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 AALA202503204398Skin · crackedAIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACK FOUND RADIATING FROM FASTENER HOLE ON NOSE SKIN PANEL AT RIGHT HAND FR 13/14 AND Z+780 - Z+950. REPAIRED SKIN PANEL PER EA 362921SDR CALA2025031902958Skin · corrodedSUPPORT TASK: E&E BAY BETWEEN STA 360 - 382 STR 27L IS CORRODED. ON INSPECTION FOUND EXFOLIATED CORROSION .002 LOSS. REMOVED CORRODED SECTION OF STRINGER FROM STA 368 388. FABRICATED NEW REPAIR STRINGER SECTION. REPAIR SPLICES AND SHIMS IAW B737 SRM 53-00-53-SDR JR2R20250318089Doubler · corrodedAFT LAV SERVICE DOOR CUT-OUT, INNER SKIN DOUBLER BY HINGE HAS CORROSION OUT OF LIMITS.SDR SWI2025F01149Skin · corrodedAVIONICS BAY INTERNAL SURROUND STRUCTURE CORROSION ON INNER SKIN FORWARD OF FS364.00 FRAME BETWEEN INTERCOSTAL STGR 26L AND 27L. REPAIRED AVIONICS BAY INTERNAL SURROUND STRUCTURE INNER SKIN FORWARD OF FS364.00 FRAME BETWEEN INTERCOSTAL STGR 26L AND 27L BY COMSDR NKVA2025032017Deck Plate · crackedDURING INSPECTION AT AFTT: 21628.9, A CRACK WAS FOUND ON THE RH TITANIUM DECK, ON THE FRONT AREA OF THE FORWARD SEATING PLANE OF THE MGB FLEXIBLE MOUNTING PLATE. THE MANUFACTURER ISSUED AN ENGINEERING REPORT ALLOWING CONTINUED OPERATION FOR UP TO 500HRS WITH CSDR QXEA2025031900063Skin · canningWHILE PERFORMING ETD2023-170-015226-3 REPAIR OF FWD FUSELAGE LOWER SKIN, DAMAGED AREA FOUND TO HAVE OIL CANNING PRESENT. CUT OUT DAMAGED AREA BETWEEN FR 16-17 AND STGR 23L AND 24L. INSTALLED FABRICATED FILLER AND DOUBLER. REF SRM 53-10-01-02-12-REPAIR 12P.SDR CALA2025031802933Doubler · damaged?DOUBLER PREVENTATIVE MOD TO THE L1 DOOR SURROUND FWD UPPER CORN ER WAS INSTALLED PER EA 5330-04213 REV D W/ DEVIATIONS NOTED IN EC/RA #: 5330-07481. ACP INSP REQUIREMENTS PER PART 2 OF THE LAT EST REV OF EC/RA #: 5330-07481 AT FUSELAGE REINFORCED AREA (P/N 14SDR DALA2025031802034Skin · dentedSHIP 3360 L/H FUSELAGE FR32 STGR34 TO STGR 35 DENT. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-21-11-300. (0862398)SDR JGVR20250317003Skin · corrodedBLENDED AREA OF CORROSION FROM FUSELAGE SKIN LOCATED AFT OF E-EXIT DOOR OPENING, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS BY CLEANING, TREATING AND PRIMING IAW NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR AALA202503204383Skin · crackedAIRCRAFT IN BASE MAINTENANCE: FATIGUE CRACK FOUND RADIATING FROM FASTENER HOLE ON NOSE SKIN PANEL AT LEFT HAND FR 13/14 AND Z+780 - Z+950. REPAIRED SKIN PANEL PER EA 362923.SDR DALA2025031802033Skin · nickedSHIP 3315 NICK FOUND ON FUSELAGE SKIN BETWEEN FR57.1 AND 57.2 AND STR 37RH. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-41-11-300-015. (0861447)SDR R61A2025031800141Skin · damagedBIRD STRIKE ON FOWARD FUSELAGE BETWEEN FRAME 1 AND FRAME 2 BETWEEN STR 26 L AND 27 L. INSTALLED FILLER AND DOUBLER IAW ETD2025-170-904080 ALSO REF VP-011298-2025 N/R #5 FOR WORK ACCOMPLISHED.SDR NACA2025031500003Skin · corrodedSKIN CORRODED , R/H AFT FUSELAGE UPPER OF H.S.T INBD STA 1725.5 - STA 1788.SDR AALA202504033921Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT LEFT RAM AIR INLET AT STA 540, S23L. ACCOMPLISHED DOUBLER REPAIR PER EA 363281.SDR UIEA2025031900246Skin · corrodedFUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP BROKEN AND WITH CORROSION.(<P>FUSELAGE SECTION 48, APU INTAKE DOOR CUTOUT, UPPER STRIP WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 127 15DEC24. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025030194201Skin · crackedFWD ENTRY DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLE 3 ON SKIN AT APPROX 10 O´CLOCK. AND CRACK INDICATION AT HOLE 4, THROUGH THE HOLE (SKIN AND BEAR STRAP) APPROX. 10 O´CLOCK AND CROSS DOWN.(<P>FWD ENTRY DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLESDR UIEA2025030400198Skin · crackedFWD SERVICE DOOR, AFT LOWER CORNER, CRACK INDICATION AT HOLE 3 ON SKIN AT APPROX 2 O´CLOCK AND CRACK INDICATION AT HOLE 4, THROUGH THE HOLE (SKIN AND BEAR STRAP) APPROX. 2 O´CLOCK AND CROSS DOWN AND AT 4 O´CLOCK.(<P>CRACK AT HOLE 4 THROUGH THE HOLE APROX. 2SDR UIEA2025022000157Skin · corrodedUPPER LOBE INTERIOR STRUCTURE, ON BODY STA 1021, BETWEEN STR 19 AND 20 RH, A CORROSION L=0.5" W=0.5"(<P>UPPER LOBE INTERIOR STRUCTURE, ON BODY STA 1021, BETWEEN STR 19 AND 20 RH CORROSION LEVEL 1 WAS REWORKED, INSPECTED, EVALUATED AND WITHIN ALLOWABLE LIMITS ISDR ASAA2025031556595Skin Panel · corrodedCORROSION ON SKIN AT STR 4L AND BETWEEN STA 947.5 AND STA 967. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANELS 147A3300-1 AND 147A3110-1 BETWEEN STA 947.5 1016 STGR 4L IAW EA 800-53EA -28395REV00. INCLUDES MIG-5 NR SA0424SDR ASAA2025031556594Skin Panel · corrodedCORROSION ON SKIN AT STR 4L AND BETWEEN STA 947.5 AND STA 967. SRXR430X. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR TO FUSELAGE SKIN PANELS 147A3300-1 AND 147A3110-1 BETWEEN STA 947.5 1016 STGR 4L IAW EA 800-53EA -28395REV00. INCLUDES MIG-5 NR SA0424SDR R61A2025031700140Skin · dentedFOWARD FUSELAGE DENTED BETWEEN FRA 17 TO FRA 18 AND STR 20R TO 21R FROM BAGGAGE CART. INSTALLED FILLER AND DOUBLER IAW ETD2025-170-904037,ALSO REF VP-006377-2025 N/R # 7 FOR WORK ACCOMPLISHED.SDR KCSA202503151037Skin · damagedFOUND EVIDENCE OF LIGHTNING DAMAGE AT BL 2020, WL 118SDR KCSA202503151036Skin · damagedPOSSIBLE EVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN STA 460 IN BETWEEN LS-5 & LS-6SDR KCSA202503151035Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE FASTENER STA 720 IN BETWEEN LS-17 & LS-18SDR KCSA202503151034Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN STA. 1080 IN BETWEEN LS-16 & LS-17SDR KCSA202503151033Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN STA 1100 IN BETWEEN LS-16 & LS-17SDR KCSA202503151031Skin · damagedEVIDENCE OF LIGHTNING STRIKE ON FUSELAGE SKIN STA. 640 IN BETWEEN LS-7 & LS-8SDR KCSA202503151030Skin · damagedLIGHTNING STRIKE FOUND AT APPROX. 540 WL 130 LH SIDE OF FUSELAGESDR KCSA202503151029Skin · damagedLIGHTNING STRIKE FOUND AT APPROX 587 WL 130 LH SIDE OF FUSELAGESDR KCSA202503151028Skin · damagedLIGHTNING STRIKE FOUND AT APPROX. STA 550 WL 130 LH SIDE OF FUSELAGESDR KCSA202503151027Skin · damagedFOUND EVIDENCE OF LIGHTNING STRIKE AT STATION 2100, WATER LINE 122SDR KCSA202503151026Skin · damagedFOUND EVIDENCE OF LIGHTNING STRIKE AT STATION 2080, WL 118SDR KCSA202503151025Skin · damagedFOUND EVIDENCE OF LIGHTNING DAMAGE AT STATION 2060, WL 118SDR SWIA2025071100314Skin · dentedDURING THE AUDIT OF 1C TASK CARD 53-900-304, EXTERNAL ZONAL INSPECTION OF THE REAR FUSELAGE FS 977.0 TO 1098.2 BELOW WL 72.5, FOUND DENTS AND SCRATCHES BELOW AND AFT OF THE LOW-PRESSURE AIR GROUND CONNECTION DOOR THAT NEEDS EVALUATED AND REPAIRED. (C-CHECK RO SDR SWIA20250508314Skin · chafedBOTTOM FUSELAGE SKIN CHAFFED AFT OF FS977.00 AT STR27 (C-CHECK RO 05/08/2025)PERFORMED REPAIR AREA ON BOTTOM FUSELAGE SKIN FS977.00 STR27 IAW MHI RJ REO 670-53-00-290 REV-F DATE: 2019-04-26, CRJ700 SRM 51-25-01. PERFORMED INSPECTION BY BARON NDT, LLC FAA CRSSDR SWAA2025042205477Plate · corrodedCORROSION PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT 2025-202769 <[01]. REPLACED PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING # 1SDR IPXA2025031742006Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR. BLENDED AREA WITHIN ALLOWABLE LIMITS AND RESTORED FINISHED TO THE REQUIREMENTS OF SRM 53-10-12 REPAIR 6.SDR IPXA2025031741956Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING. PERFORMED A DVI AT STATION 2410 35 INCHES BELOW WING RIGHT HAND SIDE. AT ORANGE TAPE THERE WAS A BLACK SPECK ON FUSELAGE. WIPED ENTIRE AREA DOWN WITH ACETONE. NO LIGHTNING STRIKE NOTED ISDR IPXA2025031442006Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE BETWEEN FR 23 AND 24, 37 INCHES BELOW LWR FWD CARGO DOOR.SDR IPXA2025031441956Skin · damagedLIGHTNING STRIKE DAMAGE ON FUSELAGE RT SIDE AT 2410 35€? BELOW WING.SDR KCSA202503141024Skin · damagedEVIDENCE OF LIGHTNING DAMAGE AT STATION 2030, WL118SDR KCSA202503141023Skin · damagedFOUND EVIDENCE OF LIGHTNING STRIKE AT STA 466, WATER LINE 132SDR FDEA202503140398Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN FR19-FR20A S37R-S42R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE SKIN FR19 - FR20A S37R - S42R WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH FEDEX DRAWING S30-53-001 REV.D AND A300-600F SRM 53-13-1SDR FDEA202503140397Skin · misrepairedEXISTING REPAIR ON FUSELAGE SKIN FR61-FR64 S42L-S45L REQUIRES EVALUATION FOR CONFORMITY. EXISTING REPAIR ON FUSELAGE SKIN FR61 - FR64 S42L - S45L WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600 SRM 53-10-12 FIG 213. DUE TO SOME DEVIATIONS WERE FOUNSDR KCSA202503141022Skin · damagedFOUND EVIDENCE OF LIGHTNING STRIKE AT STA 430 WATER LINE 130SDR SWIA2025090900313Skin · corrodedSKIN AROUND DRAIN HOLES ON FUSELAGE LOWER SKIN HAVE CORROSION AT APPROXIMATELY FS945.00 BETWEEN STGR26L AND STGR26R AS MARKED (C-CHECK RO 09/07/2025)REMOVED CORROSION ON SKIN AROUND DRAIN HOLES ON FUSELAGE LOWER SKIN AT APPROXIMATELY FS945.00 BETWEEN STGR26L SDR SWIA20250514313Skin · damaged** MAJOR REPAIR ** FUSELAGE SKIN DAMAGED AFT OF THE AFT CARGO DOOR. (FILED CLOSED) PERFORMED A TEMPORARY REPAIR TO THE FUSELAGE SKIN JUST AFT OF THE AFT CARGO DOOR BETWEEN FRAMES 80-82 AND STRINGERS 22R-24R IN REFERENCE TO ETD2025-170-903877 REV: A. THSDR ASAA2025031356604Skin · corrodedCORROSION AT STR 14R AND BETWEEN STA 767 AND STA 807 SRXR430R. 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 SRX430R.SDR ASAA2025031356603Skin · corrodedCORROSION AT STR 14R AND BETWEEN STA 767 AND STA 807 SRXR430R. 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 SRX430R.SDR DALA2025031702015Skin · dented(LOG 0856374) DURING INSPECTION OF THE FUSELAGE SKIN PANEL (P/N 147A3110-51), A CREASED DENT WAS FOUND AT BS 1010 ABOVE S-13L. DENT REPAIRED PER ERA 624682-14.
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