JASC 5330
Service difficulty reports · 79,347
Reports filed under 5330 · Fuselage Main, 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 = '5330' 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 = '5330' 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 SWAA2022020931304Scuff Plate · crackedAFT CARGO PIT FWD CORNER SCUFF PLATE CRACKED / RECEIVED FROM BACK SHOP ON W/O 37006-100-0001 AFT CARGO PIT FWD CORNER SCUFF PLATESDR FDEA201802101561Skin Panel · corrodedMAIN DECK APPROX STA 1370 RBL 102 SMALL AREA OF VISIBLE CORROSION DISCOVERED. REPAIRED REF EA 8-5730-T0338774 P1-P5 WING PLATES & SKINS - CTR WING - UPPER AFT SKIN PANEL AT REA SPAR - CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR.SDR IPXA2018022426837Skin · corrodedINSPECTION TYPE: 3C, CORROSION ON UPPER SKIN AT APPROX XCW 82 - 98 STRINGER 15. ACCOMPLISHED PERMANENT REPAIR IAW EA 0115730-01-A7139, REV IR AND EO MD11-5730-67528-A.SDR DALA2018021200923Skin · chafedUPPER FUSELAGE EXTERNAL SURFACE AT BS1582 TO BS1654.5 BETWEEN S-2L AND S-3L AREA FOUND CHAFING C/W ERA 565570-14.SDR CALA2018021100592Skin · chafedLEFT FUSELAGE SKIN STA2110-2120 STR2L FND CHAFING. LEFT FUSELAGE SKIN STA2110-2120 STR 2L REPAIRED AS PER SRM 53-70 -01 REPAIR 2 REV 75 AND ECRA 5330-06315.SDR CALA2018021100591Skin · chafedRIGHT FUSELAGE STA 2110-2121 STR2R FND CHAFING. CARRIED OUT REPAIR AS PER EC/RA 5330-06315.SDR DALA2018021000870Skin · dentedLOWER EXTERNAL SKIN DENTED, FRAME 69, BETWEEN STRINGERS 30L & 31L. REPAIRED IAW PRI 565255-14, REV 0-1, AND ERA 565255-14AD, REV ORIGINAL.SDR DALA2018021000829Doubler · wornDURING INSPECTION, FOUND A WORN REPAIR ON THE EXTERNAL POWER CUTOUT INNER DOUBLER, AFT EDGE. MAINTENANCE REPLACED THE DOUBLER IAW SRM 53-10-15, REPAIR 4.SDR DXTA2018020900094Skin · corrodedCORROSION ON THE AFT FUSELAGE SKIN.SDR DXTA201802090090Skin · damagedRIGHT NOSE SKIN DAMAGED.SDR SWAA2022020968222Scuff Plate · crackedAFT CORNER SCUFF PLATE IN AFT CARGO COMPARTMENT CRACKED . / REPAIRED BY VENDOR AIRCRAFT DUCTING REPAIR INC ON 15FEB18 UNDER RO# 7530220-AHR. SCUFF PLATE TO BE REINSTALLED ON TASKCARD 753-140-00-02Y.SDR SWAA2022020972948Scuff Plate · crackedUPON RE-INSPECTION OF FORWARD CARGO DOOR CENTER SCUFF PLATE SPEED TAPE CONDITION; FOUND CENTER SCUFF PLATE CREASED FROM IMPACT DAMAGED AND MULTIPLE CRACKS ON FORWARD EDGE OF CENTER SCUFF PLATE / REMOVED AND REPLACED FWD CARGO SCUFF PLATE. REF AMM 53-11-02.SDR SWAA2019072935308Skin · dentedFUSELAGE SKIN DENTED AT BS. 360, 3" BELOW STR. 25R. REPAIRED SKIN PER EA.SDR SIMA2018091108006Skin · corrodedSURFACE CORROSION FOUND ON SKIN JOINT STRAP AT FRAME 13 BETWEEN STRINGERS 21L AND 21R. SKIN STRAP AT FR 13 BLENDED IAW SRM 51-10-05 REF FCBS 53-10-14-001 BLEND DIMENSION L 2.800 X W 2500" X D 0.004 IS OUT OF LIMITS IAW SRM 51-10-05 AT FRAME 13 BETWEEN STRINGERSDR SCNA20180208056Skin · damagedINVESTIGATE MATERIAL LOSS COMMON TO FASTENER HEADS ON LT & RT FLIGHT DECK CROWN SKIN DUE TO PRIOR NR ON FLIGHT DECK LT AND RT UPPER SKIN PANELS. NDT MAPPED 5" X .5" GRID OF MATERIAL REMAINING DIMENSIONS AND SUBMITTED. REPLACEMENT OF SKIN PANELS ACCOMPLISHED. FSDR SCNA20180208037Nut Plate · defectiveBAD NUTPLATE UNDER PANEL 194HR, BELLY SKIN RIGHT SIDE AFT OF WHEEL WELL, FLAGGED. REMOVED AND REPLACED NUTPLATE UNDER PNL 194HR, BELLY SKIN RIGHT SIDE AFT OF WHEEL WELL.SDR ABXR2018020800027Doubler · corrodedANTENNA DOUBLER IS CORRODED ON THE INTERIOR SURFACE LOCATED BTW STA 390 AND STA 412 BTW STR 39L AND STR 39R.SDR ABXR2018020800025Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED (VERIFIED WITH EDDY CURRENT)AT LOWER AFT CORNER OF R-1 DOOR CUTOUT.SDR FDEA201802080324Skin · crackedFUSELAGE SKIN BS 535 AT UPPER AFT CORNER OF THE NR 3 PACK DOOR CUT OUT, HAS A .600 INCH CRACK PROPAGATING THROUGH FASTENER HOLE. REPAIRED IAW SRM 53-50-00, FIG 3A.SDR SWAA2022020991360Scuff Plate · crackedFSD THRESHOLD IS CRACKED AT FWD CORNER / REPAIRED FSD THRESHOLD FWD CORNER IAW EA #1-A53-2076 REV II.SDR ASOA201802077007Skin · dentedTYS A/C IS IN A C-CHECK STATUS WHEN INSPECTION FOUND FUSELAGE DENTED BETWEEN FRAME 20-21 STR-11L AND 12L. MAINTENANCE REPAIRED AREA IAW ETD 2018-002931. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ASOA201802077005Skin · dentedTYS A/C WAS IN A-CHECK STATUS WHEN INSPECTION FOUND A DENT AT FR. 7 BELOW LT WIPER. MAINTENANCE REPAIRED THE DENT IAW ETD 2018-002936. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR ABXR201802070004Bear Strap · corrodedLEFT FWD OVERWING EXIT CUTOUT, FWD LOWER CORNER CORRODED.SDR SWAA2022020957438Scuff Plate · crackedAFT CARGO THRESHOLD CRACKED IN THE RADIUS 2.5 INCHES LONG. CRACK IS LOCATED 2 INCHES FORM FORWARD EDGE / B) INSPECTION COULD NOT BE ACCOMPLISHED. REPAIR CONFIGURATION/CONDITION HAS CHANGED; HOWEVER; AIRCRAFT IS OKAY FOR SERVICE. REQUIRES BOTH AN AMT/INSPECTIONSDR SWAA2022020969487Scuff Plate · crackedAFT CARGO COMPARTMENT AFT CORNER SCUFF PLATE CRACKED / REPAIRED PER # 1-A53-2076 REV 11 AFT CARGO CPMPARTMENT AFT CORNER SCUFF PLATE.SDR SWAA2022020985300Scuff Plate · crackedFOUND CRACK INDICATION AT DENT DEFECT DOCUMENTED ON ORDER # W2591818 'AFT CARGO DOOR CENTER SCUFF PLATE' USING HFEC PART 6; 51-00-00 PROC. #3 / REMOVED AND REPLACED AFT CARGO DOOR CENTER SCUFF PLATE IAW AMM 53-11-02 REF SA-M 326 A1132970SDR SWAA2022020991315Scuff Plate · corrodedACB; FWD. SCUFF PLATE (NET ATTACH POINT) BS 794; RBL 20; CORRODED. / REPLACED ACB; FWD SCUFF PLATE BS 794; RBL 20. NEW SCUFF PLATE SWABFG #453A2611-1; PO # 671199/1; IAW 737 AIPC 25-52-10-02; REV 81. PART TO BE INSTALLED ON CUSTOMER CARD NUMBER: JPANEL-141-CLOSDR SWAA2022020991316Scuff Plate · corrodedACB; AFT. SCUFF PLATE (NET ATTACH POINT) BS 847; RBL 20; CORRODED. / REPLACED ACB; AFT. SCUFF PLATE BS847; RBL 20 IAW 737 AIPC 25-52-01-02 REV. 81. NEW PART SWACFE7251465 PO # 671751/1 TO BE INSTALLED ON CUSTOMER CARD NUMBER: JPANEL-141-CLOSE.SDR SWAA2018031220321Skin · crackedR1 DOOR CUTOUT INTERNAL SKIN, 2 INCH CRACKED AT BS 293, STRINGER 9R FORWARD UPPER LATCH FITTING. REPAIRED THE SKIN IAW EA.SDR RAIA201802060001Skin · crackedFUSELAGE SKIN HAS CRACKS AT FRAME 78 BETWEEN STRINGERS 6L - 8L. CUTOUT THE DAMAGE AND INSTALLED A DOUBLER.SDR DALA2018020800786Skin · dentedDURING C CHECK IN MSP, A FOLLOW UP INSPECTION OF A PREVIOUS GOUGE BLENDOUT ON THE FUSELAGE SKIN, PER LP 8758397, WAS SCHEDULED. THE ORIGINAL WRITE UP WAS DATED 28APR16 AND THE INTERNAL AND EXTERNAL HFEC INSPECTION WAS DEFERRED PER SRM 53-21-11DIAGRAM 102. THE SDR SWAA2022020933575Skin · crackedTRANSFERRED FROM L/P 0018015E. FOUND 2 CRACKS 3/4' LONG THROUGH FASTENERS ON ELECT. GRND PWR RECEPTICLE SURROUND DOUBLER. / AS PER EA 53EA-04756 TRIMMED OUT DAMMAGE PER SRM 53-10-15 (62334) FABRCATED TRIM FILLER + DOUBLER PER SRM 53-10-15 (62334) INSTALLED DOUSDR SWAA2022020952742Scuff Plate · crackedFORWARD CARGO FORWARD SCUFF PLATE IS CRACKED. / REPAIRED PER R.O. 7530028-AKR.SDR SWAA2022020969476Scuff Plate · crackedFWD CARGO COMPARTMENT FWD LOWER CORNER THRESHOLD SCUFF PLATE CRACKED / FWD CARGO FWD LOWER CORNER OF SCUFF PLATE CRACKED ; REPAIRED CRACKED SCUFF PLATE ON E.A 1-A53-2072 REV 11.SDR ASAA2018020525041Skin · scratchedSCRATCH ON FUSELAGE SKIN BETWEEN STA 500C AND 500D BETWEEN STRINGERS 25L AND 26L. GROUNDED - YES. REPAIRED PER SRM 53-00-01 2R3. REINSPECT PER PARA (5) INSPECTION THRESHOLD OF 50,000 FLIGHT CYCLES PER TABLE 203.SDR SWAA2022020969427Support Angle · corrodedLEFT HAND; L1 DOOR SILL PLATE; SUPPORT STRUCTURE HAS MULTIPLE AREAS OF CORROSION / BLENDED OUT CORROSION AT L1 DOOR SILL PLATE SUPPORT ANGLE IAW B737 SRM 51-10-02. ORIGINAL THICKNESS 0080'; MATERIAL LOSS 0.020'. THE MATEIRAL REMAINING 0.060'; THE AREA FOUND TOSDR IPXA2018022126729Skin · dentedINSPECTION TYPE: C4, SKIN DENTED BS 451, STRINGER 25 - 26R. REPAIRED IAW SRID 3-4105366013 AND EO B767-5330-67377-A.SDR YENA201802040064Skin · crackedDURING HEAVY MAINTENANCE, A CRACK WAS FOUND IN THE EXTERNAL SKIN ON THE LOWER FUSELAGE. REPAIRED THE SKIN IAW EA 57-0004-18, AND EC E18-043-01.SDR SWIA2018031344403Skin · chafedEXTERNAL SKIN HAS CHAFE DAMAGE FWD OF BS 559+96 BELOW AFT LAV FILLER, STRINGER 22R. REPAIRED THE SKIN IAW REO.SDR SWAA2018030520193Skin · corrodedFUSELAGE SKIN CORRODED AROUND VACUUM WASTE EXHAUST HOLE. REPAIRED THE SKIN IAW ER AND EA.SDR SWIA2018022144314Skin · dentedFUSELAGE SKIN HAS A DENT JUST FWD OF BS 250 BETWEEN STRINGERS 23 AND 24L. REPAIRED IAW REO.SDR SWAA2018020719531Skin · crackedEXTERNAL POWER CUTOUT LOWER CENTER EDGE CRACKED AT LOWER LATCH PAD. REPAIRED CUTOUT IAW EA.SDR CALA2018020300463Skin · corrodedUPPER FUSELAGE SKIN HAS CORROSION AT APPX B STA 1787 BETWEEN S4R AND S6R JUST FWD OF APU INLET DOOR AS MARKED 034-001 B757-53-3-6 042. REMOVED APU INLET DOOR, REPLACED SURROUNDING SKIN STRAP. REINSTALLED APU INLET DOOR IAW SUA 49-15-08-004-001, SRM 51-40-02, ASDR WVER2018020307Skin · dentedFUSELAGE IS DENTED BETWEEN FS 193-FS 202.75 STR 5R-6R. REPLACE FUSELAGE SKIN IAW SRM.SDR DALA2018020200695Skin · damagedFOUND SKIN DAMAGE APPROXIMATELY TWO FEET AFT OF THE DOOR AT FLOOR LINE. REPAIRED IAW SRM 53-00-01, REPAIR 36.SDR CALA2018020200417Skin · corrodedFUSELAGE EXTERNAL SURFACE AROUND VOR CABLE (4RSB) AT CONNECTION TO FIN 7102VC IS CORRODED. ACCOMPLISHED ALL STEPS OF ECRA 5341-01113.SDR CALA2018020200415Skin · corrodedFUSELAGE EXTERNAL SURFACE AROUND VOR HARNESS (4RSA) CONNECTION AT FIN 7113VC IS CORRODED. ACCOMPLISHED ECRA 5341-01113.SDR DALA2018020200651Doubler · corroded(AIRCRAFT 3758, L/P 0407716) AWR HIDDEN CORROSION: AFTER MAKE ACCESS WAS FOUND CORROSION ON DOUBLER OF PRODUCTION STA= 747 TO 767 BTW STGR 27R TO 27L AT AFTER CARGO COMPARTMENT ON REFERENCE OF JOB FOLLOW-UP NRC
00027. CORROSION LEVEL II.- PRODUCTION DOUBLER/ SDR SWAA2022020811754Scuff Plate · crackedFWD CARGO BAY; FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY FWD FWD CORNER SCUFF PLATE IAW EA #1A53-2076 REV11SDR SWAA2022020828926Scuff Plate · crackedFWD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FWD CARGO BAY FWD CORNER SCUFF PPLATE IAW SWA EA 1-A53-2076 REV 11
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