JASC 5300
Service difficulty reports · 8,203
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 DXTA2026101910231Unknown · unknownDURING CLIMB, MULTIPLE BUMPS WERE FELT FROM THE NOSE LANDING GEAR AREA. A TOTAL OF THREE OCCURRENCES WERE NOTED OVER APPROXIMATELY 25 MINUTES. NO CAS MSG'S.SDR IXXA20261015002Structure · mechanic errorHOLE MISDRILLED AFT OF BS 764 AT STR 2R, 2ND HOLE.SDR UIEA2026081200744Structure · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3, AT STA 260 WL 20 L/H, FOUND EXISTING HOLE SIZE 04 EA DEVIATED FROM DRAWING: 141U1192. EXISTING HOLE SIZE = 3/16, DWG HOLE = 1/4; FOUND SHORT EDGE MARGIN. FITTING COMMON TO SEAT TRACK AND CHORD P/N: 65B11784U507.(<P >L/H ANSDR UIEA2026081200745Structure · abnormalWHILE ACCOMPLISHING SB747-53A2562 R3, AT STA 260 WL 20 RH, FOUND EXISTING HOLE SIZE 04 EA DEVIATED FROM DRAWING 141U1192. EXISTING HOLE SIZE = 3/16, DWG HOLE = 1/4; FOUND SHORT EDGE MARGIN- FITTING COMMON TO SEAT TRACK AND CHORD P/N: 65B11784U508.(<P >R/H ANGLSDR IXXA20260928001Skin · corrodedAREA FWD OF ALC, INTERNAL SKIN IS CORRODED BETWEEN STRINGERS 37L-38L APPROX STA 1087. REFERENCE AMES WO N337AZ-44 NR 194024-0100-0093.SDR HNAA2026092500911Structure · damagedBIRD STRIKE TO L/H SIDE OF NOSE. PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-50-08. SEE LOGPAGE 380834-3 FOR DAMAGE MAPPING.SDR IPXA2026092251034Unknown · vibrationATB, UNKNOWN NOISE & VIBRATION FROM AIRCRAFT DURING CLIMBOUT. RESULTED IN AIR TURN BACK.SDR R61A2026100900298Stringer · corrodedCENTER FUSELAGE 3 STINGER23R HAS CORROSION AROUND RIVET HEAD AT FRAME 89-90.PERFORMED PERMANENT REINFORCING REPAIR AT CENTER FUSELAGE 3 STINGER 23R FRAME 89-90 REF. ETD2026-170-016498 REV. CSDR FDEA202609071273Floor Panel · puncturedPUNCTURED FLOOR PANEL 251KFF IN THE MAIN DECK CARGO COMPARTMENT. (ONE LOCATION) FLOOR PANEL 251 KFF , MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR 4-B FIG 201 SHEET 2 REV. 94 DEC 15/2025SDR CNMA20260910003Fastener · misinstalledIMPROPER INSTALLATION OF FASTENER LOWER FUSELAGE STATION 1217 STRINGER 39RSDR ABXR2026082800015Support · corrodedCORROSION ON THE CUTOUT/ SUPPORT STRUCTURE FOR PANEL 195ML, AT THE LEFT UPPER FILLET AREA, AS VIEWED WITH DOOR OPEN. REMOVED CORROSION FROM PNL 195ML'S SUPPORT STRUCTURE, LH UPR FILLET AREA LOST .037 FROM .080 MATERIAL IS FOUND TO BE OUT OF LIMITS. REPAIRED INSDR SWAA2026090191566Panel · delaminatedPANEL 193CR LEADING EDGE HAS AREA OF EROSION AND DELAMINATION. R&R 193CR PER AMM 53-51-21. INSPECTED C/A 1. R&R 193CR PER AMM 53-51-21.SDR UIEA2026061300476Doubler · corrodedNR 3 FUEL AFT BOOST PUMP FOUND CUTOUT DOUBLER CORROSION. DOUBLER FABRICATED AS PER BOEING DWG 65B19560 AND PL, NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR HNAA2026090100841Floor Support · corrodedLEFT FLOOR SUPPORT FROM FR 29 TO FR 35 WAS CORRODED. REMOVED AND REPLACED THE LT FLOOR SUPPORT FROM FR 29 TO FR 35 IAW SRM 51-40-02-PR, STEP 2.B AND 3.B.SDR FDEA202607281046Floor Panel · puncturedPUNCTURE ON 241AGF FLOOR PANEL, MAIN DECK CARGO COMPARTMENT ON 241AGF FLOOR PANEL, MAIN DECK CARGO COMPARTMENT WAS REPAIRED I.A.W. B767 SRM 53-00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR DALA2026071304096Not Reported · not reportedPERFORM SB 57-3081 INSPECTION AT FASTENER HOLE A AND B AT LH FR40 STG 1 AREA. COMPLIED WITH ERA 635419-14 REV ORIGINAL. (1694971) AIRCRAFT WAS GROUNDED.SDR FDEA202607070849Floor Panel · damagedPUNCTURED FLOOR PANEL 232HFF AT MDCC FLOOR PANEL 232HFF AT MDCC WAS REPAIRED IAW SRM 53-00-50-2R PAR 4-B, FIG 201, SHEET 2, REV. 94 DEC 15/2025SDR DALA2026070603921Repair · not reportedER/A 635410-14 PERFORMS A REPAIR AT FR29 & S-1 LH & RH PER SRM T ASK 53-21-11-300-087. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN THE SOONER OF 40000FC OR 80000FH FROM SECTION I AND EVERY SOONER OF 2900FC OR 5800FH THEREAFTER. ASSOCIATED ER/A 14-SDR REXA2026082401568Access Panel · corrodedCORROSION ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET AND 832FT ALSO ENLOGANTED SUPPORT ANGLE AND BROKEN ACCESS PANEL 832FT. CORROSION WAS REMOVED ON ACCESS PANEL 832AT, 832BT, 832CT, 832ET PER SRM 51-21-06-001-001-A01 AND WERE FOUND WITHIN LIMITS PER SRM 52-11SDR CALA2026062517341Adapter · damagedUPPER FUSELAGE STA 385, NR 2 TCAS ANTENNA MOUNTING SURFACE HAS MULTIPLE TOOLING MARKS. REQUIRES EVALUATION. REMOVED AND REPLACED TCAS ANTENNA ADAPTER AT UPPER FUSELAGE IAW DWG: 143A3180 REV V, PL:143A3180 REV J, SRM 51-40-02-0G -0 STEP 4, 51-40-05--0G-0, AMM SDR SWAA2026071417058Strap · no discrepancyBS 328 FRAME STRAP CONFIGURATION LOCATED ON S20R TO S22R DOES NOT MATCH WITH FIGURE 15. IAW EA 26-153-01702; THE CONFIGURATION IS ACCEPTABLE.SDR YENA2026072900632Structure · wornDURING HEAVY MAINTENANCE, WEAR VERTICAL MEMBER Y254 FR24A ON FWD CARGO BAY. WO 2026 312/1 NR 2026-391904, REPLACED VERTICAL MEMBER Y254, FR 24A IN FWD CARGO BAY IAW SRM-51-72-11.SDR FDEA202606160756Floor Panel · puncturedPUNCTURED FLOOR PANEL 242AFF. SEC 45 OF MDC. FLOOR PANEL 242AFF. SEC 45 OF MDC. WAS REPAIRED IAW SRM 53-00-50-2R PAR. 4-B FIG. 201 SHEET 2. REV. 94 DEC 15,2025.SDR SWIA2026071476646Antenna · damagedCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 07/13/2026)COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). NO SDR SWIA2026071476645Antenna · damagedCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). NO CHANGE TO WEIGHT AND BALASDR SWIA2026071476643Antenna · damagedCOMPLY WITH RT SIDE ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT DOUBLER REPAIR TO PREVIOS ANTENNA INSTALLATION AREA REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-5SDR SWIA2026071476642Antenna · damagedCOMPLY WITH LT SIDE ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) COMPLIED WITH LT SIDE ATG ANTENNA PERMANENT REPAIR. IAW DWG 170-2365-02-314 APPENDIX A. NO CHANGE TO WEIGHT AND BALANCE.SDR DALA2026060903436Not Reported · corrodedIN REFERENCE TO NRC 706 WIP NR 9, CORROSION OUT OF LIMITS AT RT SIDE. REPAIRED IAW SRM 53-00-55 (1628543) (AIRCRAFT GROUNDED)SDR CALA2026060816920Skin · damagedFUSELAGE SKIN DAMAGE AT STR20L- STA847-867. REMOVED DAMAGE TO EVALUTE 11.75 L X 5.125 W REMOVED DAMAGE AREA OF THE FUSELAGE SKIN. RECTANGLE WITH THE SIDES PARALLEL AND PERPENDICULAR TO THE STRINGER SRM 53-00-01-2R-36 REPAIR INSTRUCTIONS 4. (C) ADD EMP:U347143SDR SWIA2026052676303Antenna · out of limitsCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 06/20/2026)COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). NO EFSDR UIEA2026040800165Skin · corrodedM/D STA 1241 FWD STR-16R - STR 17R INT SKIN FOUND CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURED ORG 0.290" L:4" X W:1" X D: 0.015", WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FUSDR DALA2026052803225Not Reported · crackedREF STEP #8 RC AA5530-01048-02 AND AD 2018-10-08 4 CRACK INDICATIONS BELOW ZFS = 52.267. REPAIRED ON ERA 564482-14AD (8342877) (AIRCRAFT GROUNDED)SDR FDEA202605150612Floor Panel · crackedPUNCTURES ON FLOOR PANEL 231DFF ON MAIN CARGO COMPARTMENT. FLOOR PANEL 231DFF ON MAIN CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53-00-50-2R REPAIR GENERAL PARAG 4B FIG 201 SHEET 2 REV. 94 DEC15/2025SDR VNAA20260512012Panel · crackedCORROSION AND CRACK ON DIVERTER PANELS (3EAS). REPAIRED PER EA 5321-2026-0502 REV - -, EA 5321-2026-0501 REV - - AND EA 5321-2026-0488 REV -.SDR SCNA20260504180Door Frame · damagedFWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING WITH SHARP EDGES. DEBURRED SHARP EGES LOCATED AT FWD ENTRY DOOR FRAME AREA AFT UPPER STOP FITTING IAW AC5300-1 SECTION 11-2-2 REV K DATED 05-11-2018SDR QXEA2026051100108Seat Track · corrodedRIGHT HAND SEAT TRACK AT STATION 17-23 HAS CORROSION IN MULTIPLE SPOTS. REMOVED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-40-08 AND RESTORED FINISH.SDR QXEA2026051100113Not Reported · corrodedFRAME 19 LBL 11 CORROSION AT SCRFW HOLE ON BEAM. AFTER REWORK FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW ARM 53-10-10-02-01. RESTORED FINISH.SDR FDEA202604180486Fitting · crackedUPPER FUSELAGE - RH "N" HOLD FOUND CRACKED AT FR47 BTW STGR25 AND STGR26. REPAIRED THE CRACKED RH HOLE N IN UPPER FUSELAGE FR47 BTW STGR25 AND STGR26 PER EA 6-5310-T0387082. TITLE: FUSELAGE - MAINFRAME - FR47 RH HOLE N CRACK REPAIR BETWEEN S-24R AND S-26RSDR IXXA20260408001Skin · dentedDENT NOTED AT FUSELAGE SKIN LOWER SIDE BETWEEN BS 390 TO BS 412. AND BETWEEN STRINGERS S-38R AND S-37R. REF XTREME AVIATION NRC 166SDR MASA20260406061Floorbeam · corrodedLH FLOORBEAM SPLICE PLATE AT FR 89, LBL 11 FOUND CORRODED. CORRODED CFIII LH FLOOR BEAM SPLICE PLATE AT FR 89, LBL 11 REPLACED WITH NEW AND INSTALLED IAW SRM 51-43-03 RELATED TO YQG- NRC#4502579_2000_0286SDR VNAA202604010050Bracket · corrodedFWD CARGO MACHINED BRACKET IS CORRODED AT FS 533, BETWEEN STGR 27 AND STGR 26L. REMOVED AND REPLACED FWD CARGO BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.SDR VNAA202604010060Seat Track · corrodedHN00250014 DISCREPANCY: RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 847 AND FS 977. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK AT RBL 9 FS 850.55-977.00 IAW CRJ 700 AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A01.SDR CALA2026033014920Paint · missingDURING INSPECTION FOUND MISSING PAINT ON NOSE RADOME. DURING PHASE 2 INSPECTION FOR LIGHTNING STRIKE. FOUND MISSING PAINT ON RADOME MEASURING APPROX. 1 SQ INCH. NO STRUCTURAL DAMAGE FOUND. APPLIED CLEAR TAPE TO EXPOSED AREA PER EC/RA 5350-02074. ACCOMPLISH ASDR VNAA20260501006Skin · dentedFUSELAGE SKIN DENT WITHIN 6341.13 FH AFTER SECTION I, REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. DENT DAMAGE ON FUSELAGE SKIN BTW FS942.00 - FS954.00 AND STR21L - STR22L WAS REPAIRED PER CRJ-900 REO 690-53-51-539 REV.--SDR FDEA202603100332Floor Panel · crackedCRACK ON 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT 242TFA FLOOR PANEL ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR.4-B FIG. 201 SHEET REV.94.SDR VNAA2026031013903Not Reported · not reportedFUSELAGE STRUCTURE BETWEEN FS333.0 - FS265.0 AND STR 17R- 26R. / PERFORMED REPAIR IAW REPAIR ENGINEERING ORDER (REO) 690-53-00-638.SDR TSAA2026022800002Not Reported · crackedCRACK FOUND 3 INCH FWD OF BS 727E ALONG STR 22RSDR IPXA2026030611423Floor Support · corrodedMAJOR REPAIR, CORRODED SUPPORT, MAIN DECK FLOOR SUPPORT AT BS 1580, LBL 110. REMOVED MAIN DECK CARGO FLOOR PANEL IAW AMM 53-21-02-404-006, REV 115. INSTALLED MAIN DECK CARGO FLOOR PANEL.SDR SWIA2026022575315Dome Nut · damagedSCREW SHANK STUCK IN THE RH ATC L-BAND ANTENNA DOME NUT (MARKED). (C-CHECK RO 02/22/2026)REMOVED THE RH ATC L-BAND ANTENNA INNER DOUBLER. COMPLIED WITH REO 670-53-21-2810 DATED: 2026-02-08 REV: -A REPAIR FOR ELONGATED HOLE AND TOOLING & CORROSIOIN DAMAGE TO SDR UIEA2026013000024Junction Box · corrodedJUNCTION BOX COVER FOR RIGHT HAND BODY GEAR HAS CORROSION ON LOWER EDGE.(<P>REPAIRED AREA OF CORROSION ON RH BODY GEAR LOWER EDGE OF JUNCTION BOX PER SRM 51-70-13-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)
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