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 These could include obsolete systems, lessee-specific modifications, or customer-tailored configurations no longer applicable for the next operator.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.

Recore of AiResearch bleed air precoolers pat numbers 194792-1, 194792-2, 194792-3, and 194792-4, with LORI core assembly part number L8742756-1

Modifies existing Flight Data Acquisition Management System (FDAMS) Flight Recorder frame format database and replaces Oil Pressure indicators

Auxiliary Fuel Tank Removal, Installation of an Engine and APU Fire Detection System, Avionics Components, and new Interior Arrangement

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 EMTEQ Engineering dual GPS Antenna Provisions.Revision 1 transferred from EMTEQ Engineering to B/E Aerospace. EASA.IM.A.S.01016

Installation of Honeywell Ground Proximity Warning System (EGPWS).Revision 1 transferred from EMTEQ Engineering to B/E Aerospace. EASA.IM.A.S.01015 FAA ST02716AT

Recore of Boeing 737 precooler heat exchanger.

Modification to be accomplilshed on repairs of Fan Duct Cowl and Thrust Reverser Assembly.

Installation of Smiths Aerospace WL202EED6 exhaust gas temperature indicator, through modification of a Smiths Aerospace WL202EED4 exhaust gas temperature indicator.