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 SWAA2023010478704Doubler · crackedEXTERNAL POWER DOOR CUTOUT DOUBLER CRACKED. TRIMMED DAMAGED AREA IAW SRM 53-10-15-2R-4. SMOOTHED SURFACE. PERFORMED HFEC INSP ON CUT OUT IAW NDT PART 6 51-00-00 PROC 23, NO CRACKS. FABRICATED A DOUBLER AND FILLER IAW SRM 53-10-15-2R-4. INSTALLED REPAIR SDR DALA2022120607830Skin · damagedDURING AN H CHECK, A DENT AND SCRATCH WAS FOUND AT FR 30 -31, S26-27L. THE DAMAGE WAS REWORKED IAW SECT III OF ERA 580319-14, REV B. FOLLOW ON MAINTENANCE/INSPECTION REF ER/A 580319-14. (2525918)SDR SWIA2022122967068Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER BETWEEN FS 589.00 - 605.00, STGR 25R - 26R. PERFORMED REPAIR TO DENT ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLER IAW REO 601R-53-61-7930 REV -.SDR SWIA2022122967067Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 640.00 - 654.00, STGR 19L - 20L. REPAIRED DENT IN FUSELAGE SKIN IAW REO 601R-53-61-7927 REV -.SDR DALA2022120507754Skin · corrodedCORROSION EXTERNAL SKIN LOCATED BTW FR 69 TO FR 70 AND STR 31R TO STR 32R AT LOWER FUSELAGE. FOUND WITHIN LIMITS AS PER SRM-53-41-11-283-065 STEP 2.SDR DALA2022120507747Skin · corrodedWING CENTER SECTION UPPER SURFACE AT STA 955,RBL 86 FOUND CORROSION, CORRECTIVE ACTION: REPAIRED THE CORROSION ON THE CENTER WING UPPER SKIN PANEL AND REAR SPAR UPPER CHORD AT STA 955;RBL 86 AS PER PRI 603514-14 REV 0 AND PRI 603514-14 (2523687)SDR VNAA202212290001Skin · dentedDENTS ON EXTERNAL FUSELAGE SKIN BTW FS409-FS421 & BTW STGR 15L-16L. (2 LOCATIONS)SDR YENA2022120801215Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION FOUND ON WASTE ACCESS CUT OUT. CORROSION REMOVED IAW SRM 51-12-03, SRM 51-10-03, FOUND OUT OF LIMITS IAW SRM 53-23-60/AD51. REPAIRED IAW SRM 53-23-60, REP 51. MAJOR REPAIR.SDR IPXA2023112756536Skin · punctured*MAJOR REPAIR* RIGHT SIDE AFT FUSELAGE SKIN PUNCTURE AT STA 1520, S-21R-REPAIR REF EO-85346***SM2/LMX6/QC2*** COMPLIED WITH EO-85346-REQ003. REPAIR UPGRADED TO CATEGORY BSDR R61A2022122900783Doubler · corrodedWHILE AC WAS IN FOR HVY CK FOUND CORROSION FOUND ON WASTE DOOR DOUBLER. REPLACED WASTE DOOR DOUBLER IAW SRM 51-41-01. PN 170-66931-001. AC REMAINS IN YQG FOR COMPLETION.SDR IPXA2022120288631Skin · damagedDAMAGE TO AIRCRAFT SKIN BEHIND AFT CARGO DOOR, MAJOR REPAIR, ALL WORK ACCOMPLISHED ON NRC 684236 & NRC 684237SDR DALA2022120207730Skin · dentedSHIP 676 ER/A 591557-14 DTA STAGE III LIMIT, TWO DENTS WERE FOUND ON THE FUSELAGE SKIN BETWEEN STA 580 AND STA 620 AND BETWEEN S-1 &S-4R. CORRECTIVE ACTION: REF ERA 591557-14 REV C. (2518816)SDR YENA2022120101187Skin · corrodedDURING HEAVY MAINTENANCE: 'CORR UPR SURF UPR SKIN CNTR WING BOX FR41-FR42 Y1292 TO Y1732 PAX CABIN; (RESOLVED ON W/O: 1170773 TASKCARD: NR-00015 ) REF AEM NR 2022-590512 FOR ALL WORK ACP RPR SKIN PER JB EC A22-925-01.'SDR DALA2022112907608Skin · crackedSHIP 198 HFEC INSPECTION FOUND 01 EA CRACK AT S-13AL ABOUT STA1660 AS MARKED.IT IS ABOUT 0.1 INCH LONG. CORRECTIVE ACTION: CARRIED OUT THE REPAIR TO THE SKIN AT STA1660 STR13AL AS PER B767-300 SRM53-80. INSPECTION INTERVAL 7500 FLIGHT CYCLES USE DVI AND LFEC ISDR DALA2022112907607Skin · crackedSHIP 198 HFEC INSPECTION FOUND 01 EA CRACK AT S-13AR ABOUT STA1661 AS MARKED.IT IS ABOUT 1.2 INCH LONG. CORRECTIVE ACTION: CARRIED OUT THE REPAIR TO THE SKIN AT STA1661 STR13AR AS PER B767-300 SRM53-80. INSPECTION INTERVAL 7500 FLIGHT CYCLES USE DVI AND LFEC ASDR AALA202301127767Skin · crackedAIRCRAFT WAS GROUNDED: CRACK IN INNER SKIN IS HORIZONTAL APPROXIMATELY 1 INCH IN LENGTH. FORWARD END OF CRACK IS LOCATED 2.7 INCHES AFT OF STIFFENER AND 0.6 INCHES BELOW NEAREST FASTENER HOLE. STA 663, STR 18L AND WATERLINE 0. PERFORMED A FLUSH DOUBLER REPAIR SDR R61A2023010400016Doubler · corrodedCORROSION FOUND ON CF 3 WASTE ACCESS DOOR CUTOUT INNER DOUBLER. REPLACED SHEET IAW SRM 53-23-60.SDR DALA2022120107690Skin · corroded(LOG 2515867) DURING INSPECTION FOUND CORROSION PREVIOS REPAIR AND SKIN OF AFT CARGO COMPARTMENT BTW STA 727K TO 727L ,27 RH STRINGER , 27 LH STRINGER. DOUBLERS WERE FABRICATED PER GOGO DWG. NO.P20196, NOTE 3, AND GOGO DWG. NO.P19754, NOTE 3. AND REPLACED PER SDR DALA2022120107689Skin · corrodedDURING INSPECTION FOUND CORROSION ON PREVIOUS REPAIR AND SKIN OF FWD CARGO COMPARTMENT BTW STA 500C TO 500D ,27 RH STRINGER , 27 LH STRINGER. DOUBLERS WERE FABRICATED PER GOGO DWG. NO.P20196, NOTE 3, AND GOGO DWG. NO.P19754, NOTE 3. AND REPLACED PER B737-900ERSDR DALA2022120107686Skin · scratchedSCRATCH ON EXTERNAL SKIN LOC. FR 23 TO FR 24 BTW STR 42 L TO STR 43 AT LOWER FUSELAGE. COMPLIED WITH ER/A 603753-14 REV ORIGINAL. APPROVED DATE 27 NOV 22, MATCHES WITH ALL STEP ON PRI 603753-14 REV 0 AND REV 1. IT ISBEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONSDR DALA2022120107685Skin · scratchedSCRATCH ON EXTERNAL SKIN LOC. FR 25 TO FR 26 BTW 39 L TO STR 40 L AT L OWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOC. FR 25 TO FR 26 BTW 39 L TO STR 40 L AT LOWER FUSELAGE AS PER A321 SRM53-11-11 -300-090 FIG. 001 SHEET 01 MESURES OF REWORKED SDR JJBA20221129032Doubler · corrodedAT REAR FUSE 1 EXT, RADIO ALT ANTENNA NO 2 AFT LOWER DOUBLER CORRODED ON BELLY SKIN BTW FR 68-70. SKIN IS REPAIRED WITH A DOUBLERSDR U2RA2022120500056Skin · gouged1.125" X 1.0" GOUGE DISCOVERED ON LOWER FUSELAGE SKIN BETWEEN BODY STATION 480 AND 500, BETWEEN STRINGERS 38R AND 39R. - ACCOMPLISHED INTERIM REPAIR PER FLIGHT VEHICLES CONSULTING INC. ENGINEERING ORDER 22204-1 REVISION IR, APPROVED ON FORM 8110-3 DATED 11/25/SDR JJBA20221129029Skin · dentedFUSELAGE SKIN DENT HAS CREASE/GOUGE. DENT IS 3.75" X 2.25" AT FR 23-24, STR 12L-13L. DEPTH 0.125, FR 23 TO DENT IS 1", FR24 TO DENT IS 1.5", STR 13L TO DENT IS .75", STR 12L TO DENT IS 2.5". REMOVED SKIN CREASE/GOUGE. DENT FR 23-24 BTW STR 12L-13L. PERFORMED HSDR AALA202301138192Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXTERNAL SKIN AT FR 16 AND S23L UNDER SCUFF PLATE. MAINTENANCE REPAIRED SKIN PER EA 341299.SDR IPXA2022112488399Doubler · damagedINSPECTION TYPE:N/AFUSELAGE SKIN PREVIOUS REPAIR DOUBLER DAMAGED AT PLANE 25, BL 0REPLACED DOUBLER IAW E.O. MD11-553-85332-ASDR VNAA2022112711110Skin · handler errorLAV CART HIT RIGHT AFT SECTION OF AIRCRAFT BY LAV SERVICE DOOR / REPAIR OF R/H AFT FUSELAGE WAS PERFORMED BY MHIRJ TECHNICIANS IAW MHIRJ WORK ORDER #MIS-5501 AND REO 690-53-51-356 INSTRUCTIONS. REPAIR IS FOUND TO BE ACCEPTABLE AND AIRCRAFT IS APPROVED FOR RETUSDR AALA202211309851Skin · crackedAIRCRAFT WAS GROUNDED: L1 DOOR LOWER HINGE CUTOUT OUTER SKIN TEAR DAMAGED. CRACK LOCATED AT STA 312 AND WATERLINE 227.54. CUT OUT DAMAGE AND TREATED SKIN PER SRM 52-10-01.SDR DALA2022112807567Skin · damagedSHIP 659 PERFORM REPAIR IN REFERENCE MON, 56 L/L, 1754290; RII; ERA 590590; AD;00659 ER/A 590590-14 SEC III REQUIRED FOR THE NO. 2 CARGO DOOR LOWER. CORRECTIVE ACTION: SUMMARY OF NRC 00106. AREA WAS REPAIRED PER ER/A 590590-14 REV A SECTION II: PERMANENT REPAISDR FDEA202211222860Skin · damagedHUB STRIKE BELOW AFT BULK CARGO DOOR. REMOVED DAMAGED SKIN AS REQUIRED FOR SKIN REPAIR PER SRM 53-00-01-2R REPAIR #1. ROTOPROBE HOLES AND HFEC DAMAGE CUTOUT IAW NDTSPM PT6.SDR VNAA2022112200003Doubler · corrodedCORROSION ON ANTENNA DOUBLER BOTTOM OF FUSELAGE BETWEEN FRAMES FS 295 AND FS 310. INSTALLED NEW SERVICABLE ANTENNA DOUBLER AT STR 27 BETWEEN F.S. 295 AND 310 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01SDR FDEA202211212941Skin · corrodedCORROSION FOUND IN UPPER MAIN CARGO LH SIDE OF WING BOX TUNNEL AREA AT STA 1260. REPAIRED CORRODED SKIN AT THE UPPER MAIN CARGO L/H SIDE OF WING BOX TUNNEL AREA AT STA 1260 STR 10 AT XCW=181,850 IAW EA 1-5710-T0372012 P1.SDR UIEA2022111901196Splice Plate · damagedCENTER WING, RH SPLICE PLATE A ST GR 6 AND RBL97.42 FUEL LEAKS(<P>FUEL LEAKS WERE REPAIRED IAW AMM 28-11-00-308-013</P>)SDR UIEA2022111901195Splice Plate · damagedRH CENTER WING, SPLICE PLATES AT ST GRL10 AND RBL97.42 FUEL LEAK(<P>LEAKS WERE REPAIRED IAW AMM 28-11-00-308-013</P>)SDR UIEA2022111801194Splice Plate · damagedLH CENTER WING AT SPLICE PLATE STGR L6 AND LBBL97.42 FUEL LEAK(<P>FUEL LEAK WAS REPAIRED IAW AMM 28-11-00-308-013 REV 137</P>)SDR 2022FA0000706Tear Strap · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION, SEC 46, AFT CARGO TEAR STRAP, FUSELAGE SKIN, BETWEEN STA 1241 AND STA 1263 AND BETWEEN STR 38R AND STR 39R.SDR 2022FA0000705Skin · damagedDURING MAINTENENCE INSPECTION FOUND SEVERAL ADJACENT BLEND OUTS BETWEEN STA 1346 AND STA 1395 AND BETWEEN STR 20R AND STR 32R.SDR 2022FA0000704Tear Strap · corrodedDURING MAINTENENCE INSPECTION FOUND CORROSION ON INTERNAL TEAR STRAP, BETWEEN STA 720 AND STA 742 AND BETWEEN STR 35R AND STR 35L.SDR 2022FA0000703Skin · damagedDURING MAINTENENCE INSPECTION FOUND BLEND OUT AMONG FASTENERS BETWEEN STA 1489 AND STA 1510.5 AND BETWEEN STR 25R AND STR 26R, ABOVE LAP SPLICE.SDR ASAA2022111941145Skin · dentedFOUND 2 OUTWARD DENT AT FRAME 69/70. STRINGER 23R/24R. GROUNDED - YES. CUTOUT DAMAGE, FABRICATED, LOCATED, AND DRILLED REPAIR DOUBLER AND FILLER IAW SRM 53-41-11. ALODINED AND PRIMED REPAIR DOUBLER FILLER, CUTOUT, AND REPAIR AREA IAW SRM 51-21-11 AND 51-23-00.SDR SWIA2023011367088Skin · dentedLEFT SIDE FUSELAGE THERE IS DENT AT UPPER AFT EMPANNAGE APPROX AFT OF FS 736.0 AND JUST FWD OF FS 755.0 AT STR7. REPAIRED LEFT SIDE FUSELAGE DENT AT UPPER AFT EMPANNAGE APPROX AFT OF FS 736.0 AND JUST FWD OF FS 755.0 AT STR7 REF REO 601R-53-71-219 REV-- DSDR ASAA2017052040892Skin · dentedDENT / SCRATCH NOTED ON LEFT FWD FUSELAGE BELOW CPT. L3 WINDOW. GROUNDED - YES. (RESOLVED ON W/O: 1921149 TASKCARD: N/R-00013 ) REPAIRED DENT ON LH FWD FUSELAGE BELOW CPT L3 WINDOW IAW B737-700 SRM 53-10-01-2R-2 LFEC REQUIRED EVERY 9,000 FLIGHT CYCLES. THIS ISSDR SWAA2022112273005Doubler · crackedPOSSIBLE DAMAGE AT APPROX. BS 235 OF THE LOWER FORWARD CORNER OF THE EXT POWER DOOR CUT OUT AREA. SUSPECTED CRACK AND SEPARATION OF BONDED DOUBLER. REMOVED DAMAGED SURROUND DOUBLER IAW SRM 53-10-15-2R-4. HFEC SURFACE INSPECTION AROUND TRIM OUT PER NDTM PARSDR DALA2022112107460Skin · dented(LOG 2502176) DURING INSPECTION FOUND DENT ON FUSELAGE STA 360+3" BETWEEN STR 23R AND STR 24R. C/W ER/A 603203-14 REV ORIGINAL SECTION 1.SDR R61A2022120900772Skin · gougedWHILE IN HEAVY CHECK - GOUGE ON FR82 @ STRINGER 3L. REMOVED DAMAGE AREA. FABRICATED AND INSTALLED DOUBLER REPAIR FR82 @ STGR 3L REF. ETD 2022-170-034920 REV.: A.SDR DALA2022112107473Skin · damagedSHIP 5639 REPAIR TO FUSELAGE SKIN EXTERNAL DOUBLER AT STA 660 & 760, S-4R & S-4L REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 595659-14 REV A, SECTION III. CORRECTIVE ACTION: REF ERA 595659-14 REV C. (2500217)SDR SWAA2022122072217Bear Strap · crackedR1 DOOR UPPER FWD CUTOUT CORNER BEAR STRAP; CRACK AT STA 291.5+4 RBL52 BETWEEN S8R AND S9R.<[01] PERFORMED HFEC INSP. AT R1 DOOR UPPER FWD CUTOUT CORNER BEAR STRAP AT STA 291.5+4 RBL52 BETWEEN S8R AND S9R. IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK LENSDR SWIA202266943Skin · chafedSKIN PANEL 429ML HAS CHAFING ON EXTERIOR OF PANEL. REMOVED AND REPLACED THE SKIN PANEL IAW SRM 51-40-08.SDR HNAA2022112800311Skin · crackedE943764 - FUSELAGE EXTERNAL SKIN CRACKED AROUND FASTENER ON FR 77 BTW STR 4R-5R. .... REPAIRED FUSELAGE EXTERNAL SKIN AROUND FASTENER ON FR 77 BTW STR 4R-5R IAE EO1-53-22-0230.SDR HNAA2022112800310Skin · crackedE943631 - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND 2 FASTENERS ON FR 77 LH SIDE BELOW VERTICAL STAB .... UPON FURTHER INVESTIGATION ONLY 1 AREA ON FUSELAGE SKIN FOUND TO BE CRACKED. REPAIRED FUSELAGE EXTERNAL SKIN AROUND FASTENER ON FR 77 LH SIDE BELOW VERTICA
Back to JASC 5330