 volt system. Removed the left engine driven hydraulic pump and installed a new Oildyne (P/N 645659, 108B1, C25-1V-13-Y) 24 volt electric hydraulic pump and system. Added two Weldon (P/N 8100H) 24 volt electrical fuel boost pumps with fuel bypass system, Added an auxiliary float fuel tank and fuel transfer system. Installed a Whelen PR and PG navigation/strobe light system, a Pulselite model 1210/2405-2A system, two Rosen (P/N 1751200-111) sunvisors, Industrial Labs (P/N AFB-193-10) defrost blower, Guardian AERO-553 Carbon Monoxide (CO) monitor/clock, Electronics International VA-1A-50 volt/ammeter, Kory (P/N 318630-1001-035) landing gear light system , Dusters and Sprayers Supply (P/N 10.00) solid rubber tail wheel and tire assembly, and ACK E-01 Emergency Locator Transmitter (ELT). Installed Cleveland 199-167 wheel and brake conversion kit with associated brake system upgrades. Installed a new .063 thick aluminum cockpit instrument panel. Installed new Oregon Aero (P/N 6A-0058-1) pilot, and co-pilot seats with Pacific Scientific rotary buckle restraint system. Installed Atlee Dodge (P/N 3147) passenger seats with associated seat belts, and new floor seat rails. Removed propeller unfeathering valve, incorporated an auxiliary wing float fuel tank system, and added an enlarged rudder trim tab. All modifications/alterations accomplished

Aircraft: G-44

Installation of Soloy Part No. 250-1001-1 fuel line.

Aircraft: 250-C20, 250-C18, 250-C20B

Vertical Separation Minimum (RVSM) non-group (individual) airworthiness approval of specific Raytheon HS.125-700A aircraft in accordance with Kohlman Systems Research (KSR) Master Drawing List Hawker 700 RVSM, Drawing No. MDL 1001, Rev. A, dated February 18, 2004, or later FAA aApproved revision.

Aircraft: HS.125 Series 700A