JASC 5341
Service difficulty reports · 489
Reports filed under 5341 · Fuselage, Wing Attach Fittings, 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 = '5341' 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 = '5341' 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 AU971474Frame · mis repair(AUS) FUSELAGE TO WING ATTACHMENT FRAME FILED OUT ON THE INSIDE RADIUS AND INCORRECT RIVET FITTED TO THE FORWARD WING MAIN SPAR SUPPORT. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART/REPAIR.SDR 97FDEA00861Fitting · crackedNR 0842 044 CRACK INDICATION NOTED LT 870 TERMINAL FITTING ROW 3, HOLE NR 3. REPAIRED LT BS 870 TERMINAL FITTING AS PER FED-EX EA NR7-5310-37383.SDR AU970724Fitting · corroded(AUS) UPPER RH FUSELAGE WING ATTACHMENT FITTING CONTAINED EXFOLIATION CORROSION ON LOWER SURFACESDR AU970780Block · corroded(AUS) FUSELAGE REAR SPAR WING ATTACHMENT BLOCK CRACKED AND CORRODEDSDR DHL9770220DFittings · rustedAT D-CHECK, AFT AIRSTAIRS BS 1342 LEFT AND RIGHT REAR SPAR ATTACH FITTINGS HAVE SURFACE RUST. REMOVED AND REPLACED REAR SPAR ATTACH FITTINGS AT STA 1342 LBL 19 AND RT BL 19 PER S/B 55-088.SDR DHL9770255DFitting · wornAT D-CHECK, RT 870 WING TO BODY FITTING BOTTLE PIN HOLE HAS LOSS OF PLATING AND PREVIOUS BURNISHING SPOTS. CHECKED LIMITS AT ALL AREAS. FOUND MATERIAL REMOVED AT 2 O' CLOCK POSITION AT 6 O'CLOCK AT, 7 O'CLOCK, 10 O'CLOCK AND 11 O'CLOCK. HFEC AREA OF BLEND OUSDR 97ZZZM854Bolt · crackedFRAME 27 LEFT AND RIGHT WING TO FUSELAGE LUG ATTACHMENT BOLT, LOWER, APPEARS TO BE BROKEN. REMOVED BOLTS, NDT SHOWED CRACKS IN BOLTS. CLEAN, INSPECTED HOLE, DIM CHECKS OK, ALODINE, INSTALLED REPLACEMENT BOLT IAW SRM AND FAX DJR/RJ0022-96, FRAME 29 LT/RT WITHSDR RAAA97B2005Fitting · corrodedDURING SCHEDULED C1 CHECK, FOUND LEFT AFT CENTER WING TERMINAL PIN FITTING CORRODED BETWEEN PREVIOUS REPAIR PLATES ON INBOARD FLANGE AT BS 870. REPAIRED PER S/B 727-53-27, DWG 65-82247 AND 65-78694.SDR 97ZZZX1893Bearing Attach · corrodedFRONT AND AFT BLOCKS (RIGHT AND LEFT SIDES) FOR WING SPAR ATTACHMENT SHOW HEAVY EXFOLIATION BETWEEN MAIN BOLT SPAR ATTACHMENT AND HOLD-DOWN BOLTS FOR BLOCK, MAY BE UNDETECTABLE WITH WINGS ATTACHED, EVEN WITH SKIRTING REMOVED. MIGHT POSSIBLY DO A MIRROR INSPESDR 97ZZZX1892Block · corrodedFRONT AND AFT BLOCKS (RIGHT AND LEFT SIDES) FOR WING SPAR ATTACHMENT SHOW HEAVY EXFOLIATION BETWEEN MAIN BOLT SPAR ATTACHMENT AND HOLD-DOWN BOLTS FOR BLOCK, MAY BE UNDETECTABLE WITH WINGS ATTACHED, EVEN WITH SKIRTING REMOVED. MIGHT POSSIBLY DO A MIRROR INSPESDR DHL9771284DFitting · corrodedAT D-CHECK, LEFT FORWARD BOTTLE PIN BORE HAS CORROSION ON INSIDE AFT SURFACE. REPLACED FITTING IAW BOEING DRAWING 65-16200, 64-8333 AND BOEING TELEX 32-9430.SDR AU970781Block · corroded(AUS) FUSELAGE REAR SPAR WING ATTACHMENT BLOCK CRACKED AND CORRODED BETWEEN BLOCKS AND INNER SURFACE OF SPARSDR 97FDEA00009Fitting · corrodedFUSE STA 740 LT WING ATTACH FWD FITTING CORRODED, FOR LT FWD BOTTLE BOLT. REMOVED CORROSION BY REAMING BORE PER BOEING SRM 57-10-7 FIG 2, SHEET 1. FABRICATED AND INSTALLED SLEEVE PER SRM 57-10-7, FIG 2 SHEET 5.SDR 9618129863Fitting · corrodedDURING H-CHECK, FOUND CORROSION IN THE LEFT WING FRONT SPAR FITTING BETWEEN FS 693 TO 712. REPLACED FITTING PER SRM 51-30-5, 51-30-1 AND DWG 5913055.SDR 96ZZZX2971Fitting · corrodedDURING ROUTINE INSPECTION, NOTED LOWER FORWARD CARRY-THROUGH SPAR FITITNG EXFOLIATING DUE TO INTERGRANULAR CORROSION.SDR AU960497Nut · cracked(AUS) WING ATTACHMENT BOLT NUT CRACKED - FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/BEECH33/41 - AIRCRAFT IS FOREIGN REGISTERED N93RSSDR AU960406Fitting · worn(AUS) LH AND RH WING REAR ATTACHMENT FITTINGS PNO TB2011001006 AND PNO TB2011001007 HAD LOOSE BUSHINGS AND WORN HOLESSDR AU960373Angle · cracked(AUS) WING ATTACHMENT ANGLES (2OFF) CRACKED ON INSIDE FACE AND CORRODED AROUND MOUNT HOLES AND LOWER HOLESSDR 9604469152Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE LOWER WING TO FUSELAGE ATTACH FITTING AT FS 494 BETWEEN LONGERONS 22L TO 23L. REPLACED FITTING (P/N 5910006-43) PER EA 91-109372.SDR ARWA9601001Fitting · corrodedLEFT WHEEL WELL FWD BULKHEAD, UPPER OUTER WING ATTACH FORGING AND ADJACENT SKIN HAS LEVEL II CORROSION. CLEANED CORRODED AREA, CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT CORRODED AREA, FABRICATED DOUBLER, TWO REPAIR STRAPS AND PLUG. INSTALLED IAW DER EO ASDR 9600389605Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT WING TO FUSELAGE ATTACH FITTING BETWEEN STR 22L - 23L, FS 598 - 620. REPLACED FITTING PER SRM 51-30.SDR 95FDEA01718Pin · corrodedLT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN.SDR 95FDEA01717Pin · corrodedLT REAR SPAR TO BODY TERMINAL PIN IS CORRODED. REPLACED CORRODED PIN WITH NEW PIN.SDR 95FDEA01548Fitting · crackedLT WING FRONT SPAR FWD TERMINAL PIN JOINT HOLE CRACKED AFT END. LEVELED AND SHORED A/C IAW SRM 51-50-1, CUT LOWER CHORD ANGLE AND WEB IAW BOEING DRWG NR 65C29064, REMOVED FS 740 AFT TRUNNION AND REPLACED WITH NEW AFT TRUNNION. SPLICED WEB AND LOWER CHORD ANGSDR 9514009955Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE ATTACH FITTING BETWEEN THE FS 598 FRAME AND THE CENTER WING FORWARD SPAR. REPLACED THE FITTING PER SRM 51-30-1.SDR 9513929922Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE WING TO FUSELAGE ATTACH FITTING, RIGHT AND LEFT SIDES FS 604. REPAIRED FITTINGS (P/N 5910465-33, -34), PER EA 99-97123.SDR 95ZZZX4476Spar Attach · corrodedDURING ANNUAL INSPECTION, COMPLIANCE WITH PIPER SB 977, INSPECTION OF REAR SPAR ATTACH FITTINGS IN THE CABIN FOR CORROSION, AND FOUND THIS AREA SEVERELY CORRODED. SB IS APPLICABLE TO ALL PA28, PA32, PA34, AND PA44 SERIES OF AIRCRAFT. ALL INTERIOR AND FIBERGLSDR 95ZZZX3864Fitting · pittedDURING ANNUAL INSPECTION INCLUDING PIPER SB 977, THE CABIN AFT WING ATTACH FITTINGS WERE FOUND DEEPLY PITTED ON ALL EXPOSED SURFACES. THEY HAD BEEN PREVIOUSLY CLEANED AND PAINTED (ZINC CHROMATE) WHICH STOPPED THE DECAY. MAINTENANCE RECORDS SHOW THE FITTINGS WSDR 95ZZZX3863Fitting · pittedDURING ANNUAL INSPECTION INCLUDING PIPER SB 977, THE CABIN AFT WING ATTACH FITTINGS WERE FOUND DEEPLY PITTED ON ALL EXPOSED SURFACES. THEY HAD BEEN PREVIOUSLY CLEANED AND PAINTED (ZINC CHROMATE) WHICH STOPPED THE DECAY. MAINTENANCE RECORDS SHOW THE FITTINGS WSDR 95ZZZX4251Fillet Panels · delaminatedCENTER WING FILLET PANELS NR 161-F AND NR 162-G HAVE AREAS OF DELAMINATION AND BARE METAL. REPAIRED DELAMINATED CENTER WING FILLET PANELS NR 161-F AND NR 162-G IAW TIMCO REO DC08-53-1574.SDR 95ZZZX4250Fillet Panel · corrodedCENTER WING FILLET PANEL NR 161K HAS AREAS OF CORROSION AND BARE METAL. REPAIRED CORRODED CENTER WING FILLET PANEL NR 161K IAW TIMCO REO DC8-53-1577.SDR 9510932709Chord · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE WING-TO-BODY RIB UPPER CHORD, BOTH UPPER AND LOWER FORWARD FASTENER HOLES BS 760, LBL 70.5. REPAIRED PER EA 27-98428.SDR 9509542709Rib · crackedDURING H-CHECK, FOUND CRACKS IN THE RIGHT WING-TO-BODY UPPER RIB CHORD BS 760 AT RBL 70.5. REPAIRED CHORD (P/N 65-18522-14) PER EA 27-98434.SDR 95ZZZX2611Fitting · wornLEFT WING REAR SPAR BOLT FOUND LOOSE AND CHAFING AT ANNUAL INSPECTION. BOLT HOLE IN THE FUSELAGE MOUNT WORN SPANWISE .030 INCH OVERSIZE, WING SPAN ATTACH PLATE IN THE WING WORN SPANWISE .025 INCH OVERSIZE (HOLES ELONGATED).SDR 95ZZZX2325Frame Assy · corrodedSEVERE CORROSION ON THE REAR WING CARRY-THROUGH SPAR LOCATED AT STA 128.737. THE CORROSION IS LOCATED WHERE THE WING REAR ATTACH FITTING IS LOCATED. PIPER SB 977 COVERS THIS SUBJECT. THIS CORROSION WAS VERY DIFFICULT TO DETECT EVEN WHEN COMPLYING WITH THE PSDR UPS202558Body Forging · corrodedWHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON STA 870 BODY FORGING, WL 90, RBL 65-70. INSTALLED REPAIR PER SRM 51-10-6, 51-10-2, 51-30-10, OHM 20-10-3, MM 51-20-00.SDR 95ZZZX1283Attach Fitting · corrodedDURING AN ANNUAL INSPECTION, LEFT AND RIGHT WING REAR ATTACH FITTINGS WERE FOUND TO HAVE CONSIDERABLE AMOUNT OF CORROSION ON LOWER PORTION OF FITTINGS. PIPER SB 977 PERTAINS TO THIS MATTER. ALSO, NOTED WAS CORROSION FOUND ON BOTH FITTINGS WHERE THEY PASS THRSDR 95ZZZX1282Attach Fitting · corrodedDURING AN ANNUAL INSPECTION, LEFT AND RIGHT WING REAR ATTACH FITTINGS WERE FOUND TO HAVE CONSIDERABLE AMOUNT OF CORROSION ON LOWER PORTION OF FITTINGS. PIPER SB 977 PERTAINS TO THIS MATTER. ALSO, NOTED WAS CORROSION FOUND ON BOTH FITTINGS WHERE THEY PASS THRSDR ABXA9500175Fitting · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON WING TO FUSELAGE FITTING ON TOP OF CENTER WING SECTION, RIGHT SIDE, AT STATION XCW 58 AND FS 604. REPLACED FITTING IAW DC-9 SRM CHAPTERS 51-30-5 AND 51-20-0.
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