JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 jasc_code = '5300' 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 jasc_code = '5300' 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 R61A2022092700573Shear Angle · corrodedSHEAR CLIP IS CORRODED AT FRAME 75 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR R61A2022092700572Shear Angle · corrodedSHEAR CLIP IS CORRODED AT FRAME 76 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR R61A2022092700571Shear Angle · corrodedSHEAR CLIP IS CORRODED AT FRAME 84 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR R61A2022092700570Shear Angle · corrodedSHEAR CLIP IS CORRODED AT FRAME 82 BETWEEN STRINGERS 27R AND 26R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR R61A2022092700569Shear Angle · corrodedSHEAR CLIP IS CORRODED AT FRAME 82 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR R61A2022092700568Shear Angle · corrodedSHEAR CLIP IS CORRODED AT FRAME 83 BETWEEN STRINGERS 28R AND 27R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR R61A2022092700567Shear Angle · corrodedSHEAR CLIP IS CORRODED AT FRAME 81 BETWEEN STRINGERS 27R AND 28R. REMOVED AND REPLACED SHEAR CLIP PER SRM 51-40-08.SDR R61A2022092700566Stringer Splice · corrodedCORROSION ON STRINGER AT RIVET ON STRINGER 19R AFT OF FRAME 88. REPAIRED STRINGER 19R PER ETD2022-170-028727.SDR UIEA2022083100934None · noneAFT CARGO STA 1960 - 1980 STR 44R FOUND EXISTING REPAIR(<P>AFT CARGO STA 1960 - 1980 STR 44R DOUBLER REPAIRED IAW RI-53-61-15841 REV A</P>)SDR UIEA2022083100933None · noneCABIN STA 1000 FRAME S14R TO S15R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REPARIED AS PER RI NO : RI-53-00-15864 REV A</P>)SDR UIEA2022083100932None · noneCABIN STA 1000 FRAME S15R TO S16R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-00-15864 REV A</P>)SDR UIEA2022083000931None · noneCABIN STA 1000 FRAME S16R TO S17R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-00-15864 REV A </P>)SDR UIEA2022083000930None · noneCABIN STA 1000 S13R TO S14R INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-00-15864 REV A</P>)SDR UIEA2022083000929None · noneCABIN STA 1000 S15L TO S16L AFT INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-01 AND REPROTECTED AS PER SRM 51-20-01 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( REF 95 DATE SDR UIEA2022083000928None · noneCABIN STA 1000 S13L TO S14L AFT INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REPAIRED AS PER RI NO : RI-53-00-15855 REV C PART 3</P>)SDR UIEA2022082900926None · noneCABIN STA 1241 FRAME STR 13R TO STR 14R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082900925None · noneCABIN STA 1241 FRAME S14R TO S15R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082900924None · noneCABIN STA 1241 FRAME S15R TO S16R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082900922None · noneCABIN STA 1241 FRAME S16R TO S17R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082900921None · noneCABIN STA 1241 FRAME S17R TO S18R FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082900920None · noneCABIN STA 1241 FRAME S15R TO STR 16R AFT INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( SRM REV 95 , DATE 20 JUN 2022 )</P>)SDR UIEA2022082900919None · noneCABIN STA 1480 FRAME S16L TO S17L FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082900918None · noneCABIN STA 1480 FRAME S9L TO S10L FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082900913None · noneKEEL BEAM LH EXTERIOR LWR CHORD STA 1072 CORROSION(<P>CORROSION REMOVED IAW SRM 51-10-02 AND REPROTECTED IAW SRM 51-20-01 CHECKED WITHIN SRM 53-40-12 ALLOWABLE DAMAGE 1 FIG 102 LIMITS REV 95 20 JUN 2022.</P>)SDR UIEA2022082600907None · noneM/D STA 2350 TO STA 2360, RH O/B FLOOR SUPPORT FOUND CORROSION (MOST O/B)(<P>FLOOR SUPPORT CORROSION AREA REPAIRED AS PER RI NO : RI-53-65-15849 REV A</P>)SDR UIEA2022082600905None · noneCABIN STA 1620 TO STA 1640 LBL 11 SEAT TRACK UNDERNEATH FOUND PREVIOUS REPAIR(<P>THE PREVIOUS REPAIR FOUND DEVIATION WITH SRM. REPLACEMENT OF REPAIR STRAP AT LOWER FLANGE ACCOMPLISHED AS PER SRM 53-00-52-<SPAN>2R-12 REPAIR 12 FIG 201 REV 95 20JUN2022</SPAN></PSDR UIEA2022082600904None · noneCABIN STA 2040 TO 2060 LBL 11" SEAT TRACK UNDERNEATH FOUND PREVIOUS REPAIR(<P>SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201.</P>)SDR UIEA2022082600903None · noneKEEL BEAM STA 1094 R/H LWR CHORD SURFACE FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-40-12 ALLOWABLE DAMAGE 1 FIG 102 LIMITS ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082600902None · noneKEEL BEAM STA #1123 R/H LWR CHORD AREA SURFACE FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-40-12 ALLOWABLE DAMAGE 1 FIG 102 ( SRM REV 95 DATE 25 JUN 2022 )</P>)SDR UIEA2022082600901None · noneKEEL BEAM STA 1074 RH LWR CHORD SURFACE FOUND CORROSION(<P>CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-40-12 ALLOWABLE DAMAGE 1 FIG 102 ( SRM REV 95 DATE 20 JUN 2022 )</P>)SDR UIEA2022082600900None · noneCABIN STA 1000 FRAME FWD S14L TO S15L FWD INTERNAL SKIN FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHECKED WITHIN SRM 53-00-01 ALLOWABLE DAMAGE 2 FIG 101 LIMITS ( SRM REV 95 DATE 20 JUN 2022 ) AND FASTENER'SDR UIEA2022082600899None · noneM/D STA 2360 RBL 11 FLOOR BEAM UPPER CAP CORRODED (MOST O/B)(<P>CORROSION FLOOR BEAM UPR CAP FABRICATED AS PER BOEING DWG 65B02634 AND PART LIST AND NEW CAP HOLES TRANSFERRED AS PER SRM 51-10-05 AND NEW CAP INSTALLED AS PER SRM 51-40-02 ( SRM REV 95 DATE 20 JUSDR UIEA2022082500898Tray · noneM/D CGO STA 1680 - 1700 S 1L-3L SATCOM DIPLEXER / LNA MOUNTING TRAY BROKEN(<P>TRAY REPLACEMENT AS PER ATLAS AIR EO NO : 4453C217 REV 0</P>)SDR UIEA2022082500897Panel · noneM/D STA 1241 RBL 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 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 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 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>)
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