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 DALA2024051905325Skin · damagedAIRCRAFT 3723, DURING ROUTINE INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE FUSELAGE SKIN (P/N 141A3521-11) AT APPROX. BS 351+6, 2" ABOVE STR 28L. CORRECTIVE ACTION: TRIMMED OUT THE DAMAGE IN THE SKIN P/N 141A3521-11 AND SPLICE STRAP P/N 141A3523-14. FABRICATSDR DALA2024051705310Skin · corroded(LOG 03458510) DURING ROUTINE INSPECTIONS, CORROSION DAMAGE WAS FOUND ON THE FUSELAGE SKIN (P/N 141A3521-11) AT APPROX. BS 357, ABOVE STR 28L. ADDITIONALLY, CORROSION DAMAGE WAS FOUND ON THE SPLICE STRAP (PN 141A3523-14) AT BS 360, ABOVE STR 28L. MAINTENANCE RSDR DALA2024051605250Skin · crackedCRACK ON FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L. SUMMARY OF NRC 00162: FUSELAGE SKIN LOCATED AT Y=1037 AND LONGERON L-14L WAS REPAIRED PER ER/A 617297-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-617297 ADDED FOR AC 9536. (LP #0SDR SWIA20240515Skin · damagedMULTIPLE DENTS,NICKS, GOUGES ,ON AFT FUSELAGE SKIN IN BETWEEN APPROX FS 1000 TO FS 1051 BETWEEN STR 21R AND STR 27 IN AREA OF GROUND A/C SERVICE DOOR. (C-CHECK RO 8/22/2024) REMOVED DAMAGE FROM EXTERNAL FUSELAGE SKIN AROUND GROUND AIRCONDITIONING SERVICSDR SWIA2024F00614Skin · gougedEXTERNAL SKIN GOUGED AND DENTED BETWEEN FS969.00 AND FS985.00 AT STGR27 AS MARKED (C-CHECK RO 8/4/2024) REPAIRED EXTERNAL SKIN BETWEEN FS 969 AND FS 985 AT STGR27 REF REO 670-53-00-290 REV -F 2019/04/26. COMPLIED WITH 51-900-1002-SKY AND PRESSURE CHECK SDR HNAA2024060600484Skin · dented00139 CENTER FUSELAGE I - SMALL DENT LOCATED AFT OF MAIN DOOR REQUIRES PERMANENT REPAIR. PAIRED PERMANENTLY ON CENTER FUSELAGE 1 - SMALL DENT LOCATED AFT OF MAIN DOOR IAW EMB 145 SRM 53-21-01SDR SWAA2024052385905Skin · crackedFOUND SMALL CRACK @ L/H FUS INT FRAME CUTOUT FLANGE ABOVE L-1 DOOR CUTOUT STA 312 MKD DOT<[01] ACCOMPLISHED REPAIR AS PER SWA EA M-22-153-01244 (TTG8Q00TCSP5);[02] VERIFIED STEP 1SDR CALA2024052201557Vent · crackedWASTE TANK FUSELAGE VENT EXHIBITS CRACKS AND CORROSION EXTERNALLY ON EXTERIOR SKIN AFT OF STATION # 907 SECTION # 47 REMOVED WASTE TANK ENCLOUSER PANELS. REF AMM 25-52-20. REMOVED POTABLE WATER TANK. REF AMM 38-11-01-00-801. REPAIR DAMAGED AREA PER SRM 53-70-0SDR DALA2024051705317Skin · dentedSHIP 176 FUSELAGE / STA. 1197 44 TO 110 AND STR 22R - 31R DENTS AND GOUGES. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 617766-14 REV. (0343914)SDR AALA202405170912Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: BUBBLING PAINT AND CORROSION AROUND LAVATORY VENT SKIN. LOCATED AT BS 907 TO 927 AT STR 20L TO 22L. INSTALLED FUSELAGE LAVATORY VENT DOUBLER AND TRIPLER AND FILLER. PER SRM 53-70-01-2R PROCEDURE.SDR FDEA202405150672Skin · damagedLOWER FUSELAGE SKIN DAMAGED AT APPROX. STATION 157. FUSELAGE SKIN REPAIRED IAW FED-RE-2403203SDR VNAA20240723007Skin · corrodedCORROSION ON JOINT PLATE UPPER LONGERON AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SURROND STRUCTURE. JOINT PLATE UPPER LONGERON WAS REPAIRED PER REO 690-53-31-847 REV. -- AND AFT HINGE BTW FS549.00 AND FS565.00 AT FWD BAGGAGE BAY DOOR SUSDR VNAA202407090010Skin · nickedNICK DAMAGE FOUND ON LOWER SKIN AT FS 307.87 WITHIN 5320 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. LOWER SKIN AT FS 307.87 WAS REPAIRED PER REO 690-53-21-1780 REV - -SDR VNAA20240618007Skin · corrodedCORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT. CORROSION ON DOOR CUT-OUT INNER SKIN AT E/E MAIN COMPARTMENT WAS REMOVED AND WAS EVALUATED WITHIN LIMITS PER REO 690-53-21-032 REV. --SDR SWAA2024061485533Doubler · crackedCUSTOMER REQUEST CRACK ON EXTERNAL GROUND ELECTRICAL POWER RECEPTACLE SURROUND DOUBLER ZONE 2 LOWER FUSELAGE 2024-339858<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N NORTEC 500D S/ N 500X1693P030457 DUE DATE: 15-OCT-24.;[02] TOOL USED ON STEP 8 ET EQUIPMENT: P/NSDR SWI202405200414Skin · puncturedHOLE IN FUSELAGE APPROXIMATELY 1 INCH BY 1 INCH APPROXIMATELY THREE FEET TO THE RIGHT OF MCD APPROXIMATELY ONE FOOT ABOVE FLOOR LEVEL. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28236263 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH PEMSDR DALA2024052005335Skin · corrodedSHIP 3219 DISC: DURING CCK AND WHILE INSPECTING PER ER/A 522877-14,REV E CORROSION FOUND ON SEVERAL LOCATIONS OF RHS NLG LATERL PANEL AND LWR CENTER SKIN PANEL AND REINFORCEMENT.PANEL REPLACEMENT NEEDED AT REV A DTE IS COMPLETED,ICA'S INCORPORATE. 197334 S PERSDR DALA2024051605268Skin · dented(LOG 0344100) DENT ON FUSELAGE SKIN BELOW WASTE TANK SERVICE PANEL AT APPROX STA 847+4", 3.5" BELOW STR 25L. C/W ER/A 617768-14 REV ORIGINAL SECTION I.SDR DALA2024051605263Skin · dented(LOG 0342104) DURING INSPECTIONS, A DENT DAMAGE WAS DISCOVERED ON THE FUSELAGE SKIN (PN 146A3231-11) AT APPROX. BS 851, BELOW S-25L. REPAIRED PER ERA 617768-14.SDR AALA202405156196Skin · corrodedAIRCRAFT WAS NOT GROUNDED: SMALL AMOUNT OF CORROSION AROUND LAVATORY WASTE VENT. PERFORMED REPAIR OF AFT LAVATORY WASTE VENT CORROSION. PER AARD 53-70-00.SDR DALA2024051505221Doubler · corrodedCORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTEMENT. SUMMARY OF NRC 00631: CORROSION LEVEL 2. CORROSION ON INTERNAL DOUBLER BTW STA Y 617-636 AND LONG L27L TO L28L AT FWD CARGO COMPARTMENT WAS REPAIRED PER ER/A 61763SDR DALA2024051405193Skin · damaged(LOG 0341373) LIGHTNING STRIKE DAMAGE AREA # 5 - STR. 2R - 3R STA. 500I-500J. COMPLIED WITH ER/A 618015-14 REV. ORIG. SECTION II PERMANENT REPAIR INSTRUCTIONS AND B737 SRM 53-00-01-2R.SDR DALA2024051405199Skin · corroded(LOG 0341655) WHILE IN SAV, MTC DISCOVERED FIVE (5) LIGHTNING STRIKE HITS TO THE FUSELAGE CROWN SKIN (P/N: 143A3111-40 AND -41) LOCATED BETWEEN STR 2R-3R AND STA 460-500J. MAINTENANCE REPAIRED DAMAGE PER ERA 618015-14.SDR ASAA2024051351616Doubler · corrodedAFT PIT AT FR64 BETWEEN STR44 AND STR43R THERE IS EVIDENCE OF CORROSION ON THE BELLY SKIN DOUBLER STRAP GROUNDED - YES. REMOVED CORROSION IN AFT. PIT AT FR64 BETWEEN STR43R-STR44 AND FOUND AREA TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM ON INTERNAL DOUBSDR SWIA20240513Skin · damagedDAMAGE TO AIRCRAFT SKIN BEHIND AND BELOW THE GALLEY SERVICE DOOR. (FLIGHT 4105 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28230431 WITH THE FOLLOWING CORRECTIVE ACTION: "REF CP 28254135 AND CP 28258891 FOR WORK PERFORMED COMPLIED WITH REO 690-5SDR SWIA202405200013Skin · damagedDURING GEAR SWINGS FOUND NOSE AFT DOOR TO BE SHIFTED TO THE LEFT. ADJUST AS REQUIRED (C-CHECK RO 5/20/2024) PERFORMED REPAIR ON DAMAGE HOLE AND GOUGE DAMAGE AT FWD STR 26R BETWEEN FS 228.42 TO FS 235.00 IAW REO 670-53-11-1954 REV -- DATE 2024-05-15,CRJ 700SDR CALA2024052001524Skin · damagedSTARTED DRILLING HOLES INTO THE DOUBLE IN THE STRUCTURAL AREA BS 807, S25L & 26L. IAW SRM 51-10-01 & AVO 12561. COMPLETED DRILLING HOLES INTO DOUBLER & COUNTERSINKNG. CUT A NEW DOUBLER, PICKED UP HOLES & FOR AVO UPDATE FROM ENG ON DAMAGED HOLE. IAW 51-10-0SDR SWIA20240511Skin · dentedRH AFT LWR FUSELAGE AT FR1031.00 10 INCHES AFT BETWEEN STR24R AND 25R THERE IS A DENT (C-CHECK RO 8/22/2024) EVALUATED AND DRESSED BACK DENT ON R/H AFT LOWER FUSELAGE AT FR 1031.00+10 INCHES AFT BETWEEN STR 24R AND 25R. NO OIL CAN CONDITION PRESENT AT SDR DALA2024061005966Skin · damagedSHIP 3426 FWD CARGO DOOR SURROUNDING AREA SKIN DMG. CORRECTIVE ACTION: COMPLIED WITH A330 SRM 53-21-11-205-033. (5270156)SDR HNAA2024060600483Skin · dented00105 CENTER FUSELAGE I - SMALL DENT LOCATED AFT OF MAIN DOOR REQUIRES PERMANENT REPAIR. REPAIRED PERMANENTLY ON CENTER FUSELAGE 1 - SMALL DENT LOCATED AFT OF MAIN DOOR IAW EMB 145 SRM 53-21-01SDR ASAA2024051149791Skin · corrodedFUSELAGE SKIN FWD OF WTB HAVE MULTIPLE BELLY DRAINS WITH CORROSION. GROUNDED - YES. REMOVED CORR FOUND TO BE IN LIMITS IAW B737-900 SRM 53-30-01-1A-1 REFINSHED AREA IAW B737-900 SRM 51-20-01 SOPM 20-44-04 THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF SDR ASAA2024051149788Skin · corrodedFUSELAGE SKIN AFT OF WTB HAVE MULTIPLE BELLY DRAINS WITH CORROSION. GROUNDED - YES. REMOVED CORR FOUND TO BE IN LIMITS IAW B737-900 SRM 53-60-01-1A-1 REFINSHED AREA IAW B737-900 SRM 51-20-01, SOPM 20-44-04 THIS IS A CAT B REPAIR WITH AN INPECTION THRESHOLD OF SDR DALA2024051705315None · noneSHIP 176 DTE TRACKING FOR ER/A 617766-14 REV. CORRECTIVE ACTION: ER/A 617766-14 REVISION ORIGINAL REQUIRES DTE WITHIN 12 MONTHS IAW PROCEDURES ESTABLISHED IN FAA AC 120-93. (0337763)SDR DALA2024051405215Doubler · corrodedCORROSION ON INTERNAL DOUBLER WAS FOUND (SETTLEMT AREA OF RETAINER RING). INTERNAL DOUBLER STIFFENER SETTLEMT AREA OF RETAINER RING) WAS REPLACED PER DWG P18308 REV. D AND PER B757-300 SRM. (0338132)SDR DALA2024051405191Door Frame · damaged(LOG 0340957) E&E ACCESS DOOR CUTOUT WEB DAMAGE AT STA 344 I/B. REMOVED AND REPLACED DAMAGE WEB AT STA 344 I/B LEFT SIDE PER B737-800 SRM 51-40-05-0G AND DWG 141A8511 REV.CSDR DALA2024051305133Doubler · corrodedCORROSION ON DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E. SUMMARY OF NRC 00186: CORROSION LEVEL 2. DOUBLER BTW L29R-L28R STA Y=199-119 AT E&E WAS REPLACED PER B717-200 DWG 9923686 REV D AND PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. FORWARD WATER DRAIN MAST SDR 9WGA2024051034401Skin · ground damageDURING WALK AROUND INSPECTION ORD, FOUND DAMAGE TO FUSELAGE SKIN AT BS 200 - 210 BETWEEN S-45L TO S45R, 30-INCH-LONG DENTED, 0.5 INCH DEEP, CAUSED BY GSE EQUIPMENT STRIKING AIRCRAFT. TEMPORARY REPAIR PERFORMED IAW EA 81-2024-083 REV IR, PREPPED FOR SPECIAL FERSDR IPXA2024052815576Skin · dentedAFT CARGO PIT - FRAME STA 1460 RH SIDE HAS A DENT IN INNER CHORD AT STR 26R. VERIFIED DENT FOUND OUT OF LIMITS.INSTALLED REPAIR J SECTION IAW SRM 53-00-07-2R-5 DETAIL I AND SRM 51-40-02-0G-0.SDR YENA2024051500743Doubler · corrodedDURING HEAVY MAINTENANCE: CORROSION ON PREVIOUS REPAIR DOUBLER PLATE OF CENTRAL LONGITUDINAL BEAM LOCATED BTW FR84-FR85 AND Y=280LH OF CABIN PAX FLOOR STRUCTURE AT CENTER FUSELAGE III (W2); (RESOLVED ON W/O: 1308135 TASKCARD: NR-00016 ) REF: TOMX W/O 2552 N/R SDR DALA2024051405189Doubler · corroded(LOG 0340893) SKIN DOUBLER, AT STA 1040, STR 2L-2R, HAS EVIDENCE OF CORROSION. REMOVED DAMAGED SKIN DOUBLER B5 1035-1040 STR 26-2R AND INSTALLED REPLACEMENT DOUBLER PER B737-800 SRM 51-40-02. REF BOEING DWG 148A3110.SDR CALA2024051301464Skin · corrodedB767-53-3-7108 STA1197+132 TO 1219 S38L FUSELAGE EXT SKIN FOUND BULGED. FUSELAGE EXTERIOR SKIN AT STA 1202 TO STA 1228 STR 34L - 39R. REPAIRED AS PER ECRA 5360-01802 REV- PART 1, ITEM 1, INTERIM REPAIR. REFERENCE LPS 7917391 AND 7917496 FOR INSPECTION REQUIRESDR DALA2024051005111Rivet · brokenSHIP 171 FOUND RIVET HEAD BROKEN ON LOWER FUSELAGE AT STA 1373 AND S-36L. CORRECTIVE ACTION: THE DAMAGE AREA TRIMED OUT AND PERFORMED REPAIR AS PER PRI:617867-14 (0335258)SDR DALA2024051005113Skin · dentedSHIP 178 LT SIDE OF FUSELAGE- SKIN IS DENTED OUTWARD AND A FASTENER IS PULLED THRU THE SKIN AT APPROX STA 1582 STR 20L. ACCOMPLISHED REPAIR PER PRI 617777-14 REV 0, PRI 617777-14 REV 1 AND ERA 617777-14 REV A.SDR CALA2024052001525Skin · dentedRAMP REPORTED DAMAGE LT SIDE FWD OF TOLIET SERVICE PANEL. JUST AFT OF BS 807 BETWEEN S25L & 26L. HOLE/ CRACK MEASSURES 2 1/2 " DENT IS APPROX 4" X 1 1/4 WIDE LOCKING FOR MX FERRY COMPLIED WITH EC/RA: 5330-07246 REMOVED FASTENERS FROM STRINGERS AND FRAME INSDR DALA2024051305145Skin · crackedSHIP 190 DURING PERFORMING 5330-01229-01B STEP 4 THEN FOUND 01EA CRACK AND 4.100 INCH IN LENGTH ON THE FUSELAGE SKIN BELOW 5TH RIVET TO 10TH RIVET AT S-13AR, AFT OF STA 1654.5. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B767-300 SRM 53-80-01-2R-7. (0331975)SDR JJBA20240522049Skin · scratchedLH EXTERNAL FWD FUSELAGE, SCRATCH FOUND LOWER GPU POWER CONNECTOR AT REPAIR DOUBLER. ON LH EXTERNAL FWD FUSELAGE, LOWER GPU POWER CONNECT AT REPAIR DOUBLER SCRATCH BLEND OUT OF LIMITS. EXISTING DOUBLER REMOVED FOR REPLACEMENT. REPAIR DOUBLER FABRICATED. REPAISDR R61A2024050900206Skin · dentedDENT FOUND ON LH FUSELAGE SKIN BETWEEN FRAMES 10&11 AND BELOW STRINGER 17L. REPAIRED IAW ETD2024-170-012852, INSTALLED FILLER AND DOUBLER. ALSO REF VP-014820-2024 N/R 4 FOR WORK PERFORMED.SDR DALA2024050905083Skin · damaged(LOG 0331599) LIGHTNING DAMAGE NOTED AT FRAME STATION 211.8, WL 186. REPAIRED PER B737 SRM 53-00-01.SDR DALA2024050905081Skin · damaged(LOG 0331591) LIGHTNING DAMAGE NOTED AT FRAME STATION 196.5, WL 220.1. REPAIRED PER B737 SRM 53-00-01.SDR AALA202406219077Skin · bulgedAIRCRAFT IN BASE MAINTENANCE: BULGE IN FUSELAGE SKIN ABOVE AFT CARGO DOOR AT STA 767, S14R. REPAIRED SKIN PER SRM 51-10-02 AND EA 353874.
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