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 ASAA2025031356592Skin Panel · corrodedCORROSION AT STR 14R AND BETWEEN STA 747 AND STA 767 SRXR430X. GROUNDED - YES. RCATEGORY "A" MINOR REPAIR ON SKIN AT STR 14R BETWEEN STA 727J AND STA 767. ACCOMPLISHED ON MIG-5 N/R SA042450 IAW EA800-53-28380 REV00 SKIN P/N 146A3151-94, 146A3151-32 SRXR430X.SDR ASAA2025031356583Skin Panel · corrodedCORROSION AT STR 14R AND BETWEEN STA 767 AND STA 807 SRXR430X. GROUNDED - YES. CATEGORY "A" MINOR REPAIR ON SKIN AT STR 14R BETWEEN STA 767 AND STA 807. ACCOMPLISHED ON MIG-5 N/R SA042450 IAW EA800-53-28380 REV00 SKIN P/N 146A3151-94 SRXR430X.SDR SWIA202503140013Skin · damaged** MAJOR REPAIR ** FUSELAGE SKIN DAMAGED AFT OF THE AFT CARGO DOOR. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR DALA2025031401974Skin · damagedABRASION ON FORWARD SKIN PANEL AT SECTION 48 RH SIDE AT STA 1725 BETWEEN S-15 RH AND S-22 RH. THE ABRASION WAS REMOVED AND MEASURED: ORIGINAL THICKNESS=0.080", MIN REMAINING THICKNESS IS 0.046", FOUND OUT OF LIMIT PER B767-400 SRM 53-80-70-1A-1 FIG 101 REV 73.SDR DALA2025031401973Skin · damagedABRASION BETWEEN S-15 LH AND S-22 LH FORWARD SKIN PANEL SECTION 48 LH SIDE AT STA 1725. THE ABRASION REMOVED AND MEASURED: ORIGINAL THICKNESS: 0.080", MIN REMAINING THICKNESS: 0.045", FOUND OUT OF LIMIT PER B767-400 SRM 53-80-70-1A-1 FIG 101 REV 73.00 21AUG24.SDR DALA2025031401972Skin · damagedABRASION ON LWR SKIN PANEL SECTION 48 BEHIND SEAL PANEL 313CLX BETWEEN STA 1725 AND STA 1746, S22L. THE ABRASION WAS REMOVED AND MEASURED: THE ORIGINAL THICKNESS T= 0.080", THE DEPTH OF CLEANUP X=0.056">20%T, FOUND OUT OF LIMIT PER B767-400 SRM 53-80-70-1A-1 RSDR 6VAR202503131001Skin · corrodedCARRIED OUT MAJOR REPAIR OF LH FUSELAGE SKIN FOR CORROSION BEHIND MAIN CARGO DECK SCUFF PLATE AT STA 588-654, STR 19-22LHSDR IXXA2025031303Skin · crackedRIGHT FUSELAGE SKIN AND BEAR STRAP R1 DOOR CUTOUT LOWER CORNER STA 334 STRINGER 20R CRACKSDR SWAA2025031704309Doubler · bulgedSUPPLEMENTAL INFORMATION: RING AROUND TOILET SERVICE PANEL ON AFT FUSELAGE HAS BULGE ON LOWER AFT CORNER. REMOVED 1 EA FASTENER AT LWR AFT CORNER OF TOILET SERVICE PANEL TO FACILITATE INSPECTION PER SRM 51-40-02. REPIRED REF EA# 25-153-00638, C/W E/A 25-15SDR SWIA20250418001Doubler · gougedUPON OPENING UPPER SKIN FOR ACCESS TO REPLACE MISSING FASTENER COLLAR (MX 29731975 HN00223848, EXISTING DAMAGE FOUND, THE INNER DOUBLER FOUND GOUGED THROUGH IN SEVERAL SPOTS. (C-CHECK RO 04/17/2025)THE R/H ELEVATOR DOUBLER (PN 601R24026-35) THAT WAS DAMAGED FRSDR VNAA202504140020Skin · wornSKIN, FUSELAGE BETWEEN FS 1031.00-FS1051.30 & STR21R-STR26R PERFORM INSPECTION EVERY 15800 FC FROM INITIAL REPAIR PER STS EA 48-2019-090 REV A. SKIN, FUSELAGE BETWEEN FS 1031.00-FS1051.30 & STR21R-STR26R WAS REPAIRED PER REO 690-53-61-1531 REV.--SDR QXEA2025040800099Doubler · corrodedDOUBLER I/B OF TEXAS DOUBLER ON FRAME 90 IS CORRODED REMOVED AND REPLACED DOUBLER IAW E175 SRM 51-40-08SDR QXEA2025040800097Doubler · corrodedFWD CARGO MODE S2 ANTENNA INTERNAL SKIN DOUBLER CORRODED. REMOVED AND REPLACED DOUBLER IAW E175 SRM 51-40-08SDR QXEA2025040800096Doubler · corrodedFWD CARGO MODE S1 ANTENNA INTERNAL SKIN DOUBLER CORRODED. REMOVED AND REPLACED DOUBLER IAW E175 SRM 51-40-08SDR QXEA2025040800091Doubler · corrodedANTENNA SKIN DOUBLER CORRODED BETWEEN FR23-24 STR28L REMOVED AND REPLACED DOUBLER IAW E175-SRM-51-40-08SDR R61A2025033000167Skin · corrodedCF3 FLOOR STRUCTURE CORROSION FOUND ON SEAT TRACK INBD LH TRACK BTWN FR84-85. MX REPAIRED TRACK IAW SRM 53-23-10 REPAIR 04.SDR 2025F00062Skin · dentedTHE L/H UPPER FUSELAGE BETWEEN STA-218 AND STA-237 HAS STRUCTURAL DAMAGE.SDR DALA2025031602003Skin · corrodedSHIP 3166 REPORTED CORROSION AROUND THE LAV OUTLET VENT, AT APPROXIMATELY 7.6 INCH AFT OF FR 69. CORRECTIVE ACTION: COMPLIED WITH ER/A 624952-14. (0854158)SDR DALA2025031201923Skin · nickedSHIP 3351 NICK AT AFT CGO DOOR SURROUNDING SKIN AT 14" AFT FR65. 6" BELOW STGR 35RH. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-41-11. (0853762)SDR IPXA2026030286670Skin · ground damageMAJOR REPAIR. DAMAGE TO FUSELAGE SKIN ABOVE AFT CARGO DOOR CONTROL PANEL AT LAP SEAM CAUSED BY CARGO LOADER RAIL. FINAL CHECKED OK.SDR AALA202505307437Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION EXTERNAL FUSELAGE SKIN BETWEEN FR 69 TO FR70 AND BETWEEN S1L AND S3L. REPAIRED SKIN PANEL PER EA 364324.SDR IPXA2025032474279Bear Strap · crackedCRACK, FWD ENTRY DOOR AFT LOWER CORNER BEAR STRAP.(REPAIR). I.A.W AMM 25-80-00-400-803 REV.144 INSTALL FORWARD CARGO INSULATION BLANKET AT STA 303 ~ 368 AND CONDITION CHECK NORMAL. INSTALLED THE CENTER SCUFF PLATE I.A.W AMM 53-13-01-424-005-REV.144. COMPLETSDR CALA2025031302764Skin · damaged4634 FR35 STGR30RH PREVIOUS REPAIR MULTIPLE FASTENER HOLE DISCREPANCIES FOUND DURING RE-INSPECTION OUTLINED IN ECRA 5330-06963. REF LOG PAGE 8992357. ACCOMPLISHED INTERIM REPAIR IAW ECRA 5330-07480 WITH NO DEVIATION. ACCOMPLISH A PERMANENT REPAIR ON THE FR35 SSDR DALA2025031201902Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH WAS REPAIRED PER B717-200 SRM 53-10-01-2R, PROCEDURE 10, REPAIR 10, FIGURE 2SDR DALA2025031201901Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH (DECAL LP 4245810). SUMMARY OF NRC 00844: EXTERNAL FUSELAGE SKIN BTW STA Y=229-237 BTW ANG LONG 17LH TO 18LH WAS REPAIRED PER B717-200 SRM 53-10-01-2R, PROCEDURE 10, REPAIR 10, FIGURE 2SDR N6WA2025031101Skin · corrodedCORROSION ON SKIN REPAIR DOUBLER AT FS939.00 - FS953.00 TO STRINGER 17R - 18R. REPLACED FUSELAGE SKIN REPAIR DOUBLER IAW GOJET EO C550-53MR-059-O.SDR DALA2025031101894Skin · damagedSKIN DAMAGE FOUND AT TWO LOCATION OF FUSELAGE STA 1746 BETWEEN S-36L AND S-36R. PERFORMED REPAIR ON FUSELAGE SKIN STA 1746 BETWEEN S-36L AND S-36R AS PER PRI 624841-14 REV O. COMPARE AND COMPLIED WITH ER/A 624841-14 REV ORIGINAL. NO DEVIATION. ASSOCIATED ER/A SDR DCGA2025081900550Skin · corrodedLIGHT CORROSION SPOTS FOUND ON LEFT AND RIGHT HAND FUSELAGAGE SKINS UNDER STAILESS ENGINE DECK. LH SKIN PART NUMBER 350A21-1022-127 AND RIGHT-HAND SKIN PART NUMBER 350A21-1022-128SDR IPXA2025032556614Skin · crackedDURING PFM J/C:EO-24301-JIC001 FOUND SKIN CRACK AT STA 1725.50 NEAR S-7R.(REPAIR). ACCOMPLISHED REPAIR I.A.W EO-93158-REQ1 REV1.SDR IPXA2025031356614Skin · crackedDURING PFM J/C:EO-24301-JIC001 FOUND SKIN CRACK AT STA 1725.50 NEAR S-7R.(REPAIR) I.A.W. EGAT W/S NO.50164 PAGE:4 OF 16 STEP:11 TABLE:II (PAGE:11 OF 16) PART NO.8 & 9, COMPLETED TO MACHINE THE FILLER AT STA 1725.50 NEAR S-7R.SDR R61A2025031300139Skin · dentedBIRD STRIKE ON FWD FUSELAGE LH SIDE FWD OF FRAME 4 BETWEEN STR 22 L AND 24 L. REPAIRED IAW ETD2025-170-903719 ALSO REF VP-010399-2025 N/R #4 FOR WORK ACCOMPLISHED.SDR DALA2025031201956Skin · cracked(LOG 0850873) DURING C-CHECK INSPECTIONS CORROSION AND CRACK WERE FOUND AT THE FUSELAGE SKIN LOWER EDGE OF THE LAVATORY VENT CUTOUT AT STA 917 BETWEEN STRINGERS S-21L AND S-22L. REPAIRED DAMAGE PER ERA 624846-14.SDR DALA2025031101892Skin · corroded-AD- CORROSION ON AFT EDGE LOWER SKIN OF WING BOX STA Y=747 X=15-25 RH AT RH MLG W/W AREA. SUMMARY OF NRC 00670: CORROSION LEVEL 1. CORROSION ON AFT EDGE LOWER SKIN OF WING BOX STA Y=747 X=15-25 RH AT RH MLG WAS REPAIRED PER ER/A 624679-14AD REV ORIGINAL SECTISDR DALA2025031101888Skin · corrodedCORROSION ON INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00183: CORROSION LEVEL 2. INNER SKIN PANEL FROM STA Y=657 TO Y=636 BTW L29L AND L29R, STA Y=588 L30 AT FWD CARGO COMPARTMENT WAS REPSDR DALA2025031001823Skin · crackedCRACK EVIDENCE ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L. SUMMARY OF NRC 0180: AREA WAS REPAIRED ON FUSELAGE SKIN LOCATED ON STA Y=1037 AND L-14L PER PRI 624765-14 REV 2 AND PER ER/A 624765-14 REV ORIG SECTION I. REPAIR APPROVAL IS LIMITED TO 24 MONTHS SDR IXXA2025031001Skin · crackedRT FUSELAGE SKIN AND BEAR STRAP AT R1 DOOR CUTOUT LOWER CORNER STA 335 CRACKEDSDR 2025FA0000179Skin · mechanic errorREPAIR - MISDRILLED DAMAGE ON OUTER SKIN, R/H STA 412, STR 16R.SDR 2025FA0000174Skin · not reportedREPAIR - SECTION 46 - FUSELAGE SKIN AT STA 1461, BETWEEN STR-30L AND STR-31L.SDR 2025FA0000173Skin · not reportedREPAIR - SECTION 46 - FUSELAGE SKIN AT STA 1480, BETWEEN STR-20L.SDR 2025FA0000171Skin · not reportedREPAIR - SECTION 46 - FUSELAGE SKIN BULK CARGO DOOR CUTOUT AFT SECTION AREA AT STA 1418, BELOW STR-30L.SDR 2025FA0000164Skin · corrodedREPAIR - CENTER WING SECTION, UPPER SKIN PANEL, CORROSION DAMAGE, U-14C, LBL83.SDR JJBA20250507030Doubler · corrodedCORROSION AROUND WATER SERVICE TUBING ON FUSELAGE DOUBLER PLATE. BLENDED CORROSION ON WATER SERVICE DOUBLER PLATE. DIMENSIONS FOR THE BLEND OUT IS 1.5"X.75"X.25" ORIGINAL THICKNESS IS .063" REMAINING IS .038" AND IS DETERMINED TO BE OUT OF LIMITS. REMOVED DOUBSDR VNAA202504140010Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BTWN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E) INTERNAL PRODUCTION DOUBLER IN STA. FS= 295 TO FS= 310 BTWN STGR 26LH TO 26RH AT MAIN AVIONICS COMPARTMEN WAS EVALUATED OUT OF LIMISDR DALA2025031201942Skin · corroded(LOG 0848137) CORROSION EXTERNAL SKIN AT LEVEL BS 540 BTW STR 28R TO STR 28L AT LOWER FUSELAGE. PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN AT LEVEL BS 540 BTW STR 28R TO STR 28L AT LOWER FUSELAGE AS PER ER/A 623918-14AD REV ORIGINAL.SDR CALA2025031002659Skin · corrodedAFT OF FWD CARGO COMPARTMENT A/C BAY BILGE SKIN CHECK FUS CUTOUT SURROUNDING AREA CORROSION BETWEEN STA 520 AND STA 540. REF AAR N/R 9939574.SDR ASAA2025030856831Skin · corrodedCORROSION ON FUSELAGE SKIN AT STGR 23L AND BETWEEN STA 967 AND STA 1016 IN 4 PLACES SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO FUSELAGE SKIN PANELS 147A3110-3 AND 147A3400-4 BETWEEN STA 967-1016 STGR 23L IAW EA# 800-53EA-28287 REV 00 SSDR SWIA202503200008Skin · damagedPOST REMOVAL -HIDDEN DAMAGE AFTER REMOVAL OF AFT HEATED DRAIN MAST FOUND CORROSION ON FUSELAGE SKIN AND INTERNAL DOUBLER AT MOUNTING AREA (C-CHECK RO 03/19/2024)REMOVED AND REPLACED INTERNAL DOUBLER BETWEEN FRAMES 86-87 REF SRM 51-40-08. RESTORED SURFACE PROTESDR QXEA2025031000060Skin · damagedFLIGHT 2045. TWO LARGE BIRD STRIKES ON NOSE AREA NEAR PITOT TUBES ON LEFT AND RIGHT SIDE OF AIRCRAFT ON DESCENT. AIRCRAFT REMOVED FROM SERVICE.DENT ON FUSELAGE FR03-02 AND STR 20R-22R MEASUREING 6.5”AT ITS LONGEST X 3.6”H X 0.1” DEPTH. NO CRACKS. DENT ON FUSELSDR R61A2025030800132Skin · damagedDURING HEAVY CHECK FOUND LIGHTING STRIKE FOUND ON FWD FUSELAGE SKIN. REPAIRED SKIN IAW ETD2025-170-90-2651SDR R61A2025030800127Doubler · corrodedDURING HEAVY CHECK FOUND FWD. CARGO SKIN DOUBLER FOR DME ANTENNA HAS LEVEL 2 CORROSION. REPLACED DOUBLER IAW SRM 51-41-02
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