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 SWAA2022092220227Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS887 - BS987 S-2R TO S-4R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 887 TO 987 S-2R TO S-4R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 907+10' 4' BELOW STR 3R<BR>2) BSDR SWAA2022092220228Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN BS845 - BS887 S-10R TO S-14R. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 845 TO 887 S-10R TO S-14R LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 867+13' 1.5' BELOW STR 13R<SDR SWIA2022081666262Doubler · corrodedMAIN AVIONICS BAY TCAS ANTENNA DOUBLER BETWEEN FS295.00 AND FS310.00 CORRODED (C-CHECK RO 8/14/2022) REMOVED AND REPLACED DAMAGED TCAS DOUBLER. REF. CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-30023 REV G. SEE CONTINUATION CARD FOR DETAILS OF WORK PESDR DALA2022062004302Skin · noneSHIP 3304 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 53 TO FR54 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 599051-14 REVISION ORIGINAL MATCHES WITH ALL STEPS ON PRI ER/A 599051-14 REV. 0 AND REVISIONSDR DALA2022062004301Skin · noneSHIP 3304 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR26 TO FR26.1 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 599051-14 REVISION ORIGINAL MATCHES WITH ALL STEPS ON PRI ER/A 599051-14 REV. 0. EXISTING ASDR CALA2022062001534Skin · corrodedINSP FOUND FUSELAGE SKIN CORROSION BULGE UP AT RH UPP FWD AREA STA 655 STR 6R TO STR 5R TRANSFER REF. NON-ROUTINE HX NRC WO.817939 AND ORIGINATED BY EMP NO. V925649SDR DALA2022062304418Repair · noneERA 595840-14 REV A HAS FOLLOW ON INSPECTIONS OF FUS SKIN REPAIR AT FR8 NEAR EXTERNAL POWER RECEPTACLE. ACCOMPLISH ERA 595840-14 REV A SECTION II WITHIN 15,700 FLIGHT C YCLES AFTER SECTION I AND THEN EVERY 4100 FLIGHT CYCLES THEREAFT ER. ASSOCIATED ER/A 14-595SDR AALA202206235605Skin Panel · damagedAIRCRAFT IN BASE MAINTENANCE: FUSELAGE SKIN DAMAGED AT BS 270 FROM S12L TO S13L. REPAIRED PER EA 336786.SDR CALA2022061701528Stringer · gougedRIGHT HAND REAR FUSEALGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 12 RMEOVED GUSSET PLATE AT FR66 STGR12 IAW SRM 51-44-11; RECEIVED N EW GUSSET PLATE TRAVELER# T22/1620912 P/N UAD5348002075900 BATCH # 0003819824 AND INSTALLED NEW GUSSET PLATE ASDR CALA2022061701527Stringer · gougedRIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 14 REMOVED GUSSET PLATE AT FR66. STGR 14. IAW SRM 51-44-11; RECEIVE D NEW GUSSET PLATE TRAVELER# T22/1620915 P/N UAD5348002075900; B ATCH# 0003819824 AND INSTALLED NEW GUSSET PLASDR CALA2022061701526Stringer · gougedRIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOUGE FROM STRINGER 10 REMOVED GUSSET PLATE AT FR66 STRINGER 10 IAW SRM 51-44-11; RECEI VED NEW GUSSET PLATE TRAVELER# T22/1620904, P/N UAD5349002075900 BATCH# 0003819824 AND INSTALLED NEW GUSSET PLASDR SCNA20220712078Strap · crackedDEFECT: FOUND STRAP DAMAGED UNDER EXTERNAL SKIN AT STA 1138 RH. BEHIND PANEL 343AT SLIDING SEAL (STRAP N/N REF 148A8713-8) RESOLUTION: 7/10/2022 - REMOVED AND REPLACED STRAP UNDER EXTERNAL SKIN STA1138 RH BEHIND PANEL 343AT SLIDING SEAL PO # 511743-1 IAW ASDR DALA2022061704249Frame · damagedSHIP 3409 FOUND DAMAGE AT FRAME 2 & 3 LT STRINGS 49, 50, & 51 FROM LIGHTNING STRIKE. CORRECTIVE ACTION: FOUND SMALL HOLE AND DAMAGE RIVET ON FRAME 2 AND 3 RIVET DAMAGE FROM STATIC DISCHARGE. SMALL HOLE PUNCTURE IN SKIN AT FRAME 2 STATION 7942, LEFT SIDE STRINGSDR CALA2022061701519Doubler · corrodedEA-5100-02129-001 ANTENNA DOUBLER LOCATED AT STA 1500-1520 STR -2 8R IS CORRODED AND GOUGED ON INTERNAL SIDE, TRANSCRIBED FROM HAE CO GSO NR LP 9281209 AF343-2108-00 REV D. HAECO GSO MECH V898621 INSP QC467 REMOVED DAMAGED DOUBLER STA 1500-1520 S28R -S29R IAW SDR SWAA2022092218943Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-2L TO S-4L BS887 - BS947+5. MARKED / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 887 TO 1016 S-2L TO S-4L LISTED BELOW PER SRM 51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 887-907 S-2L TO S-3L<BR>2) BSDR SWAA2022092218944Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-4L TO S-6L BS887 - BS947+6. MARKED S-6L TO S-9L BS927 - BS947. MARKED S-9L TO S-11L BS887 - BS927. MARKED. S-9L TO S-10L BS927 - BS927+15. MARKED. S-11L TO S-14L BS887 - BS907. MARKED. / [01] PERFORMED CLAD PENETRATION TEST SDR SWAA2022092218946Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-10L TO S-14L BS827 - BS887. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 727 TO 887 S-10L TO S-14L LISTED BELOW PER SRM 51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 827-847 S-13L TO S-14L<BR>SDR SWAA2022092218948Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-16L TO S-19L BS787 - BS827. MARKED. / [01] EVALUATED ANOMALIES ON FUSELAGE SKIN AT BS 787+14.5 6.5'BELOW STR 19L D=.0006'; BS 787+12 1'BELOW STR 18L D=.0005'; BS 787+11 6'BELOW STR 17L D=.001'; BS 807+6 6'BELOW STR 18L D=.00SDR SWAA2022092218947Skin · defectiveANOMALY ON EXTERNAL FUSELAGE SKIN S-14L TO S-16L BS827 - BS887. MARKED. / [01] PERFORMED CLAD PENETRATION TEST IN SEVERAL LOCATIONS ON SKIN PANEL BS 727 TO 887 S-14L TO S-23L LISTED BELOW PER SRM51-10-07-0G-0 PARA. 5D-E<BR><BR>1) BS 807-827 S-16L TO S-17L<BR>2SDR SWAA2022071418835Skin · corrodedCORROSION ON FUSELAGE CROWN SKIN FROM STA 1016+5 TO STA 1016+61; RBL 13 TO LBL 13; WL 306.5. / [01] REMOVED FASTENERS ON FUSELAGE CROWN SKIN FROM STA 1016+5 TO STA 1016+61; RBL 13 TO LBL 13; WL 306.5. PER REF SRM 51-40-02 -0G;[02] REMOVED CORROSION FROM CROWN SDR IPXA2022062283371Panel · corrodedINSPECTION TYPE:CAFT CARGO PIT DOOR SILL AT FS 1455 RBL 30 HAS EXFOLIATION CORROSIONREMOVED SIDE PANEL AND ISNTALLED REPLACEMENT 146N5391-2 SIDE PANEL PER SRM 51-40-02SDR IPXA2022062183340Panel · corrodedINSPECTION TYPE:CAFT LOWER CARGO PIT AT FS 1445 RH SIDE TRANSITION PANEL HAS EXFOLIATION ON FWD RH ENDSPLICED A REPAIR SIDE PANEL SEGMENT PER SRM 51-70-11-0GSDR CALA2022061501505Plate · gougedRIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 14SDR CALA2022061501504Plate · gougedRIGHT HAND REAR FUSEALGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 12SDR CALA2022061501503Plate · gougedRIGHT HAND REAR FUSELAGE STRUCTURE - FR66 GUSSET PLATE HAS A GOU GE FROM STRINGER 10SDR VNAA2022082799911Skin · damagedDAMAGED ANCHORED NUT BTW FS985 / FS1000 AND STGR 16LH / STGR 17LH AT AFT BAGGAGE BAY COMPARTMENT (CCT)SDR VNAA2022082799910Support Plate · corrodedCORROSION ON PLATES SUPPORT FLOOR BTW FS1000 / FS1047 AND LBL 35.16 / LBL 40.74 AT AFT BAGGAGE BAY COMPARTMENT (CCT)SDR DALA2022061704223Skin · corroded(LOG 2276552) DURING INSPECTION FOUND CORROSION ON FUSELAGE SKIN PREVIOUS REPAIR TRIPLER AROUND OF LAVATORY BLOW OUT EXHAUST. DOUBLER AND TRIPLER ON THE PREVIOUS SKIN REPAIR AROUND OF LAVATORY BLOW OUT EXHAUST WERE REPLACED PER ER/A 558864-14.SDR DALA2022061504196Skin · dentedSHIP 686 DENT ON EXTERIOR FUSELAGE SKIN STA 440 TO 460 AND BTW S28L AND S29L ( FUS ). CORRECTIVE ACTION:SUMMARY OF NRC 00044: DENT ON EXTERIOR FUSELAGE SKIN STA 440 TO 460 AND BTW S28L AND S27L WAS REPAIRED PER PRI 600093-14 REV. 0 AND ERA 600093-14 REV. ORIG SDR YENA2022061400607Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 87 AND BTW STGR 27R-28R; REF TOMX NR 00281, W/O 1931: NEW SHEAR CLIP WAS INSTALLED PER EMB 190 SRM 51-41-01 PAR 6 AND SRM 51-41--02 PAR 6. ACCOMPLISHED BY 201534008 RII BY 200702030.SDR YENA2022061400606Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP AT FR 82 BTW STGR 27R--28R; REF TOMX NR 00289, WO 1931. A NEW SHEAR CLIP WAS INSTALLED PER EMB 190 SRM 51-41-01 PAR 6 AND SRM 51-41--02 PAR 6. ACCOMPLISHED BY 201534008, RII BY 201429329.SDR DALA2022061404164Door · damagedSHIP 3351 RAMP REPORTED DAMAGE AT LOWER RIGHT FWD OF FWD CARGO DOOR. CORRECTIVE ACTION: FOUND WITHIN REWORK LIMITS AND REWORKED LOWER RIGHT DAMAGE FORWARD OF FWD CARGO DOOR PER A330 SRM 53-21-11. (8511193)SDR VNAA202208279996Skin · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANELS 196AR AND 196DR.SDR SWAA2022092217456Skin · corrodedSKIN PITTING AND ANOMALIES BS 907 - BS 927 STR 6L - STR 7L / [01] REMOVED SKIN PITTING AND ANOMALIES FROM FUSELAGE SKIN AT BS 907-927; STR 6L-7L IAW SRM 51-10-02-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] ACCOMPLISHED UT INSPECTION OF BLENDED AREA LOWEST TSDR SCNA20220712077Skin Panel · crackedDEFECT: EXTERNAL SKIN DAMAGE WAS FOUND TO BE DAMAGED AT STA 1138 RH BEHIND PANEL 343AT SLIDING SEAL. RESOLUTION: 7/10/2022 - ACCOMPLISHED REPAIR TO EXTERNAL SKIN AT STA 138 RH BEHIND PANEL 343AT SLIDING SEAL IAW ATS CR 22-01896 AND ENG-57SCA-10984.SDR ASAA2022061038737Web · corrodedAFT PIT DOOR CUTOUT LWOER SILL WEB HAS CORROSION. (FOUND UPON REMOVAL OF CENTER SCUFFPLATE FOR REPAIR). GROUNDED - YES. REMOVED AND REPLACED OUT OF LIMITS SILL WEB IN AFT CARGO IAW B737-900 SRM 51-40-02-0G-0W 1.25" O .050" R .041" L 42" D .009".SDR DALA2022061504206Skin · noneER/A 599938-14 HAS BEEN ISSUED FOR A FUSELAGE SKIN REPAIR AT FR6 6/67 AND S-41/43RH. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 6 MONTHS (182 DAYS) FROM 09JUN22 WHILE A DAMAGE TOLERANCE ANALYSIS ( DTA ) CAN TAKE PLACE. ER/A TO BE REVISED PRIOR TO THSDR DALA2022061504202Skin · damagedMON, 30 L/L, 8749824;VIS ;FOUND DAMAGE TO FUSELAGE APPX 10" AFT OF FRAME 66 BETWEEN. REPAIRED DAMAGED EXTERIOR FUSELAGE SKIN BETWEEN FR66 AND FR67, AND BETWEEN S-41RH AND S-43RH IAW ER/A 599938-14 REV ORIGINAL ASSOCIATED ER/A 14-599938 ADDED FOR AC 3085. (LP# SDR IXXA2023080901Skin · crackedHFEC OPEN FASTENER HOLE ROTARY SCAN REVEALED DEFECT INDICATIONS AT EACH OF THE LOWER THREE FASTENER HOLES OF THE FWD SERVICE DOOR CUTOUT, STA 332 TO 339, S-19R TO SILL CHORD.SDR I5EA2023060800001Skin · dentedDENT AT STA380 - STA400 BETWEEN STR14L TO STR16LSDR SWAA2022071316537Gusset · crackedFWD CARGO COMPARTMENT AFT L/H SIDE WALL SUPPORT GUSSET CRACKED @ S-19L STA 500D / [01] REMOVED DAMAGED GUSSET REF. SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET REF. 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] OK TO TREAT AND PRIME HOLES;[05] TREATESDR SWAA2022071316538Gusset · crackedFWD CARGO COMPARTMENT AFT R/H SIDE WALL SUPPORT GUSSET CRACKED @ S-19R STA 500D / [01] REMOVED DAMAGED GUSSET REF. SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET REF. 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] OK TO TREAT AND PRIME HOLES;[05] TREATESDR SWAA2022070116559Gusset · crackedFWD CARGO COMPARTMENT L/H SIDE WALL SUPPORT GUSSET CRACKED @ S-19L STA 500D MKD DOT / [01] REMOVED L\H GUSSET AT S-19L STA 500D FWD CARGO COMPARTMENT PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW HOLES TO NEW GUSSET PER B737-700 SRM 51-10-02-0G-0;[03] VERSDR SWAA2022070116561Gusset · crackedFWD CARGO COMPARTMENT R/H SIDE WALL SUPPORT GUSSET CRACKED @ S-19R STA 500D MKD DOT / [01] REMOVED R/H GUSSET AT S-19R STA 500D FWD CARGO COMPARTMENT PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW HOLES AT NEW GUSSET PER B737-700 SRM 51-10-02-0G-0SDR DALA2022070104602None · none(LOG 2269788) DURING OPERATION BY LION AIR, PRIOR TO AIRCRAFT BEING OPERATED BY DELTA, A DENT WAS DISCOVERED IN THE FUSELAGE SKIN BETWEEN STA 500B AND STA 500C, STR 24R-25R. MAINTENANCE REPAIRED DAMAGE PER ERA 598771-14.SDR DALA2022060904050Tail Cone · dentedDENT IN SKIN ON TAILCONE, 0 BL, APPROX 10" AFT OF RUDDER POSITION INDICATOR. INSTALLED REPAIR AT TAILCONE 0 BL APPROX. 10" AFT OF RUDDER POSITION INDICATOR IAW A321 SRM 53-51-11-300-002. REPAIR IS CAT "A". (LP# 2269258)SDR SWAA2022061516067Baffle · crackedFWD CARGO COMP BETWEEN STA 500 AND STA 500A STR 26L BAFFLE CRACKED / [01] REMOVED BAFFLE AT FWD CARGO COMP BWT STA 500 AND STA 500A; STR 26L AS PER B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1 OK TO INSTALL NEW BAFFLE;[03] INSTALLED NEW BAFFLE 143A7510-15;SDR YENA2022060900587Floor Support · corrodedDURING HEAVY MAINTENACE, CORR LATERAL FLOOR SUPPORT Y -1200 FR16; REF ALL WORK ACP ON TOMX W/O N266JB-1946 NR 00636 RPL FLOOR SUPPORT PER SRM 51-41-02.SDR YENA2022060900585Fastener · damagedDURING HEAVY MAINTENACE, LIGHTNING STRIKE FR 24 BTW STR 13L-14L CTR FUSELAGE; RE TOMX NR 1946-00023 - LIGHTNING STRIKE AT FASTENER FR 24 STR 13L-14L REPAIRED IAW EMB 190 SRM 53-00-00 REPAIR 53.SDR YENA2022060900579Shear Tie · corrodedDURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP FR88 AND STGR 27-28 RH, AFT CARGO; ALL WORK ACCOMPLISHED ON TOMEX NRC 394, CORROSION ON SHEAR CLIP FR 88 AND STGR 27-28 RH WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT LIMITS. THE SHEAR CLIP WAS REPLACED PER
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