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 IPXA2019111328937Skin · corrodedINSPECTION TYPE:2CCENTER WING BOX UPPER SKIN HAS CORROSION AT STR. 3 AND BETWEEN XCW=-101 TO XCW=-110.REPAIRED CORRODED CENTER WING BOX UPPER SKIN AT STR 3. AND BETWEEN CXW=-101 AND XCW=-110 IAW VT SAA EA 011-5730-01-A7939 REV. I/R AND UPS EO MD11-5730-74536-SDR CALA2019102981843Skin · dentedB757-53-3-6037 AFT LOWER HALF OF FUSELAGE LEFT SIDE BETWEEN STA 1580 AND STA 1600 PROTRUDING DENT. MARKED CVC210-018 REF ST ENG N/R 0075751 REF. N/R#0075751 FOUND DENT OUT OF LIMITS. ACCOMPLISHED ZONE A C AT B REP. IAW 757 SRM#53-00-01 REPAIR 29. INITIATE D DSDR CALA2019102901847Skin · dentedEXTERNAL FUSELAGE SKIN DENTED AFT OF JACK PAD STA 1088 STR 25R FROM CONTACT WITH JACK. SEE LOG PAGE 3665579 FOR DIP AFTER EVALUATED DAMAGE IN AREA FOUND L:1.20" W:1.00 D:0.083" W/Y:1.0"/0.083"=12.04 OUT OF LIMITS. IAW B737-800 SRM 53-00-01 ALLOW DAMAGE 1 FIG 1SDR DALA2019102606181Vent · corrodedAFT LAV VENT HAS CORROSION AROUND VENT, REMOVED EXISTING FASTENERS IN REPAIR AREA REMOVED CONNECTION PLATE AND CUTOUT DAMAGE SKIN AREA AND DEBURR THE EDGES, STEP 2A 1 THRU 6. NDT OPEN HOLE ROTARY INSP PER A320 NDTM 51-10-01 PBG PROCEDURE AND SURFACE SCAN FOR CSDR C77A2020020530044Skin · damagedDURING BASIC CHECK AT EAMS, 4 TOOL MARKS DAMAGES WERE DISCOVERED ON THE CENTER FUSELAGE III LH LOWER SKIN PANEL UNDER THE L2 DOOR SCUFF PLATE. REFERENCE ETD2019-170-144701 FIGURES 1 & 2 FOR DETAILS, FOR THE DAMAGE LOCATIONS AND DIMENSIONS. EAMS REQUESTED AND RSDR SWIA2019121746939Skin · corrodedA/C BELLY INNER SKIN HAS CORROSION AND PITS ALL THE WAY AROUND THE FWD E&E BAY DOOR OPENING (C-CHECK) RO:12/14/2019 REPAIRED INNER SKIN DAMAGE IAW CRJ-200 REO .SDR SWAA2019110838705Skin · dentedDENT COMMON TO FUSELAGE SKIN AT STA 1040, 2" BELOW S-16L. / DENT @ FUSELAGE SKIN STA. 1040, 2" BELOW S-16L IS FOUND TO BE "OUT OF LIMITS" AS PER B7373 SRM 53-00-01-1A-1 FIG 103 DETAIL G. ACCOMPLISHED SKIN REPAIR TO FUSELAGE SKIN STA. 1040 S-16L AS PER B737-800SDR 2019FA0000353Bear Strap · corrodedAIRBORNE/PEMCO NON-ROUTINE 2601N484 DISCREPANCY: C/R EVAL REPAIR-CORROSION ON BEAR STRAP BETWEEN STA1346-STA1351M STR34R - STR35R PER ATTACHED REA NO. B653-5510MR CORRECTIVE ACTION: REPAIR TO BE ACCOMPLISHED ON NR 2601N495 PER EO 19421 REV 1R AIRBORNE/PEMCO SDR SWAA2022032365552Skin · corrodedT996808 ***CORROSION*** AT FUSELAGE SKIN LWR LOBE STA 1017 BETWEEN STR- 24R - 24L ; / REPAIRED FUSELAGE SKIN BS 1017 STR 24R - 24L IAW EA1-753-36022 REV IR AND ATS ER 19-05498 REV IR. APPLIED DENT DOT IAW MPM 53-03-01-02. NO FURTHER ACTION OR INSP REQ IAW EA 1SDR SWAA2019110638651Skin · dentedTWO SKIN DENTS AT BS 1040 +13 BETWEEN STR-20-21R DEEPEST DENT MEASURES L-.5 X W-.3 X Y-.012 W/Y=25. / REPAIRED TWO SKIN DENTS THAT WERE OUT OF LIMITS BS-1040+12- BS-1040+14.5, BETWEEN STR-20-21R. PER SRM 53-00-01-1A-1. FABRICATED AND INSTALLED SKIN RESDR DALA2019102906260Skin · dentedSHIP 652 DURING SCHEDULED MOD IN MSP OCT 2018, MTC WAS ACCOMPLISHING EO 2330-01349 2KU ANTENNA INSTALLATION. DURING THE PROCESS, MTC FOUND EXISTING. THE DENTS ARE SUSPECTED TO BE FROM A HAIL STORM WHICH RECORDS REVIEW INDICATES HAVE NOT BEEN PREVIOUSLY EVALUATSDR SWAA2019102538197Skin · crackedGROUND POWER DOOR FRAME SKIN CRACKED AFT OF DOOR. / REPAIRED SKIN PER SRM.SDR COEA201911222810Skin · corrodedWO 205731 NR 200141 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE UPPER L/H SKIN INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 40-41, ABOVE STRINGER 7L. CORRECTIVE ACTION: DOUBLER REPAIRED PER SRM 530000-300-803-A01.SDR FDEA2019102422729Skin · gougedL\H SIDE OF EMPENNAGE HAS 2 EACH SMALL GOUGES AT STABILIZER LOWER SLIDING SEAL AREA BETWEEN B.S. 1800 AND B.S. 1810 BLENDED GOUGES ON L\H SIDE OF EMPENNAGE STA 1800 TO 1810 IAW B757 SRM 51-10-02. AFTER FURTHER EVAL FOUND STA 1810 TO BE OUT OF LIMITS IAW B7SDR R61A2019102821164Skin · damagedMAJOR REPAIR: DAMAGE TO FUSELAGE SKIN FWD OF FPB BETWEEN STGRS 22R AND 24R. CUT OUT SKIN DAMAGE BETWEEN FRAME 1 AND 2, STGR 22R AND 24R. INSTALLED FILLER AND DOUBLER, RESTORED TOPCOAT.SDR EBVR20191022001Skin · corrodedDURING INSPECTION FOUND CORROSION UNDER FLOORBOARD PANEL 162AC. COMPLIED WITH AQRD ERO-962576 FUSELAGE REPAIR, REVISION IR, DATED OCTOBER 26, 2019. AND 8110-3 DATED: OCT.22,2019.SDR SWAA2022032365535Doubler · corroded***CORROSION*** ON ANTENNA SKIN DOUBLER IN FCB BILGE STA 500A-500B BETWEEN STR 28L-28R WL 152 (MARKED) / REMOVED ANTENNA SKIN DOUBLER ON FCB BILGE STA500A-500B BETWEEN STR 28L-28R I.A.W SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW CHANNEL I.A.W DWG 143A3233 ID:00SDR FDEA201910212728Skin · damagedAIRCRAFT FUSELAGE STRUCK BY CONTAINER DURING STORM, LEAVING HOLE IN SKIN JUST FORWARD AND BELOW BULK CARGO DOOR. INSTALLED REPAIR REF MD-10 SRM 53-20-00 FIG 6 AND E.A. 8-5330-T0350329 P1 FUSELAGE - PLATES & SKINS - CONTAINER STRIKE LWR AFT L/H FUSELAGE -SDR DALA2019102426124Skin · corroded(AIRCRAFT 5640, L/P 1325676) CORROSION ON INBD SIDE OF FUSELAGE SKIN BTW STA:1190 TO 1200 AND S-29L TO S-29R AT AFT CARGO COMPARTMENT. (FUS). CORRECTIVE ACTION: CORROSION LEVEL 1: AREA WAS REPAIRED PER ETI-57-19-140 REV. ORIGINAL AND ERA 582278-14 REV. ORIGINASDR AALA202001069043Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON INTERNAL SKIN SURFACE BETWEEN FR 59 AND FR 60 AND BETWEEN S42L AND S43L. REPAIRED FUSELAGE SKIN PER EA 299855.SDR REXA2019111821635Access Panel · crackedHIDDEN DAMAGE [DURING REMOTION OF STIFFENER IN REF NRC 452: CRACK ON SKIN AT ACCESS 172CR AND 171CL. (FUS).
SUMMARY: SKIN AT ACCESS 172CR AND 171CLL WAS REPAIRED PER REO 670-53-82-430 REV. --SDR DALA2023102508762Unknown · unknownMAIN ENTRANCE DOOR, (L-1), HOLD OPEN HOOK CAVITY IS GOUGED ON THE AFT SIDE. REPAIRED FUSELAGE SKIN AT L-1 DOOR HOLD OPEN HOOK CAVITY IAW B717 SRM 53-10-01-2R-7. INSPECTION REQ AT 8000 F.C. FROM DATE OF REPAIR INSTALL & REPEAT EVERY 8000 F.C. THERE AFTER INSP RSDR DALA2019102206084Skin · damagedAIRCRAFT ROLL BACK AND STRUCK GROUND EQUIPMENT CAUSING DAMAGE TO FUESLAGE, BELLY SKIN DAMAGE FROM FRAME 51 TO FRAME 61 AND BETWEEN STR 42 LH AND STR 42H, REPAIRED PER ER/A 582105-14SDR DALA2019102206083Skin · damagedAIRCRAFT ROLL BACK AND STRUCK GROUND EQUIPMENT CAUSING DAMAGE TO FUESLAGE, BELLY SKIN DAMAGE FROM FRAME 51 TO FRAME 61 AND BETWEEN STR 42 LH AND STR 42H, REPAIRED PER ER/A 582155-14SDR DALA2019102206082Skin · damagedAIRCRAFT ROLL BACK AND STRUCK GROUND EQUIPMENT CAUSING DAMAGE TO FUESLAGE, BELLY SKIN DAMAGE FROM FRAME 51 TO FRAME 61 AND BETWEEN STR 42 LH AND STR 42H, REPAIRED PER ER/A 582147-14SDR DALA201910226081Skin · damagedAIRCRAFT ROLL BACK AND STRUCK GROUND EQUIPMENT CAUSING DAMAGE TO FUESLAGE, BELLY SKIN DAMAGE FROM FRAME 51 TO FRAME 61 AND BETWEEN STR 42 LH AND STR 42H, REPAIRED PER ER/A 582114-14SDR FDEA201910182685Skin · corrodedAFT ACCESSORY COMPARTMENT HAS CORROSION ON R/H SIDE WALL REPAIR IN REF. TO MD-11 SRM 53-70-01-2R; FIG. 201.SDR SWAA2019110438557Skin · corrodedEXTERIOR SKIN CORRODED UNDER ANTENNA AT BS. 360-6, BL 0. / REPAIRED SKIN IAW SRM & EA.SDR DALA2019102286075Skin · indication(AIRCRAFT 668, L/P 1320305) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1562 MARKED. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.SDR DALA2019102286074Skin · indication(AIRCRAFT 668, L/P 1320303) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1565 MARKED. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.SDR DALA2019102286073Skin · indication(AIRCRAFT 668, L/P 1320302) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1573 MARKED. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 58SDR DALA2019102286072Skin · indication(AIRCRAFT 668, L/P 1320301) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1581 MARKED. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.SDR DALA2019102286071Skin · indication(AIRCRAFT 668, L/P 1320300) EXTERNAL DFEC INSPECTION OF STR 14R SHOWS INDICATION AT STA 1581 MARKED. CORRECTIVE ACTION: COMPLIED WITH PRI 581984-14AD REV 0 THRU 4 WHICH MATCHES COMPLIED WITH ERA 581984-14AD REV. 0.SDR ABXA2019102517162Skin · gougedGOUGE IN THE FUSELAGE SKIN AT FUSELAGE STATION 522, STRINGER 25R. THE GOUGE WAS CAUSED BY GROUND EQUIPMENT CONTACT. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR DALA2019102186043Repair · noneSHIP 668 REMOVE R/H WIFI DOUBLER NEAR F.S. 1533 TO FACILITATE REPAIR, MULTIPLE CRACK INDICATION FINDINGS WERE REPORTED. CORRECTIVE ACTION: SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/036 00425 COMPLIED WITH ERA 582231-14 REV A. (1320002)SDR DALA2019101806004Skin · crackedSHIP 668 CRACK INDICATION FOUND (MARKED) AT STR 14R STA 481 DURING DFEC INSPECTION PER AMDS STANDARD NDT 1087-3. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 113-0001:5331-01282-03/018 00302 COMPLIED WITH PRI/ERA 581625-14AD LATEST REVISION REVSDR C77A2020020430048Skin · dentedDURING BASIC CHECK AT EAMS, INSPECTION DISCOVERED MULTIPLE DENTS ON FORWARD FUSELAGE RH LATERAL SKIN PANEL P/N 170-03385-004 FROM FR01 TO FR05 BETWEEN STGR8R/STGR18R. REFER ETD2019-170-138883 FOR DENTS LOCATIONS AND MEASUREMENTS.
THE DAMAGE IS OUT OF LIMITS OSDR A6WA2019110946984Skin · dentedSMALL DENT ON R/H AFT FUSELASGE TAIL SECTION APPROX FS 733 & R/H STRINGER 19 AIRCRAFT REMOVED FROM SERVICE REWORKED DENT ON R/H AFT FUSELAGE TAIL SECTION AT APPROX FSS 733 AND ABOVE S19R IN AN AREA OF 1" X 1" X .002"D FROM ORIGINAL DEPTH OF .012"D FOUND TO BSDR SWAA2019110438553Skin Splice · corrodedAFT CARGO COMPARTMENT BILGE SKIN SPLICE CORRODED AT BS. 887, BETWEEN LBL 8 TO RBL 6. / REPAIRED SKIN SPLICE IAW SRM & EA.SDR SWAA2022040607907Skin · corroded***CORROSION*** ON FUSELAGE SKIN; UNDER DORSAL FIN; AT B.S. 887-1007; W.L. 306.5. / REPAIRED CORROSION DAMAGE ON FUSELAGE SKIN UNDER DORSAL FIN; AT BS 887-1007. WL 306.5 PER ER# 19-05337 REV IR AND EA #1-753-35956 REV IR.SDR REXA2019102451509Doubler · corrodedHIDDEN DAMAGE IN REF. JOBCARD 900-34-900-702. CORROSION ON DOUBLE IN SETTLEMENT AREA OF TRANSMIT ANTENNA 2 E19. (SM) (FUS).
SUMMARY: DOUBLES (SPACER) WAS FABRICATED PER E/A CRJ 953-09832 REV IR. AND WAS INSTALLED PER CRJ 900 SRM 51-42-06-001-001-A01.SDR DALA2019101505901Access Panel · corrodedCORROSION ON INTERNAL STRUCTURE OF WATER WASTE ACCESS PANEL. WATER WASTE PANEL WAS REPLACED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G AND DWG 5965767 REV. J.SDR FDEA201910142638Skin · corrodedEMPENNAGE RIGHT UPPER FUSELAGE SKIN BS 2122 TO 2164, LONGERONS 33-35R, FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED IAW SRM 51-21-01-0G, AND FOUND OUT OF LIMITS IAW SRM 53-70-01-2R, FIGURE 201, REPAIR 3. REPAIRED IAW EA 1-5330-T0350371, PART 1. SDR CALA2019101801762Skin · dentedAFT UPPER L/H TAIL SECTION OF FUSELAGE HAS DENT/CREASE ON SURFAC E BETWEEN FR 72-FR73 STRGRS 6L-8L A3NB-05-3-6062 PER HAECO LCQ N R 9292189 GENERATED BY V901665 DURING C-2 HAECO LCQ TECHNICIAN V892069 AND QC LC-32 REPAIRED DE NT INSTALLING REPAIR DOUBLER L=1.5SDR DALA2019101755956Doubler · crackedDURING INSPECTION CRACK ON INTERNAL DOUBLER CUTOUT LOWER AREA AT EXTERNAL POWER RECEPTACLE . INTERNAL DOUBLER CUTOUT LOWER AREA AT EXTERNAL POWER RECEPTACLE WAS REPAIRED (PERMANENT REPAIR) PER B737-800 SRM 53-10-15 REPAIR 4.SDR REXA20191118596Plate · wornAWR:IN REF EO R53582 WEAR ON LP GROUND CONNECTION PLATE.(SM)(FUS).
LP GROUND CONNECTION PLATE WAS REPAIRED PER EA CRJ953-09785 RV: IRSDR R61A201910281158Doubler · corrodedCORROSION_FWD WET AREA FWD L.HAND DOUBLER FR13-FR16. BLENDED CORROSION ON FWD WET AREA FWD L.HAND DOUBLER FR.13 - FR.16. MATERIAL LOSS .025.OUT OF LIMITS REF.SRM 53-10-10. REMOVED AND REPLACED L.HAND DOUBLER FR.13 - FR.16. REF. SRM 51-40-08, SRM 51-40-02 REF SDR DALA2019101765966Skin · damagedCROWN SKIN DAMAGED BS 550 - 661 STR 10L TO 10R. COMPLIED WITH ERA 581456-14, COMPARED ERA 581456-14 REV ORIGINAL WITH PRI 581456-14 REV 0 THUR 4, BOTH MATCH.SDR V0XD201910130001Skin · dentedEXTERNAL FUSELAGE SKIN AFT OF LOW PRESSURE AIR GROUND CONNECTION DOOR HAS MULTIPLE SCRATCHED AND DENTS. CORRECTIVE ACTION: REPAIRED EXTERNAL FUSELAGE SKIN AFT OF LOW PRESSURE AIR GROUND CONNECTION DOOR BUT CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING REPAISDR FDEA2020061622615Skin · corrodedAFT ACCESSORY COMPARTMENT HAS EVIDENCE OF CORROSION ON R/H SIDEWALL. REPAIR IN REF. TO MD11 SRM 53-70-01-2R; FIG. 201.
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