N419MC
Service difficulty reports · 287
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 = 'N419MC' 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 = 'N419MC' 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 UIEA2023090500827Rvdt · unknownFLAPS DRIVE CAUTION MESSAGE ON RETRACTION BETWEEN FLAPS 5 AND 1(<P>REPLACED LH & RH OUTBOARD RVDT'S, ADP, ADP DRIVE, AND EDP IAW AMM 27-58-01. OPS CHK GOOD.</P>)SDR UIEA2022092000997None · noneM/D STA 460 LBL 95 - 98 FLOOR BEAM UPPER CAP FOUND CORROSION(<P>FLOOR BEAM UPPER CAP CORROSION AREA REPAIRED AS PER RI NO.RI-53-10-15897 REV.A</P>)SDR UIEA2022092000998None · noneNO.1 ENG - LH CORE COWL #2 FRAME PREVIOUS REPAIRED ANGLE CHAFING WORN(<P>CHAFING AREA ANGLE REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092000999None · noneM/D STA 1197 TO 1198 RBL 116 FLOOR SUPPORT FOUND CRACKED(<P>FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI NO: RI-53-40-15879 REV.A</P>)SDR UIEA2022092001000None · noneM/D STA 1780 TO 1840 RBL 77 TO 99 CASTER MAT 2 LOCATIONS SKIN FOUND CRACKED(<P>CASTER MAT 2 LOCATIONS SKIN REPAIRED AS PER ATLAS AIR EO 4425A500 REV.1</P>)SDR UIEA2022092101001None · noneNO.2 ENG - RH CORE COWL #4 FRAME (COUNT FROM FWD) PREVIOUS REPAIRED ANGLE CHAFING WORN AS MARKED(<P>CHAFING AREA ANGLE REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092101002None · noneM/D - STA 1780 TO 1840 LBL77 TO 99 CASTER MAT SKIN FOUND CRACK.(<P>CASTER MAT SKIN REPAIRED AS PER ATLAS AIR EO 4425A500 REV.1</P>)SDR UIEA2022092101003None · noneNO.4 ENG - RH CORE COWL EXTERNAL SKIN CRACK FOUND JUST BELOW PRE-COOLER EXIT VANE(<P>SKIN REPAIRED AS PER SRM 54-41-01-2R-3 REPAIR 3 FIG 201 REV 95 DATE 20JUN2022</P>)SDR UIEA2022092101004None · noneAFT CARGO BILGE SKIN FOUND CORROSION AT BS 1487 RBL 6 BILGE LONGERON MOUNT BOLT AREA(<P>CORROSION AREA REPAIRED AS PER RI NO: RI-53-61-15881 REV.B</P>)SDR UIEA2022092101005None · noneNO.3 ENG RH CORE COWL EXTERNAL SKIN CRACK FOUND JUST BELOW PRE-COOLER EXIT VANE(<P>SKIN CRACK AREA REPAIRED AS PER SRM 54-41-01-2R-3 REPAIR 3 FIG 201 REV 95 DATE: 20JUN2022</P>)SDR UIEA2022092101006None · noneBULK CGO COMPT FLOOR INTERCOSTAL I/B AND O/B FLANGE FOUND CRACKED AT RBL 7.625 STA 2080(<P>FLOOR INTERCOSTAL I/B AND O/B FLANGE REPAIRED AS PER RI NO: RI-53-61-15877 REV.A</P>)SDR UIEA2022092101007None · none#2 ENG RH CORE COWL UPPER FAIRING CHAFING THROUGH AT AFT AREA(<P>FAIRING CHAFING AREA REPAIRED AS PER SRM 54-41-01-2R-5 REPAIR 5 FIG 202</P>)SDR UIEA2022092101008None · noneFWD CGO COMPT STA 740 RBL 12" FRAME WEB UPPER AREA FOUND PUNCTURE(<P>FRAME WEB PUNCTURE AREA REPAIRED AS PER RI NO: RI-53-20-15878 REV.A</P>)SDR UIEA2022092101009None · noneFWD CGO COMPT STA 570-600 RBL 38-56 BALL MAT PANEL FOUND DAMAGED(<P>BALL MAT SKIN REPAIRED AS PER SRM 53-00-53-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092101010None · noneFWD CGO COMPT STA 600-660 RBL 38-56 BALL MAT PANEL FOUND DAMAGED(<P>BALL MAT SKIN REPAIRED AS PER SRM 53-00-53-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092101011None · noneM/D CGO - REDO THE REPAIR ON THE NOSE CARGO DOOR RH STA 140 - 160, STRINGER S39-S42A AS PER TAR 44073(<P>NOSE CARGO DOOR SKIN REPAIRED AS PER RI NO: RI-52-30-15882 REV.B</P>)SDR UIEA2022092101012Doubler · crackedFUSELAGE RHS STA 2521 - TWO CRACKS FOUND ALONG RADIUS OF UPPER LOBE DOUBLER AT FUSELAGE AND VERTICAL STAB, ATTACH FITTING AREA(<P>CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A224 REV 8 PART 2 STEP 5.</P>)SDR UIEA2022092101013Doubler · crackedFUSELAGE LHS STA 2521 - CRACK FOUND ALONG RADIUS OF UPPER LOBE DOUBLER AT FUSELAGE AND VERTICAL STAB, ATTACH FITTING AREA(<P>CRACK AREA REPAIRED AS PER ATLAS AIR EO 4453A224 REV 8 PART 2 STEP 4</P>)SDR UIEA2022092101014Skin · cracked1EA CRACK FOUND ON SKIN AT LH BS980 DRAG FITTING AT STR 38 CRACK APPROX 0.125" INCH LENGTH, RUNNING TO AFT DIRECTION(<P>SKIN REPAIRED AS PER SRM 53-20-01-2R-2 REPAIR 2 FIG 201 AND ATLAS AIR EO 4453A499 REV 13 PART 3</P>)SDR UIEA2022092101015Fitting · not reportedFUSELAGE STA 2598 BULKHEAD FRAME FITTING REPLACEMENT AS PER ATLAS AIR EO 4453A770 2&&3(<P>FRAME FITTING REPLACEMENT AS PER ATLAS AIR EO 4453A770 2&3 AND EXISTING FASTENERS INSTALLED (6EA) AS PER RI NO: RI-53-80-15889 REV A</P>)SDR UIEA2022092101016Skin · crackedL/H BODY GEAR SHOCK STRUT I/B DOOR AFT UPPER CORNER INTERNAL SKIN FOUND CRACK(<P>SKIN REPAIRED AS PER RI NO: RI-52-80-15886 REV.A</P>)SDR UIEA2022092101017Shear Tie · crackedFUSELAGE - CENTER SECTION - BS1000 FRONT SPAR SHEAR TIE FOUND CRACK AT RBL 33.99 LOCATION PART 8.(<P>SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO 4453C024 PART 8 AND RI NO.RI-53-00-15890 REV.A</P>)SDR UIEA2022092101018Lug · crackedFUSELAGE - CENTER SECTION - BS1000 FRONT SPAR INTERCOSTAL LUG FITTING FOUND CRACK AT RBL 11.33 LOCATION.(<P>INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 PART 7 STEP 3</P>)SDR UIEA2022092101019Lug · crackedFUSELAGE - CENTER SECTION - BS1000 FRONT SPAR INTERCOSTAL LUG FITTING FOUND CRACK AT RBL 11.33 LOCATION.(<P>INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 PART 7 STEP 3</P>)SDR UIEA2022092101020Support · corrodedRHW OLES 1530 L/E LOWER FWD FIXED PANEL FWD SUPPORT FOUND CORROSION AFTER BULGE DEFECT FOUND CORROSION AFTER BULGE DEFECT FOUND(<P>SUPPORT BEAM CORROSION AREA REPAIRED AS PER RI NO. RI-57-41-15885 REV.A </P>)SDR UIEA2022092101021Web · crackedLHW #2 PYLON O/B `D` FAIRING REAR WEB FOUND CRACK(<P>CRACK PREVIOUS WEB REPLACED AS PER RI NO: RI-57-41-15892 REV.A</P>)SDR UIEA2022092101022Fairing · crackedLHW #10 VC FLAP SECTION I/B `D` FAIRING REAR UPPER CHORD FOUND CRACK(<P>UPPER CHORD CRACK AREA REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092101023Web · crackedLHW #10 VC FLAP SECTION I/B `D` FAIRING REAR WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092101024Fairing · crackedRHW #17 VC FLAP SECTION I/B `D` FAIRING REAR UPPER CHORD FOUND CRACKED(<P>UPPER CHORD REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092101025Web · crackedRHW #17 VC FLAP SECTION I/B `D` FAIRING REAR WEB FOUND CRACK(<P>WEB REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022092101026Seat Track · corrodedM/D - STA 991 TO 993, RBL 98 SEAT TRACK O/B FLANGE FOUND CORROSION(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-6 REPAIR 6 FIG 201</P>)SDR UIEA2022092101027Seat Track · brokenM/D - STA 785 TO 794, RBL 11 SEAT TRACK FOUND BROKEN(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201</P>)SDR UIEA2022092101028Seat Track · crackedM/D - STA 2280 TO 2300 RBL 11 SEAT TRACK FOUND CRACKED(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201</P>)SDR UIEA2022092101029Seat Track · crackedM/D - STA 980 TO 1000, RBL 75" SUBSTITUTE SEAT TRACK FOUND CRACK(<P>SUBSTITUTE SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201</P>)SDR UIEA2022092101030Seat Track · crackedM/D - STA 1485 TO 1486 AND STA 1572 - 1573, RBL 75 SUBSTITUTE SEAT TRACK FOUND CRACKED(<P>SUBSTITUTE SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201</P>)SDR UIEA2022092101031Stringer · crackedR/H BODY BS 2598 BULKHEAD FWD STR 11 LOWER FITTING ONE EACH FASTENER HOLE FOUND CRACK AND TWO EACH EXISTING FASTENER HOLES SIZE (DIAMETER 0.278") LARGE THAN EO FASTENER HOLES SIZE (DIAMETER 0.250")(<P>CRACK FTG REPLACEMENT AND 2EA LARGE FASTENER HOLES INSTALLESDR UIEA2022092301041Frame · crackedEMP TAIL CONE RH SIDE BTN BS 2664.19, WL302 FRAME FOUND CRACK(<P>FRAME CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201</P>)SDR UIEA2022092801051Skin · corrodedAFT CARGO COMPT STA 1700 - STA 1720 S45R - S46R INTERNAL SKIN FOUND CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR UIEA2022092801052Skin · corrodedAFT CARGO COMPT STA 1680 - STA 1700 S50L - S51L INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR UIEA2022092801053Skin · corrodedAFT CARGO COMPT STA 1720 - STA 1740 S50R - S51R INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR UIEA2022092801054Skin · corrodedAFT CARGO COMPT STA 1720 - STA 1740 S51L - S51R INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS</P>)SDR UIEA2022092801055Skin · corrodedAFT CARGO COMPT STA 1680 - STA 1700 S50R - S51R INTERNAL SKIN FOUND SURFACE CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS </P>)SDR UIEA2022092801056Floor Support · corrodedU/D STA 400-460 LBL 20 - RBL 20 FLOOR BEAM CORROSION AT STA 400 LBL 10 TO LBL 14(<P>CORROSION REMOVED AND REPROTECED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMITS </P>)SDR UIEA2022092801057Floor Support · corrodedU/D STA 400-460 LBL 20 - RBL 20 FLOOR BEAM FOUND CORROSION AT STA 426 TO STA 446 LBL 20(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMITS</P>)SDR UIEA2022092801058Floor Support · corrodedU/D STA 400-460 LBL 20 - RBL 20 FLOOR BEAM FOUND CORROSION AT STA 406 TO STA 426 LBL 20(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMITS</P>)SDR UIEA2022092801059Stringer · corrodedAFT CARGO COMPT STA 1800 - STA 1820 S49L STRINGER CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-03 ALLOWABLE DAMAGE 1 FIG 101 REV.95 20 JUN 2022 LIMIT.</P>)SDR UIEA2022092901060Floorbeam · corrodedM/D - STA 2240, LBL 60 TO 84 FLOOR BEAM FOUND CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMITS</P>)SDR UIEA2022092901061Floorbeam · corrodedM/D - STA 2260, RBL 13 TO 15 FLOOR BEAM FOUND CORROSION(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 1 FIG 101 LIMITS</P>)SDR UIEA2022100301070Rib · damagedLHW O/B MID FLAP THE MOST I/B RIB FWD FOUND PREVIOUS EXISTING REPAIR(<P>PREVIOUS EXISTING REPAIR AREA REPAIRED AS PER SRM 51-10-02 AND NEW RIB HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW RIB INSTALLED AS PER SRM 51-40-02</P>)SDR UIEA2022100301074Skin · delaminatedLHW O/B FORE FLAP L/E FOUND DELAMINATION AT (46" FROM I/B )(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)
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