JASC 5730
Service difficulty reports · 27,262
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 FDEA201804060875Doubler · crackedRIGHT WING BEADED DOUBLER FOUND CRACKED AT XOS 766. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR YENA201804060164Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND AT PREVIOUS BLEND AREA RT TOP WING SKIN NR 2 TE OVERHANG LWR SURF RIB 13 PLUS 13"; COMPLIED WITH JB EC A18-182-01.SDR YENA201804060163Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND AT PREVIOUS BLEND AREA RT TOP WING SKIN NR 2 TE OVERHANG LWR SURFACE I/B NR 2 SPOILER ACT HINGE FTG; COMPLIED WITH JB EC A18-182-01.SDR YENA201804060162Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND AT PREVIOUS BLEND AREA RT TOP SKIN NR 2 TE OVERHANG LWR SURFACE RIB 14 I/B NR 3 SPOILER ACTUATOR FTG; COMPLIED WITH JB EC A18-182-01.SDR FDEA201804060880Skin · crackedLEFT WING FIXED LEADING EDGE LOWER PANEL CUTOUT CRACKED AT XOS 600 INBD OF FUEL PANEL HINGE DOOR. DOUBLER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW DOUBLER IAW DRAWING ARB2933, REVISION AJ. INSTALLED THE NEW DOUBLER IAW SRM 51-31-01-0G. THE REPAIR WASDR DALA2018040702315Access Panel · corrodedCORROSION OUT OF LIMITS IAW NRC 00520. CORROSION ON FUEL ACCESS PANEL 520EB, LT WING. THE FUEL ACCESS PANEL WAS REPLACED IAW AMM 28-00-00 AND JIC CARD 2040-0010 JOB 001-0295.SDR SWAA2022021486452Panel · delaminatedR/H LOWER WING PANEL 621VB HAS DISBOND FWD I/B CORNER AND DRAIN HOLE / R/H LOWER WING PANEL 621VB DISBOND FWD I/B CORNER REPAIRED IAW SRM 57-41-01-2R-1 TABLE 202 AND IA SRM 51-70-05-2R-10SDR SWAA2022021314059Plate · brokenR/W T/E WIGGLE PLATE FWD OF PANEL 651GB IS BROKEN / REMOVED AND INSTALLED NEW WIGGLE PLATE FWD OF PANEL 651GB IAW SRM 51-40-02-0G-0 PARA 4. REFERENCE IPC 57-50-00-30 FOR FASTENER CALLOUT.SDR SWAA2022021492517Retainer · crackedLEFT WING TRAILING EDGE BULB SEAL RETAINER FWD OF TRANSVERSE WEB JUST ABOVE #1 PYLON TIP IS CRACKED / REMOVED AND REPLACED TRANSVERSE WEB LEFT WING TRAILING EDGE BULB SEAL RETAINER THAT WAS CRACKED IAW 51-40-012-0G SRM AND FASTENERS IAW AIPC 57-50-00-25 89813USDR SWAA2022021411533Retainer · crackedRT. WING; CRACK IN BULB SEAL RETAINER APPROX. 272 ON FIXED T/E SUPPORT. / REMOVED AND REPLACED BULB SEAL RETAINER BRACKET ON RH WING TE STRUCTURE AT APPROX 272 IAW SRM 51-40-02-00G-0 PAR 4 AND FIG 8SDR SWAA2022021313246Angle · crackedRIGHT WING; TRAILING EDGE PANEL 651FB HAS CRACKED 'L' ANGLE. LOCATED ON THE FWD. SIDE OF PANEL. MARKED / REMOVED AND REPLACED PANEL 651FB L ANGLE ON FWD SIDE OF PANEL REF SRM 51-40-02.SDR DALA2018040202114Access Panel · crackedCRACKED FUEL TANK ACCESS PANEL 520CB ON THE LT WING. THE ACCESS PANEL WAS REPLACED.SDR YENA201803300909Skin · crackedDURING BRIDGE CHECK AT (YRQ) DATED 03/2018, A CRACK WAS FOUND ON THE LT WING LOWER SKIN AT RIB 10 & SPAR II. SEE REF /1/ ETD FOR MORE DETAILS. YRQ REMOVED THE DAMAGE BY CUT-OUT, WHICH IS 1.130” L X 0.795” W. THE DAMAGE IS FOUND TO BE OUT OF REF /2/ SRM APPLICASDR SWAA2018052222170Fairing · crackedRT WING FORWARD OF OUTBOARD AFT DRAIN HOLE FAIRING 642BB INNER SKIN CRACKED. REPAIRED FAIRING IAW ER AND EA.SDR DALA2018032902017Skin · buckledDURING INSPECTION, FOUND A SECTION OF THE WING SKIN, INBOARD OF THE LEFT ENGINE BUCKLED, SEVERAL RIVET HEADS HAVE PULLED THROUGH SKIN. MAINTENANCE REPAIRED THE SKIN IAW STEP 4E, IAW SRM 57-41-01, REPAIR 7.SDR FDEA201803270974Skin · crackedRT WING SKIN AT THE INBOARD UPPER CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT HAS A .500 INCH CRACK PROPAGATING THROUGH AN EXISTING STOP DRILL. INSTALLED A REPAIR DOUBLER PER SRM 57-10-00 FIG 103.SDR UIEA2018040400563Skin · corrodedFOUND THE LT UPPER WING BETWEEN FILL PORT ADAPTER AND WING UPPER SKIN CORRODED. REPAIRED IAW EI T2017A57M-2414, REV 2. CHECKED NORMAL.SDR UIEA2018040500614Skin · corrodedFOUND THE RT WING UPPER BETWEEN THE WING UPPER SKIN AND THE FILL PORT ADAPTER CORRODED. ACCOMPLISHED DAMAGE AREA IAW EI NO: T2017A57M-2414 REV.2 2. ORIGINAL EI ATTACHMENT NRC 266 3. CONDITION CHECKED NORMAL.SDR FQAR20180326026Skin · crackedDURING A SCHEDULED INSPECTION, FOUND THE INBOARD LOWER WING SKIN CRACKED, CRACK WAS LOCATED 4INCHES OUTBOARD OF THE BUTT RIB AND RUNNING PARALELL TO THE SPAR, 2INCHES FORWARD OF THE SPARSDR EE4Y2018041906384Skin · crackedDURING THE ACCOMPLISHMENT OF SRM 57-20-10, REPAIR 4, FOUND THE LT WING UPPER SKIN, TWO FASTENER HOLES CRACKED. ONE FASTENER HOLE LOCATED AT FASTENER ROW 1, SPECIFICALLY AT WBL 181.4, IT WAS REPAIRED IAW SRM B737-57-20-10, REPAIR 7. THE OTHER FASTENER HOLE LOSDR IPXA2018041528577Skin · corrodedINSPECTION TYPE: 3C, RT WING UPPER SKIN HAS CORROSION BETWEEN XORS 97 & 130, STRINGERS 11 - 15. REPAIRED THE SKIN IAW EA 011-5730-01-A7199, REV I/R, AND EO MD11-5730-68143-A.SDR SWAA2018040420978Plate · crackedRIGHT WING WIGGLE PLATE OUTBOARD OF PANEL 651DB CRACKED AT IRSS. 215. R & R THE WIGGLE PLATE IAW SRM.SDR IPXA2018041028434Skin · corrodedINSPECTION TYPE: 3C, LT WING, UPPER SKIN HAS CORROSION AROUND SEVERAL FASTENERS HEADS MIDSPAR AT FUSELAGE. REPAIRED THE WING SKIN BETWEEN XORS 97 AND 130.40, BETWEEN STRINGERS 14 AND 16 IAW EA 011-5730-01-A7197, REV IR, AND EO MD11-5730-68095-A.SDR IPXA2018040628264Skin · crackedINSPECTION TYPE: 3C, LEFT WING L/E LOWER SKIN IS CRACKED AT THE SLAT TRACK CUT-OUT AT XOS 889. REPAIRED THE SKIN IAW SRM 57-40-02, REPAIR 7, FIG 201. MAJOR.SDR FQAR20130321025Skin · crackedDURING A SCHEDULED INSPECTION ON THE LEFT WING, FOUND A ONE INCH LONG CRACK IN THE WING SKIN, 14 INCHES AFT OF THE SPAR, 1 INCH OUTBOARD OF THE BUTT RIB.SDR IPXA2018041228495Skin · chafedINSPECTION TYPE: 3C, LEFT WING L/E SKIN CHAFED ON EITHER SIDE OF THE NR 1 SLAT, NR 1 TRACK CUT OUT. REPAIRED THE WING SKIN IAW SRM 57-40-02, REPAIR 5, FIGURE 201. MAJOR.SDR IPXA2018040928397Doubler · crackedINSPECTION TYPE: 3C, RT WING, FIXED L/E BEADED DOUBLER IS CRACKED AT XOS. 633.4 - 636.8. REPAIRED THE DOUBLER IAW EA 011-5730-01-A7191, REV I/R, AND EO MD11-5730-68054-A. MAJOR.SDR YENA201803190905Skin · crackedDURING B6 CHECK AT (YRQ) DATED 02/18, A CRACK WAS FOUND ON THE LT WING LOWER SKIN AT RIB 10 & SPAR II. SEE REF /1/ ETD FOR MORE DETAILS. YRQ REMOVED THE DAMAGE BY CUT-OUT, WHICH IS 0.800” L X 0.720” W. THE DAMAGE IS FOUND TO BE WITHIN THE REF /2/ SRM REPAIR 54SDR ABXA20180318024Panel · corrodedCORROSION ON THE LEFT WING LOWER TRAILING EDGE PANEL LOWER SURFACE BETWEEN WING STATIONS 903 AND 909. THE PANEL WAS REPAIRED. AIRPLANE WAS GROUNDED.SDR ABXA201803280019Skin · corrodedCORROSION ON THE RIGHT WING UPPER SKIN LOWER SURFACE AT WING STATION 470. THE SKIN WAS REPAIRED. THE ACFT WAS GROUNDED.SDR GTIA2018031602517Skin · corrodedCORROSION FOUND ON THE TOP SKIN PANEL, WS 5512 RIB 10. REPAIR CLASSIFIED AS MAJOR.SDR JGVR20180316001Skin · corrodedREPAIRED TWO CORRODED AREAS ON THE UPPER LT WING SKIN AT WS 37 NEAR THE DRAG ANGLE.SDR SWAA2022021161595Skin · crackedR/H INBD LEADING EDGE SKIN FASTENER HOLE HAS A CRACK INDICATION IN THE FASTENER HOLE/COUNTERSINK COMMON TO THE FRONT SPAR AT KRAS 206.2 +12IN APPROX. PER BOEING NDT MANUAL PART6;51-00-00 PROC.16 AND 53-30-00 PROC.3 / INSTALLED REPAIR IAW SRM 57-41-01-2R3 REPAISDR SWAA2018032220607Skin · crackedRT WING INBOARD LEADING EDGE SKIN FASTENER HOLE CRACKED, FRONT SPAR AT KRAS 206.2+11". REPAIRED SKIN PER EO.SDR SWAA2018032020564Skin · crackedRT WING INBOARD LEADING EDGE SKIN FASTENER HOLE CRACKED AT FRONT SPAR KRAS 206.2+12". REPAIRED SKIN PER SRM.SDR FDEA201803140684Skin · crackedLEFT WING FIXED LEADING EDGE AT XOS 991.5 LEADING EDGE SKIN FOUND CRACKED ABOUT 8 INCHES. REPAIRED IAW SRM 57-40-01-2R, FIG 261, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140683Doubler · crackedLEFT WING FIXED LEADING EDGE AT XOS 991.5 LOWER SURFACE DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-01-2R, FIG 201, REPAIR 9. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140680Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140679Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 654 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201803140678Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 670 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIG 203, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140681Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 623 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201803140682Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 627 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR DALA2018031301628Access Panel · crackedCRACKED RT WING LOWER ACCESS PANEL AT THE TRAILING EDGE AREA XRS 150. THE ACCESS PANEL WAS REPAIRED SRM 57-50-01-2R, 51-41-01 0G, AND 51-41-05-0G.SDR DALA2018031301626None · noneEXCESSIVE CORROSION ON FUEL ACCSESS PLATE #620CT, 520CT, AND 520DT AT SETTLEMENT AND COUNTERSINK AREA RH/LH WING IN REFERENCE NRCS 00549, 00553, AND 00554. NRC 00603: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 620CT WERE REPLACED DUE TO BLEND OUT REPAIR SDR IPXA2018033128026Skin · crackedINSPECTION TYPE: 2C, RT WING LOWER SKIN HAS TWO CRACKS AROUND FUEL ACCESS PANEL LANDING BETWEEN XORS 683.4 - 713.6. REPAIRED THE SKIN IAW SRM 57-20-02, REPAIR 5, FIG 201.SDR IPXA2018033028006Skin · crackedINSPECTION TYPE: 2C, LEFT WING SKIN LOWER SURFACE HAS SIX CRACKS AROUND FUEL ACCESS PANEL LANDING BETWEEN XORS 683.4 AND 713.6. REPAIRED THE SKIN IAW SRM 57-20-02.SDR YENA201803110906Skin · crackedDURING CURRENT (03/2018) HMV AT SAL, DAMAGE WAS FOUND ON THE LT WING AFT REAR SPAR LOWER SKIN (P/N: 190-33065-009) AFT EDGE, AT RIB 10+1” LEVEL. THE DAMAGE CONSISTS OF A CRACK MEASURING APPROXIMATELY 1.332” IN LENGTH (REF. /1/ FOR DETAILS). THE DAMAGE WAS ASSESDR DALA2018031201623Access Panel · corrodedCORROSION OUT OF LIMITS ON ACCESS PANEL 620AT. THE ACCES PANEL WAS REPLACED IAW SRM 57-10-01-2R-2, PAR 5.SDR IPXA2018032627827Skin · corrodedINSPECTION TYPE: 2C, LT WING UPPER SURFACE HAS CORROSION AROUND RIVET AFT OF NR 2 L/E SLAT. REPAIRED THE LT WING UPPER FWD SKIN AT XORS 151 AND STRINGER 19 IAW EA 011-5730-01-A7170, REV IR, AND EO MD11-5730-67882-A.SDR IPXA2018032127685Skin · corrodedINSPECTION TYPE: 2C, LT WING UPPER SKIN HAS CORROSION FWD OF THE NR 2 SPOILER XORS 538.49. REPAIRED THE SKIN IAW EA 011-5730-01-A7168, IR AND EO 5730-67845-A.
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