# N305GT: 1997 Boeing 737-4H6, registration cancelled 2025-01-27

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 27, 2025
- Exported to: Brazil
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-4H6](https://openairdocs.org/model/boeing-737-4h6) (registry code 138441A)
- Engine: [CFM International CFM56-3C1](https://openairdocs.org/engine/cfm-international-cfm56-3c1) (registry code 13077)
- Serial number: 27674
- Year built: 1997
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 16, 2014
- Certificate issued: February 12, 2019
- Last registry action: July 18, 2023
- Mode S code: A3328D
- 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/N305GT
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=305GT
- Page: https://openairdocs.org/deregistered/N305GT-2025-01-27

From the FAA registry file of November 5, 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 737-4H6: https://openairdocs.org/model/boeing-737-4h6.md

## Service difficulty reports (48)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR MASA2021072000162](https://openairdocs.org/sdr/MASA2021072000162), Jul 20, 2021: SWITCH. UNSECURE. UNABLE TO TURN OFF EMERGENCY LIGHTS - MX RESECURED PILOTS OVHD PANEL EMER EXIT SW. OPS CK NORMAL. STS MX
- [SDR EE4Y2020090721598](https://openairdocs.org/sdr/EE4Y2020090721598), Sep 7, 2020: SKIN. DENTED. DURING ROUTINE MAINTENANCE AT MAINTENANCE FACILITY, THE LOWER FUSELAGE EXTERNAL SKIN JUST BELOW THE SERVICE DOOR, AT BS 301.5, BETWEEN STR-17 R AND STR-18 R WAS
- [SDR EE4Y2020090711597](https://openairdocs.org/sdr/EE4Y2020090711597), Sep 7, 2020: SKIN. DENTED. DURING ROUTINE MAINTENANCE AT THE COOPESA MAINTENANCE FACILITY IN SAN JOSE, COSTA RICA (SJO), THE FUSELAGE SKIN BETWEEN STA 498 AND STA 502 AND BETWEEN S-21R AN
- [SDR EE4Y2020090711596](https://openairdocs.org/sdr/EE4Y2020090711596), Sep 7, 2020: KEELBEAM. CORRODED. DURING ROUTINE MAINTENANCE AT THE COOPESA MAINTENANCE FACILITY IN SAN JOSE, COSTA RICA (SJO), THE KEEL BEAM STRAP BETWEEN STA 630 AND STA 646 WAS FOUND TO HAVE 
- [SDR EE4Y2020090711595](https://openairdocs.org/sdr/EE4Y2020090711595), Sep 7, 2020: SKIN. DENTED. DURING MAINTENANCE VISIT, A DENT WAS NOTED ON THE FUSELAGE SKIN AT STA. 345.5, ABOVE STR. 20R. THE DENT WAS OUT OF LIMITS PER 737-400 SRM. THE DAMAGE WAS REPAIR
- [SDR EE4Y2020090701594](https://openairdocs.org/sdr/EE4Y2020090701594), Sep 7, 2020: WEB. CORRODED. DURING SCHEDULED MAINTENANCE AT THE COOPESA MAINTENANCE FACILITY IN SAN JOSE, COSTA RICA (SJO), THE WING CENTER SECTION FRONT SPAR WEB AT BS 540.00 AND LBL 8 WA
- [SDR EE4Y2020090711586](https://openairdocs.org/sdr/EE4Y2020090711586), Sep 7, 2020: SKIN. CRACKED. DURING SCHEDULED MAINTENANCE AT COOPESA FACILITY IN SAN JOSE, COSTA RICA (SJO), THE FUSELAGE SKIN BETWEEN STA 827 AND STA 847 AND BETWEEN STGR-1 AND STGR-2L UND
- [SDR Q2SA20190325415](https://openairdocs.org/sdr/Q2SA20190325415), Mar 25, 2019: CONTROL PANEL. FAILED. AIRCRAFT GROUNDED. MCP, AUTOPILOT AND FLIGHT DIRECTOR FAILED IN FLIGHT ON CLIMB OUT. REPLACED MCP IAW AMM 22-11-34. OPS CK NORMAL. (LP 71462 ITEM 2) REF LP 7146
- [SDR EE4Y2019032208467](https://openairdocs.org/sdr/EE4Y2019032208467), Mar 22, 2019: SKIN. DENTED. DURING THE STRUCTURE INSPECTION, IT WAS FOUND AT ENGINE NR 1 NOSE COWL LIP SKIN WITH DENS AT 8 O'CLOCK AND 11 O'CLOCK POSITION. THE DAMAGED AREAS WERE REPAIRED 
- [SDR EE4Y2019032208466](https://openairdocs.org/sdr/EE4Y2019032208466), Mar 22, 2019: SKIN. CORRODED. DURING THE STRUCTURE INSPECTION, IT WAS FOUND AT LOWER FUSELAGE SKIN WITH CORROSION AT BS 648 BETWEEN STRINGER 28R AND 28L, DME2 ANTENNA AREA. THE DAMAGED AREA 
- [SDR EE4Y2019032208495](https://openairdocs.org/sdr/EE4Y2019032208495), Mar 22, 2019: FLOOR SUPPORT. CORRODED. DURING THE STRUCTURE INSPECTION, IT WAS FOUND AT AFT CARGO COMPARTMENT FLOOR SUPPORT ZEE WITH CORROSION FROM BS 727 TO BS 947, STRINGER 26L. THE DAMAGED PART WA
- [SDR EE4Y2019032208485](https://openairdocs.org/sdr/EE4Y2019032208485), Mar 22, 2019: FRAME. CORRODED. DURING THE STRUCTURE INSPECTION, IT WAS FOUND AT AFT CARGO COMPARTMENT FRAME WITH CORROSION AT BS 727F BETWEEN STRINGER 26R AND 26L. THE DAMAGED PART WAS REPAIR
- [SDR EE4Y2019032108470](https://openairdocs.org/sdr/EE4Y2019032108470), Mar 21, 2019: DOOR SILL. CRACKED. UPPER FUSELAGE CARGO CABIN BS 294.5, STR-17R, LOWER MAIL SILL WEB CRACKED. THE MENTIONED PART WAS REPLACED IAW EO3753A008 REV. 1 DATED 17 SEP 2018 AND SB 737-53
- [SDR EE4Y2019032108472](https://openairdocs.org/sdr/EE4Y2019032108472), Mar 21, 2019: INTERCOSTAL. CRACKED. UPPPER FUSELAGE CARGO CABIN STR-8AR, BETWEEN BS 332.1 AND BS 344 INTERCOSTAL T-CHORD CRACKED. THE MENTIONED T-CHORD WAS REPLACED IAW AIR EO3753A37 DATED MAR 01,
- [SDR EE4Y2019032108479](https://openairdocs.org/sdr/EE4Y2019032108479), Mar 21, 2019: FITTING. CORRODED. AFT CARGO COMPARTMENT FRAME ATTACH CLIP WITH CORROSION AT BS 787 STR-26R. THE MNETIONED CLIP WAS REPLACED AS PER SRM 51-10-02 PARAG. 8.
- [SDR EE4Y2019032108478](https://openairdocs.org/sdr/EE4Y2019032108478), Mar 21, 2019: FITTING. CORRODED. AFT CARGO COMPARTMENT CLIP WITH CORROSION AT BS 787 STR-27R. THE MENTIONED CLIP WAS REPLACED AS PER SRM 51-10-02 PARAG. 8.
- [SDR EE4Y2019032108477](https://openairdocs.org/sdr/EE4Y2019032108477), Mar 21, 2019: FRAME. CORRODED. AFT CARGO COMPARTMENT FRAME WITH CORROSION AT BS 787 BETWEEN STR-26L AND 27L. FRAME SECTION WAS REPLACED BY NEW ONE AS PER SRM 51-10-02 PARG. 8.
- [SDR EE4Y2019032108471](https://openairdocs.org/sdr/EE4Y2019032108471), Mar 21, 2019: BULKHEAD. CANNING. LOWER FUSELAGE BS 1016 AFT PRESSURE BULKHEAD WEB, FROM THE AFT SIDE OF BULHEAD AT LEVEL OF STR-8L WEB WITH OIL CANNING. THE WEB WAS REPAIRED AS PER SRM 53-80-08
- [SDR EE4Y2019032108473](https://openairdocs.org/sdr/EE4Y2019032108473), Mar 21, 2019: SUPPORT FITTING. CRACKED. AFT CARGO COMPARTMENT FRAME SUPPORT CLIP WITH CRACK AT BS 787 STR-26L. THE MENTIONED PART WAS REPLACED BY A NEW ONE AS PER SRM 51-10-02 PARAG 8.
- [SDR EE4Y2019032108474](https://openairdocs.org/sdr/EE4Y2019032108474), Mar 21, 2019: FRAME. CRACKED. MAIN CARGO COMPARTMENT BS 616 WL 201 RBL 64 FRAME WITH CRACK. PERFORMED REPAIR FRAME AT BS 616 WL 201 RBL64 IAW SB 737-53A1254 SECTION 3B6 PART 6 FIG. 20, 21 AN
- [SDR EE4Y2019032108476](https://openairdocs.org/sdr/EE4Y2019032108476), Mar 21, 2019: FRAME. CORRODED. AFT CARGO COMPARTMENT FRAME WITH CORROSION AT BS 807 BETWEEN STR-25L AND 27R. THE MENTIONED FRAME WAS REPAIRED AS PER SRM 53-00-07 FIG. 202 REPAIR 17 DETAIL V.
- [SDR EE4Y2019032108468](https://openairdocs.org/sdr/EE4Y2019032108468), Mar 21, 2019: WEB. CORRODED. AFT CARGO COMPARMENT WEB WITH CORROSION FROM BS 794 AND BS 847 AT SCUFF PLATE AREA. THE MENTIONES WEB WAS REPLACED BY A NEW ONE AS PER SRM 51-10-02 PARG. 8
- [SDR EE4Y2019032108475](https://openairdocs.org/sdr/EE4Y2019032108475), Mar 21, 2019: SUPPORT FITTING. CORRODED. AFT CARGO COMPARTMENT FRAME SUPPORT CLIP WITH CORROSION AT BS 807, STR-27R, THE MENTIONES CLIP WAS REPLACED BY A NEW ONE AS PER SRM 51-10-02 PARAG 8
- [SDR EE4Y2019032108481](https://openairdocs.org/sdr/EE4Y2019032108481), Mar 21, 2019: SUPPORT ANGLE. CORRODED. AFT CARGO COMPARTMENT FRAME SUPPORT ANGLE WITH CORROSION AT BS 807 ON STR-27L. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02 PARG. 8
- [SDR EE4Y2019032108469](https://openairdocs.org/sdr/EE4Y2019032108469), Mar 21, 2019: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT FLOOR SUPPOR ANGLE WITH CORROSION AT BS 947.5 BETWEEN STR-26L AND 26R. THE DAMAGED PART WAS REPLACED IAW SRM 51-10-02 PARAG 8.
- [SDR EE4Y2017090304254](https://openairdocs.org/sdr/EE4Y2017090304254), Aug 28, 2017: STRINGER CLIP. CRACKED. DURING A STRUCTURAL INSPECTION, FOUND THE STRINGER CLIP AT BS 360, STRINGER 10L, CRACKED. THE STRINGER CLIP WAS REPLACED IAW SRM 51-10-02, PARAGRAPH 8.
- [SDR EE4Y2017090304261](https://openairdocs.org/sdr/EE4Y2017090304261), Aug 27, 2017: FITTING. DAMAGED. DURING THE STRUCTURAL INSPECTION AT THE UPPER FUSELAGE MAIN CARGO CABIN, IT WAS FOUND AT BS 927 STR 17RH, THE FRAME ATTACH FITTING WITH FASTENER HOLE WITH BROKE
- [SDR EE4Y2017090304260](https://openairdocs.org/sdr/EE4Y2017090304260), Aug 27, 2017: WEB. CORRODED. DURING A STRUCTURAL INSPECTION AT THE LT MAIN WHEEL WELL, FOUND SIDE WEB CORRODED, BS 695 - 706, STRINGER 18AL. THE WEB WAS REPLACED IAW SRM 51-10-02, PARAGRAPH
- [SDR EE4Y2017090304253](https://openairdocs.org/sdr/EE4Y2017090304253), Aug 27, 2017: FITTING. CORRODED. DURING THE STRUCTURAL INSPECTION IN THE FWD CARGO BAY AREA, FOUND AT BS 540, THE STRINGER 27L WITH THE END FITTING CORRODED. THE DAMAGED END FITTING WAS REPLACE
- [SDR EE4Y2017090104228](https://openairdocs.org/sdr/EE4Y2017090104228), Aug 27, 2017: SHEAR WEB. CRACKED. DURING A STRUCTURAL INSPECTION, FOUND BS 348.2, BETWEEN STRINGERS 16L AND 17L SHEAR WEB CRACKED. THE SHEAR WEB WAS REPLACED IAW SB737-53A1240, WORK INSTRUCTIONS
- [SDR EE4Y2017090104227](https://openairdocs.org/sdr/EE4Y2017090104227), Aug 27, 2017: ATTACH ANGLE. CRACKED. DURING A STRUCTURAL INSPECTION, FOUND BS 348.2, STRINGER 15L, AN INTERNAL ATTACH ANGLE FOUND CRACKED. THE ATTACH ANGLE WAS REPLACED IAW SB 737-53A1240, WORK INS
- [SDR EE4Y2017090104226](https://openairdocs.org/sdr/EE4Y2017090104226), Aug 27, 2017: FRAME. CRACKED. DURING A STRUCTURAL INSPECTION, FOUND THE BS 348.2FRAME CRACKED AT STRINGER 15L, THE FRAME SECTION WAS REPLACED IAW SB 737-53A1240, WORK INSTRUCTIONS PART 4A, R
- [SDR EE4Y2017083104206](https://openairdocs.org/sdr/EE4Y2017083104206), Aug 27, 2017: FRAME. CRACKED. DURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 500F FRAME WEB WAS FOUND WITH CRACK BETWEEN STR 8L AND STR 9L, SPECIFICALLY AT AC SUPPORT ATTACH BRACKET
- [SDR EE4Y2017083004198](https://openairdocs.org/sdr/EE4Y2017083004198), Aug 27, 2017: FRAME. CORRODED. DURING THE STRUCTURAL INSPECTION AT AIR CONDITION DISTRIBUTION BAY, IT WAS REPORTED AT BS 520 THE FRAME SECTION BETWEEN STRINGERS 27L AND 28L CORRODED. THE DAMA
- [SDR EE4Y2017090304259](https://openairdocs.org/sdr/EE4Y2017090304259), Aug 26, 2017: CHANNEL. CORRODED. DURING THE STRUCTURAL INSPECTION AT THE LOWER FUSELAGE WATER WASTE PANEL AREA, FOUND THE INNER SIDE CHANNEL CORRODED BETWEEN BS 986 - 1006, STRINGERS 25 - 26R. 
- [SDR EE4Y2017083104207](https://openairdocs.org/sdr/EE4Y2017083104207), Aug 26, 2017: FRAME. CRACKED. DURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 727B FRAME WEB WAS FOUND WITH CRACK BETWEEN STRINGERS 8R AND 9R, SPECIFICALLY AT AC SUPPORT ATTACH BRACK
- [SDR EE4Y2017083104200](https://openairdocs.org/sdr/EE4Y2017083104200), Aug 26, 2017: FRAME. CRACKED. DURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 500A FRAME WEB WAS FOUND WITH CRACK BETWEEN STRINGERS 8R AND 9R, SPECIFICALLY AT AC SUPPORT ATTACH BRACK
- [SDR EE4Y2017090104229](https://openairdocs.org/sdr/EE4Y2017090104229), Aug 23, 2017: BEAM. CRACKED. DURING THE STRUCTURAL INSPECTION, FOUND AT BS 178 RBL 71.1 WBL 226 - 231 THE VERTICAL BEAM WEB CRACKED, THE BEAM WAS REPAIRED IAW SRM 53-10-08, FIG 201, REPAIR 
- [SDR EE4Y201708314210](https://openairdocs.org/sdr/EE4Y201708314210), Aug 23, 2017: FRAME. CRACKED. DURING THE STRUCTURAL INSPECTION AT CARGO CABIN, THE BS 727B FRAME WEB WAS FOUND WITH CRACK BETWEEN STRINGERS 8L AND 9L. THE DAMAGE WAS REPAIRED IAW SB737-53-12
- [SDR EE4Y2017090304255](https://openairdocs.org/sdr/EE4Y2017090304255), Aug 20, 2017: SPAR WEB. DAMAGED. DURING A STRUCTURAL INSPECTION AT THE RT WING REAR SPAR WEB, FOUND TWO FASTENER HOLES ELONGATED AT RSS 206.11 AND RSS 273. THE ELONGATED FASTENER HOLES WERE REP
- [SDR EE4Y2017082204133](https://openairdocs.org/sdr/EE4Y2017082204133), Aug 19, 2017: FRAME. DAMAGED. DURING THE STRUCTURAL INSPECTION, BS 907 FRAME, STRINGER 17L AND 17R, FOUND SEVERAL FASTENER HOLES DAMAGED, THE FRAME AND ATTACHING PARTS WERE REPAIRED IAW EO 5
- [SDR EE4Y2017082204076](https://openairdocs.org/sdr/EE4Y2017082204076), Aug 19, 2017: FRAME. CRACKED. DURING THE INSPECTION ACCOMPLISHMENT PER EAM3353009-1 REV NR 3 RELATED WITH AD2016-11-04, IT WAS FOUND AT THE LOWER FUSELAGE FWD CARGO COMPARTMENT. STA500G, BET
- [SDR EE4Y2017082204079](https://openairdocs.org/sdr/EE4Y2017082204079), Aug 18, 2017: FRAME. CRACKED. DURING THE STRUCTURAL INSPECTION OF THE UPPER FWD FUSELAGE IT WAS FOUND AT BS 178 WL 207 THE BULKHEAD LH SIDE CHORD WITH CRACK. THE AFFECTED CHORD HAS BEEN REPL
- [SDR EE4Y2017082204077](https://openairdocs.org/sdr/EE4Y2017082204077), Aug 18, 2017: SKIN. CANNING. DURING THE STRUCTURAL INSPECTION OF THE UPPER REAR FUSELAGE IT WAS FOUND THE FUSELAGE SKIN WITH AN OIL CAN AT BS 1006 3 INCH BELOW STRG 16L. THE AFFECTED SKIN A
- [SDR EE4Y2017082204134](https://openairdocs.org/sdr/EE4Y2017082204134), Aug 10, 2017: SKIN. CRACKED. DURING INSPECTION, THERE WERE FIVE CRACKS FOUND IN THE UPPER SKIN, T/E AREA BETWEEN RSS 238 AND 267, THE RT WING UPPER SKIN WAS REPAIRED IAW SRM 57-20-01, REPAI
- [SDR EE4Y2017082204081](https://openairdocs.org/sdr/EE4Y2017082204081), Aug 5, 2017: SKIN. CRACKED. DURING INSPECTION, OF THE LT REAR SPAR UPPER CHORD, THERE WERE FOUND THREE CRACKS AT UPPER SKIN T/E AREA, THE AFFECTED LT WING UPPER SKIN AREA WAS REPAIRED.
- [SDR EE4Y2017082204082](https://openairdocs.org/sdr/EE4Y2017082204082), Aug 1, 2017: SPAR. CRACKED. DURING THE STRUCTURAL INSPECTION, THE RT WING REAR SPAR WEB AND UPPER CHORD WERE FOUND WITH A CRACK AT RSS 224. THE AFFECTED WEB AND UPPER CHORD SECTIONS WERE R
- [SDR EE4Y2017082204080](https://openairdocs.org/sdr/EE4Y2017082204080), Aug 1, 2017: SPAR. CRACKED. DURING THE STRUCTURAL INSPECTION THE LT WING REAR SPAR UPPER CHORD WAS FOUND CRACKED AT RSS 223, THE AFFECTED SPAR SECTION WAS REPAIRED IAW SRM 57-20-10, REPAIR

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20201229018709I](https://openairdocs.org/incident/20201229018709I), Dec 29, 2020: Boeing 737-4H6 (N305GT), Omaha, NE, No damage. ? CA is a current B737 line check airman ? Both CA and fo have low time in type at 160 and 40 hours respectively ? But highly experienced aviators otherwise. ?…

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