N489MC
Service difficulty reports · 217
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 = 'N489MC' 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 = 'N489MC' 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 UIEA2022082500896Panel · noneM/D STA 1241 LBL 77" - 99" CLOSURE PANEL FOUND CRACK(<P>CLOSURE PANEL REPLACEMENT AS PER SRM 51-40-05 AND SRM 51-40-02 REV 95 DATE 20 JUN 2022</P>)SDR UIEA2022082500895None · noneAFT CARGO STA 1780 WEB RBL 8-16 FOUND EXISTING REPAIR(<P>AFT CARGO STA 1780 WEB RBL 8-16 DOUBLER REPAIRED IAW RI-53-62-15839 REV A</P>)SDR UIEA2022082500894None · noneAFT CARGO STA #1800 WEB RBL 4-8 FOUND EXISTING REPAIR(<P>AFT CARGO STA #1800 WEB RBL 4-8 DOUBLER REPAIRED IAW RI-53-62-15840 REV A</P>)SDR UIEA2022081900877None · noneLHW I/B FORE FLAP UPPER SURFACE FOUND DENT(<P>PERFROMED REPAIR AT DENT AREA <SPAN>SRM 51-70-07 PAR.5A</SPAN></P>)SDR UIEA2022081800874None · noneFUSELAGE - SECTION 48 - BODY SATION 2598 BULKHEAD - HORIZONTAL STABILIZER HINGE SUPPORT FRAME CRACKING - MODIFICATION AND REPAIR - 747-53A2837 / AD 2014-14-03(<P>EXISTING REPAIR AREA FASTENERS REMOVED AND REINSTALLED AS PER RI NO : RI-53-83-15844 REV A</P>)SDR UIEA2022081800873None · noneFUSELAGE - SECTION 48-BODY STATION 2598 BULKHEAD - HORIZONTAL STABILIZER HINGE SUPPORT FRAME CRACKING - MODIFICATION AND REPAIR - 747-53A2837 / AD 2014-14-03(<P>EXISTING REPAIR AREA FASTENERS REMOVED AND REINSTALLED AS PER RI NO : RI-53-83-15843 REV A</P>)SDR UIEA2022081800871None · noneFWD CARGO STA 1000 FRONT SPAR SHEAR TIE AT RBL 75.92 FOUND 1EA CRACK(<P>SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 2 PART 10</P>)SDR UIEA2022081800870None · noneFWD CARGO STA 1000 FRONT SPAR SHEAR TIE AT LBL 75.92 FOUND 1EA CRACK(<P>SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 2 PART 6</P>)SDR UIEA2022081800869None · noneFWD CARGO STA 1000 FRONT SPAR INTERCOSTAL LUG FITTING AT LBL 11.33 FOUND 1EA CRACK(<P>INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 2 PART 3</P>)SDR UIEA2022081800868None · noneFWD CARGO STA 1000 FRONT SPAR INTERCOSTAL LUG FITTING AT RBL 11.33 FOUND 1EA CRACK(<P>INTERCOSTAL LUG FITTING REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 2 PART 7</P>)SDR UIEA2022081800867None · noneFWD CARGO STA 1000 FRONT SPAR SHEAR TIE AT RBL 57.5 FOUND 1EA CRACK(<P>SHEAR TIE REPLACEMENT AS PER ATLAS AIR EO 4453C024 REV 2 PART 9 AND RI NO : RI-53-43-15801 REV A</P>)SDR UIEA2022081700866None · noneM/D STA 1220 RBL 99" TO RBL 121" OVERWING WEB SECTION FOUND PREVIOUS EXISTING REPAIR(<P>WEB REPAIRED AS PER RI NO: RI-53-40-15853 REV A</P>)SDR UIEA2022081700865None · noneCABIN STA 1000 FWD FRAME S12L TO S14L FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION SKIN AREA REPAIRED AS PER RI NO : RI-53-00-15855 REV C PART 1</P>)SDR UIEA2022081700864None · noneRHW 2 EA HOLE FOUND CRACK AT RHW ILES 1014.95 AND 1048.25 RIB LAYER(<P>2EA RIBS CRACK HOLES REPAIRED AS PER RI NO : RI-57-41-15854 REV A</P>)SDR UIEA2022081700863None · noneRHW I/B FORE FLAP O/B UPPER SURFACE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A REV.95 ,JUN20/2022</P>)SDR UIEA2022081300856None · noneLH STA 2598 BULKHEAD LOWER CORNER 2EA FASTENER HOLES FOUND CRACK AT 6 O/C WEB LAYER.(<P>2EA FASTENER HOLES CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15826 REV A</P>)SDR UIEA2022081300855None · noneLH STA 2598 BULKHEAD LOWER CORNER 1EA FASTENER HOLE FOUND CRACK AT 6 O'CLOCK OF FWD INNER SUPPORT LAYER WITH APPROX 0.050" DEPTH(<P>1EA FASTENER HOLE CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15826 REV A </P>)SDR UIEA2022081000849None · noneRHW L/E OLES 1117 L/E D FAIRING LOWER SKIN SPLICE STRAP AND LOWER CHORD FOUND CRACKED.(<P>LOWER CHORD CRACK AREA REPAIRED AS PER RI NO : RI-57-41-15815 REV A</P>)SDR UIEA2022081000848None · noneRHW OLES 1202 L/E D FAIRING UPR CHORD CRACK(<P>CRACK AREA REPAIRED AS PER RI NO. RI-57-00-15825 REV A</P>)SDR UIEA2022081000847None · noneRHW OLES 1202 L/E D FAIRING AFT WEB CRACK(<P>CRACK AREA REPAIRED AS PER RI NO : RI-57-00-15825 REV A</P>)SDR UIEA2022081000846None · noneRHW ILES 1107 L/E D FAIRING ATT WEB UPR CHORD FOUND CRACKED(<P>CRACK AREA REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022081000845None · noneLHW ILES 1117 L/E 'D' FAIRING UPPER CHORD CRACK.(<P>CRACK AREA REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2 FIG 201</P>)SDR UIEA2022080900844None · noneLHW ILES 1117 L/E 'D' FAIRING NOSE BEAM LWR CHORD CRACK(<P>LWR CHORD CRACK AREA REPAIRED AS PER RI NO : RI-57-41-15814 REV A</P>)SDR UIEA2022080900842None · noneRHW L/E ILES 1117 L/E 'D' FAIRING SKIN LOWER FASTENER HOLE ELONGATED(<P>L/E SKIN REPAIRED AS PER RI NO : RI-57-41-15852 REV A</P>)SDR UIEA2022080900841None · noneM/D STA 780 TENSION TIE LBL 24" TO 29" AFT CHANNEL INT. FOUND CORROSION(<P>AFT CHANNEL CORROSION AREA REPAIRED AS PER RI NO : RI-53-25-15752 REV A.</P>)SDR UIEA2022080900840None · noneM/D STA 800 TENSION TIE LBL 20" AFT CHANNEL UPPER EDGE FOUND CRACK(<P>CHANNEL CRACK AREA REPAIRED AS PER RI NO : RI-53-25-15753 REV A</P>)SDR UIEA2022080900839None · noneM/D STA 780 TENSION TIE RBL 2" TO 9" AFT CHANNEL INT FOUND CORROSION(<P>AFT CHANNEL CORROSION AREA REPAIRED AS PER RI NO : RI-53-25-15754 REV A</P>)SDR UIEA2022080900838None · noneLOWER FUSELAGE EXTERNAL SKIN AT STA 275 STR 22R TO 23R FOUND DENT.(<P>DENT AREA MEASURED L:5" X W:4" X D:0.015" A/Y = 266.6 . CHECKED WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL III LIMITS REV 95 DATE 20 JUN 2022</P>)SDR UIEA2022080800837None · noneAPU COMPARTMENT STA 2664 WL 306 R/H FRAME FOUND CRACK UPPER : 0.50" AND LOWER : 0.750"(<P>FRAME CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201</P>)SDR UIEA2022080800836None · noneSKIN CORROSION AT FX STA 1660-1680 STR 2L - STR 1R SATCOM ANTENNEA ADAPTOR PLATE BONDING JUMPER TO SKIN AREA(<P>SKIN CORROSION AREA REPAIRED AS PER RI NO : RI-53-41-15846 REV A</P>)SDR UIEA2022080800835None · none#3 PYLON ACCESS PANEL #472LR 2EA SCREW HOLES ELONGATED(<P>2EA SCREW HOLES ELONGATE AREA REPAIRED AS PER RI NO: RI-54-00-15810 REV A</P>)SDR UIEA2022080800834None · noneM/D STA 1140 RBL 30 - 33 WING CTR SECTION UPPER SKIN CORROSION(<P>SKIN CORROSION AREA REPAIRED AS PER RI NO : RI-57-00-15842 REV A</P>)SDR UIEA2022080800833None · noneLH BS 2231 S25L 2EA HOLES FOUND CRACK AT CHORD LAYER RUNNING 3 O/C POSITION APPROX 0.040 INCH, RUNNING 4 O/C POSITION APPROX 0.040 INCH(<P>CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15797 REV A</P>)SDR UIEA2022080800832None · noneLH BS 2231 S24L 1EA HOLE FOUND CRACK AT CHORD LAYER, RUNNING 1 O/C POSITION APPROX 0.040 INCH(<P>CRACK AREA REPAIRED AS PER RI NO. RI-53-00-15797 REV A</P>)SDR UIEA2022080800831None · noneLH BS 2231 S16L 1EA HOLE FOUND CRACK AT STRAP LAYER RUNNING AT 9 O/C POSITION APPROX 0.050"(<P>FRAME STRAP CRACK AREA REPAIRED AS PER SRM 53-60-15 REPAIR 2 AND RI NO. RI-53-00-15784 REV A</P>)SDR UIEA2022080800830None · noneM/D STA 1200 RBL 98 - 121 FLOOR WEB FOUND CRACK(<P>WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-9 REPAIR 9 AND RI NO : RI-53-00-15791 REV B</P>)SDR UIEA2022080800829None · none1EA CRACK FOUND ON NWW LHS SIDE PANEL WL 180 BETWEEN BS 280 AND BS 300 APPROX 5" IN LENGTH(<P>LOCATION CRACK AREA REPAIRED AS PER RI NO : RI-53-00-15789 REV A</P>)SDR UIEA2022080800828None · none1EA CRACK FOUND ON NWW LHS SIDE PANEL WL 180 BETWEEN BS 260 AND BS 280 APPROX 1/2" IN LENGTH(<P>LOCATION CRACK AREA REPAIRED AS PER RI NO : RI-53-0015789 REV A</P>)SDR UIEA2022080800825None · noneFX KEEL BEAM L/H EXTERIOR SURFACE LOWER CHORD STA 1000 - 1026 FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI NO. RI-53-00-15790 REV A</P>)SDR UIEA2022080800824None · none1EA CRACK INDICATION WAS FOUND ON SKIN LAYER AT LH BS 980 S38L DRAG SPLICE FITTING(<P>SKIN REPAIRED AS PER SRM 53-20-01-2R-2 REPAIR 2 FIG 201 DETAIL III AND ATLAS AIR EO : 4453A499 PART 3</P>)SDR UIEA2022080800823None · none1EA CRACK INDICATION AS PER ON SKIN LAYER AT RH BS 980 S38R DRAG SPLICE FITTING(<P>SKIN REPAIRED AS PER SRM 53-20-01-2R-2 REPAIR 2 FIG 201 DETAIL IV AND ATLAS AIR EO 4453A449 PART 4 </P>)SDR UIEA2022080800822None · noneFX - KEEL BEAM R/H #4 STIFFENER FOUND CORROSION (COUNT FROM FWD)(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-00-15771 REV A </P>)SDR UIEA2022080800821None · noneFX KEEL BEAM R/H #5 STIFFENER (COUNT FROM FWD) FOUND CORROSION.(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-49-15778 REV A </P>)SDR UIEA2022080800820None · noneFX KEEL BEAM R/H #6 STIFFENER FOUND CORROSION ( COUNT FROM FWD )(<P>CORROSION AREA REPAIRED AS PER RI NO: RI-53-00-15772 REV A</P>)SDR UIEA2022080800819None · noneM/D STA 780 TO 860, LBL 22" CEILING SUPPORT FOUND CRACKED.(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-25-22-15782 REV A</P>)SDR UIEA2022080800818None · noneM/D STA 780 - 820 LBL 23 CEILING FOUND CRACK(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-25-22-15783 REV A.</P>)SDR UIEA2022080200813None · noneLHW OB MID FLAP AFT UPPER SKIN FOUND 2EA SCREW HOLES ELONGATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)SDR UIEA2022080200812None · noneLHW O/B T/E FORE FLAP L/E FAIRING AT MID EXTERIOR SURFACE DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)SDR UIEA2022080200811None · noneRHW O/B T/E FORE FLAP L/E FAIRING AT MID EXTERIOR SURFACE DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM51-70-07 PAR.5C</P>)SDR UIEA2022070700733None · noneM/D SCD AFT O/B DOOR SILL LOWER SKIN FOUND 2 LOCATIONS FWD CUTOUT 1" & AFT CUTOUT 1" X 2" CRACK.(<P>2 LOCATIONS CUT OUT SKIN REPAIRED AS PER ATLAS AIR EO : 4425A500 REV 1.</P>)
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