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 DALA2023050103386Unknown · unknownDENT ON FUSELAGE A FR50+10 2" ABOVE STR8 R. REPAIRED DENT ON FUSELAGE SKIN @ FR50+10 2" ABOVE STR 8 IAW A321 SRM 53-00-11-300-029. DENT MEASURED 2.7"L X 2.0"W X .062"D, DENT FOUND TO BE OUT OF LIMITS IAW A321 SRM 53-41-11-283-005. (LP# 2738490)SDR IPXA2023051393216Skin Panel · delaminatedINSPECTION TYPE:SEG4*MAJOR REPAIR* LARGE DENT ON TOP OF TAIL CONE. AFT RUDDER, APPROX. BETWEEN S1L AND S2LREPAIRED PANEL IAW B757 SRM 51-70-10-2R REPAIR PER EA 757-5380-27-A3220SDR SWIA20230626424Unknown · dentedADM# N960SW-5025 DENT LOCATED BELOW CARGO DOOR AT FS589.00 BETWEEN STGR 19L AND 20L. DENT IS .408" X .398" AND .031" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECKSDR SWAA2023052442225Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 500H TO 500I LBL 24 WL 156.<[01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 500B+12 TO 500I PER SRM 53-00-53-2R-5.REFERENCE NON ROUTINE CARD #TTG8Q00KM7HK FOR WORK COMPLETED.;[02] INSPECTION C/W L/H SDR SWAA2023052442511Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 500G TO 500H LBL 24 WL 156.<[01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 500B+12 TO 500I.<BR>REFERENCE NON ROUTINE CARD #TTG8Q00KM7HK FOR WORK TO BE ACCOMPLISHED.;[02] INSPECTION C/W L/H TRANSITIOSDR SWAA2023052442512Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 500F TO 500G LBL 24 WL 156.<[01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 500B+12 TO 500I.<BR>REFERENCE NON ROUTINE CARD #TTG8Q00KM7HK FOR WORK TO BE ACCOMPLISHED.;[02] INSPECTION C/W L/H TRANSITIOSDR SWAA2023052442513Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 500E TO 500F LBL 24 WL 156.<[01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 500B+12 TO 500I.<BR>REFERENCE NON ROUTINE CARD #TTG8Q00KM7HK FOR WORK TO BE ACCOMPLISHED.;[02] INSPECTION C/W L/H TRANSITIOSDR SWAA2023052442514Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 500D TO 500E LBL 24 WL 156.<[01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 500B+12 TO 500I.<BR>REFERENCE NON ROUTINE CARD #TTG8Q00KM7HK FOR WORK TO BE ACCOMPLISHED.;[02] INSPECTION C/W L/H TRANSITIOSDR SWAA2023052441480Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 420 TO 440 LBL 24 WL 156.<[01] BLENDED SCRIBE MARK PER 51-10-02.REMOVED .002 OF MATERIAL THICKNESS; WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. TREATED AND PRIMED PER SRM 51-20-01.;[02] VERIFIED DAMAGSDR SWAA2023052443072Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 500B TO 500C LBL 24 WL 156.<[01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 500B+12 TO 500I.<BR>REFERENCE NON ROUTINE CARD #TTG8Q00KM7HK FOR WORK TO BE ACCOMPLISHED.;[02] INSPECTION C/W L/H TRANSITIOSDR SWAA2023052443071Angle · scratchedFWD CARGO L/H TRANSITION ANGLE HAS SCRIB MARKS FROM STA. 500C TO 500D LBL 24 WL 156.<[01] L/H TRANSITION ANGLE WILL BE REPLACED FROM STA 500B+12 TO 500I.<BR>REFERENCE NON ROUTINE CARD #TTG8Q00KM7HK FOR WORK TO BE ACCOMPLISHED.;[02] INSPECTION C/W L/H TRANSITIOSDR SWIA202305160001Skin · dentedCOMPLY WITH ETD2023-170-009941 DIPOSITION A. TEMPORARY REPAIR FOR DAMAGES #1 TO #4, (SEE FIG 1 AND FIG 5). MAJOR REPAIR. (FILED CLOSED)COMPLIED WITH TEMP REPAIR TO RT FUSELAGE BETWEEN FR 20 AND FR23 AND BETWEEN STGR 23R AND 26R PER ETD 2023-170-009941 REV B. DSDR R61A2023051600286Skin Splice · damagedREPAIR RH SKIN SPLICE 170-03589-001 FR 12-17 ABOVE STR 20R. REPAIRED THE SKIN SPLICE AS PER THE PROCEDURE. REF ETD2023-170-009823 REV B.SDR SWIA20230424001Unknown · dentedCOMPLY WITH ETD2023-170-009941 DIPOSITION A. TEMPORARY REPAIR FOR DAMAGES #1 TO #4, (SEE FIG 1 AND FIG 5). MAJOR REPAIR. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR DALA2023042503208Unknown · unknownSHIP 5029 MISDRILLED IN SEVERAL SPOTS WHILE INSTALLING WI-FI. CORRECTIVE ACTION: COMPLIED WITH AA 4430-01005-01R, -01E, -01G, 01H, -01I, -01J, -01K, -01O. (2735328)SDR IXXA2023042403Skin · crackedCRACK IN SKIN AND BEARSTRAPSDR JJBA20230616016Skin · dentedDENT LOCATED BELOW RVSM AREA ON RH SIDE OF AC BETWEEN FRAMES 14&15 AT SKIN SPLICE. "REMOVED RIVETS IN AFFECTED AREA & RECONTOURED AREA. PERFORMED HIGH FREQ EDDY CURRENT INSPECTION OF RECONTOURED AREA, INTERNAL AND EXTERNAL AREAS, NO DAMAGE NOTED. ENLARGE CUT-SDR JJBA20230616015Skin · dentedDENTS AT FR16 & FR15 BETWEEN STRINGER 16R & 17R NEAR SKIN SPLICE HAS OIL CANNING. PERFORMED HFEC ON THE CUT STRINGER. NO CRACKS FOUND. ENLARGE CUT-OUT. FABRICATED DOUBLER/FILLER, MATCH DRILLED FASTENER LOCATIONS, COUNTER SUNK FOR BRF2AD5 RIVETS, BEGAN INSTALLASDR IPXA2023051993271Skin · corrodedINSPECTION TYPE:3C*** MAJOR REPAIR *** AFT FUSELAGE R/H SIDE BODY FAIRING AREA STA Y=2140-Y=2160 AND LONGERON 33R-35R LWR EXTERNAL SURFACE HAS CORROSION.REPAIRED CORRODED SURFACE SKIN AT THE AFT FUSELAGE R/H SIDE BODY FAIRING BETWEEN STA Y=2140-Y=2160 AND LONSDR DALA2023042703276Unknown · unknownSHIP 3302 LIGHTNING DAMAGE FOUND ON 2 FASTENERS ON STR23L BETWEEN FR 26.2 AND 26.3. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER A330 SRM 53-21-11. (2734148)SDR DALA2023042703286Unknown · unknownTASK CARD NUMBER: 001-0231:2520-1002/002 REF NR 00325. FOUND CORROSION ON SKIN UNDER FORWARD DRAIN MAST. CORROSION LEVEL 2. REPLACED DOUBLER AND INTERCOSTAL PER B717 DRAWING 9923686. (LP #2731615)SDR SWIA20230421Unknown · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA74228-670-53-21-2167 N724SK MXCODEID59543-PR - ONE BURN MARK ON FUSELAGE SKIN LOCATED .25" FROM RIVET ON STGR-5L AFT OF FS295. BURN MARK IS .023" DEEP. REO. 670-53-21-2167 REV --, DATED 2021-10-14. COMPLIED WITH TEMPOSDR SWAA2023052430115Scuff Plate · crackedFWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON RADIUS OF FWD CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.B.(2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583 CASDR FDEA202304210727Doubler · corrodedLOWER FUSELAGE BELLY STATION 1721 -1741 LONGERON 51 LEFT DRAIN MAST CUTOUT DOUBLER FOUND CORRODED. LOWER FUSELAGE BELLY STATION 1721 - 1741 LONGERON 51 LEFT DRAIN MAST CUTOUT DOUBLER CORROSION REMOVED AND FOUND OUT OF LIMIT AS PER SRM 53-00-00-2R FIGURE SDR SWAA2023052529555Doubler · crackedCUSTOMER REQUEST CRACK ON EGPR SURROUND DOUBLER AT BS 235.8 LOWER FUSELAGE 2023-282414<[01] TOOL USED: CALIPER PN: 500-196-30 S/N: A22046819 DUE DATE: 22/JUN/23;[02] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:60009161631; DUE DATE: 31-JAN-24;[03] PERSDR FDEA202304200865Skin · dentedFUSELAGE SKIN FOUND 1EA DENT AT FR99 PLUS 5",S-4L PLUS 5" REPAIRED THE DAMAGE AREA WITH DOUBLER, THIS IS CAT.A REPAIR I.A.W A300-600 SRM 53-19-12- 201, PARA.5, FIG.201, PAGE.204~208 "MAJOR REPAIR"SDR IPXA2023050993163Skin · corrodedINSPECTION TYPE:3CMAIN CABIN R/H CTR WING BOX UPPER SURFACE FWD EDGE HAS CORROSION BETWEEN STA XCW=-96.5 AND XCW=-81.REPAIRED CORRODED SURFACE SKIN AT THE MAIN CABIN R/H CTR WING BOX UPPER FWD EDGE BETWEEN STA XCW=-96.5 AND XCW=-81 IAW VTSAA EA 011-5710-01-A99SDR IPXA2023050993167Skin · corrodedINSPECTION TYPE:3CMAIN CABIN R/H CTR WING BOX TUNNEL HAS 3EA AREA OF CORROSION BETWEEN STA Y=1256-1305 AND 105 - 108 INCH FROM CL.REPARIED CORRODED SKIN AT THE MAIN CABIN R/H CTR WING BOX TUNNEL BETWEEN STA Y=1256-1305 AND 105-108 INCH FROM CL IAW VTSAA EA 011SDR IPXA2023050993166Skin · corrodedINSPECTION TYPE:3CMAIN CABIN L/H CTR WING BOX SKIN AT STRINGER 15 HAS CORROSION 98 INCH FROM CL.REPAIRED CORRODED SKIN AT THE MAIN CABIN L/H CTR WING BOX AREA AT STA XCW=94 - XCW=98 IAW VTSAA EA 011-5730-01-A9947 I/R UPS MD11-5730-86789-A DATED 05/05/23 (MINORSDR R61A2023051000270Skin Panel · corrodedCFIII, CORROSION FOUND ON SKIN, UNDER R2 DOOR SCUFF PLATE AT LOWER AFT FASTENER HOLE BETWEEN FR 8 , FR 87, AND BETWEEN STR 17R - STR 18R. CFIII, CORROSION ON SKIN UNDER R2 DOOR SCUFFPLATE AT LOWER AFT FASTENER HOLE BTWN FR 88 - FR 87. BTWN STR 17R - 18R REPAISDR SWAA2023050929680Doubler · corrodedCORROSION ON DOUBLER UNDER VERTICAL FIN AT WL 308 BS 1016+23 RBL 8.<EVALUATED DAMAGE ON DOUBLER UNDER VERTICAL FIN AT WL 308; BS 1016+23; RBL 8. MAXIMUM MATERIAL LOSS 0.8' X 0.8' X 0.004' ORIGINAL THICKNESS 0.040' REMAINING THICKNESS 0.036' FOUND TO BE OUT OF SDR DALA2023042403182Skin · corrodedAIRCRAFT 3931, CORROSION ON UPPER FUSELAGE EXTERIOR SKIN UNDER ADF 1 ANTENNA STA 685-706 S1-2R. CORRECTIVE ACTION: COMPLIED WITH DELTA ER/A # 607361-14 REV ORIGINAL ASSOCIATED ER/A 14-607361 ADDED FOR AC 3931. (LP 2729033)SDR CALA2023042101197Skin · damagedFWD CARGO DOOR FUSELAGE CUTOUT FWD EDGE CENTER SKIN BENT. REF. AAR N/R:9670307 REPAIR, DUE (LFEC) FOR DAMAGE IN THE SKIN AROUND WORK ACCOMPLISHED BY V095636 THE FASTENERS AT EACH 3.500 FLIGHT CYCLES INTERVAL. DO THE INSPECTION THAT FOLLOW FOR DAMAGE IN THE BEASDR FDEA202304200723Unknown · unknownFUSELAGE SKIN AT STA 1600 - 1620 STR1R/2R DENTED. ACCOMPLISHED FEDEX EA# F-5330-T0374201: FUSELAGE - PLATES AND SKIN - STA 1609 -S-1 - S- 2R, DENT REPAIR DOUBLER.SDR SWAA2023051229329Baffle · damagedFOUND ELONGATED HOLES DAMAGE AT BAFFLE UNDER 'Z' CHANNEL RBL 21; STA 400 - 420<[01] REMOVED;LOCATED AND DRILL AND INSTALLED NEW BAFFLE AT FWD CARGO BETWEEN STA 400-STA420 RBL21 AS PER SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0;[02] VERIFIED STEP 1SDR ASAA2023041943168Skin · corrodedFUSE SKIN CORRODED AT AFT LAV VENT. GROUNDED - YES. REPAIRED SKIN IAW 737-800 SRM 53-70-01-2R-3W .5" O .125" R .085" L 1" D .040".SDR AALA202305052608Skin · crackedAIRCRAFT IN BASE MAINTENANCE: EXTERNAL POWER RECEPTACLE INTERNAL DOOR FRAME IS CRACKED / MISSING MATERIAL. LOCATED BETWEEN 235.8 AND 243.7 AND STR 21R AND 22R. INSTALLED DOUBLER REPAIR PER SRM.SDR CALA2023042101187Angle · cracked(SUPPORT TASK) Z-ANGLE (P/N 141A8112-2) UNDER L1 DOOR MID SCUFF PLATE CRACKED. TRANSCRIBED FROM HAECO GSO NR 9282324 REMOVED CRACKED Z-ANGLE IAW B737-900ER SRM 51-40-02. INSTALLED N EW Z-ANGLE IAW BOEING DRAWING 141A8110 SHT 11 REV - AND B737-900 SRM 51-40-02 SDR CALA2023042101186Intercostal · cracked(SUPPORT TASK) INTERCOSTAL LOCATED AT STA 344-360 BL0 IS CRACKED AT FASTENER HOLES ON UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NR 9282328 REMOVED CRACKED INTERCOSTAL IAW B737-900 SRM 51-40-02. INSTALLE NEW INTERCOSTAL IAW BOEING DRAWING 141A5400 SHT 32 REV-SDR DALA2023042003116Unknown · unknownSHIP 5017 SKIN DAMAGE ON FRAME 5 MAJOR REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA 608099-14. (2727274)SDR DALA2023042003109Unknown · unknownCRACK ON FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH. SUMMARY OF NRC 00043: FUSELAGE SKIN Y=1037 BTW L13-RH & L14-RH WAS REPAIRED PER PRI 606978-14 REV.2 AND ER/A 606978-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-606978 ADDED FOR AC 9551. (LSDR SWAA2023052228845Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #242AF TOP SKIN PEELING OFF SEVERAL AREAS<[01] APPLIED GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON MAIN CABIN CENTER FLOOR PANEL #242AF. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#: 17385SDR IPXA2023042793005Skin Panel · damagedINSPECTION TYPE:SV*MAJOR REPAIR* SKIN DAMAGE STA 340 TO 355 BETWEEN STR 11L AND 12LREPAIRED PER VTMAE EA 757-5310-27-A3202 AND UPS EO B757-5330-86624-ASDR SWIA202304260003Unknown · dentedSMALL DENT FOUND ABOUT 2 INCHES FWD OF NOSE FUSELAGE JACK PAD. (FILED CLOSED)PERFORMED REPAIR OF DENTED AREA FWD OF NOSE FUSELAGE JACK PAD REF REO 690-53-11-1552 REV -- DATED 2023-04-20 FOR THE REPAIR TO LOWER FUSELAGE STRUCTURE BTW FS 265- FS 280 AND BTW SSTRSDR 2023F00111Skin · damagedOBLONG HOLE IN RH NOSE SKIN REF ENGINEERING MEMO DQ37272M1.SDR 2023F00110Skin · damagedOBLONG HOLE IN RH NOSE SKIN REF ENGINEERING MEMO DQ37272M1.SDR 2023F00109Skin · damagedOBLONG HOLE IN RH NOSE SKIN REF ENGINEERING MEMO DQ37272M1.SDR DALA2024041004278Skin · damaged(LOG 2722842) FUSELAGE / SKIN / BS 727D - 727E S-1 TO S-2L VIASAT INSTL HAS ELONGATED HOLES. DAMAGE REPAIRED PER ERA 607697-14 REV A.SDR DALA2023041803054Unknown · unknownSHIP 1708 FOUND FUSELAGE FROM STA 1582 TO 1629 ADJACENT ACCESS PANEL 322AL WORN. CORRECTIVE ACTION: DAMAGED AREA REPAIRED THE DAMAGED AREA AS PER PRI 607702-14 (722299)SDR SWAA2023050927775Skin · debondedPANEL 191FR OUTER SKIN IS DISBONDED. (MARKED)<[01] IDENTIFIED PANEL 191FR IAW SRM 53-30-70-0I-1; FIGURE 2; SHEET 1; TABLE 2; ITEM 4.<BR><BR>CLEANED PANEL FOR EVALUATION IAW AMM 51-21-11-150-815 PARA 17. C.<BR><BR>VISUALLY EXAMINED DAMAGE AND TAP TESTED WITH DI
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