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 MASA20240705016Skin · damagedBIRD STRIKE: MAJOR REPAIR: LH FWD LOWER SKIN DAMAGED AT FS193-202. LH FWD LOWER SKIN REPLACED AT FS193-202 PER: RO# CRJS-53-5311SDR MASA20240705015Skin · dentedDENT ABOVE RH PILOT PROBE IN RVSM AREA AFTER BIRDSTRIKE. REMOVED AND REPLACED RH UPPER SKIN FS202-280 (DENT ABOVE RH PILOT PROBE IN RVSM AREA) PER RO# CRJ9-53-5313SDR MASA20240705014Skin · dentedDENT IN SKIN PANEL AFTER BIRDSTRIKE BETWEEN FS177.00- FS185.00 BELOW ADG BAY. C/W DRESS-BACK OF DENT IN SKIN PANEL BETWEEN FS177.00 - FS185.00 BELOW ADG BAY PER RO# CRJ9-51-4379SDR MASA20240705013Skin · damagedRH FWD SKIN DAMAGED AFTER BIRDSTRIKE AT FS 193-202/REPLACED LH FWD LOWER SKIN PER RO# CRJS-53-5312SDR CALA2024051301455Skin · corrodedAFT. UPPER FUSELAGE, ELT ANT. HAS CORRODED/ SMOKING RIVETS PART I. ELT ANTENNA UPPER FUSELAGE SKIN, BETWEEN FR64 - FR65 AND BETWEEN STGR 1LH AND STGR 1 RH, PERMANENT REPAIR IAW EC/RA # 5341-01453 .SDR IPXA2024040866276Skin · gougedSKIN GOUGE RH FUSELAGE APPROX 26€? FORWARD OF LOWER FWD CARGO DOOR. (APPROX. FUSELAGE STATION 453 BETWEEN STRINGER 26R & 25R). MARKED WITH TAPE. REINSTALLED SAME SERVICEABLE FWD.LOWER CARGO COMPARTMENT SIDE WALL PANEL I/A/W B767 AMM 25-52-01SDR IPXA2024040166276Skin · gougedSKIN GOUGE RH FUSELAGE APPROX 26€? FORWARD OF LOWER FWD CARGO DOOR. (APPROX. FUSELAGE STATION 453 BETWEEN STRINGER 26R & 25R). MARKED WITH TAPE. MATERIAL ID & TRACEABILITY AS FOLLOWS:<BR>2024-T3 .071 PO# SP2730176<BR>2024-T3 .080 PO# SP2668300<BR>2024-T3 .040SDR CALA2024040400976Access Panel · missingPDA 1 PANEL 196CR (GROUND AIR CONDITIONING PANEL) DELAMINATED AND 12X37 AREA BROKE OFF. REF IPC 53-96-51 ITEM 370. REF TO LOGPAGE 7519283.SDR SCNA20240429230Doubler · crackedLOWER FUSELAGE EXTERNAL POWER RECEPTACLE DOOR CUTOUT AREA INTERNAL DOUBLER CRACKED. REPLACED INTERNAL DOUBLER PN: 141A3722-12SDR SWIA2024052000330Skin · gougedFUSELAGE EXTERNAL SKIN HAS A GOUGE AT FS977 AT STR 27 (C-CHECK RO 5/20/2024) REPAIR FUSELAGE EXTERNAL SKIN AT F.S.977 STR.27 IAW CRJ700 SRM 51-42-21,53-51-01,AND MHIRJ REO 670-53-00-290 REV.-F DATED 2019-04-26, NO DEFACTS NOTED AT TIME OF INSPECTION,SEE RSDR DALA2024040204012Skin · damaged(LOG 5414548) SKIN DAMAGE AT BS 500 + 13.5 3 " ABOVE STRG 20R. PERFORMED REPAIR ON SKIN DAMAGE AT BS 500+ 13.5 3" ABOVE STGR 20R IAW SRM 53-00-1-2R PROCEDURE 3 REPAIR 3.SDR SWIA20240419329Skin · gougedDAMAGE 4 & 5) GOUGE MEASUREMENTS 9.5 INCHES LONG AND 0.5 INCH WIDE. DEPTH IS FROM 0.005 INCH TO 0.059 INCH DEEP. LOCATED 0.5 INCH AFT OF FS 421 BETWEEN STGR24R AND STGR 27.DAMAGE 5) GOUGE 13.5 INCHES LONG AND 0.5 INCH WIDE DEPTH NOT MEASURED, DUE TO ALL BEING SDR DALA2024040404066Skin · dented(LOG 0272631) DENT ON EXTERNAL FUSELAGE STA 887 BETWEEN STRGR S14L AND S15L. DENT ON EXTERNAL FUSELAGE STA 887 BTW STGR S14L AND S15L WAS REPAIRED I.A.W. B738-800ER/A 616607-14.SDR DALA2024040204027Skin · unknownSHIP 699 DTE, ERA 616137-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE PARTIAL SKIN REPLACEMENT BETWEEN BS 585-635 AND STRINGERS 13L-20L. CORRECTIVE ACTION: REF ERA 616137-14. (0267126)SDR DALA2024040204021Skin · corrodedSHIP 5656 CORROSION ON INTERNAL SKIN STA 1790 BTW STRINGER 3R/S4R AT AFT ACCESORY COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00118: STRAP ON INTERNAL SKIN STA 1790 BTW STRINGER 3R/S4R AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B757-200 SRM. (0267884)SDR UIEA2024032600228Skin · dentedRH SIDE SECTION 46 13" AFT MIDWAY UP FROM AFT CARGO DOOR CUTOUT 3" X 3" CIRCULAR BLEND. REPAIR IAW SRM 51-10-02 AND SRM 51-20-01 REV 42 DATE 20 FEB 2024 AND RI-53-60-16802 REV A. NO FURTHER DEFECTS NOTED.SDR DALA2024040203969Skin · unknownSHIP 5657 PENDING FAA APPROVAL ERA 614858-14 REV. B FUSELAGE / SKIN / FS508-FS520, S-28L TO S-28R. CORRECTIVE ACTION: REF ERA 614858-14SDR MASA20240401004Skin · damagedPILOT REPORTED DENT AFT DOOR L 1 OUTTER PANEL IS DAMAGED. PERFORMED PERMANENT REPAIR TO FWD FUSELAGE LH SKIN IAW E175 SRM 1153-10-01/REPAIR 12P.SDR DALA2024040103961Skin · scratchedSHIP 3324 RAMP REPORTED SCRATCH BELOW LEFT AFT WING SCAN LIGHT. SCRATCH IS LOCATED AT STRINGER 27L BET FRAME 30 AND 31 BELOW LT AFT WING SCAN. CORRECTIVE ACTION: REPAIRED PER A330 SRM 53-21-11-300-015. (5575722)SDR DALA2024040103957Skin · dented(LOG 0268030) DENT WAS FOUND ON THE LH FUSELAGE SKIN BETWEEN STA 807.00 & STA 827 AND BETWEEN STRINGERS 14L AND 15L. MAINTENANCE REPAIRED DENT PER ERA 616607-14.SDR SWIA2024041700328Skin · damagedLIGHTNING STRIKE DAMAGE ON SKIN BETWEEN FRAMES 60 - 73 AND BETWEEN STRINGER 6L - 7L. (C-CHECK RO 4/16/2024) REMOVED LIGHTING STRIKE DAMAGE BY INSTALLING REPAIR DOUBLER AT CF III, EXTERNAL SKIN BETWEEN FRAMES 60-73 AND STRINGERS 6L-7L AS MARKED. SEE CONTINSDR CALA2024040200938Skin · crackedSUPPORT TASK - EA5315-01152 OP 002 , 1EA FASTENER HOLE FOUND CRACK ON BEAR STRAP AND 1EA FASTENER HOLE FOUND CRACK ON FUSELAGE SKIN AND BEAR STRAP ON RH SERVICE DOOR - TRANSFER REFER NON-ROUTINE WO.2843280 FUSELAGE SKIN REPAIRED ON RH SERVICE DOOR AFT LOWER CUSDR DALA2024040203978Skin · damagedSHIP 3272 DISC: OVERSIZE HOLES 1 THRU HOLE 19 AND HOLES A TO D (23E/A) FOUND GREATHER THAN MINIMUM STARTING HOLE DIAMETERS AS PER TABLE 2 OF THE CARD 5311- 1246-03B LOC ON JOGGLE AREA FR16 RH AT FWD GALLEY AREA. COMPLIED WITH ER/A 571448-14AD, REV. A (LP: 026SDR DALA2024040103944Skin · damaged(LOG 0265590) PREVIOUS LIGHTNING STRIKE FASTENER 1EA DAMAGE BS500I STR19R. COMPLIED WITH ER/A 616880-14 REV ORIGINAL.SDR LR7A2024032803408Skin Panel · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH LOWER CENTER WING SKIN PANEL AND STRINGER WITH A HOLE AT FS548, CWS81R, WL257. / REPAIRED IAW LAC MEA 382-57-24-028. NR# 1001102563.SDR LR7A2024032803400Skin · gougedDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC4914, FOUND LH FUSELAGE SKIN GOUGED AT FS472, LBL84.5, WL192. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001087722. / PSE# 53-40-08, AD 2012-06-09SDR LR7A2024032803396Skin · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH AFT FUSELAGE SKIN CRACKED AT FS847, LBL62, WL182. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001086589.SDR LR7A2024032803393Skin · crackedDURING SCHEDULED C-4 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH FUSELAGE CURB CRACKED AT FS623, WL152, RBL62. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1001086518.SDR LR7A2024032803375Skin · corrodedDURING SCHEDULED C-4 CHECK WHILE PERFORMING SP-310, FOUND RH CENTER WING UPPER SKIN CORRODED AT FS580, CWS217, WL286. / REPAIRED IAW LAC MEA 382-57-12-019. NR# 1001085608. / PSE# 57-30-01, AD 2012-06-09SDR SCNA20240402175Skin · handler errorTHE AIRCRAFT JACKING PROCESS, THE UPPER FUSELAGE AT CROWN AREA WAS TOUCHED BY ADJACENT SCAFFOLDING, AND CAUSED DAMAGES AT TWO SEPARATED AREAS AS FOLLOWS: DAMAGE LOCATION 1– DENT #1 LOCATED AT STA 500C+20.5” AND BETWEEN STR 8RH AND STR 9RH. DAMAGE LOCATION 2- SDR DALA2024040103954Skin · cracked(LOG 0265294) DURING REPLACEMENT OF TWO REPAIR BLIND FASTENERS (PREVIOUS LIGHTNING STRIKE REPAIRS) PER 737-900ER SRM 53-00-01 REPAIR 41, CRACK DAMAGE WAS DISCOVERED IN THE FUSELAGE SKIN (PN 143A3252-62) AT APPROXIMATELY BS 500I, S-19R AT ONE PRODUCTION HOLE LOSDR DALA2024040103953Skin · cracked(LOG 0265241) DURING REPLACEMENT OF TWO REPAIR BLIND FASTENERS (PREVIOUS LIGHTNING STRIKE REPAIRS) PER 737-900ER SRM 53-00-01 REPAIR 41, CRACK DAMAGE WAS DISCOVERED IN THE FUSELAGE SKIN (PN 143A3252-62) AT APPROXIMATELY BS 500G, S-22R AT TWO PRODUCTION HOLE LOSDR DALA2024040103943Skin · damaged(LOG 0265453) PREVIOUS LIGHTNING STRIKE FASTENER 2 EA DAMAGE BS500G STR22R. COMPLIED WITH ER/A 616881-14 REV ORIGINAL.SDR DALA2024040103941Doubler · corroded(LOG 0265251) FWD CARGO BAY PREVIOUSE REPAIR FROM DELETED ANTINNA IS CORRODED BETWEEN STA 500C AND 500D LBL 4 TO RBL 4. REMOVED AND INSTALLED REPLACEMENT PARTS (DOUBLER, NUTPLATE RETAINER AND -RETAINING RING) ATG ANTENNA STA 500C-500D LBL 4 TO RBL 4 IAW SRM 73SDR YENA2024032800474Skin · ground damageDURING HEAVY MAINTENANCE: GSC EQUIPMET HIT BELOW LEFT AFT AIRCRAFT DOOR ABOUT 10 BELOW SILL; REF CAS WO # 905-1320666, REMOVED DAMAGED SKIN BETWEEN FRAME 66 AND 67 STRINGER 26 AND 28 - MANUFACTURED FILLER, MANUFACTURED DOUBLER. REPAIRED IAW SRM 53-41-11-300-08SDR SWAA2024032768066Skin · crackedFUSELAGE CRACK ON S4L BETWEEN B.S. 525 AND B.S. 530 MULTIPLE FUSELAGE CRACK INDICATIONS ON S4L AT CHEM-MILL BETWEEN B.S. 525 AND B.S. 530. INSPECTION RESULTS CONFIRMED CRACK PER 737 PART 6 53-30-18 AND 737 PART 4 53-30-07. REPAIRED USING EA 24-153-00813.;[02] SDR IXXA2024032704Skin · crackedL1 DOOR CUTOUT SKIN LOWER AFT CORNER IS CRACKED.SDR IXXA2024032703Skin · corrodedFUSELAGE SKIN CORRODED AT STA. 1084SDR JJBA20250403012Skin · dentedDENT FOUND ON EXTERNAL SKIN BTW FR 19-20 AND BETWEEN STR 11L-12L. PAINT STRIPPED ON EXTERNAL SKIN BTW FR 19-20 BTW STR 11L-12L FOR INVESTIGATION. ON LH CENTER FUSE I SKIN, BTW FR19-20 AND BTW STR 11L-12L SKIN OUT TO REMOVE THE DAMAGE. SKIN REPAIRED BTW FR19-20SDR ASAA2024032649592Skin · corrodedAFT AVIONICS BAY LEFT HAND SKIN AIR INLET VALVE LOCATION, INTERNAL DOUBLER AROUND CUTOUT IS CORRODED GROUNDED - YES. REMOVED AND REPLACED INTERNAL DOUBLER IAW AIRBUS DWG D53113482 AND A320 SRM 51-42-11. NO ALLOWABLE LIMITS FOR AREA. REMOVED AND INSTALLED FILTESDR CALA2024032900906Skin · corrodedRADIO ALTIMETER ANTENNA HAD BROKEN NUT PLATE, WHILE REPLACING FOUND CORROSION UNDER ANTENNA. CORROSION WAS BLENDED AND DOUBLER INSTALLED PER ECRA 5341-01446. & PART 1.2 REQ''S DIP FOR FUSELAGE SKIN AT FR60-61 BETWEEN STR43R ART 2 OF LATEST REVISION ECRA5341-0SDR DALA2024032803890Skin · damagedFUSELAGE SKIN / FR 49-50, S8L-S9L / LIGHTNING STRIKES / EXTERNAL DOUBLER REPAIR AT FR49 AND STGR8L. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAGE 3 DTA APPROVAL. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAGSDR DALA2024032803889Skin · damagedFUSELAGE SKIN / FR 49-50, S8L-S9L / LIGHTNING STRIKES / REPAIRED FASTENER AT FR50 AND ABOVE STGR7L. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAGE 3 DTA APPROVAL. THIS IS A DTA MONITOR LOG FOR ERA 607631-14AD REV A WHICH REQUIRES STAGSDR DALA2024032603788Skin · dented(LOG 0261976) FUSELAGE SKIN DENTED AT BTW STA 178.00 & 203.80 AND BL0 & RBL15. DENT REPAIRED PER ERA 616420-14.SDR SWAA2024032567409Doubler · crackedEXTERNAL GROUND POWER RECEPTACLE (EGPR) DOUBLER CRACK AT DOOR CUTOUT<[01] CUT OUT THE DAMAGED AREA PER SRM 53-10-15-2R-4 REPAIR 4 FIG 204;[02] PERFORMED NDT OF DAMAGE CUTOUT PER NDT 51-00-00 PROCEDURE 23. NO DEFECTS NOTED.;[03] PERFORMED NDT OF DAMAGE CUTOUT PSDR SWIA20240418324Skin · damagedRH ELEVATOR HAS EVIDENCE OF LIGHTNING STRIKE DAMAGE ON UPPER SKIN BETWEEN RIB 8 AND 9 AND APPROXIMATELY AN INCH AND A HALF FROM THE TRAILING EDGE (C-CHECK RO 4/17/2024) REPAIRED LIGHTNING DAMAGE ON RH ELEVATOR UPPER SKIN REF. CRJ 900 SRM 55-21-01-201-001SDR DALA2024032603827Skin · damagedSHIP 6815 DURING BHEC INSPECTION FASTENER HOLES PER STEP 12 OF WORKCARD, FOUND 1 EA. FASTENER HOLE UNINSPECTABLE DUE TO PLUG AND TOOLING DAMAGE ADJACENT TO FASTENER HOLE. CORRECTIVE ACTION: REF ERA 616745-14. (0260182)SDR DALA2024032503744Skin · damagedSHIP 3407 DAMAGE ON AFT CARGO DOOR FRAME SURROUNDING SKIN PANEL FR59A STR 40RH. CORRECTIVE ACTION: REWORKED DAMAGE IN ACCORDANCE WITH A330 NEO SRM 53-41-11-283-022. OK TO CONTINUE. (4283432)SDR SWAA2024042566942Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; RBL 12; AND LBL 12.<[01] VERIFIED STEPS 1; 2; 5.;[02] REMOVED DAMAGE ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; 10'SDR CALA2024040300953Skin · crackedGENERATING ITEM EA 5315-01152 LOWER AFT CORNER OF R1 DOOR FUSELAGE SKIN AND BEAR STRAP STA 335 STRINGER 20R HAS CRACK INDICATION WHILE PERFORMING HFEC OPEN HOLE SCAN. INSTALLED REPAIR PARTS IAW SRM 53-10-01-2R-1, REPAIR 1 53-10-01-2R-1, REPAIR 1, FIG 201, SHT
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