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 SWAA2022021760497Web · crackedNOTED CRACK COMMON TO THE L/H SPAR VERTICAL PRESSURE WEB STA.663 WL. 200 LBL 29 / REPAIRED PER EA 1-757-15464 REV. IR AND ER 18-03794 REV. IR.SDR SWAA2022021029002Web · crackedTRANSFERRED FROM LOG PAGE 0600962: TRANSFERRED FROM NON ROUTINE NUMBER T750454 'PREVIOUS REPAIR CRACK FOUND ON VERTICAL PRESSURE WEB LEFT SIDE. SEE PREVIOUS OPERATOR REPAIR RECORD NUMBER (WI02.A) EO 3757033 AND SWA EA 1-751-0901 PART 1 / REMOVED DAMAGED PART OSDR SWAA2022021029003Web · crackedTRANSFERRED FROM LOG PAGE 0600963: TRANSFERRED FROM NON ROUTINE NUMBER T750455 'PREVIOUS REPAIR CRACK OF 0.875 ON VERTICAL PRESSURE WEB BTW RBL 40.0 & 45.64. SEE PREVIOUS OPERATOR REPAIR RECORD NUMBER (WI02.B) EO 3757033 AND SWA EA 1-751-0901 PART 1 / REMOVED SDR SWAA2022020967971Web · crackedINTERIOR SIDE WELL SPAR VERTICAL PRESSURE WEB AT STA.663 RBL 41 (4 INCHES DOWN FROM TOP OF PRESSURE DECK 1/2 INCH CRACK INDICATION PER NDT MANUAL PART 6 51-00-00 PROCEDURE 23. (MARKED) / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR SWAA2022020923030Fitting · out of toleranceCTR TANK UPR SURFACE AT RBL 15.04 SHEAR FITTING LOCATION; AFT FASTENER HOLE ENTERANCE IS OUT OF ROUND / REPAIRED CTR TANK UPPER SURFACE AT RBL 15.04 SHEAR FITTING LOCATION; AFT FASTENER HOLE IAW SRM 51-40-05; SRM 51-40-08; ATS ER 18-01670 REV IR; DATED 07MAR18SDR SWAA2022020220303Spar · damagedUNABLE TO COMPLETE CCN:14030-57 STEPS 2.D THROUGH 2.F AS AREAS HAVE NOT BEEN PROPERLY PREPARED FOR INSPECTION. INSPECTIONS AREAS LISTED IN STEP 2.D REQUIRE CLEANING AND REMOVAL OF VAPOR BARRIER TO FACILITATE INSPECTION. FASTENER HOLES LISTED IN STEPS 2.E AND FSDR DALA2017071405412Structure · crackedHFEC INSPECTION OF RIGHT SIDE CENTER WING SHOWS A CRACK INDICATIONON AFT ROW OF S-17 AT 7TH FASTENER OUTBOARD IN SCAN AREA. CRACK EXTENDS APPROX. 1/4" INBOARD OF FASTENER HEAD. REMOVED FASTENER AT CRACK INDICATION. REPAIRED PER PRI560178-14 REV 0-6 252477 PRI SDR SWAA2022012539835Web · crackedWHILE PERFORMING HFEC ON CUSTOMER CARD 753-200-00-02 FOUND CRACK ON LEFT HAND BL 42 AT BS 663 VERTICAL WEB APPROX. WL 198 / ACCOMPLISHED REPAIR OF CRACK AT APPROX. LBL 42; BS 663; VERTICAL WEB WL 198 IAW SRM 57-10-10-2R-3 REAPIR 3 ALT. 2SDR HYTA20150908001Structure · crackedCRACKS FOUND IN UPPER TUBE OF CARRY THRU ASSEMBLY, PN 391-030-401-30, AT LOW POINT OF THE TWO CUT OUTS WHICH ARE MILLED IN THE TUBE TO ALLOW INSTALLATION OF WING ATTACH BOLT. THE MILLING PROCESS LEFT A SHARP EDGE THAT CREATED A STRESS RISER. THIS IS A CRITICSDR HYTA20150904001Structure · crackedCRACKS FOUND IN CARRY THRU ASSEMBLY AT LOW POINT OF MILLED CUT OUTS IN UPPER TUBE OF ASSEMBLY. THE MILLING PROCESS LEFT A SHARP EDGE CREATING A STRESS RISER. THIS WAS A FACTOR CONTRIBUTING TO CRACKS DEVELOPING. WE HAVE DRESSED OUR OTHER CARRY THRU ASSEMBLIESDR SWAA2015031237391Angle · corrodedZ ANGLE CHANNEL UPPER SURFACE CORRODED BETWEEN BS 727C+8 - 827+2, LBL 22. R & R Z ANGLE IAW SRM.SDR CALA2014032490694Structure · corrodedCORROSION FOUND UPPER WING BOX AREA STATION 950 LBL 87. BLENDED CORROSION & RESTORED SURFACE IAW ECRA 5714-01031.SDR FDEA201402270416Panel · crackedCENTER WING BOX REAR SPAR & BOTTOM PANEL FOUND CRACKED. REAMED CRACK LAYERS IAW SRM 51-40-44 . PERFORMED ROTO-TEST INSPECTION IAW NTM 51-10-01. NO CRACK FOUND. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201402270415Panel · crackedCENTER WING BOX REAR SPAR & BOTTOM PANEL FOUND CRACKED. REAMED IAW SRM 51-40-44 . PERFORMED ROTO-TEST INSPECTION IAW NTM 51-10-01. NO CRACK FOUND. MAJOR REPAIR IAW IAW GMM6-2-100.SDR FDEA201402270414Panel · crackedCENTER WING BOX REAR SPAR & BOTTOM PANEL FOUND CRACKED. REAMED LAYERS IAW SRM 51-40-44 . PERFORMED ROTO-TEST INSPECTION IAW NTM 51-10-01. NO CRACK FOUND. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201402270413Panel · crackedFUSELAGE CENTER WING BOX REAR SPAR & BOTTOM PANEL FOUND A CRACK SIGNAL. REAMED THE CRACK LAYERS OF HOLE BY 0.4MM STEP BY STEP UNTIL CRACK REMOVAL IAW SRM 51-40-44 . PERFORMED ROTO-TEST INSPECTION PER NTM 51-10-01. NO CRACK FOUND. MAJOR REPAIR IAW GMM6-2-1SDR FDEA201402270412Panel · crackedFUSELAGE CENTER WING BOX REAR SPAR & BOTTOM PANEL HAS A CRACK SIGNAL. REAMED THE CRACK LAYERS OF HOLE BY 0.4MM STEP BY STEP UNTIL CRACK REMOVAL IAW SRM 51-40-44 . PERFORMED ROTO-TEST INSPECTION IAW NTM 51-10-01. NO CRACK FOUND. MAJOR REPAIR IAW GMM 6-2-100SDR FDEA201402270411Panel · crackedRIGHT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE INTERNAL FITTING ONLY STEP BY STEP 0.4 MM PER SRM 51-40-44 AND COMPLIED WITH EA 6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201402270410Panel · crackedLEFT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE CRACKED LAYERS FROM INTERNAL TO EXTERNAL PER SRM 51-40-44 AND COMPLIED WITH EA 6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201402270409Panel · crackedLEFT WING CENTER WING BOX REAR SPAR & BOTTOM PANEL WITH A CRACK SIGNAL. REAMED THE PICK-UP ANGLE AND LOWER KEEL BEAM ONLY STEP BY STEP 0.4MM PER SRM 51-40-44 AND COMPLIED WITH EA 6-5710-T0306021 P1. MAJOR REPAIR IAW GMM6-2-100.SDR FDEA201402270408Structure · crackedCENTER WING BOX REAR SPAR & BOTTOM PANEL CRACKED. REPAIRED IAW EA6-5710-T0306021 PT1. MAJOR REPAIR IAW GMM6-2-100.SDR DALA2016102608025Structure · corrodedCORROSION ON UPPER SURFACE OF CENTER WING BOX LOC AT LEVEL FR 42 AND BTW -Y1732 TO -Y 1292 PAX CABIN MEASURE L=1.500" W=1" D=0.002" APPROX. REPAIR ON UPPER SURFACE OF CENTER WING BOX LOCATED AT LEVEL FR41 TO FR42 BTW Y-1292 TO Y-1732 AND RIB 1 PAX CABIN PER ESDR FDEA201401260197Structure · crackedCENTER WING JOINT AT FRAME 40 LT SIDE FOUND CRACKED. REPAIRED IAW EA 6-5710-T0305842.SDR FDEA201311202830Doubler · crackedCRACKS WERE FOUND ON HOLE NR 1 & NR 2 AT CTR WING BOX FRAME 44 BEAM RT CUTOUT DOUBLER Y212. REMOVED THE CRACK, INSTALLED THE BUSHING FOR HOLE NR 1, COMPLETED WITH EA6-5710-T0303307.SDR AALA20131002004Structure · corrodedCORROSION DISCOVERED ON CENTER WING BOX LOWER SKIN AT STATION 540.5 & STRINGER 21 & 22 RT. ACCOMPLISHED CORROSION REMOVAL IAW SRM 51-10-02 & REPAIRED IAW EA B737-57-031846.SDR AALA20131002003Structure · corrodedCORROSION ON CENTER WING BOX LOWER SKIN FWD SECTION LT SIDE, STRINGERS 21 TO 22 LT & STATION 540.5. ACCOMPLISHED CORROSION REMOVAL IAW SRM 51-10-02 & REPAIR IAW EA B737-57-031846.SDR IPXA3M79085Skin · corrodedINSPECTION TYPE:2C, MAIN CABIN SUBFLOOR CENTER WING UPPER SKIN CORRODED ABOVE STR16, LBL 102. REPAIRED CENTER WING SKIN AT LBL 102 ABOVE STR16 IAW STASA EA 011-5730 -01-A4712 REV IR AND EO MD11-5730-51179-A. (MINOR)SDR IPXA3M79084Skin · corrodedINSPECTION TYPE:2C, CENTER WING UPPER SURFACE CORRODED ABOVE STR 16 AT RBL 103 MAIN CABIN SUBFLOOR. REPAIRED WING EXTERIOR SKIN AT RBL 103, STR 16 IAW STASA EA 011-5730-01 -A4712, REV IR AND EO MD11-5730-51179-A. (MINOR)SDR IPXA3M79042Skin · corrodedINSPECTION TYPE:2C, CENTER WING UPPER SKIN CORRODED IN MAIN CABIN SUBFLOOR OVER S15 AT RBL103. REPAIRED CORROSION ON CENTER WING UUPER SKIN PANEL IAW STASA EA 011- 5730-01-A4712 REV IR AND EO MD11-5730-51179-A. (MINOR)SDR SWAA2013041514852Support · crackedCENTER WING VERTICAL SUPPORT CRACKED AT BS 737, RBL 44. REMOVED AND REPLACED SUPPORT IAW SRM.SDR SWAA2013041214783Support · crackedCENTER WING AT BS 737 LBL 44 VERTICAL SUPPORT CRACKED BELOW SEAT TRACK. REMOVED & REPLACED SUPPORT IAW SRM.SDR SWAA2013030813493Stiffener · crackedWING CENTER SECTION FRONT SPAR, VERTICAL STIFFENER UNDER RBL 24 CRACKED AT STA 661. REMOVED AND REPLACED STIFFENER PER SRM.SDR ASOA2013032103247Skin · corrodedCENTER WING TANK CUTOUT, 510BB, HAS AREAS OF CORROSION ON OTBD EDGE. REPAIRED IAW REO 601R-57-21-030 AND SRM 51-21-06.SDR UALA2013022501107Web · corrodedLEFT MAIN WHEEL WELL, REAR SPAR WEB CORRODED AT BS 955, LBL 78. REPAIRED THE BS 955 LT SIDE CTR WING SECTION REAR SPAR BULKHEAD WEB & MODIFICATION OF FAILSAFE STRAP IAW REO-G15835, AND ECRA 5340-01497.SDR SWAA2013021112582Vapor Barrier · crackedCENTER WING REAR SPAR VAPOR BARRIER MATERIAL HAS DIAGONAL CRACK APPROX 6 INCHES LONG, LOCATED LOWER SPAR APPROX RBL 31 - RBL 35. CRACK APPEARS TO TERMINATE AT FASTENER HOLES ON BOTH ENDS. INSTALLED FIBERGLASS PATCH OVER DAMAGED AREA.SDR DALA13003089238Skin · corrodedDURING HMV, CORROSION WAS FOUND ON THE RT WING CENTER SECTION UPPER WING SKIN AT STA 954 AND BL 0. SUBSEQUENTLY, THE CORROSION WAS R & R IAW ER/A 504829-14. ACCOMPLISHED SECTION 1 OF REPAIR IAW ER/A 504829-14, REV O. REMOVED CORROSION FROM CENTER TANK, RBL SDR SWAA2013012812013Angle · crackedWING CENTER SECTION FRONT SPAR AT FS 660, RBL 24.5 CRACKED ANGLE. REMOVED AND REPLACED ANGLE IAW SRM.SDR QXEA2012121201679Structure · corrodedUPPER CENTER WING DRY BAY PANEL LANDING FOR PANEL 521AT HAS AREAS OF CORROSION. BLENDED AND REMOVED CORROSION REF RD 8/4-57-441. MIN REMAINING THICKNESS .167, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. PANEL LSDR QXEA2012121001639Panel · corrodedUPPER CENTER WING DRY BAY PANEL LANDING FOR PANEL 521BT HAS AREAS OF BARE METAL AND CORROSION. REMOVED CORROSION IAW RD 8/4-57-441 AND RD 8/4-57-879. REMOVED GANG CHANNELS FOM IAW RD 8/4-57-879. CONFIRMED AFFECTED AREAS CRACK FREE REF NTM 51-00-06-910-801 PT SDR QXEA2012120801662Structure · corrodedUPPER CENTER WING DRY PANEL LANDING FOR PANEL 621BT HAS AREAS OF BARE METAL AND CORROSION. REMOVED CORROSION REF RD 8/4-57-441. REAMED 22 HOLES REF RD 8/4-57-879. COUNTERSUNK HOLES REF RD 8/4-57-441 AND 8/4-57-879. ALODINED REPAIR IAW RD 8/4-57-441. FILLED SDR QXEA2012110801662Structure · corrodedUPPER CENTER WING DRY PANEL LANDING FOR PANEL 621BT HAS AREAS OF BARE METAL AND CORROSION. REMOVED CORROSION REF RD 8/4-57-441. REAMED 22 HOLES REF RD 8/4-57-879. COUNTERSUNK HOLES REF RD 8/4-57-441 AND 8/4-57-879. ALODINED REPAIR IAW RD 8/4-57-441. FILLEDSDR FDEA201210243735Spar · crackedONE CRACK WAS FOUND AT FASTENER HOLE "F" OF LT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.SDR FDEA201210243734Spar · crackedONE CRACK WAS FOUND AT FASTENER HOLE "F" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.SDR FDEA201210243733Spar · crackedONE CRACK WAS FOUND AT FASTENER HOLE "C" OF RT CENTER WING BOX OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163148.SDR FDEA201210173655Web · corrodedLEFT WING CENTER TANK FUEL QTY HARNESS FEED THRU JUST OTBD OF WBL 79.50 ON L/E SPAR CORRODED. COMPLIED WITH EA F-5710-162408 (WING-SPAR WEB CORROSION AT FUEL GAUGE CONNECTOR). CAT "A" REPAIR REF: FAA FORM 8100-9. CORROSION WAS DETERMINED TO BE OUT OF LIMITS SDR USAA2012101500011Stiffener · crackedC2 CHECK - CRACK ON WING CENTER SECTION VERTICAL STIFFENER AT BS 663.15, WL 170.4, RBL 6.15. WING CENTER SECTION VERTICAL STIFFENER AT BS 663.15, WL 170.4, RBL 6.15 IAW EO 5704V245 & EA 104233.SDR FDEA201207112536Spar · damagedCENTER WING BOX REAR SPAR & BOTTOM PANEL DAMAGED, BUSHING REPAIRED IAW EA 6-5710-161497.SDR QXEA2012062300507Skin · corrodedCENTER WING SKIN UPPER DRY BAY LANDING FOR PANEL 621BT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-441. CONFIRMED BLENDED AREA CRACK FREE REF NTM 51-00-06-910-801. PERFORMED UT THICKNESS IAW NTM 51-00-04-910-801, PT 1. FOUND BLENDING WITHIN LISDR QXEA2012062100506Panel · corrodedCENTER WING UPPER DRY BAY PANEL 521AT HAS AREAS OF CORROSION ON MATING SURFACE. REMOVED CORROSION AND BLENDED DAMAGE IAW RD 8/4-57-425, STEP 1. EVALUATED AND FOUND OUT OF LIMITS. CONFIRMED BLENDS CRACK FREE REF NTM 51-00-06-910-801. FOUND TO BE WITHIN LIMITSSDR SPUY20120620005Skin · corrodedCENTER SECTION LOWER SKIN SHOWS CORROSION STA 804-5 - STA 825.95, LBL25.
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