TEN 845Installation of an auxiliary rack E8-1V that provides provisions forLRUs to be installed in the Electronics and Engineering Bay. The E8-1Vis located between FS 312 - FS 328and LBL 3.75 - LBL 27.4 at WL200. Itis weight limited to hold up to 50 lbs of equipment.

Installation of high temperature, semi-rigid, coaxial fire/overheat detection wire harness cable assemblies in accordance with FAA approved Meggitt Safety Systems 737-600/700/800/900 Simi-Rigid, Engine Fire Cable STC Master Drawing List No. 904629, Revision A, dated July 10, 2003, or a later FAA approved revision.

Relocation of High Frequency Tranceivers 1 and 2 (HF1 and HF2), Cockpit Voice Recorder (CVR), Flight Data Recorder (FDR), and Auxiliary Power Unit Electronic Control Unit (APUECU); and Removal of E6 Electronics Rack.

Conversion of a Boeing 737-700 Increased Gross Weight (IGW) aircraft configuration airplane to an Airborne Early Warning & Control (AEW&C) aircraft configuration in accordance with Boeing Documents D725-10371-5, aircraft serial number (S/N) 33474, Modification Revision Master Drawing List (MDL), dated May 7, 2009; D751-10350-4, aircraft S/N 33962, Modification Revision MDL, dated July 1, 2010; and D772-10427-2, aircraft S/N 34700, Modification Revision MDL, dated July 27, 2011. The modification includes structural changes to support the addition of external antennas and radars, in-flight refueling system, ventral fins for increased stability control, reduced speed envelope, an increase in electrical generation capability from 180 to 360 KVA, a new interior to provide crew operation of the radar systems, avionics in the main deck to support the radar operation, and a crew rest area, an increased in engine thrust, and modification to the flight deck avionics to reflect the new configuration.airplane to an Airborne Early Warning & Control (AEW&C) aircraft configuration

Installation of a Stage 3 hushkit when powered by P&W JT8D-7, JT8D-9, JT8D-15, or JT8D-17 Series Engines.

Installation of thrust reverser short track.