JASC 5330
Service difficulty reports · 79,329
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 DALA2023113009824Unknown · unknownSHIP 192 FOUND RH THS LOWER CUTOUT SKIN DOUBLE PLATE CRACK. CORRECTIVE ACTION: THE REPAIR SKIN FABRICATED AND INSTALLED AS PER B767-300 SRM53-80-01-2R PROCEDURE 3 REPAIR 3. REV.121.00-APR-25-2023. AND PRI:613800-14 REV.O. B767-300 SRM53-80-01 (0077887)SDR SWAA2023112724566Doubler · crackedGPU DOOR LOWER SURROUND DOUBLER CRACK.<[01] CUT OUT DAMAGE; FAB; DRILLED UP DOUBLER AND FILLER PER SRM 53-10-15-2R-4;[02] ACCOMPLISHED HFEC OF CUT OUT AREA PER NDT PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS FOUND.;[03] INSTALLED REPAIR PARTS PER SRM 53-10-15-2RSDR SWIA2024012200055Skin · dentedMULTIPLE DENTS, NICKS AND GOUGES ON AFT FUSELAGE FROM FS1000 TO FS1051, BETWEEN STRINGERS 21R-27 (C-CHECK RO 1/19/2024) REMOVED DAMAGED AREAS ON FUSELAGE SKIN BETWEEN FS1000 - FS1051, STGR21R - STGR27 REF CRJ700 SRM 51-12-00-001-001-A01. FOUND TO BE OUT OFSDR CALA2023120603569Skin · crackedSUPPORT TASK - EA5310-06900 REV.D OP 014 STEP 21.3, 1EA CRACK WAS FOUND APPROX 0.125" IN LENGTH AT FUSELAGE SKIN SURFACE AT 2 O''CLOCK POSITION. TRANSFER REF.NON-ROUTINE HX NRC WO.2405692 AND . REVISION OF ECRA 5331-03067 PART 2 ON OR BEFORE REACHING 22,165 4,SDR JJBA20231128032Unknown · unknownCRACKS SUSPECTED (3X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 & BTW STR 3R-9R. AFTER NDT INVESTIGATION, 1 CRACK FOUND, SKIN REPAIRED WITH 1 BUSHINGSDR JR2R20231122177Skin · puncturedFUSELAGE SKIN DAMAGE AT FR24 BETWEEN STR23L AND STR24LSDR SWAA2024010423643Angle · crackedCRACK ANGLE LOCATED BS500H AT LEVEL STR26L AT FWD CARGO COMPARTMENT 2023-719798<[01] REPLACED ANGLE LOCATED BS500H AT LEVEL STR26L AT FWD CARGO COMPARTMENT IAW B737-800 SRM 51-10-02 ITEM 9 AND DWG: 143A7505 SHEET: 108 REV: -<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOSDR DALA2023112809791Unknown · unknownSHIP 685 DENT FOUND ON ARRIVAL APROX 6FT FWD OF L2 DOOR ON STRINGER #16 5 '' AFT OF STATION 620. CORRECTIVE ACTION: REF ERA 613885-14 AND 613956-14. (5563658)SDR DALA2023112809747Unknown · unknownSHIP 1810 AFT FUSELAGE, BETWEEN STA 1540 + 13" AND STGRS 23L AND 24L, SKIN WITH CORROSION. CORRECTIVE ACTION: CORROSION WAS FOUND ON AFT FUSELAGE, SKIN BETWEEN STA 1540+13" AND STGRS 24L AND 25L AND WAS BLENDED IAW B767-400 SRM 51-10-02- 0G REV 68.00 MAY-16-20SDR IPXA2023112388846Skin · punctured*SUPPLEMENTAL SDR* *MAJOR REPAIR* LOAD REPORTS DAMAGE TO AIRCRAFT STRUCTURE FWD OF LOWER FWD CARGO PIT. C/W EO-88772-REQ1SDR DALA2023112209649Unknown · unknownCRACK AT STA 1086.5 AND LONGERON 13RH APROX ON EXTERIOR FUSELAGE. SUMMARY OF NRC 00014: CRACK AT STA 1086.5 AND LONGERON 13RH APROX WAS REPAIRED PER PRI 613146-14 REV 2 AND ER/A 613146-14 REV ORIGINAL, SECTION I. PERMANENT REPAIR.ACCOMPLISH SECTION II. REPETITSDR DALA2023112209630Unknown · unknownSHIP 3119 DENT INTERNAL STRUCTURE DOOR AT LOWER FORWARD CORNER IN AFT CARGO COMP ARTMENT. CORRECTIVE ACTION: REPAIRED PER ER/A 613185-14. (0076074)SDR IPXA2023112188846Unknown · unknownLOAD REPORTS DAMAGE TO AIRCRAFT STRUCTURE FWD OF LOWER FWD CARGO PIT.SDR DALA2023112109626Unknown · unknownSHIP 3303 FWD CARGO FWD SKIN AND FRAME C20A DAMAGED BY K LOADER. CORRECTIVE ACTION: C/W ALL STEP OF PRI 613875-14, ER/A 6613875-14. (0073513)SDR DALA2023112009529Unknown · unknownCRACKS (2 EA) ON EXTERNAL FUSELAGE SKIN ON PREVIOUS REPAIR AREA, BTW STA 503-522 AND BTW LONG 27RH AND 29RH. SUMMARY OF NRC 00505: EXTERNAL FUSELAGE SKIN BTW STA 503-522 AND BTW LONG 27RH AND 29RH WAS REPAIRED PER B717-200 SRM 53-03-01-2R FIGURE 205 SHEET 1, 5SDR YENA2023112201449Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: MULTIPLE DENTS ON FWD FUSELAGE LOWER SKIN BTW FR 17/23 AND STGR 25R/25L; (RESOLVED ON W/O: 1269682 TASKCARD: NR-00011 ) REF TOMX WO 2384 NR 00001 MULTIPLE DENTS ON FWD FUSELAGE LOWER SKIN BTW FR 17/23 AND STGR 25R/SDR VNAA202401050021Skin · scratchedSEVERAL SCRATCHES ON EXTERNAL FUSELAGE SKIN BELOW VENTRAL FIN FAIRINGS COVER LH AT REAR FUSELAGE. SCRATCHES ON EXTERNAL FUSELAGE SKIN BELOW VENTRAL FIN FAIRINGS COVER LH AT REAR FUSELAGE WERE BLENDED OUT PER CRJ900 SRM 51-12-00-001-A01 AND EVALUATED WITHIN LISDR CALA2023121503647Skin · damagedMISSED DRILLED FASTENER HOLE FOUND IN FUSELAGE SKIN PANEL 146A3201-38 UPON REMOVAL OF PREVIOUS FUSELAGE SKIN REPAIR AT LAV. SERVICE PANEL AT INTERSECTION OF FRAME BS-847 AND STRINGER SR-23L ACCOMPLISHED HFEC INSPECTION OF CUTOUT/REAMED AREA OF MIS-DRILLE D FASSDR HNAA2023122800498Unknown · unknown53-2021 CRACKS ON FUSELAGE SKIN AT FR78-80, STR4-9R. REPAIRED IAW EO1-53-23-0432SDR HNAA2023122800497Unknown · unknown53-2020 CRACKS ON FUSELAGE SKIN AT FR77-79, STR5-9L. REPAIRED IAW EO1-53-23-0432SDR SWIA202312071117Unknown · damagedBLENDED AREAS OF LH FWD FUSELAGE SKIN BETWEEN FR10 - FR11 AND STGR 17L - STR18L REQUIRE PERMANENT REPAIR IN REF TO SRM 53-10-01/REPAIR 12P. (FILED CLOSED)REPAIRED DAMAGED AREAS OF LH FWD FUSELAGE SKIN BETWEEN FR10 - FR11 AND STGR 17L - STR18L IN REF TO SRM 53-SDR GTIA2023112137624Skin · corrodedCORROSION FOUND ON R1 LOWER DOOR SKIN AT FR 18 STR 23R MEASURING 1.6" W 0.023" D. RAF-01 CREATED. SDR SUBMITTED-ACCOMPLISHED PERMANENT REPAIR REF HAECO SO 122182 EA 5311-2385 AND OPS 38399SDR DALA2023112009520Unknown · unknownCRACK ON UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLIDING WINDOW CUTOUT IN REF TO NRC 00651. SUMMARY OF NRC 00663: UPPER AFT CORNER OF FUSSELAGE SKIN AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. (LP #0069478)SDR AALA202311209057Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXISTING SKIN REPAIR DOUBLER AT STA 2000, S10L. REPAIRED SKIN PER SRM 53-00-01-2R-3.SDR DALA2023112809748Unknown · unknownSHIP 1810 AFT FUSELAGE, BETWEEN STA 1562+ 10" AND STGRS 23L AND 24L, SKIN WITH CORROSION. CORRECTIVE ACTION: CORROSION WAS FOUND ON AFT FUSELAGE SKIN, BETWEEN STA 1562+10" AND STGRS 24L AND 25L AND WAS BLENDED IAW B767-400 SRM 51-10-02 -0G REV 68.00 MAY-16-202SDR AALA202311164149Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: LEFT HAND SIDE OF FUSELAGE SKIN HAS AREAS OF CORROSION AROUND LAVATORY VENT AT AIRCRAFT STA 917 AND STR 21L TO 22L. CUT OUT DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER AND TRIPLER REPAIR. PER B737-NG SRM 53-70-01-2R-3.SDR MASA20240424010Skin · damagedPREVIOUS DAMAGE PLACED ON MRO WAS REVALUATED AND PATCH REPAIRED IN ACCORDANCE WITH EMBRAER ETD2023-170-028986 REV C.SDR VNAA202401050013Skin · damagedLIGHTNING STRIKE DAMAGE FS 510.75 WITHIN 1,628.27 FH (BEFORE 20,510.04 FH) AFTER ACCOMPLISHMENT OF SECTION I, REPAIR, OR REPLACE THE DISCREPANT AREAS IN ACCORDANCE WITH APPROVED PROCEDURES. LIGHTNING STRIKE DAMAGE BTW FS 510.75 AND STRG 16LH /17LH WAS REPAIRSDR VNAA202401050004Skin · damagedLIGHTNING STRIKE DAMAGE FS 171.00 WITHIN 1,628.27 FH (BEFORE 20,510.04 FH) AFTER ACCOMPLISHMENT OF SECTION I, REPAIR, OR REPLACE THE DISCREPANT AREAS IAW APPROVED PROCEDURES. LIGHTNING STRIKE WAS FOUND ON LH SKIN PANEL FS 171 & STGR23LH WAS REPAIRED PER REO 6SDR SWAA2023121121942Skin · crackedCRACK ON FUSELAGE SKIN BS907+10' JUST ABOVE STR22L COMMON TO WASTE TANK EXHAUST PORT CUTOUT<[01] THIS IS A CATEGORY B REPAIR AS PER SRM 53-70-01-2R-3.;[02] TASK COMPLETE.;[03] CORRECTION TO CORRECTIVE ACTION STEP 2 SHOULD STATE ' CRACK WAS FOUND TO BE OUT OF LSDR YENA2023111701409Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON UPPER SKIN AND FASTENERS AREA COVERED BY LIVE TV RADOME; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00038 ) REPAIRED PER LETBLUE EC E23-991-0. REF TOMX NR 00168.SDR YENA2023111601395Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE III / FR 80 BTW STGR 28R - 27R / CORROSION- TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601394Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE III / FR 80 BTW STGR 28R - 27R / CORROSION- PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601392Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / STR27R / BWTN FR86-FR87 /CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601391Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE SKIN / FR 62-66 & STGR 02L-02R / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR DALA2023111609471Unknown · unknownSHIP 6812 DENT ON FUSELAGE SKIN ON BS 705 BTW STRINGERS 25LH & 26LH SIDE. CORRECTIVE ACTION: THE DENT WAS EVALUATED AND FOUND OUT OF LIMITS. SUMMARY OF NRC 00033: DENT ON FUSELAGE SKIN ON BS 705 BTW STRINGERS 25LH & 26LH SIDE WAS REPAIRED PER ERA 613647-14. (0SDR DALA2023111609459Unknown · unknown(LOG 0066732) DENT FOUND ON EXTERIOR SURFACE OF FUSELAGE SKIN @STA. 887+15, 2.15" OUTBD OF STR. 27L. REPAIRED FUSELAGE SKIN PER ER/A 613176-14 REV. ORIGINAL.SDR DALA2023111609458Unknown · unknown(LOG 0066702) DENT FOUND ON EXTERIOR SURFACE OF FUSELAGE SKIN @STA. 887+15, 2.2" INBD OF STR. 27R. REPAIRED FUSELAGE SKIN PER ER/A 613176-14 REV. ORIGINAL.SDR DALA2023111609456Unknown · unknown(LOG 0066692) DENT FOUND ON EXTERIOR SURFACE OF FUSELAGE SKIN @887+15, 3.0" INBD OF STR. 27L. REPAIRED FUSELAGE SKIN PER ER/A 613176-14 REV. ORIGINAL.SDR DALA2023111609455Unknown · unknown(LOG 0066676) DENT FOUND ON EXTERIOR SURFACE OF FUSELAGE SKIN @STA 887+15, 1.7 OUTBD OF STR. 27R. REPAIRED FUSELAGE SKIN PER ER/A 613176-14 REV. ORIGINAL.SDR VNAA202401040037Skin · wornWEAR ON FUSELAGE EXTERNAL SKIN, LOCATED BTW FS= 897.70 / FS=927.00 AND STGR 27. WEAR ON FUSELAGE EXTERNAL SKIN, LOCATED BTW FS= 897.70 / FS=927.00 AND STGR 27 WAS REPAIRED PER REO 690-53-51-390 REV - - DISPOSITION.SDR VNAA2024010400003Skin · nickedSEVERAL NICKS ON LOWER FUSELAGE, FS235.00 TO FS310.00 BTW STGR 25RH TO STGR 25LH. SEVERAL NICKS ON LOWER FUSELAGE, FS235.00 TO FS310.00 BTW STGR 25RH TO STGR 25LH WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND LOWER SKIN FWD FUSELAGE BTW FS235 TO FS28SDR IXXA2023112001Skin · crackedRI DOOR LOWER CORNER CRACKS ON FUSELAGE AND BEARSTRAPSDR AALA202311177748Skin · corrodedAIRCRAFT IN BASE MAINTENACE: LOWER FUSELAGE EXTERIOR SKIN HAS EVIDENCE OF CORROSION AROUND BELLY DRAINS AT BS 727J + 3. BETWEEN BLO AND LBL9. INSTALLED DOUBLER REPAIR PER EA 348642.SDR IXXA2023111701Skin · crackedFUSELAGE SKIN AND BEAR STRAP AT THE LOWER TWO HOLES OF THE R1 DOOR LOWER CORNER ARE CRACKED.SDR DALA2023111609454Unknown · unknown(LOG 0064624) DURING INSPECTIONS, FOUR (4) DENTS WERE DISCOVERED ON THE FUSELAGE SKIN (PN 147A3400-5) AT APPROX. BS 902, BETWEEN S-26L AND S 26R. REPAIRED DAMAGE PER ERA 613176-14.SDR DALA2023111409354Unknown · unknownCRACK ON INNER SKIN WAS FOUND ON UPPER AFT CORNER AT LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00707: CRACK ON INNER SKIN ON UPPER AFT CORNER AT LH SLIDING WINDOW CUTOUT WAS REPAIRED PER B-717 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1. (LP #0063939)SDR DALA2026080504505Doubler · corrodedER/A 613288-14 ISSUED FOR CORROSION ON THE AFT WASTE BOX AND INTERNAL DOUBLER. C/W REP INSP PER ER/A 613288-14 SEC II REV. ORIG. NO FURTHER DEFECTS NOTED. OK TO CONT ON MON.ERA REVISED TO REV 'A'. SECTION IV ADDED IN THIS REVISION. LOGPAGE 1727108 IS CREATEDSDR SWIA2024012531113Skin · gougedDURING AUDIT OF 6YR TASK CARD 53-900-502(EXTERNAL GENERAL VISUAL INSPECTION OF THE SIDE AND LOWER SKIN PANELS COVERED BY THE WING-TO-FUSELAGE FAIRING - FS801.25 TO FS977.00 LH AND RH) FOUND GOUGED SKIN PANEL AND RIVETS AT STGR 27 AND APPROXIMATELY FS977.00 WHESDR FDEA202311131895Skin · dentedFUSELAGE TAIL SKIN FOUND 1EA BULGED AT FR93 PLUS 5.3",S-16R PLUS 3.5",POS. CUT OUT DAMAGE AREA,FABRICATED THE REPAIR DOUBLER,WET INSTALLED REPAIR DOUBLER WITH FASTENERS. I.A.W A300-600F SRM 53-19-12-201,PARA.6B,FIG202,PAGE213~PAGE218. "MAJOR REPAIR"
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