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 FDEA202402120143Doubler · crackedRIGHT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 654 FOUND CRACK ABOUT 0.4 INCH. RT WING FIXED LEADING EDGE AT XOS 654 CRACKED BEADED DOUBLER REPAIR CARRIED OUT IAW MD-11 SRM 57-40-02-2R, REPAIR 15, FIGURE 203. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA202402120141Doubler · crackedLEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 582 FOUND CRACK ABOUT 0.8 INCH. LT WING FIXED LEADING EDGE AT XOS 582 CRACKED BEADED DOUBLER REPAIR CARRIED OUT IAW MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202402120140Doubler · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACK ABOUT 1 INCH. LEFT WING FIXED LEADING EDGE AT XOS 906 CRACKED RIB DOUBLER REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-OG. RIB DOUBLER FABRICATED AS PER DOUGLAS DRAWING ARB 3954 REVISION K.SDR SWAA2024030754507Panel · delaminatedRIGHT WING LOWER L/E PANEL#621HB IS DELAMINATED AT THE AFT EDGE<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #621HB AS PER B737 SRM 51-70-04-2R-13 PARAG 4 D-G; MATERIAL USED RESIN PO#1791128; FIBERGLASS PO#1473815; EQUIPMENT USED: HOT BONDERSDR SWAA2024030754509Panel · delaminatedRIGHT WING LOWER L/E PANEL#621JB IS DELAMINATED AT THE AFT EDGE<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #621JB AS PER B737 SRM 51-70-04-2R-13 PARAG 4 D-G; MATERIAL USED RESIN PO#1791128; FIBERGLASS PO#1473815; EQUIPMENT USED: HOT BONDERSDR SWAA2024030754508Panel · delaminatedRIGHT WING LOWER L/E PANEL#621YB IS DELAMINATED AT THE AFT EDGE<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON PANEL #621YB AS PER B737 SRM 57-41-01-2R-6 PARAG 4-J-M; MATERIAL USED: PO#2039275;[02] VERIFIED APPLIED PERMANEMT REPAIR ON DAMAGE AREA ASSDR REXA2024102801054Access Panel · chafedRH FLAP ACCESS PANEL 684EB IS CHAFED. REMOVED AND REPLACED 684EBSDR SWAA2024022751013Support · crackedR/WING TRAILING EDGE ACCESS PANEL 661AB MUST O/B FWD SUPPORT STRUCTURE HAS A CRACK AT O/B EDGE MKD 107-010<[01] REMOVED AND REPLACE DAMAGED WIGGLE PLATE AT R/WING T/E ACCESS PANEL 661AB FWD SUPPORT STRUCTURE SRM 51-40-02-0G-0 AND DWG115A3760;[02] VERIFIED STEPSDR A6WA202402068716Skin · dentedCREW REPORTED DENT LOCATED ON UPPER LH WINGSKIN DURING WALKAROUND. WORKING WITH MHI, DENT WAS FOUND TO BE A PREVIOUS BLEND REPAIR WITH UNDERLYING FREEZE PLUG IN THE FWD AND MID WING PLANKS. MHI OR AWA COULD NOT FIND ANY DOCUMENTATION FOR THIS REPAIR. MHI ISSDR VNAA202402050024Skin · wornWEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN. SETTLEMENT AREAS OF FAIRINGS 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01; SETTLEMENT AREAS OF SDR VNAA202402050023Skin · wornWEAR ON SETTLEMENT AREA OF FAIRINGS 583AB, 586AB, 592AB, 595AB AND 597AB AT LH WING LOWER SKIN. SETTLEMENT AREAS OF FAIRINGS 583AB, 586AB, 592AB, 595AB AND 597AB AT LH WING LOWER SKIN WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-001-A01; SETTLEMENT AREAS OF FSDR REXA2024102801038Access Panel · chafedPNL 684HT IS CHAFED. CHAFED AREA ON ACCESS PANEL 684HT EVALUATED AND FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS IAW CRJ-900 SRM 57-52-01-101-001-A01. RECEIVED NEW SERVICEABLE VANE ACCESS PANEL 684HT (P/N CC670-14027-3), LOCATED AND DRILLED NEW PANEL IAW CRJ-90SDR SWAA2024030848716Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLES UNDER THE T/E SEAL (MARKED)<[01] R/W T/ E PANEL 661BB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] JOB COMSDR VNAA202403010001Access Panel · wornLH AILERON FLUTTER DAMPER ACCESS PANEL (552KB) WITHIN 1,892.85 FHS FROM IR (BEFORE 8000 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. LH AILERON FLUTTER DAMPER ACCESS PANEL (552KB) WAS REPAIRED PER REO 690-57-22-077 REV -SDR REXA2024022700226Skin · chafedRH LEADING EDGE PANEL 631AR IS CHAFED. REMOVED THE DAMAGE ON RH LEADING EDGE PANEL 631AR IAW. CRJ900 SRM 51-12-00-001-001-A01. C/W AND ACCOMPLISHED EA# CRJ957-16065 REV IR. DATE 2/6/2024.SDR NACA2024020200001Skin · cracked4.5 INCH CRACK FOUND AT #3 SLAT ACTUATOR CUTOUT. WORK IN PROGRESS.SDR YENA2024020600230Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION ON LH WING TOP SKIN LOWER SURFACE OVERHANG AT TRAILING EDGE AREA BTW RIB 6 AND RIB 7; ACCOMPLISHED THE REPAIR OF CORROSION ON LH WING TOP SKIN PANEL 2 FALSE REAR SPAR TE OVERHANG LOWER SURFACE BETWEEN WX3622-WX4013 IN ACCORSDR DALA2024020101458Skin · mechanic error(LOG 0180347) LH WING UPPER SKIN BTWN RIB 22 / RIB 24 AND STGR U-13.5 / MISDRILLED HOLES. REPAIRED PER ERA 614975-14.SDR DALA2024020101456Skin · mechanic error(LOG 0180822) MISDRILLED HOLES ON THE LH WING UPPER SKIN RIB 22 / RIB 24 AND U-13.5, REAPIR AS REQUIRED. AT LH WING UPPER SKIN RIB 22/ RIB 24 AND U-13.5 THE MISDRILLED HOLES WERE REPAIRED I.A.W B737-800, ER/A 614975-14 REV. 1.SDR NACA2024013000002Skin · corrodedDURING NRC:CA1528/152 , CORROSION WAS FOUND AT LH WING UPPER SURFACE , WBL79 , S-11 AREA. REMOVED CORROSION LEVEL 2 AT LH WING UPPER SURFACE WBL 83,S11 AREA FROM P/N 65C25204-15 ORIGINAL THICKNESS 0.160" REMOVES 0.028"AND REMAINING THICKNESS IS 0.132" IS OVER SDR SWAA2024030546405Panel · crackedLT WING T/E PANEL 561AB AFT ROW OF FASTENER HOLES HAVE CRACKS AROUND THEM<[01] PANEL 561AB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024030546419Panel · crackedRT WING T/E PANEL 661CB AFT ROW OF FASTENER HOLES HAS HOLES WITH CRACKS AROUND THEM<[01] PANEL 661CB FASTENER HOLES HAVE BEEN REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024022346610Access Panel · crackedCRACK ACCESS PANEL 642BB AT RT WING 2024-68291<[01] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18185761 DUE DATE: 24-JAN-25.;[02] TOOL USED SCALE P/N:CR5200 S/N: 8343110878 DUE DATE: 21-FEB-24.;[03] TOOL USED: SÏ¿½CALE P/N: CR5200; S/N: 8342514597; DUE DATE: 21SDR YENA2024013000160Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG LOC. AT LEVEL BTW RIB 7 TO RIB 8 ON RH WING; REF AEROMAN W/O 2023 363/1 N/R 2023-749626 EVALUATED REWORKED AREA AND FOUND WITHIN LIMITS ON TRAILING EDGE TOP SKIN LOWER SURFACE OVSDR SWAA2024022346117Access Panel · crackedLEFT WING LOWER MID T/E ACCESS PANEL 561CB HAS SEVERAL FASTENERS HOLES WICTH SMALL CRACKS.<[01] **SUMMARY**<BR>1.ACCOMPLISHED PULSE-ECHO ULTRASONIC INSP. FOR DELAMINATION IAW B737 NDT P. 1; 51-01-02 AND P. 4; 51-00-01. DAMAGE NOTED AND LOCATION IDENTIFIED. EQUSDR SWAA2024022346119Access Panel · crackedLEFT WING LOWER MID T/E ACCESS PANEL 561AB HAS SEVERAL FASTENERS HOLES WICTH SMALL CRACKS.<[01] MEASUREMENTS;[02] REPAIRED DAMAGE AREA AT LEFT WING LOWER T/EDGE ACCESS PANEL #561ABAS PER SRM 51-70-04-2R-9.MATERIAL USED EY 3804 A/B PO 20038047 PLUS BMS9-3-120 TSDR SWAA2024022346118Access Panel · crackedLEFT WING LOWER MID T/E ACCESS PANEL 561BB HAS SEVERAL FASTENERS HOLES WICTH SMALL CRACKS.<[01] APPLIED REPAIR AT PANEL# 561BB PER B737 SRM 51-70-04-2R-9 AND 737SRM 51-70-04-2R-0 PARAGRAPH 4.N.2 MATERIAL USED RESIN EY3804 PO#2038047 FIBERGLASS PO#1690463.APPLISDR AALA202402139280Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE UPPER SKIN PANEL; #2 BETWEEN RIBS 10 AND 11. REPAIRED LEFT WING UPPER SKIN PANEL PER EA 349927.SDR YENA2024013100218Skin · crackedDURING HEAVY MAINTENANCE: INITIAL INSPECTION: CRACK ON LH WING UPPER SKIN PANEL T/E BTW RIB 15-17; (RESOLVED ON W/O: 1267464 TASKCARD: NR-00005) REF TOMX W/O# 2452. N/R# 00027. LH WING UPPER SKIN PANEL T/E BTW RIB 15-17 WAS REPAIRED PER EMB 190 SRM 57-50-01 RSDR YENA2024012900128Skin · crackedDURING HEAVY MAINTENANCE: INITIAL INSPECTION: CRACK ON RH WING LOWER SKIN BTW RIB 11/12 (2EA) AND SPAR II ; (RESOLVED ON W/O: 1267464 TASKCARD: NR-00123) REF TOMX W/O3 2452. N/R 00344.. CRACK ON RH WING LOWER SKIN LOCATED AT RIB 11/12 AND SPAR II WERE REPAIREDSDR YENA2024012900127Skin · crackedDURING HEAVY MAINTENANCE: INITIAL INSPECTION: CRACK ON RH WING LOWER SKIN LOCATED AT RIB11/12 AND SPAR II ; (RESOLVED ON W/O: 1267464 TASKCARD: NR-00124) REF TOMX W/O# 2452. N/R 00028. CRACK ON RH WING LOWER SKIN LOCATED AT RIB 10/11 AND SPAR II WAS REPAIRED SDR YENA2024012900113Skin · crackedDURING HEAVY MAINTENANCE: WINGS / RH WING / TRAILING EDGE LOWER SKIN REAR SPAR / RIBS 10-11,11-12 / CRACK DAMAGE 1-3 / MATERIAL SUBSITUTION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR).SDR YENA2024012900112Skin · crackedDURING HEAVY MAINTENANCE: WINGS / RH WING / TRAILING EDGE LOWER SKIN REAR SPAR / RIB 10-12 / CRACK - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR R61A202401250003Skin Panel · crackedCRACK RH WING BOTTOM SIDE AT RIB 4A . PERFORMED TEMPORARY REPAIR BY CUTOUT, FILLER/DOUBLER REPAIR ON RH WING BOTTOM SIDE AT RIB 4A IN ACCORDANCE WITH, REF ETD2024-170--000607.SDR IPXA2024013116972Access Panel · damagedALL FASTENER HOLES IN THE LWR SIDE OUTER WING SKIN, FOR FUEL TANK ACCESS PANEL 550MB (NEAR RIB 24), HAVE CORROSION INDICATIONS INSIDE THE HOLES AND SURROUNDING OUTER SURFACE. REMOVED LIGHT CORROSION BY HAND IN HOLE AND SURROUNDING OUTER SURFACE IN PANEL 550MB,SDR IPXA2024013017376Access Panel · corroded13EA FASTENER HOLES IN THE LWR SIDE OUTER WING SKIN, FOR FUEL TANK ACCESS PNL 650LB (NEAR RIB 23), HAVE CORROSION INDICATIONS INSIDE THE HOLES AND 1EA OUT OF ROUND. ROTO PERFORMED ON FASTENER HOLES. NO DEFECTS FOUND IAW 51-10-01.SDR SWAA2024030544029Panel · damagedR/W T/E REAR SPAR LOWER PANEL 651GB INB SUPPORT RODS UPPER SUPPORT FITTING EXCESSIVE PLAY AND ELONGATATED HOLES MKD DOT<[01] REMOVED AND REPLACED SUPPORT FITTING AT R/W T/E REAR SPAR LOWER PANEL 651GB REF. SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2024021243908Access Panel · crackedCRACK ACCESS PANEL 632NB ON FLOAT FUEL TANK AT RT WING 2024-67341<[01] REPLACED FUEL TANK FLOAT AT RT WING ON ACCESS PANEL 632NB IAW B737-700 CMM 28-40-11 SAFRAN STEP 3.A (2) (E);[02] CORRECTED STEP 1<BR>REPLACED FUEL TANK FLOAT AT RT WING ON ACCESS PANEL 632NSDR SWAA2024021243909Access Panel · crackedCRACK ACCESS PANEL 632QB ON FLOAT FUEL TANK AT RT WING 2024-67340<[01] REPLACED FUEL TANK FLOAT AT RT WING ON ACCESS PANEL 632QB IAW B737-700 CMM 28-40-11 SAFRAN STEP 3.A (2) (E);[02] CORRECTED STEP 1<BR>REPLACED FUEL TANK FLOAT AT RT WING ON ACCESS PANEL 632QSDR DALA2024012601186Skin · corrodedSHIP 5649 RIGHT WING UPPER SURFACE, SKIN HAS SEVERAL SPOTS OF CORROSION, BETWEEN BBL.70.50, UP TO WS.177.50, FROM REAR SPAR, UP TO WING SPLICE.DOT#24/001. CORRECTIVE ACTION: COMPLIED WITH RH WING UPPER SKIN CORROSION REPAIR PER DELTA ERA 522812-14 REV. A. (016SDR CALA2024012400217Skin · corrodedR/H WING FRONT SPAR CORD HAS CORROSION AT APPROX OFSS 667.5. THIS ELB WAS CREATED FOR A SIGNIFICANT FINDINGS REPORT. SPAR CORD W AS REPAIRED ON BAM N/R 001787959. SIGNIFICANT FINDINGS REPORT CREATED(SFR NUMBER 1034910) FOR R/H WING LOWER SKIN CORROSION FWD OF SDR SWAA2024021243573Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2024-67333<[01] TOOL USED CALIPER PN: 500-197-30; SN: 15120589; DUE DATE: 13/FEB/24.;[02] TOOL USED HOTBONDER P/N HCS9200B; S/N 18165044 DUE DATE 26-MAR-24.;[03] TOOL USED SCALE P/N CR5200 S/N 83431108SDR 2024FA0000130Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR DALA2024012501159Skin · corrodedSHIP 5649 DTA MONITOR INSPECTION LOG REF ERA 522812-14 REV A, CORROSION ON THE RH WING UPPER SKIN SURFACE BETWEEN WBL=80.0 TO WS=204.5 AND BETWEEN THE WING REAR SPAR TO W-STR 14R. CORRECTIVE ACTION: REF ERA 522812-14. (0166707)SDR SWAA2024021243112Plate · crackedCRACK PLATE ASSY TRAILING EDGE LOCATED ORSS284 AT RT WING 2024-67271<[01] REPLACED PLATE ASSY TRAILING EDGE LOCATED BTW ORSS278 TO ORSS321 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3700 SHEET 27 REV -. SEE INDIVIDUAL SIGNOFFS BELOW;SDR SWAA2024021243111Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 217 AT LT WING 2024-67260<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 217 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A2001 SHEET 1 REV B. SEE INDIVIDUAL SIGNOFFSSDR SWAA2024021243106Plate · crackedCRACK ON CORRUGATED PLATE TRAILING EDGE LOCATED IRSS232 AT RT WING 2024-67273<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS232 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9;SRM 51-40-02 AND DWG # 115A2001 REV. B.SEE INDIVIDUAL SIGNOFFS BELOW.;[02] RESDR SWAA2024022742622Panel · corrodedRIGHT WING LEADING EDGE FUELING STATION PANEL 621GB; FUELING GAUGE BRACKET IS CORRODED<[01] REPLACED REFUEL PANEL (P15) PER AMM 28-21-00-000-801; AMM 28-21-00-400-801 STEP 3.A THRU 3.G. PERFORMED GOOD BONDIG CHECK RECORDING VALUE 1.48 MILLIOHMS<BR>MULTIMETER CSDR SWAA2024020542629Access Panel · crackedL/H WING UPPER I/B ACCESS PANEL 551 DT CRACK AT T/E<[01] APPLIED REPAIR AT PANEL#551DT PER B737 SRM 51-70-04-2R-0 PARAGRAPH 4.N MATERIAL USED RESIN EY 3804 PO#20400614 FIBERGLASS PO#1690463.;[02] VERIFIED STEP 1SDR IPXA2024012228494Skin · debonded*SDR FILED OPEN* *MAJOR REPAIR* FAULT - DISBOND SKIN, LH WING LE NO.4 SLAT INBD TE CORNER. (REPAIR) 1.OK TO INSTALL CHECK SATISFIED.<BR>2.I.A.W. AMM 27-81-02-424-099 REV.141 STEP 1.A TO 1.H(15) INSTALL NO.4 SLAT OF THE LH WING LEADING EDGE.
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