JASC 5310
Service difficulty reports · 38,479
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 SWAA2026061505461Crossbeam · crackedBREAK PANEL SUPPORT CRACKED AT BS 540, RBL 1, WL 208.1. REMOVED AND REPLACED BREAK PANEL SUPPORT AT BS 540, WL 208.1, RBL1 IAW SRM 51-40-02, AND DWG 143A0060, REV A.SDR SWAA2026070105686Window Frame · crackedCAPTAINS #1 WINDOW FRAME HAS CRACK IN LOWER INBOARD CORNER<[01] ACCOMPLISHED HFEC SURFACE SCAN OF SUSPECTED CRACKED LOCATION IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. REMOVED SKIN PANEL 141A3816-9 TO F.O.M I.A.W SRM 51-40-02-0G-0. INSTALLED FASTENESDR AALA202605282771Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL AT STA 540 AND BL 0. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR AALA202605280520Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL AT STA 540 AND LBL 12. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR AALA202605286761Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL AT STA 540 AND RBL 1. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR DALA2026052703211Fitting · damagedDURING M2 AND WHILE ACCOMPLISHING EM 2515-01014-02A, MATERIAL BURR WAS FOUND IN THE LT LWR LATERAL FITTING OF RACK FIN 80VU. PER SECTION II OF ER/A 633192-14AD ACCOMPLISH SECTION II INITIAL INSEPCTION WITHIN 19,500 FC FROM SECTION I (22MAY26). REPEAT SECTION SDR DALA2026052703180Fitting · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D PER ER/A 633743-14AD FOR MIRROR FITTING INSTALLATION AND CONTI NUITY FITTING REPLACEMENT. SECTION I IS LIMITED TO 60000FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/CSDR DALA2026052703179Fitting · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR MIRROR FITTING REPAIR AND CONTINUITY FITTING REPLACEMENT PER ER/A 633743-14AD. C/A: SECTION I IS LIMITED TO 29500FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATESDR DALA2026052703178Fitting · not reportedER/A 633743-14AD ISSUED FOR CONTINUITY FITTING REPLACEMENT AND MIRROR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 27000FC FROM SECTION I AND EVERY 4700F C THEREAFTER. ASSOCIATED ER/A 14-633743 ADDED FOR AC 3168. (LP: 1607258) AIRCRASDR 4VAA202605210022Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FRAME AFT OF THE CARGO DOOR. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060682.SDR VNAA202607310001Door Sill · corrodedCORROSION ON LOWER SILL BTW FS1000 TO FS1047 AT SURROUND STRUCTURE OF THE AFT BAGGAGE-BAY DOOR CUT OUT. CORROSION ON LOWER SILL BTW BS 1000 TO BS 1047 AT SURROUND STRUCTURE OF THE AFT BAGGAGE-BAY DOOR CUT OUT WAS REMOVED PER CRJ-900 SRM 51-21-06-001-001-A01 SDR VNAA202607300002Door Frame · wornWEARS ON SURROUND STRUCTURE (04 CORNERS) ON FWD & CTR BAGGAGE BAY DOOR. WEAR 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 ASAA2026052167094Plate · corrodedAFT CARGO L/H SIDEPLATE IS CORRODED FROM STA 727-787. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO L/H SIDEPLATE FROM STA 727-787 I.A.W. B737-800 SRM 51-40-02-0G-0W= 1 1/2" O= .040 R= .030 L= 1" D= .010.SDR ASAA2026052166971Door Sill · corrodedFWD CARGO DOOR SILL WEB HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO DOOR SILL WEB IAW SRM 51-40-02-0G-0.SDR ASAA2026052166970Web · corrodedAFT CARGO DOOR SILL WEB IS CORRODED. GROUNDED - YES. REMOVED CORROSION SILL WEB FOUND OUT LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED AFT CARGO SILL WEB IAW SRM 51-40-02-0G-0.SDR DALA2026052703214Window Frame · damagedSHIP 3241 DISC: DTE ERA 633400-14AD REV. ORIGINAL. REPAIR AT FR4 LATERAL WINDOW FRAME REQUIRES DTE FOLLOW UP PRIOR TO 64,502 TFC. C/A: REVISE AND UPDATE ERA 633400-14AD WITH DTE RESULTS PRIOR TO 64,502 TFC. REFERENCE AIRBUS DOSSIER 81769612. ASSOCIATED AA 5311SDR FDEA202605210634Door Frame · crackedRH PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPLACED THE CRACKED SEGMENT ON RH PAX DOOR FRAME AT FR14C PER A300-600F SRM51- 40-21 AND DWG: F52181299(ISSUE: G). RSC TRACKING EA: 6-5210-T0387549 RAISED AND ACCOMPLISHED. TITLE: DOORS - PASSENGER/CREWSDR CALA2026052516490Panel · corrodedNLG WHEEL WELL PANEL 113BW HAS SURFACE CORROSION ADJACENT TO ATTACHMENT FASTENER. EVALUATED PANEL TO BE BEYOND REPAIRABLE LIMITS IAW SRM 53-10-14. RECEIVED REPLACEMENT PANEL IAW AIPC 32-22-11-02 ITEM 35 FOR EFFECTIVITY.SDR CALA2026052516488Panel · corrodedNLG WHEEL WELL PANEL 114AC HAS SURFACE CORROSION ADJACENT TO ATTACHMENT FASTENER. EVALUATED PANEL TO BE BEYOND REPAIRABLE LIMITS IAW SRM 53-10-14. RECEIVED REPLACEMENT PANEL IAW AIPC 32-22-11-02 ITEM 35 EFFECTIVITY. EVALUATED PANEL TO BE BEYOND REPAIRABLE LSDR AALA202605228100Door Frame · unsecureAIRCRAFT WAS NOT GROUNDED: FLLIGHT DECK DOOR STICKS AND IS HARD TO OPEN / CLOSE. MAINTENANCE RE-TORQUED FLIGHT DECK DOOR FRAME SCREWS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-51-11.SDR AALA202605218726Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT FRAME INNER CHORD FITTING AT BS 787 AND LEFT S18A. REPLACED FITTING PER EA 374293.SDR REXA2026080401422Door Sill · crackedCRACK ON AFT RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR). AFT RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ-900 SRM 51-42-10-0SDR SWAA2026062505064Crossbeam · crackedCRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABI IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 143A0060; SHEET: 46; REV - .SDR SWAA2026062505068Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN I.A.W B737-700 SRM 53-40-51-2R-2 REPAIR 2; SRM 51-40-02.SDR CALA2026060116672Stub Frame · crackedR1 DOOR CUTOUT FWD LOWER STUB FRAME CRACKED AT LOWER I/B AREA REF AAR N/R 100028200 REMOVED AND REPLACED R1 DOOR CUTOUT FWD LOWER STUB FRAME PER B737-800 SRM 51-40-02-0G-0 AND DRWG # 141A8370. WORK ACCOMPLISHED BY V927234 INS-10 CREATED SFR ESFR INFORMATION UPSDR JR2R20260520864Doubler · corrodedFWD WET AREA FR16 L/H FWD DOUBLER CORRODED. REPLACED PER SRM.SDR SWIA2026051976994Door Sill · corrodedFOUND CORROSION IN MULTIPLE AREAS ON PAX DOOR LOWER SILL UNDER FUSELAGE SIDE HALF HINGE BETWEEN BS 310 - 349. COMPLIED WITH REO 601R-53-21-3820 REV-.SDR REXA2026070301034Door Frame · crackedCRACK ON UPPER AFT SHIELD OF CORNER FRAME AT FWD BAGGAGE DOOR. UPPER AFT SHIELD OF CORNER FRAME AT FWD BAGGAGE DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-41-02-001-001-A01SDR 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 07
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