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 SWAA2014100932829Bracket · crackedLEFT WING AFT SPAR BEHIND NR 1 ENG T BRACKET CRACKED. REPAIRED BRACKET IAW SRM.SDR SWAA2014101532967Angle · crackedRIGHT WING TE L ANGLE ON FWD SIDE OF SHELF SUPPORT CRACKED. R & R L ANGLE IAW SRM.SDR SWAA2014110433659Panel · delaminatedRIGHT WING TE PANEL 8501 DELAMINATED AT CORNER. R & R PANEL IAW SRM.SDR SWAA2014101733120Splice · crackedSPLICE ASSEMBLY CRACKED AT REAR SPAR ON LOWER SURFACE OF WING BETWEEN RSS 180 TO 210 RT SIDE. R & R SPLICE ASSEMBLY IAW SRM & DWG.SDR FDEA201410042968Panel · delaminatedLEFT LOWER REAR CAP WING ROOT PANEL ASSEMBLY SHOWS DELAMINATION & EVIDENCE OF CORROSION. REPAIRED PANEL ARC0446-503 PER SRM 81-71-00 VOL.IISDR SWAA2014102933479Plate · crackedRIGHT WING TE WAFFLE PLATE JUST INBD OF NR 2 PYLON AFT TIP CRACKED. R & R WAFFLE PLATE IAW SRM.SDR SWAA2014102933478Gusset · crackedRIGHT WING UPPER TE PANEL LOWER SUPPORT GUSSET CRACKED AT TRANSVERSE WEB LOWER ATTACH POINT ABOVE NR 2 PYLON AFT TIP. R & R GUSSET IAW SRM.SDR SWAA2014101532970Plate · crackedLEFT WING TE WAFFLE PLATE JUST ABOVE NR 3 FLAP TRACK FAIRING CRACKED. R & R WIGGLE PLATE IAW SRM.SDR SWAA2014101532969Plate · crackedLEFT WING TE WAFFLE PLATE AFT OF AFT STRUT FAIRING CRACKED AT OTBD FASTENER HOLE. R & R WIGGLE PLATE IAW SRM.SDR SWAA2014101032863Attach Angle · crackedLEFT WING TE DEFLECTOR RIB FIXED ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW SRM.SDR SWAA2014100832763Web · crackedLEFT WING FIXED TE PANEL INBD OF DEFLECTOR RIB WEB CRACKED. R & R WEB IAW SRM & DWG.SDR IXXA20150115007Channel · corrodedLOWER PANEL DIAGONAL ATTACH CHANNEL INBD OF H BLOCK AT WS 289 SPLIT ON EDGE. R & R IAW SRM 51-40-02.SDR SWAA2014100232551Angle · crackedLEFT WING UPPER WING SUPPORT UNDER PANEL 5735 26 INCHES AFT RS & 8 UP FROM NR 3 FLAP TRACK ANGLE CRACKED. R & R ANGLE IAW SRM.SDR FY4Y20141003004Plate · corrodedDURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 520 TO WS 526. DIMENSIONS OF CORROSION AREA 6 INCHES X 1.5 INCHES. AFTER THE CORROSION BLEND OUT THE MIN REMAINING THICKNESS OF 0.141 INCH, ORIGINAL THICKNESS ISSDR FY4Y20141003003Plate · corrodedDURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 701 TO WS 696. DIMENSIONS OF CORROSION AREA 5 INCHES X 1.5 INCHES. AFTER THE CORROSION BLEND OUT THE MIN REMAINING THICKNESS OF 0.126 INCH, ORIGINAL THICKNESS ISSDR FY4Y20141003002Plate · corrodedDURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 726 TO WS 734. DIMENSIONS OF CORROSION AREA 8 INCHES X 2 INCHES. AFTER THE CORROSION BLEND OUT, THE MIN REMAINING THICKNESS OF 0.031 INCH, ORIGINAL THICKNESS IS SDR FY4Y20141003001Plate · corrodedDURING PERFORMED C CHECK CORROSION WAS FOUND ON THE LT WING FRONT SPAR LOWER CHORD PLATE FROM WS 738.5 TO WS 742. DIMENSIONS OF CORROSION AREA IS 3.5 INCHES X 1.5 INCHES. AFTER THE CORROSION BLEND OUT THE MIN REMAINING THICKNESS OF 0.104 INCH, ORIGINAL THICKSDR FDEA201409302868Lug · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN THE BORE & FACES. COMPLIED WITH EA 6-5710-T0311839 P1 WINGS BASIC WING STRUCTURE LT RIB 5 FWD LUG CORROSION.SDR SWAA2014110633873Support Angle · crackedRIGHT WING TE, UPPER MOST INBD NO STEP PANEL INBD SUPPORT ANGLE CRACKED AT AFT END. R & R ANGLE IAW SRM.SDR SWAA2014103033551Web · crackedLEFT WING TRANSVERSE WEB CRACKED JUST INBD OF MAIN FLAP PROGRAM ROLLER ATTACH ANGLE. R & R WEB IAW SRM.SDR SWAA2014103033550Angle · crackedRIGHT WING FIXED TE UPPER PANEL, SEAL RETAINER ANGLE CRACKED JUST AFT OF PYLON. R & R ANGLE IAW SRM.SDR SWAA2014102833394Plate · crackedLEFT WING WAFFLE PLATE CRACKED INBD OF NR 1 PYLON STATION RSS 260. R & R PLATE IAW SRM.SDR SWAA2014102833393Plate · crackedRIGHT WING WAFFLE PLATE CRACKED INBD OF NR 1 PYLON STATION RSS 260. R & R PLATE IAW SRM.SDR SWAA2014102933473Plate · crackedLEFT WING TE CAVITY WIGGLE PLATE CRACKED LOWER AFT SPAR INBD SIDE OF NR 1 ENG STRUT. R & R WIGGLE PLATE IAW SRM.SDR SWAA2014102933472Intercostal · crackedLEFT WING TE CAVITY SUPPORT INTERCOSTAL CRACKED OTBD END COMMON TO UPPER TE PANEL ABOVE NR 1 ENG STRUT. R & R INTERCOSTAL IAW SRM.SDR ABXA20140925319Support · corrodedRIGHT WING UPPER PANEL SUPPORT TEE INBD END OF 651MT EXFOLIATED NEAR AFT END OF TEE. R & R UPPER CLAMP LAW SRM 51-40-2. CORRODED L2, PN 113T1623-158, PART NAME CHORD, SN NSN, EXACT STRINGER & WS LOCATION ON NC 273WS TO 275WS. ACFT WAS GNDED.SDR ABXA20140925311Channel · damagedWING TE PANEL ATTACH CHANNEL LOWER CHORD SPLIT ON EDGE AT WS 424.22 INCHES FROM REAR SPAR. INSTALLED NEW CHORD IAW REA B657-61210-MR & SRM 51-40-02. PANEL 552JB INSTALLED IAW SRM 51-40-02. SDR INFO PN 113T1407-1, PART NAME SPOILER BEAM CHORD, L2 CORROSION, SDR SWAA2014092932357Angle · crackedRIGHT WING TE INBD UPPER PANEL ANGLE BRACKET CRACKED. REPAIRED ANGLE IAW DWG & SRM.SDR IXXA20150115010Structure · corrodedPANEL 661AB REAR SPAR TO TE ATTACH RIB LOWER CHORD SPLIT ON EDGE WS 435. LOWER CHORD R & R IAW SRM 51-40-02.SDR SWAA2014102233229Support Angle · crackedLEFT WING SUPPORT ANGLE CRACKED ON STABILIZING LINKS BETWEEN MLG BEAM & REAR SPAR. R & R ANGLE IAW SRM & DWG.SDR SWAA2014101432930Angle · crackedLEFT WING ANGLE CRACKED ON TRACK FAIRING NR 3 INBD SIDE UPPER STRUCTURE. R & R ANGLE IAW SRM & DWG.SDR FDEA201409242751Fitting · crackedCENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE WITH CRACK SIGNAL. REPAIRED CENTER WING INSP REAR SPAR INTERNAL ANGLE & TEE FITTING LT NR 10 FASTENER HOLE PER EA 6-5710-T0312253. MAJOR REPAIR IAW GMM 6-2-100SDR SIMA20140924004Structure · leakingFUEL SMELL IN COCKPIT TAXIING IN, REPEAT WRITE UP. APU OFF NO REPORT OF SMELL IN CABIN. PERFORMED GVI OF WINGS & OF ALL PREVIOUS REPAIRS, NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY WHILE PERFORMING TAXI CHECK. REFERENCE WORK ORDER 1142R1695, FOUND FSDR SWAA2014092632328Bracket · crackedRIGHT WING BRACKET CRACKED AT INBD OF INBD FLAP OTBD TRACK FAIRING. R & R BRACKET IAW SRM.SDR ABXA20140926316Beam · crackedLEFT WING NR 8 123 BEAM HAS 1 CRACK INDICATION. YOU CAN SEE THE DEFECT AT THE BOTTOM OF THE HOLE LOOKING FROM INBD OUT. REAMED HOLE CLEAN & ROUND IN 1/64TH INCREMENTS & COMPLIED WITH HFEC HOLE SCAN. REPAIRED NR 8 1-2-3 BEAM IAW REA CO57-61254-MR. ALSO REFESDR ABXA20140919306Angle · corrodedRIGHT WING UPPER TE PANEL SUPPORT CORRODED ON UPPER AFT SURFACE AT WS 853. FOUND TO BE OUT OF LIMITS, MANUFACTURED NEW TEE ANGLE IAW REA B757-61206. INSTALLED TEE IAW SRM 51-40-02. CORRODED, PN 123T1673-33, PART NAME CHORD, SN NSN, LOCATION 852.20 TO 854.00SDR FDEA201409192685Fitting · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. COMPLIED WITH EA 6-5710-T0311611 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.SDR FDEA201409192683Fitting · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE & FACES. COMPLIED WITH EA 6-5710-T0311611 P1 WING BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.SDR ABXA20140915310Structure · corrodedREAR SPAR TO WING TE RIB AT WS 433 UPPER CHORD CORRODED AROUND NUTPLATES ON INBD SIDE. R & R CHORD IAW SRM 51-40-02. L2 CORROSION, PN 113T1510-33, PART NAME UPPER CHORD, SN NSN, LOCATION FROM 433 TO 433. ACFT WAS GNDED.SDR SWAA2014091832076Plate · crackedRIGHT WING LOWER SHELF WIGGLE PLATE CRACKED AT RSS 261. R & R PLATE IAW SRM.SDR IXXA20150101130Structure · corrodedAIRCRAFT GNDED FOR HVY MX. REAR SPAR TO WING TE UPPER PANEL ATTACH BEAM UPPER CAP CORRODED AROUND NUTPLATES AT STATION 288. FABRICATED & INSTALLED UPPER CHORD IAW DWG 113T1623 & SRM 51-40-02.SDR SWAA2014101733119Web · crackedRIGHT WING FUEL TANK WEB CRACKED AT WBL 198.6 RIB, NEXT TO UPPER STRINGER 5. REPAIRED WEB IAW EO & EA.SDR SWAA2014100632650Angle · crackedRIGHT WING ANGLE CRACKED ON MLG STABILIZER BEAM, REAR SPAR. R & R ANGLE IAW SRM.SDR AALA20140914004Pad · damagedLATCH PAD DAMAGED ON WING BEAM OTBD OF HIGH PRESS DOOR. ACCOMPLISHED REPAIR IAW EA B737-57-036563.SDR SWAA2014093032491Support Bracket · crackedLEFT WING NR 2 SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.SDR SWAA2014093032490Support Bracket · crackedLEFT WING NR 1 SUPPORT BRACKET CRACKED. R & R BRACKET IAW SRM & DWG.SDR SWAA2014092932387Support Bracket · crackedRIGHT WING NR 8 SUPPORT BRACKET CRACKED LOCATED ON PLATE TRANSITION. R & R BRACKET IAW SRM & DWG.SDR SWAA2014092932386Support Bracket · crackedRIGHT WING NR 7 SUPPORT BRACKET LOCATED ON PLATE TRANSITION CRACKED. R & R BRACKET IAW SRM & DWG.SDR SWAA2014091531978Bracket · crackedRIGHT WING AILERON COVE BRACKET CRACKED AT LOWER RADIUS. R & R BRACKET IAW SRM.SDR ABXA20140911309Channel · corrodedWING TE PANEL ATTACH CHANNEL LOWER CHORD SPLIT ON EDGE AT WS 1050. R & R DAMAGED CHORD IAW SRM 51-40-02. CORRODED L2 PN 113T1912-29, PART NAME BEAM, STRINGER & WS LOCATION WS 1040 TO 1060. ACFT WAS GNDED.
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