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 JR2R20210408071Beam · corrodedLONGITUDINAL FLOOR BEAM AT LBL9 FR86 - FR89 CORRODEDSDR JR2R20210408073Beam · corrodedLONGITUDINAL FLOOR BEAM AT RBL9 FR86 - FR89 CORRODEDSDR JR2R20210408066Beam · corrodedLONGITUDINAL FLOOR BEAM CORRODED AT LBL9 BETWEEN FR90 AND FR90ASDR JR2R20210408079Gusset · corrodedGUSSET AT FR 84 LBL 24 CORRODED OUT OF LIMITSSDR R61A2021040700323Door Sill · corrodedR2 DOOR CORROSION UNDER BOTH GIRT BAR FITTINGS. REMOVED CORROSION ON THE R 2 DOOR UNDER BOTH GIRT BAR FITTINGS. MAX MATERIAL LOSS IS =0.102"X0.181" AND IS OUT OF ALLOWABLE LIMITS REF: EMB SRM 53-23-11/AD03. REMOVED, LOCATED, DRILLED AND ALODINE, INSTALLED NEW SDR R61A2021040700322Doubler · corrodedCORROSION-AFT RH COCKPIT FLOOR DOUBLER FR11-12, RBL 12" CUT AND REMOVED DAMAGED SECTION OF CO-PILOT FLOOR DOUBLER. CUT NEW FLOOR DOUBLER FILLER SECTION, LOCATED, DRILLED AND PREPPED FOR INSTALLATION REF: ETD2021-170-008369 REV. A. :INSTALLED COCKPIT CO-PILOT SDR DALA2023050303443Unknown · unknownSHIP 3319 GOUGE EXTERNAL SKIN BTW FR 73 TO FR 74 AND BTW STR 30L AND STR 31L AT LOWER FUSELAGE. CORRECTIVE ACTION: CUT OUT DAMAGE, FABRICATED REPAIR PARTS FROM .071 2024 T3 AND INSTALLED REPAIR PARTS DOUBLER AND FILLER REF A330 SRM 53-41-11-300-016. TREATED PRSDR QXEA2021040500173Keelbeam · corrodedCORROSION ON KEEL BEAM STR 31P AT FSX 71.2 AND CROSS BRACE ATTACH BOLT. COMPLIED WITH PERMANENT SPILCE REPAIR FOR CORROSION DAMAGE TO KEEL BEAM STR 31P BETWEEN FS X49-50-X71-20 IAW RD84-53-10135.SDR EE4Y2023031017357Skin · nickedDURING THE VISUAL INSPECTION PER TASK CARD CR 20-3_P1-VISUAL INSP/011, MULTIPLE NICKS WERE FOUND COMMON TO LOWER REAR FUSELAGE SKIN BETWEEN FR55 AND FR56 AND BETWEEN STR 39R AND STR 40R. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER AIRBUS DOSSIER#SDR JJBA20210326043None · noneEXISTING DOUBLER BETWEEN FRAMES 1-2 STRINGER 11-12 RIGHT. REPAIRED FWD FUSELAGE SKIN BETWEEN FR 1- FR 2 STRG 11R-12RSDR R61A2021041100326Crossbeam · corrodedCORROSION - FR 84 CROSS BEAM SCRATCHED AND CORRODED AS MARKED ALONG ENTIRE LENGTH FROM STR17L TO STR 17R. CUT OUT DAMAGE AREA, FABRICATED ''L'' ANGLES ,FILLER, SHIMS AND INSTALLED REPAIR PARTS FOR CROSSBEAM FRAME 84 REFER ETD2021-170-008524. RESTORED SURFACE SDR JJBA20210316046None · noneEXISTING DOUBLER BETWEEN FRAMES 15 AND 16 BETWEEN STRINGERS 10R AND 11R. REPAIR WAS ACCOMPLISHEDSDR DALA2021070203667Fitting · unknownSHIP 3260 COULD NOT CLEAN FITTING LOCATION #7 FRAME 16 LH SIDE HOLES. CORRECTIVE ACTION: HOLES CLEANED PER PRI 590581-14AD REV. 0, REV.1, REV. 2, AND REV. 3 AND ERA 590581-14AD REV. ORIGINAL. (1755486)SDR DALA2021070203666Fitting · unknownSHIP 3260 COULD NOT CLEAN FITTING LOCATION #1 FRAME 16 LH SIDE HOLES. CORRECTIVE ACTION: REPAIRED PER PRI 590581-14AD REV. 0, REV.1, REV. 2, AND REV. 3 AND ERA 590581-14AD REV. ORIGINAL. (1755484)SDR R61A202103240070Panel Support · corrodedWHILE AC WAS IN FOR HVY CK FOUND CENTER FUSELAGE 3 PAX FLOOR STRUCTURE CORROSION FOUND ON FORMED SECTION FR 88 RBL36. REPLACED PANEL SUPPORT PN 170-86181-005 IAW SRM 51-42-01, 5143-03. SEE AAR NRC# 4500867-2000-0075 FOR DETAILS OF WORK PERFORMED. AC REMAINS INSDR R61A202103240069Shear Panel · corrodedWHILE AC WAS IN FOR HVY CK FOUND CENTER FUSELAGE 3 PAX FLOOR STRUCTURE CORROSION FOUND ON SHEAR PLATE BETWEEN FR 86-87 BL 0-BL 6. REPLACED SHEAR PANEL PN 170-65928-001 IAW SRM 51-42-01. SEE AAR NRC# 45000867-2000-0071 FOR WORK PERFORMED. AC REMAINS IN YQG FOR SDR R61A202103240068Gusset · corrodedWHILE AC WAS IN FOR HVY CK FOUND CENTER FUSELAGE 3 PAX FLOOR STRUCTURE CORROSION ON GUSSET @FR 89 RBL 23. REPLACED GUSSET PN 170-60259-001 IAW SRM 51-41-02. SEE AAR NRC# 4500867-2000-0070 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.SDR JJBA20210322027Frame · crackedMULTIPLE CRACKS FOUND ON RH SKIN ON FRAMES 77-78-79 AND BTW STR 3R-10R. CRACKS (X7) ARE REPAIREDSDR CALA2021031000282Stringer · corrodedAFT CARGO PIT, ON STR37R, NEXT AT FR64 HAS CORROSION. -A3NB-53-4 -6179-. GENERATED ON HAECO LCQ N/R 9296639 (22639) BY MECH N0783 39. REMOVED AND REPLACED STRINGER 37 RT FROM FR61-FR63 IAW A319 SRM 51-72-11. DOT REMOVED. PERFORMED BY MECH V052030 AND ISNPECTEDSDR MASA20210405129Stringer · corrodedCORROSION ON STRINGER 19 RH IN STA. FS280 TO FS319|CORRECTIVE ACTION: STRINGER 19 RH IN STA. FS280 TO FS319 WAS REPLACED PER CRJ900 SRM 51-42-06-001-A01 PAR 6A AND SRM 51-42-20-001-A01 PAR 6A.SDR JJBA20210306048None · noneEXISTING DOUBLER BETWEEN FRAMES 70-72 + AND BETWEEN STRINGER 11-14L. REMOVED DOUBLER AND REPAIRED REAR FUSELAGE SKIN BETWEEN FRAMES 70-72 AND STRINGERS 11L-14L.SDR JJBA20210306047None · noneFUSELAGE EXISTING REPAIR LOCATED BETWEEN FRAMES 19-20 STGR 2-4R. REMOVED DOUBLER AND REPAIRED CENTER FUSELAGE I SKIN AT FR 19-20 AND STGR 2-4R.SDR JJBA20210305044None · noneRECOMPLY WITH EC5310-01446 IN FORWARD AVIONICS BAY. RECOMPLIED WITH EC5310-01446 IN FORWARD AVIONICS BAYSDR JR2R20210303681Beam · corrodedFLOOR BEAM AT RBL9 BETWEEN FR20 AND 21 IS CORRODEDSDR JR2R20210301982Beam · corrodedRH SEAT TRACK END CORRODED OUT OF LIMITS BETWEEN FR84 AND FR85SDR DU4R2021030100013Support Angle · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND CORRODED BELLY PANEL SUPPORT ANGLE AT R/H W/W AFT WALL STA. 727. S/O 660004, N/R 44329SDR JR2R20210228780Shear Panel · corrodedCENTER SHEAR PANEL FR86 - FR87 CORRODED OUT OF LIMITSSDR JR2R20210228771Gusset · corrodedRH BEAM GUSSET PLATE AT FR90 CORRODED OUT OF LIMITSSDR JR2R20210228775Panel · corrodedRH SHEAR PANEL FR86-FR87 CORRODED OUT OF LIMITSSDR JR2R20210228678Beam · corrodedFLOOR BEMA AT LBL 9 CORRODED FROM FR17 TO FR19SDR JR2R20210228680Beam · corrodedCROSSBEAM AT BL 0 AND FR17 CORRODED OUT OF LIMITSSDR DALA2021070203679Panel · corrodedSHIP 3250 ER/A 590221-14 ISSUED FOR CORROSION ON THE LH AND RH LATERAL PANEL ASSY TRUNNION BORES. CORRECTIVE ACTION: COMPLIED WITH ER/A 590221-14. (1741905)SDR JR2R20210225768Gusset · corrodedLH BEAM GUSSET PLATE AT FR 89 CORRODED BEYOND ALLOWABLE LIMITSSDR JR2R20210225772Gusset · corrodedRH O/B BEAM GUSSET PLATE AT FR90 CORRODED OUT OF LIMITSSDR SWIA202157867Not Reported · corrodedFOUND PART CORRODED UPON REMOVAL AT FS364 STR 23R - 24R (C-CHECK RO 4/25/2021) RECIEVED AND DRILLED UP NEW PART FROM AIRCRAFT, IAW CRJ 200 SRM 51-40-06, 51-40-11. PART TO BE INSTALLED ON MX TRANS# 22329418 ITEM 11.SDR JR2R20210224811Spacer · corrodedACCESS PANEL 192CR SPACER CORRODED OUT OF LIMITSSDR JR2R20210224816Spacer · corrodedACCESS PANEL 192CR SPACER CORRODED OUT OF LIMITSSDR JR2R20210223978Waste Box · corrodedLAV SERVICE PANEL BOX INTERNAL PLATE CORRODED OUT OF LIMITS.SDR JR2R2021022370993Seat Track · corrodedFLOOR SEAT TRACK AT RBL 9 AND FR 17 CORRODED OUT OF LIMITS. REPAIRED SEAT TRACK IAW EMBRAER ETD 2021-170-004620.SDR JR2R20210223770Gusset · corrodedRT LONG BEAM GUSSET PLATE AT FR 89 CORRODED OUT OF LIMITS.SDR WX0A1900010074273None · none(VDR ID 32512) PERFORM PERMANENT REPAIR TO TAIL SKIN FR79-80, STR 1-2 R./ PERFORMED PERMANENT REPAIR. DAMAGE AT FRAME 79 & 80 & STR 2LT TO 2RT IAW AIRBUS REPORT 80887126.NO DEFECTS NOTED"SDR JJBA20210220029Door · rustedBAGGAGE DOOR LATERAL AFT L-SHAPE CORRODED. CORROSION AT BAGGAGE DOOR LATERAL AFT SHAPED SHEAR CLIP REPAIRED.SDR JJBA20210301034Skin · chafedCHAFFING FOUND ON EXTERNAL RH SKIN BETWEEN FR 67-68 AND BTW STR 7-8 INSIDE ENGINE PYLON. EXTERNAL SKIN BTW FR 67-68 AND BTW STR 7-8 RH SIDE INSIDE ENG. PYLON REPAIRED.SDR JJBA20210225030Skin · crackedCRACK SUSPECTED ON EXTERNAL SKIN AT FR 78 BTW LT STR 6-7. ON EXTERNAL SKIN AT FR 78 BTW LH STR 6-7 DOUBLER LOCALLY FABRICATED FOR REPAIR. ON EXTERNAL SKIN AT FR 78 BTW LH STR 6-7 CRACK REPAIRED.SDR JJBA20220212009Not Reported · not reportedPOSSIBLE CORROSION LAV FLOOR (LATERAL) SUPPORT FR 59-60+8 STR 15R. REMOVED AND REPLACED NEW SILL.SDR JJBA20210212040None · noneFUSELAGE SKIN DAMAGED AT FR29 TO FR31 BETWEEN S12R TO S13R. REMOVED DAMAGED FUSELAGE SKIN STR 13R FR 29R TO 31R. LOCATED AND DRILLED REPAIR DOUBLER AND FILLER. TRIMMED AND DEBURRED REPAIR FILLER AND REPAIR DOUBLER AND COUNTERSUNK REPAIR DOUBLER. TREATED AND PRSDR EE4Y2023031017356Seat Track · corrodedDURING THE JOB ACCOMPLISHMENT PER ALLEGIANT TASK CARD E2500-0032-_P2-ADS-MOD-SYS, IT WAS FOUND AT FWD FUSELAGE PAX CABIN, THE SEAT TRACK AT FR20+60MM, Y-765 WITH CORROSION ON CROWN AREA. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER A320 SRM TASK 5SDR K11A2021022200044Skin · crackedTWO CRACKS ON LT AFT BELLY JUST AFT OF WING TO BODY FAIRING.SDR EE4Y2023031017354Skin · dentedDURING THE VISUAL INSPECTION PER ALLEGIANT TASK CARD ZL-200-02-1-001_P1-VISUAL, MULTIPLE DENTS WERE FOUND COMMON TO REAR FUSELAGE UPPER SKIN BETWEEN FR69 AND FR70 AND BETWEEN STR 19L AND 20L, DENTS WERE EVALUATED AND DETERMINED AS OUT OF A319-SRM LIMITS. CORRSDR EE4Y2023031017353Skin · dentedDURING VISUAL INSPECTION PER ALLEGIANT TASK CARD 51-000-001_P1-VISUAL INSP. THERE WERE FOUND TWO DENTS COMMON TO THE FUSELAGE REAR CONE LOWER SKIN, BETWEEN FR73 AND FR74 AND BETWEEN STR 28R AND STR 31R, DENTS WERE EVALUATED AND DETERMINED AS OUT OF SRM LIMITS.
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