JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous 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 = '5720' 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 = '5720' 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 UPS96420594Web · crackedINSPECTION TYPE-C, RT WING LE FOUND CRACK IN WEB OF D-BEAM AT WS 1140. REPAIRED WEB OF D-BEAM IAW SRM 51-40-02.SDR 9614829940Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE FITTING LOCATED AT WING STR 15 AND THE RIGHT WS 69 FRAME. REPLACED FITTING PER SRM 51-30-5.SDR UPS96220631Angle · crackedINSPECTION TYPE-C, RT WING L/E RIB TO SPAR ANGLE WS 127 CRACKED. REMOVED, FAB'D AND INSTALLED ANGLE PER SRM 57-10-2, 57-10-3, 51-30-2, 51-10-2 AND DRAWING 69-20117.SDR DL757961787Te Wedge · delaminatedTRAILING EDGE WEDGE DELAMINATED. REPLACED WEDGE PER SRM 57-43-02.SDR 9615329940Splice · corrodedDURING M-CHECK, FOUND CORROSION ON THE LOWER FORWARD SPAR CAP SPLICE PLATE AT XRS 91, LEFT SIDE. REPAIRED SPLICE (P/N 3912208-1) PER EA 99-109071.SDR AALA960991Angle · corrodedTUL - CORROSION ON FRONT SPAR LOWER CHORD ANGLE, STA 196. REMOVED CORROSION. INSTALLED DOUBLER PER ESO 11697 DATED 6-17-96. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR AALA960982Angle · corrodedTUL - ANGLE, LOWER CORD ANGLE, BADLY CORRODED AROUND RIVETS BELOW LEFT EDGE FUEL TANK PLATE. REMOVED CORROSION AND INSTALLED DOUBLER PER ESO 11697. REF: E-58 NR 1771441, DATED 6-17-96. TST: 64,997 HOURS. CYCLES, 44,491. (X)SDR DL72S961580Stiffener · crackedTHE OUTBOARD ACTUATOR ATTACH RIB STIFFENER ON THE NR 2 SLAT ACTUATOR WAS FOUND CRACKED. THE DAL MFG PART NUMBER FOR THE INBOARD AND OUTBOARD STIFFENERS IS (57-0367-002). THE ERA REPLACED BOTH THE INBOARD AND OUTBOARD ATTACH RIB STIFFENERS PER EO 4-59271-3AD.SDR AALA960979Bracket · crackedTUL - FOUND HYD LINE SUPPORT BRACKET HAD LIGHT CORROSION WHEN CLEANED .5 INCH CRACK WAS FOUND. NEW BRACKET WAS DUPLICATED AND INSTALLED IN PLACE OF CRACKED PART PER DC-10 SRM 51-10-00. (M)SDR 97ZZZX319Bolts · damagedATW - INSPECT ATTACHMENT BOLTS AND NUTS OF THE REAR SPAR ROOT JOINT ATTACHMENT FITTINGS AT RIB 2 IAW EO E92/083/657C. CORRECTIVE ACTION: C/W EO E92/083/657 REV C AND REPLACED BOLT WASHER AND NUT IN POSITION E, LT REAR WING SPAR. GENERATED CARD FOR LEAK CHECSDR 97ZZZX318Jo Bolt · looseATW - REPLACED JO BOLT AT RIB 2 AND RIB ZERO PER BAE REPAIR INSTRUCTIONS HC571H9033. CORRECTIVE ACTION: REMOVED AND REPLACED ALL JO BOLTS AT RIB 2 (LT AND RT) STRINGER CROWNS AND RIB ZERO STRINGER CROWNS. ALL WORK PERFORMED PER BAE 146 REPAIR INSTRUCTIONS HSDR 96FDEA01262Pl1 Washer · misinstalledDISCREPANCY: WHILE INCREASING MTOGW (SB 57-20) DISCREPANCY WAS FOUND THAT THE PL1-20-1336 WASHER AND PL1-16-1336 WASHERS ON THE UPPER AND LOWER BOLTS (81139-20-99 AND 81139-16-99) HAD BEEN INCORRECTLY INSTALLED PER MM 20-20-01, FIG 201. (ALSO DPS 1.336). PESDR 96FDEA01183Fitting · crackedDISCREPANCY: CENTER FUEL TANK NR 2 RT COMPARTMENT STA XORS 230, 600, RIB REAR SPAR ATTACH FITTING IS CRACKED APPROXIMATELY 1.5 INCHES AT TOP (REF N0432). REMOVED AND REPLACED ARB3216-502 WITH NEW PART PER N/R 0432.SDR ABXA9700077Fitting · misdrilledDURING C-CHECK, FOUND A .1875 INCH HOLE DRILLED THROUGH THE UPPER SURFACE OF THE WING INBOARD FLAP ATTACH FITTING. REPAIRED IAW ABX REA D957-15559-MR.SDR CALA9600994Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT OUTBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. A 1.5 INCH CRACK WAS ALSO FOUND IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 8 LEADING EDGE SLAT. THE CRACKED AREAS WERE CUT OUT, REPAIRS WERE FABRICSDR CALA9600993Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 7 LEADING EDGE SLAT. THE CRACKED ANGLE WAS REMOVED AND NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2.SDR ABXA9600573Tee Cap · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON STA XRS 69 T-CAP IN THE LEFT WING. REPAIRED IAW ABX REA D957-15418-MR.SDR ARWA9606042Fillet · brokenRIGHT WING UPPER SURFACE TRAILING EDGE HAS BROKEN FILLET AT STA XRS 289.000. FABRICATED FILLET IAW DC-8 SRM 57-3-3 AND 51-1-4. REMOVED AND REPLACED FILLET IAW DC-8 SRM 51-1-15.SDR ARWA9606013Former · crackedCRACK AT LT WING LEADING EDGE FORMER AT XFS 766.250. REPAIRED AREA IN ACCORDANCE WITH CF DRAWING CF-N441J-16/96, FAA 8110-APPROVED.SDR ARWA9606012Former · crackedCRACK AT LT WING LEADING EDGE FORMER AT XFS 728.750 THROUGH 747.500. REPAIRED AREA IN ACCORDANCE WITH CF DRAWING CFN441J-16/96, FAA 8110-APPROVED.SDR ARWA9606011Former · crackedA 2 INCH CRACK AT LT WING LEADING EDGE FORMER AT XFS 766.250. REPAIRED AREA IN ACCORDANCE WITH CF DRAWING CF-N441J-16/96, FAA 8110-APPROVED.SDR 96FDEA01137I Beam · corrodedNR5046, LEFT WING AFT I BEAM DIRECTLY BELOW AND 20 I/B NR 1 SPOILER, EXHIBITS HEAVY INTERGRANDLAR CORROSION.SDR 96FDEA01127Fitting · corrodedSNRM 5054, LEFT MLG FITTING EXHIBITS EXFOLIATION CORROSION APPROX 2 SQ IN AT LEFT LWR INTERNAL SURFACE. *S/D* CLEAN AND TREAT CORROSION, REMOVED AND REPLACED LT LWR FWD AUX SPAR SPLICE PER EA 8-5710-28974.SDR 96FDEA01124Beam · corrosionSNRM 5046 LT WING - AFT I BEAM, DIRECTLY BELOW AND 20 I/B OF NR 1 SPOILER, EXHIBITS HEAVY INTERGRANULAR CORROSION. *S/D* REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-00-1, CLOSED 6/16/96.SDR AU961186Angle · corroded(AUS) DURING INSPECTION OF LH AND RH WINGS MISSING RIVET HEADS WERE FOUND ON THE WING UPPER SKIN THROUGH THE MAIN SPAR INBOARD TOP CAP - FOLLOWING REMOVAL AND DISASSEMBLY OF THE WINGS THE SEVERE EXFOLIATION CORROSION WAS FOUND ON THE FOLLOWING ANGLES ANDPLATSDR 96ZZZX4950Bulkhead · crackedDURING SCHEDULED INSPECTION, BULKHEAD WAS FOUND CRACKED AND BUCKLED AT UPPER INBD ATTACHMENT TO FUEL TANK. INITIAL CRACK APPEARS TO HAVE STARTED AT RIVET HOLE ON FLANGE ATTACHING TANK SKIN TO BULKHEAD. THIS RIVET HOLE HAD INSUFFICIENT EDGE DISTANCE. CRACK PSDR CA960614010Wing Tip · cracked(CAN) STUDENT ATTEMPTING TO LAND DRAGGED LEFT WING TIP ON RUNWAY. WING TIP CRACKED, NO OTHER DAMAGE.SDR COMA9610164Angle · crackedLEFT WING ROOT FAIRING ATTACH ANGLE IS CRACKED. REPLACED FAIRING ATTACH ANGLE.SDR 96ZZZX5197Tee Cap · corrodedDURING ACCOMPLISHMENT OF AD 90-18-03, REF DC-9, SB 57-98, REV 8, FOLLOWING DISCREPANCIES: RT WING LOWER TEE CAP AT STA XCW 58.00 BTWN STR'S 11-17 EXFOLIATON CORROSION EXISTS. REMD CORROSION BTWN STR'S 11-12, .100 INCH MATERIAL LOSS; STR'S 12-13, .067 MATL LOSDR 96ZZZX5196Tee Cap · corrodedDURING ACCOMPLISHMENT OF AD 90-18-03, REF DC-9 SB 57-98, REV 8, FOLLOWING DISCREPANCIES: RT WING LOWER TEE CAP AT STA XCW 58.00 BETWEEN STR'S 11-17, EXFOLIATION CORROSION EXISTS. REMOVED CORROSION BTWN STR'S 11-12, .100 INCH MATL LOSS; STR'S 12-13, .067 INCHSDR CALA9600948Doubler · corrodedINSPECTION FOUND CORROSION ON RT WING LOWER MAIN LANDING GEAR SUPPORT DOUBLER. THE AREA WAS REPAIRED IAW ECRA 5730-01448.SDR MALA965013Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD LOWER WING TO NACELLE TRANSIT ANGLE CRACKED AT THE LEADING EDGE AREA. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR DOUBLER IAW EA-01-96043. (M)SDR 96ZZZX3440Bulkhead · crackedFOUND TIP TANK MOUNTING BULKHEAD CRACKED. REPLACED BULKHEAD. SUBMITTER STATES CRACKING MAY HAVE BEEN CAUSED BY AN UPWARD FORCE APPLIED TO AFT END OF TIP TANK.SDR CALA9600873Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN RIB SUPPORT ANGLE INSIDE LEADING EDGE, 13 INCHES OUTBOARD OF NR 8 SLAT TRACK AT XRS 270. A SUPPORT ANGLE AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-01.SDR 96ZZZX3522Stiffener · crackedTHIS PART HAS BEEN FOUND CRACKED IN EACH OF FOUR 550'S. THE CRACKS ARE LOCATED ON THE FLANGES OF THE STIFFENER AND ARE VERY MINUTE. SUBMITTER STATED NOT SURE WHAT THE CAUSE OF THESE CRACKS ARE, THEY ARE ALL IN THE SAME LOCATION AND CAN BE SEEN BY LOOKING UP SDR UPS96220193Hat Channel · corrdedINSPECTION TYPE-C, CHANNEL AT BS 304 TO 344 RBL 17, WL 708 WAS FOUND TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED HAT CHANNEL, FABRICATED NEW CHANNEL, REINSTALLED IAW SRM 53-10-01, 51-30-2.SDR 97ZZZX2702Support · corrodedDURING CPC INSPECTION, THE FOLLOWING LEVEL 2 ITEMS WERE NOTED: W/C 0067, RT W/W STA 870 SUPPORT UNDER SPOILER MIXER. ALL ITEMS WERE CORRECTED DURING C-CHECK ON THE LISTED CARDS. REF: OPERATOR CONTROL NR GAIA9731 AND 97ZZZX2697 THROUGH 97ZZZX2701.SDR AU960930Block · failed(AUS) DURING INVESTIGATION OF A WRINKLE IN THE FABRIC COVERING ON THE TOP WING (INBOARD) TRAILING EDGE, THE DRAG/ANTI-DRAG WIRE REAR ATTACHMENT BLOCK AT REAR SPAR WAS FOUND BROKEN WHICH IN TURN CAUSED THE TRAILING EDGE TO CENTRE HOOP ATTACHMENT BLOCK TO FAILSDR 97ZZZX2833Block · failedAUS - DURING INVESTIGATION OF A WRINKLE IN THE FABRIC COVERING ON THE TOP WING (INBOARD) TRAILING EDGE, THE DRAG/ANTI-DRAG WIRE REAR ATTACHMENT BLOCK AT REAR SPAR WAS FOUND BROKEN WHICH, IN TURN, CAUSED THE TRAILING EDGE TO CENTRE HOOP ATTACHMENT BLOCK TO FAILSDR DL757961766Te Wedge · delaminatedTRAILING EDGE WEDGE UPPER AND LOWER SKIN DELAMINATED AT INBOARD END. REPLACED TRAILING EDGE WEDGE. REF SRM 57-43-02.SDR AALA960597Angle · corrodedTUL - FOUND CORROSION ON FRONT SPAR LOWER CHORD ANGLE UNDER LEADING EDGE PANEL. REMOVED CORROSION AND INSTALLED CHORD ANGLE REPAIR PER SRM 57-30-2 PAGES 1-3 FIG 1. (M)SDR 96ZZZX3027Angle · crackedMCI - DURING SPECIAL CHECK, FOUND A 2 INCH CRACK AT TOP OF CLOSURE RIB ATTACH ANGLE IN RIGHT WING, IWS 503. REPAIRED BY INSTALLING NEW ATTACHED ANGLE PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 2. AIRCRAFT TT: 60,229 HOURS; 22,908 CYCLES.SDR W8PA960043Fitting · corrodedPITTING DISCOVERED ON OVERWING ATTACH FITTING JUST FORWARD OF FRONT SPAR. BLENDED OUT AND APPLIED PRIMER PER SRM 57-20-90. (X)SDR DHL9670911CAngle · corrodedAT C-CHECK, FOUND CORROSION ON TRAILING EDGE ANGLE AT OUTBOARD HINGE OF OUTBOARD AILERON OF LEFT WING. REMOVED AND REPLACED LOWER ATTACH ANGLE PER SRM 51-10-1, REPAIR 10 BY 2 BY 1.SDR UPS96820223Fitting · crackedINSPECTION TYPE-C, STR NR 58 FITTING CRACKED AT O/B END APPROX XRS 435, ACCESS PANEL 505B, RT WING NR 4 ALT TANK. REMOVED AND REPLACED STRINGER END FITTING IAW SRM 51-1-8, 51-3-2 AND 51-1-23.SDR UPS96220068Stiffener · corrodedINSPECTION TYPE 'C', CORROSION ON LT WING FRONT SPAR VERT STIFFENER 5TH STIFFENER O/B FROM ACCESS CUTOUT 7340. REMOVED CORRODED STIFFENER, INSTALLED NEW SIFFENER PER SRM 51-3-2, 57-10-4 AND MM 28-11-0.SDR EISA96045Angle · crackedLEFT WING SKATE ANGLE CRACKED AT AFT HOLE, JUST OUTBOARD OF NR 4 FLAP TRANSMISSION, WING LOWER SURFACE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-03. (M)SDR 9611532295Web · crackedDURING H-CHECK, FOUND A 3 INCH CRACK AND BUCKLING OF THE RIGHT WING AUXILIARY SPAR NR 5 SPOILER SUPPORT WEB. REPAIRED WEB (P/N 65-16216-150) PER EA 22-105281.SDR UPS96820075Cap · crackedINSPECTION TYPE 'C', UPPER AUX SPAR CAP HAS CRACK IN ATTACHMENT HOLE WHICH EXTENDS TO EDGE. DRILLED FITTING AND INSTALLED IAW 51-3-2, 51-1-20D AND 51-1-24 TO BE INSTALLED ON UPS TASK CARD NR 1056.SDR UPS96820073Cap · crackedINSPECTION TYPE 'C', LWR AUX SPAR CAP HAS A CRACK IN THE BOLT HOLE. DRILLED NEW FITTING AND INSTALLED FITTING IAW SRM 51-1-20D, 51-3-2, 5 1-1-24 AND UPS EO DC8-5720-0956F.
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