JASC 5714
Service difficulty reports · 1,451
Reports filed under 5714 · Wing, Center Box, 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 = '5714' 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 = '5714' 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 2008UALA03798Panel · corrodedMAIN CABIN STA 955, UPPER SURFACE OF WING BOX PANEL CORRODED AT LBL 36. REMOVED CORROSION DAMAGE TO CENTER WING BOX PANEL AT LBL36, TRIMMED THE FLOORBEAM LOWER CHORD AND THE UPPER WING SKIN. FABRICATED A FILLER FOR THE WING SKIN CUT-OUT, A -1 AND -4 FILLER, -SDR CALA0800662Structure · wornWING CENTER SECTION RIGHT-HAND LOWER CHORD AT STATION 530 40RBL HAS A HOLE. REPAIR COMPLETED PER ECRA 5351-01064 ON WING TO BODY FAIRING SUPPORT RBL 40.1 LOWER CHORD REPAIR.SDR CA081112002Shroud · mismanufactured(CAN) DURING PRODUCTION OF 4208 IT WAS DISCOVERED THAT THE CENTER WING LOWER SHROUD RT DRAIN HOLES WERE NOT PRESENT. A DISCREPANCY WAS RAISED AND CLEARED BY DRILLING NEW HOLES IN SITER. UPON THE DELIVERY/ACCEPTANCE FLIGHT, IT WAS DISCOVERED THAT THE AFT COFFEESDR SWAA082611Stiffener · crackedDURING SCHEDULED BRDG CHECK, FOUND CENTER FUEL TANK VERTICAL STIFFENER CRACKED AT STA 547, RBL 57. REMOVED AND REPLACED STIFFENER PER SRM.SDR 08FDEA01707Skin · corrodedMAIN DECK CENTER WING UPPER SKIN SURFACE AT STA 1341 X = 101 FOUND CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-113145, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 08FDEA01357Skin · delaminatedDELAMINATION OUT OF LIMIT FOUND ON SPOILER NR 5 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-53 PB 400.SDR HNA2008F00006Bracket · crackedIN WING BOX, UNDER ACCESS PANEL 261 FT BRACKET ANGLE BETWEEN LT STRINGER 2 AND WING BOX FRAME AT FS 369.511 FOUND CRACKED. REPLACED WITH NEW PN 85350270-101 IAW SRM 51-40-00 CRACK MINOR IN NATURE, NON STRUCTURAL IN TYPE. (K)SDR KCSA081138Skin · corrodedCENTER TANK SKIN HAS CORROSION AT SUMP DRAIN AREA AT STA-1057 RBL-114.SDR UPS08851825Structure · damagedINSPECTION TYPE:C3 FH WING CENTER LE HAS LWR ATTACH SCREW HOLE DAMAGED AFT OF SLOT DOOR. REMOVED DAMAGED, FAB AND INSTALL REPAIR DOUBLER IAW SRM 57-3-1 FIG4, EO DC8-5720-4087 APPD C, 51-1-8.SDR TRAX200800147Fairing · crackedRIGHT SIDE WING BOX FAIRING FR 28A FACING CRACKED. REPAIR ACCOMPLISHED IAW SRM 51-25-01
SDR COEA0803819Angle · crackedFOUND DURING HEAVY CHECK, LT AND RT AFT UPPER WING PRESSURE DECK INTERNAL SPLICE ANGLES CRACKED. AFT OF FRAME 27 AT STRINGERS 4L AND 4R. LT ANGLE PN IS S53573201210, RT S53573201211. SRAS, SHEET REF: SO/TS-232/08/4462. DAMAGES LEFT, AS IS AFTER INSPECTION SDR 08FDEA00062Skin · corrodedMAIN DECK CARGO COMPT, FOUND UNDER FLOOR STRUCTURE WITH CORROSION AT STA 1230, LBL 105". REPAIR CARRIED OUT AS PER FEDEX EA 1-5330-117256, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR SWAA076433Support Beam · crackedDURING SCHEDULED 22Y CHECK, FOUND WING CENTER SECTION SUPPORT BEAM WEB CRACKED AT BS 616, BL 40.8. REPAIRED WEB PER AAR EA.SDR LR7A07173Beam · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2, FOUND BEAM CAP HOLE CRACK COMMON TO WING ATTACH ANGLE AT FS 517, CWS61R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076.SDR LR7A07172Stringer · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2 FOUND HOLE CRACK IN STRINGER LEG COMMON TO WING ATTACH ANGLE AT CWS61L WL256 STRINGER 20 HOLE 36Y. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-076.SDR LR7A07170Rib · crackedDURING SCHEDULED C-3 CHECK, PER SB382-57-85 R2, FOUND CENTER WING LOWER RIB CAP CRACKED AT CWS61R, STGR 24. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-085.SDR LR7A07167Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS101L, WL285. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-078.SDR LR7A07166Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS517, CWS101L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-074.SDR LR7A07165Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 597, CWS140R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075.SDR LR7A07164Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140R, WL285. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-079.SDR LR7A07163Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075.SDR LR7A07162Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND RT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 517, CWS140R, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075.SDR LR7A07161Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119, FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 597, CWS101L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-074.SDR LR7A07160Rib · crackedDURING SCHEDULED C-3 CHECK, PER JOB CARD HSP57119 FOUND LT CENTER WING BULKHEAD FOOT RIB CAP CRACKED AT FS 597, CWS140L, WL256. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-07-075.SDR TRAX200701805Structure · crackedRT WING BOX FR 28 CRACKED, RESOLVED ON W/O: 75891 TASKCARD: N/R-00126. ON RT WING BOX FR 28 CRACK REMOVED IAW SRM 51-10-10 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRMSDR TRAX200701804Frame · crackedFOUND RT WING BOX FR 284 FACE PLATE CRACKED. REPLACED AS PER SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACOMPLISHED IN ACCORDANCE WITH SRM 51-25-01.SDR TRAX200701802Intercostal · crackedWING BOX RT INTERCOSTAL BTW FR 23D AND 24 L BRACKET CRACKED (291AL) BTW STR 2-3-4.
SDR TRAX200701801Intercostal · crackedWING BOX LT INTERCOSTAL BTW FR 23D AND 24 L BRACKET CRACKED (291AL) BTW STR 2-3-4.SDR TRAX200701740Structure · crackedWING BOX RIGHT FR 28 FACE PLATE CRACKED.SDR WRLA2007121Skin · corrodedDURING C-CHECK INSPECTION CORROSION FOUND ON RIGHT CENTER WING TANK UPPER SKIN AT XCW=110S1. ACCOMPLISHED ENGINEERING INSTRUCTION NO.W2007A57B-668 REV.00, REPAIR CORROSION ON CENTER WING UPPER SKIN UPPER SURFACE AT XCW=110 S1. REF EGAT NRC U05027.SDR TRAX200701651Angle · crackedRIGHT WING BOX FRAME 28A REPAIR ANGLE CRACKED.SDR TRAX200701761Fairing · crackedRIGHT WING BOX FAIRING PLATE CRACKED AT FR 28A.SDR TRAX200701637Intercostal · brokenWING BOX INTERCOSTAL ANGLE BROKEN AT FR 23D RIGHT STR 2R. A NEW ANGLE HAS BEEN FABRICATED IAW SRM 53-91-72 FIG 101 AND INSTALLED IAW SRM 51-25-01.SDR TRAX200701615Intercostal · crackedINTERCOSTAL CRACKED ON RIGHT WING BOX BETWEEN FAIRING FR 25 + 26. REPAIRED IAW NTO ANA/YUL07/260/338-005 REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH NTO NA/YUL/07/260/3SDR TRAX200701614Structure · crackedWING BOX RIGHT FR 22 CRACKED. FABRICATION COVER ON W/C 2000-119 WING BOX R/H FR 28 ANGLE REPLACED IAW SRM 51-25-01REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25SDR TRAX200701596Angle · brokenWING BOX INTERCOSTAL ANGLE BROKEN AT FR 23D, RIGHT STR 2. TRANSFER ON W/C 2000-8. SUPPLEMENTAL - SDR CLOSED 11/01/07.
SDR TRAX200701558Bracket · crackedWING BOX FR 24 L-BRACKET CRACKED 291BL.SDR TRAX200701453Intercostal · crackedWING BOX FR 23, JUNCTION WITH INTERCOSTAL, ANGLE CRACKED.SDR C1HA200781001Skin · corrodedWING CENTER SECTION LWR SKIN CORROSION, LT PRIMARY HEAT EXCHANGER PLENUM AREA. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW B727 SRM 57-30-1 FIG 4. REPAIRED IAW CHAMPION AIR, EO-727-5710-05.SDR 07FDEA03438Panel · failedFOUND WRONG INSTALLED FASTENERS AT CENTER WING BOX, FRAME 40-47. REPAIR PERFORMED BY INSTALLING NEW OVERSIZED BULL NOSE FASTENERS IAW EA 6-5710- 95919 AND RAS/042817/015/2006 ISSUE A.SDR 07FDEA03253Fitting · damagedDAMAGE FOUND IN ALL LAYERS OF HOLE (APPEARED TO BE TOOL MARKS) INSIDE CENTER WING BOX, FRAME 47 LHS LOWER CORNER ANGLE FITTING. REPAIR PERFORMED BY OVERSIZING HOLE AND INSTALLING FASTENER NSA5351-10 WITH TRANSITION FIT IAW EA 6-5710-99144 AND RAS/043285/014SDR COEA0749821Spar · chafedFOUND DURING HEAVY CHECK. MAJOR REPAIR, LEVEL 2 CORROSION ON CENTER WING BOX FRONT AND REAR SPAR UPPER EXTRUSION. CHAFES, BETWEEN RIBS 4L AND 4R. CORROSION ON AFT SPAR EXTRUSIONS IN SAME AREAS AS CHAFES. BLENDED CHAFES AND CORROSION IAW SRAS DS/ET 603.600/SDR 07FDEA03206Skin · chafedFOUND DEEP CHAFING MARKS IN LOWER SKIN OF TRIM TANK CENTER BOX UNDER THE WATER DRAIN INTAKE, INSIDE THE CENTER BOX. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5511-112507 AND RAS/CASA/5733/2007 ISS "A".SDR 07FDEA03045Angle · damagedDAMAGES, CRACKS AND CORROSION FOUND IN ANGLE FITTING HOLES IN CENTER WING BOX FRAME 47 RHS. REPAIR PERFORMED BY OVERSIZING THE HOLES AND CUT OUT THE EXTERNAL FITTING IAW EA 6-5710-112481 AND RAS/053362014/2007 ISS "A".SDR 07FDEA03044Angle · damagedDAMAGES, CRACKS AND CORROSION FOUND IN ANGLE FITTING HOLES IN CENTER WING BOX FRAME 47. REPAIR PERFORMED BY OVERSIZING THE HOLES IAW EA 6-5710-112481 AND RAS/013359/011/2001 ISS "A" AND RAS/053362014/2007 ISS "A".SDR UPS07M50972Structure · corrodedINSPECTION TYPE:C LEFT SIDE CENTER WING BOX TOPSIDE AT STA 1239.0 - 1189.0 X=108.0 FOUND CORROSION AROUND FASTENERS AS MARKED. LEFT SIDE CENTER WING BOX TOPSIDE AT STA 1239.0-1189.0 X=108.0 FASTENER AS MARK & CORRODED AREAS REMOVED. CORROSION ON UPP SKIN REMSDR 2007002Spar Cap · crackedWHILE PERFORMING AD 2003-18-01, CRACKS WERE FOUND UNDER THE LT LOWER, FWD, SPAR CAP DOUBLER IN THE CAP, SPAR WEB AND THE DOUBLER ITSELF. CRACKS WERE ALSO FOUND IN THE WING SKIN CUTOUTS AT ALL 4 LOWER CENTER WING BELT FRAME CUT-OUTS. RT FWD LOWER SPAR CAP CRACSDR 2007001Spar Cap · crackedWHILE PERFORMING AD 2003-18-01, CRACKS WERE FOUND UNDER THE LT LOWER, FWD, SPAR CAP DOUBLER IN THE CAP, SPAR WEB AND THE DOUBLER ITSELF. CRACKS WERE ALSO FOUND IN THE WING SKIN CUTOUTS AT ALL 4 LOWER CENTER WING BELT FRAME CUT-OUTS. RT FWD LOWER SPAR CAP CRACSDR 2007FA0000619Skin · corroded(5) MISSING AN426-3 RIVET HEADS ON LOWER CENTER SECTION SKINS PN F13147-L/-R PROMPTED INSPECTION HOLE INSTALLATION IAW SB-31 FOR REPAIR ACCESS. LIGHT SURFACE CORROSION WAS FOUND ON LOWER SKINS AND STIFFENERS. BOTH SIDES WERE CLEANED AND TREATED FOR CORROSION. SDR CALA0700336Vapor Barrier · crackedINSPECTION FOUND MLG WHEEL WELL LEFT FORWARD BULKHEAD HAD A CRACK ON VAPOR BARRIER, REAR SPAR CENTER SECTION, LT SIDE THAT HAD MIGRATED BEYOND A STOP DRILL. THE CRACK WAS NOW 18 INCHES LONG. A TEMPORARY REPAIR HAD BEEN PERFORMED PREVIOUSLY A FEW MONTHS PRIOR
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