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 QXEA9700619Angle · crackedPDX - BACKUP STRUCTURE ANGLE IS CRACKED. REPAIRED IAW SRM 57-02-08 PAGE 2.SDR P5CA9701513Brace · brokenLEFT WING SUPPORT BRACE BROKEN BY NR 6 LEADING EDGE. REMOVED AND REPLACED TUBE ASSY AS PER BOEING MM 57-21-00.SDR DL72S971673Stiffener · crackedFOUND DURING A-1 LETTER CHECK, FOUND 1.5 INCH CRACK AT WING L/E VERTICAL STIFFENER NR 6 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21.SDR RRXA97251Angle · corrosionDURING C-CHECK INSPECTION, FOUND LT WING INBD L/E UPPER SCREW ATTACH HOLES CORRODED AT ATA XFS 41 TO 55. *S/D* REMOVED CORROSION AND FOUND LEADING EDGE UPPER SPAR ATTACHMENT ANGLE DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED ATTACHMENT ANGLE, FABRICATEDSDR MWEA97742Doubler · out of limitsDURING D-CHECK, FOUND A PREVIOUSLY BLENDED AREA ON RT WING LOWER SURFACE AT STA XRS 295. MTC REPAIRED IAW SRM 57-03 FIG 24.SDR P5CA9701447Angle · crackedCRACKED WING LEADING EDGE STIFFENER WEB AT NR 18 LEADING EDGE DEVICE. REPAIRED PER BOEING SRM 51-30-02.SDR AALA971591Stringer · crackedTUL - CRACK IN MOUNTING FLANGE FOR FUEL COMPENSATOR. REPLACED STR NR 8 INSIDE LEFT WING PER AARD 57-20-00-11 AND ESO 7349 DATED 8-18-97. TST: 77,609 HOURS. CYCLES: 23,351. (X)SDR MZZA97252Hilock · fuel leakKUL - DURING B-CHECK FOUND FUEL LEAKAGE FROM TOP OF RIGHT HAND PRIMARY EXCHANGER AFT SIDE. LEAK TRACED TO PREVIOUS REPAIR OF LOWER STIFFENER, AFT OF REAR BAFFLE, CONSISTING OF 15 HILOCKS. 14 HILOCKS REMOVED, 14 REINSTALLED IAW SRM 51-30-2. ONE HILOCK OVERSISDR DL72S971659Stringer · crackedRIGHT WING STRINGER TO RIB AT WS 656.50 STR 5 HAS CRACK FROM HOLE AND ALONG ANGLE. STARTED DRILLING REPAIR PER M/M 57-13-0. DISCONNECTED LINE AT WS 686.5 AND COMPLETED DRILLING. REINSTALLED VENT LINE AND WIRE CLAMPS.SDR ABXA9701862Doubler · crackedRIGHT WING CENTER LEADING STATION XFS 518 HAS CRACK ORIGINATING FROM FASTENER HOLE. REPAIRED IAW ABX REA D857-20383MR.SDR 9715819619Bracket · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON CENTER WING MAIN FRAME TIE FITTING FS 598 TO 617, RBL 58. REPLACED FITTING (P/N 5913055-502) PER SRM 51-30-05.SDR CKSA97484Chord · corrodedDURING ROUTINE CPCP CHECK INSPECTION, FOUND INTERGRANULAR CORROSION ON LOWER CHORD LBL 48, FS 740 FUEL TANK CENTER SECTION. INSTALLED DOUBLER REPAIR IAW EA B2-57-008 DTD 12 AUG 97 AND IAW SKETCH NR AIA/E/2608 REV A DTD 11 AUG 97. CORROSION TASK CARD NUMBER CSDR AALA971536Angle · corrodedTUL - FOUND CORROSION ON LATERAL FALSE SPAR UPPER AFT CAP ANGLE. INSTALLED SHIM AND REINSTALLED ARC0295 SUPPORT POST PER ESO 7349 DATED 8/11/97. (M)SDR P5CA9701411Fasteners · brokenRIGHT WING PANEL UPPER FASTENERS DAMAGED. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.SDR P5CA9701410Fasteners · damagedRIGHT WING UPPER LEADING EDGE DAMAGED FASTENERS. REMOVED AND REPLACED FASTENERS PER BOEING SRM 51-30-02.SDR 98ZZZM58Stiffener · crackedLEFT WING, TRAILING EDGE AREA AFT OF REAR SPAR HAS A CRACKED STIFFENER ON LOWER SHROUD SKIN BETWEEN WING RIBS NR 7 AND 8. REPLACED STIFFENER AND PAINTED.SDR ABXA9701345Angle · crackedRT WING L/E STA XWO RIB ATTACH ANGLE TO UPPER FRONT SPAR CRACKED. REPAIRED IAW DC-8 SRM 51-3-0, 51-1-8 AND 51-1-1.SDR 98ZZZM57Stiffener · crackedLEFT WING T/E SHROUD AREA BETWEEN WING WIBS NR 8 AND 9 HAS THE TWO UPPER SKIN STIFFENERS WITH CRACKS AT THEIR FWD ENDS. REPAIRED OUTBOARD STIFFENER PER FAX JM/RJ0317/97, REPLACED INBOARD STIFFENER PER SRM ALSO REF BAE FAX RA/RJO595-97.SDR 98ZZZM56Bracket · crackedLEFT WING T/E AREA AT WING RIB NR 8 HAS A CRACKED HYD LINE BRACKET WHICH IS ALLOWING HYD LINE TO CHAF ON THE TAIL RIB. HYD LINE IS GOING OUT OT OUTBOARD LIFT SPOILER JACK. INSPECTED LINE OK. REPLACED CRACKED BRACKET.SDR QXEA9700537Fitting · chafedPDX- LEFT HAND NR 3 BATHTUB FITTING CHAFED BY THE FLAP SECONDARY DRIVE HOUSING. REPAIRED PER EA 9-53-312.SDR QXEA9700536Fitting · chafedPDX- RIGHT HAND NR 3 BATHTUB FITTING CHAFED BY FLAP SECONDARY DRIVE HOUSING. REPAIRED PER EA 9-53-311.SDR P5CA9701523Support Beam · crackedCRACK RIGHT WING SPOILER SUPPORT BEAM MOST INBOARD PORTION. REPAIRED PER BOEING SRM 51-40-03.SDR QXEA9700535Intercostal · crackedPDX- INTERCOSTAL AT OUTBOARD OIL COOLER HINGE IS CRACKED. REPAIRED PER EA 9-54-135.SDR 97ZZZX3956Doubler · crackedDURING SERVICE CHECK AT ANC, RT WING NR 6 PLANK LEAP DOUBLER WAS DISCOVERED CRACKED AT RWS 257. CRACK RAN BETWEEN FASTENERS. VERIFIED RACK DID NOT CONTINUE BY BOLT HOLE EDDY CURRENT AFTER FASTENER REMOVAL. REPAIRED BY PATCHING PER DRAWING NR C95-R02 AND SESDR 97ZZZX3955Doubler · crackedDURING SERVICE CHECK AT ANC, A CRACK WAS DISCOVERED IN LWS 248 DOUBLER AT NR 4 PLANK. CRACK RUNS FORWARD .20 INCH AND AFT .075 INCH FROM FASTENER HOLE. REMOVED CRACK PER LAC SRM 57-2-1, PAGE 41. DEFECT CONSIDERED NEGLIGIBLE DAMAGE AFTER CLEAN UP, SEALED ARESDR 97ZZZX3954Doubler · crackedDURING SERVICE CHECK AT ANC, NR 6 LEFT WING PLANK LEAP DOUBLER WAS DISCOVERED CRACKED, LWS 237.30. LONG CRACKS EMANATED FROM FASTENER HOLES. RECEIVED LOCKHEED AUTHORIZATION TO CONTINUE SERVICE UNTIL PHASE CHECK NOT TO EXCEED 500 HOURS. RE-INSPECTED AREA OF SDR 98ZZZM50Stiffener · crackedLEFT WING TRAILING EDGE AREA AFT OF REAR SPAR BETWEEN WING RIBS NR 7 AND 8 HAS AN UPPER SKIN STIFFENER THATS CRACKED AT FORWARD END. REPAIRED IAW ATTACHED FAXES RA/RJO595-97 AND OTHERS RELATED.SDR 97ZZZX4302Reinforcement · corrodedSEVERE CORROSION FOUND DURING ANNUAL. THIS OCCURED SINCE LAST ANNUAL JULY, 1996. CORROSION COULD NOT BE OBSERVED THROUGH INSPECTION HOLES IN WING. CAN ONLY BE SEEN WITH AILERON FULLY IN UP POSITION AND LOOKING UPWARD FROM THE GROUND. IT IS NOT READILY SEENSDR 97ZZZX3950Doubler · crackedDURING SERVICE CHECK INSPECTION AT ANC, A LEAP DOUBLER CRACK WAS DISCOVERED AT WS 240R. CRACK LENGTH WAS 1.3 INCHES; AN ADDITIONAL CRACK WAS DISCOVERED AT RWS 241.75, .50 INCH LENGTH. REPAIRED BY PATCHING PER LAC SRM CHAPTER 57-2-1, PAGE 43. SEALED AREA PERSDR P5CA9701519Support · corrodedLEVEL 2 CORROSION RIGHT WING LEADING PANEL LOGITUDINAL SUPPORT AT ILES 445 AND 476. REPLACED PER BOEING SRM 51-10-01.SDR 97ZZZX3685Bathtub Fitting · brokenWHILE JACKING UP AIRCRAFT DURING ANNUAL INSPECTION, A 'POPPING' NOISE WAS HEARD COMING FROM CENTER SECTION. INSPECTION REVEALED RIGHT CENTER SPAR STRAP BATHTUB FITTING HAD ITS UPPER FORWARD EAR BROKEN OFF. THIS STRAP HAD BEEN INSTALLED UNDER HAMILTON STC NR SDR P5CA9701518Support Beam · crackedCRACK LEFT WING SPOILER SUPPORT BEAM WEB LOWER CHORD AT OUTBOARD OF NR 6 SPOILER AREA. REPAIRED PER BOEING SRM 51-40-04.SDR DL72S971509Stiffener · crackedWING L/E SPAR STIFFENER CRACKED NR 4 SLAT INBD TRACK INBD SIDE. REPLACED ANGLE PER M/M 57-20-21.SDR 97FDEA00490Clip · crackedAT STA XORS - 402, STRINGER NR 37, FOUND CLIP CRACKED ON RIGHT WING LOWER SURFACE. *S/D* REMOVED AND REPLACED CLIP (REF DWG ARB 0807), PER SRM 51-31-01.SDR 97FDEA00489Clip · crackedAT XORS - 402, STRINGER NR 36, FOUND CLIP CRACKED ON RIGHT WING LOWER SURFACE. *S/D* REMOVED AND REPLACED CLIP (REF DWG ARB 0807), PER SRM 51-31-01.SDR 97FDEA00488Clip · crackedVCE: N 1617, AT STA XORS 402, STRINGER NR 36, FOUND CLIP CRACKED ON LEFT WING LOWER SURFACE.SDR MWEA97680Angle · corrosionDURING D-CHEC, FOUND CORROSION ON RT WING LOWER 'T' ANGLE OUTBOARD LEG STATION 58 INBETWEEN STRINGERS 16 AND 1, MTC REPAIRED IAW DAC DRAWING 5910465 AND SRM 51-30-5 AND 51-30-2.SDR UPS97824038Doubler · corrodedINSPECTION TYPE-C, MODERATE CORROSION UNDER WING BOX FINGER DOUBLER FS 920 TO 922 LBL 60. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW SRM 53-1-0 AND 51-1-20D.SDR UPS97824458Fitting · corrodedINSPECTION TYPE-C/CK, LEFT HAND STA 98 LOWER SUPPORT FITTING OUTBOARD STUD MOUNTING HOLE H AS PITTING CORROSION. REPAIRED IAW REO 03417 REV A, FASTENERS TO BE INSTALLED ON UPS NR 70 7586.SDR UPS97824140Clip · crackedINSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 THE UPPER ATTACH CLIP IS CRACKED IN HALF. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 57-5-2, 51-1-21, 51-1-20D.SDR UPS97224001Str Vent Tab · crackedINSPECTION TYPE-C, RT WS 629.0 STR 14 VENT FWD TAB IS CRACKED. ALSO, STR 13 IS CRACKED. CRACKS IN TABS AT STR 14 AND STR 13 STOP DRILLED IAW EO B727-5710-0 314 APP 8.3, REPAIR CARRIED OUT IAW EO B727-5710-0314 APP 8.3SDR CALA9701180Angle · crackedINSPECTION FOUND A 2.25 INCH CRACK IN ANGLE INSIDE LT WING FIXED LEADING EDGE AT NOSE RIB, SLAT STA 0. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-1 AND 51-30-2.SDR UPS97824374Doubler · crackedINSPECTION TYPE-C/CK, REPAIR IS CRACKED ON INTERNALS L/E SECTION BETWEEN NR 1 AND NR 2 PYLONS AT I/B END OF SLOT DOOR. REPAIRED IAW 57-2-1 BY FABBING NEW DOUBLER, INSTALLED IAW DC8 51-30- 0 AND 57-2-1 ALODINED AND DPRIMED AS REQUIRED IAW DC8 SRM D51-1-8.SDR MWEA97659Strap · corrodedDURING D-CHECK, FOUND LEFT WING STRINGER NR 22 FORWARD FLANGE UPPER SURFACE PREVIOUSLY BLENDED. MTC REPAIRED IAW 57-08 FIG 2 SHEET 1 AND TELEX SVC-ORD-0162/KJL.SDR MWEA97658Doubler · corrosionDURING D-CHECK, FOUND RIGHT WING LOWER SKIN HAS AREA OF PREVIOUS CORROSION BLENDING SURROUNDING ACCESS PANEL 1474A. MTC REPAIRED IAW DOUGLAS TELEX SVC-ORD-0129/KJL.SDR UPS97824461Aux Spar · elongated holesINSPECTION TYPE-C/CK, LEFT MAIN LANDING GEAR OUTBOARD AUX SPAR HAS ELONGATED HOLES ON VERTICAL UPPER AND LOWER HORIZONTAL FLANGES. REPAIRED IAW REO 03047 BY INSTALLING REPAIR BUSHINGS IAW DC8 SRM 51-1-25.SDR UPS97824415Fitting · crackedINSPECTION TYPE:C/CK, STRINGER END FITTING IS CRACKED AT APPROX XRS 365-370 LOWER STRINGER 66 LEFT WING. REMOVED CRACKED END FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-2 AND 51-1-21.SDR 9714309619Clip · corrodedDURING M CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON STRINGER CLIP FITTING AT WS 111 BETWEEN STR 13 AND 14. INSTALLED NEW CLIP (P/N 4911499-615) PER SRM 51-30-05.SDR W8PA971365Hinge Structure · crackedLEFT WING T/E, CRACK DISCOVERED OUTBOARD EDGE OF LOWER CHORD T/E OF AILERON HINGE STRUCTURE. REPLACED WITH NEW PART PER SRM 51-40-05. (X)SDR 9714299610Clip · corrodedDURING M CHECK, FOUND CORROSION ON STRINGER CLIP FITTING AT LEFT WING XRS 111.5 BETWEEN STR 12 AND 13. REPLACED FITTING PER SRM 51-30-5.
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