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 DHL2002805042Attach Angle · crackedMAIN CARGO COMPT FUS AFT CTR SPAR FRAME TO WING ATTACH ANGLE CRACKED 1.5 INCH AT STA 798.000 RBL 48.SDR AUS20020033Fitting · cracked(AUS) RT FRONT SPAR ATTACHMENT FITTING ON FUSELAGE LOCATED AT RT STN 124.250 CRACKED IN REAR LAMINATE. CRACK LENGTH 10MM (0.39IN).SDR ASOA01277Attach Fitting · damagedDURING C-CHECK INSPECTION IN BNA, THE LEFT AFT WING FITTING AT FRAME 27 WAS FOUND TO BE ELONGATED. THE HOLE IN THE FRAME WAS ALSO ELONGATED. MAINTENANCE FABRICATED A NEW FITTING AND REPAIRED THE ELONGATED HOLE IAW ASA EO 72-53-0122. THIS EO REF SRM 51- AND SDR AUS20011197Bolt · cracked(AUS) WING ATTACHMENT BOLT CRACKED. FURTHER INVESTIGATION FOUND THATTHE WASHER HAD BEEN INCORRECTLY FITTED WITH THE WASHER BEVELLED EDGE FACING AWAY FROM THE BOLT HEAD. THE WASHER WAS ALSO DAMAGED. FOUND DURING INSPECTION IAW AD/BEECH55/79 AMDT1.PERSONNEL/MAINSDR 01FDEA00805Pin · corrodedCORROSION ON LT AFT TERMINAL PIN BS 870. REMOVED AND REPLACED TERMINAL PIN PER 57-41-001-4.SDR GTIA011042Attach Angle · corrodedFTW - CENTER WING TANK TO FUSELAGE SKIN ATTACH ANGLE CORRODED, FS 880L UNDER FLOORWEB. FABRICATED AND DRILLED REPAIR DOUBLERS IAW MD80 SRM 51-10-1 AND EA SCB008. INSTALLED REPAIR IAW EA SCB 008. (M)SDR HNAA0100057Angle · crackedWING FRONT SPAR TO FUSELAGE L/H CLOSING ANGLE CRACKED. REPLACED CLOSING ANGLE.SDR 2001FA0000258Block · corrodedDISSIMILAR METAL CORROSION ON WING ATTACH POINTS. BLOCKS ARE ATTACHED TO FUSELAGE SPAR ASSEMBLY. PN 0511162-S WITH (4) AN3-21A BOLTS. REMOVE FOR INSPECTION.SDR 2001FA0000257Block · corrodedDISSIMILAR METAL CORROSION ON WING ATTACH POINTS. BLOCK ARE ATTACHED TO FUSELAGE SPAR ASSEMBLY PN 05121246 WITH (4) AW320A BOLTS. REMOVE FOR INSPECTION.SDR CALA0100237Bolt · shearedINSPECTION FOUND BOLT SHEARED IN RT WING FORWARD SPAR TO FUSELAGE ATTACH ANGLE. THE BOLT WAS REPLACED IAW SRM 51-38-01.SDR CA010411003Taper Pin · corroded(CAN) AIRCRAFT TT: 18965.4 HRS CYC: 24946 PART TT: APP. 7200 HRS. IF REPLACED AT LAST C12 INSP. TAPER PIN CONE BUSHINGS ALSO AFFECTED. PIN DID NOT COME OUT WITH MANUFACTURERS SPECIAL TOOL PRESS. NEW PINS AND CONES REQUIRED. PIN HAD TO BE DRILLED AND CUT BY MASDR COM0160009Attach Angle · crackedTHE AIRCRAFT LEFT AND RIGHT WING ATTACH ANGLES ARE CRACKED. THE ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM CHAPTER 53-20-13 PAGES 205 AND 206 AND AERODESIGN REPORT 1226-21.SDR 20001127SH015Rivet · shearedDURING ANNUAL INSPECTION, FOUND SHEARED RIVETS AT BOTH REAR WING ATTACH FITTINGS AS FOLLOWS: BS 136 RT SIDE, ALL RIVETS SHEARED THRU PLATE PN 23662-00, FITTING ASSY P/N 23663-00, DOUBLER P/N 23664-02. EXTENSIVE MOVEMENT BETWEEN PLATE AND FITTING ASSY CAUSED SDR CA001106016Bushing · cracked(CAN) DURING AD CF-82-26R1, FOUND THAT TIE BAR BUSHINGS WERE NOT OF NORMAL TYPE PER PARTS MANUAL. TIE BAR BUSHINGS WERE REMVD&VISUAL&DYE CHECK INSP CARRIED OUT ON END FITTING. DURING NDT INSPE CTION, IND.S WERE THAT CRACK RADIATING FROM BUSHING HOLE ON TOP INSDR 00683Fitting · crackedDISCREPANCY: DURING HEAVY CHECK FOUND: FUSELAGE FITTING AT FS 870 STR 18 HAS A CRACK INDICATION ON LOWER AFT BOLT HOLE CORRECTIVE ACTION: REPAIRED FITTING IAW TIMCO REO S00342 BY REAMING OUT DAMAGE AND INSTALLING A FREEZE PLUGSDR SWAA001863Beam · crackedDURING SCHEDULED D-CHECK, FOUND LONGITUDINAL BEAM CRACKED AT BS 727A, RBL 43, WL 208. REPAIRED BEAM PER ER 00-1041.SDR AU000817Fitting · corroded(AUS) LEFT AND RIGHT WING REAR ATTACHMENT FITTINGS CORRODED. (X)SDR AU000627Fitting · cracked(AUS) RIGHT LOWER WING ATTACHMENT FITTING CRACKED PER PITTS SERVICE BULLETIN 25. (X)SDR 20001127SH010Fitting · crackedCRACK FOUND DURING AN ANNUAL INSPECTION. (X)SDR DHL20070950DStructure · crackedRT WING TO FUSELAGE FILLET AREA STR 18 A CRACKED AT FS 948. VERIFIED CRACK WITH HFEC INSP. REMOVED FASTENERS PER SRM 51-30-2. FABRICATED REPAIR PER DRWNG DHL-MIA 00-00022H. STOP DRILLED END OF CRACK PER SRM 51-10-1. APPLIED PRIMER PER SRM 51-10-2. INSTALSDR ABXA9900750Fitting · crackedDURING C-CHECK, FOUND RIGHT WING TO FUSELAGE ATTACH FITTING CRACKED AT STATION 642. REPAIRED FITTING IAW ABX REA D957-33523MR.SDR 99FDEA00466Casting · scoredNR 999 - LT WING BS 870 FWD AND AFT BOTTLE PIN CASTINGS ARE SCORED, AFT CASTING HAS 2 PREVIOUSLY BLENDED (DISHED OUT) AREAS (MARKED). REMOVED SCORING AND BLENDING. INSTALL TERMINAL PIN BUSHINGS IAW S/B 727-57-0175 NSC01, EA 7521045399 AND SRM 5240-1.SDR SWAA990618Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND FWD GALLEY DOOR, LOWER HINGE CUTOUT HAS A .5 INCH LONG CRACK AT FUSELAGE SKIN. REPAIRED SKIN PER DALFORT XEA NR X2-53-241.SDR DL72S990461Fitting · corrodedAT HMV2, FOUND CORROSION IN BORES AND MATING SEAM OF AFT RT WING AND FUS REMINAL FITTINGS. BLENDED CORROSION, CHECKED, REWORKED PER ERA 366788-14, INSTALLED BUSHNG.SDR DL72K990265Pin · corrodedAT HMV, FOUND BOTTLE PIN CORRODED. PITTED ON AFT FACE, RUSTY ON CAFER, AND BORE IS CORRODED. MACHINED BORE TO 40501 PER SRM 53-40-1. REMOVED ALL PER SAME AND INSTALLED.SDR DL72K982640Fitting · corrodedAT HMV FOUND BUSHING BORE AT LT AFT BOTTLE PIN BODY BORE CORROSION. AFTER BUSHING REMOVAL FOUND SEVERAL SPOTS AROUND BORE. MACHINED BORE PER SRM 53-40-1. TREATED, REPAIRED AND INSTALLED SLAVE.SDR DHL9872057DFitting · corrodedAT D CHECK, RIGHT WING ATTACH FITTING AT STA 950 RBL 56 STR 18 A IS CORRODED. REMOVED AND REPLACED FITTING PER SRM 51-30-2, N/R 7696.SDR 98ZZZX3938Angle · corrodedWHILE C/W SB 977, CORROSION WAS FOUND ON TOP OF LEFT, AFT WING ATTACH AND LOWER CABIN DOOR POST ATTACH. SUSPECT WATER LEAKING IN AFT CABIN DOOR AT SOME PREVIOUS TIME. LEFT CABIN INTERIOR WAS REMOVED FOR AVIONICS INSTALL AND PROVIDED ACCESS FOR BETTER INSPECTSDR AU980891Bolts · missing(AUS) WING SPAR TO FUSELAGE ATTACHMENT FITTING BOLTS MISSING. 1. AN4-17A - 4 BOLTS MISSING. 2. AN3-16A - 6 BOLTS MISSING. 3. AN3-17A - 9 BOLTS MISSING. PERSONNEL/MAINTENANCE ERROR.SDR ABXA9800599Fitting · crackedSTRINGER END FITTING CRACKED AFT SIDE OF STRINGER NR 51 OUTBOARD IN NR 2 MAIN TANK AT STATION 74.000. REPAIRED IAW DC8 SRM 51-1-24 AND 51-1-20D.SDR CA980707058Tie Bar · corroded(CAN) INSPECTION PER CF82-26R1 CORROSION WAS FOUND ON END FITTINGS BEYOND .040 INCH. TIE BAR REPLACED IAW WITH SB 3/37.SDR AU981183Fitting · corroded(AUS) FUSELAGE TO RIGHT WING REAR ATTACHMENT FITTING CONTAINED INTERGRANNULAR CORROSION BETWEEN THE FITTING AND THE CARRY-THROUGH SPAR. PART TC: 11,194.SDR AU981182Fitting · corroded(AUS) FUSELAGE TO LEFT WING REAR ATTACHMENT FITTING CONTAINED INTERGRANNULAR CORROSION BETWEEN THE FITTING AND THE CARRY-THROUGH SPAR. PART TC: 11,194.SDR AU980581Fitting · cracked(AUS) LT AND RT WING/FUSELAGE ATTACHMENT FITTING CLUSTERS CRACKED IN THE FOLLOWING LOCATIONS: LT FORWARD CLUSTER CONTAINED ONE 3MM (0.118 INCH) CRACK IN THE FORWARD LUG LOWER SURFACE AND ONE 7MM (0.275 INCH) CRACK IN THE AFT LUG LOWER SURFACE. RT FORWARD CLUSDR C2XA98IA155Fitting · crackedIAH - DURING C-CHECK INSPECTION, FOND LEFT SIDE WING TO FUSELAGE FITTING AT FRAME 27 TO HAVE A CRACK INDICATION AT BOLT HOLE NR 1 USING EDDY CURRENT INSPECTION METHOD IAW ATR-42 NDTM 53-56-03. MAINTENANCE REMOVED AND REPLACED THE RADIUS FILLER IAW CONTINENTALSDR C2XA98IA154Fitting · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WING TO FUSELAGE FITTING AT FRAME 27 TO HAVE A CRACK INDICATION AT BOLT HOLE NR 2 USING EDDY CURRENT INSPECTION METHOD IAW ATR-42 NDTM 53-56-03. MAINTENANCE REPAIRED THE CRACK IAW CONTINENTAL EXPRESS ENGINEERINSDR C2XA98IA153Fitting · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WING TO FUSELAGE FITTING AT FRAME 27 TO HAVE A CRACK INDICATION AT BOLT HOLE NR 3 USING EDDY CURRENT INSPECTION METHOD IAW ATR-42 NDTM 53-56-03. MAINTENANCE REPAIRED THE CRACK IAW CONTINENTAL EXPERSS ENGINEERINSDR CA980529009Bolt · sheared(CAN) DURING THE HIGH CYCLE FUSELAGE INSPECTION, A SHEARED BOLT WAS FOUND INSIDE THE FUSELAGE IN THE AREA OF STA 190 RIGHT SIDE WHERE THE FORWARD SPAR PASSES THROUGH THE FUSELAGE. SUBMITTER STATED AS THIS ITEM IS IMPORTANT TO THE STRUCTURAL INTEGRITY OF THE ASDR AU980509Block · corroded(AUS) CARRY-THROUGH SPAR REAR WING ATTACHMENT BLOCKS (2OFF) CONTAINED SEVERE EXFOLIATION CORROSION.SDR ABXA9800265Fitting · corrodedDURING C-CHECK, FOUND RIGHT OUTBOARD T-FITTING BETWEEN FUSELAGE AND RIGHT SLANT PANEL CORRODED AT STATION 690. REPLACED T-FITTING IAW DC9 SRM 51-30-5.SDR CA980406002Tube · cracked(CAN) PRIOR TO RESKINNING, MAGNETIC PARTICLES CHECK OF TUBE REVEALED STRESS CRACKS.SDR CA980317054Bolt · sheared(CAN) THE PORT MAIN SPAR TO FUSELAGE FITTING ONE OF THE INBOARD JO-BOLTS FOUND SHEARED. FASTENER FOUND PROTRUDING APPROX .010 INCH.FASTENER SHEARED 3/8 INCH BELOW TOP OF FASTENER. BOTH INBOARD FASTENERS REPLACED.SDR DHL98726114Fitting · crackedAT D CHECK, WING FITTING CRACKED IN BORE FOR LEFT FWD BOTTLE PIN. CUT OUT SECTION OF FRONT SPAR LOWER CHORD AND SPAR WEB. REMOVED FASTENERS AND TERMINAL FITTING PER SRM. REMOVED FWD SECTION OF BL 70.5 WEB PER SRM. HFEC OF ALL HOLES. INSTALLED TERMINAL FISDR DHL9872672DBottle Pin · scratchedAT D CHECK, RIGHT AFT BOTTLE PIN FORGING IS SCRATCHED. REMOVED CORROSION AND REBORED TO 4.5 PER SRM 57-10-7, N/R 3735.SDR C2XA98IA031Fitting · crackedIAH - DURING NDT INSPECTION OF THE AFT CENTER BOLT HOLE ON THE LEFT WING TO FUSELAGE FITTING AT FRAME 27, A CRACK INDICATION WAS FOUND IN THE OUTER STRAP. MAINTENANCE REAMED THE AFFECTED HOLE TO SECOND OVERSIZE AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERSDR CALA9800195Fitting · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING TO FUSELAGE DAGGER FITTING AT STA 605, LONGERON 22-23R. AN ATTACH ANGLE REPAIR WAS INSTALLED IAW ECRA 5341-01002.SDR 98FDEA00068Fitting · corrodedCORROSION (C57-174-01) ON RT BOTTLE PIN CASTING BS 867, WL 176 TO 170, RBL 65, WHILE WORKING NR 0734. *S/D* REMOVED AND REPLACED FITTING AT BS 867, WL 176 TO 170, RBL 65 IAW FED-EX EA 7-5310-37362A.SDR CALA9800102Fitting · crackedINSPECTION FOUND A 3 INCH CRACK IN RT WING TO FUSELAGE ATTACH FITTING AT FRONT SPAR. A STRAP WAS INSTALLED ON WING TO FUSELAGE ATTACH ANGLE IAW ECRA 5340-0100.SDR 98ZZZX2730Bolt · brokenATW - RT FR 29 WING TO FUSELAGE LUG ATTACH BOLT BROKE AT STR NR 12. REMOVED AND REPLACED BOLT IAW BAE FAX DJR/RJ022-96 AND 146 MM.SDR 97FDEA00874Bottle Fitting · corrodedWHILE WORKING NR0748, DISCOVERED CORROSION ON AFT SIDE OF RT BOTTLE FITTING, BS 870, RBL 66, WL 184. *S/D* REMOVED CORROSION, BLENDED ON AFT SIDE OF RT BOTTLE PIN COATING, FOUND COATING TO BE IN LIMITS PER FED EA 7-5710-35103.
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