N477MC
Service difficulty reports · 265
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 = 'N477MC' AND registry_match = 'registration' 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 = 'N477MC' AND registry_match = 'registration' 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 UIEA2026041500200Support · cracked1EA CRACK FOUND ON RHS BS 2598 UPPER CORNER HORI STAB HINGE SUPPORT FRAME(<P>FRAME CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A749 REV 7 PART 2 STEP 4 (B) AND STEP 5. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041600201Support Fitting · crackedRHW T/E I/B CAVITY #7 SPOILER ACTUATOR SUPPORT FITTING O/B LOWER EDGE FOUND CRACKED.(<P>SUPPORT FITTING O/B LOWER EDGE CRACK AREA REPAIRED AS PER RI-57-51-18166 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041700202Fairing · cracked#2 PYLON AFT FAIRING FWD UPPR RH SKIRT ANGLE FOUND CRACK(<P>SKATE ANGLE CRACK AREA REPAIRED AS PER RI-54-56-18197 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041700208Frame · chafed#1L CORE COWL REAR FRAME MIDDLE AREA FOUND CHAFING.(<P>FRAME CHAFING AREA REPAIRED AS PER ATLAS AIR EA-1971A269 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041700209Web · corrodedU/D LBL 10 TO 20 BS 480 TO 500 FLOOR SUPPORT WEB FOUND CORROSION(<P>WEB FABRICATED AS PER DWG 141U5421 AND PL, WEB REPLACED AS PER SRM 51-10-02, AND NEW WEB HOLES TRANSFERRED AS EPR SRM 51-40-05, AND NEW WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOSDR UIEA2026041700210Doubler · corrodedU/D LBL 10" - LBL 14" BS 480-500 FLOOR SUPPORT WEB ATT. DOUBLER CORROSION(<P>DOUBLER FABRICATED AS PER DWG 141U5422, AND PL DOUBLER REPLACED AS PER SRM 51-10-02, AND NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW DOUBLER INSTALLED AS PER SRM 51-40-SDR UIEA2026041800211Panel · corrodedRHW I/B T/E AFT FLAP MID UPPR PNL FWD LWR SURFACE SEVERAL AREA CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-53-18206 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800212Web · crackedLH BS 1480 WEB CRACKED 1/4" ADJACENT LONGERON FITTING LOWER AREA(<P>WEB REAIRED AS PER SRM 53-40-08-2R-1 REPAIR 1 FIG 201 AND RI-53-40-18137 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800214Fairing · cracked#1R T/R COWL 6 O/C T/E FAIRING FOUND CRACKED(<P>FAIRING CRACK AREA REPAIRED AS PER ATLAS AIR EA-1978A270 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800216Channel · crackedRH H.STAB O/B T/E WEDGE FWD CHANNEL FOUND CRACKED(<P>CHANNEL REPLACED AS PER RI-55-10-18182 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041800217Structure · corrodedRH WLG W/W STA 1241 AREA CENTER TANK RIGHT O/J PUMP ( M225 ) CUTOUT FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI-57-10-18226 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041900219Frame · chafed2L CORE COWL INNER FRAME AT 8 O'CLOCK FOUND CHAFING(<P>FRAME CHAFING AREA REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 REV 106 DATE: 20 FEB 2026 AND ATLAS AIR EA-1971A-270 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041900220Beam · crackedLHW L/E NEAR #2 PYLON O/B D-BEAM WEB FOUND CRACK ( ILES 693 )(<P>WEB CRACK AREA REPAIRED AS PER RI-57-41-18207 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026041900221Frame · noneAFT CARGO STA 1800 FRAME WEB NEAR STR 38R - STR 40R FOUND UNIDENTIFIED EXISTING REPAIR(<P>EXISTING REPAIR PART REINSTALLED AS PER BOEING NCR 408271F. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042000222Rib · crackedLHW FRONT SPAR TO L/E CAVITY ILES 756 SUPPORT RIB FOUND CRACK(<P>RIB CRACK AREA REPAIRED AS PER RI-57-41-18176 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042000223Rib · crackedRHW L/E TO FRONT SPAR CAVITY ILES 756 SUPPORT RIB FOUND CRACK(<P>RIB CRACK AREA REPAIRED AS PER RI-57-41-18175 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200232Beam · crackedRHW L/E NEAR #4 PYLON I/B D-BEAM WEB CRACK ( ILES 1116 )(<P>CRACK WEB REPLACED AS PER SRM 51-10-02, AND NEW WEB HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW WEB INSTALLED AS PER SRM 51-40-02 AND RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042200233Beam · crackedRHW L/E NEAR #4 PYLON I/B D-BEAM UPPR CHORD FOUND CRACK ( ILES 1116 )(<P>UPPER CHORD CRACK AREA REPAIRED AS PER RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200234Beam · crackedRHW L/E NEAR #4 PYLON I/B D-BEAM LOWER CHORD CRACK(<P>LWR CHORD CRACK AREA REPAIRED PER RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200235Floor Panel · puncturedBULK CARGO CTR FLOOR PANEL AT STA 2040 TO 2060 RH SIDE AREA WITH A PUNCTURE.(<P>FLOOR PNL PUNCTURE AREA REPAIRED AS PER RI-25-54-18173 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042200236Skin · cracked2L CORE COWL EXTERIOR SURFACE T/E AT 12 O'CLOCK POSITION FOUND CRACKED(<P>SKIN CRACK AREA REPAIRED AS PER ATLAS AIR EA-1971A268 REV 1. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042400245Floorbeam · corrodedU/D LBL 10 TO 30 BS 500 FLOOR SUPPORT SPLICE PLATE FOUND CORROSION(<P>SPLICE PLATE FABRICATED AS PER BOEING DWG 141U5422 AND PL, AND NEW SPLICE PLATE HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW SPLICE PLATE INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS SDR UIEA2026042400246Web · crackedU/D LBL 10 TO LBL 35 BS 500 - BS 540 FLOOR SUPPORT SHEAR WEB CORROSION(<P>SHEAR WEB FABRICATED AS PER BOEING DWG 141U5421 AND PL, AND NEW SHEAR WEB HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW SHEAR WEB INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTEDSDR UIEA2026042600248Floor Support · crackedM/D BS 1860 - 1880 RHS O/B RBL 116" FLOOR SUPPORT L ANGLE FOUND CRACK.(<P>FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI-25-21-18246 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2026042700250Seat Track · crackedM/D - BS 1050-1070 RBL 77 SEAT TRACK RHS FLANGE FOUND CRACK(<P>SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-40-52-2R-3 REPAIR 3 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042700252Skin · misrepairedFUSELAGE SKIN AT STA 2564-2575 STR 38R - STR 42R FOUND UNIDENTIFIED EXISTING REPAIR(<P>SKIN REPAIRED AS PER RI-53-80-18257 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042700253Stringer · noneFWD CARGO STA 790 - 810 STR 43L FOUND UNIDENTIFIED EXISTING REPAIR(<P>EXISTING REPAIR REINSTALLED AS PER BOEING NON-CONFORMANCE NUMBER 430034F. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800254Duct · crackedNHR 3 ENG RH CORE COWL PRECOOLER OUTLET DUCT INNER GILL FOUND CRACKED.(<P>NEW PRECOOLER DUCT REPAIRED AND INSTALLED AS PER ATLAS AIR EA-1971A274 REV 0. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800256Skin · corroded1EA CORROSION FOUND ON FUSELAGE LOWER SKIN INNER SURFACE AT STA 2185 STR 47R(<P>SKIN CORROSION AREA REPAIRED AS PER RI-53-60-18178 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800257Longeron · cracked1EA CRACK WAS FOUND ON RH BS 1480 LONGERON EXTENSION FITTING RADIUS AREA APPROX 1/4" IN LENGTH(<P>CRACK LONGERON EXTENSION FITTING REPLACEMENT AS PER ATLAS AIR EO 4453A818 REV 20 PART 8. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800258Web · crackedFX RH BS 1480 WEB CRACK 5/8" ADJACENT LONGERON EXTENSION FITTING LOWER AREA(<P>WEB CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 8 AND RI-53-20-1823 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800259Rib · crackedRHW L/E TO FRONT SPAR CAVITY ILES 790 SUPPORT RIB FOUND CRACK(<P>L/E RIB CRACK AREA REPAIRED AS PER RI-57-41-18188 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800260Skin · cracked2EA CRACK WERE FOUND ON SKIN 2EA FASTENER RUNNING AFT ON RH FUSELAGE SKIN LAP BETWEEN BS 1438 AND BS 1460 STR 23R(<P>SKIN LAP CRACK AREA REPAIRED AS PER RI-53-40-18228 REV. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042800261Rib · crackedRHW L/E TO FRONT SPAR CAVITY ILES 766.45 SUPPORT RIB FOUND CRACK(<P>RIB CRACK AREA REPAIRED AS PER RI-57-41-18205 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042800262Door · abnormalAFT CARGO DOOR LOWER AFT CORNER FOUND EXISTING REPAIR(<P>DOOR SKIN REPAIRED AS PER RI-52-35-18240 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026042900263Seat Track · crackedM/D STA 1375 RBL 11" LONGITUDINAL SEAT TRACK FOUND CRACKED(<P>SEAT TRACK CRACK AREA REPAIRED AS PER RI-53-40-18239 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900265Beam · damagedLHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD AREA FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER RI-57-41-18199 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900266Skin · damagedL/E SKIN REPAIRED FOR LHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900267Skin · damagedL/E SKIN REPAIRED FOR LHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900268Skin · unsecureLHW L/E SKIN NEAR #1 PYLON I/B AREA FOUND RIVETS LOOSE.(<P>L/E SKIN REPLACED AS PER SRM 51-10-02, AND NEW L/E SKIN HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW L/E SKIN INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026043000269Skin · crackedRHW L/E SKIN NEAR #4 PYLON O/B AREA FOUND CRACK(<P>L/E SKIN CRACK AREA REPAIRED AS PER RI-57-41-18141 REV B. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026043000270Beam · damagedRHW L/E D-BEAM NOSE SKIN AT #4 PYLON I/B FASTENER HOLES FOUND ELONGATED(<P>L/E SKIN REPAIRED AS PER RI-57-41-18210 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100278Panel · crackedM/D STA 2320 TO 2350 LH S/W LOWER DADO PANEL FOUND CRACK(<P>DADO PANEL CRACK AREA REPAIRED AS PER RI-53-60-18177 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100279Beam · crackedRHW L/E #17 VC FLAP CAVITY I/B D-BEAM O/B WEB FOUND CRACK ( #3 PYLON O/B )(<P>WEB REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100280Beam · crackedRHW L/E #17 V/C FLAP CAVITY I/B D-BEAM O/B UPPER CHORD FOUND CRACK(<P>UPPER CHORD REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100281Skin · damagedSKIN REPAIR FOR RHW LE D-BEAM FOR O/B UPPER CHORD REPAIR (3 PYLON OB)(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 AND RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100282Panel · crackedCOCKPIT LHS FLOOR FLIGHT KIT STOWAGE BASE PNL FOUND CRACK(<P>BASE PNL CRACK AREA REPAIR AS PER RI-25-10-18213 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100283Skin · damagedL/E SKIN REPAIRED AT #4 PYLON I/B D-BEAM FOR UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 AND RI-57-41-18200 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050100284Strap · corrodedRHW L/E D-BEAM LOWER STRAP AT ILES 665 FOUND HEAVY CORROSION(<P>CORROSION STRAP FABRICATED AS PER BOEING DWG 65B12246 AND PL, AND NEW STRAP REPLACED AS PER SRM 51-10-02, AND NEW STRAP HOLES TRANSFERRED AS PER SRM 51-40-05, AND STRAP INSTALLED AS PER SRM 51-40-SDR UIEA2026050100285Beam · crackedRHW L/E D-BEAM ILES 693 LOWER CHORD FOUND CRACK(<P>LWR CHORD REPAIRED AS PER RI-57-41-18181 REV A. NO FURTHER DEFECTS NOTED</P>)
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