JASC 5341
Service difficulty reports · 489
Reports filed under 5341 · Fuselage, Wing Attach Fittings, 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 = '5341' 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 = '5341' 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 RAIA201912310003Support Bracket · crackedR/H WING I/B UPPER SURFACE AT FR 41 BELLY FAIRING L ANGLE SUPPORT BRACKET IS CRACKED....R&R R/H UPPER WING L ANGLE AT FR 41SDR FDEA201906281475Fitting · crackedDURING PERFORMING ROTOTEST INSPECTION OF FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RH UPPER HOLE FOUND CRACK SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0347502 PT1, EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE UPPER HOLESDR DALA2019041002369Fitting · crackedCRACK ON RIGHT MAIN FRAME WING TO FUSELAGE FITTING, LONGERON NUMBER 22. NRC 00464: FITTING WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND 51-41-01-0G. (LP #1023991)SDR A6WA2019022746432Angle · crackedFS 484 RBL 27 OUTBD CLIP CRACKED. REPLACEDSDR ABXR2019010800014Splice Plate · corrodedLEFT FUSELAGE UPPER WING TO BODY SPLICE STA 785-955 CORRODED IN MULTIPLE AREAS.SDR SIMA20190108003Support · crackedRT UPEER WING/FUSELAGE SUPPORT IS CRACKED APROX. 3/4" BETWEEN THE RIVETS. JUST AFT OF FRAME 50. C/A-INSTALLED NEW RT UPPER WING/FUSELAGE SUPPORT IAW SRM 51-40-02.SDR AWHA201812180001Attach Fitting · corrodedDURING ROUTINE INSPECTION, CORROSION WAS FOUND IN THE NR 3, 5, AND 6 BOLT HOLE LOCATIONS IN THE RT UPPER AFT WING FITTINGS ATTACHMENT TO THE FUSELAGE AS REFERENCED IN THE NONDESTRUCTIVE TESTING MANUAL 53-20-06. REMOVAL OF THE CORROSION REQUIRED THE REAMING OF SDR A6WA2018110646139Attach Angle · crackedLEFT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 450.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.SDR A6WA2018110646138Attach Angle · crackedLEFT WING TO FUSELAGE PANEL ATTACH ANGLE CRACKED AT FS 476.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.SDR A6WA2018110646136Attach Angle · crackedRIGHT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS 476.00. REPLACED ANGLE IAW CRJ 200 SRM 51-42-06.SDR A6WA2018110646137Attach Angle · crackedRIGHT WING TO FUSELAGE PANEL ATTACH ANGLE IS CRACKED AT FS450.00. REPLACED ANGLE IAW CRJ200 SRM 51-42-06.SDR RAIA2018111130005Attach Fitting · cracked#4 R/H UPPER WING TO FUSELAGE ATTACHMEBNT FITTING IS CRACKED ..............REMOVED AND REPLACED #4 R/H SIDE UPPER WING TO FUSELAGE ATTACHMENT FITTINGSDR RAIA2018110810003Attach Fitting · cracked#3 L/H SIDE UPPER WING TO FUSELAGE ATTACHMENT FITTING IS CRACKED.................REPAIRED #3 L/SIDE UPPER WING TO FUSELAGE ATTACHMENT FITTINGSDR RAIA2018110810002Attach Fitting · cracked#2L/H SIDE UPPER WING TO FUSELAGE ATTACHMENT FITTING IS CRACKED ........REMOVED AND REPLACED #2 L/H SIDE UPPER WING TO FUSELAGE ATTACHMENT FITTINGSDR FDEA201810093248Support · corrodedEVIDENCE OF CORROSION ON INBOARD FLAP TRACK SUPPORT STRUCTURE FITTING IN RT MLG WHEEL WELL AFT BULKHEAD BS 1180. CORROSION REMOVED IAW SRM 51-10-02 REV 125. REPAIR CARRIED OUT IAW EA F-5340-TO343107.SDR WVER20180821004Bushing · gougedUPON REMOVAL OF LH REAR SPAR LINK ASSY BOLTS, FOUND BUSHING ON TOP FWD FUSELAGE FRAME LUG TO BE GOUGED.SDR CA180706012Bolt · cracked(CAN) BOLTS WERE PROCURED IN A LOT OF 26 FOR USE AS WING ATTACHMENT BOLTS ON CANADIAN MILITARY CC130H HERCULES AIRCRAFT. PRIOR TO INSTALLATION THE RCAF TECHNICAL ORDER REQUIRES THAT THESE BOLTS UNDERGO MAGNETIC PARTICLE TESTING. DURING MAGNETIC PARTICLE TESTSDR R61A201712160946Flange · corrodedWHILE IN HVY MX CHECK - CORROSION ON THE AIRCRAFT ON THE AFT WING TO FUSELAGE ATTACH FLANGE. MARKED IN WHITE. REMOVED AND REPLACED RH AND LH AFT WING TO FUSELAGE ATTACH FLANGES REF
SRM 51-23-04, 51-40-02, 51-40-08, 51-23-05, 51-23-06
P/N'S 170-92409-003 AND SDR 2017FA0000516Wing Root · crackedAT INSPECTION, FOUND BOTH R/H WING ROOT SKIN DOUBLER CRACKED. CONTACTED THE MANUFACTURER, FOUND THAT THIS IS A COMMON PROBLEM.SDR FQAR20171011092Frame · crackedDURING ROUTINE MAINTENANCE, A FUSELAGE FRAME THAT ACTS AS THE FORWARD WING ATTACH STRUCTURE WAS FOUND TO BE CRACKED AT THE UPPER RIGHT END.SDR DALA2017091606926Fitting · crackedCRACK ON MAIN FRAME WING TO FUSELAGE FITTING BS 661, LONGERON 22L. REPAIRED IAW ETI-17-17-155, REV ORIGINAL, AND ER/A 560940-14, REV ORIGINAL.SDR AALA201706119009Stop · wornWEAR ON SCREW DOOR STOP AT AFT GALLEY DOOR AFT POSITIONS 1, 2, AND 5. REPLACED AND PERFORMED ADJUSTMENT ON SCREW DOOR STOP IAW AMM 52-13-31, AND AMM 52-13-00.SDR EBVR20160929001Bolt · crackedWHILE COMPLYING WITH THE MAGNETIC PARTICLE INSPECTION OF THE WING ATTACH BOLTS THE RT FORWARD UPPER BOLT WAS FOUND TO BE CRACKED. THE CRACK WAS FOUND ON THE SHANK JUST BELOW THE THREADS OF THE RETAINING (NON LOAD BEARING) SECTION OF THE SPECIAL BOLT. THE CRACKSDR SWAA2016071854021Angle · corrodedAFT GALLEY DOOR Z-ANGLE CORRODED. REPAIRED THE ANGLE IAW SRM.SDR HALA2016040400111Support Fitting · corrodedWING TO BS 832 LOWER END OF SUPPORT FAIRING CORRODED. LT SIDE, ON EXISTENT REPAIR. REMOVED CORROSION AT WING TO BS 832 LOWER END OF SUPPORT FAIRING LT SIDE ON EXISTENT REPAIR, FOUND 100 PERCENT TO BE OUT OF LIMITS IAW SRM 53-00-00 AND R & R PREVIOUS REPAIR ISDR HALA2016032300110Fitting · corrodedWING TO BS 832 FITTING ON LONGERON 30 CORRODED. REMOVED CORROSION AT WING TO BODY BS 832 FITTING ON LONGERON 30 ORIGINAL MATERIAL 125" REMAINING .098" AND LOSS OF .027", FOUND OUT OF LIMITS IAW SRM 53-00-00. R & R FITTING IAW DWG 5971098, REV E AND DWG S1440SDR SIMA20160112005Attach Angle · crackedLEFT WING TO FUSELAGE UPPER ATTACH ANGLE CRACKED, BETWEEN FRAMES 48 & 49. REPAIRED IAW SRM 53-23-12.SDR REXA2015091400875Link · crackedLEFT AFT WING ATTACH FITTING LINK FS 797, LBL45 SPHERICAL BALL APPEARS TO HAVE A CRACK. COMPLIED WITH SB 670BA-57-016 PART A OP 1214.SDR CA150722009Drag Angle · cracked(CAN) LT WING TO FUSELAGE DRAG ANGLE CRACKED. REPAIRED UNDER REO 215-57-40-033.SDR 2015FA0000285Attach Fitting · crackedRIGHT UPPER FWD WING BOLT FITTING CRACKED.SDR ASOA2015061713120Seat Track · corrodedLEFT SIDE SEAT TRACK SEGMENT BS 784-861 IS CORRODED SEVERAL AREAS. FOUND BEYOND ALLOWABLE LIMITS SRM 53-41-49 & REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801, A03.SDR 7AHR2015043000138Fitting · crackedWING TO FUSELAGE FITTING CRACKED LT SIDE BS 600, LONGERON 22L. R & R THE FITTING IAW SRM 51-30-1, 51-10-02, 51-10-4, 5110-2 AND 57-31-4.SDR 7AHR2015043000137Fitting · crackedRIGHT WING TO FUSELAGE FITTING IS CRACKED AT BS 600-LONGERON 22R. R & R THE FITTING IAW SRM 51-30-5, PGS 12-14, 51-30-01,51-10-4.51-10-2 AND 57-31-4.SDR GLBA2015041000511Fitting · crackedDURING A SCHEDULED INSPECTION MX FOUND A CRACK ON THE RT SIDE FUSELAGE AT FS 8089.7. WING TO FUSELAGE FITTING IN THE BEND RADIUS AT THE UPPER END OF THE FITTING, 1.9 INCHES IN LENGTH. REPAIRED IAW EO 15-120-57-004. MAJOR REPAIR.SDR R61A201503110202Bracket · corrodedDURING HEAVY CHECK, WING TO FUSELAGE FAIRING ATTACH BRACKET AIR FRAME SIDE WHERE FAIRING 191FL IS CORRODED. MAINTENANCE R & R 4 EACH ATTACH FAIRING BRACKETS IAW SRM 51-41-02, 51-42-02. AIRCRAFT REMAINS UNTIL HEAVY CHECK IS COMPLETED.SDR 7C7A201502220011Bolt · corrodedLT AND RT REAR SPAR WING/FUSELAGE JOINT BOLTS CORRODED. REPLACED THE BOLTS IAW AMM .SDR SIMA20141228015Attach Angle · crackedLEFT UPPER WING TO FUSELAGE LOWER ATTACHMENT ANGLE ON WING FWD OF SPAR 3 HAS A 1 INCH CRACK ON THE FWD EDGE OF ANGLE. REPAIRED IAW ETN EM-53-142.SDR FDEA201412254184Attach Fitting · crackedCENTER WING JOINT AT FRAME 40, FOUND LT SIDE CRACKED. REPAIRED IAW EA 6-5710-T0314674 P1.SDR ASOA2014122211914Fitting · chafedLEFT FUSELAGE AND WING FITTING FWD SIDE OF AFT FLANGE HAVE CONTACT MARKS FROM LINKS. REMOVED DAMAGED FROM FUSELAGE AND WING FITTINGS IAW SRM 51-12-00-001-A01, TR 51-0050.SDR SWIA201439625Lug · crackedRT FUSELAGE JUST FWD OF BS 473.15, RBL47 WING TO BODY LUG A INTERCOSTAL ASSY CRACKED ABOUT HALFWAY UP. C-CHECK, REMOVED AND INSTALLED NEW RT INTERCOSTAL ASSY JUST FWD OF WING TO BODY LUG AT FS 473.15, RBL 47, STS EA.SDR SWIA201439624Lug · crackedRIGHT FUSELAGE JUST AFT OF BS 473.15, RBL47 WING TO BODY LUG A INTERCOSTAL ASSY CRACKED ABOUT HALF WAY UP. C-CHECK, REMOVED AND INSTALLED NEW RT INTERCOSTAL ASSY JUST FWD OF WING TO BODY LUG AT FS 473.15, RBL 47 IAW STS EA.SDR A6WA201441825Fitting · crackedPRESS FLOOR SUPPORT BEAM LBL 27 & LBL 36 CLIPS TO INTERCOSTAL AT FS 484 IS CRACKED.SDR SWIA201438364Attach Fitting · chafedRT WING TO FUSELAGE ATTACH FITTING AT BS 473.15 CHAFED AT OTBD FWD CORNER. C-CHECK, REPAIRED ATTACH FITTING IAW EA.SDR FDEA201405050947Splice · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING AT FRAME 44. FOUND TWO CRACK SIGNALS. REPAIRD IAW EA 6-5710-T0308161 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201405050946Splice · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING AT 7 INCHES IN FRONT OF FRAME 44 STIFFENER LOCATION, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308161 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201405030927Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201405030926Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201405030925Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201405030924Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201405030923Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.
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