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 R61A2021111800903Doubler · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK ** CENTER FUSELAGE 3 WASTE BOX INNER DOUBLER FOUND CORRODED. MX REPAIRED DOUBLER PN 2024T3.125 IAW SRM 53-23-60 REPAIR 7.SDR MASA20211105530None · corrodedFUSELAGE FRAME AT FS 1000 WAS FOUND WITH CORROSION DAMAGE AT THE THREE LOCATIONS BETWEEN STR 23R AND STR 25L. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-06-003-A01, FIGURE 5453-61-06-991-804, ITEM 2, EA 69-2021-185SDR CALA2021110502041Beam · elongatedB767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 SDR R61A2021110500866Skin Panel · damagedDENT ON LH FWD FUSELAGE BETWEEN FR10/11 AND STGR 17L/18L. REPAIRED DENT ON LH FUSELAGE IAW SRM 51-75-14SDR JR2R20211104427Shear Panel · corrodedRH SHEAR PANEL IS CORRODED AT FR88SDR JR2R20211104434Beam · corrodedFLOOR BEAM IS CORRODED BETWEEN FR13 AND FR14 AT RBL9SDR SWIA202163860None · corrodedFWD FLOOR FITTING OF GALLEY #1 IS CORRODED (MARKED WITH GREEN TAPE) (C CHECK RO 1/16/2022) REPAIRED FWD FLOOR FITTING OF GALLEY #1 WHERE IS CORRODED BY INSTALLING NEW REPLACEMENT DOUBLER BRACKET PN:9335071-1 AND NEW REPLACEMENT FLOOR FITTING PN:CDSP2019-SDR SWIA202163370None · cracked* FWD EQUIPMENT BAY FLOOR SKIN CRACKED AT R/H FS 193.00 FRAME CUT-OUT. ( NEAR ADG STOW PUMP BASE PLATE ) (C CHECK RO 12-31-21) REPAIRED FWD EQUIPMENT BAY FLOOR SKIN AT RH FS193.00 FRAME CUTOUT (NEAR ADG STOW PUMP BASE PLATE) REF REO 670-53-11-509 REV. E SDR SWAA2021112340425Intercostal · crackedPASSENGER CABIN FLOOR STRUCTURE STA 290 BL0; INTERCOSTAL IS CRACKED AT FASTENER HOLE. / REPLACED CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 277 TO 294.5 BLO IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 141A5400 SHEET 1 REV-. LOCATED FLOORBOARD HOLES AND BONDED NEW NSDR R61A2021111900920Support · corrodedWHILE AC WAS IN FOR HVY CK FOUND FUSELAGE 3 FLOOR STRUCTURE RH PANEL SUPPORT FOUND CORRODED AT FR 89. MX REPLACED PANEL SUPPORT PN 170-86181-005 IAW SRM 51-43-03. SEE AAR NRC# 4500985-1000-0062 FOR WORK PERFORMED. AC REMAINS IN YQG FOR COMPLETION.SDR R61A2021111800906Track · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK ** FWD RH IB SEAT TRACK BTWN FR 12-29 FOUND WITH CORROSION. MX REPLACED SEAT TRACK PN 170-03263-001 IAW SRM 51-41-01, 51-41-02, 51-43-01SDR R61A2021111800910Shear Panel · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK** FUSELAGE 3 FLOOR STRUCTURE RH SHEAR PANEL BTWN FR 87-88 FOUND CORRODED. MX REPLACED SHEAR PANEL PN 170-91919-001 IAW SRM 51-43-01SDR R61A2021111800909Upper Sheet · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK** FUSELAGE 3 FLOOR STRUCTURE RH UPPER SHEET FOUND CORRODED BTWN FR-85-86. MX REPLACED UPPER SHEET PN 170-86101-001 IAW SRM 51-41-01,51-43-03SDR R61A2021111800908Shear Web · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK** FWD WET AREA FWD RH SHEAR WEB FROM FR 12-15 CORRODED. MX REPLACED SHEAR WEB PN 170-05663-003 IAW SRM 51-41-02, 51-43-02SDR R61A2021111800907Seat Track · corroded** WHILE AIRCRAFT WAS IN HEAVY CHECK** FWD LH IB SEAT TRACK BTWN FR 12-20 FOUND CORRODED. MX REPLACED SEAT TRACK PN 170-03264-001 IAW SRM 51-41-01, 51-41-02, 51-43-03, 51-43-04SDR JJBA20211103005None · noneLH OB FLOOR SILL SHOWS SIGNS OF CORROSION BETWEEN FRAMES 36-42. REMOVED AND REPLACED FLOOR SILL FRAME 36-42 LH OB SIDESDR JR2R20211103424Gusset · corrodedGUSSET AT FR90 AND RBL9 CORRODEDSDR CALA2021110402034Skin · noneDUE TO THE MAJOR REPAIR AT STATION 1985-2000 AND STRINGER 30L. AN ESFR(SIGNIFICANT FINDINGS REPORT) NEEDS TO BE SUBMITTED. REF BASE NR 000490297 UPDATED WRITEUP TO RII COMPLETED ESFR 7138978 VERIFIED ESFR 7341139 WAS SUBMITTED. UPDATE THE CORRECT ESFR NUMBER ISDR CALA2021110402033Plate · corrodedFWD CARGO PIT FR24-FR28 UPPER TORQUE BOX WEB HAS CORRODED AREAS PER HAECO LCQ NR 9292521/36521 GENERATED BY V061704 REMOVED AND REPLACED TORQUE BOX COVER SHEET AT FWD CARGO PIT BET WEEN FR 24 AND FR 28 IAW A319 SRM 51-72-11-911-001 AND SRM 51-72 -11-911-002 ANSDR JR2R20211103429Gusset · corrodedGUSSET AT RBL9 AND FR89 CORRODEDSDR JR2R20211103426None · corrodedRH FLOOR SILL CORRODED AT FR89SDR JR2R20211103419Shear Panel · corrodedCENTER SHEAR PANEL IS CORRODED AT FR 87SDR JR2R20211103431Strap · corrodedFLOOR BEAM STRAP CORRODED BETWEEN FR85 AND FR86 AT RBL9SDR JR2R20211103436Beam · corrodedFLOOR BEAM CORRODED AT FR 17 AND LBL9SDR CALA2021110302028Radome · noneBIRD STRIKE ON CLIMB.8000AGL. 250KIAS.FLAPS UP. PIC ADDED CLEANED BIRD IMPACT AREA AT TOP OF RADOME AND CAPT WINDOW. PERFORMED BIRD STRIKE INSPECTION REF AMM 05-51-14-200-803-A. NO DAMAGE FOUND. OK TO CONTINUE.SDR CALA2021110302031None · noneB767-53-3-7141 CABIN STA 544 LBL 55-68 FLOOR SUPPORT HOLE FOUND ELONGATE. TRANSFER REF. NON-ROUTINE LP 9131173 AND ORIGINATED BY EMP V927004. CABIN BS 544 FLOOR BEAM UPPER CHORD BETWEEN LBL 55 AND LBL 88 REPAIRED AS PER EC/RA 5315-01163 REV-. ADD EMP:V896920 SDR SWIA202163789None · dentedDENT FOUND ON LEFT HAND OUTER SKIN FROM FS 533 TO FS 549, BETWEEN STGR 16L AND STGR 17L. (C-CHECK RO 1/13/2022) REPAIRED DENTED AREA AT FUSELAGE STATION FS 533.00 STGR 16L TO STGR 17L PER REO 670-53-31-749 REV -- DATED 2021-12-03. PLEASE REFERENCE CONTSDR SWIA202163788None · dentedDENT FOUND ON LEFT HAND OUTER SKIN FROM FS 235 TO FS 250, AT BUT JOIN STGR16L. (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON SKIN AT FS235 TO FS250, STGR16L PER MHIRJ REO 670-53-11-1754 REV. -- DATED: 2021-11-24. PLEASE REFER TO CONTINUATION CARD FOR DISPSDR SWIA202163045None · dentedPAX DOOR HAVE A DENT ON AFT CORNER OUTER SKIN BETWEEN FS338.00 AND FS347.25 (C-CHECK RO 12/04/2021) REPAIRED PAX DOOR DENT ON AFT CORNER OUTER SKIN BETWEEN FS338.00 AND FS347.25 PER REO601R-52-11-2902 DATED 2021-11-14. COMPLIED WITH 51-900-1003-SKY.SDR JJBA20211102026None · noneMAIN CABIN CENTER BOX AREA, RH SIDE MOST O/B BUTT STRAP ATTACH ANGLE BELOW FRAME 46 PLUS "5" INCHES THRU PLUS "17" INCHES HAS SEVERAL HI-LOCS THAT HAVE SURFACE CORROSION SHOWING. REMOVED AND REPLACED OB BUTT STRAP ATTACHE ANGLE BELOW FRAME 46 PLUS "5" INCHES TSDR JJBA20211102004None · noneREINFORCEMENT SILL SHOWS SIGNS OF CORROSION AFT OF SERVICE DOOR STARTING AT FRM 22. REPAIRED AREA AT AFT OF SERVICE DOOR STARTING AT FR 22. CORROSION LEVEL 2SDR MASA20211105537None · corrodedFUSELAGE FRAME AT FS 985 WAS FOUND WITH CORROSION DAMAGE BETWEEN STR 25R AND STR 26R, THE DAMAGE IS ON THE OUTBOARD FLANGE INTERNAL SURFACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 53-61-06-003-A01, FIGURE 5453-61-06-991-804, ITEM 2, EA 69-2021-189.SDR CALA2021110302027Skin · noneDENT ALONG STRINGER 22L BETWEEN FRAME 21 AND 23 REQUIRES REPAIR PER 9290286/44286 GEN BY V079529 REPAIRED DENT ALONG STRINGER 22L BTWN FRAME 21 AND 23 IAW A319 S V079529 INSP BY V898117 RM 53-11-11-300-041 FIG.002 SHEET 01 THIS REPAIR IS CONSIDER CAT EGORY B PSDR CALA2021110302022Stringer · corrodedAFT CARGO COMPT FLOOR BILDGE STR39 RH FR61 HAS CORROSION EVIDENCE. DOT 61-052 0003827275 AND COUPLING A53986217 BATCH 0003853799 IAW SRM SHEETS 02 AND 05. WORK ACCOMPLISHED ON VT MAE N/R 0015734 BY OF ADL/REPAIR EMBODIMENT FC 60000 / FH 120000 WHICHEVER ACHIEVSDR CALA2021110302021Beam · noneB767-53-3-0166 CABIN - BS1500 RBL10 FLOOR SUPPORT HOLE ELONGATED AS MARK. TRANSFER REF. NON-ROUTINE LP 9131246 AND ORIGINATED BY EMP V896926. CABIN BS 1500 FLOOR BEAM UPPER CHORD RBL 10 REPAIRED AS PER SRM 53-00-51 REPAIR 2 FIG 201. ATTACHED FORM 44-0008 ITEMSDR CALA2021110302024Stringer · corrodedAFT CARGO COMP: FLOOR BILDGE STR42 LH FR55 HAS CORROSION EVIDENCE. DOT 61-046 BATCH 000382727 AND COUPLING A53986217 BATCH 0003853799 IAW SRM 04, 05 & 06. WORK ACCOMPLISHED ON VT MAE N/R 0015728 BY VT MAE /REPAIR EMBODIMENT FC 60000 / FH 120000 WHICHEVER ACHIESDR SWIA202162983None · crackedBAT ANGLE AT WS:48.3 RH SIDE IS CRACKED (C-CHECK RO 12-4-2021) REMOVED R/H BATT ANGLE AT WS 48.3 AND INSTALLED NEW R/H BATT RIB ANGLE P/N 600-10204 AT WS 48.3, REF: DWG 600-10204, REV: M, CRJ200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKYSDR SWIA202162982None · chafedAPRON SKIN ON LH SIDE IS CHAFED (C-CHECK RO 12-4-2021) REPAIRED APRON SKIN ON LH SIDE REF REO 601R-53-41-115 REV -A DATE 2005-07-20. COMPLIED WITH ALL STEPS OF REO 601R-53-41-115 REV -A DATE 2005-07-20 COMPLIED WITH 51-900-1003-SKYSDR SWIA202162981None · chafedAPRON SKIN ON RH SIDE IS CHAFED (C-CHECK RO 12-4-2021) REPAIRED APRON SKIN ON RH SIDE REF REO 601R-53-41-115 REV -A DATE 2005-07-20. COMPLIED WITH ALL STEPS OF REO 601R-53-41-115 REV -A DATE 2005-07-20 COMPLIED WITH 51-900-1003-SKYSDR A6WA202111227980Skin · dentedAIRCRAFT HAS 2EA DENTS LOCATED ON R/H FUSELAGE SKIN EXTERIOR BETWEEN FS 589+5 TO FS 589+8 JUST BELOW S25R. DENT DIMENSIONS (D1) 1.100L X .900W X .003D (D2) 1.100L X .900W X .009D. (P1) AND (P2) ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. SDR A6WA202111227982Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 5 EACH DENTS AT FS 589.00 TO FS 605.00 AND S24R - S25R. DENT DIMENSIONS ARE: (P1) .500L X .400W X .006D; (P2) .450L X .400W X .004D; (P3) .200L X .200W X .001D; (P4) .350L X .200W X .001D; (P5) .350L X .300W X .003D. EVALUATED DESDR A6WA202111517971Skin · dentedDENTS (11 TOTAL) ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED 11 DENTS ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. DENTS DIMENSION: FS654.50 Ï¿½ FS672.2 AND S22R Ï¿½ S23R: P1= L = SDR A6WA202111217960Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R DENT DIMENSIONS P1- L = 1.200Ï¿½ X W = 0.900Ï¿½X D = 0.006Ï¿½. PERFORMED HFEC WSDR A6WA202111117959Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSIONS P1- L = 0.900Ï¿½ X W = SDR A6WA202111107956Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT TO RE-FORM ORIGINAL CONTOUR ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. DENT DIMENSION L = 0.500Ï¿½ X W = 0.400Ï¿½ X D = 0.008Ï¿½. PSDR JJBA20211101011None · noneSMALL DENT FOUND IN BOTTOM CORNER OF MAIN DOOR. CUT OUT PERFORMED, FILLER AND DOUBLER FABRICATED. DENT ON BOTTOM AFT CORNER OF THE MAIN DOOR REPAIRED.SDR JJBA20211101010None · noneAS PER CUSTOMER REQUEST, REPAIR DOUBLER ON RH CENTER FUSE 1 BTW FR 22A-23 AND BTW STR 13R-14R, NEED TO BE REMOVED FOR INVESTIGATION. REMOVED REPAIR DOUBLER ON RH CENTER FUSE 1 BTW FR 22A-23 & BTW STR 13R-14R FOR INVESTIGATION. CUT AWAY DAMAGE ON RH CENTER FUSESDR JJBA20211101009None · noneCORROSION FOUND ON LH AFT L-SHAPE CARGO DOOR SURROUND STRUCTURE AT FR68 BTW STR 15-17. AT FR 68 BTW STR 15 AND 17 SHEAR CLIP BLENDED AND FOUND OUT OF LIMIT. "L" SHAPE AT FR68 BTW STR 15-17 LOCALLY FABRICATED. RPAIR PARTS INSTALLED ("L" SHAPE) AT CARGO DOOR FR6SDR JJBA20211101008None · noneNICKS FOUND ON TOP SKIN AROUND EXISTING REPAIR DOUBLER BTW FR 54 TO 55 AND STR 1R TO 1L IN CENTER FUSE IV AREA. ON TOP SKIN AROUND EXISTING REPAIR DOUBLER BTW FR 54 TO 55 AND STR 1R-1L, NICKS FOUND OUT OF LIMITS. ON TOP FUSE BTW FR 54 TO 55 AND STR 1R TO 1L SKSDR JJBA20211101007None · none2 DENT FOUND SKIN BTW FR 6 AND JUN 1 BTW STR 13-15 LH. ON LH FWD FUSE 1 SKIN, BTW FR 6-7 AND BTW STR 13L-15L DENTS (2X) ARE OUT OF LIMITS. PERFORMED CUT OUT AND FABRICATED REPAIR DOUBLER AND QTY 2 FILLERS. INSTALLED REPAIR DOUBLER & 2 FILLERS ON SKIN BTW FR56
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