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 DALA2023021001072Unknown · unknownSHIP 5637 COMPLY WITH FINAL ERA 604249-14 REV.B. CORRECTIVE ACTION: REF ERA 604249-14 REV B. (2620837)SDR DALA2023021401133Unknown · unknownWORN ON PREVIOUS REPAIR (2EA) OF FWD CARGO DOOR BARRIER LATCHES. SUMMARY OF NRC 00547: REPAIR DOUBLERS WERE REPLACED PER ER/A 559579-14MA REV ORIGINAL, SECTION I. PERMANENT REPAIR ASSOCIATED ER/A 14-559579 ADDED FOR AC 9553. (LP #2618071)SDR DALA2023021001063Unknown · unknownSHIP 1200 WHEN PERFORM AIRCRAFT ARRIVE INSPECTION,FOUND A HEAVY DENT WITH A PERVIOUSLY INVALID LOG NUMBER(LOG:6926914)ON THE FUSELAGE SKIN EXTERNAL SURFACE BETWEEN STA 1562 AND STA 1582, JUST ABOVE STR20L.RE-EVALUATE THE DENT REUIRED. CORRECTIVE ACTION: DAMAGESDR DALA2023020801011Not Reported · not reported(LOG 2618946) DURING HEAVY MAINTENANCE CHECK/ENTRY INTO SERVICE AT FLIGHTSTAR (VQQ), A DENT WITH CREASE WAS FOUND AFFECTING THE EXTERNAL SKIN APPROX. AT STA 200.00 & LBL 30.00. MAINTENANCE REPAIRED DAMAGE PER ERA 605177-14.SDR SWI2023F00023Unknown · unknownPERFORM SPLICE REPAIR TO L/H INBD FLAP LWR INBD SKIN (C-CHECK RO 3/11/2023) PERMEANANTLY REPAIRED L/H INBD FLAP LWR SKIN DENT BUY PERFORMING AND COMPLYING WITH LWR SKIN SPLICE REPAIR REF BOMBARDIER REO 601R-57-52-1544 REV -- 2010-01-07. COMPLIED WITTH SDR SWIA20230315012Unknown · unknownPERFORM SPLICE REPAIR TO L/H INBD FLAP LWR INBD SKIN (C-CHECK RO 3/11/2023) PERMEANANTLY REPAIRED L/H INBD FLAP LWR SKIN DENT BUY PERFORMING AND COMPLYING WITH LWR SKIN SPLICE REPAIR REF BOMBARDIER REO 601R-57-52-1544 REV -- 2010-01-07. COMPLIED WITTH SDR SWAA2023030299628Panel · crackedPASSENGER CABIN FLOOR BREAK PANEL ASSY BS 540; BL 0 - LBL 25; WL 208 IS CRACKED.<[01] REMOVED AND REPLACED PASSENGER CABIN FLOOR BREAK PANEL ASSY BS 540; BL 0 - LBL 25; WL 208 IAW SRM 51-40-02-0G-0 AND AIPC 53-31-00-05;[02] VERIFIED CORRECTIVE ACTION 1;[03] UPSDR SWAA2023022499992Doubler · crackedCUSTOMER REQUEST: GROUND POWER DOOR DOUBLER FWD. LOWER SIDE HAS A CRACK. WORKED CARD IN CONJUNCTION WITH CARD TTG8Q00HUQ7A<[01] VERIFIED CRACK ON EXTERNAL GROUND POWER DOOR; CRACK LOCATED AT SURROUND DOUBLER FWD SIDE; 1.75' ABOVE LOWER DOOR CUTOUT; CRACK LENGTSDR DALA2023021001059Unknown · unknownSHIP 1200 THE LH MLG UPPER SKIN OF CABIN END FITTING CRACK AT STA 852. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER PRI 605518-14 (2616521)SDR SWAA2023032099274Angle · crackedCRACK ANGLE LOCATED BS500D AFT FACE AND STR 27R AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT 2023-106213<[01] INSTALLED ANGLE LOCATED BS500D AFT FACE AND STR 27R AT LEVEL FLOOR STRUCTURE FWD CARGO COMPARTMENT;[02] JOB RII COMPLETESDR SWAA2023031699275Angle · crackedCRACK ANGLE LOCATED BS500B AND STR25 FWD CARGO COMPARTMENT 2023-106219<[01] REPLACED ANGLE LOCATED BS500B AND STR25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED IAW SRM 51-40-02 AND DWG 143A7505 SHEET5 REV B. DUE TO NOT FOUND ALLOWABLESDR SWAA2023030699309Structure · crackedCRACK ACCESS PANEL 321A RIB 8 INTERNAL STRUCTURE VERTICAL STABILIZER 2023-99283<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24.;[02] REPLACED RIB 8 INTERNAL STRUCTURE VERTICAL STABILIZER IAW B737-700 SRM 51-10-SDR DALA2023020700979None · noneSHIP 3308 DENT EXTERNAL SKIN FR68 TO FR69 AND STR52R TO STR56R LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 605293-14 PRI REV-0, VALIDATED WITH ER/A 605293-14 REV-ORIGINAL MATCHES HAS BEEN WITH PRI REV-0, PERFORMED PERMANENT REPAIR ON DENT AREA LOC. BSDR DALA2023020700978None · noneSHIP 3308 DENT ON EXTERNAL SKIN LOC BTW FR 66 TO FR 67 AT LEVEL OF STRG 56R TO 57R. CORRECTIVE ACTION: COMPLIED WITH ER/A 605293-14 PRI REV-0, REV-1 AND PRI REV-2 AND VALIDATED WITH ER/A 605293-14 REV-ORIGINAL MATCHES PRI 605293-14REV-0, REV-1 AND REV-2, PERFOSDR DALA2023020700977None · noneSHIP 3307 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR30 AND STR27L AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 605067-14 REV. 0, VALIDATED ER/A 605067-14 REV. ORIGINAL MATCHES PRI 605067-14 REV. 0. EXISTING REPAIRINSTALLESDR DALA2023020700972None · noneSHIP 3307 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR73 TO FR74 BTW STR30L TO STR31L AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 605067-14 REV. 0, VALIDATED ER/A 605067-14 REV. ORIGINAL MATCHES PRI 605067-14 REV. 0. EXISTSDR DALA2023020700966None · noneSHIP 3308 DENT EXTERNAL SKIN FR58 TO FR59 AND STR55L TO STR56L LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 605293-14 PRI REV-0, VALIDATED ER/A 605293-14 REV-ORIGINAL HAS BEEN MATCHES WITH PRI-REV-0, PERMANENT REPAIR ON DENT AREA LOC. BTW FR58 TO FR59SDR SWAA2023030698951Angle · crackedCRACK ANGLE LOCATED BS500B AT LEVEL STR26R AT FWD CARGO COMPARTMENT 2023-99199<[01] REPLACED ANGLE LOCATED BS500B AT LEVEL STR26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 DWG 143A7505 SHEET 82 REV. - SEE INDIVIDUAL SIGN OFF BESDR SWAA2023030698948Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2023-99190<[01] REPLACED GUSSET LOCATED BS500D STR19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 AND DWG 143A7902 SHEET 209 REV - ;SEE INDIVIDUAL SIGNOFF BELOW;[02] SDR SWAA2023030698949Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-99193<[01] REPLACED GUSSET LOCATED BS500D STR19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 PARAGRAPH 9 AND DWG 143A7902 SHEET 209 REV - ;SEE INDIVIDUAL SIGNOFF BELOW;[02] SDR SWAA2023030698950Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 480 AND BETWEEN STR23L TO STR24L AT FWD CARGO COMPARTMENT 2023-99196<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE - SUPPORT LOCATED BS 480 AND BETWEEN STRSDR SWAA2023030698947Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500C TO BS500D AND AT LEVEL STR26L FWD CARGO COMPARTMENT 2023-99198<[01] REPLACED WEB -INTERCOSTAL LOC. BTW BS500C TO BS500D STR26L IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DRAWING # 143A7505 REV. - SEE INSDR DALA2023121110133Unknown · none(LOG 2613157) DURING THE ORIGINAL INSTALLATION OF THE IDTV INSTALLATION THE INSTALLATION JIG WAS INCORRECTLY LOCATED SEVEN INCHES FORWARD OF THE CORRECT LOCATION RESULTING IN MULTIPLE PLUGGED FASTENER LOCATIONS AND ENLARGED REINFORCING DOUBLERS. DAMAGE WAS REPSDR SWAA2023030698657Stringer · crackedCRACK STRINGER 24R LOCATED BS540 AND WL161.3 AT FWD CARGO COMPARTMENT 2023-99165<[01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N: 221859911 DUE DATE: 07-NOV-23;[02] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138203; CAL DUE DATE: 11-ASDR SWAA2023030698653Stringer · crackedCRACK STRINGER 26R LOCATED BS540 AND WL 152.7 FWD CARGO COMPARTMENT 2023-99166<[01] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 210138203; CAL DUE DATE: 11-APR-23.;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE SDR SWAA2023030698655Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS500D AND STR28L AT FWD CARGO COMPARTMENT 2023-99168<[01] REPLACED ANGLE - SUPPORT LOCATED BS500D AND STR28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 ;DWG 143A7902 SHEET 1 REV E. MATERIAL USED ALUMINSDR SWAA2023030698687Panel · crackedCRACKED PLEXIGLAS ON RH EMERGENCY EXIT DOOR ACTUATOR CORRECTION TO FAULT DESCRIPTION: CRACKED PLEXIGLASS GUARD OVER R/H EMERGENCY EXIT COUNTERBALANCE ASSEMBLY<[01] REMOVED SIDEWALL PANEL 232 YJW FOR ACCESS IAW AMM 25-21-46-000-801;[02] REMOVED AND REPLACED R/HSDR DALA2023020700981None · noneSHIP 3308 DURING HCK, MULTIPLE DENTS WERE FOUND ON THE REAR FUSELAGE LOWER SKIN PANEL. THE DENTS WERE REWORKED AND INSPEC TED PER SECT I OF ERA 605293-14. CORRECTIVE ACTION: ACCOMPLISH THE SECT III DVI INSPECTION OF THE SECTION I REWORKED DENTS PER DELTA ERA 6SDR DALA2023020700955None · noneSHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR29 TO FR31 BTW STR51L TO STR51R AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 486923-14. ISSUE C, WITHSUPPLEMENTAL INSPECTIONS ALREADY TRACKED AS PER DALSDR DALA2023020700980None · noneSHIP 3308 DURING HCK, A DENT ON THE FUSELAGE SKIN WAS FOUN D AT FR 66 TO 67, STR 56R TO 57R. THE DENT WAS REWORKED AND INSP ECTED PER SECT II OF ERA 605293-14. CORRECTIVE ACTION: THE DENT REORKED AND INSPECTED PER SECTION II IS APPROVED. (2613663)SDR AALA202302074333Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON FUSELAGE SKIN PANEL AROUND THE LAVATORY VENT CUTOUT AT FR 69 AND S31R. MAINTENANCE REPAIRED SKIN PANEL PER SRM 53-41-11-300-004SDR IPXA2023021490996Stiffener · crackedINSPECTION TYPE:2CAFT CARGO AT STA 1841 L/H SIDE HAS A VERTICAL STIFFENER IS CRACKED.REMOVED, FABRICATED, REPLACED CRACKED VERTICAL STIFFENER IN AFT CARGO AT STA 1841 L/H SIDE IAW SRM 51-31-01, SRM 51-33-01 (MINOR)SDR DALA2023020600907Not Reported · not reportedSHIP 689 DENT WAS REEVALUATED PER TASK CARD 2020-9002 (ADF FILE), APPROX ON STA.1709 BTW S-15L TO S-16L , WAS FOUND OUT LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00585. AREA WAS REPAIRED PER ER/A 605611-14 REV ORIGINAL AND PRI 605611-14 REV.0. (2611575)SDR DALA2023020600891Not Reported · not reported(LOG 2611297) DURING INSPECTION FOUND CORROSION FOUND ON MULTIPLE AREAS OF ANTENNA BASE FITTING STA 727. BLENDED AREAS OF CORROSION ON ANTENNA BASE FITTING AT STA 727 IAW HAECO B 737-900 AMM 44-20-00 PG 801 PROCEDURE 2-C-3. FOUND TO BE OUT OF LIMITS WITH 100% SDR DALA2023020400872Not Reported · not reportedSHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.83 TO FR.84 BTW STR33R TO 36R AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER NWA EA 33-201684, REV B. ALSO INSPECTIONS AND INSTALLATION OF MISSING FASTENERS WSDR DALA2023020400871Not Reported · not reportedSHP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.27 TO FR.28 BTW STR 50L TO STR 51L AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 486923-14, DUE THE DISCREPANT FASTENER LOCATION ENCOUNTERED AS PER INSPESDR DALA2023020400869Not Reported · not reportedSHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.27 TO FR.28 BTW STR50L TO STR51L AT LOWER FUSELAGE. CORRECTIVE ACTION: EXISTING REPAIR INSTALLED PER ER/A 486923-14, INSPECTIONS ALREADY TRACKED AS PER DAL LP 0437802. ALSO, DUE TSDR CALA2023020300315Skin · not enteredMOVE CREW REPORTED SKIN SCRATCH ON LEFT SIDE OF AIRCRAFT BETWEEN STATION 410-420. PICTURES INCLUDED STR 21L. A DIP IS BEING CREATED FOR THE REINSPECTION CRITERIA AT 7,000 CYCLES, INTERNAL HFEC AT 36,000 CYCLES, EXTERNAL LFEC DV AT 36,000 CYCLES. INSPECTION THSDR SWIA202302012None · dentedPROTRUDING DENT FOUND ON REAR FUSELAGE SIDE SKIN PANEL BETWEEN FR93 AND FR94, AND BETWEEN STGR 19RH AND STGR 21RH. (C-CHECK RO 2/20/2023) PERFORMED PERMANENT REPAIR TO PROTRUDING DENT FOUND ON REAR FUSELAGE SIDE SKIN PANEL BETWEEN FR93 AND FR94, AND BETSDR DALA2023020600887Not Reported · not reported(LOG 2610348) DURING CCK AT QRO, WHILE PERFORMING STEPS 17 & 18 OF WORK CARD 2330-01337-1001, FOUR (4) CRACKED HOLES AND TWO (2) ELONGATED HOLES WERE FOUND ON FUSELAGE SKIN BETWEEN STA. 727E & 727H, STRINGER S-3R & STRINGER S-3L AT LOCATIONS SHOWN IN FIGURE 1 SDR DALA2023020300848Not Entered · not enteredSHIP 1200 ERA 605103-14 ISSUED FOR SKIN REPAIR AT STA 1562 - 1582, S20L. D TA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED AT OR BEFORE 37499 TOTAL FLIGHT CYCLES. (2609943)SDR BLUA2023052500444Skin · corrodedLEFT AND RIGHT LOWER FUSELAGE SKIN AT FORWARD BELLY FAIRING ATTACHMENTS LIGHT CORROSION. REPAIRED UNDER BOMBARDIER REO 604-53-21-420.SDR SWIA20230100031None · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA82128-ETD2023-170-001500 MXCODEID65703-PR - DENT ON FORWARD FUSELAGE SKIN LH SIDE BETWEEN FRAMES 9-11 AND STRINGERS 17L-18L.DENT DIMENSIONS: DEPTH: 1.7 MM X LENGTH: 147.32 MM X WIDTH: 66.675 MM. DENT REQUIRES PERMANENTSDR IPXA2023020990817Skin · corrodedINSPECTION TYPE:2C*MAJOR REPAIR* R/H TAIL AFT BODY SECTION SKIN HAS CORROSION BETWEEN STA Y= 2119.685, Y=2163.681 AND BEWEEN LONGERON 32R, 35R.REPAIRED CORRODED SKIN AT THE TAIL R/H AFT BODY SECTION BETWEEN STA Y=2119.685, Y=2163.681 AND BETWEEN LONGERON 32R, SDR ASAA2023013042727Skin · dentedLESSOR ITEM 2:FUSELAGE-TAIL CONE, MIDDLE, HAS 2 DENTS TO BE EVALUATED. GROUNDED - YES. MEASURED DENT 1 Y=.900, X=.900 DEPTH=.020 DENT LOCATION BETWEEN FR 83 TO FR 84, STR1 RH AND STR2 RH FOUND TO BE WITHIN LIMITS REF A320 SRM 53-51-11-283-024/53-00-11-283-005 SDR ASAA2023013042642Skin Panel · dentedLESSOR ITEM: RIGHT HAND AFT FUSELAGE ABOVE CABIN WINDOWS, DENT TO BE EVALUATED GROUNDED - YES. MEASURED DENT , FOUND TO BE OUT OF LIMITS DUE TO GOUGE IN DENT,REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED, INSTALLED REPAIR AND RESTORED COATINGS REF A320 SRM 53-SDR ASAA2023013042502Skin Panel · dentedLESSOR ITEM: L/H AFT FUSELAGE AT FWD VERTICAL FIN JUNCTION, DENT TO BE MEASURED GROUNDED - YES. ACCOMPLISHED DVI OF DENT, FOUND TO BE OUT OF LIMITS DUE TO GOUGE IN DENT.REMOVED DAMAGE, FABRICATED , LOCATED, DRILLED , INSTALLED REPAIR ANDRESTORED COATINGS RESDR DALA2023020200829Not Entered · not entered(LOG 2607114) DURING GOGO 2KU INTERNET, RADOME AND ANTENNA DEMOD ON 737-800 RADOME PER WC 2330-01334-21D AND 2330-01337- 42, MTC NOTED TWO HOLES WITHOUT A MINIMUM FASTENER SPACING. MAINTENANCE REPAIRED DAMAGE PER ERA 605622-14.SDR UIEA2023013100070Skin · crackedTWO CRACKS FOUND AND 1EA CORROSION FOUND ON LT FUSELAGE SKIN BETWEEN BS 1680 AND 1700, STR 43L. FUSELAGE SKIN CORROSION AND CRACK AREA REPAIRED IAW RI-53-00-16037 REV A.SDR UIEA2023013180054Skin · corroded1EA CORROSION FOUND ON STA 1720 STR 43L.(<P>FX - STA 1720 STR 43L FUS SKIN CORROSION AREA REPAIRED IAW RI-53-00-16035 REV.A</P>)
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