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 SWAA2012100108167Channel · crackedLEFT WING CHANNEL CRACKED AT WBL 191.0. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.SDR FDEA201209263466Angle · crackedLEFT WING KREUGER FLAP WELL IN WING LE IB UPPER RIB JUST OB OF KREUGER ACTUATOR CRACKED 2.5 IN. IN THE RADIUS. REMOVED AND REPLACED REINFORCING ANGLE IAW SRM 51-40-21SDR KPVA2012092607Plate · crackedINSTALLED PERMANENT PER RD 8-57-5531 AND RD 8-57-876 REPAIR FOR CRACKED LADDER PLATE AT YW 139-2 AND STR 6.SDR SAJF2012101700040Strap · corroded(B-18608) CORROSION WAS FOUND ON RT WING L/E FRONT SPAR LOWER ATTACH STRAP APPROXIMATE AT OSS 210. MFG TEAM PROVIDE ON-SITE TECH ASSISTANCE; SIMILAR CORROSIONS WERE ALSO REPORTED ON B-18605 AND B-18608 LT WING L/E LOWER ATTACH STRAP. ANALYSIS AND INVESTIGATISDR IPXA2M75684Doubler · crackedINSPECTION TYPE: 3C, PREVIOUSLY INSTALLED REPAIR DOUBLER CRACKED IN LT WING FIXED L/E ON STRINGER, NEAR XOS906. REPLACED REPAIR DOUBLER IN LT WING FIXED L/E NEAR XOS906 IAW SRM 57-40-03, REPAIR 1, FIG 201. (MAJOR)SDR AALA20120923003Vapor Barrier · crackedVAPOR BARRIER BETWEEN LEFT WHEEL WELL AND A/C BAT CRACKED. INSTALLED CROSSBRACE REPAIRS TO BAYS 5L AND 7L PER SRMSUP 57-10-10-2R 2.SDR SWAA2012110509066Support Angle · crackedRIGHT WING SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR SWAA2012092708086Angle · crackedLEFT WING CRACKED ON ANGLE LOCATED AT LEVEL RSS 527 TRAILING EDG AREA. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR A6WA20120921531Angle · crackedRIGHT WING ANTI-ICE TRANSITION DUCT MOUNTING PLATE UPPER ANGLE BETWEEN 620JL & 630JL IS CRACKED IN OUTBOARD. REMOVED AND REPLACED UPPER ANGLE IAW CRJ 200 SRM 51-42-10, 51-42-02.SDR CHQA20120915359Structure · bentDURING INSPECTION, THE RIGHT OUTBOARD LEADING EDGE WAS BENT AT THE OUTBOARD FRAME. THE RIGHT OUTBOARD LEADING EDGE WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-013240A.SDR A6WA20120921542Angle · crackedLEFT WING ANTI-ICE TRANSITION DUCT MOUNTING PLATE UPPER ANGLE BETWEEN 520JL & 530L IS CRACKED IN OUTBOARD CORNER. REMOVED AND REPLACED UPPER ANGLE IAW CRJ 200 SRM 51-42-10, 51-41-02.SDR FDEA201209143324Angle · crackedRIGHT WING LOWER L/E RIB 1 VERTICAL WEB STIFFENER ANGLE HAS 3 INCH CRACK. R & R RT WING L/E RIB 1 VERTICAL WEB STIFFENER IAW FSRM 51-72-10, PG 2-3.SDR A6WA20124M521Diaphragm · damagedTOOLING MARKS ON RIGHT O/B LEADING EDGE UPPER AND LOWER RADIUS OF THE DIAPHRAM ENTINRE LENGTH OF THE LEADING EDGE. REMOVED AND REPLACED SHROUD EDGING, INBOARD AND OUTBOARD UPPER, INBOARD LOWER.SDR R61A201209130499Bracket · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND ANGLE BRACKET AFT EDGE RIGHT WING FOR PANEL 195ER CRACKED. MAINTENANCE REMOVED AND REPLACED BRACKET IAW EMB 170 51-30-00, AND 51-43-02. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR R61A201209130493Attach Bracket · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE ANGLE BRACKET FOR ATTACHING PANEL 195FL LOCATION BOTTOM TRAILING EDGE RIGHT WING CRACKED. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKET IAW EMB 170 SRM 51-40-02. THE AIRCRAFT IS OUT OF SERVICE IN SDR ABXA20120911275Splice Plate · corrodedLEFT WING LOWER SPLICE PLATE CORRODED REQUIRES REPAIR REF: COI59797-001. REMOVED DAMAGED SECTION OF LOWER SPLICE PLATE & SPLICED IN REPLACEMENT SECTION IAW ABX REA B657-59997, ACFT WAS GROUNDED.SDR ABXA20120909263Attach Angle · corrodedTRAILING EDGE PANEL ATTACH ANGLE AT LEFT WING STATION 1050 CORRODED. FABRICATED NEW ANGLE AND INSTALLED IAW B767 SRM 51-40-02 AND DRAWING 113T1912, ACFT WAS GROUNDED.SDR A6WA20120920023Support · crackedRIGHT WING PICCOLO TUBE SUPPORT FOR INBOARD AND CENTER TUBE JOINT IS CRACKED IN THE UPPER OUTBOARD CORNER. REMOVED AND REPLACED SUPPORT WITH SERVICEABLE PART IAW CRJ 200 SRM 57-41-12 AND 51-24-16.SDR USAA2012090500063Plate · cracked2S CHECK - CRACK ON LEFT WING PYLON MOUNTING PLATE AFT OF WING REAR SPAR BETWEEN RIB 7 AND RIB 8. REPLACED LEFT WING PYLON MOUNTING PLATE IAW A319 SRM 57-21-11, FIGURE 204 AND SRM 51-75-12.SDR ABXA20120904271Support Beam · corrodedSUPPORT BEAM UNDER PNL 651YBX AT RIGHT WING STA 368.7" AFT OF REAR SPAR FWD END IS EXFOLIATED ALSO ON THE TOP AFT PORTION. REMOVED AND INSTALLED SUPPORT BEAM UNDER PANEL 651YBX IAW B767 SRM 51-40-02, 51-40-04 AND AMM 20-10-23-4, ACFT WAS GROUNDED.SDR ASAA2012092592948Angle · crackedLT WING T/E LOWER ANGLE OTBD OF PYLON IS CRACKED. R & R ANGLE IAW SRM 51-40-02.SDR ASAA2012092592947Angle · crackedRT WING T/E LOWER ANGLE OTBD OF PYLON IS CRACKED. R & R ANGLE IAW SRM 51-40-02.SDR IPXA2M75528Angle · corrodedINSPECTION TYPE:4C, UPPER SURFACE OF CENTER WING AT STRINGER 1 TO REAR SPAR BETWEEN FS 136 1-1371 RT SIDE HAS INTERGRANULAR AND EXFOLIATION COROSSION. REMOVED, FABRICATED AND INSTALLED CENTER WING UPPER SURFACE OTBD SLAT PANEL ANGLE REF STASA EA 011-5310-0SDR CA120828001Angle · cracked(CAN) WHILE PERFORMING AN INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION IAW TASKS RJ2-57-510-502 AND RJ2-57-900-320, THERE WERE CRACKS FOUND IN THE CENTER WING TANKS FWD OF THE COLLECTOR TANKS. CRACKS WERE FOUND AT INSIDE FUEL PANEL LOCATION 510AB LT SSDR R61A201208270445Screw · corrodedWHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON HARDWARE OF ADEL CLAMPS AT LEFT SPAR 3. MX REMOVED AND REPLACED HARDWARE IAW EMB 170 AMM 24-00-03. P/N NAS1149FN 832P SCREW. A/C REMAINS IN CMH FOR HEAVY CHECK COMPLETION.SDR R61A201208270444Washer · corrodedWHILE A/C WAS IN FOR HEAVY CHECK FOUND LEVEL 2 CORROSION ON HARDWARE ON NUMEROUS ADEL CLAMPS AT LEFT WING SPAR 3. MX REMOVED AND REPLACED HARDWARE AT LEFT SPAR 3 IAW EMB 170 AMM 24-00-03. P/N NAS1801-08-8 WASHER. A/C REMAINS IN CMH FOR HEAVY CHECK. COMPLETISDR FDEA201208263168Cover · crackedLT WING T/E FOUND 1EA COVER CRACKED POSITION NEAR LT MAIN LT MLG AFT TRUNNION INBD SIDE. REMOVED COVER FOR FABRICATION IAW DWG A57240775 THEN REPLACED IAW SRM 51-72-10 & 51-40-21. INSTALLED COVER AND CONDITION CHECKED GOOD. REPAIR CLASSIFIED AS MINOR PER GMSDR UALA2012082704769Structure · crackedTHE 1LT DRY BAY CUTOUT CRACK. REPAIRED CRACK PER SRM. INSPECTED REPAIRED IN FUEL TANK DRY BAY CUTOUT ON LT WING. PER EG ACCOMPLISH ECRA 5720-02322. (REF PTT 1322013). COMPLETED ITEMS 2&3 OF ECRA 5720-02322. INSP'D AREA FOR CLEARANCE TO CLOSE INT PNL 532HSDR SPUY20120820035Stiffener · corrodedDURING ROUTINE C CHECK INSPECTION, RIGHT WING FRONT SPAR AREA - STIFFENER CORRODED AT FS 232.0 REF NR 0133.SDR UALA2012082204697Structure · leakingFUEL FROM LEFT WING DRYBAY DRAIN HOLES. WIPED DOWN AFTER FUELING NO SEEPAGE NOTED, OK FOR DISPATCH. TO BE RE-CHECKED BEFORE EACH FLIGHT AFTER FUELING COMPLETE.SDR ABXA20120817265Support Beam · gougedRIGHT INBOARD FLAP OUTBOARD SUPPORT BEAM GOUGED INBOARD SIDE JUST AFT OF NR 10 JOINT. REPAIRED SUPPORT BEAM IAW REA B657-59987 MR, ACFT WAS GROUNDED.SDR AALA20120816002Vapor Barrier · crackedLEFT VAPOR BARRIER IS CRACKED BETWEEN BAYS 2 AND 4 LEFT. INSTALLED CROSSBRACE REPAIRS TO BAYS 2 AND 4 LEFT PER SRMSUP 57-10-10-2R 2.SDR A6WA201240784Fairing · chafedLEFT STUB FAIRING IS CHAFED. R & R LT STUB FAIRING, IAW SRM 51-24-36 AND 51-42-06.SDR AALA20120813001Vapor Barrier · crackedCRACK ON RIGHT VAPOR BARRIER IN THE RIGHT MAIN LANDING GEAR WHEEL WELL, RIGHT BUTTLINES 10 TO 15. INSTALLED CROSS BRACE REPAIR AT BAYS 2R AND 4R PER SRMSUP 57-10-10-2R.SDR SWAA2012100308245Structure · crackedLEFT WING UPPER CHORD INTERNAL AREA OF FUEL TANK CRACKED AT WBL 114. REPAIRED CHORD IAW EO AND EA.SDR SWAA2012100308238Web · crackedLEFT WING WEB CRACKED INTERNAL AREA OF FUEL TANK, WBL 198.6. REPAIRED WEB IAW EA AND EO.SDR SWAA2012100108150Web · crackedRIGHT WING WEB CRACKED AT WBL 198.60. REPAIRED WEB IAW EA AND EO.SDR DALA1244089260Doubler · crackedLEFT WING INTERIOR XRS 146 INTERIOR SPLICE DOUBLER HAS APPROX 2.5 INCH CRACK. REPAIRED PER SRM 51-30-02 FIG 1 51-30-05 FIG 12 51-10-05 FIG 1.SDR ASAA2012082292760Support Bracket · crackedRIGHT WING PANEL SUPPORT BRACKET BROKEN AT NR 2 ENGINE AFT STRUT. ACFT GROUNDED. R & R RT WING PANEL SUPPORT BRACKET.SDR 2012FA0000528Block · corrodedCORROSION FOUND ON FORWARD AND AFT WING SPARS UNDER FUEL TANK SPACER BLOCKS, IN FUEL TANK MOUNTING BAY. PROBLEM DISCOVERED WHEN FUEL TANKS WERE REMOVED FOR REPAIR. NO VISUAL CORROSION INDICATIONS NOTED AROUND SPACERS WHEN MOUNTED. SPACERS REMOVED ON A "HUNCH"SDR R61A201207270392Bracket · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND BRACKET FOR HYDRAULIC LINE RIGHT AFT E2 PYLON CUTOUT BROKEN. MAINTENANCE REMOVED AND REPLACED BRACKET FOR HYDRAULIC LINE RIGHT AFT E2 PYLON CUTOUT IAW EMB 175 SRM 57-50-00, AND 51-41-01. THE AIRCRAFT IS OUTSDR IPXA12M74964Angle · crackedINSPECTION TYPE:4C, RT WING T/E VERTICAL SUPPORT ANGLE BROKEN AT INBD OF RT MLG AFT TRUNNION. REMOVED, FABRICATED AND INSTALLED RT WING T/E VERTICAL SUPPORT INBD OF RT MLG AFT TRUNNION REF DWG ARC0298 AND SRM 51-33-01 PAGE 30 AND 45.SDR AALA20120726002Hinge · crackedRIGHT WING PANEL 1603A BUTE DOOR FORWARD HINGE HAS A 1/2 INCH CRACK LOCATED APPROXIMATELY 3 FEET INBOARD OF THE 4TH FLAP HINGE FAIRING. INSTALLED MIDDLE HINGE AND REPAIR STRAP PER EA.SDR AALA20120726001Hinge · crackedLEFT WING PANEL 1503A BUTE DOOR FORWARD HINGE HAS A 1/2 INCH CRACK LOCATED APPROXIMATELY 3 FEET INBOARD OF THE 4TH FLAP HINGE FAIRING AND PANEL 1502C BUTE DOOR FORWARD HINGE HAS A 3/8 INCH CRACK LOCATED APPROXIMATELY 6 INCHES OUTBOARD OF THE 2ND FLAP HINGE FAISDR ABXA20120725232Beam · corrodedAREA OF CORROSION ON LOWER T-CAP OF UPPER PANEL ATTACH BEAM INBOARD OF GEAR AT WS 255, 23 INCHES FROM LEADING EDGE. BLENDED CORROSION SIZE:7.25 LONG X 1.00 WIDE LOCATION: WS 255, OUTBOARD HORZ FLANGE OF LWR CHORD. ON LOWER TEE CAP OF ATTACH BEAM AT WS 255. FSDR ABXA20120724243Beam · corrodedWING STA 819 EXFOLIATION CORROSION FOUND ON LOWER SURFACE OF RIGHT WING T/E PANEL SUPPORT BEAM AT WS 257, 22 INCHES AFT OF AFT WING SPAR UNDERNEATH "I" BEAM SUPPORT. BLENDED CORROSION IAW REA B657-59954-MR, ACFT WAS GROUNDED.SDR AALA20120723003Stiffener · crackedSTIFFENER CRACKED AT INBOARD FASTENERS ON LEFT VAPOR BARRIER. INSTALLED NEW STIFFENER PER AARD 51-00-05-1 AND BOEING DOCUMENT 111A1000.SDR AALA20120723002Vapor Barrier · crackedVAPOR BARRIER CRACKED 1ST BAY OUTBOARD OF KEEL BEAM. INSTALLED CROSSBRACE REPAIRS TO BAYS 1L,2L AND 4L PER SRMSUP 57-10-10-2R 2.SDR AALA20120713006Fitting · wornLEFT WING INBOARD SIDE FAILSAFE WING FITTING HAS WEAR. INSTALLED DOUBLER PER EA B767-57-016371.SDR USAA2012071600011Strut · corroded2S CHECK - CORROSION ON RIGHT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862, RIB 1 OUTBOARD FLAP. REPLACED RIGHT WING INTERCONNECTING STRUT BETWEEN WS 4067 TO WS 4862, RIB 1 OUTBOARD FLAP IAW A320 AMM 27-51-44.
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