# N306GT: 1993 Boeing 737-45D, registration cancelled 2025-12-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 4, 2025 - Status when cancelled: Valid registration - Airframe: [Boeing 737-45D](https://openairdocs.org/model/boeing-737-45d) (registry code 13844B9) - Engine: [CFM International CFM56-3C1](https://openairdocs.org/engine/cfm-international-cfm56-3c1) (registry code 13077) - Serial number: 27157 - Year built: 1993 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 21, 2014 - Certificate issued: February 9, 2019 - Last registry action: July 18, 2023 - Mode S code: A33644 - Owner when cancelled: [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N306GT - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=306GT - Page: https://openairdocs.org/deregistered/N306GT-2025-12-04 From the FAA registry file of November 7, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Boeing 737-45D: https://openairdocs.org/model/boeing-737-45d.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR MASA2023071900094](https://openairdocs.org/sdr/MASA2023071900094), Jul 20, 2023: UNKNOWN. UNKNOWN. CABIN ALTITUDE WARNING - [SDR MASA20210407157](https://openairdocs.org/sdr/MASA20210407157), Mar 30, 2021: FRAME. DAMAGED. FORWARD CARGO COMPARTMENT, REINFORCEMENT FRAMES INSTALLED PER IAI CARGO CONVERSION STA 400+9.000” AND STA 400+13.500” WITH DOUBLE HOLES (2EA). THE FRAMES WERE R - [SDR MASA20210407158](https://openairdocs.org/sdr/MASA20210407158), Mar 21, 2021: ACOUSTIC PANEL. CORRODED. ENGINE #2, INLET COWL RH LWR ACOUSTIC PANEL WITH BULKHEAD BETWEEN 6 AND 7 O’CLOCK POSITION. NOTE: THE AREA WERE REPAIRED PER STS EA 72-2021-007 REV IR(REFE:JOB - [SDR EE4Y201910119892](https://openairdocs.org/sdr/EE4Y201910119892), Oct 11, 2019: FRAME. DAMAGED. UPPER CARGO CABIN AT BS 907 STR 17R LEVEL FRAME NOTCH WITH HOLE ENLONGATE.WAS REPAIRED PER AERONAUTICAL ENGINEERS EO9670 REV P2,REPAIR INSTRUCTIONS (REF:JOB:A1H - [SDR EE4Y201910119891](https://openairdocs.org/sdr/EE4Y201910119891), Oct 11, 2019: SKIN. DAMAGED. FUSELAGE SKIN FROM BS500F+10 TO BS540, BETWEEN S-16LH AND S-19LH WING TO BODY FAIRING AREA, EXTERNAL SURFACE WITH EXISTING BLENDOUT.WAS REPAIRED PER AERONAUTICA - [SDR EE4Y201910029890](https://openairdocs.org/sdr/EE4Y201910029890), Oct 2, 2019: STRINGER. DAMAGED. FWD CARGO COMPARTMENT AT STA 440 STRINGER 21LH WITH DOUBLE HOLE. HE STRINGER WAS REPAIRED PER EO9640 REPAIR INSTRUCTIONS. - [SDR EE4Y201910019889](https://openairdocs.org/sdr/EE4Y201910019889), Oct 1, 2019: SKIN. PUNCTURED. RIGHT ELEVATOR TOP SKIN SURFACE PUNCTURED AT ELEV. STA 30.5. THE ELEVATOR SKIN WAS REPAIRED IAW SERVICE REQUEST ID: 4-4567857880 AND MANUFACTURER REPAIR INSTRUC - [SDR EE4Y201910019887](https://openairdocs.org/sdr/EE4Y201910019887), Oct 1, 2019: SUPPORT FITTING. CRACKED. RH WING RSS 224.14 REAR SPAR UPPER CHORD, MLG SUPPORT BEAM - AFT SUPPORT FITTING OPEN FASTENER HOLE WITH CRACK. NOTE: THE AFT SUPPORT FITTING WAS REPAIRED PER S - [SDR EE4Y2019100109886](https://openairdocs.org/sdr/EE4Y2019100109886), Oct 1, 2019: SPAR. CRACKED. RH WING RSS 224.14 REAR SPAR UPPER CHORD OPEN FASTENER HOLE CRACKED. NOTE: REAR SPAR UPPER CHORD WAS REPAIRED AS PER SRM 57-20-10 REPAIR 4 INSTRUCTIONS. - [SDR EE4Y2018041906384](https://openairdocs.org/sdr/EE4Y2018041906384), Mar 26, 2018: SKIN. CRACKED. DURING THE ACCOMPLISHMENT OF SRM 57-20-10, REPAIR 4, FOUND THE LT WING UPPER SKIN, TWO FASTENER HOLES CRACKED. ONE FASTENER HOLE LOCATED AT FASTENER ROW 1, SPEC - [SDR EE4Y2018041806376](https://openairdocs.org/sdr/EE4Y2018041806376), Mar 24, 2018: ATTACH FITTING. CORRODED. DURING AN INSPECTION OF THE A/C BAY AREA, FOUND AT LT PRIMARY AND SECONDARY HEAT EXCHANGERS AREA, THE ATTACHING FRAME WITH SEVERAL POINTS OF CORROSION. THE DAMA - [SDR EE4Y2018041806375](https://openairdocs.org/sdr/EE4Y2018041806375), Mar 24, 2018: LINK. CORRODED. DURING A STRUCTURAL INSPECTION, THE SWING LINK WAS FOUND CORRODED AROUND ONE OF ITS BORES, THE AFFECTED SWING LINK WAS REPLACED IAW AMM 57-15-00. - [SDR EE4Y2018041906379](https://openairdocs.org/sdr/EE4Y2018041906379), Mar 21, 2018: SKIN. CORRODED. FOUND THE SKIN BETWEEN LBL 45.61 AND LBL 65 AT STRINGER 1C, WITH CORROSION. THE DAMAGED AREA WAS REPAIRED IAW SR 3-4185490079. - [SDR EE4Y2018041906378](https://openairdocs.org/sdr/EE4Y2018041906378), Mar 20, 2018: VERTICAL BEAM. CRACKED. DURING INSPECTION OF THE BS 178 BULKHEAD, FOUND A VERTICAL BEAM CRACKED AT RBL 5.7 AND WBL 181.5. THE DAMAGED VERTICAL BEAM WAS REPAIRED IAW SB 737-53A1225. - [SDR EE4Y2018041806377](https://openairdocs.org/sdr/EE4Y2018041806377), Mar 15, 2018: SUPPORT ANGLE. CORRODED. DURING THE INSPECTION OF THE MAIN LANDING GEAR AREA, IT WAS FOUND AT BS 706, RBL 65 AND WBL 200, THE SUPPORT ANGLE P/N 65-50733-34, VERTICAL FLANGE WITH CORROSI - [SDR EE4Y2018041906383](https://openairdocs.org/sdr/EE4Y2018041906383), Mar 12, 2018: SPAR. DAMAGED. DURING A STRUCTURAL INSPECTION, FOUND THE LT WING, INBD MID FLAP DENTED ON THE NOSE SKIN INBD END, FOUND BEYOND SRM LIMITS. THE DAMAGED SKIN SECTION WAS TRIMMED - [SDR EE4Y2018041806374](https://openairdocs.org/sdr/EE4Y2018041806374), Mar 12, 2018: SKIN. DENTED. DURING A STRUCTURAL INSPECTION, SEVERAL DEFORMATIONS AND DINGS (FROM INSIDE TO OUTSIDE) WERE FOUND AT MCD SURROUNDING AREA, COMMON TO LOWER FRAME SKIN BS 360 TO - [SDR Q2SA20180303390](https://openairdocs.org/sdr/Q2SA20180303390), Mar 3, 2018: WIRE. ARCED. SPARKS FROM OVERHEAD PANEL DURING ROLL-OUT. FOUND ARCING BEHIND DOOR INDICATION PANEL. FOUND DAMAGED WIRING AT D642 AND D1406 D482. REPAIRED THE WIRING IAW WPM - [SDR Q2SA20170707383](https://openairdocs.org/sdr/Q2SA20170707383), Jul 7, 2017: CONTROL VALVE. STUCK. DURING CLIMB OUT PASSING 15000 FT, CABIN ALTITUDE LIGHT ILLUMINATED. PERFORMED QRH PROCEDURE, VERIFIED ALL SWITCHES WERE CORRECT. MX TROUBLESHOT AIRCRAFT BLEED --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.