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 R61A2024102900518Skin · dentedREF DMI R949811/2 DENT ON RH RVSM CRITICAL AREA REQUIRES DET INSPECTION EVERY 750FH REF LP R949811/1SDR R61A2024102900517Skin · dentedTWO SMALL DENT BELOW FO'S WINDOW BY THE GOLD PAINT STRIPE LEFT AS PERMENT REPAIRSDR R612024F00007Skin · dented***MAJOR***REF DMI R949811/3 DENT ON RII RVSM CRITICAL AREA REQUIRES PERMANENT REPAIR WITHIN 7500 FH REF LP R949811/1***MAJOR***SDR DALA2024101410044Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN EDGE, AROUND HANDLE ON PASSENGER DOOR (L1). SUMMARY OF NRC 00302: EXTERNAL FUSELAGE SKIN EDGE AROUND HANDLE ON PASSENGER DOOR (L1) WAS REPAIRED PER ER/A 620705-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620705-14 REV 1.SDR CALA2024101402642Skin · crackedLH #3 WINDOW FRAME, E-F POST THIRD (LOWER CORNER) FASTHER HOLE WITH CRACK SIGNAL INDICATION, DIRECTION OF INDICATION 9 O''CLOCK POSITION. (REF: AAR NR 1000016743) REPAIRED LH NO. 3 WINDOW FRAME IAW EA 5310-08195 OP 003, AAR RFD EA NO. 240547 & ECRA 5310-08430 SDR WRXR20241011002Skin · gougedMULTIPLE GOUGES ON THE LOWER SKIN PANEL AT FS 1000 TO FS 1031 BETWEEN STR25R TO STR27. BLENDED AREAS A-G TO A 20:1 RATIO ON THE LOWER SKIN PANEL AT FS 1000 TO FS 1031 BETWEEN STR25R TO STR27 IAW REO 670-53-61-2384 REV--.SDR SWAA2024120547323Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2024-633633<[01] REPLACED TIE CLIP AND FASTENERS LOC. BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV - AND DWG 141A8380 SHEET 21 REV -.SDR R61A2024102800508Doubler · corrodedFWD FUES FWD CARGO FR19-20 STR 26R TO 27R, INTERNAL DOUBLER FOR TRANSPONDER ANTENNA CORRODEDSDR CALA2024102302709Skin · dentedEXISTING DENT AT STA 196.5 FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1. REF AAR N/R 9907416 AS PER ECRA 5331-03130 STEP 3 INITIATE A DIP LP TO READ AS FOLLOWS AFTER THE ACCUMULATION OF 49,000TOTAL F/C BUT BEFORE 50,000 PERFORMED AN INSP OF THE FUSELAGE SKISDR GTIA2024101238433Skin · dentedDENT EMPINAGE SKIN BETWEEN FRAMES 78-80 STRINGER 3L -4L RAF-01 CREATED AND SDR -ACCOMPLISHED EMPINAGE SKIN REPAIR FR 78-80 STR 3L - 4L IAW SRM 53-51-11-300-002 CAT A REPAIR NO REINSPECTION REQUIRED REF HAECO S.O. 122204 OPS 34424SDR CALA2024101102632Skin · crackedDURING HFEC INSPECTION OF THE FASTENER OPEN HOLE, WAS FOUND A CRACK LENGTH 0.040" AT THE FWD SERVICE DOOR CUTOUT AFTER LOWER CORNER.SDR CALA2024101102629Skin · damagedAS PER CUSTOMER REQUEST AFT CARGO DOOR SURROUNDING SKIN AND BEAR STRAP DAMAGE PERFORM PERMANENT REPAIR BETWEEN STA 827- STA 847 AND STR 24R STR 25R REF AAR N/R 9902778 ACCOMPLISHED REPAIR AT AFT CARGO DOOR SURROUNDING SKIN AND BEAR STRAP BETWEEN STA 827-STA 84SDR DALA2024101109968Skin · crackedCRACK INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 702: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RSDR DALA2024101109967Skin · crackedCRACK INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 702: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RSDR DALA2024101109966Skin · crackedCRACK NTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 701: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RESDR DALA2024101109970Skin · crackedCRACK NTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 701: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RESDR UATA2024101045305Skin · corrodedLOWER LH SKIN BETWEEN FRAME 17 AND 18 CORRODED. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAIL.SDR UATA1901010245301Skin · damagedLOWER RH SIDE SKIN BETWEEN FRAME 17 AND 18 CORRODED. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAILSDR FDEA202410101465Skin · crackedFORWARD CARGO - FORWARD CARGO DOOR LOWER AFT DOOR JAMB DOUBLER FOUND CHAFFED AT STATION 1002.3 LONGERON -40 RIGHT TO LONGERON -41 RIGHT. FORWARD CARGO - FORWARD CARGO DOOR LOWER AFT DOOR JAMB AT STATION 1002.3 LONGERON -40 RIGHT TO LONGERON -41 RIGHT CHAFFSDR FDEA202410101464Skin · chafedCENTER CARGO - AFT OF CENTER CARGO DOOR LOWER DOUBLER FOUND CHAFFED AT STATION 1781, LONGERON -38 RIGHT TO LONGERON -41 RIGHT. CENTER CARGO - AFT OF CENTER CARGO DOOR LOWER AT STATION 1781, LONGERON -38 RIGHT TO LONGERON -41 RIGHT DOUBLER CHAFFED AREA REPASDR R61A2024102800502Doubler · corrodedFWD FUSE FWD CARGO FR19-20 STR 26-27L FOUND INTERNAL DOUBLER FOR TRASNPONDER ANTENNA CORRODEDSDR DALA2024100909867Skin · chafedSHIP 1806 SECTION 48 FWD OF STA 1746 BETWEEN S-15R TO S-22R UNDER H/STAB SEAL AREA FWD REPAIR SKIN PANEL FOUND CHAFED. CORRECTIVE ACTION: REPAIRED DAMAGED AREA PER B767-400 SRM 53-80-01. (0599331)SDR DALA2024100909866Skin · chafedSHIP 1806 SECTION 48 FWD OF STA 1746 BETWEEN S-15R TO S-22R UNDER H/STAB SEAL AREA LOWER REPAIR SKIN PANEL FOUND CHAFED. CORRECTIVE ACTION: REPAIRED DAMAGED AREA PER B767-400 SRM 53-80-01. (0599327)SDR IPXA2025010930003Skin · dented*SDR FILED OPEN* REF BARCODE T3F18E005AYYG DENT ON TAIL OF FUSELAGE, TO THE LEFT OF TAIL SKID. APPROXIMATELY 6" FORWARD OF STRINGER AT ST 1702.0. RE-OPENED DUE TO REVISED RECURRING INSPECTION ADJUSTMENT. REPAIR IAW: SRM 53-00-01-2R-10 REPAIR MATERIAL: -1 DOUBSDR IXXA20241115004Skin · crackedR1 DOOR AFT LWR CORNER 2ND OPEN HOLE FROM BOTTOM FOUND CRACKED AS MARKED. HAECO WO 320009 NON ROUTINE 46090SDR SWIA2024103008Skin · crackedRH WING MAIN BOX LOWER SKIN (LOWER SURFACE) ALONG SPAR 01 HAS SUSPECTED CRACK AT RIVET IN BETWEEN SLAT #3 AND #4. (C-CHECK RO 10/30/2024) (FILED OPEN)REPAIRED CRACK IN RH WING MAIN BOX LOWER SKIN AT RIB 20 BY FILLER AND DOUBLER REPAIR REF ETD2024-170-027059. SDR SWAA2024102846499Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN UNDER VERTICAL STAB BS1016 - BS1085 LBL14 TO RBL14 WL308.5. MARKED<[01] VERIFIED STEP 1;[02] VERIFIED APPLICABILITY OF SRM; REMOVED CORROSION PER SRM SRM 53-00-01-1A-1 ; AND COMPLETED EA 24-153-02815-WIP1 AND EA-24-153-02815SDR ASAA2024100853201Skin · corrodedSEC 47 AT STA 907 TO STA 927 AT STR 23L LAP JOINT HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR ON SKIN P/N'S: 147A3110-3 AND 147A3400-4 IAW EA NO. 800-53EA-27730 REV 00.SDR ASAA2024100853200Skin · corrodedAT STA 887 FROM STR 23L TO STR 23R SEC 46 TO SEC 47 BUTT JOINT HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR ON SKIN P/N'S: 146A3231-49 AND 147A3400-4 IAW EA NO. 800-53EA-27729 REV. 00.SDR ASAA2024100853196Skin · corrodedAFT LAV VENT AT STA 907 TO STA 927 SEC 47 L/H HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY B MINOR REPAIR ON SKIN P/N: 147A3110-3 IAW EA NO. 800-53EA-27722 REV 00.SDR EE4Y2024100820976Skin · corrodedDURING THE STRUCTURE INSPECTION IT WAS FOUND THE FUSELAGE SKIN WITH CORROSION AT THE INTERNAL SURFACE. DUE TO THE DAMAGE AREA IS BEYOND ERJ190 SRM PART II, REPAIR PROPOSAL WAS SENT TO EMBRAER FOR TECHNICAL SUPPORT EVALUATION AND APPROVAL. PERFORMED TEMPORARY SDR EE4Y2024100820975Skin · deformedOUR CUSTOMER REPORT US, THE FUSELAGE SKIN WITH EXISTING TOOL MARKS AT FR 15, STR-22LH +115MM, EVALUATED AFFECTED AREA, FOUND IT OUT OF LIMITS IAW ERJ190 PART II SRM 53-10-01 AD51, PARAG 4B, TABLE 102, FIG 101. DUE TO THIS FACT WE ARE CONTACTING ERJ FOR TECHNICSDR EE4Y2024100820974Skin · deformedDURING PRESENT CHECK ON CENTER FUSELAGE, IT WAS FOUND TOOLING MARK ON FUSELAGE SKIN LOCATED AT FR32+120MM, STRG-25LH, THE MENTIONED DAMAGE WAS EVALUATED AS PER ERJ SRM PART II 53-21-01 AD 51 PARAG 5A TABLE 102 (RIVETED AREA), FIG 104, ZONE GRAY (NO DAMAGE ALLOSDR EE4Y2024100820973Skin · deformedDURING PRESENT CHECK ON CENTER FUSELAGE I, IT WAS FOUND A TOOLING MARK ON FUSELAGE SKIN LOCATED AT FR30+205MM, STRG-23LH+190MM, THE MENTIONED DAMAGE WAS EVALUATED AS PER ERJ SRM PART II 53-21-01 AD 51 PARAG 5A TABLE 102 (RIVETED AREA), FIG 104, ZONE GRAY (NO DSDR EE4Y2024100820970Skin · damagedDURING PRESENT CHECK LIGHTNING STRIKE ON FUSELAGE SKIN WAS REPORTED. THE DAMAGE WAS REWORKED AS PER ERJ SRM PART II 51-40-02 PARAG 4 AND EVALUATED THROUGH DAMAGE AS PER ERJ SRM PART II 53-10-01 AD 53 PARAG 4B(6), HOLE FOUND OUT ALLOWABLE DAMAGE LIMITS. DUE TO SDR EE4Y2024100820968Skin · corrodedDURING THE STRUCTURE INSPECTION IT WAS FOUND THE FUSELAGE SKIN WITH CORROSION AT THE INTERNAL SURFACE. DUE TO THE DAMAGE AREA IS BEYOND ERJ190 SRM PART II, A REPAIR PROPOSAL WAS SENT TO EMBRAER FOR TECHNICAL SUPPORT EVALUATION AND APPROVAL. PERFORMED PERMANENSDR REXA2024122401607Doubler · chafed"FUSELAGE LOWER SKIN REPAIR DOUBLER,F.S.969 TO F.S.985 AT STGR 27 IS CHAFED REMOVED 03 HI LITE FOR REMOVE DAMAGE. REMOVED DUCT FOR ACCESS BETWEEN FS931-FS1031 IAW CRJ700 AMM 21-23-44-000-801(CONF. A01). REMOVED BOTTOM DOUBLER IAW CRJ700 SRM 51-42-21-001-001-SDR ASAA2024100753699Skin · corrodedFUSELAGE SECTION 48, SIGNS OF CORROSION ON SKIN AT BUTT SPLICE STA 1016 STR 23R-23L. GROUNDED - YES. REMOVED CORROSION & FOUND IN LIMITS IAW BOEING 737-700 SRM 53-00-01-1A-1 AT FUSELAGE SECTION 48 BUTT SPLICE STA 1016 STR 23R-23LW=.600" O=.080 R=.078 L=10" D=.SDR IPXA2024101697157Bear Strap · crackedFAULT - FOUND CRACK ON THE NO.1 FORWARD ENTRY DOOR AFT LOWER CORNER BEAR STRIP. (REPAIR) REVIEWEDSDR SWAA2024101045744Skin · crackedPOSSIBLE CRACK INDICATION LOCATED @ STRINGER S1 STA 787 -8IN<[01] VERIFIED CRACK INDICATION @ LOCATION STRINGER S1 STA 787 -8IN PER NDT PART 6 53-30-18 & PART 4 53-30-07. CRACK FOUND TO BE 1.4IN IN LENGTH.SDR SWAA2024101045764Doubler · crackedREF TTG8Q00W81A7; EXTERNAL GROUND POWER RECEPTACLE (EGPR) DOUBLER CRACK AT DOOR CUTOUT<[01] REMOVED DAMAGED SECTION OF EXTERNAL GROUND POWER DOUBLER (ZONE 2) PER SRM 53-10-15-2R-4; ALTERNATIVE 2;[02] PREFORMED HFCE SURFACE PER NDT PART 6 51-00-00 PRO 23;[03] RSDR DALA2024100809790Skin · damagedCREASE IN FUSELAGE SKIN WAS FOUND ON REPAIR AREA. SUMMARY 00593: CREASE WAS REPAIRED PER ER/A 620891-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620891-14 REV 0. ACCOMPLISH SECTION II REPETITIVE INSPECTION INSTRUCTIONS WITHININ EVERY 8,000 FLIGHT CYCLESDR IXXA2024100702Skin · crackedL-1 DOOR CUTOUT AFT LOWER CORNER CRACKED S19L BODY ARM 332-339SDR SWIA20250127006Skin · dentedADM# N679SA-8142THERE IS A DENT ABOVE AND AFT OF LOW PRESSURE AIR ACCESS PANEL, BETWEEN APPROXIMATELY FS589-FS605, AND STRINGER 21R-22R. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRASDR DALA2024100709764Skin · gougedSHIP 3133 GOUGE EXTERNAL SKIN LOC. FR 54 TO FR 55 BTW STR 41 TO STR 42 LH SIDE AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 620925-14. (0595545)SDR SWIA20241223005Skin · damagedBIRD STRIKE DAMAGE TO UPPER SKIN PANEL (DWG: CC670-33105 REF), UPPER ELEC. BAY DOOR (DWG: CC670-33070 REF) AND UNDERLYING STRUCTURE (FRAME FS 193 (DWG: CC670-34201 REF) & STRINGER STR 14L (DWG: CC670-33145 REF)), LOCATED BETWEEN FS 193.00 - FS 202.75 AND STR 1SDR SWIA202412161005Skin · damagedBIRD STRIKE DAMAGE TO UPPER SKIN PANEL (DWG: CC670-33105 REF), UPPER ELEC. BAY DOOR (DWG: CC670-33070 REF) AND UNDERLYING STRUCTURE (FRAME FS 193 (DWG: CC670-34201 REF) & STRINGER STR 14L (DWG: CC670-33145 REF)), LOCATED BETWEEN FS 193.00 - FS 202.75 AND STR 1SDR ASAA2024100553078Skin · corrodedSECTION 47; FUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT, STA 907-927 STGR 25R-27R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO AFT FUSELAGE SKIN P/N 147A3400-4 AT STA 907-927 STGR 25R-27R AT WATER SERVICE PANEL CUTOUT ISDR ASAA2024100553077Butt Joint · corrodedSECTION 47; FUSELAGE SKIN BUTT-JOINT AT STA 1016 STGR 25R-26L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" REPAIR (MINOR) AT SECTION 47 FUSELAGE SKIN BUTT JOINT STA 1016 STGR 25R - 266 IAW EA #800-53EA-27708 REV 00.SDR ASAA2024100553076Butt Joint · corrodedSECTION 46/47 ; FUSELAGE SKIN BUTT-JOINT AT STA 887 STGR 23R-23L HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR AT SEC 46/47 FUSELAGE SKIN BUTT JOINT STA887 BETWEEN STGR 23R - 23L IAW EA #800-53EA-27710 REV 00.
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