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 SWIA202158155Skin · dentedTRANSFER FROM EAML 636913 : TRANSFERRED FROM CAMP 22790038. 1-OFF DENT WITH GOUGE ON THE FUSELAGE SKIN BETWEEN 43.75% MID SPAR / DATUM - 55.63% AND BETWEEN STR15R-STR17R (DWG MM670-38101, AL 2024-T42, 0.080" NOMINAL / THK, 0.050" AND 0.045" CHEM-MILL POCKET THSDR UIEA2021041800930Skin · damagedFX - STA 240 R/H S-28A TO S-30R SKIN FOUND PREVIOUS BLEND OUT AREA AT 2EA RIVET LOCATION.(<P>FX - STA 240 RH S-28A TO S-30R SKIN BLEND OUT AREA 2EA RIVET REPLACED AS PER RI-53-00-14544 REV A</P>)SDR VNAA 202105169998Skin · corrodedINTERNAL SKIN CORRODED BETWEEN STGR 26L AND 26R FROM FS 677.00 TO 693.00. REPAIRED PER REO 670-53-31-630 AND REO 670-53-31-648SDR EE4Y2021051612774Skin Panel · dentedDURING MAINTENANCE ACCOMPLISHMENT WERE FOUND THREE DENTS LOCATED BETWEEN FR28 AND FR29, BETWEEN STR28RH AND STR30RH, THE DENTS WERE FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM TASK 53-21-11-283-020 PARAG. 2A, DUE
TO THIS FACT A REPAIR WAS PERFORMED ASDR SWIA202160018Skin · dentedDENT BETWEEN FS672.20 TO FS 700.0 BETWEEN STRINGERS 18L AND 19L MEASURES 18" LONG BY 0.500" WIDE AND 0.013" DEEP IS WITHIN LIMITS AND YELLOW DOTTED. (C-CHECK RO 8/1/2021) REPAIRED FUSELAGE SKIN BETWEEN FS672.20 TO FS 700.0 BETWEEN STRINGERS 18L AND 19L SDR FDEA202105151313Skin · damagedDURING LOADING OPERATIONS AT IND, A LOADER STRUCK THE FUSELAGE BELOW THE MAIN CARGO DOOR AND BOLT PUSHED A HOLE INTO THE FUSELAGE WITH A CORRESPONDING DENT IN THE IMPACT AREA (STA 603.5 AND STRINGER 19L) JUST ABOVE A SKIN SPLICE NEAR THE AFT CORNER OF THE MCSDR SWAA2021061682364Skin · dentedDENT EXTERNAL SKIN LOC BTW BS 224.8 TO BS 235.8 AND 4 INCHES BELOW STR 24R AT LOWER FUSELAGE ; 2021-215620 / REPAIRED EXTERNAL FUSELAGE SKIN LOCATED BETWEEN BS 219.8 AND BS 235.8 + 6 AND 14 ABOVE OF STR 24R AND 10 BELOW OF STR 24R IAW EA # 21-153-01532-WIP1 ANSDR REXA2021052800373Doubler · corrodedLOWER TCAS ANTENNA INTERNAL DOUBLE AT FS300 TO FS305.00 CORRODED. REMOVED AND REPLACED TCAS ANTENNA INTERNAL DOUBLER IAW SRM 51-42- 06-001-001-A01 AND 51-42-21-001-001-A01, REMOVED AND INSTALLED STRINGER 27 FILLET SEALED IAW CRJ 900 SRM 51-23-00-001-001-A01.SDR MASA20210521192Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) |DAMAGED INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BETWEEN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT WAS REPLACESDR DALA2021051802771Skin · damagedSHIP 690 NRC IS ISSUED INSTEAD OF NRC SERIAL NUMBER 00412 DUE TO WRONG DESCRIPTION: PREVIOUS BLEND OUT ON EXTERNAL FUSELAGE SKIN BTW STA:1540-1560 AND STGR.26R - 28R. CORRECTIVE ACTION: SUMMARY OF NRC 00441: EXTERNAL FUSELAGE SKIN BTW STA:1540-1560 AND STGR.26SDR DALA2021051802770Skin · damagedSHIP 690 NRC IS ISSUED INSTEAD OF NRC SERIAL NUMBER 00412 DUE TO WRONG DESCRIPTION: PREVIOUS BLEND OUT ON EXTERNAL FUSELAGE SKIN BTW STA:1540-1560 AND STGR.26R - 28R. CORRECTIVE ACTION: SUMMARY OF NRC 00441: EXTERNAL FUSELAGE SKIN BTW STA:1540-1560 AND STGR.26SDR SWIA202158152Skin · dentedSURFACE DAMAGE TO DENT ON LH SIDE OF AC FWD OF THE MCD BELOW THE O2 BLOWOUT PLUG IS DETERMINED TO BE OUT OF LIMITS PER SRM. 53-21-01. COMPLY WITH REO 690-53-21-1370 FOR REPAIR. THIS IS CLASSIFIED AS A MAJOR REPAIR. SEE CP 22796534 FOR MAJOR REPAIR DETERMINATIOSDR FDEA202105141223Skin · dentedLOWER AFT FUSELAGE SKIN AT STA 2020 BELOW LONGERON 46L DENTED AND CREASED REPAIRED PER E.A. 8-5330-T0361489SDR MASA20210514190Skin · damagedEXTERNAL SKIN PANELS BETWEEN FRAME 22 AND X=7070.7 AND AT STRINGER 28R - LIGHTNING STRIKE DAMAGE. REPAIRED DAMAGE REFERENCE ETD2021-170-014822SDR MASA20210513189Skin · gougedSMALL GOUGE ON LOWER FUSELAGE BETWEEN FRAMES 19-20 STRINGERS 28L-28R. REPAIRED GOUGE IN ACCORDANCE WITH SRM 51-75-09 AND RO# 175-53-4421SDR CALA2021051400656Skin · damagedSUPPORT TASK - RH CTR SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131403. RH CTR SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS 0.128" ORIGINAL 0.130" WITHIN LIMIT AS PER SRM 51-10-01-2R-1 REPASDR CALA2021051400655Skin · damagedSUPPORT TASK - LH R SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131400. LH R SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS IS 0.129" ORIGINAL THICKNESS 0.130" WITHIN LIMIT AS PER SRM 51-10-01-SDR CALA2021051400654Skin · damagedSUPPORT TASK - RH R SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131401. RH R SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS IS 0.129" ORIGINAL THICKNESS 0.130" WITHIN LIMIT AS PER SRM 51-10-01-SDR CALA2021051400653Skin · damagedSUPPORT TASK - LH L SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131404. LH L SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR, AND SMOOTHED OUT AREA MEASURED REMAINING THICKNESS 0.129" ORIGINAL THICKNESS 0.130" WITHIN LIMIT AS PERSDR CALA2021051400652Skin · damagedSUPPORT TASK - RH L SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131402. RH L SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS 0.129" ORIGINAL THICKESS 0.130" WITHIN LIMIT AS PER SRM 51-10-01-2R-1SDR SWIA202158601Doubler · corrodedLEFT HAND DOUBLER HAS CORROSION AF OF CROSS BEAM FR 19 AS MARKED (C-CHECK RO 5/25/2021) REMOVED AND REPLACED L/H DOUBLER AF OF CROSS BEAM FR 19 REF EMB SRM 51-40-08SDR DALA2021051702729Skin · dentedSHIP 687 INITIAL INSPECTION:DENTS (2EA) ON RH CUTOUT OF THE MAIN E/E COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00157: DENTS ON RH CUTOUT OF THE MAIN E/E COMPARTMENT WERE REPAIRED PER ER/A 591491-14 REV. ORIGINAL SECTION I. (1808270)SDR MASA20210513188Skin · dentedFWD LH UPPER FUSELAGE SKIN DENT. REPAIRED DENT IAW ETD2021-170-013406SDR SWIA2021081060256Doubler · corroded*CORROSION ON DOUBLER FOR DRAIN MAST BETWEEN FS 1031.00 €“ 1051.30, STGR 27 €“ 26R (C-CHECK RO 8/9/2021) REPLACED DOUBLER AT DRAIN MAST BETWEEN FS1031-1051 STGR 27-26R REF- DWG MM670-43200 REV-N AND CRJ-700 SRM 51-42-06-001-001 A01,LEAK CHECK GOOD,NO SDR SWIA2021072159622Skin · dented*NINE PROTRUDING DENTS BETWEEN FS672.00 AND FS718.00 STGR21R €“ STGR25R WITH A SEGMENTED CREASE RUNNING THRU FS682.00 €“ FS718.00 STGR21R €“ STGR22R. ALL MARKED IN RED. (C-CHECK RO 7/18/2021) REPAIRED DENTED AREAS BETWEEN FS672 AND FS718 STR21R-25R. SDR SWAA2021070173821Bear Strap · crackedCRACK FOUND AT R1 DOOR CUTOUT INTERNAL. ; / DURING INSPECTION PER SB 737-53A1383 R1 (SWA SI 5313-I-15021-NG REV 2), CRACK DAMAGE WAS DISCOVERED ON THE FORWARD GALLEY DOOR SURROUND BEARSTRAP (P/N 141A3313-1) ON THE UPPER FORWARD CORNER IN A FASTENER HOLE AT STASDR SWAA2021070174474Bear Strap · crackedCRACK FOUND AT R1 DOOR CUTOUT INTERNAL. ; / EA 21-153-01327 WAS ATTACHED TO FAULT #TTG8Q0050WRM. CUT AND REMOVED DAMAGE FROM R1 DOOR BEAR STRAP PER B737-700 SRM 51-10-02-0G-0 AND SRM 53-10-01-2R-6 REPAIR 6, FIG 202SDR SWAA2021061776938Skin · corrodedCORROSION AROUND FWD FASTENER HOLE OF ADF #1 ANTENNA ; CORROSION ON ACFT SKIN AROUND FWD ; CENTER; FASTENER HOLE; OF ADF #1 ANTENNA BS 674; RBL 4; WL 308 / COMPLETED STEPS 4-8; COMPLETED AMT STEPS OF 21-153-01387-WIP1 (N732 - ATS(PAE) - REPAIR - FUSELAGE CROWNSDR SWAA2021061771524Skin · corrodedCORROSION ON ACFT SKIN AROUND AFT LEFT FASTENER HOLE OF ADF # 1 ANTENNA ; CORROSION ON ACFT SKIN AROUND AFT; LEFT; FASTENER HOLE OF ADF #1 ANTENNA; BS 702; RBL 3; WL 308 / EVALUATED DAMAGE REMOVAL ON FUSELAGE SKIN AT BS 702; RBL 3; WL 308. MAX DEPTH OF DAMAGE SDR SWAA2021061771522Skin · corrodedCORROSION AROUND FWD FASTENER HOLE OF ADF #1 ANTENNA ; CORROSION ON ACFT SKIN AROUND FWD ; CENTER; FASTENER HOLE; OF ADF #1 ANTENNA BS 674; RBL 4; WL 308 / EVALUATED DAMAGE REMOVAL ON FUSELAGE SKIN AT BS 674; RBL 4; WL 308. MAX DEPTH OF DAMAGE REMOVAL FOUND TOSDR SWAA2021061472147Skin · corrodedCORROSION ON SKIN AT AFT CARGO BAY BS919 JUST ABOVE S-22L WL180. VERIFIED ALL TASK IS COMPLETED PER EA 21-153-01461 CUSTOMER SYSTEM ID TTG8Q005C4YQ.; VERIFIED ALL TASK IS COMPLETED PER EA 21-153-01461 CUSTOMER SYSTEM ID TTG8Q005C4YQ.; VERIFIED ALL TASK IS COMSDR SWAA2021061476893Skin · corroded***CORROSION*** ON SKIN AT AFT CARGO BAY BS919 JUST ABOVE S-22L WL180. APPLIED CORROSION INHIBITING COMPOUND ON WORK AREA IAW SRM 51-20-01; ACCOMPLISHED CLEAN AT WORK AREA IAW AMM 20-60-07; CARD COMPLETE.SDR SWAA2021061479854Skin · corrodedCORROSION ON SKIN AT AFT CARGO BAY BS919 JUST ABOVE S-22L WL180. ; /SDR REXA2021060200398Doubler · gougedPREVIOUS REPAIR IS GOUGED AT FS 977.00 AND STRINGER 27. - REPAIRED AREA AT FS 977 STR 27 IAW CRJ 700 SRM 51-24-21-001-001-A01, 51-24-36-001-001-A01, 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.SDR SWAA2021051772224Bear Strap · crackedCRACK FOUND AT PERIPHERY OF R1 DOOR BEAR STRAP CUTOUT. PERFORMED HFEC ROTO ON OPEN FASTENER HOLES WITHIN REPAIR AREA OF R1 DOOR CUTOUT IAW NDTM PART 651-00-00 PROCEDURE 16. NO CRACKS. PERFORMED COUNTERSINK INSPECTION ON OPEN FASTENER HOLES WITHIN REPAIR AREASDR GTIA2021051335731Skin · dentedFOUND ON WALKAROUND: DENT AT FR 68-69 STR 19 LH MEASURES 2.75 LENGTH 1.5 WIDTH AND .035 DEPTH. RAF-01 2760207-01 OPENED-ACCOMPLISHED PERMANENT REPAIR OF FUSELAGE SKIN LH FR68+4.5" STR 19L IAW A319 SRM 53-41-11-300-095. REF REO 5341-2115 CAT A REPAIR NO REINSPESDR 7C7A2021051100005Skin · dentedR/H FUSELAGE, DENT FOUND ABOVE STR 23S AND FWD OF FR STA X 202.75. REPAIRED BY INSTALLING EXTERNAL PATCH IAW ECO 008.53-21.03SDR SWIA2021072159618Skin · dented*DENT ON EXTERNAL FUSELAGE SKIN BETWEEN FS 589.00 €“ 605.00, STGR 25R €“ 26R (C-CHECK RO 7/18/2021) REPAIRED DENT AT FS589 - 605, STR25R - 26R. REF REO 601R-53-61-7663 (REV --) DATED 2021-06-29. NO LEAKS NOTED / COMPLETED SKYWEST TASK CARD 51-900-1003SDR SWAA2021061771392Bear Strap · crackedCRACK INDICATION FOUND AROUND FASTENER LOCATED BEAR STRAP AT LEVEL FITTING-LATCH; STA 294.5 BETWEEN S-8R AND S-9R ; 2021-215390 / DIGITAL CALIPER P/N: 500-197-30;S/N: B20189527; DUE DATE: 23-NOV-21.;REMOVED RAIN GUTTER (2E/A) AND FASTENERS LOCATED BTW BS 291.5SDR FDEA202105111173Skin · crackedSURFACE HFEC INSPECTION FOUND 02EA CRACKS (FWD CRACK APPROX.0.700 INCH IN LENGTH AND AFT CRACK APPROX.0.650 INCH IN LENGTH) ON THE EXTERNAL SUR FACE OF THE FUSELAGE SKIN AROUND THE 2 HOLES COMMON TO THE LEFT SIDE UNDERWING LONGERON AND FUSELAGE SKIN ASSDR SWIA202158219Skin · damagedDAMAGE FOUND ON FUSELAGE SKIN PANEL BTW FS437.00-FS453.00 AND BTW STR22R-STR19R (FILED CLOSED) REMOVED DAMAGED SKIN AND INSTALLED DOUBLER AND TRIPPLER IAW REO 690-53-21-1368 REV. -- DATED 2021-05-17 / COMPLIED WITH NDT EDDY CURRENT INSPECTION, SEE CP 22SDR SWIA202158218Skin · damagedDAMAGE FOUND AT FS409-FS421 AND STR 22R-24R (FILED CLOSED) REMOVED DAMAGED SKIN AND INSTALLED DOUBLER IAW REO 690-53-21-1367 REV. -- DATED 2021-05-17 / COMPLIED WITH NDT EDDY CURRENT INSPECTION, SEE CP 22787318SDR FDEA202105111172Skin · crackedSURFACE HFEC INSPECTION FOUND 01EA CRACK APPROX.0.650 INCH IN LENGTH ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN AROUND THE 01EA HOLE COMMON TO THE RIGHT SIDE UNDERWING LONGERON AND FUSELAGE SKIN AS MARK AS PER W/C EO G-5310- E0332629 K P6 STEP 9. C. COSDR ABXA2021510059Skin · crackedDURING AIRCRAFT C-CHECK, MAINTENANCE DISCOVERED A CRACK ON THE FUSELAGE SKIN (SECTION 46) LOCATED AT STATION 1541 AND STRINGER S29L. THE DAMAGE WAS EVALUATED PER 767-200 SRM 53-00-01, FIGURE 101 AND FOUND TO EXCEED ALLOWABLE LIMITS, REQUIRING A REPAIR. THE DSDR SWAA2021061470913Skin · crackedCRACK IN RADIUS OF B.S. 310 FRAME JUST ABOVE THE FORWARD ENTRY DOOR CUTOUT. ; / CAL ID IS000450 DUE 12/2021; VERIFIED; VERIFIEDSDR ASAA2021051034891Skin · dentedLH FUSELAGE UPPER LOBE EXTERNAL SKIN HAS A DEEP DENT, BS 500F - BS 500G,S-5L. GROUNDED - YES. EVALUATED DENT ON THE FUSELAGE SKIN AT STA 500J+10, STR-5L, LBL 33 MEASUREDW=0.690" Y= 0.097, W/Y=7.113 FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-00-01-1A-1 FIGURSDR SWIA2021081060245Skin · chafed* FUSELAGE EXTERIOR SKIN CHAFED IN 3 LOCATIONS BETWEEN FS977 €“ FS985 STGR27 (C-CHECK RO 8/9/2021) PERFORMED REPAIR TO THE FUSELAGE EXTERIOR SKIN CHAFED AREAS BETWEEN FS977-985 AT STGR 27 REF REO 670-53-00-660 REV -- DATED 2021-05-31AND REO 670-53-00-2SDR SWIA202158429Skin · gougedGOUGE ON EXTERIOR FUSELAGE SKIN BETWEEN STRINGER 2R & 4R AND FS1098 & FS1126 (C-CHECK RO 5/22/2021) GOUGE ON EXTERIOR FUSELAGE SKIN BETWEEN STRINGER 2R AND 4R AND FS1098.00 AND FS1126.00 WAS BLENDED, CHEMICAL CONVERSION COATING APLLIED AND PROTECTIVE FISDR DALA2021051202684Skin · dentedSHIP 3140 - DENT EXTERNAL SKIN AT FR 14 AND 15 INCHES ABOVE OF RH SIDE STGR LOWER FUSELAGE. CORRECTIVE ACTION: EVALUATED DENTS LOC. FR14 TO FR15 ABOVE OF RH STRINGER AND FOUND WITHIN LIMITS AS PER A319 SRM 51-11. (1804531)SDR DALA2023091407569Unknown · unknownRAMP REPORTED DENT BELOW 1L DOOR. ER/A 591549-14 REV B PRI REV 0 AND FINAL ER/A 591549-14 REV B SECTION IV, PERMANEMT REPAIR, HAVE BEEN ACCOMPLISHED. REF LP 2962820 FOR ER/A DEF. OK TO CLOSE THIS LOG. (LP# 7425648)
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