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 IPXA2023050993161Angle · bentINSPECTION TYPE:3CL/H MLG W/W AREA O/B LWR AFT SIDE WALL ANGLE FRAME HAS A BENT.REPLACED BENT ANGEL AT THE L/H MLG W/W AREA O/B LWR AFT SIDE WALL IAW SRM 51-31-01 (MINOR)SDR IPXA2023042216071Shear Web · corrodedFAULT - SHEAR WEB CORR FRS 470/510 & LBL 11.0/33.0 DISPLACED 2 CEILING PANELS IN FWD CARGO PIT LOWER FRS 470 AND FRS 510 FOR ACCESS IAW SRM 51-40-02. REMOVED SHEAR WEB PANEL DAMAGE, IAW SRM 51-40-02. INSPECTED PANEL, OUT OF LIMITS IAW B767 SRM 53-30-53-1A-1. FSDR AALA202304263036Window Shade · faultedAIRCRAFT WAS NOT GROUNDED: THE WINDOW SHADE AT EXIT ROW SEAT 17A WON'T OPEN ALL THE WAY. **SUPPLEMENTAL REPORT FOR AALA202304193036: REMOVED AND REPLACED WINDOW SHADE AT EXIT ROW SEAT 17A PER AMM 25-21-12.** (CLOSED)SDR A6WA202304188564Cap · corroded3 EA. TOP PLATES CORRODED ON FLOOR BEAM AT FS589 BETWEEN LBL9 AND RBL9 *********AIRCRAFT REMOVED FROM SERVICE********* UPON INVESTIGATION FOUND DAMAGE TO BOTH LBL9 AND RBL 9 TO BE WITHIN LIMITS. LBL9 CAP SPLICE: LOWEST REMAINING 0.076". ORIGINAL THICKNESS WAS SDR A6WA202304188565Diaphragm · corrodedJUST FWD. OF F.S.621 @ FWD. FLOOR BEAM (PRESSURE DIAPRAM AREA) TOP BEAM CAP IS CORRODED (AS MARKED) UNDER 281CLF ********AIRCRAFT REMOVED FROM SERVICE*********** DIAPHRAGM ASSEMBLY REQUIRES REPLACEMENT RECEIVED LOCATED AND DRILLED NEW SERVICEABLE DIAPHRAGM ASDR CALA2023041901170Skin · unknownON OR BEFORE FEBRUARY 13, 2025, PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR THE FUSELAGE SKIN AND BULKHEAD CHORD REPAIR BETWEEN STA 500H AND STA 540, STR 26L AND STR 26 R ON AIRCRAFT N12216 IN ACCORDANCE WITH PART 2 OF THE LATEST REV ISSDR CALA2023041901169Intercostal · damaged(B737-06-3-0040) DAMAGED INTERCOSTAL IN MAIN DECK AROUND A NUTPLATE BS 320, LBL 45 REMOVED AND REPLACED INTERCOSTAL IN MAIN DECK BS 320 LBL 45 IAW B737-800 SRM 51-40-02-0G-0 PARA 7D. DATA WAS TRANSCRIBED FROM PA PER DOC AERSALE WO 3875 NR 29620 WORK ACP BY MECSDR 2023FA0000219Unknown · unknownLIGHTNING STRIKE BURN, FUSELAGE AND PYLON, SKINS, MULTIPLE LOCATIONS. REPORT NUMBER FR-680-0149-11733 REV - DATED 31 MARCH 2023 WITH FAA FORM 8100-9 DATED 7 APRIL 2023.SDR 2023FA0000218Unknown · unknownLIGHTNING STRIKE BURN, FUSELAGE AND PYLON, SKINS, MULTIPLE LOCATIONS. REPORT NUMBER FR-680-0149-11733 REV - DATED 31 MARCH 2023 WITH FAA FORM 8100-9 DATED 7 APRIL 2023.SDR COEA2023060703919Floorbeam · crackedWO 246760 NR 100006 HEAVY CHECK COE/MAJOR REPAIR: R/H LONGITUDINAL FLOORBEAM BETWEEN FRAMES 30-31 IS CRACKED. CORRECTIVE ACTION: REPLACED R/H LONGITUDINAL FLOORBEAM IAW EMPIRE AIRLINES E.O. 5315-01.SDR FDEA202304170800Floorbeam · crackedFOUND CRACK ON FLOOR BEAM AT STA 580 AT LBL 45 ON UPPER FLANGE LOWER AREA WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A# F-5310-T0374058-FLOOR BEAM AT STA 580 AND LBL 45- CRACKED-REPAIR PER DRAWING SR 57-53-004-TRACKING MAJOR REPAIRSDR JJBA20230426014Unknown · unknownCF1, CRACKS (2X) FOUND ON LH OMEGA BEAM #1 FLOOR STRUCTURE BTW FR 18-24. CF1, CRACKS (2) FOUND ON LH OMEGA BEAM 31 FLOOR STRUCTURE BTW FR 18-24 BEAM REPAIRED WITH 2 DOUBLERSSDR JJBA20230426013Unknown · unknownCRACK FOUND ON TOP OVERHEAD MIDDLE FRAME RH SIDE AROUND NUT PLATE ON WINDSHIELD SURROUND STRUCTURE COCKPIT AREA. CRACK FOUND ON TOP OVERHEAD MIDDLE FRAME RH SIDE AROUND NUT PLATE ON WINDSHIELD SURROUND STRUCTURE COCKPIT AREA. RIB REPAIRED WITH A DOUBLERSDR JJBA20230426012Unknown · unknownCF1, RH BEAM HAT SECTION TOP SURFACE AT FR24, FOUND CORRODED. CF1, RH, BEAM HAT SECTION TOP SURFACE AT FR24, FOUND CORRODED. BEAM REPAIRED WITH A DOUBLERSDR CALA2023041901156Beam · corroded(SUPPORT TASK) MAIN CABIN FLOOR BEAM STA 324 RBL 45 UPPER SURFAC E CORRODED. TRANSCRIBED FROM HAECO GSO NR 9280358. HAECO GSO MECH V900838 INSP QC204 REPAIRED STA 324 UPPER 7 CHORD IAW B757-200 SRM 53-10-08-2R-1 RE PAIR 1 FIG 201 THIS IS A CATEGORY B REPAIR.SDR CALA2023041901155Unknown · corrodedAFT LOWER CARGO DRAIN MAST DOUBLER AND SUPPORT BRACKETS HAS CORROSION. REMOVED DRAIN MAST DOUBLER AND BLENDED CORROSION FOUND 100% MATERIAL LOSS. FABRICATED AND INSTALLED NEW DOUBLER IAW B757- 300 SRM 51-40-02 PARA 4AND7 AND BOEING DRAWING 146N3700SDR CALA2023041901154Beam · corrodedB737-53-3-0711 MAIN CABIN FLOOR BEAM UPPER SURFACE HAS CORROSION STA 986 LBL 34 & LBL 43 REPAIRED FLOOR BEAM STA 986 IAW SRM 53-70-51-2R-6 SEE PARTIAL WO RK FOR WORK ACCOMPLISHED. DATA WAS TRANSCRIBED FROM PAPER DOC AE RSALE WO 3875 NR 29571 WORK ACP BY MECH VSDR CALA2023041901153Unknown · corrodedR2 PAX DOOR SILL HAS CORROSION MULTIPLE SPOTS. GEN BY V937268 ON HAECO LCQ NR 9290267/36267 REPAIRED AREA ON R-2 DOOR SILL IAW A320 SRM 53-41-14-300-001 ACM P BY MECH V077956 INSP BY V892442SDR CALA2023041901150Access Door · missingDUE TO REPORT OF A PANEL FOUND ON 9R AT LHR, ACCOMPLISH A GVI OF THE AIRCRAFT FOR ANY MISSING PANELS "P" AND "F". SEE GMM 02-30-95 FOR PDA PROGRAM LHRMM WENT TO AIRSIDE OPS TO COLLECT PANEL, SEE PHOTOS ATTACHED, THIS PARTS MEASURES 8"X7" IN ITS LONGEST SIDE ANSDR V0XD20230417001Unknown · chafedBAGGAGE COMPARTMENT FLOOR SILL CHAFED R/H AFT BETWEEN FRM 70- FRM 71. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SILL AT R/H AFT BETWEEN FRM 70 TO FRM 71 IAW EMB 135 SRM 51-40-02.SDR DALA2023041703021Unknown · unknown(LOG 9895654) DURING INSPECTION FOUND DENT DAMAGE NEAR STA 887 STR 26R-27L. DAMAGE IS AT AFT LWR FUSELAGE. C/W REPAIR ON NRC 003 AND ERA 607906-14 REV ORIG.SDR HNAA2023051900164Unknown · unknownE969788 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FR78 BETWEEN STR5R AND 6R. REPAIRED IAW PIEDMONT EO1-53-23-0117SDR HNAA2023051900163Unknown · unknownE969778 POSSIBLE CRACK ON EXTERNAL FUSELAGE AT FR77 BETWEEN STR4R AND 5R. REPAIRED IAW PIEDMONT EO1-53-23-0117SDR HNAA2023051900162Unknown · unknownE969647 WASTE SERVICE BUCKET (LAV BUCKET) IS CORRODED (LEVEL 2). R&R'D BUCKET IAW EMB145 SRM051-40-02. REPAIRED IAW PIEDMONT EO1-53-23-0117SDR IPXA2023042263672Shear Web · corrodedFAULT - SHEAR WEB CORROSION STA 280, RBL 18- RBL 28 REMOVED FASTENERS (50EA) AT MAIN CARGO FWD FLOOR PAN SHEAR WEB STA 280 BETWEEN RBL 18 TO RBL 28 IAW B767 SRM 51-40-02. CLEANED & INSPECTED DAMAGED AREA, PITTING CORR NOTED BETWEEN RBL 27.00 TO RBL 30.50 FROM SDR DALA2023041703020Unknown · unknown(LOG 2721314) DURING INSPECTION FOUND FLOOR SUPPORT ANGLE STA 500D-500E CHAFED. REPAIRED FLOOR BEAM (SUPPORT) AT STA 500D-500E LH IAW BOEING 737-800 SRM 53-00-53-2R-2.SDR A6WA202304158559Former · corrodedPAX DOOR FWD FORMER IS CORRODED IN MULTIPLE AREAS FS 311.75 ******AIRCRAFT REMOVED FROM SERVICE******** REMOVED AND REPLACED PAX DOOR FWD FORMER P/N601R318031-5 IAW CRJ 200 SRM 51-40-11 ,51-42-06 AND 52-42-21SDR A6WA202304158558Cleat · corrodedCORROSION FOUND ON PAX DOOR CLEAT AT FS313.56 DD4. *****AIRCRAFT REMOVED FROM SERVICE********* INSTALLED NEW CLEAT AT FS 313.56 DD4 REF CRJ-200-SRM 51-42-06 AND DRAWING 601R31702 REV NSDR A6WA202304158556Former · corrodedPAX DOOR AFT FORMER IS CORRODED IN MULTIPLE PLACES. ********AIRCRAFT REMOVED FROM SERVICE******* REMOVED AND REPLACED PAX DOOR AFT FORMER P/N 601R318034-5 IAW CRJ 200 STM 51-42-06 AND 51-42-21SDR A6WA202304158553Angle · corrodedFLOOR SUPPORT ANGLE BETWEEN RBL 18.0 AND RBL 27.0 FS 621.00 CORRODED AROUND OUTBOARD NUTPLATE HOLE *******AIRCRAFT REMOVED FROM SERVICE********* REPAIRED FLOOR SUPPORT ANGLE BETWEEN RBL 18 AND RBL 27 IAW MHIRJ REO 601R-53-61-8004 REV -- DATED 2023-04-13SDR A6WA202304158561Former · corrodedPAX DOOR FWD FORMER HAS CORROSION BETWEEN DD6-DD5 *********AIRCRAFT REMOVED FROM SERVICE******* REPLACED NEW PAX DOOR FWD FORMER REF DRAWING 601R31702 REV NSDR A6WA202304158555Frame · corrodedFRAME AT FS 333 HAS CORROSION STGR23L-25R ********AIRCRAFT REMOVED FROM SERVICE******** REPLACED FRAME AT FS333 REF CRJ-200-SRM 51-42-06,CRJ-200-SRM 51-42-21, AND DRAWING 601R32004 REV MSDR CALA2023041701133Skin · damagedEXTERNAL FUSELAGE REPAIR AT AFT EDGE OF FWD CARGO DOOR HAS DAMAG E TO EDGE OF THE REPAIR DOUBLER (RED AAR NR 99960253) T REPAIR BY ECRA 5331-02582 (DIP LOGPAGE 4368800). BOTH EXISTING DOOR CUTOUT ON AIRCRAFT N12216 IN ACCORDANCE WITH PART 2 OF THE REPAIRS WERESDR CALA2023041701132Fitting · crackedSHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED SUPPORT TASK NSA EMX N/R 00076.SDR CALA2023041701131Fitting · crackedSHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED SUPPORT TASK NSA EMX N/R 00075.SDR CALA2023041701130Fitting · crackedSHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED SUPPORT TASK NSA EMX N/R 00077.SDR CALA2023041701129Fitting · crackedSHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED SUPPORT TASK NSA EMX N/R 00074.SDR AALA202306230347Fitting · crackedAIRCRAFT IN BASE MAINETNANCE: FLIGHT DECK WINDSHIELD LEFT HAND FRAME 4 UPPER NODE FITTING FASTENER HOLE #19 CRACKED AT FR 4 BETWEEN +7675 AND +Y835. REPLACED FITTING PER EA 344137.SDR DALA2023041703019Unknown · unknown(LOG 2719718) DURING INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN LH STRG 3 STA 500. FUSELAGE SKIN LH STGR 3 STA 500, LIGHTNING STRIKE WAS REPAIRED WITH INSTALLATION OF SOLID RIVET IAW ERA 607621-14 REV. ORIGINAL AND B737-900 SRM 51-40-02-0G.SDR DALA2023041703018Plate · corroded(LOG 2719807) DURING INSPECTION FOUND FWD CARGO L/H FLOOR TRANSITION PLATE STA 480 - STA 500 HAS EVIDENCE OF CORROSION AT UPPER SIDE. FABRICATED & INSTALLED NEW REPLACEMENT TRANSITION PLATE STA480-500 L/H IAW BOEING 737-800 SRM 51-4-05, 51-40-02, 51-20-01 & SOSDR DALA2023041703017Plate · corroded(LOG 2719796) DURING INSPECTION FOUND FWD CARGO R/H FLOOR TRANSITION PLATE STA 500F- STA 500I HAS EVIDENCE OF CORROSION AT UPPER SIDE. FABRICATED REPLACEMENT SECTION OF AND INSTALLED R/H TRANSITION PLATE STA 500F - 500I IAW BOEING 737-800 SRM 51-40-05, 51-40-0SDR DALA2023041703016Baffle · damaged(LOG 2719779) DURING INSPECTION FOUND BAFFLE AT STA LH 500A-500B IS DAMAGED. REMOVED AND REPLACED BAFFLE IAW B737-800 SRM 51-40-02-0G.SDR UIEA2023041400343Shear Tie · unknownCRACK WAS FOUND ON STA 1000 FRONT SPAR BULKHEAD LBL 57.50 SHEAR TIE(<P>1) REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 97 & EO 4453C24 PART 5 REV 3. 3) PERFORM EI T2023A53M-620 REV 0. 4) ACCOMPLISHED IAW ESDR UIEA2023041400344Unknown · unknownFOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STA 1920 TO STA 1940 BETWEEN S-31R TO S-34R(<P>1) REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORM EI T2023A53M-724 SEQUENCE A REV 0. 3) PERFORMED EI T2023A53M-724 REV 1 SEQUENCE B. 4) ASDR UIEA2023041400345Unknown · unknownFOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STA 1940 TO STA 1960 BETWEEN S-48R TO S-50R(<P>1) REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORM EI T2023A53M-722 SEQUENCE A REV 0. 3) PERFORM EI T2023A53M-722 SEQUENCE B REV 1. 4) ACCSDR UIEA2023041400347Unknown · unknownFOUND SLOT CUTOUT AREA CORROSION AT STA 2154 LBL 11.33 SEAT TRACK(<P>1) REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-782 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 & DWG 65B28253, SHEET 55 REV A, SSDR UIEA2023041400348Unknown · unknownFOUND M/D FLOOR STRUCTURE CORROSION AT STA 2040 RBL 85(<P>1) REMOVED THE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-754 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 & DWG 6538102 SHEET 10 REV - ,SDR UIEA2023041400349Unknown · unknownFOUND FLOOR BEAM CORROSION AT STA 986 LBL 85(<P>1) REMOVED THE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-798 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 & DWG 65B28049, SHEET 13 REV A. 4) ACCOMSDR UIEA2023041400350Unknown · unknownCRACK DAMAGE ON STRAP OF STA 2231 AT S-16L(<P>1) REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORMED EI T2023A53M-746 REV 1 SEQUENCE B AND SEQUENCE A AND DWG 65B04-35 SH 13 REV D. 3) ACCOMPLISHED EI T2023A53M-746 REV 2. 4) CONDITION CHECK SDR UIEA2023041400351Unknown · unknownFOUND SEAT TRACK CORROSION AT STA 1015 & 1035 LBL 98.58(<P>1) REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-799 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 AND DWG 111U0805 SHEET 2 REV 3, SH
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