JASC 5310
Service difficulty reports · 38,501
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 AALA202606039349Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-42-11.SDR AALA202606032186Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER SHAPE FITTING PER SRM 51-72-11.SDR CALA2026052216467Crease Beam · corrodedMAIN CABIN STA 400 RH CREASE BEAM INNER CHORD CORRODED UPPER SURFACE. REPAIRED THE RT CREASE BEAM INNER CHORD AT STA 400 IAW SRM 51-70-12-2R-1 ,51-40-02, AND BAC DWG 143A5900, REV D, AND REV-.SDR F3LA202605190416Door Sill · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FOUND CORROSION ON RT AFT DOOR SILL. REQUIRES TO BE EVALUATED IAW SRM 53-41-14 REV 49. CORROSION WAS REMOVED AND REPAIR WAS PERFORMED ON DOOR SILL AT FR. 68 IAW SRM 53-41-14 REV 49. MX ACTION IS ACCESDR SWIA2026051876419Door Frame · corrodedFRAME, FS313.56, DD4 AND DD5 IS CORRODED. REMOVED AND REPLACED CORRODED FRAME AT FS313.56 WITH NEW PASSENGER DOOR FRAME AT FS313.56 USING NEW FASTENERS, REF. SRM 51-42-06-001-001-A01 REV 38 AND BOMBARDIER DWG 601R31702 REV -N. SEE CONITNUATION STEPS FOR MORE SDR SWIA2026051876403Door Frame · corrodedCLEAT COMMON FRAME BS 338.963 IS CORRODED. REMOVED PASSENGER DOOR CLEAT COMMON FRAME BS 338.963 IAW SRM 51-42-06-001-001-A01 & INSTALLED NEW PASSENGER DOOR CLEAT COMMON FRAME BS 338.963 IAW SRM 51-42-06-001-001-A01 REV 38, AND DWG 601R31702 REV -N, & COMPLSDR SWIA2026051876269Door Sill · corrodedGALLEY SERVICE DOOR LOWER SILL IS CORRODED JUST FORWARD OF THE FORWARD DOOR FITTING. REPLACED ANGLE LOWER SILL REF DWG SH670-31950 REV Y & SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SIMA20260518004Beam · corrodedCORROSION ON LH BEAM AT FR 87, Y= -10.748". (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED CORROSION ON LH BEAM AT FR 87, Y=-10.748" IAW E-175 SRM 51-10-03. ORIGINAL THICKNESS .063 IAW EMBRAER DRAWING 170-86100-001. MATERIAL REMOVED .040" MATERIAL REMAINING .023" SDR REXA2026060400919Landing · crackedCRACKS ON AFT RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR REPLACE PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01SDR AALA202606024067Stub Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND STUB BEAM AT STA 616 BETWEEN RBL 66.00 AND RBL 70.8. REPAIRED STUB BEAM PER EA 375084.SDR AALA202606022935Stub Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT HAND STUB BEAM AT STA 616 BETWEEN LBL 68.25 AND LBL 72. REPAIRED STUB BEAM PER EA 375082.SDR SWAA2026051804069Sill Drain · odorCLIMBING THROUGH 10.000FT. FAS REPORT ACIDIC SMELL IN AFT GALLEY. GALLEY POWER WAS TURNED OFF AND SMELL DISSAPATED<[01] WITH GALLEY POWER APPLIED PERFORMED OPS CHECK OF COFFEE MAKERS PER 25-30-01 AND INSPECTED GALLEY WIRING WITH NO DEFECTS NOTED. FOUND ODER FRSDR SWIA2026051777199Pressure Deck · corrodedLEFT PRESSURE FLOOR SKIN HAS EVIDENCE OF CORROSION BETWEEN BS 513 - 529. REPAIRED LT PRESSURE FLOOR SKIN CORROSION BTWN BS 513- 529 IAW REO 601R-53-41-666, REV C. SKY CARD 51-900-1003-SKY. NO WEIGHT CHANGE.SDR AALA202605226049Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT ENTRY WAY LOWER SILL INNER CHORD (CREASE ANGLE) BETWEEN STA 947 AND STA 994 AT RBL 54. REPLACED CHORD PER AARD 51-00-05-1.SDR JR2R20260517875Beam · corrodedAFT WET AREA LBL11 O/B SIDE BEAM FR84 CORRODED. REPAIREDSDR JR2R20260517877Crossbeam · corrodedAFT WET AREA FR84 CROSSBEAM LBL11 - LBL30 CORRODED. REPAIREDSDR JR2R20260517869Crossbeam · corrodedFWD WET AREA LH CROSSBEAM FR19 FLOOR SUPPORT CORRODED. REPAIREDSDR JR2R20260517874Crease Beam · corrodedAFT WET AREA FR84 RBL11 - LBL11 CROSSBEAM CORRODED. REPAIREDSDR JR2R20260517857Beam · corrodedFWD WET AREA RBL11 BEAM BETWEEN FR12 AND FR14 CORRODED. REPLACEDSDR VNAA202607300003Door Frame · wornWEARS ON SURROUND STRUCTURE (04 CORNERS) ON FWD & CTR BAGGAGE BAY DOOR. WEARS ON SURROUND STRUCTURE (04 CORNERS) ON FWD & CTR BAGGAGE BAY DOOR WERE REPAIRED PER REO 690-52-35-643 REV. - - AND REO 690-52-35-644 REV - -SDR SWAA2026063003558Crease Beam · corrodedCORROSION ON CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208. REMOVED AND TREATED CORROSION OF CREASE BEAM WEB AT BS 727A+16 LBL 69 WL 208 PER SRM 51-10-02-0G-0 AND EA 26-153-01357.SDR R61A2026060400158Doubler · corrodedRH COCKPIT FLOOR DOUBLER IS CORRODED AT SEVERAL LOCATIONS FROM FR 8 TO FR 12 AS MARKED.TECHNICIAN REPAIRED R/H COCKPIT FLOOR DOUBLER BETWEEN FR 8- FR12 IAW 53-10-10 REPAIR 07SDR CALA2026052616540Window Frame · crackedEA 5310-08195 REV C OP 003 - OPERATION 003 - AS REQUIRED PER STEP 26 ITEM IS BEING GENERATED FOR EGNINEERING PURPOSES FOUND CRACK ON FASTENER HOLE # 2 CURRENT DIMENSION.424" AND CRACK ON #3 HOLE CURRENT DIMENSION .300" REQUIRE FURTHER ASSISTANCE. REF AAR N/R 1SDR SWIA2026051577304Fitting · wornPASSENGER DOOR CUTOUT AFT CAM FITTING WORN. REMOVED AND INSTALLED A NEW CAM FITTING IAW SRM 51-42-21-00 AND DWG 600-31900, REV K. PAX DOOR OP TESTED GOOD.SDR SWIA2026051577302Fitting · wornPASSENGER DOOR CUTOUT FORWARD CAM FITTING WORN. REMOVED AND INSTALLED A NEW FITTING ON PASSENGER DOOR CUTOUT FORWARD IAW DWG 601R31900, REV F, AND SRM 51-42-21, REV 39. OP TESTED GOOD.SDR SWIA2026051577297Door Sill · corrodedPASSENGER DOOR OPENING, LOWER SILL ANGLE HAD MULTIPLE SPOTS OF CORROSION BTWN BS 310 - 349. INSTALLED NEW LOWER SILL ANGLE IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-13, AND DWG 601R31527, REV AM, OPS TEST OF THE PAX DOOR WARNING SYSTEM WAS GOOD.SDR ASAA2026051566477Baffle · crackedLEFT BAFFLE AT BS 500J - 500K IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED BAFFLE IAW SRM 51-40-02-0G-0.SDR DALA2026051903062Pan · crackedCRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PAXCABIN. CRACK ON UPPER DOOR JAMB PAN AT LH FWD OVERWING EMERGENCY EXIT CUT OUT AT PAXCABIN WAS REPAIRED PER ER/ A 634007-14 REV ORIG. AND PRI 634007 REV 1. (1595786) (AIRCRAFT GROUNDSDR SWIA2026051477175Door Frame · damagedPAX DOOR, FRAME AT BS 327. 763 BETWEEN DD6 AND DD8. PAX DOOR, FRAME AT BS 327.763 BETWEEN DD6 AND DD8 WAS R & R BY A NEW ONE IAW SRM 51-40-11-00, SRM 51-42-06-00 AND SRM 51-42-21-00 COMPLETED TASK CARD 51-900-1003-SKY. NO WEIGHT CHANGE. REF CONTINUATION CASDR SWIA2026051477169Door Frame · corrodedPAX DOOR, FRAME AT BS 338.963 WAS CORRODED. THE DOOR FRAME WAS REMOVED & REPLACED IAW SRM 51-42-06-00, AND SRM 51-42-21-00.SDR CALA2026082718980Pressure Web · crackedCRACK FOUND AT VERTICAL PRESSURE WEB BETWEEN RBL 40.00 AND RBL 45.64. CRACK LENGTH 1". (REF AAR N/R 100012821)CUT AND REMOVED DAMAGED PART ,FABRICATED AND INSTALLED NEW REPAIR PART , [1] REPAIR WEB, NEW [2] , NEW [3] FILLERDOUBLER, [5] SHIM, AT STA 663 FROM RBSDR ASAA2026051466520Crossbeam · crackedPANEL BREAK AT STA 540 LBL 24 TO BL 0 CRACKED. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK IAW B737-800 SRM 51-40-02-0G-0.SDR ASAA2026051466519Crossbeam · crackedPANEL BREAK AT STA 540 LBL 24 TO LBL 48 CRACKED. GROUNDED - YES. REMOVED AND REPLACED IAW B737-800 SRM 51-40-02-0G-0.SDR ASAA2026051466518Crossbeam · crackedPANEL BREAK AT STA 540 LBL 60 TO LBL 48 CRACKED. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK IAW SRM 51-40-02-0G-0.SDR ASAA2026051466370Crossbeam · crackedPANEL BREAK AT STA 540 RBL 60 TO RBL 48 CRACKED. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK IAW B737-800 SRM 51-40-02-0G-0.SDR ASAA2026051466099Support Beam · damagedCENTER SECTION LOWER SUPPORT BEAM LOWER CHORD CHAFED THROUGH GROUNDED - YES. CAT A REPAIR REF SRM 57-10-13-2R-3SDR DALA2026051803042Fitting · not reportedREMOVE AND INSPECT LH PICKLE FORK FITTING PER ERA 634146-14. REMOVED AND INSPECTED LH PICKLE FORK FITTING PER ERA 634146-14AD REV. ORIGINAL. (LOG 1593271 - AIRCRAFT WAS GROUNDED).SDR DALA2026051803041Failsafe · crackedREFERENCE AA 5300-01157-02A. CRACK WAS FOUND IN THE FAILSAFE STRAP AT FRAME STA 663.75. REMOVED AND REPLACED LH & RH PICKLE FORK FITTINGS IAW ERA'S 634145-14AD REV ORIGINAL, 634146-14AD REV ORIGINAL, 634147-14AD REV ORIGINAL, 634148-14AD REV ORIGINAL, & 634149SDR DALA2026051803040Fitting · not reportedREMOVE AND INSPECT RH PICKLE FORK FITTING PER ERA 634147-14. REMOVED AND INSPECTED RH PICKLE FORK FITTING PER ERA 634147-14AD REV. ORIGINAL. (LOG 1592569 - AIRCRAFT WAS GROUNDED).SDR SWAA2026051802875Fitting · crackedPOSSIBLE CRACK FOUND ON THE S-18A WEB ASSEMBLY NEAR THE RH PICKLE FORK.<[01] C/W 26-153-01296 (AD - N7704B - MINOR ACTION - BS 663 PICKLE FORK FITTING AND STRINGER 18A WEB ASSEMBLY);[02] 26-153-01296-WIP1 (AD - N7704B - MINOR ACTION - BS 663 PICKLE FORK FITTINSDR SWAA2026051802874Fitting · crackedPOSSIBLE CRACK FOUND ON THE RH PICKLE FORK UPPER BOLTS. SUSPECT CRACK LOCATED BETWEEN FASTENER #1 AND #5 POSSIBLE CRACK FOUND ON THE RH PICKLE FORK UPPER BOLTS.<[01] C/W 26-153-01296 (AD - N7704B - MINOR ACTION - BS 663 PICKLE FORK FITTING AND STRINGER 18A WEBSDR DALA2026051503020Threshold · fodL1 ENTRY DOOR WILL NOT ARM. REMOVED DEBRIS FROM THRESHOLD. ALL FUNCTIONS NORMAL. (8615896) AIRCRAFT WAS GROUNDEDSDR JR2R20260517878Shear Panel · corrodedAFT WET AREA FR87 - FR88 RH SELL DOUBLER CORRODED. REPLACEDSDR N6WA2026051508Buttstrap · corrodedPOSSIBLE CORROSION ON FS280 BETWEEN STGR27 AND STGR26RH NEEDS EVALUATION. PERFORMED REPAIR ON BUTT STRAP AT FS280 BETWEEN STGR21R AND STGR26L IAW STS EA 129-2026-096.SDR SWAA2026062901514Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK RBL 39, BS 663+2, L: 0.300. REPAIRED HORIZONTAL PRESSURE DECK AT BS 663 - BS 675; RBL 39 - RBL 62 IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2026061002373Door Sill · corrodedCORROSION UPPER MAIN SILL ON UPPER SURFACE LOCATED BTW BS 794 TO 847, STR 18R, WL 198 IN THE AFT CARGO BAY. REPLACED UPPER MAIN SILL LOCATED BTW BS 794.37 - 847, STR 18R, WL 198 IAW SRM 51-10-02, ITEM 9, AND DWG 146A0080, SHEET 16, REV A, & DWG 146A8111, SHEESDR MAS2026F00009Crossbeam · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII, FLOOR STRUCTURE CORROSION FOUND ON CROSSBEAM AT FR 84, 3 SPOTS FROM RBL8 TO RBL 34. CROSSBEAM HAS BEEN REPAIRED IAW ETD2026-170-008647.SDR IPXA2026051761740Plate · wornPLATE, RH BODY GEAR INBD WHEEL WELL DOOR INBD FWD AND AFT STOP (REPLACE). NSTALL NEW PLATE I.A.W SRM 51-40-02-0G REV.48 AND IPC 32-14-01-01A REV.54.SDR IPXA2026051663269Plate · wornWORN PLATE , LT BODY GEAR W/W INBD DOOR FWD AND AFT STOP PLATES , INSTALL NEW PLATE I.A.W SRM 51-40-02-0G REV.48 AND BOEING DWG NO: 149U1608 SH 2 REV.- REVIEWED TASK PER GMM-MTX 09.05.01.09.SDR DALA2026051803037Fitting · not reportedREPLACE RH PICKLE FORK FITTING PER ERA 634149-14. REPLACED RH PICKLE FORK FITTING PER ERA 634149-14AD REV. ORIGINAL. (LOG 1592581 - AIRCRAFT WAS GROUNDED).
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