As part of lease return, phase-out, or aircraft transition processes, removal or reversal of previously installed STCs is often required. These could include obsolete systems, lessee-specific modifications, or customer-tailored configurations no longer applicable for the next operator.

Fokker Services provides certified engineering support for the full demodification process, ensuring compliance, traceability, and airworthiness restoration aligned with the requirements of the new lessee or owner.

Fokker Services offers a minor modification to support the use of Turbonycoil oils (600 or 640) from Nyco (France) for your aircraft's engine, APU, or IDG systems.

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.

Installation in accordance with Transport Canada Civil Aviation (TCCA) approved Phoenix Aero Aviation Engineering Ltd. Master Data List MDL-PA-18-019 Rev. Orig, dated October 5, 2018.

Modify the aircraft interior to match standard passanger configurations, in accordance with AeroDesign Services and Engineering Master Data List Document number ADS252016-MDL-02, Rev. A, dated October 12, 2018, or later FAA approved revisions.