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 DALA2023051103721Unknown · unknownSHIP 6801 PROTUBERANCES (2) ON EXTERNAL FUSELAGE SKIN BTW STA 395 AND BTW S-23L - S-24L. CORRECTIVE ACTION: SUMMARY OF NRC 00009 PROTUBERANCES (2) ON EXTERNAL FUSELAGE SKIN AT STA 395 AND BTW S-23L/S-24L WERE REPAIRED PER PRI NO.607955- 14 REV.3 AND ER/A NO.60SDR DALA2023051003699Unknown · unknownSHIP 671 ER/A 599012-14 / SECTION III ONE-TIME INSPECTION. CORRECTIVE ACTION: REF ERA 599012-14 REV A. (2759091)SDR CALA2023051001450Skin · damagedBULK CARGO EXISTING DOUBLER REPAIR RIVET INSTALLED POOR CONDITIO N AT STA1518-1502S-25L AS PER JC 64-5300-1-2562 STALLED ON FUSELAGE SKIN BETWEEN STA 1502 & 1518 AND S24L & 25L EACHING 30,000 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTION AT INT HAS BEEN APPROVED SDR CALA2023050901423Skin · unknownPREVIOUS REPAIR DOUBLER FOUND ON FUSLAGE SKIN AT STA 1916 STR S-42L. WORK TRANSFER NON ROUTINE WO.1767552 AND ORIGINATED BY V897425. FUSELAGE SKIN AT STA 1916 STR S-42L REPAIRED PER SRM 53-00-01-2R-3 REPAIR 3 RII APPROVED BY HX126723 FUSELAGE SKIN AT STA 191SDR AALA202306292842Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT INTERNAL DOUBLER BETWEEN FR 30 AND FR 31, BETWE S42L AND S43L. REPLACED DOUBLER PART NUMBERS D53230947000 (AALA202306292842) AND D53230947001 (AALA202306294132) PER SRM 51-72-11.SDR AALA202306294132Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT INTERNAL DOUBLER BETWEEN FR 30 AND FR 31, BETWE S42L AND S43L. REPLACED DOUBLER PART NUMBERS D53230947000 (AALA202306292842) AND D53230947001 (AALA202306294132) PER SRM 51-72-11.SDR DALA2023050703548Unknown · unknownAIRCRAFT 3121, ELONGATED HOLE LEADING EDGE ON OUTER WING FRONT SPAR AND AT LEVEL OF R IB 1 ON INBOARD EGDE OF SLAT 1 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FIXED LEADING EDGE INBOARD SIDE LH WING AS PER ER/A 607848-14. (LP 2755098)SDR SWI2023F00058Unknown · crackedDURING THE AUDIT OF 1C TASK CARD 53-160-301, INTERNAL ZONAL INSPECTION OF THE RIGHT MAIN LANDING GEAR WHEEL WELL (EWIS), FOUND THE RH HYDRAULIC FUSE BRACKET CRACKED. (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW BRACKET P/N 601R75278-11 FROM RIGHT MSDR SWIA202305150006Skin · dentedTRANSFER FROM EAML 1134038 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1133456. FOUND DENT AND GOUGE BETWEEN FR 86 AND 87, AND STGR 21R AND 23R. (FLT 5301 FILED CLOSED)REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FR 86 AND 87, AND STGR 21R AND 23R INSDR DALA2023051003684Unknown · unknown(LOG 4174674) DURING INSPECTION FOUND SEVERAL LIGHTENING STRIKES ON RT SIDE OF A/C IN FRONT AND BEHIND WING. REPAIED 10 EACH LIGHTENING STRIKES ON ELECTRONIC NR'S 1-5, 7, AND 10-13 PER B737 AMM 53-00-01.SDR SWIA2023050900016Unknown · dentedTRANSFER FROM EAML 1134038 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1133456. FOUND DENT AND GOUGE BETWEEN FR 86 AND 87, AND STGR 21R AND 23R. (FLT 5301 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR SWIA20230628505Unknown · dentedDENT ON EXTERIOR SKIN AT FS265 BETWEEN STGR26L-STGR25L (C-CHECK RO 6/25/2023) REPAIRED EXTERIOR SKIN AT FS265 BETWEEN STGR26L-STGR25L REF REO 601R-53-11-3867 REV -- DATED 2023-06-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUASDR SWI2023F00091Unknown · cracked* NOSE LANDING GEAR WHEEL WELL, CLIP AT RBL9, FS202 IS CRACKED. (C-CHECK RO 6/20/2023) REMOVED AND INSTALLED NEW FABRICATED CLIP AT NOSE LANDING GEAR WHEEL WELL, AT RBL9, FS202 REFCRJ200 SRM 51-42-06 AND DWG#604-33101 REV-P. COMPLIED WITH TASK CARD 51SDR DALA2023050803554Unknown · unknown(LOG 2753206) WHILE REMOVING AND REPLACING THE LH STA 663.75 PICKLE FORK FITTING TOOLING DAMAGE OCCURRED TO THE CENTER WING REAR SPAR WEB (111A1101-2) AND THE REAR SPAR TERMINAL FITTING (112A1511-201) AT THE HOLE COMMON TO THE OUTBOARD BOTTOM MOST FASTENER OF SDR DALA2023050803553Unknown · unknown(LOG 2753155) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER EM 5300-01157, MAINTENANCE FOUND A CRACK ON THE FAILSAFE STRAP COMMON TO THE LH FS663 PICKLE FORK FITTING. MAINTENANCE REPAIRED CRACK PER ERA 607710-14AD.SDR CALA2023050501367Skin · corrodedAFT LOWER CORNER FASTENER HOLE HAS CORROSION IN IT AT THE L1 DOOR CUTOUT. REPAIRED L1 DOOR SKIN AT AFT LOWER CORNER IAW B767 SRM 53-10-01 REPAIR 1 FIG 201 DETAIL III, AND ECRA 5310-08135.SDR SWAA2023061648909Doubler · crackedEXTERNAL POWER RECEPTACLE LOWER FRAME IS CRACKED<[01] ACCOMPLISHED PERMANENT REPAIR AT EXTERNAL POWER RECEPTACLE SURROUND DOUBLER ON LOWER SIDE REF B737-700 SRM 53-10-15-2R-4 FIG 204.;[02] VERIFIED STEP 1SDR SWAA2023061445783Gusset · crackedCRACK GUSSET LOCATED STA 500D AND STR 19L FWD CARGO COMPARTMENT 2023-310302<[01] REPLACED GUSSET LOCATED STA 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG: 143A7902 SHEET: 174 REV: - . SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLASDR SWAA2023061445784Gusset · crackedCRACK GUSSET LOCATED STA 500D AND STR 19R FWD CARGO COMPARTMENT 2023-310305<[01] REPLACED GUSSET LOCATED STA 500D AND STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7902 REV:- SHEET 174. SEE INDIVIDUAL SIGNOFFS BELOW;[02] CERTIFIED SDR SWAA2023051945646Doubler · crackedEXTERIOR ELECTRICAL GROUND POWER RECEPTACLE LOWER SIDE FOUND CRACK ON SURROUND DOUBLER<[01] AUDIT CWSDR DALA2023050503539Unknown · unknownSHIP 672 DENT ON PREVIOUS REPAIR (PLUG) BTW STA 356/ STA 377 AND S-3L/S-4L ON FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00052: DENT ON PREVIOUS REPAIR (PLUG) BTW STA 356 / STA 377 AND S-3L/S-4L ON FUSELAGE SKIN WAS REPAIRED PER ER/A 608028-14 REV. ORIGISDR DALA2023050503532Unknown · unknownSHIP 3241 NEED TO COMPLY WITH CRACK MONITOR INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 602461-14 REV B SECT V. (2752135)SDR DALA2023050503531Unknown · unknownSHIP 3241 FUSELAGE/WASTE SERVICE PANEL CUTOUT/602461-14 REV B SECT IV SKIN INSPECTION AT OVERSIZED HOLES. CORRECTIVE ACTION: REPAIRED PER 602461-14 REV B SECTION IV. (2752131)SDR DALA2023050503530Unknown · unknownSHIP 3241 NEED TO COMPLY WITH CRACK INSPECTION. CORRRECTIVE ACTION: COMPLIED WITH ERA 602461-14 REV B SECT III. (2752122)SDR DALA2023050503507Unknown · unknown(LOG 2751708) DURING CHECK AT FLIGHTSTAR (VQQ), WHILE PERFORMING INSTRUCTIONS PER TASK CARD 2020-9001, A DENT WAS FOUND AFFECTING THE EXTERNAL PANEL SKIN P/N 143A3252-31, BETWEEN STA 360 & STA 400 AND BETWEEN S-20R & S-21R. MAINTENANCE REPAIRED DENT PER ERA 60SDR GTIA2023050537168Skin · dentedDENT ON FR 8 RIGHT SIDE BELOW FIXED WINDOW. RAF 01 CREATED. SDR SUBMITTED.-ACCOMPLISHED SPIRIT EA 5311-2336SDR SWAA2023052545067Angle · crackedFWD CARGO R/H SIDEPLATE HAS POSSIBLE CRACK AT I/B ATTACH FASTENER RBL 21; STA. 500B.<[01] CRACKED FOUND OUT OF LIMIT .I.A.W. SRM 53-00-53-1A-2.;[02] REMOVED RH TRANSITION ANGLE STA 500B-500I PER SRM 51-40-02;[03] LOCATE AND DRILL REPAIR PARTS FROM STA 500B TO SDR SWAA2023052545083Plate · crackedFWD CARGO L/H SIDEPLATE HAS POSSIBLE CRACK AT I/B ATTACH FASTENER LBL 21; STA. 500B.<[01] FWD CARGO L/H SIDE PLATE FROM STA 440+10 TO STA 500I REPLACED ON FAULT TTG8Q00KSRV.;[02] CORRECTIVE ACTION #1 ENTERED INCORRECTLY. FWD CARGO L/H SIDE PLATE FROM STA 440+1SDR SWAA2023052445065Plate · crackedFWD CARGO L/H SIDEPLATE HAS PUNCTURE WITH CRACK AT LBL 24; STA. 500C +13'<[01] PUNCTURE FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2.;[02] CUT AND REMOVED THE DAMAGED TRANSITION ANGLE FRO STA 450 TO STA 500I L/H PER SRM 53-00-53-2R-5.;[03] LOCATED AND DRISDR ASAA2023050343260Skin · gougedLATE FIND, MISSED ON PRIMARY. FUSELAGE SKIN ABOVE R/H HORZ ROOT@ BLADE SEAL TRACK IS HAS GOUGE. GROUNDED - YES. EVALUATED DAMAGE ON FUSELAGE SKIN @ STA 1145 ABOVE R/H HORZ ROOT.ORIGINAL THICKNESS .100,MAT REMOVED .060,MAT REMAINING .040.FOUND TO BE OUT OF LIMISDR SWIA2023050900003Unknown · dentedTRANSFER FROM EAML 1132488 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1132169FOUND THREE DENTS IN SKIN FWD OF LT TRU DOOR. ONE DENT IS 3.25"BY 2.25" BY .016" DEEP. THE NEXT DENT IS 1.5" BY 2.75" BY .094" DEEP WITH THE UNDERLYING STRINGER DEFORMEDSDR DALA2023050503542Unknown · unknownSHIP 672 DTA MONITOR INSPECTION LOG REF ERA 608028-14. CORRECTIVE ACTION: REF ERA 608028-14SDR FDEA202305030798Skin · chafedFORWARD CARGO DOOR AFT LOWER JAMB CUTOUT DOUBLER FOUND CHAFED. REPAIRED AS PER EA # 1-5330-T0318205 A P3 & P4 TITLE: FUSELAGE - PLATES & SKINS - FWD CARGO DOOR CUTOUT AFT JAMB, STA1002, L-39R TO L-41R - SRM 53-00-15, REPAIR 8. REPAIR CLASSIFIED AS MAJOR PSDR IXXA2023052202Skin · crackedCRACK INDICATION EXISTS IN THE FUSELAGE SKIN AND BEAR STRIP AT THE LOWER AFT CORNER L1 DOOR CUTOUT.SDR AALA202305106540Skin · brokenAIRCRAFT IN BASE MAINTENANCE: BROKEN DRAIN EXTERNAL SKIN STA1016 BETWEEN S25R AND S27R AT LOWER FUSELAGE. REPLACED DRAIN EXTERNAL SKIN STA1016 BETWEEN S25R AND S27R AT LOWER FUSELAGESDR DALA2023050303444Unknown · unknownSHIP 3319 2 DENTS FOUND AT FRAME 74 BETWEEN STR L30 AND L31. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR REF A330 SRM 53-41-11-300-016. (2748383)SDR DALA2023050303441Unknown · unknownSHIP 3319 2 DENTS FOUND AT FRAME 74 BETWEEN STR L30 AND L31. CORRECTIVE ACTION: REPAIRED REF A330 SRM 53-41-11-300-016. (2748387)SDR IPXA2023050293079Skin · crackedINSPECTION TYPE:NA*MAJOR REPAIR* RIGHT SIDE AIRCONDITION DOOR SKIN CRACK UPPER AFT CORNER.REPAIRED PER EO MD11-5330-86147B.SDR SWAA2023052443688Shield · corrodedFWD CARGO BAY AFT SHEILD AT BS 492-500A RBL 24 WL 156 IS CORRODED<[01] CORROSION ON ACB FWD SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO ENTRIES IN SRM FOR ALLOWABLE DAMAGE; PART TO BE REPAIRED BY REPLACEMENT IAW. SRM 51-10-02-0G-0 PAR-9.C.;[02] RECEIVED SHIELD SDR DALA2023052204050Unknown · unknownINNER LAP SKIN HAS SURFACE CORROSION. STA 1006-1047, JUST ABOVE STR 26L. -MARKED-. SUMMARY SEE NRC 077-0001:0514-2001/008 00375: REPLACED INNER SKIN SIN LAP FINGER DOUBLER REF DACDWG 5919707. (LP #2746141)SDR CALA2023050301315Skin Splice · corrodedCORROSION FOUND IN LAP SPLICE STA 1660 RH SIDE S25R-S26R. NSPECTION THRESHOLD 37500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY R COMES LATER, REF TABLE 206 ZONE A *[6] ALTERNATIVE I *[1]. WOR AND INSPECTOR (RII) QC 68 V932161. OR REPEAT INSPECTION INTERVAL AFTER THSDR ASAA2023043043072Skin · corrodedSKIN AT STA 364 TO STA 370 STR 26L HAS AREAS OF CORROSION. GROUNDED - YES. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS B737-900 SRM 53-00-01-1A-5. REPAIRED SKIN IAW ASA EA 900-53EA-25528. FOR WORK ACCOMPLISHED SEE ASA T101 W/O 1944292/ N/R-00024 AAR W/O 10211SDR IPXA2023042993040Skin · damagedINSPECTION TYPE:SPV*MAJOR REPAIR* LH FUSE STA 518 BELOW SCUFF PLATE HAS A DENTREPAIRED PER EO B757-5330-86739-ASDR IPXA2023042993039Skin · damagedINSPECTION TYPE:SPV*MAJOR REPAIR* LH FUSE STA 550 BELOW SCUFF PLATE HAS DENT AND CRACKREPAIRED PER EO B757-5330-86711-ASDR SWIA20230428Skin · gougedUPON REMOVAL OF VWS BOX FOUND 4 AREAS OF GOUGES ON EXTERNAL CF III SKIN AROUND FASTENER HOLES, AND 29 HOLES DRILLED OUT OF ROUND BETWEEN FR 88- 89, BETWEEN STGR 28R- 25R AS MARKED. (C-CHECK RO 5/12/2023) REPAIRED 4 AREAS OF GOUGES ON EXTERNAL CF III SKISDR SWAA2023050242588Support · crackedWING TO BODY FAIRING 191AL AFT VERTICAL SUPPORT CRACKED AT WING LEADING EDGE<[01] REMOVED AND REPLACED WING TO BODY FAIRING 191AL AFT VERTICAL SUPPORT AT WING LEADING EDGE IAW SRM 51-40-02SDR DALA2023050203391Unknown · unknownDENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE, IN REFERENCE TO LP 1614671 AND LP 1614671. SUMMARY OF NRC 00535: FUSELAGE EXTERNAL SKIN BTW STA Y=229 TO 237 AND L-17L TO L-18L WAS PERMANENT REPAIRED PER B717-200 SRM 53-10-01-2R REPASDR DALA2023042803322Unknown · unknownDENTS ON EXTERNAL SKIN BTW STA Y=218 TO 245 AND L-17L TO L-18L AT FUSELAGE. SUMMARY OF NRC 00525: DENTS ON EXTERNAL SKIN BTW STA Y=218 TO 229 AND L-17L TO L-18L AT FUSELAGE WAS ATTENDENTED WITH LOG 1614618, 1614633, & 1614629 AND FOUND WITHIN ALLOWABLE LIMITS SDR SWAA2023052441421Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9. REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL;FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACESDR SWAA2023052441423Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02 PARAG 9.REPAIRABLE BY REPLACEMENT.;[02] PRIOR TO REMOVAL;FOUND PART HAS NOT ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRABLE BY REPLACEM
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