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 UPS06448116Structure · corrodedINSPECTION TYPE:C FX WING CTR SECTION RT LOWER CHORD FOUND HEAVY CORROSION AT STA983 RBL 78 TO RBL 86 EXTERNAL SURFACE. CORROSION BLEND OUT 0.151" BY 1.5" BY 5" EXCEED SRM LIMIT. FX WING CTR SECTION RT LOWER CHORD REPAIRED AT RBL75 TO RBL87 AREA AS PER RS R5SDR LR7A06156Web · crackedDURING SCHEDULED C 2 CHECK PER JOB CARD HSP57170, FOUND RT CTR WING REAR BEAM WEB CRACKED AT CWS 80. REPAIRED WEB IAW LAC MEA 382-57-06-078.SDR QXEA200602278Panel · damagedYYC: CENTER WING UPPER ACCESS HOLE REBATES FROM STA RT YW42.00 TO LT YW42.00 HAVE FRETTING CORROSION AROUND BOLT HOLES AND SCRATCHES ON THE UPPER SURFACE. MAINTENANCE REPAIRED IAW Q400 SRM 51-21-00-350-801, SRM 51-21-10-380-801 AND SRM 51-25-10-370-801.SDR LR7A06058Web · crackedDURING SCHEDULED C6 CHECK PER SB 382-57-85 FOUND RT CNTR WING REAR WEB CRACKED AT RT CWS 84.3-140. REPAIRED WEB IAW SMP583 57-30-22.SDR 06FDEA2021Frame · corrodedCENTER WING, LWR BARREL SECTION, FOUND CORROSION BETWEEN STA -Y 1319 TO 1339, LONG 50L TO 50R; ON FRAMES, CHORDS, LONGERONS SKIN. FASTENERS REMOVED IAW SRM 53-33-01, CORROSION REMOVED IAW SRM 1-21-01 PARA 34. INSPECTED PERFORMED SKIN REPAIR, COMPLETED IAW SRSDR CALA0600269Stiffener · crackedINSPECTION FOUND A CRACK IN THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT LBL AND RBL 6.15. THE VERTICAL STIFFENER WAS REPAIRED IAW ECRA 5714-01018.SDR SWIA200616978Fitting · crackedCENTER WING BOX FS 484.00 LBL 27; BELOW WL 73.50 CLIP CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601R31171-17 PER CRJ200 REO 601R 53-41-059 REV 'A' AND SKYWEST RII 53-401.SDR 06FDEA1621Structure · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND CENTER BOX LOWER SURFACE STA XCW 20 LT - XCW 17 RT STRINGER 39, CORROSION ON PREVIOUSLY REWORKED AREA'S. REMOVED CORROSION IAW 57-20-00 FIG 8 SH 2, AND ACCOMPLISHED ATTACHED EA 8-5710-96136.SDR 06FDEA1620Structure · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: AT STA 1290, X= -110 CORROSION UNDER FITTING AND UPPER SURFACE CENTER WING. REMOVED FITTING ANB7440-515, SHIM ANB7444-501 AND STIFFENER, REMOVED CORROSION, COMPLETED WORK PER EA 8-5710-93150 ATTACHED.SDR 06FDEA1619Fitting · corrodedDURING AIRPLANE'S CONVERSION FROM P TO F/ACF FOUND: AT STA 1290, X= -110 CORROSION UNDER FITTING AND UPPER SURFACE CENTER WING. REMOVED FITTING ANB7440-515, SHIM ANB7444-501 AND STIFFENER, REMOVED CORROSION, COMPLETED WORK PER EA 8-5710-93150 ATTACHED.SDR 06FDEA01002Skin Panel · corrodedUPPER CARGO COMPARTMENT, UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1204 RBL 107.SDR 06FDEA01001Skin Panel · corrodedUPPER CARGO COMPARTMENT UNDER FLOOR AREA, CENTER WING TANK TOP SURFACE FOUND WITH CORROSION FS STA 1239 LBL 02.SDR ARWA20060214Finger Doubler · corrodedDURING "C" CHECK INSPECTION, MAIN CARGO COMPARTMENT STA.920, STA.940, STA.960, XCW 0 - XCW 23 CENTER WING SECCTION RT FINGER DOUBLER WITH CORROSION. REPAIRED FUSELAGE CENTER SECTION PRESSURE PANEL BETWEEN STA 920 AND FS 940 IN ACCORDANCE WITH DRAWING AIPSAC-SDR CALA0600039Stiffener · crackedINSPECTION FOUND THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER CRACKED AT LBL 6.15. A REPAIR WAS INSTALLED IAW ECRA 5714-01014. A DIP WAS ISSUED TO REINSPECT THE AREA EVERY 4,500 FLIGHT CYCLES AND TO REPLACE BOTH STIFFENERS PRIOR TO THE ACCUMULATION OSDR AU510002071Vapor Barrier · faultyFUEL VAPOR BARRIER LOCATED IN CENTER WING BOX WAS FOUND TO BE BELOW MINIMUM THICKNESS AND LIFTING. FOUND DURING INSPECTION IAW AD/737/245 AND BOEING SB 737-57-1250.SDR AU510002045Vapor Barrier · out of limitsWING CENTER SECTION FUEL VAPOR BARRIER UNDER LIMITS IN THE FOLLOWING SIX AREAS ON THE TRIANGLE POCKET-FRONT SPAR/SIDE OF BODY, TP3-R THICKNESS 1.7 2. TP3-L 2.2, TP6-L 5.9 4. TP9-L 2.0 SHEAR FITTING, FRONT SPAR CORNER WITH TOP PANEL 5. SF4-R 6.3 6. SF5-R 5.8 FSDR ABXA050333Fitting · crackedFOUND CRACKED END FITTING AFT SIDE OF PRESSURE BULKHEAD AT LONGERON 29 RIGHT. REPLACED END FITTING IAW DC9 SRM.SDR ABXA050299Doubler · corrodedDOUBLER CORRODED TOP OF WING CENTER SECTION PRESSURE DECK, STA. 683, RT BUTT LINE 10. REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8 AND REA D853-52529.SDR IXXA05RNG092SSkin · corrodedDURING INSPECTION CHECK, CORROSION FOUND ON UPPER SKIN AT OUTBOARD PYLON NR 3 RT. UPPER SKIN AT OUTBOARD PYLON NR 3 WAS REPAIRED IAW SRM 57-2-1 FIG 38 AND EWO ATI-57-057.SDR DHL2005742530Structure · corrodedCORROSION ON CENTER WING BOX APPROX 830 AT RBL 10.0. MECHANICALLY REMOVED CORROSION ON CENTER WING BOX STA 830 RBL 10 IAW B727 SRM 51-10-6. ULTRASONIC INSPECTION OF BLEND AREA IAW ASTM E797-95, HIGH READING .209" LOW READING .128" MATERIAL LOSS .082" FOUND OSDR UPS05845718Spar Cap · crackedFOUND CRACK ON CENTER WING REAR SPAR LWR CAP, INSIDE KEEL BEAM BOX RT SIDE. STOP DRILLED CRACK AT REAR SPAR IAW SK SAA 866-832589, NDT VERIFIED CRACK TERMINATES AT STOP DRILL IAW NDT SPM 06-10-01.001 REPAIRED RT WING, REAR SPAR, LWR CAP CENTER LINE AT XCW-0 ISDR QXEA200501326Bracket · loosePDX: LT TRAILING WING BOX BRACKET IS LOOSE YW 52. MAINTENANCE REMOVED AFT 2 CHERRY MAX RIVETS IAW Q400 SRM 51-42-45-330-801. DRILLED HOLES TO AN ALTERNATE FASTENER SIZE REF RD8/4-57-257. HFEC AROUND HOLES IAW 1-84-78A, PT-6, 51-00-06. NO CRACKS NOTED. INSSDR 05FDEA03047Skin · corrodedCORROSION AT CENTRAL WING UPPER SKIN SURFACE FR 46 Y- 2126. REMOVED/INSTALLED ELEMENTS PER SRM 51-40-21 & 51-40-44. REMOVED CORROSION PER SRM 51-74-10 & 51-29-00 PG. 201. PERFORMED EDDY CURRENTS FOUND "OK". PAINTED PER SRM 51-75-10-08.SDR UPS05845428Doubler · corrodedINSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX STA 960 TO 980 RBL 65 FINGER DOUBLER HAS CORROSION. REMOVED FINGER DOUBLER, REMOVED CORROSION FROM DOUBLER AND SUBFLOOR FOUND DOUBLER OUT OF LIMITS. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 51-1-21, 53-02-SDR 05FDEA02744Spar · crackedCRACK FOUND DURING UT & HFEC INSP AT WING CENTER SECTION UPPER REAR SPAR WEB BS 870 LBL 6 - 7.5. REPAIRED UPPER REAR SPAR CHORD AT BS 870, LBL 6-7.5 PER EO 7-5710-7-3325.SDR 05FDEA02449Structure · corrodedCTR WING LWR BARREL STA 1216 LONGERON 48 REWORK OF CORROSION 40 PERCENT. MATERIAL LOSS TO STANDING LEG. CUT OUT CORRODED SECTION OF LONGERON IAW SRM 53-00-01 FIG 7 VOL I GN 16.SDR 05FDEA02448Flange · corrodedCTR WING LWR BARREL AT STA 1216 REWORK TO STR 47 BASE FLANGE TO REMOVE CORROSION MATERIAL PLUS 50 PERCENT. REPAIRED LONGERON IAW SRM 53-00-01 FIG 9 VOL I.SDR 05FDEA02405Skin · corrodedUPPER CARGO COMPT FOUND CORROSION WITH EXFOLIATION ON CTR WING UPPER PANEL AT STA 1235 X=-100. ACCOMPLISH EA 1-5720-88880.SDR 05FDEA02389Structure · unknownREPAIR ASSESSMENT (EO 1-5100-7-5001) FOUND EXT DOUBLER LOCATED ON CTR WING BOX RT SIDE LOWER STA 1235. REPAIR IS IN COMPLIANCE WITH FAA FORM 8100-9.SDR UPS05845471Spar · crackedINSPECTION TYPE:C1 POSSIBLE CRACK ON LOWER SURFACE SKIN AFT CTR SPAR RT CTR AUX TANK. NDT VERIFIED 2 INCH CRACK AT RT CTR AUX TANK AFT CTR SPAR. REMOVED CRACKED SECTION OF CTR SPAR, FABRICATED REPLACEMENT SECTION OF CTR SPAR AND REPAIR PARTS, AND INSTALLED ISDR 05FDEA01868Bracket · crackedCTR WING LOWER STRUCTURE; RT BARREL STA 1277 INTERCOSTAL PRIMARY ATTACH BRACKET CRACKED. AS MARKED. ACCESS THRU CLG OR CAC. REMOVED AND REPLACED CRACKED BRACKET P/N AYB7035-12 AS PER S.R.M. 51/00/01, 51/33/01. REF.N/R N00612SDR 05FDEA01867Bracket · crackedCTR WING LOWER STRUCTURE; RT BARREL STRUCTURE STA 1237 INTERCOSTAL PRIMARY ATTACH BRACKET CRACKED THRU AS MARKED IN RED. ACCESS THRU CLG WHEEL WELL OR CAC0. REMOVED AND REPLACED CRACKED BRACKET P/N AYB7033-10 AS PER S.R.M. 51/00/01, 51/33/01, REF N/R N006SDR 2005UALA00600Skin · corrodedBS 955 CENTER WING BOX UPPER SKIN AT RBL 3 AT AFT SPAR CORRODED, SKIN SPLICE FITTING AND AFT SPAR. CORROSION CAUSED BY MOISTURE IN THE AREA. BLENDED WING SKIN, FABRICATED REPAIR SHIM BETWEEN SKIN AND FITTING, BLENDED SPAR CHORD, AND FABRICATED MODIFIED FITTSDR LR7A2009051200071Keelbeam · crackedDURING SCHEDULED B-1 CHECK PER JOB CARD HB2703, FOUND CENTER WING FRONT BEAM WEB CRACK AT FS 517, WL265, RBL20.5. REPAIRED IAW SMP 583 FIG 57-30-32.SDR ABXA050126Fitting · crackedDURING LINE MAINTENANCE, FOUND THE CENTER WING TANK FRONT SPAR LT SUPPORT FITTING CRACKED AT STA XCW 67. REPLACED FITTING IAW DC-8 SRM 51-3-0.SDR ABXA050227Shear Tie · crackedRIGHT XCW 23 STRINGER 15 - 16, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIP IAW DC-9 SRM.SDR ABXA050226Shear Tie · crackedRIGHT XCW "0" STRINGER 17 - 18, HAD CRACKED SHEAR CLIP. REMOVED AND REPLACED SHEAR CLIPS IAW DC-9 SRM.SDR 20050415Frame · crackedCARRY-THRU CRACKS, REWORKED TO B-401-5 TO MEET REQUIREMENTS OF AD 82-16-08. TOTAL TIME ON THE CARRY THRU IS UNKNOWN. WHILE PERFORMING A 100HR INSPECTION, CRACKS WERE FOUND RADIATING FROM CUT-OUT FOR UPPER WING ATTACH BOLTS ON BOTH SIDES OF CARRY-THRU. 2 LOSDR UPS05844373Finger Doubler · corrodedINSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX SUB FLOOR, FINGER DOUBLER HAS SHEAR HEAD FASTENERS AND CORROSION AT STA 960 TO 980 LBL 65. REMOVED FINGER DOUBLER AND REMOVED CORROSION ON SUB FLOOR. FOUND TO BE WITHIN LIMITS. REPLACED FINGER DOUBLER IAW SRM 51SDR ASOA05215Doubler · crackedDURING A C-CHECK IN YUL, THE DOUBLER IN THE WING BOX AT FRAME 28A LT WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IN THE WING BOX AT FRAME 28A LT IAW SRM 51-25-01. (M)SDR WRLA2005066Skin · corrodedDURING "C04" CHECK INSPECTION, FOUND CORROSION IN CENTER WING SECTION UPPER SURFACE AT S-15 STR X=47.5 TO X=-47.5.SDR ASOA05177Angle · crackedDURING A C-CHECK IN YUL, THE ANGLE IN THE WING BOX AT FS 28 RT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE ANGLE IN THE WING BOX AT FS 28 RT IAW SRM 51-25-01. (M)SDR AU510002076Vapor Barrier · out of limits(AUS) SECONDARY FUEL VAPOUR BARRIER OUT OF LIMITS IN THE FOLLOWING AREAS:- TP3-R 0.001, TP3-L 0.001, TP6-R 0.001, TP6-L 0.001, TP9-R 0.001, TP9-L 0.003, SF2-R 0.005, SF1-L 0.003, SF2-L 0.002. SF3-R 0.002, SF4-R 0.004, SF3-L 0.002, SF4-L 0.006 FOUND DURING INSPSDR RU3A0420Splice Plate · leakingCREW REPORTED SMELL OF FUEL IN AFT CABIN AT ALTITUDES OF 2500 FT AND BELOW IN LEVEL FLIGHT. IT WAS ALSO NOTICEABLE ON GROUND. IT WAS LESS NOTICEABLE AT HIGHER ALTITUDES AND UNDER PRESSURIZATION. MAINT LOCATED SOURCE OF SMELL. FWD WING CENTERLINE SPLICE PLASDR 04FDEA03059Skin · corrodedSEVERAL CORROSION ON PANEL ASSY UPPER SKIN CTR BOX WING.SDR 04FDEA03058Panel · corrodedFOR SAME DEFECT AND RECOMMENDED ACTION SEVERAL CORROSION ON PANEL ASSY UPPER SKIN CTR BOX WING.SDR 04FDEA03057Panel · corrodedDURING PASSENGER TO FREIGHT CONVERSION, FOUND STA 1179, STA 1189, 1219 AND 1229 X= -100 BEFORE INSTALL PANEL ASSY FOR CARGO MOD, FOUND MANY SEVERE CORROSION ON UPPER SKIN OF CTR BOX. REMOVED CORROSION, REMOVED FASTENERS, PERFORMED DYE CHECK RESIDUAL THICKNESSSDR SWAA043148Beam · crackedDURING SCHEDULED 1/2D CHECK, FOUND CENTER WING LONGITUDINAL BEAM CRACKED AT BS 616, LBL 45.57. REPAIRED BEAM PER SWA EA.SDR LR7A04194Spar · crackedDURING SCHEDULED B1 INSPECTION IAW JOB CARD HB5302, FOUND CENTER WING FRONT SPAR WEB CRACKED AT FS 517, CWS 20.5R, WL 273. REPAIRED IAW EA 382-53-04-088. NR 0017.SDR ABXA040340Skin · corrodedTEE CAP FS 618, LONGERON 30, HAD POPPED AND BULGING WEB SEEN FROM AFT SIDE. REPAIRED AREA IAW REA D953-50780 MR.
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