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 UIEA2023013120069Structure · cracked1EA CRACK FOUND ON AFT UPR CORNER OF MAIN ENTER DOOR 5L CUTOUT, CRACK FOUND ON SECOND LAYER RUNNING TO FORWARD.(<P>FX - MAIN ENTER DOOR 5L CUTOUT AFT UPPER CORNER BEAR STRAP AND SKIN CRACK AREA REPAIRED AND MODIFICATION IAW EO 4453A804 PART 3.</P>)SDR YENA2023013100112None · noneDURING HEAVY MAINTENANCE: (CPCP FINDING) REF NRC 00332:CORRROSION ON SHEAR CLIP BTW FR 83, STRG 27R-28R IN AFT CARGO COMPARTMENT; (RESOLVED ON W/O: 1177513 TASKCARD: NR-00044 ) REF NRC 00322:CORROSION IS OUT OF LIMITS R & R SHEAR CLIP PER EMB 190 SRM 51-41-01SDR YENA2023013100111None · noneDURING HEAVY MAINTENANCE: (CPCP FINDING) CORROSION ON STRG 23LH LOCATED BTW FR 86/ FR 90 AT CENTER FUSELAGE III INTERNAL STRUCTURE; (RESOLVED ON W/O: 1177513 TASKCARD: NR-00048 ) REF NRC 00328: CORROSION IS OUT OF LIMITS. REPAIRED STRINGER PER EMB E190 SRM 53SDR YENA2023013100110None · noneDURING HEAVY MAINTENANCE: (CPCP FINDING) CORROSION ON STRG 21LH, LOCATED BTW FR 86/ FR 90 AT CENTER FUSELAGE III INTERNAL STRUCTURE; (RESOLVED ON W/O: 1177513 TASKCARD: NR-00049 ) REF NRC 00327: CORROSION IS OUT OF LIMITS. REPAIRED PER EMB 190 SRM 53-23-03 REPSDR FDEA2023013020177Skin · chafedTAILCONE RH INNER SKIN - APPROX STA.2163 UPPER AREA - WORN/CHAFED.SDR CALA2023013000254Skin · corrodedSKIN BUBBLED JUST AFT OF LOWER CARGO DOOR AT APPROX STA 1440 STR 30 BL0. FOUND STR 30 CORRODED. CUT OUT DAMAGE AND INSTALLED REPAIR IAW SRM 53-00-03-2R-1. WORK PEROFRMED ON AMES ILN N/R 154944-010 0-0010.SDR VNAA202301298006Skin · gougedEXTERNAL FUSELAGE SKIN HAS 2EA.SCRATCHES APPROX. 1 INCH LONG AT F,S.265, 3 INCHES BELOW PILOT WINDSHIELD.
CORRECTIVE ACTION: REPAIRED FUSELAGE SKIN AT F.S. 265 STGR 12 IAW OLIVER WYMAN EA 23-C7-53-0096 REV IR, DATED 01/23/2023.SDR DALA2023013000754Skin · corrodedSHIP 3209 CORROSION SKIN EXTERNAL DOUBLER REPAIR LOCATED BETWEEN FR69 TO FR70 AN D STR30R TO STR32R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 605435-14 REV.0 VALIDATED ER/A 605435-14AD REV.ORIGINAL. (2604681)SDR DALA2023013000753Skin · dentedSHIP 3209 DENT EXTERNAL SKIN LOCATED FR59 AND BETWEEN STR34L TO STR35L LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 605406-14 REV. ORIGINAL. (2604393)SDR DALA2023012900728Access Door · missingAC 3701, ON ARRIVAL INSPECTION; FOUND HIGH PRESSURE ACCESS DOOR MISSING (192 DR). CORRECTIVE ACTION: REPLACED DOOR 192DR. LP 7890778SDR DALA2023012900727Skin · damagedAC 3895, REF: AC LOG 9602200 AND 2603084 FWD CARGO DOOR FUSELAGE SKIN DAMAGE. CORRECTIVE ACTION: COMPLIED WITH ERA 605597-14 REV A, B, C STEP 6 OF REVISION B COMPLIED WITH ON PRI 605597-14 ERA REV B PRI REV 0 ALL STEPS ON PRI MATCH ERA 605597-14 REV ORIGINAL, SDR VNAA202301280001Skin · damagedSEVERAL NICKS AT LOWER SKIN OF AFT FUSELAGE BETWEEN FS 1015.0 AND FS 1047.0 AND BETWEEN STRG 27L AND STRG 25R. REPAIRED PER EA 23-C9-53-0053 REV. IR, SECTION III - PERMANENT REPAIRSDR SWIA20230505127Unknown · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA80832-690-53-11-1487 N833SK,MXCODEID64329-PR - BIRD STRIKE DENT FOUND ON RHS NOSE JUST AFT OF LOWER REAR CORNER OF TRU DOOR. FOUND DAMAGE LOCATED AT FUSELAGE SIDE SKIN PANEL BTW FS193.00-FS202.75 & BTW STR15R-STR16R. SDR SWIA20230127None · damagedINBOUND EVALUATION OF HAIL DAMAGE TO THE FWD FUSELAGE LEFT HAND SKIN (P/N 170-03385-003) FOUND TO BE BEYOND ECONOMICAL REPAIR. (C-CHECK RO 2/20/2023) REMOVED AND REPLACED FWD FUSELAGE L/H SKIN (P/N 170-03385-003) REF EMB 175 SRM 51-40-08. THIS ACTION DOSDR DALA2023013000759Skin · corrodedSHIP 3209 CORROSION WAS FOUND ON EXISTING REPAIR DOUBLER, FILLER, INTERNAL REINFORCEMENT PLATE, AND INTERNAL SKIN LOCATED BETWEEN FR 69 AND 70 AND STRG 30 AND STRG 32 RHS. CORRECTIVE ACTION: COMPLIED WITH ERA 605435-32. (2603286)SDR DALA2023012700720Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1087 BTW LONGERONS 14LH AND 15LH. SUMMARY OF NRC 00141: EXTERNAL FUSELAGE SKIN STA Y=1087 BTW LONGERONS 14LH AND 15LH WAS REPAIRED PER ER/A 605226-14 REV. ORIGINAL SECTION I: TEMPORARY REPAIR. ASSOCIATED ER/A 14-605226 ADDSDR DALA2023110909242Unknown · unknown(LOG 2601233) DAMAGE TO THE FORWARD EDGE OF THE FORWARD CARGO DOOR SURROUND SKIN (P/N: 143A3252-31) AND BEAR STRAP (P/N: 143A3254-6). DAMAGE REPAIRED PER B737-900 SRM 53-00-01-2R AND ERA 605597-14.SDR SWIA202300315006Unknown · corrodedRH AFT LOWER WING PLANK HAS CHAFING DAMAGE RBL45 WHERE 193AB IS INSTALLED (C-CHECK RO 3/11/2023) REPAIRED CHAFING DAMAGE ON THE R/H, AFT LOWER WING PLANK AT RBL 45, COMMON TO PANEL 193AB (ZONE A**) REF GENERIC REO 601R-57-21-880 REV-D, DATED 2017/03/06SDR SWAA2023021695627Gusset · crackedCRACK GUSSET LOCATED AT BS 500D S-19R WL 200 FWD CARGO COMPARTMENT 2023-83717<[01] REPLACED GUSSET LOCATED AT BS 500D S-19R WL 200 FWD CARGO COMPARTMENT AND FASTENERS IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 AND DWG 143A7902 SHEET 209; REV-. ?SEE INDIVSDR SWAA2023021695623Angle · crackedCRACK ANGLE LOCATED AT BS 500A S-26L WL 156 FWD FACE FRAME FWD CARGO COMPARTMENT 2023-83713<[01] REPLACED ANGLE LOCATED AT BS 500A S-26L WL 156 FWD FACE FRAME FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7505; SHEET 81; REV: -. SEE INDIVIDUAL SISDR SWAA2023021695628Gusset · crackedCRACK GUSSET LOCATED AT BS 500D S-19L WL 200 FWD CARGO COMPARTMENT 2023-83716<[01] REPLACED GUSSET AND FASTENERS LOC LOCATED AT BS 500D S-19L WL 200 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV -. SEE INDIVIDUAL SDR SWAA2023021695624Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS 492 AND BS 500A AT LEVEL S-26R WL 156 AT FWD CARGO COMPARTMENT 2023-83711<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 492 AND BS 500A AT LEVEL S-26R WL 156 AT FWD CARGO COMPARTMENT IAW B737-70SDR HNAA2023013010027Skin · damagedEXTERIOR FUSELAGE SKIN BETWEEN FR. 25-26/ STGR. 20L-21L HAS POSSIBLE BURN. REPAIRED EXTERIOR FUSELAGE SKIN BETWEEN FR. 25-26/ STGR. 20L-21L BURN MARK IAW SRM 53-00-01, AND PIEDMONT EO1-05-23-0024.SDR REXA2022012700184Skin · chafedSKIN CHAFE AT F.S.942.00 STRINGER 27 REPAIRED FUSELAGE SKIN AT F.S.942 IAW MHI RJ REO 690-53-51-372 REV -- DATED 2023-01-23SDR U2RA2023012760004Skin · crackedWHILE PERFORMING TC 534178-01-8 FOUND CRACK INDICATION AT 3 FASTENER HOLES IN COUPLING AT STR11 RH B/W FR58-59 (REF LP 66178-1), STR 12 RH (REF LP 66177-3) AND STR 13 RH (REF LP 66177-2) B/W FR57-58. APPLIED PERMANENT REPAIR SOLUTION, PERFORMED HFEC INSPECTIOSDR LR7A2023012603262Skin · dentedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB5301, FOUND LH FUSELAGE SKIN ABOVE ICE SHIELD DENTED AT FS378-386, RBL79.5, WL230. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12.SDR SWAA2023030695232Panel · crackedBS 540 CENTER PANEL BREAK IS CRACKED COMMON TO FWD HI-LOK AT LBL 1<[01] REMOVED AND REPLACED FLOOR BOARD CENTER PANEL BREAK AT BS540 LBL1; AND MATCHED DRILLED FLOOR BOARD HOLES IAW SRM 51-40-02 AND SRM 51-40-05;[02] CERTIFIED CORRECTIVE ACTION 1;[03] NO ALLOWASDR SWAA2023030695236Panel · crackedBS 540 CENTER PANEL BREAK IS CRACKED COMMON TO FWD HI-LOK AT RBL 1<[01] REMOVED AND REPLACED FLOOR BOARD CENTER PANEL BREAK AT BS540 RBL1; AND MATCHED DRILLED FLOOR BOARD HOLES IAW SRM 51-40-02 AND SRM 51-40-05;[02] CERTIFIED CORRECTIVE ACTION 1;[03] UPDATED MSDR AALA202302284365Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXTERNAL SKIN PANEL INNER SURFACE UNDERNEATH THE L2 DOOR SURROUND STRUCTURE BETWEEN FR 66 AND FR 68, BETWEEN S22L AND S26L. MAINTENANCE REPAIRED SKIN PANEL PER EA 342363A.SDR AALA202302284380Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON EXTERNAL SKIN PANEL INNER SURFACE UNDERNEATH THE L2 DOOR SURROUND STRUCTURE BETWEEN FR 66 AND FR 68, BETWEEN S22L AND S26L. MAINTENANCE REPAIRED SKIN PANEL PER EA 342363A.SDR ASAA2023012541712Intercostal · corrodedAFT CARGO PIT, L/H TRANSITION PANEL STA 727-727I CORRODED. GROUNDED - YES. EVALUATED & FOUND TO BE OUT OF LIMITS DUE TO 100% MAT. LOSS IN MULTIPLE AREAS. REMOVED DAMAGED TRANSITION PNL FAB'D, LOCATED & DRILLED, ALODINED, PRIMED & INSTALLED IAW B737-800 SRM 53-SDR DALA2023012500638Skin · dentedSHIP 6815 DENT ON SKIN OF FUSELAGE BTW STA 470&480 AND BTW S22&23 RH. DENT ON FUSELAGE SKIN BTW STA 470-480, LONG 22-23 RH WAS REPAIRED PER ER/A 604885-14 REV.ORIGINAL.SDR VNAA202301251111Skin · damagedGOUGE & DENT DAMAGE TO FUSELAGE SKIN BTW FS1015.00 - FS1051.30 AND STR21R - STR26R. PERMANENT REPAIR WAS PERFORMED IAW EA 22-C7-53-0942.SDR SWAA2023030694769Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 19L.<[01] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED GUSSET IAW SRM 51-40-02;[03] UPDATED MEASUREMENTS PARAMETERS;[04] LOCATED AND DRILLED NEW GUSSET AT SDR SWAA2023030694777Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 19R.<[01] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 19R IAW SRM 51-40-02;[03] LOCATED AND DRILLED NEW GUSSETSDR SWAA2023030694778Gusset · crackedCRACK ON FWD CARGO BAY GUSSET AT BS 500D STRINGER 21L.<[01] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM; MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED GUSSET AT B/S 500D STRINGER 21L IAW SRM 51-40-02;[03] LOCATED AND DRILLED NEW GUSSET AT B/S 500D STRSDR SWAA2023030694779Angle · crackedCRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT BS 400+1 LBL 24.<[01] ENTERED MEASUREMENTS;[02] 737-700 SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS EVALUATION.<BR>NO ALLOWABLE DAMAGE FOUND FOR CLIP PN 143A7502-155 IN SRM 53-00-53-1A-2.<BR>REPAIR BY REPLACESDR R61A2023021000111Floor Support · corrodedDRAIN MAST SUPPORT BRKT AND CLIP AT FR 86-87, BTWN STR 27R-28R CORRODED. R&R IAW SRM 51-41-01.SDR HNAA2023013000026Skin · crackedE953561 - POSSIBLE CRACKS AROUND 3 RIVETS ON FRAME 79 BETWEEN STRINGERS 4R – 9R. FURTHER INVESTIGATION FOUND ONLY ONE CRACKED AREA AT RIVET. REPAIRED FUSELAGE SKIN BY REMOVING CRACK AND INSTALLING A BUSHING ON FRAME 79 AT FASTENER BETWEEN STRINGERS 4R – 5R IASDR DALA2023012600668Skin · corroded(LOG 2598071) THE PREVIOUS OPERATOR FOUND A BULGE AT THE SECTION 46 FUSELAGE SKIN AT STA 867, STR S-17R. BOEING WAS CONTACTED AND A PERMANENT REPAIR WAS PERFORMED BY MAINTENANCE. PER 605315-14, SECTION I MUST BE ACCOMPLISHED DURING UPCOMING C-CHECK, PRIOR TO RSDR SWAA2023021694367Baffle · crackedBAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 IS CRACKED<[01] REMOVED BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 PER SRM 51-40-02-0G-0.;[02] CRACK BAFFLE UNDER L/H FLOOR TO SIDEWALL SUPPORT BS 400-420 LBL 25 WITH NEXT DIMENSIONS L=SDR DALA2023012500628Skin · dentedSHIP 6815 DENT ON EXTERNAL FUSELAGE SKIN STA 660 AND STG 17 LH SIDE. REPAIR WAS PERFOMED PER ER/A 604879-14 REV.ORIGINAL. AND PER ER/A 604879-14 PRI REV.1.SDR EE4Y2023012317007Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN EXISTING REPAIR LOCATED BETWEEN FR87 AND FR89 AND BETWEEN STRINGER 13L AND 15L.WAS REPAIRED FOLLOWING EMBRAER REPAIR INSTRUCTIONS UNDER ETD2022-190-034656 REV 00 AND COOPESA EO# COO-EO-2022-16655-R00 AND APPROVSDR EE4Y2023012317006Skin · damagedDURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN INTERNAL REPAIR ANGLE WITHOUT RECORDS LOCATED BETWEEN FR 91 AND FR 92 AND BETWEEN STRINGERS 6L AND 7L.WAS REPAIRED FOLLOWING EMBRAER REPAIR INSTRUCTIONS UNDER ETD2022-190-036011 REV 00 AND COOPESA EO# COO-EO-20SDR DALA2023081106571Unknown · unknownSHIP 3354 LIGHTNING STRIKE DAMAGE IN SKIN 3" AFT OF FRAME 0 AT STRINGER 54R. CORRECTIVE ACITON: FOUND DAMAGE OUT OF BLEND LIMITS AFTER REMOVAL OF SURFACE PROTECTION COATING. PERFORMED CATEGORY C TEMPORARY REPAIR IAW A 330 SRM 53-11-11-300-016. RESTORED SURFACESDR AALA202302225602Skin · crackedAIRCRAFT IN BASE MAINTENANCE: SEVERAL AREAS OF CORROSION IN AFT CARGO COMPARTMENT INTERNAL FUSELAGE SKIN BETWEEN STA 727I AND STA 787 STR 27L-27R. PERFORMED DOUBLER REPAIR PER SRM.SDR DALA2023012400606Plug · damagedPLUG (BOLT) ON EXTERNAL FUSELAGE BS 460, S25 - 26R. THE PLUG (BOLT) BS 460 S25-26R WAS REPAIRED PER ER/A 605364-14 REV. ORIGINAL SECTION I PERMANENT REPAIR.SDR DALA2023033102463Unknown · unknownSHIP 172 ACCOMPLISH REPETITIVE INSPECTIONS PER ER/A 604730-14. CORRECTIVE ACTION: ACCOMPLISH SECTION II REPETITIVE INSPECTIONS OF 604730-14 EVERY 9000 FC BEGINNING AT 37500 TOTAL AC FC. ASSOCIATED ER/A 14-604730 (2590860)SDR DALA2023012400548Skin · handler errorDURING AVOD MOD VISIT, THE FUSELAGE SKIN WAS DAMAGED FROM CONTACT WITH A WORK STAND. THE DAMAGE WAS TRIMMED OUT TO A 1.0 INCH CIRCLE IN THE POCKETED AREA OF THE SKIN JUST BELOW S-4L AND JUST AFT OF BS 727H. PERFORMED NEW ADDITIONAL REPAIR PER ERA 540727-14AD RSDR DALA2023012300481Skin · corrodedSHIP 5636 CORROSION ON FUSELAGE SKIN STA. 1720, BTW S- 30 TO S-27R. CORRECTIVE ACTION: SUMMARY OF NRC 0026: FUSELAGE SKIN STA. 1720, BTW S-30 TO S-27R WAS REPAIRED PER ER/A 605475-14 REV. ORIGINAL SECTION I. (2592064)
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