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 DALA2023072405961Unknown · unknownSHIP 3355 DURING ACCOMPLISHMENT OF EM 5330-01152, FASTENERS THAT ATTACH THE FR 84, 85, 86, AND 87 REINFORCEMENT ANGLES (LEFT HAND SIDE) CANNOT BE INSTALLED AS THE TAIL OF THE FASTENER IS TOO CLOSE TO THE FASTENERS INSTALLED THROUGH THE SKIN. THE AFFECTED LOCATSDR SWIA2023072101Unknown · dentedTRANSFER FROM EAML 1176225 : EXT AIR START PANEL DOOR DISCOVERED OPEN ON TAXI IN, SEE EAML 1175774.TWO (2) DENTS (1.20" L X 1.00" W X 0.0375" DEEP & 2.10" L X 1.70" W X 0.0725" DEEP) TO LOWER FUSELAGE SKIN (DWG 601R35005, AL ALLOY CLAD 2024-T42, 0.036"+/-0.002SDR CALA2023072102297Skin · damagedAC DAMAGE BELOW R1 DOOR FWD FUSELAGE. PUNCTURE HOLE. REQUIRES SHEET METAL. CUT OUT DAMAGED SKIN AND REQUIRES HFEC AROUND CUT OUT, REF SRM PERFORMED HFEC AROUND CUT-OUT, REF PART 6, NDT 51-00-01. NO 53-00-01-2R-14, STEP 4, NDT PART 6, 51-00-01. INDICATION NOTEDSDR SWAA2023081780484Access Panel · delaminatedDELAMINATED WING TO BODY FAIRING ACCESS PANEL 193B INTERNAL AREA AT MAIN WHEEL WELL COMPARTMENT 2023-447751<[01] TOOL USED= CALIPER P/N: 500-196-30; S/N:A20231600; DUE DATE: 12-SEP-23;[02] TOOL USED= HOT BONDER P/N: HCS9200B; S/N: 18165044; DUE DATE: 26-MAR-24SDR DALA2023072405939Unknown · unknown(LOG 2874072) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN STA 679 TO STA 706 BETWEEN S1 AND S-2R. C/W ER/A 610200-14 REV ORIGINAL.SDR DALA2023072405938Unknown · unknown(LOG 2874064) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN STA 730 TO STA 727B BETWEEN S1 AND S-2R. C/W ER/A 610223-14 REV ORIGINAL.SDR IPXA2023071993694Skin · crackedINSPECTION TYPE:N/A*MAJOR REPAIR* RT SIDE AIR CONDITIONING DOOR JAMB CORNEWR SKIN CRACKEDREPAIRED IAW EO# MD11-5330-87120-BSDR REXA2022071900508Skin · corroded"FRAME AT FS.847.00+16.00 IS CORRODED BETWEEN STR.26R AND STR.26L. REPLACED FRAME SECTION AT FS 847+16"" FROM STR 25L TO 25R IAW CRJ900 SRM 53-00-06-201-001-A03."SDR MK1Y20230719003Unknown · unknownL/H WING, LOWER SKIN, CORROSION DAMAGE WAS FOUND ON THE LOWER SKIN PANEL (P/N 112T4703-1) AROUND FUEL SUMP DRAIN VALVE HOLE BETWEEN STRINGERS L-11 AND L-12 NEAR SIDE OF BODY.SDR DALA2023072405937Unknown · unknown(LOG 2872786) DURING INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE EXTERNAL SURFACE OF THE FUSELAGE CROWN UPPER SKIN BETWEEN APPROX. BS 678 AND BS 702, STR S-1 AND S-2R. REPAIRED CORROSION PER ERA 610200-14.SDR DALA2023072405935Unknown · unknown(LOG 2872766) DURING INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE EXTERNAL SURFACE OF THE FUSELAGE CROWN UPPER SKIN (PN 146A3101-38), BETWEEN APPROX. BS 727+16 AND BS 727A+17, STR S-1 AND S-2R. REPAIRED CORROSION PER ERA 610223-14.SDR DALA2023072405934Unknown · unknown(LOG 2872350) DURING INSTALLATION OF THE STRUCTURAL PROVISIONS FOR THE VIASAT RADOME PER AA 4430-01008-01D, SAL REPORTED THAT THEY HAD MISLOCATED A DOUBLER AT FITTING #2 RESULTING IN FASTENERS INSTALLED THROUGH THE CHEM-MILL LINE JUST INBOARD OF S-2R. HOWEVER,SDR IPXA2023071893686Skin · damagedINSPECTION TYPE:CRH LWR FUSE BELOW FWD CARGO DOOR REPAIR HAS AN INDICATION STICKING OUYREPAIRED AREA IAW SRM SRM 53-10-12-201SDR DALA2023071805820Unknown · unknownLIGHTNING STRIKE DAMAGE LOCATED ON STATION 1166, LH SIDE OF FUSELAGE. (LABELED #7) COMPLIED WITH ER/A 610530-14 REV ORIG. ALL PRI REVISION INSTRUCTIONS ARE COMPLIED WITH AND MATCH FINALE ER/A 610530-14 REV ORIG SECTION I PERMANENT REPAIR INSTRUCTIONS. FUSELAGESDR JGVR20230718002Unknown · unknownBLENDED CORRODED AREA OF THE EXTERIOR FUSELAGE LH SKIN FORWARD OF THE CABIN DOOR AT FS145 AND WL 107.7, PERFORMED NDT AND SUBMITTED FOR REPAIR DISPOSITION. TREATED, PRIMED, AND TOP COATED REPAIR AREAS PER TEXTRON FIELD REPAIR.SDR DALA2023072005881Unknown · unknown(LOG 2870942) TAIL STRIKE DAMAGE TO LOWER FUSELAGE SKIN BETWEEN STA 844. COMPLIED WITH ER/A 610419-14 REV. ORIG. ALL PRI 610419-14 REVS. 0 THRU 4 ARE COMPLIED WITH AND MATCH FINALE ER/A 610419-14 REV. ORIG.SDR DALA2023072005879Unknown · unknown(LOG 4833910) TAIL STRIKE ON LANDING DURING A BOUNCED LANDING PITCH ATTITUDE. BELLY SKIN DAMAGE BETWEEN STATIONS 847-887. REPAIRED ON NR 2 PER ERA 610419-14 REV ORG. TAIL SKID SHOE REPLACED ON NR 4, REF LOG 4833920. TAIL SKID CARTRIDGE REPLACED ON NR 5, REF LOSDR DALA2023072005878Unknown · unknown(LOG 2871014) CORROSION ON EXTERIOR FUSELAGE SKIN BETWEEN STA727 AND 727C, STR 2R AND 2L. C/W ER/A 610021-14 REV ORIGINAL.SDR CALA2023071902275Skin · corrodedCORROSION ON FUSELAGE BELLY SKIN AROUND BILGE DRAIN JUST AFT OF BS 727J LEFT DRAIN #35. ACCOMPLISHED FUSELAGE BELLY SKIN REPAIR AT BILGE DRAIN STA 727J. REF ECRA 5330-07105, SEE PARTIAL WORK ACCOMPLISHED. TRANSCRIBED FROM AERSALE DOC # 33748 WORK PERFORMED BYSDR DALA2023071705782Unknown · unknownLIGHTNING STRIKE DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L. (LABELED #1) REPAIRED SKIN DAMAGE LOCATED BETWEEN STATION 487 AND STRINGER 28L PER B717 SRM 53-03-01-2R PROCEDURE 1. CLASS II REPAIR ZONE 1. EXTERNAL LFEC OR EXTERNAL ULTRASONIC INITIAL INSPSDR R61A2023073000123Finger Doubler · corrodedFORWARD CARGO DOOR CUTOUT, AT FWD FINGER DOUBLER, A GOUGE, CORROSION, SCRATCHES, AND WEAR MARKS BETWEEN FR 24-27REMOVED AND REPLACED FWD CARGO FWD FINGER DOUBLER REF EMB SRM 51-40-08. SEE ATTACHED WIP'S AND TASKS FOR ADDITIONAL WORK ACCOMPLISHEDSDR AALA202307184074Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FUSELAGE SKIN SURROUND FOR EXTERNAL POWER ACCESS DOOR LOCATED FROM BS 229 TO BS 235 AND FROM S19R TO S20R. REPAIRED SKIN PER SRM 53-10-15-2R PROCEDURE 4 REPAIR 4.SDR DALA2023071705781Unknown · unknownCORROSION ON PLATE IN STA Y=1053 BTW LONGERONS 29R-29L AT AFT BULKHEAD AT AFT CARGO COMPARMENT. SUMMARY OF NRC 203: LEVEL CORROSION 2. DOUBLER (PLATE) WAS REPLACED PER B-717-200 SRM 51-41-05-0G AND PER DGW 5910130-61 REV "ET". (LP #2869463)SDR IPXA2023081593918Skin · corrodedINSPECTION TYPE:3C*** MAJOR REPAIR *** MAIN CABIN AFTER REMOVAL OF FLOOR PANEL ON CENTER WING AREA FOUND CORROSION ON L/H TUNNEL AT STA 1239, XCW= 101.8 AND XCW= 108.REPAIRED CORRODED AREA AT THE CENTER WING L/H TUNNEL AT STA XCW=101.8 AND XCW=108 IAW VTSAA EASDR IPXA2023081493899Skin · corrodedINSPECTION TYPE:4CMAIN CABIN AFTER REMOVAL OF FLOOR PANEL CENTER WING AREA FOUND CORROSION AT STRINGER #8 BETWEEN STA XCW=101.8, XCW=108.REPAIRED CORRODED SKIN AREA AT THE CENTER WING ON MAIN CABIN AT STRINGER #8 BETWEEN STA XCW=101.8, XCW=108 IAW VTSAA EA 01SDR DALA2023071705777Unknown · unknownFOUND CRACK IN SKIN TO BE OUT OF LIMITS. COMPLIED WITH PRI 610480-14 AD REV 0. COMPLIED WITH PRI 610488-14AD REV 1 ALL INSTRUCTIONS ON PRI 610480-14AD REV 0 AND REV 1 ARE C/W AND MATCH FINAL ERA 610480-14 REV ORIGINAL. (LP #2866614)SDR CALA2023071702266Skin · unknownFOUND 1 EA LIGHTNING STRIKE ON SKIN AT LHS FR8 Z-339 CREATED BY MEHRDAD PARSA 91105046 60000 FC/120000 FH IAW SRI 53-11-11-205-037 REPAIR EMBODIMENT AT ZONE 1. PERFORMED PERMANENT REPAIR CATEGORY B IAW SRM 53-11-11-3000-041. IT IS NECESSARY TO INSPECT THIS REPSDR HNAA2023080700284Unknown · unknownE986248 REAR FUSELAGE SKIN BUSHING REPAIRS AT FR 77 STGR 4R-5R (LOWER BUSHING), AND STGR 8R-9R. REQUIRE DT INSPECTION IAW EMB 145 SRM 53-32-01, ITEM 10. ACCOMPLISHED DVI ON REAR FUSELAGE SKIN BUSHING REPAIRS AT FR 77 STGR 4R-5R (LOWER BUSHING), AND STGR 8R-9SDR DALA2023071905830Unknown · unknownSHIP 0687 DTE, ER/A 610024-14; FUSELAGE / SKIN / AFT LAV. SERVICE PANEL CUTOUT / STA. 1676 TO 1705, S-26R TO S-29R / CORROSION. CORRECTIVE ACTION: REF ERA 610024-14. (2865570)SDR DALA2023071705784Unknown · unknownSHIP 3118 DENT EXTERNAL SKIN OF EXISTEN REPAIR LOCATED FR 74 TO FR 75 AND STR 33R TO STR 32R LOWER FUSELAGE. CORRECTIVE ACTION: REMOVED AND REPLACED DOUBLER REPAIR LOC ON EXTERNAL SKIN OF EXISTEN REPAIR LOCATED FR 74 TO FR 75 AND STR 33R TO STR 32R LOWER FUSELSDR SWAA2023071779085Skin · crackedEXTERNAL POWER RECEPTACLE LOWER EDGE EXTERNAL LAYER CRACKED REF TSR - 2023005558<[01] GVI DAMAGE AREA AND COMPLIED WITH EA 23-153-02205. ALSO; PERFORMED CONDITIONAL INSPECTION 05-51-59; NO FURTHER DAMAGE NOTED.SDR IPXA2025012106319Skin · ground damagePUNCTURE TO FUSELAGE SKIN BY CARGO VEHICLE FWD OF AFT LOWER CARGO DOOR OPENING, ABOVE CARGO DOOR CONTROL PANEL. ACCOMPLISHED REPAIR I.A.W UPS EO-87620-REQ3 REV.1 REVIEW COMPLETEDSDR DALA2023111709486Unknown · unknownSHIP 179 FOUND CRACK ON LEFT SIDE FUSELAGE FORWARD OF FORWARD STATIC PORT. CORRECTIVE ACTION: COMPLIED WITH B767 SRM 53-00-01-2R PROCEDURE 1 REPAIR 1 FORWARD TO MONITOR CAT B REPAIR, REPETITIVE INSPECTION REQUIRED EVERY 6000 F/C. OK FOR SERVICE (4778186)SDR SWAA2023081681886Access Panel · crackedLEFT FWD O/B FUSELAGE ACCESS PANEL # 193CL HAD BULGING/CRACKED FASTENER HOLES<[01] ALL STEPS COMPLETED.;[02] SUMMARY=PREPARED DAMAGED AREA FOR REPAIR AS MARKED ON PANEL #193CL AS PER B737 SRM 51-70-04-2R-9.<BR>APPLIED REPAIR IN DAMAGED AREA (FASTENER HOLE) ON SDR HNAA2023080700283Unknown · unknownUNDER AFT BELLY PANEL EXTERNAL FUSELAGE STGR 19R REPAIR BTW FR 52--53 NO REPAIR INFO. REMOVED PREVIOUS REPAIR UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STR 19R BTW FR 52-53 WITH NO REPAIR INFORMATION AND REPAIRED STR 19R IAW PIEDMONT EO EO1-53-23-0211 AND EMB 1SDR HNAA2023080700282Unknown · unknownUNDER AFT BELLY PANEL EXTERNAL FUSELAGE STGR 19L PREVIOUS REPAIR IS CHAFED BTW FR 52-53. REMOVED CHAFED PREVIOUS REPAIR UNDER AFT BELLY PANEL EXTERNAL FUSELAGE STR 19L BTW FR 52-53 AND REPAIRED STR 19L IAW PIEDMONT EO1-53-23-0210 AND EMB 145 SRM 53-24-02RE ITSDR IPXA2023071606319Skin · unknown*** SDR FILED OPEN *** PUNCTURE TO FUSELAGE SKIN BY CARGO VEHICLE FWD OF AFT LOWER CARGO DOOR OPENING, ABOVE CARGO DOOR CONTROL PANEL.***SM EVAL REQ*** DEFERRED PER EO 87620- REQ. 1SDR DALA2023071705746Unknown · unknown(LOG 2864641) CORROSION ON EXTERIOR FUSELAGE SKIN BETWEEN STA 663 AND 727, STR 2R AND 2L. C/W ER/A 610008-14 REV ORIGINAL.SDR DALA2023071405737Unknown · unknownAFTER LONGERON 26 LH BTW STA Y=900 TO STA Y=1053 REMOVAL, CORROSION WAS FOUND AT FUSELAGE SKIN BTW STA 1000 TO STA 1006 L-26 LH. SUMMARY OF NRC 00688: CORROSION LEVEL 2. FINGER DOUBLER AT STA 946 TO 1006 LONGERON 26 LH WAS REPLACED PER B717-200 SRM 51-41-02-0GSDR FDEA202307131211Skin · crackedCRACK (APPROXIMATELY 1 INCH) FOUND ON THE FUSELAGE SKIN AT THE RIGHT AIR- CONDITIONING COMPARTMENT UPPER AFT CORNER OF THE DOOR CUTOUT. FUSELAGE - CRACK (APPROXIMATELY 1 INCH) FOUND ON THE FUSELAGE SKIN AT THE RIGHT AIR- CONDITIONING COMPARTMENT UPPER AFT COSDR SWAA2023081477855Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500B TO BS500C AND STR26R AT FWD CARGO COMPARTMENT 2023-413327<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS500B TO BS500C AND STR26R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 SRM 51-10-02 ISDR SWAA2023080977905Skin · chafedCHAFING ON INNER FUSELAGE SKIN AT FWD CABIN BS277+5; 3'OB OF S-2L LBL10.<[01] UPDATED MEASUREMENT TABLE.<BR>VERIFIED SRM 53-00-01-2R-38 IS APPLICABLE TO REPAIR SMALL DAMAGE IN FUSELAGE SKIN.<BR>DRILLED OUT DAMAGE TO A .125 DIAMETER PER SRM 53-00-01-2R-38 PARA.SDR CALA2023071402259Skin · damagedFOUND 1 EA LIGHTNING STRIKE ON SKIN AT LHS FR8 Z-339 CREATED BY MEHRDAD PARSA 91105046 60000 FC/120000 FH IAW SRI 53-11-11-205-037 REPAIR EMBODIMENT AT ZONE 1. PERFORMED PERMANENT REPAIR CATEGORY B IAW SRM 53-11-11-3000-041. IT IS NECESSARY TO INSPECT THIS REPSDR DALA2023071305683Unknown · unknownAIRCRAFT 5036, JETBRIDGE CONTACTED FUSELAGE CAUSING 2 DENTS & 1 SCRATCH FWD OF 1L DOOR LWR BETWEEN STRINGERS 23 & 24 FR 12 & 14. CORRECTIVE ACTION: FOUND A 1" VERTICAL CRACK FWD OF FRAME 14 BETWEEN STRINGERS Z-520 & Z-627. PERFORMED DETAILED INSPECTION EXTERNASDR DALA2023071205665Unknown · unknownCORROSION TYPE EXFOLATION ON FUSELAGE SKIN (LOWER CUTOUT) AT AFT CARGO COMPARTMENT STA 974. SUMMARY OF NRC 00512: CORROSION LEVEL 2. FUSELAGE SKIN LOWER CUTOUT AT AFT CARGO COMPARTMENT STA 974 WAS REPAIRED PER PRI 610235-14 REV 1 AND ER/A 610235-14 REV ORIGINASDR DALA2023080406299Unknown · unknownER/A 610235-14; FUSELAGE SKIN AFT CARGO DOOR CUTOUT SKIN AND DOUBLER STA Y=954 TO 994, L-28R IS CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 610235-14, SECTION II REPETITIVE INSPECTION WITHIN 8,000 FLIGHT CYCLES FROM 32,098 TOTAL FLIGHT SDR DALA2023071205644Unknown · unknownSHIP 3355 DENTS EXTERNAL SKIN LOC.FR30 STR25L TO STR27L AT LOWER FUSELAGE (2 E/A). CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC. ON EXTERNAL SKIN BTW FR29 TO FR30 STR27L TO STR29L AT LOWER FUSELAGE AS PER A330 SRM 53-21-11-300-016. (2860972)SDR CALA2023071202229Skin · damagedDAMAGE OCCURRED TO AIRCRAFT FROM BOARDING STAND LEFT SIDE OF FUSELAGE 10 INCHES AFT OF STA 580 AT STRINGER 20L. .057" WIDTH 1.10" A/Y=19.2 ALLOWABLE A/Y=30. REPAIRED AREA IAW 0100-0191. B757-200 SRM 53-00-01-2R-28 REPAIR 28. ACCOMPLISHED ON AMES NR EVALUATED DSDR DALA2023071105610Unknown · unknownSHIP 3422 FAA APPROVAL PENDING ERA610110-14 REV. ORIG. AFT CARGO DOOR SURROUND SKIN / GROUND DAMAGE. CORRECTIVE ACTION: C/W ERA 610110-14. (2859992)SDR DALA2023071105609Unknown · unknownSHIP 3422 AFT CARGO DOOR SURROUND SKIN GROUND DAMAGE PERMANENT REPAIR. CORRECTIVE ACTION: C/W ERA 610110-14. (2859980)
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