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 SWAA2022013158219Skin · wornSUPPLEMENTAL INFORMATION: CROWN SKIN WEAR UNDER DORSAL FIN STATION 847 TO 878 BETWEEN STR. 2L AND 2R. ; / [01] OK TO INSTALL REPAIR PARTS; [02] REPAIRED CROWN SKIN DAMAGE UNDER DORSAL FIN AT BS 847-878; STR 2L - 2R PER EA 22-153-00030.; [03] VERIFIED CORRECTIVSDR SWAA2022021458017Bracket · brokenBROKEN BRACKET ASSY INSULATOR LOCATED BS344 TO BS727 AND BETWEEN STR10R TO STR15R AT PASSENGER CABIN (8 EA) ; 2021-585095 / [01] REPLACED BRACKET ASSY INSULATOR LOCATED BS344 TO BS727 AND BETWEEN STR10R TO STR15R AT PASSENGER CABIN (8 EA) IAW B737-700 SRM 51-4SDR SWAA2022021458018Bracket · brokenBROKEN BRACKET INSULATOR LOCATED BETWEEN BS578 TO BS727 AND BETWEEN STR10L TO STR15L AT PASSENGER CABIN (6 EA) ; 2021-585094 / [01] REPLACED BRACKET INSULATOR LOCATED BETWEEN BS578 TO BS727 AND BETWEEN STR10L TO STR15L AT PASSENGER CABIN (6 EA) IAW B737-700 SRSDR IPXA2022012078063None · noneINSPECTION TYPE:1CFORWARD FUSELAGE COCKPIT FLOOR CRACK STA. Y=360 BETWEEN X=5.25 AND X=-13.25.REPAIRED CRACKED COCKPIT FLOOR STA. Y=360 BETWEEN X=5.25 AND X=-13.25 IAW SRM 53-10-51 REPAIR 1 FIG 202 REV 68.01 (MAJOR).SDR SWIA202263365None · noneREFERENCE ML/CP 24108715 FOR ORIGINAL DISCREPANCY. PUNCTURE AND DENT DAMAGE ON LHS FUSELAGE BETWEEN FS 394.00-FS409.00 AND STGR 15L AND STGR 16L. THIS IS CLASSIFIED AS A MAJOR REPAIR. GENERATED FORM M-337. (FILED - CLOSED) COMPLIED WITH REPAIR ON LH FUSESDR MASA20220104008None · dentedTHE LOWER FUSELAGE SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-003-A02, FIG. 53-61-01-991-806, ITEMS 1 AND E (REV.37 DATED 15 AUG 2019). DEFECT LOCATION: FS 1015.00 - FS 1031.00 AND STGR, 23L - STGR. 24LSDR MASA20220104007None · noneTHE FUSELAGE SKIN WAS FOUND WITH A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-01-001-007-A01, FIG. 53-21-01-991-808, ITEMS 1A AND D (REV. 33 DATED JUN. 25, 2017). DEFECT LOCATION: FS 421.00. FS 437,00 AND STGR 19R. STGR 20RSDR HNAA2022010400043None · noneE894729 - #3 R/H OVER WING BRACKET HAS MISSED DRILLED HOLE ON SKIN BETWEEN FR 49-50 STRINGER 14R-13R ... REPAIRED #3 R/H OVER WING BRACKET HOLE ON SKIN BETWEEN FR 49-50 STRINGER 14R-13R BY INSTALLING BUSHING IAW ETD2021-145-042169 AND PIEDMONT EO1-53-21-0354.SDR SWAA2022010757976None · crackedSUPPLEMENTAL INFORMATION: FWD CARGO STRG 25L BETWEEN STA500 AND STA500A FOUND BAFFLE SUPPORT CRACK AT UPPER RADIUS ; / [01] REMOVED AND REPLACED BAFFLE AT FWD CARGO COMPARTMENT STRG 25L BETWEEN STA 500 AND STA 500A IN REF SRM 51-40-02-OG-0; [02] VERIFIED STEP SDR IPXA2022012078056Skin · damagedINSPECTION TYPE:1CFUSELAGE NOSE LWR SKIN E&E BAY JAMB SKIN AND PAN HAS DENT AT STA. Y=348.00 & X=14.812.REPAIRED DAMAGED FUSELAGE NOSE LWR SKIN E/E BAY JAMB SKIN DOUBLER AND PAN AT Y=348.00 AND X=14.812 IAW VT-SAA EA011-5300-01-A94522 REV I/R AND UPS EO MD11-5SDR MASA20220103005None · noneTHE FUSELAGE SKIN WAS FOUND TO HAVE 5 EACH DENTS. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-21-01, FIG. 53-21-01-991-808, ITEM 1A (REV. 38 DATED 25 JUL. 2020).SDR MASA20220103004None · noneTHE FUSELAGE SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-004-A02, SRM 53-61-01-101-004-A02 STRUCTURAL IDENTIFICATION, AND ALLOWABLE DAMAGE. DEFECT LOCATION: FS 1051.3-FS 1069.75, STRG. 19R - STRG. 20RSDR MASA20220103003None · noneTHE FUSELAGE SKIN WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-11-01-001-004-A01, REFERS TO SRM 53-00-01-101-A01 FOR STRUCTURE IDENTIFICATION AND FUSELAGE SKINS AND PLATING, ALLOWABLE DAMAGE.SDR IPXA2022010277467Skin · noneINSPECTION TYPE:N/AHOLE IN FUSELAGE SKIN AT FR 20 S-33RREPAIR IN ACCORDANCE WITH A300-5330-82455-ASDR MK1Y202201011Tear Strap · corrodedTEAR STRAP, INNER SKIN, STA 544, S-1R AND S-4R, DOOR SURROUND ZONE: SHOP DISCOVERED DEEP CORROSION ON TEAR STRAP EDGE COMMON TO S-2R (LAP SPLICE). THE DAMAGED AREA IS LOCATED IN CONVERSION INSTALLATION ZONE.SDR ASAA2022010137087Skin · dentedON WALKAROUND, PILOT REPORTED DENT, RH SI DE OF FUSELAGE BELOW R1 DOOR CUTOUT STA 312 BETWN STR 21-22. DIMS MEASURED AT: 0.075" D X 2.0" L X 3.0" W. COMMON TO FRAME AT STA 312. OUT OF SRM LIMITS, REQUIRED REPAIR. GROUNDED - YES. ACCOMPLISHED SRM REPAIR PER B73SDR DALA2022010400081None · noneSHIP 6822 CORROSION ON DOUBLER BELOW SIDE PANEL AT LBL 16.10 AND STA 1530 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00447. DOUBLER BELOW SIDE PANEL AT LBL 16.10 AND STA 1530 IN AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2072035)SDR DALA2022010300036None · noneSHIP 5811 ON WAKE UP WALK AROUND FOUND AFT LAV SERVICE PANEL CORROSION AROUND OUTER EDGE POPPING THRU SEALER AND PAINT. CORRECTIVE ACTION: REPAIRED PER ERA 596269-14 REV ORIG. (8145715)SDR DALA2022010300013None · noneSHIP 3248 DENT EXTERNAL SKIN ON DOUBLER REPAIR LOCATED AT FR74 AND BTW STR 30R TO STR 31R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A #496943-14 REV.B. (2070969)SDR DALA2022010300010None · noneHIDDEN DAMAGE DURING THE DOUBLER REMOVE PROCESS. WEB DAMAGE WAS FOUND ON LEFT HAND SIDE, LOCATED ON INTECECTION STA 674 AND STGR 18LH. SUMMARY OF NRC 00175: WEB ON STA 674 LH WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4. (LP #2071146)SDR SWAA2022013157260None · crackedCRACK INNER CHORD LOCATED AT BS 294.5 AT RBL 50 AND WL 208.1 AT FWD GALLEY AREA ; 2021-577502 / [01] TOOL USED CALIPER P/N:500-197-30 S/N:A21143464 DUE DATE:16-OCT-22.; [02] REPLACED INNER CHORD LOC AT BS 294.5 AT RBL 50 AND WL 208.1 AT FWD GALLEY AREA. IAW B7SDR SWAA2022013157208Angle · deformedFWD CARGO SMALL TRANSITION ANGLE JUST FWD OF DOOR CUTOUT IS DEFORMED AFT END.(MARKED) ; / [01] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01; [02] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01.<BR>INSPECTION C/W.; [03] INSTALLED PER SRMSDR DALA2022010300040None · noneSHIP 5811 CORROSION FOUND ON INTERCOSTAL ON TOP OF LAV PAN IN THE FWD INBD CORNER. THREE SPOTS. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 002-0001:0514-2001/00900009 REPAIRED INTERCOSTAL PER ERA 596280-14 REV. ORIG. (2070169)SDR DALA2022010308208None · noneSHIP 5811 CORROSION DAMAGE DISCOVERED COMMON TO THE FUSELAGE SKIN IN THE VICINITY OF THE AFT LAVATORY SERVICE PANEL CUT-OUT. FUSELAGE SKIN REPAIR ADDRESSED IN ER/A 596269-14. FOLLOW ON ACTION REQUIRED. CORRECTIVE ACTION: DOUBLER/TRIPLER REPAIR INSTALLED IN THESDR CALA2021123002485Fastener · missingPDA 3 FASTENER MISSING ON PANEL 191KB OUTBOARD SIDE 4 FROM THE AFT. SEE LOGPAGE 7715638 FOR DIP. PER LP 7715638 OK TO CARRY FO 30 F/C''S PER AMM 53-35-00-200-002, REQUIRES INSPECTION EVERY 10 F/C''SSDR SWAA2022021457098None · crackedCRACK CLIP LOCATED ON AFT FACE BS 500C AT LEVEL STR 26R AT FWD CARGO COMPARTMENT ; 2021-576210 / [01] REPLACED CLIP LOCATED ON AFT FACE BS 500C AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG DWG 143A7505 SHEET 10 REV A. SEE SDR SWAA2022021457094None · crackedCRACK CLIP LOCATED ON FWD FACE BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT ; 2021-576209 / [01] REPLACED CLIP LOCATED ON FWD FACE BS 500B AT LEVEL STR 26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND B737-700 SRM 51-40-02 AND DRAWING 143A7505 RSDR SWAA2022021456854Gusset · crackedCRACK ANGLE - SUPPORT GUSSET LOCATED ON BS 500D AT LEVEL STR 21L AT FWD CARGO COMPARTMENT ; 2021-576199 / [01] REPLACED SUPPORT GUSSET LOCATED ON BS 500D AT LEVEL STR 21L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902; [02] REPLACEDSDR SWAA2022021456855Gusset · crackedCRACK ANGLE - SUPPORT GUSSET LOCATED ON BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT ; 2021-576200 / [01] REPLACED ANGLE SUPPORT GUSSET AND FGASTENERS LOCATED ON BS 500D AT LEVEL STR 19R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 ANDSDR SWAA2022021456851Gusset · crackedCRACK ANGLE - SUPPORT GUSSET LOCATED AT BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT ; 2021-576198 / [01] REPLACED ANGLE SUPPORT GUSSET LOCATED AT BS 500D AT LEVEL STR 19L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SSDR WX0A1900010073984None · noneNRC 1000-0014: 031-4 DURING ACCOMPLISHMENT C/W EO E5331-0006 AND REFERING TO AD 2018-06-04, CRACKS FOUND AND EXTEND OUT OF REPAIR ZONE LIMIT AT LH AIR CONDITIONNING BAY AREA OF FRAME 36 PRESSURE PANEL AND LONGITIDINAL BEAM AT Y1292. / LH AIR CONDITIONING BASDR DALA2021123008171None · none(LOG 2068576) DURING INSPECTION FOUND CRACED VAPOR BARRIER ON RH WING CENTER SECTION REAR SPAR , BULKHEAD STA 663. CRACK OF 2.755 IN LENGTH ON VAPOR BARRIER ON RH WING CENTER SECTION REAR SPAR , BULKHEAD STA 663 WAS REPAIRED PER B737-800 SRM 57-10-10-2R PROCEDSDR DALA2021123008170None · none(LOG 2068491) EXTERNAL POWER RECEPTACLE WAS REPAIRED PER B737-800 SRM 53-10-15-2R PROCEDURE 5, REPAIR 5.SDR DALA2024031103213Skin · damagedRH FUSELAGE WINDOW BELT WINDOW #12 AT STA 446-465 HAD A LIGHTNING STRIKE. FOLLOW ON ACTION REQUIRED. ERA 596251-14 ISSUED. FOLLOW ON ACTION REQUIRED SECT I TBA DURING C-CHK VISIT IN MSP DEC2021. SECT II HFEC INSPECTIONS TBA AT EVERY 24 MONTH INTERVALS AFTER SESDR SWAA2021123056728Doubler · crackedEXTERNAL POWER CUTOUT LOWER DOOR LATCH BLOCK ATTACH POINT CRACKED ; / [01] CUT-OUT DAMAGE AT EXTERNAL POWER CUTOUT LOWER DOOR LATCH BLOCK ATTACH POINT IAW SRM 53-10-15-2R-4 REPAIR 4 STEP(4); [02] VERIFIED NEW DOUBLER MATERIAL AS 2024-T3-.050/ ALSO VERIFIED NEWSDR DALA2021122808084None · none(LOG 2066142) DURING INSPECTION FOUND FWD ELECTRONIC BAY, DRAIN MAST BASE SHOW SIGNS OF CORROSION. REPAIRED REF B717 SRM 53-01-01 AND B717 DRW # 9923686 .SDR DALA2021122808108None · none(LOG 2065320) DURING INSPECTION CRACK WAS FOUND AND DELIMITED WITH A MEASURE OF 0.250 IN LENGTH AT PREVIOUS BLEND OUT LOCATED AT FUSELAGE SKIN STA.500E+1" AND S-21 RH AND 22 RH.SDR MK1Y20211226003None · noneDURING MAINTENENCE INSPECTION FOUND SCRATCH DAMAGE ON FUSELAGE SKIN, STA 412 TO STA 434, STR 32L TO STR 33L.SDR MK1Y20211226002None · noneDURING MAINTENENCE INSPECTION FOUND BLENDOUT AND DENT ON FUSELAGE SKIN AT STA 1417 BETWEEN STR 26L AND STR 34L.SDR MK1Y20211226001None · noneDURING MAINTENENCE INSPECTION FOUND TWO ADJACENT BLENDOUTS AT STA 256 TO STA 303, STR 28R TO 30R.SDR DALA2021122808107None · none(LOG 8202900) DURING INSPECTION FOUND ELECTRICAL ARC DAMAGE 3FT AFT OF L1 DOOR AT LAP JOINT -ARC CAUSED DUE TO POWER CORD INSTALLED UPSIDE DOWN + ENERGIZED AIRCRAFT ARCED TO AUTO LEVEL ARM ON JETWAY. MAINTENANCE REPAIRED DAMAGE PER ERA 596192-14.SDR FDEA202112243138None · noneFUSELAGE EXTERNAL SKIN, STA 460 STR28R, HAS 2EA DEEP GOUGES ACCOMPLISHED FEDEX EA# F-5330-T0365972-P1: FUSELAGE - PLATES AND SKIN - STA 456, S- 27R - S-28R, GOUGES, DOUBLER REPAIR.SDR SWAA2022020755872Support · crackedMAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED BELOW FLOOR PANEL @ LBL-1.5 STA 540 MKD DOT ; / [01] REMOVED AND REPLACED FLOOR SUPPORT ( BREAK PANEL ASSY) AT MAIN CABIN STA 540 LBL1.5 PER B737-700 SRM 51-40-02-0G-0 AND DRWG # 143A0060.; [02] CERTIFIED.; [0SDR SWAA2022013155884Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 400 AND BS 420 STRINGER 25L FWD CARGO COMPARTMENT ; 2021-577407. REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS 400 AND BS 420 STRINGER 25L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM B737-700 51-40-02SDR SWAA2021123055826Skin · crackedEXTERNAL POWER DOOR CUTOUT FRAME SKIN CRACKED AND BROKEN AT LOWER LATCH BLOCK ; / [01] VERIFIED MATERIAL; -2 DOUBLER 2024 T3 .050' ATAG A34144; -3 FILLER 2024-T3 .040' ATAG A12631 IAW SRM 53-10-15-2R-4 TABLE 201.; [02] VERIFIED STEP 1; [03] CUT AND REMOVED DAMSDR DALA2021122808113None · noneER/A 595953-14 SECTION I WAS ISSUED FOR FUSELAGE SKIN DAMAGE AT THE AFT FRAME OF THE BULK CARGO DOOR OPENING. SECTION I WAS ACCOMPLISHED DURING SPECIAL VISIT IN MSP 10DEC21 ON N/R 8. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II PERMANENT REPAIR WITHIN 2SDR SWAA2022011855694None · crackedFWD. CARGO COMPT. INTERCOSTAL/BAFFLE HAS CRACKED FWD. CLIP AT BS 400; LBL 21;(143A7502-5) ; / [01] REMOVED CLIP AT FWD CARGO COMPT. INTERCOSTAL/ BAFFLE IAW B737-700 SRM 51-40-02-0G-0; [02] LOCATED HOLES AT NEW CLIP. IAW B737-700 SRM 51-40-05-0G-0; [03] VERIFIESDR DALA2021122808111None · noneWHILE JACKING A/C FOR NOSE STRUT SERVICING, JACK FAILED AND DAMAGED SKIN @ FR 8, 10.5" R/H OF CENTER LINE NEAR EXTERNAL POWER RECEPTACLE. REPAIRED DAMAGED SKIN @ FR 8, 10.5" R/H OF CENTERLINE NEAR EXTERNAL POWER RECEPTACLE PER ERA 595840-14. REPAIR APPROVAL ISSDR DALA2021122708053None · noneSHIP 670 CONTACT LIAISON ENGINEERING.ADDITIONAL ENGINEERING DOCUMENTATION APPROVED AS AN AMOC TO AD 2019-07-04,MAY BE REQUIRED BEFORE FURTHER FLIGHT. STA. 570 S-14L. CORRECTIVE ACTION: THIS REPAIR MEETS THE REQUIREMENTS OF AD 2019-07-04 AND SB 757-53A0111 AS PSDR DALA2021122207981None · noneSHIP 3248 TOOLING DAMAGE ON AFT SIDE OF SKIN CLIP, BETWEEN FRAMES 73 AND 74, BETWEEN STRINGERS 34 AND 33L. CORRECTIVE ACTION: REPLACED CLIP PER A320 SRM 51-72-11. (2060599)
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