N305GT, cancelled Jan 27, 2025
Service difficulty reports · 48
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N305GT' AND deregistration_id = 'N305GT-2025-01-27' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N305GT' AND deregistration_id = 'N305GT-2025-01-27' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MASA2021072000162Switch · unsecureUNABLE TO TURN OFF EMERGENCY LIGHTS - MX RESECURED PILOTS OVHD PANEL EMER EXIT SW. OPS CK NORMAL. STS MXSDR EE4Y2020090721598Skin · dentedDURING 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 FOUND TO HAVE A SHALLOW DENT.SDR EE4Y2020090711597Skin · dentedDURING 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 AND S-25R WAS FOUND TO HAVE 3 EA. DENTS. REPAIRED PER ENGINEERING AUTHORIZATION Nº 72-2020-179 AND DOCSDR EE4Y2020090711596Keelbeam · corrodedDURING 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 CORROSION. WAS REPAIRED PER ENGINEERING AUTHORIZATION Nº 72-2020-181 UNDER JOB: A1J170 NRI 1-61.SDR EE4Y2020090711595Skin · dentedDURING 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 REPAIRED PER ENGINEERING AUTHORIZATION Nº 20-2020-028 AND DOCUMENTED UNDER JOB: A1J170 NRI 1-32.SDR EE4Y2020090701594Web · corrodedDURING 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 WAS FOUND TO HAVE CORROSION DAMAGE. WAS REPAIRED PER ENGINEERING AUTHORIZATION Nº 32-2020-118 AND DOCSDR EE4Y2020090711586Skin · crackedDURING 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 UNDER THE ELT ANTENNA WAS FOUND WITH OIL CANNING AND CRACK DAMAGE. THE DAMAGE WAS REPAIRED PER ENGINEESDR Q2SA20190325415Control Panel · failedAIRCRAFT 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 71462 ITEM #1 - AUTOPILOT FAIL INFLIGH . CHANGE FCC B PRECAUTIONARY PER MX CTL. R & R FCC B REF AMM 22-1SDR EE4Y2019032208467Skin · dentedDURING 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 IAW SRM 54-10-01 FIGURE 201 REPAIR 1 DETAIL II.SDR EE4Y2019032208466Skin · corrodedDURING 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 WAS REPAIRED PER INSTRUCTIONS PROVIDED ON SR 4-4392840368 AND APPROVED UNDER FAA FORM 8100-9 PROVIDESDR EE4Y2019032208495Floor Support · corrodedDURING 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 WAS REPAIRED IAW SRM 53-60-53 FIGURE 201 REPAIR 4 FROM ZEE FROM BS 787 TO BS 947 AT STR 26L, THE OTHERSDR EE4Y2019032208485Frame · corrodedDURING 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 REPAIRED IAW SRM 53-00-07 FIGURE 202 REPAIR 17 DETAIL IV.SDR EE4Y2019032108470Door Sill · crackedUPPER 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 737-53A1241 R1 DATED NOV 06, 2013.SDR EE4Y2019032108472Intercostal · crackedUPPPER 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, 2017, PART 1 STEP 4 AND 5 AND SB 737-53A1108 REV. 7 DATED JULY 07, 2017 PART 4 STEP 5 AND 6.SDR EE4Y2019032108479Fitting · corrodedAFT 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 EE4Y2019032108478Fitting · corrodedAFT CARGO COMPARTMENT CLIP WITH CORROSION AT BS 787 STR-27R. THE MENTIONED CLIP WAS REPLACED AS PER SRM 51-10-02 PARAG. 8.SDR EE4Y2019032108477Frame · corrodedAFT 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 EE4Y2019032108471Bulkhead · canningLOWER 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 FIG. 203 REPAIR 12.SDR EE4Y2019032108473Support Fitting · crackedAFT 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 EE4Y2019032108474Frame · crackedMAIN 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 AND 22 REV. 2 FEB 22, 2012SDR EE4Y2019032108476Frame · corrodedAFT 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 EE4Y2019032108468Web · corrodedAFT 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. 8SDR EE4Y2019032108475Support Fitting · corrodedAFT 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 8SDR EE4Y2019032108481Support Angle · corrodedAFT CARGO COMPARTMENT FRAME SUPPORT ANGLE WITH CORROSION AT BS 807 ON STR-27L. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-10-02 PARG. 8SDR EE4Y2019032108469Floor Support · corrodedAFT 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 EE4Y2017090304254Stringer Clip · crackedDURING 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 EE4Y2017090304261Fitting · damagedDURING 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 BROKEN SCREW. THE AFFECTED FRAME ATTACH FITTING WAS REPAIRED AS PER AEI E.O.5332 AND APPROVED UNDER FAA 8SDR EE4Y2017090304260Web · corrodedDURING 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 8, DRAWINGS 69-78163, AND 65-46877.SDR EE4Y2017090304253Fitting · corrodedDURING 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 REPLACED IAW SRM 51-10-02, PARAGRAPH 8.SDR EE4Y2017090104228Shear Web · crackedDURING 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, PART 4, PARAGRAPH F, REV 1, AND EAM3353020-4, SECTION 6.SDR EE4Y2017090104227Attach Angle · crackedDURING 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 INSTRUCTIONS, PART 4, PARAGRAPH C, REV. 1 AND EAM 3553020-4, SECTION 3.SDR EE4Y2017090104226Frame · crackedDURING 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, REV 1, AND EAM 3553020-4, SECTION 1.SDR EE4Y2017083104206Frame · crackedDURING 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. MENTIONED DAMAGE WAS REPAIRED IAW SB737-53-1216 PART III FIGURE 8.SDR EE4Y2017083004198Frame · corrodedDURING THE STRUCTURAL INSPECTION AT AIR CONDITION DISTRIBUTION BAY, IT WAS REPORTED AT BS 520 THE FRAME SECTION BETWEEN STRINGERS 27L AND 28L CORRODED. THE DAMAGED FRAME SECTION WAS REPAIRED IAW SRM 53-00-07, FIGURE 201 REPAIR 5.SDR EE4Y2017090304259Channel · corrodedDURING THE STRUCTURAL INSPECTION AT THE LOWER FUSELAGE WATER WASTE PANEL AREA, FOUND THE INNER SIDE CHANNEL CORRODED BETWEEN BS 986 - 1006, STRINGERS 25 - 26R. THE CHANNEL WAS REPLACED IAW SRM 51-10-02, PARAGRAPH 8, AND DRAWING 65-55843.SDR EE4Y2017083104207Frame · crackedDURING 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 BRACKET. THE DAMAGE WAS REPAIRED IAW SB737-53-1216, PART III, FIGURE 8.SDR EE4Y2017083104200Frame · crackedDURING 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 BRACKET. REPAIRED IAW SB737-53-1216, PART III, FIGURE 8.SDR EE4Y2017090104229Beam · crackedDURING 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 12, DETAIL V.SDR EE4Y201708314210Frame · crackedDURING 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 SB737-53-1216, PART III, FIGURE 8.SDR EE4Y2017090304255Spar Web · damagedDURING 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 REPAIRED IAW S/R 3-3949229341, AND EO COO-EO-2017-3990-R01.SDR EE4Y2017082204133Frame · damagedDURING THE STRUCTURAL INSPECTION, BS 907 FRAME, STRINGER 17L AND 17R, FOUND SEVERAL FASTENER HOLES DAMAGED, THE FRAME AND ATTACHING PARTS WERE REPAIRED IAW EO 5136.SDR EE4Y2017082204076Frame · crackedDURING 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, BETWEEN STR20R AND STR21R FRAME WITH CRACK AT THE 0.500 INCH DIAMETER HOLE. THE AFFECTED FRAME BS 500G SDR EE4Y2017082204079Frame · crackedDURING 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 REPLACED IN ACCORDANCE WITH SB 737-53A1208SDR EE4Y2017082204077Skin · canningDURING 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 AREA HAS BEEN REPAIRED IAW SRM 53-80-01, REPAIR 6.SDR EE4Y2017082204134Skin · crackedDURING 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, REPAIR 7.SDR EE4Y2017082204081Skin · crackedDURING 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 EE4Y2017082204082Spar · crackedDURING 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 REPAIRED IAW SRM 57-20-10, REPAIRS 4 AND 6.SDR EE4Y2017082204080Spar · crackedDURING 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 4.
Back to N305GT, cancelled Jan 27, 2025