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 AALA202210130105Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN PANEL AT THE BOTTOM EDGE OF THE LAVATORY DISCHARGE VENT. BETWEEN FR 69 AND FR 70, BETWEEN S31R AND S32R. REPAIRED FUSELAGE SKIN PANEL PER EA 338951 AND SRM 53-41-11-300-004.SDR DALA2022091506149None · noneAIRCRAFT 0662, A.A. - A.D. DISBOND (4.800IN LENGTH X 1.600IN WIDTH) ALONG THE EDGE OF THE CUTOUT AT L1 DOOR CUTOUT. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED ON THE EDGE OF THE CUT OUT AT L1 DOOR STA 330- 355, S6L-S10L (SKIN AND BEAR STRAP) PER ER/A 60SDR ASAA2022091340893Skin · crackedGROUND POWER DOOR CUT OUT (FLANGE) LOWER FORWARD CORNER IS CRACKED AND BENT. GROUNDED - YES. (RESOLVED ON W/O: 1921149 TASKCARD: N/R-00012 ) REPAIRED GROUND POWER DOOR CUT OUT LOWER FWD CORNER IAW B737-700 SRM 53-10-15-2R-5, LFEC AND HFEC REQUIRED EVERY 6,000 SDR JJBA20221017008Skin · corrodedCORROSION FOUND ON INTERNAL FUSELAGE SKIN AROUND CUTOUT FOR RAT #2 ANTENNA CABLE. REPAIRED REAR FUSELAGE SKIN AT RAT #2 ANTENNA.SDR JJBA20221017007Skin · corrodedREAR FUSELAGE I SKIN HAS CORROSION UNDER RAR #2 ANTENNA BASE. REPAIRED SKIN UNDER RAR #2 ANTENNA WITH REPAIR DOUBLER FILLERSDR DALA2022091406110None · noneSHIP 662 DTE, ER/A 601884-14AD FUSELAGE / SKIN / L1 DOOR CUTOUT SKIN & BEAR STRAP / STA 330-355, S6L-S10L / CRACK, DISBOND, INTERFERENCE AND ELONGATED HOLES. CORRECTIVE ACTION: REF ERA 601884-14AD. (2407209)SDR DALA2022091406124None · none(LOG 2405728) DURING INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT ANTENNA BLANKING PLATE BETWEEN STA 787 AND STA 807. REPAIRED AREA PER ERA 602160-14 REV A.SDR DALA2022110707198None · noneSHIP 654 DTE, ERA 601567-14 REV -, MONITOR INSPECTION LOG REPAIR AT FUSELAGE L1 ENTRY DOOR CUTOUT UPPER FORWARD CORNER SKIN AND BEAR STRAP REPAIR BETWEEN BS 333-355, STRINGER 5L AND #2 DOOR STOP. CORRECTIVE ACTION: REF ERA 601567-14. (2404227)SDR ASAA2022091140108Skin · corrodedFUSELAGE SKIN AROUND VACUUM LAV EXHAUST VENT AT FS917 IS CORRODED. GROUNDED - YES. DAMAGE FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE AND REPAIRED SKIN IAW B737-900 SRM 53-70-01-2R-3 THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 77,931 TOTAL FLIGHT CYCLESDR IPXA2022100386780Skin · corrodedINSPECTION TYPE:3CEMPENNAGE THRU ACCESS 311 INSIDE AREA UPPER FWD COMP L/H SIDE FUSELAGE SKIN HAS CORROSION NEAR AT NUT PLATE AT BETWEEN STA 1986.798 CANT STA 2014.982 AND BETWEEN L10L - L11L .REMOVED, REPAIRED CORRODED AFT SKIN BETWEEN STA 1986.798 AND CANT-SDR F3LA2022091300102Skin · corrodedFOUND CORROSION AFT OF R2 DOOR, BY LAV VACUUM EXHAUST PORT - (AC TO FERRY TO AIRBORNE FOR REPAIRS). REPAIRED LAV VENT HOLE SKIN IAW A320 SRM 53-41-11-300-004. REF PEMCO NR 13027-0010. ORIGINAL SUBMISSION DATE: 09/13/2022SDR DALA2022091406133None · noneSHIP 654 SEVERAL DENTS (4 E/A) ON EXTERNAL FUSELAGE SKIN, BTW STA. 600 AND STA. 660, AND BTW S-19L AND S-16L. CORRECTIVE ACTION: SUMMARY OF NRC 00027 DENTS BTW STA. 600 AND STA. 640, WERE APPROVED AS PERMANENT REPAIRS PER ER/A 548936-14 REV ORIG AND ER /A 6013SDR DALA2022091406097None · noneSHIP 654 AA (AD) 37 FASTENER HOLES DAMAGED BY MISDRILLING IN REFERENCE CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00617 : 37 FASTENER HOLES DAMAGED BY MISDRILLING WERE REPAIRED PER ERA 601567-14AD REV. ORIGINAL AND PRI 601567- 14AD REV 5. (2404452)SDR DALA2022091306080None · noneDENT ON EXTERNAL SKIN LOC AT LEVEL FR27 TO FR28 BTW STRG 35 STRG 36 LH SIDE LOWER FUSELAGE (REFERENT TO LOG PAGE 5071925). PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOC AT LEVEL FR27 TO FR28 BTW STRG 35 STRG 36 LH SIDE LOWER FUSELAGE AS PER SRM A321 53-21-11SDR SWIA202266450Skin · dentedTRANSFER FROM EAML 990088 : RAMP CREW INFORMED MAINTENANCE ,THEY FOUND A DENT ON FUSELAGE NOSE SECTION LEFT SIDE ABOUT 1 INCH, SHOWN TO MAINTENANCE TEAM. DENT HAS BEEN DETERMINED TO BE A MAJOR REPAIR PER GMM 3-26 . FORM M-337 WILL BE REQUIRED. (FILED CLOSEDSDR FDEA202209102718Skin · not reportedCENTER SKIN SECTION NEEDS REMOVED FROM FR78.5 TO FR72 STRINGER 52L TO 52R REPLACED CENTER SKIN SECTION FROM FR72 TO FR80 STRINGER 51L TO 51R IAW E.A. 6-5330- T0370451 PART 2 STEPS 11 AND 12. THIS IS A MAJOR REPAIR. SEE JPF FOR WORK STEPS. SEE N95 FOR INSTALSDR SWAA2022092751990None · crackedCRACK ANGLE - CLIP LOCATED BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-441639 / [01] REPLACED ANGLE - CLIP LOCATED BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 9 REV: A;[02] REPLACED ASDR DALA2022091306070None · none(LOG 2402593) DURING INSPECTION FOUND EXISTING REPAIR DOUBLER ON CROWN SKIN DURING VIASAT INSTALL. REPAIRED PER ERA 602131-14.SDR SWAA2022092051751Gusset · crackedGUSSET CRACKED BS 500D STR 19L / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP#9.<BR><BR>VERIFIED SRM 51-10-02 IS APPLICABLE FOR REPAIR.<BR><BR>REMOVED GUSSET CRACKED AT BS500D STR.19SDR SWAA2022092051752Gusset · crackedGUSSET CRACKED BS 500D STR 19R / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PAT IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP#9.<BR><BR>VERIFIED SRM 51-10-02 IS APPLICABLE FOR REPAIR.<BR><BR>REMOVED GUSSET CRACKED AT BS 500D STR.19SDR DALA2022091306074None · noneSHIP 3331 PLEASE ACCOMPLISH ER/A 599049-14 REV A, SECTION III: ONE-TIME INSPECTION. CORRECTIVE ACTION: REFERENCE ER/A 599049-14. (2401463)SDR DALA2022091206037None · none(LOG 2401631) DURING INSPECTION FOUND FUSELAGE / SKIN / NEAR STA 420, BETWEEN S-21L TO S-22L / DENT. REPAIRED PER ERA 602049-14.SDR DALA2022091206036None · none(LOG 2401835) DURING INSPECTION FOUND DAMAGED HOLE WHILE ACCOMPLISHING ERA 602068-14 REV ORIG EXTERNAL SKIN REPAIR LOCATED ON I/B SIDE OF FUSELAGE SKIN ATTACH HOLE ALONG STR 27R AT 3RD HOLE FWD OF STA 767. COMPLIED WITH STRINGER 27R OVERSIZE HOLE ERA 602133-14SDR FDEA202209082248Doubler · crackedREFERENCE TO SNRM # N01369 HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON ACCESSED FASTENER HOLES WITHIN THE AREA OF THE REMOVED NCA6244-3 DOUBLER FOOTPRINT AREA AT STATION 595 AND FOUND 03 EACH HOLES WITH CRACK INDICATION. FUSELAGE - MASDR IXXA2022101303Skin · corrodedSKIN BULGE AT SKIN SPLICE AT BS 1740 BELOW STR 25L SPOTS OF CORROSIONSDR SWAA2022092651401Angle · crackedCRACK ANGLE LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT 2022-493563 / [01] TOOL USED POWER PACK P/N:FMK0003223;S/N:PE0412/63335;DUE DATE:26-JAN-23.MULTIMETER P/N:FLUKE-37;S/N:5335022;DUE DATE:04-DEC-22;THERMOMETER P/N:FLUKE 566;S/N:AE-405697;DUE DATE:30SDR SWAA2022092278332Web · crackedCRACK WEB LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT 2022-493562 / [01] REPLACED WEB AND FASTENERS LOCATED BTW STA 500D TO STA 520 AT STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9. AND DWG#143A7902 REVSDR SWAA2022092278333Angle · crackedCRACK ANGLE LOCATED STA 500D AND STR 28L FWD CARGO COMPARTMENT 2022-493563 / [01] TOOL USED POWER PACK P/N:FMK0003223;S/N:PE0412/63335;DUE DATE:26-JAN-23.MULTIMETER P/N:FLUKE-37;S/N:5335022;DUE DATE:04-DEC-22;THERMOMETER P/N:FLUKE 566;S/N:AE-405697;DUE DATE:30SDR DALA2022090906013None · none(LOG 2400320) WHILE IN LGA, DAMAGE WAS FOUND ON BOTH THE FWD AND AFT NATS AIRPHONE ANTENNAS. FOLLOWING ANTENNA REMOVAL, CORROSION WAS FOUND AND REMOVED FROM THE UNDERLYING AFT LOWER SKIN PANEL (P/N 146A3231-21) AT BOTH ANTENNA MOUNTING LOCATIONS (STA 757.48 & SDR DALA2022090906006None · noneSHIP 180 ERA 594309-14REV A ISSUED FOR SKIN REPAIR AT STA 1451, S-19L. FO LLOW ON INSPECTIONS ARE REQUIRED. CORRECTIVE ACTION: ACCOMPLISH ERA 594309-14 REV A AT OR BEFORE 37500 TOTAL FLIGHT C YCLES, THEN EVERY 3000 FLIGHT CYCLES THEREAFTER. (2399756)SDR AALA202209219734Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND ON SKIN LOCATED ON HORIZONTAL STABILIZER AT STABILIZER STATION 101.90. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED ON STA 101.90 LOWER SURFACE ON LEFT HORIZONTAL STABILIZER PER 51-10-01-2R-11.SDR DALA2022091206047None · noneSHIP 654 REFERENCE ER/A 601397-14 FUSELAGE SKIN / UPPER SKIN / BTW STA 640 & STA 660 AND BTW S-17 & S-19L / DENT. CORRECTIVE ACTION: REF ERA 601397-14. (2398210)SDR DALA2022090805994None · noneSHIP 1701 RIGHT SIDE LOWER EXTERNAL SKIN DAMAGED ALONG STR 37R BETWEEN STA 1205 AND 1213, CORRECTIVE ACTION: FABRICATED REPAIR PART PER B767 SRM 53-00-01-2R REPAIR 1. INSTALLED REPAIR PARTS PER B767 SRM 53-00-01-2R REPAIR 1 (2398602)SDR AALA202212079220Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN PANEL AT THE BOTTOM EDGE OF THE LAVATORY DISCHARGE VENT. BETWEEN FR 69 AND FR 70, BETWEEN S31R AND S32R. REPAIRED FUSELAGE SKIN PANEL PER EA 338951 AND SRM 53-41-11-300-004.SDR DALA2022091306072None · none(LOG 2397370) DURING INSPECTION FOUND FUSELAGE / SKIN / FS727G-727H, S-2L - S-2R ALTERNATE FASTENER PATTERN. REPAIRED PER ERA 602078-14.SDR SWAA2022091250648Support · crackedCRACK CLAMP SUPPORT ON VERTICAL ANGLE LOC STA 500C LBL 25 AT FWD CARGO COMPARTMENT 2022-447795 / [01] REPLACED CLAMP SUPPORT ON VERTICAL ANGLE LOC STA 500C LBL 25 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 STEP 9;[02] TASK COMPLETEDSDR ASAA2022090639894Skin · corrodedREF DEFECT 60413749 CORROSION FOUND ON SKIN AT LAV VENT HOLE. GROUNDED - YES. DAMAGE FOUND TO BE 100% THRU, CUT OUT DAMAGE & REPAIRED SKIN IAW B737-800 SRM 53-70-01-2R-3 THIS IS A CAT B REPAIR WITH AN INSP THRESHOLD OF 67, 260 CYCLES TOTAL & 5,000 CYCLE INTERVSDR DALA2022090906016None · noneSHIP 654 ET- DR L1 CUTOUT (GR 2) , 757-REPAIR DBL, TRP AND QDR / RII / NDT ; SECTION 02. CORRECTIVE ACTION:IN REFERENCE CARD 5331-01232-02H, REPAIR WAS COMPLETED. (2396893)SDR CALA2022090702305None · crackedA3NB-27-3-6001 LH LATERAL AVIONICS BAY AREA FR 16 WASTE TUBE SUP PORT BRACKET NEAR STR 32L IS CRACKED ON AFT SIDE OF FRAME. REMOVED, FRABRICATED AND REPLACED MOUNT IAW SRM 51-42-11, D53916 787. EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBISDR SWAA2022100382581Access Panel · erodedEROSION ACCESS PANEL 193AR AT LOWER FUSELAGE 2022-488810 / [01] TOOL USED CALIPER P/N 500-197-30 S/N 15120589 DUE DATE 28 NOV 22;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196021 DUE DATE 16 JAN 23;[03] TOOL USED SCALE P/N CL5000 S/N AE-39087 DUE DATE 20 SDR FDEA202209052205Skin · dentedLEFT SKIN BETWEEN STATION 595 TO 615 AND LONGERON 37 AND LONGERON 46 FOUND DENT. REPAIR CARRIED OUT AS PER EA NUMBER: 1-5330-T0370337 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. ORIG SUB DATE: 9/6/2022SDR FDEA202209042699Skin · deformedSKIN DEFORMATION AT FR 77 AT STR 47R (MEASURED 0.142? TO 0.172?) REPAIRED SKIN DEFORMATION AT FR76 AND FR77 STRINGER 47R IAW EA 6-5330-T0370451 PART 2 STEPS 13 AND STEP14. THIS IS A MAJOR REPAIR.SDR SWAA2022100379016Gusset · crackedCRACK GUSSET LOCATED BS 500D AND STR 19R FWD CARGO COMPARTMENT 2022-488770 / [01] REPLACED GUSSET LOCATED AT BS 500D AND STR 19R FWD CARGO COMPARTMENT; IAW B737-700 SRM 51-40-02; AND DWG# 143A7902. REV. ?-?. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSET LSDR SWAA2022100379013Gusset · crackedCRACK GUSSET LOCATED BS 500D AND STR 19L FWD CARGO COMPARTMENT 2022-488768 / [01] REPLACED GUSSET LOCATED BS 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSSDR SWAA2022100350237Gusset · crackedCRACK GUSSET LOCATED BS 500D AND STR 19L FWD CARGO COMPARTMENT 2022-488768 / [01] REPLACED GUSSET LOCATED BS 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSSDR DALA2022090705971None · noneSHIP 3324 LOADING CREW REPORTED SCRATCH IN PAINT AND SCUFF ON EDGE OF DOOR CUT OUT FWD CARGO DOOR. CORRECTIVE ACTION: FOUND EDGE SCUFF ON FR 25A, BETWEEN STGR 40-41RH. REWORKED PER A330 SRM 53-21-11. IN LIMITS REQUIRES GVI REINSPECT EVERY 5200FC PER 51-90-00, SDR FDEA202209032708Skin · deformedSKIN DEFORMATION AT FR 77 AT STR 47L (MEASURED 0.082? TO 0.087?) REPAIRED SKIN DEFORMATION AT FRAME 76.5 TO FR77.5 STRINGER 47L TO 51L IAW EA 6-5330- T0370451 PART 2 STEPS 15,10 REF FIGURE 3 OF 3 FOUND IN STEPS 3. SEE N109 FOR EDGE SEALING AND PAINT SEE JPFSDR SWAA2022100645341None · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26L WL153. MARKED / [01] VERIFIED THE APPLICABILITY OF SRM 53-00-03-2R-1 REPAIR 1;[02] CUT AND REMOVED THE DAMAGED PART OF STRINGER 26L BETWEEN BS 500D +11 TO BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1 . AND UPDSDR SWAA2022100645342None · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED / CUT AND REMOVED THE DAMAGED PART OF STRINGER 26R BETWEEN BS 500D+11' AND BS 540. AND UPDATED STEPS 2 AND 3 RECEIVED NEW REPLACEMENT STRINGER SECTION FROM O.S.S AFTER BEING FORMED AND FABSDR SWAA2022100649921None · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26L WL153. MARKED / [01] VERIFIED THE APPLICABILITY OF SRM 53-00-03-2R-1 REPAIR 1;[02] CUT AND REMOVED THE DAMAGED PART OF STRINGER 26L BETWEEN BS 500D +11 TO BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1 . AND UPD
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