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 AALA20120710016Vapor Barrier · crackedRIGHT VAPOR BARRIER CRACKED APPROXIMATELY 2.25 INCHES AT INBOARD EDGE OF PACK EXHAUST DUCT. INSTALLED CROSS BRACE REPAIR STRAPS AND ANGLES AT BAYS 2R AND 4R PER / SRMSUP 57-10-10-2R.SDR AALA20120728003Vapor Barrier · crackedVAPOR BARRIER IS CRACKED ON THE LEFT SIDE AT BAY 6 LEFT. INSTALLED DOUBLERS IN VAPOR BARRIER BAY 7 LEFT PER SRMSUP 57-10-10-2R 2.SDR SWAA2012071905972Support Angle · crackedLEFT WING SUPPORT ANGLE CRACKED AT WBL 183.40 OUTBOARD SIDE INTERNAL TRAILING EDGE AREA. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR SPUY20120627021Support · corrodedLEFT WING REAR SPAR AREA. REAR SPAR SUPPORT TO FLAP TRACK NR 4 SHOWS CORROSION AT WS 224.50. (FWD PART)SDR SWAA2012072006026Angle · crackedRIGHT WING TRAILING EDGE ANGLE CRACKED AT RSS 533+12. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR AALA20120622015Vapor Barrier · crackedVAPOR BARRIER CRACKED AT RIGHT WHEEL WELL. REPAIRED PER SRMSUP 57-10-10-2R 2.SDR QXEA2012062100511Support Fitting · chafedRT SHROUD SUPPORT FITTING AT YW 60.9 IS CHAFED. BLENDED CHAFED AREA IAW SRM 51-14-00-02-01. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801. DAMAGE IS WITHIN LIMITS IAW RD 8/4-57-1841. ALODINED AND PRIMED IAW RD 8/4-57-1841. COMPLIED WITH TASKSDR QXEA2012062100510Support Fitting · chafedRT SHROUD SUPPORT FITTING AT YW 79.9 IS CHAFED. BLENDED AREA IAW SRM 51-14-00-02-01. CONFIRMED BLEND CRACK FREE REF NTM 51-00-06-910-801 PT 1. BLENDED AREA IN LIMITS IAW RD 8/4-57-1841. ALODINED AND PRIMED IAW RD 8/4-57-1841. COMPLIED WITH TASK CARD RD 8/4SDR QXEA2012062100509Support Fitting · chafedRT SHROUD SUPPORT FITTING AT 98.6 IS CHAFED. BLENDED CHAFED AREA IAW SRM 51-14-00-02-01. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801. BLENDS FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-1841. ALODINED AND PRIMED IAW RD 8/4-57-1841. COMPLIED WITSDR QXEA2012062100508Support Fitting · chafedRT SHROUD SUPPORT FITTING AT YW 117.5 IS CHAFED. BLENDED CHAFE AREA IAW SRM 51-14-00-02-01. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801. BLEND WITHIN LIMITS RD 8/4-57-1841. ALODINED AND PRIMED IAW RD 8/4-57-1841. COMPLIED WITH TASK CARD RDSDR REXA2012061900949Support · corrodedJACK FITTING AT FS 278, LEFT SUPPORT CORRODED. REMOVED AND REPLACED LT JACK FITTING SUPPORT AT FS 278 IAW SRM 51-42-06 AND 51-42-21.SDR REXA2012061900948Support · corrodedJACK FITTING AT FS 278, RIGHT SUPPORT CORRODED. REMOVED AND REPLACED JACK FITTING SUPPORT, RT SIDE, AT FS 278 IAW SRM 51-42-06 AND 51-42-21.SDR IPXA12574043Skin · dentedNR 9 SLAT DENTED. REPAIR IAW SRM 51-70-10-2R.SDR SIMA20120618004Angle · crackedDURING HEAVY MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING TO FUSELAGE ATTACH ANGLE CRACKED ON THE AFT END OF NR 1 SECTION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RIGHT OVERWING ANGLE IAW ETN-EM-53-142. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR U2RA20120626Attach Angle · crackedRIGHT WING FUEL PANEL LATCH ANGLE FOUND CRACKED. CRACK LENGTH .5"SDR QXEA2012061500453Panel · corrodedCENTER WING UPPER DRY BAY PANEL 621BT HAS AREAS OF CORROSION ON MATING SURFACE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-425. CONFIRMED BLENDED AREA CRACK FREE REF NTM 51-00-06-910-801. ALODINED AND PRIMED IAW SRM 51-25-40-02-01. COMPLISDR U2RA201206200003Bracket · crackedRT WING T/E CAVITY AT WING BS 280 BRACKET FOUND CRACKED, CRACK LENGTH .5".SDR U2RA201206200001Retainer · crackedLEFT WING STRUT DOOR LOWER SECTION FIXED FAIRING RETAINER FOUND CRACKED. CRACK LENGTH 1".SDR FDEA201206132227Support · crackedLT WING LOWER L/E INBD OF ACCESS PANEL NR 526DB FWD SUPPORT AT STA XORS 799, FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-03, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR AALA20120608004Vapor Barrier · crackedLEFT VAPOR BARRIER IS CRACKED BETWEEN BAYS 2 AND 4. INSTALLED CROSSBRACE REPAIRS TO BAYS 2L AND 4L PER SRM - WINGLET APB SUPPLEMENT 57-10-10-2R 2.SDR AALA20120607003Stiffener · crackedLEFT VERTICAL STIFFENER OUTBOARD OF PACK EXHAUST DUCT CUTOUT IS CRACKED AT LOWER END. REMOVED CRACKED STIFFENER AND INSTALLED NEW VERTICAL STIFFENER PER AARD 51-10-05-R1 AND BOEING DRAWING NUMBERS 111A1000 AND 111A-1308.SDR AALA20120606019Vapor Barrier · crackedRIGHT VAPOR BARRIER IS CRACKED BETWEEN BAYS 2 AND 4. INSTALLED REPAIR STRAPS AND ANGLES ON RIGHT VAPOR BARRIER AT BAYS 1, 2 AND 4 PER SRM SUP 57-10-10-2R, REPAIR 2.SDR AALA20120604007Fitting · crackedLEFT WING AFT OUTBOARD PITCHLOAD FITTING HOLE CRACKED. FREEZE PLUG INSTALLED PER ECO C3194.SDR ABXA20120602358Doubler · corrodedLIGHT CORROSION INSIDE RT WING OUTBOARD FLAP BOX AT TRAILING EDGE OUTBOARD END RIB. REMOVED AND REPLACED DOUBLER INSIDE RT WING OUTBOARD FLAP BOX AT TRAILING EDGE OUTBOARD END RIB IAW B767 SRM 51-40-02 RT OUTBOARD FLAP, ACFT WAS GROUNDED.SDR USAA2012062600029Plate · worn2S CHECK - WEAR ON RE-INFORCING PLATE LOCATED ON LOWER AFT SURFACE IN AREA COVERED OF PYLON FAIRING LEFT WING BETWEEN RIB 7 TO RIB 8 TRAILING EDGE. REPLACED PLATE MOUNTING ON LOWER LEFT WING BETWEEN RIB 7 TO RIB 8 TRAILING EDGE IAW A319 SRM 51-72-11 & AIRBUS SDR SWAA2012061805024Structure · crackedRIGHT WING UPPER CHORD CRACKED ON UPPER CHORD LOCATED AT WBL 114.00. REPAIRED CHORD IAW EA.SDR SWAA2012061805023Structure · crackedLEFT WING UPPER CHORD CRACKED ON UPPER CHORD LOCATED AT WBL 114.00. REPAIRED CHORD IAW EA.SDR SWAA2012061905081Web · crackedRIGHT WING WEB CRACKED AT WBL 198.6 BETWEEN REAR SPAR AND STR 5. REPAIRED WEB IAW EA AND EO.SDR AALA20120609001Vapor Barrier · crackedTEMP VAPOR BARRIER CRACKED BETWEEN BAYS 2 AND 4. INSTALLED REPAIR TO BAYS 2L AND 4L PER SRM SUP 57-10-10-2R 2.SDR DALA1240710918Rub Strip · corrodedON REMOVAL OF RT WING UPPER FUEL ACCESS PANEL 1436C RUB STRIP FOUND CORRODED. COMPLIED ER/A 504287-14 REV ORIG.SDR SAJF201206141018Strap · corroded(B18605) LEFT WING L/E FRONT SPAR LOWER ATTACH STRAP HAS A 3.5 X 1.3 INCH AREA CORROSION. CORRODED AREA R & R IAW EO 738-57-00-0152.SDR USAA2012052300023Angle · damagedC1 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-323 A/C'S AT RIB 1 / FR 42, OUTER ANGLES REMOVED & RE-INSTALLED / REPLACED AS REQUIRED. REPLACED OUTER ANGLE ON RIGHT SIDE AT FR42, RIB 1 IAW EA 103839A.SDR USAA2012052300022Angle · damagedC1 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-323 A/C'S AT RIB 1 / FR 42, OUTER ANGLES REMOVED & RE-INSTALLED / REPLACED AS REQUIRED. REPLACED OUTER ANGLE ON LEFT SIDE AT FR42, RIB 1 IAW EA 103839A.SDR ABXA20120520350Closeout Panel · corrodedLEFT WING, LEADING EDGE CLOSE OUT PANEL BETWEEN SLAT AND AUX TRACKS CORRODED WS 775. REMOVED AND REPLACED CLOSE OUT PANEL, INSTALLED HI-LOKS & RIVETS IAW 767 SRM 51-40-02. ACFT WAS GROUNDED.SDR SWAA2012053004464Angle · crackedRIGHT WING FIXED TRAILING EDGE ANGLE CRACKED BETWEEN WBL 203.00 AND WBL 212. REMOVED AND REPLACED ANGLE IAW SRM & DWG.SDR FDEA201205181859Tee Fitting · corrodedLT WING T/E LOWER TEE FITTING FOUND CORRODED AT PANEL 641JB FORWARD CUT-OUT AREA. R & R IAW SRM 51-31-01 AND 51-33-01 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201205171956Angle · corrodedLT MLG WHEEL WELL FWD WALL HAS THE STRUCTURE SPLIT AND LIFTING AT THE OTBD LOWER CORNER OF THE SLANT PANEL. REPAIRED IAW SRM 53-40-00, FIG 11.SDR IPXA12M73823Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS 730-736. REPAIRED RT WING FIXED L/E COMPT BETWEEN XFS730-736 REF EO MD11- 5730-42916-D.SDR SWAA2012052104210Support Angle · crackedLEFT WING SUPPORT ANGLE CRACKED BETWEEN WBL 71.24 TO WBL 78. REMOVED AND REPLACED ANGLE IAW SRM & DWG.SDR FDEA201205101780Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT CUT-OUT INBD EDGE FOUND CRACKED. REPAIRED IAW EA 8-5740-160608 PART 1, REPAIR CLASSIFIED MAJOR IAW GMM-2-100, REV 114.SDR FDEA201205081763Shim · migratedLT WING BETWEEN OTBD NACELLE FITTING AND LOWER WING SKIN, FOUND SHIMS MIGRATING AT LWS 303.5. SHIMS TRIMMED IAW EA F-5740-158167, PART 1. REPAIR IS CLASSIFIED AS MAJOR.SDR A6WA201240497Bracket · brokenLT OTBD L/E INBD MOUNTING BRACKET BROKE. REMOVED UNSERVICEABLE LT OTBD L/E INBD MOUNTING BRACKET AND INSTALLED SERVICEABLE INBD MOUNTING BRACKET IAW SRM 51-40-11, 51-41-00, 51-42-10.SDR AALA20120503002Vapor Barrier · crackedLEFT VAPOR BARRIER IS CRACKED 3 INCHES BETWEEN BAYS 2 AND 4 LEFT AT AFT END OF A/C BAY. INSTALLED REPAIR ANGLES AND STRAPS FOR BAYS 2 AND 4 LEFT PER SRMS 57-10-10-2R REPAIR 2.SDR SWAA2012120310147Panel · crackedCRACK ON BOTH SIDES OF FASTENER HOLE ON PYLON/WING PANEL AFT OF 58710R. REPLACED PANEL 5871 OR ON PYLON/WING RIGHT IAW SRM B737-500 51-40-05 AND DWG 65C27356.SDR ABXR2012043000047Bracket · crackedDURING C INSPECTION, FOUND LT WING FUEL FILL LINE BRACKET CRACKED ABOVE STRINGER 5 WS 665. R & R BRACKET IAW SRM.SDR ABXR2012043000046Fitting · gougedDURING C-CHECK, FOUND RT WING BACKUP FITTING BETWEEN RIBS 8 7 9 GOUGED WS 394. REPAIRED IAW REA B651-59769-MR.SDR ABXR2012043000045Fitting · gougedDURING C-CHECK FOUND RT WING RIB 8 BACKUP FITTING HAS TOOLING MARKS AT WS 375. REPAIRED IAW WITH REA B657-59769-MR.SDR ABXR2012043000044Shim · migratedDURING C CHECK FOUND LT WING BACKUP FITTING AT RIB 8 HAS SHIM MIGRATING BETWEEN STRINGERS 18 & 19. REPAIRED IAW REA B657-59770-MR.SDR V0XR2012042700011Plate · corrodedLADDER PLATE FOR PANEL 624BT HAS PITTING. REPAIRED LADDER PLATE BETWEEN STATIONS YW=261-333 RT WING IAW REPAIR DWG 8-57-633.SDR V0XR2012042700009Plate · corrodedLADDER PLATE FOR PANEL 624AT HAS PITTING. REPAIRED LADDER PLATE BETWEEN STATIONS YW=171.2-261.0 IAW REPAIR DWG 8-57-611.
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