JASC 5330
Service difficulty reports · 79,312
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 UIEA2025082501136Skin · corrodedCORROSION - SKIN, LH AFT LWR FUSELAGE SKIN STA 1732, S42L(<P>1) REPAIR THE DAMAGE IAW SRM 53-00-01-2R-1 REV 104 & W/S 50620. 2) CONDITION CHK NORMAL AND JOB COMPLETED</P>)SDR UIEA2025082501139Skin · corrodedCORROSION ON LH FUSELAGE OUTER SKIN NEAR STA 1700, S42L(<P>1) REMOVED FASTENERS IAW SRM 51-40-02-0G-0 REV 104. 2) REPAIR DAMAGE SKIN IAW EI T2025A53M-1733 REV 104. 3) JOB COMPLETED AND CONDITION CHK NORMAL</P>)SDR CALA2025082908259Skin · corrodedTAIL AREA, APU INLET DOOR FWD SIDE, CUTOUT H AS EVIDENCE OF CORROSION. REPAIRED STRAP FOR THE AUXILIARY POWER UNIT AIR STA 1825.00 BETW EEN STG 3 TO STA 6 R/H IAW B757-200 53-80-15-2R-1.SDR CALA2025082908258Bear Strap · crackedL1 DOOR SUROUND THE 7TH CRITICAL FASTENER HOLE. COUNTING RT TO LT IAW FIGURE -00 2 OF EA5330-04213 REV D, HAD A CRACK INDICATION AT THE BEAR STRAP L AYER. ACCOMPLISHED REPAIR IAW EA 757-5310-A4078 AND EA 5330-04213 REV D. OPERATION 2 & EC/RA # 5330-07569.SDR AALA202508279624Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON FUSELAGE SKIN AROUND LAVATORY VENT LOCATED FROM BS 907 TO BS 927, FROM S21L TO S22L. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR DALA2025082606339Skin · damagedDAMAGE FOUND ON FUSELAGE BETWEEN FRAMES 1175 AND 1197 LEFT AT STR 20L. REMOVED DAMAGE PER B767 SRM 53-00-01-2R-29 FIG 201. RII PERFORMED HFEC SURFACE SCAN OF CUT OUT AREA PER B767 NDT 51-00-19 NO FAULTS NOTED. C/W INSTRUCTIONS OF ERA 628660- 14 REV ORG SECTISDR SWIA202602275357Skin · dentedDENT ON FUSELAGE SKIN BETWEEN FS349.00 AND FS 364.00 AND BETWEEN STGR 22L AND STGR 23L. (C-CHECK RO 02/25/2026)COMPLIED WITH REO 670-53-21-2681 DATED: 2025-08-28 REV -- PERMANENT DISPOSITION FOR REWORKED DENTS ON LOWER FUSELAGE SKIN BETWEEN FS349.00 - FS409.SDR CALA2025102410501Skin · nickedEXT LOWER FUS SKIN STA 510 STRG 27R-28R WITH NICKS (2EA) C/W REPAIRED EXT LWR FUS SKIN STA 510 STRG 27R-28R IAW SRM 53-00-01-2R-29 CAT B REPAIR. ACCOMPLISHED & VERIFIED IAW SRM 53-00-01-2R-29, PERFORM LFEC & EXTERNAL DETAILED VISUAL INSPECTION.SDR HNAA2025091100605Skin · crackedLH REAR FUSELAGE 2 UPPER SKIN RIVET ON FR77, STGR 6L HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON LH REAR FUSELAGE 2 UPPER SKIN AT FR77, STGR 6L IAW EMB 145 SRM 53-32-01 REF STEP 9 AND PIEDMONT EO1-53-25-0286.SDR AALA202508269039Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER REAR SPAR LEFT EXHAUST CUTOUT DOUBLER CRACKED AT BS 663.75. REPLACED DOUBLER PER SRM 51-40-02.SDR ABXA20250823189Skin · damagedDURING THE CURRENT C-6 HEAVY MAINTENANCE CHK, MAINT FOUND AT BS 871.5, RT FWD OVERWING EMERG EXIT DOOR HAD NICK DAMAGE ABOVE WINDOW-PLUG CUTOUT. FASTENERS REMOVED AT AFFECTED AREA IAW SRM 51-40-02 & DAMAGE BLENDED OUT IAW SRM 52-20-01 RESULTING IN THE FINAL BLSDR REXA2025092500878Doubler · crackedCRACK ON DOUBLER ON FWD EQUIPMENT COMPARTMENT INTERNAL STRUCTURE BTW BS 193, S16L, ADG RESTOW PUMP AREA, DOUBLER ON FWD EQUIPMENT COMPARTMENT INTERNAL STRUCTURE BTW FS 193.00 AND STGR 16L REPLACED IAW SRM 53-11-43-201-001-A01.SDR SWI2025F01325Panel · dentedDUE TO BIRDSTRIKE TO LHS HYD BAY FUSELAGE PANEL, FOUND FORWARD DENTED AREA (NO. 1) MEASURES 5.375" L X 3.875" W X 0.375" MAX. DEPTH AND IS LOCATED BETWEEN THE ELECTRICAL BAY DOOR AND HYDRAULIC BAY ACCESS DOOR, JUST FORWARD OF FS193.00.REF. REO-53-11-2169 FOR DSDR SWI2025F01324Skin · crackedUPON DRESS BACK OF AFT DENTED AREA (NR . 2), OPERATOR REPORTS THAT THE SKIN PANEL WAS CRACKED OVER A LENGTH OF APPROX. 1.25" LONG. ADDITIONALLY, OPERATOR REPORTS THE INTERNAL UPPER STRAP(DWG: CC670-34124, 0.050" NOMINAL THK, REF) TO HAVE BEEN DEFORMED.REF. REOSDR SWIA202509240822Skin · dentedDUE TO BIRDSTRIKE TO LT HYD BAY FUSELAGE PANEL, THE AFT DENTED AREA (NR 2) MEASURES 11.00" L X 6.00" W X 1.75" MAX. DEPTH AND IS LOCATED BETWEEN FS193.00 - FS202.75 & BETWEEN STR16L - STR21L.REF. REO-53-11-2169 FOR DAMAGE REPORT. (FLIGHT 1300 - FILED CLOSSDR REXA2025091800870Skin · wornWEAR ON FUSELAGE SKIN BTW FS 913 TO FS 927 STGR 27. FUSELAGE SKIN BTW FS 913 TO FS 927 STGR 27 WAS REPAIRED PER REO 670-53-00-290 REV. F AND INSPECTION REQUIREMENTS FOR 40,000 FLIGHT CYCLES PER SDIR 670-53-00-290SDR HNAA2025091100609Skin · crackedREAR FUSELAGE 2, SKIN AT FR78 AND BETWEEN STGR 6R-7R AROUND A RIVET HEAD HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2 SKIN AT FR78 AND BTWEEN STGR 6R/7R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0385.SDR HNAA2025091100608Skin · crackedREAR FUSELAGE 2 SKIN AT FR77 AND BETWEEN STGR 6R 7R AROUND A RIVET HEAD HAS A POSSIBILITY CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2 SKIN AT FR77 AND BETWEEN STGR 6R-7R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0285.SDR HNAA2025091100607Skin · crackedREAR FUSELAGE 2, SKIN AT FR77 AND BETWEEN STGR 5R/6R AROUND A RIVET HEAD HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2, SKIN AT FR77 AND BETWEEN STGR 3R/4R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0285.SDR CALA2025090208387Skin · dentedUPPER FUSELAGE DENT APROX .5" FWD OF FR 12 & 1" ABOVE STGR 1L. PERFORMED A DOUBLER REPAIR TO EXTERNAL SKIN AT LOCATION OF DAMAGE FR12 STRG 1L IAW SRM 53-11-11-300-054. THIS IS A CATEGORY B REPAIR.SDR AALA202508262464Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CENTER REAR SPAR RIGHT EXHAUST CUTOUT DOUBLER CRACKED AT BS 663.75. REPLACED DOUBLER PER AARD 51-00-05-1 AND SRM 51-40-02.SDR SWI2025F01119Panel · dentedDUE TO BIRDSTRIKE TO LHS HYD BAY FUSELAGE PANEL, FOUND FORWARD DENTED AREA (NO. 1) MEASURES 5.375" L X 3.875" W X 0.375" MAX. DEPTH AND IS LOCATED BETWEEN THE ELECTRICAL BAY DOOR AND HYDRAULIC BAY ACCESS DOOR, JUST FORWARD OF FS193.00.REF. REO-53-11-2169 FOR DSDR SWI2025F01118Skin · crackedUPON DRESS BACK OF AFT DENTED AREA (NO. 2), OPERATOR REPORTS THAT THE SKIN PANEL WAS CRACKED OVER A LENGTH OF APPROX. 1.25" LONG. ADDITIONALLY, OPERATOR REPORTS THE INTERNAL UPPER STRAP(DWG: CC670-34124, 0.050" NOMINAL THK, REF) TO HAVE BEEN DEFORMED.REF. REO-SDR SWIA2025082500022Panel · dentedDUE TO BIRDSTRIKE TO LHS HYD BAY FUSELAGE PANEL, THE AFT DENTED AREA (NO. 2) MEASURES 11.00" L X 6.00" W X 1.75" MAX. DEPTH AND IS LOCATED BETWEEN FS193.00 - FS202.75 & BETWEEN STR16L - STR21L.REF. REO-53-11-2169 FOR DAMAGE REPORT. (FLIGHT 1300 - FILED OPESDR U2RA2025082100020Skin · crackedDURING A CHECK AT RKSI, WHILE PERFORMING FCD 744-53-0076 R2, 250 FLIGHT CYCLE (FC) REPETITIVE INSPECTIONS FOR SCRIBE LINE FINDINGS ON SB 747-53A2563 LIMITED RETURN TO SERVICE (LRTS) PROGRAM, IT WAS DISCOVERED THAT SKIN PANEL 33L WITH P/N: 65B04135-343 HAVE 02 SDR SWI2025F01588Skin · corrodedFS1051.30 NEXT TO RIGHT SILL HAS CORROSION AS MARKED (C-CHECK RO 11/22/2025)COMPLIED WITH STEPS 1-13 OF REO 670-53-61-2569 REV -- DATE 2025-09-28 STEP 1) ENSURE CORROSION DAMAGE WAS BLENDED TO SMOOTH CONTOUR, STEP 2) INSPECT REWORKED AREA USING LPI OR EDDY CUSDR SWI2025F01587Doubler · crackedCRACK IN RADIUS OF DOUBLER UNDER ADG HYDRAULIC STOW PUMP. (C-CHECK RO 11/22/2025)REPAIRED CRACK IN RADIUS OF DOUBLER UNDER ADG HYDRAULIC STOW PUMP. REF REO 670-53-11-2186 REV -- DATED 2025-10-21 AND REO 670-53-11-509 REV -E DATED 2018-02-08. COMPLIED WITH SKSDR SWI2025F01318Skin · corrodedCORROSION ON INTERNAL SKIN AT STGR 23L-21L FR 88- 89 (C-CHECK RO 09/14/2025)REPAIRED SKIN AT FR 88-89 STGR 21L-23L REF EMB ETD2025-170-926997 REV:/. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. THIS REPAIR IS A TEMP REPAIR AND IS VALID UNTILL AUGUST 21SDR HNAA2025091100606Skin · crackedREAR FUSELAGE 2, SKIN AT FR77 AND BETWEEN STGR 3R/4R AROUND A RIVET HEAD HAS A POSSIBLE CRACK. INSTALLED REPAIR BUSHING ON REAR FUSELAGE 2 SKIN AT FR77 AND BETWEEN STGR 3R/4R IAW EMB 145 SRM 53-32-01 STEP 9 (I) AND PIEDMONT EO1-53-25-0285.SDR SWIA2025082075373Doubler · gougedTWO SMALL SCREW GOUGES ON A DOUBLER AT STGR 27 BETWEEN BS 969 AND 985 ON THE EXTERIOR OF THE AIRCRAFT. COMPLIED WITH REO 670-53-61-352, REV A. REPAIRED THE FUSELAGE SKIN AT BS 977 AND STR 27 BY REMOVING AND REPLACING A NEW SERVICEABLE DOUBLER. MAJOR REPAIR.SDR HNAA2025100300671Skin · crackedF066756 REAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FR 77 BETWEEN STGR 6R / 7R. ACCOMPLISHED BUSHING REPAIR ON REAR FUSELAGE EXTERNAL SKIN AT FR 77 BETWEEN STGR 6R /7R IAW EO1-53-25-0351 AND EMB-145 SRM 53-32-01 RE, ITEM 9, FIGURE 213, SHEETS 1-3.SDR YENA2025082100855Skin · deformedDURING HEAVY MAINTENANCE: DEFORMATION SKIN LOCATED BETWEEN FR 72 TO FR 75 AND STR 31L TO STR 31R JACKING POINT AREA REAR FUSELAGE; (RESOLVED ON W/O: 1391229 TASKCARD: NR-00041 ) PERFORMED PERMANENT REPAIR ON THE AFT FUSELAGE BOTTOM SKIN BETWEEN FR 72 TO FR 75 SDR FDEA202508191507Skin Panel · damagedLH FUSELAGE SKIN BETWEEN STA 368/390 AND STG 26 LH WITH PREVIOSLY REWORK WAS REPAIRED LH FUSELAGE SKIN BETWEEN STA 368/390 AND STG 26 LH IAW SRM 53-00-01-2R REPAIR 12 REV 92 APR 15 2025SDR FDEA202508191501Skin · crackedFUSELAGE RIGHT HAND FUSELAGE AFT OF NUMBER 3 AIRCON DOOR CUTOUT SKIN SUSPECT CRACK ON FASTENER AREA AT STATION 535 BETWEEN LONGERON 32 TO LONGERON 33. FUSELAGE RIGHT HAND FUSELAGE AFT OF NUMBER 3 AIRCON DOOR CUTOUT SKIN CRACK ON FASTENER AREA AT STATION 5SDR JR2R20250819821Skin · corrodedAPU INLET PANEL 351GL SKIN HAS MULTIPLE CORRODED SPOTS.SDR KCSA202508191117Skin · damagedEXTERNAL FUSELAGE SKIN DAMAGE, 2 INCHES AFT OF STA 1580 BETWEEN RS-29/30- 1 INCH LONGSDR SWIA2025081875422Skin · dentedCOMPLY WITH PERMANENT REPAIR ON RA ID: 93923DENT ON RHS FUSELAGE SKIN PANEL BTWN FS185.00 - FS193.00 AND BL0.00 - BL6.10. COMPLIED WITH REO 601R-53-11-3946 NO OTHER DEFECTS NOTED. PERM REPAIR DUE WITH IN 1600 FH. COMPLIED RA93923-REO 601R-53-11-3946 MXCODEID7SDR SWI2026F00019Skin · damagedPERMANENT DISPOSITION FOR BLENDED SKIN AND MISDRILL DAMAGE TO FUSELAGE SKIN BETWEEN FS559+112 €“ FS574.00 & STR15L €“ STR16L., COMPLIED WITH PERMANENT REPAIR ON FUSELAGE SKIN BETWEEN FS559+112-FS574.00, STGR15L-STGR16L, REF. REO 601R-53-61-8417, REV. --, DATSDR SWI2026F00018Skin · damagedPERFORMED TEMPORARY REPAIR TO 4 DAMAGED RIVETS AND 1 BURN MARK ON RH SIDE OF FUSELAGE BETWEEN FS409+16 AND FS409+32, ALSO BETWEEN STR23R AND STR24R. WORK DONE IN ACCORDANCE WITH REO 601R-53-31-1134 REV A DATED: 2020-08-19. COMPLIED WITH EDDY CURRENT INSPECTISDR IPXA2025082531501Skin · bentNLG LEFT CUTOUT PANEL IS BENT AND HAS 2 CRACKS. INSTALLED NEW NLG LT CUTOUT PANEL IAW SRM 51-40-21.SDR IPXA2025090630285Skin · dentedLEFT FWD SIDE OF FUSELAGE HAS 4EA DENTS AFT OF RADOME AT APPROX FS 211 L21L . REMOVED 2EA FASTENERS FOUND WITHIN 0.5" OF DENT PERIPHERY AT LT FUSELGE SKIN BETWEEN FRAMES 199.09/215.25 AND STGR 23L IAW SRM 51-40-02-0G-0. INSTALLED 2EA FASTENERS AT LT FUSELGE SSDR IPXA2025090435259Skin · corrodedTHREE FASTENERS HAVE CORROSION AT LOWER FUSELAGE, APPROX BS 1380- 1385. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-94896-REQ1 AND VT-SAA EA 757-5310-01-B0558 REV IR.SDR FDEA202508181499Skin Panel · damagedPREVIOUS REWORK, RH FUSELAGE SKIN, STA. 654 110, BETWEEN STGRS S-20R AND S-21R, AT 2" FROM STGR S-21R. DAMAGE ON RH FUSELAGE SKIN, STA 654 110, BETWEEN STGRS S-20R AND S-21R, AT 2" FROM STGR S-21R WAS REPAIRED IAW SRM 53-00-01-2R REPAIR 29 FIG 201 (SHEET 1SDR FDEA202508181498Skin Panel · damagedLH FUSELAGE SKIN BETWEEN STA 390/412 AND STG 30 LH WITH PREVIOUSLY REWORK WAS REPAIRED. I.A.W. SRM 53-00-01-2R REPAIR 1. REV. 92 APR 15,2025.SDR FDEA202508181497Skin · damagedPREVIOUS REWORK ON FUSELAGE SKIN, BTW STA 654 66 AND 654 88, STG 39R. FUSELAGE SKIN, BTW STA 654 66 AND 564 88, STG 39R. WAS REPAIRED I.A.W. SRM 53-00-01-2R, REPAIR 1 FIG 201 SHEET 2 REV.92 APR 15 2025.SDR DALA2025081906189Skin · damagedFUSELAGE SKIN DAMAGE FS 887 BTWN S-26L AND S-27L. C/W ERA 628536-14 REV ORIG FUSELAGE SKIN DAMAGE FS 887 BTWN S-26L AND S-27L. ENSURED PRI 628536-14 REV 0,1,2,3 MATCHES ERA 628536-14 REV ORIG.SDR IXXA20250818002Skin · dentedSTA 1576 STR 15L NEW DENT ON AFT FUSELAGESDR AALA202509058701Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXTERNAL SKIN GOGO ANTENNA DOUBLER / COVER PLATE BETWEEN FR 56 AND FR 57, BETWEEN S42L AND S43L. REPLACED GOGO ANTENNA DOUBLER / COVER PLATE PER SRM 51-72-11.SDR DALA2025081906184Skin · dentedDENT DAMAGE TO THE FUSELAGE SKIN SUSTAINED IN BOS. THE DENTED AREA EXISTS BETWEEN STA 891-902 AND BETWEEN STRINGERS 26L TO 27L. MAINTENANCE REPAIRED DAMAGE PER ERA 628536-14.SDR CALA2025081907929Skin · dentedSHARP DENT ON LOWER CENTER OF EMPANNAGE APPROXIMATELY 10 INCHES FWD OF THE APU AIR INLET STRUCTURE. PERFORMED SKIN REPAIR IAW A320 SRM 53-51-11-300-082 REPAIR REQUI RES REINSPECT AT 60,000 FC / 120,000 FH FROM TIME OF ADL/REPAIR EMBODIMENT SUBSEQUENT INSPECT
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