JASC 5330
Service difficulty reports · 79,347
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 JR2R20181125010Skin · dentedDENT ON FWD FUSELAGE SKIN BETWEEN FR14 AND FR15 STR 21L AND 22L. PERMANENT REPAIR PERFORMED IAW SRM 53-10-01 REPAIR 02P.SDR ASOA2018120763070Skin · corrodedDURING HEAVY CHECK INSPECTION CORROSION WAS FOUND ON THE LOWER FUSELAGE SKIN AT THE RADIO ALTIMETER II LOCATION. FRAME 65 TO FRAME 66.MAINTENANCE REPAIRED I/A/W EMBRAER ETD2018-145-124281 AND SRM 53-00-23SDR ASAA2018112427159Skin · dentedLOWER LT SKIN IS DENTED AT FR61 TO FR62 S36L GROUNDED - YES. ACCOMPLISHED REPAIR TO 2 EA DENTED AREAS BETWEEN FR61 TO FR62 STR 35L TO 37L PER SRM 53-00-11-300-029/042/043.SDR R61A2018112841180Skin · dented***WHILE AIRCRAFT WAS IN FOR C-CHECK*** MAINTENANCE REPORT DENTS BELOW PILOT'S WINDOW BETWEEN FR 10 & 11, STR 14L & 15L. MAINTENANCE PERFORMED A MAJOR REPAIR TO DENTS BELOW PILOT'S WINDOW BETWEEN FR 10 & 11, STR 14L & 15L IAW EMBRAER ETD2018-170-084906. REF AASDR DALA2018112756827Skin · crackedRH FUSELAGE SKIN FOUND 01EA CRACK AT BS1725. SKIN REPAIRED PER SRM 53-80-01. (LP 0838599)SDR CALA2018112302414Skin · crackedREF NR LP 9131011,SUPPORT TASK AD 2017-16-10 EA5310-06900 OP12 RH BS1035 UNDERWING LONGERON FX SKIN AREA 2EA FASTENER HOLES FOUND CRACK AT SKIN,DETAIL REFER ATTACHED FIG ACP PART 1 ECRA 5331-02302 INTERIM REPAIR. WORK ACP ON HAECO HKG NR STS510128 TECH V887387SDR DALA20181126808Skin · corrodedSHIP 6802 INITIAL INSPECTION. CORROSION ON WING CENTER SECTION UPPER SKIN BTW STA 1020 TO 1040, RBL 65 ALSO LBL 33 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00224. ATTENDED WITH ETI-57-18-035 REV. ORIGINAL AND ER/A:572819-14 REV. ORIGINAL. (0835624)SDR DALA2018112610775Skin · crackedFUSELAGE AT STA 1633 S-14R.EXTERNAL CRACKED SKIN REPAIRED (LP 0835521)SDR CALA2018112302409Skin · corrodedCORROSION FOUND ON EXTERNAL SKIN AROUND AFT LAVATORY SERVICE DOOR FRAME. REF. AAR N/R:9725921 ACCOMPLISHED REAPAIR AT LAV SERVICE PANEL CUT OUT BEWEEN STA1540 & 1560 STRINGER 27R - ,29R AS PER U.A.L EC/RA#5331-02300 REV - ( FOR FURTHER DETAILS SEE PARTIAL WORSDR ASOA2018121305336Skin · dentedREF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 DENT ON LH FUSELAGE SKIN AFT OF PITOT PROBE. REPAIRED IAW WITH STS EA 30-2018-224 DATED 11/01/2018.SDR ASOA201812135335Skin · dentedREF BOMBARDIER TUCSON AIR CENTER JOB# 2746375 5 DENTS ON LH FUSELAGE SKIN BETWEEN FS 364.00 AND 394.00, 14L-17L. REPAIRED IAW STS EA 48-2018-074 DATED 11/02/2018.SDR SWAA2018121327665Doubler · corrodedANTENNA RING DOUBLER CORRODED AT BS 310, STR 28L. REPAIRED DOUBLER IAW ER & EA.SDR SWAA2018121327664Bear Strap · corrodedBEAR STRAP CORRODED AT BS 310, STR 28L. REPAIRED BEAR STRAP IAW ER & EA.SDR SWAA2018121327640Doubler · corrodedBASE PLATE CORRODED AT BS 310, STR 28L. REPAIRED DOUBLER IAW ER & EA.SDR ASOA201811205328Skin · dentedFUSELAGE SKIN HAS A SHARP DENT AT FS 591.00 BETWEEN STRINGERS 25R-26R. DENT MEASURES .065" DEEP AND APPROX .758" IN LENGTH. REPAIRED DAMAGE IAW REO 601R-53-61-6773 REV-, DATED 2018-11-15 AND REO 601R-53-61-6773 REV 0, DATED 2018-11-16.SDR DALA2018120407034Skin · corrodedDURING INSPECTION, CORROSION FOUND AT DRAIN MAST STA 1407 ON FUSELAGE SKIN C/W ER/A 572980-14 AND SRM 53-00-01.SDR DALA2018112906875Skin · corrodedMD-88 FUSELAGE STA 480 & L-30 CORROSION - REQUIRED PERMANENT REPAIR ACCOMPLISHMENT. CURRENT REVISION LEVEL OF ER/A 563889-14 IS REV. A. RESULTS OF DTA/DTE HAVE BEEN INCORPORATED AT THIS REVISION LEVEL. ACCOMPLISH SECTION II: PERMANENT REPAIR AT OR PRIOR TO THESDR SWIA2019010845419Doubler · corrodedAV DOOR SURROUND INNER SKIN DOUBLER LIP PITTED AND CORRODED. (C-CHECK) RO: 01/05/2019 REPAIRED THE AVI BAY DOOR BY FABRICATING AND INSTALLING ALUMINUM STRIPS IAW REO, LEAK CHECKS GOOD.SDR DALA2018112106739Access Panel · corroded(LOG 0833827) DURING INSPECTION FOUND CORROSION ON ACCESS PANEL 192 F. ACCESS PANEL 192F WAS REPAIRED PER B-737-800 S R.M 51-70-14 REPAIR 1.SDR DALA2018112006708Skin · corroded(LOG 0833566) DURING INSPECTION FOUND CORROSION ON LOWER FUSELAGE SKIN , BELLOW AFT AIRPHONE ANTENNA. CORROSI?N 2, AREA WAS REPAIRED PER ETI-37-18-550 REV 6 AND ER/A 573121-14 REV: ORIG.SDR DALA2018112006707Skin · dented(LOG 0833553) DURING HCK AT QRO, THREE DENTS WERE FOUND ON FUSELAGE SKIN 141A372115 (M/F 0.071 2024 T3 CLAD SHEET) LOCATED BETWEEN BS 7.73 211.67, AND STRINGERS 17L24L. MAINTENANCE REPAIRED DAMAGE PER ERA 573089-14.SDR FDEA201811193305Repair · tornAFT TAIL COMPARTMENT, RIGHT HAND SIDE, UPPER, FRAME 95, BETWEEN STR 2 & 3, SKIN IS TORN. REMOVED DAMAGED SKIN, CUTOUT IAW SRM 53-19-12 FIG. 202. FABRICATED AND INSTALLED DOUBLER REPAIRES IAW A300 SRM 53-19-12, FIG 202, CAT 'A' AND MAJOR REPAIR.SDR SWAA2022022505663Skin · dentedPRE EXISTING DENT AT STA 380-2 DENT DOT #1033887 APPEAR TO HAVE ADDITIONAL DAMAGE ON STR 17 L=3.5 W=3.0 D=.032 MOD / REPAIR ACCOMPLISHED IAW EA 1-753-34650.SDR DALA2018112696769Skin · crackedCRACK FOUND IN FUSELAGE APROX 4 FT FORWARD AND IN LINE WITH BOTTOM OF BULK CARGO DOOR STATION 1370, STRINGER 32L SKIN. REPAIRED. (LP 5212189)SDR CALA2018111902399Skin · crackedTAIL SKIN CRACK AT STA 1725.5 RHS JUST BELOW APU INLET CORNER. REPAIRED PER SRM 53-80-01 REPAIR 5 PAGE 201 PERFORM CATEGORY B REPAIR INSPECTION PER TABLE 3 SRM 53-80-01 REPAIR 5 PAGE 203 AT 6000 CYCLES AFTER REPAIR. DIP 53-DIP PLEASE IDENTIFY WHICH CORNER OF TSDR DALA2018112686768Skin · corrodedAFT LOWER LEFT EXTERNAL FUSELAGE SKIN BULGING, FUS STA 1370, STRINGER 32LEFT INSTALLED REPAIR PER SRM 53-00-01. (LP 0830715)SDR AALA2018112017010Skin · crackedSKIN CRACKED AT BS 1380, STRINGER 14L. REPAIRED THE SKIN IAW SRM 55-01-00.SDR SWIA2019010845417Skin · bentGROUND AIR CONDITION DOOR CUT OUT INNER FLANGES FWD AND AFT EDGE IS BENT. (C-CHECK) RO: 01/05/2019 COMPLIED WITH ALL STEPS OF REPAIR IAW REO.SDR SWAA2018122027779Skin · corrodedFUSELAGE UNDER DORSAL FIN CORRODED BETWEEN BS 887 TO BS 1007. REPAIRED DORSAL FIN PER ER AND EA.SDR SWAA2018121427672Skin · corrodedFUSELAGE EXTERIOR SKIN CORRODED BETWEEN BS 887 TO BS 1016, BETWEEN STR 2L TO STR 2R. REPAIRED SKIN IAW ER AND EA.SDR IPXA2018111636017Skin · puncturedFUSELAGE SKIN WAS PUNCTURED AT BS 540 - 560, STRINGER 33 - 34R. INSTALLED A TEMP DOUBLER REPAIR IAW EO B747-5330-70630-A.SDR 7C7A2018111650461Skin · dentedMULTIPLE DENT DAMAGE TO FUSELAGE SKIN PANELS BETWEEN STA. X312.35 - X333.3 AND STR. 3P - 2S. REMOVED DAMAGE AND ENSURE REMAINING DENT MEETS REQUIREMENT AS STATE IN RD, INSPECT FOR CRACK AND DISBOND INDICATIONS, FABRICATE AND INSTALL AN EXTERNAL REPAIR DOUBLERSDR SWAA2022022809690Landing · brokenA/C EXTERNAL POWER DOOR CUT OUT HAS A PIECE BROKEN OFF AND BENT SECTIONS NEAR MIDDLE DOOR LATCH PAD. / REPAIRED ELECTRICAL GROUND POWER RECEPTACLE LANDING IAW SRM 53-10-15-2R-4 REPAIR 4SDR COEA2018111505807Skin Panel · corrodedWO 187945 NR 200099 HEAVY CHECK COE/MAJOR REPAIR: REAR FUSELAGE LT UPPER SKIN PANEL INTERIOR SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 41-42, STRINGERS 3L-4L. CORRECTIVE ACTION: REPAIRED PER SRAS ES-0089130-01...13814 DATED 12/4/2018.SDR DALA2018111606662Skin · damaged(LOG 0828245) DURING HCK AT QRO, TWO DENTS AND A CREASE WERE FOUND AFFECTING THE FUS. SKIN 143A3212-8 (MADE FROM 0.090, 2024-T3 -STOCK- THICK CLAD SHEET, 0.040 THICK ON THE DAMAGED AREA) BETWEEN BS 380-400 AND BETWEEN S17L-S18L. MAINTENANCE REPAIRED DAMAGE PSDR 7C7A2018111500457Skin Panel · dentedMULTIPLE DENT DAMAGE TO THE LT FUSELAGE SKIN PANEL BETWEEN STA X270.5 - X291.4 AND STR 8P - 9P. REPAIRED IAW RD 8-53-15931 AND ECO 008.53-18.51.SDR MK1Y20181115005Lap Joint · corrodedFOUND CORROSION AT STA 1197+132 TO STA 1219 COMMON TO STR 36R LAP JOINT SPLICE UPPER ROW OF FASTENERS ON THE LOWER SKIN.SDR MK1Y20181115004Skin · corrodedFOUND DEEP CORROSION IN THE DRAIN HOLE AREA ON THE INNER SIDE OF THE FUSELAGE SKIN AT STA 1087 BETWEEN STRINGERS 39R TO 39L.SDR SWAA2022022870248Scuff Plate · crackedSUPPLEMENTAL INFORMATION: FWD CARGO; AFT CORNER THRESHOLD CRACKED. / R&R FWD CARGO; AFT CORNER SCUFF PLATE PER AMM 53-11-02.SDR DALA2018112746823Skin · corrodedCORROSION LEVEL: 2 FUSELAGE SKIN AT STA 1395- 1417 S35R - S36R FOUND CORROSION AFT DRAIN MASK. C/W ERA 572980-14SDR A6WA2018112146174Landing · crackedLH TRU DOOR PANEL LANDING SKIN IS CRACKED BY THE AFT LATCH. REPLACED REPLACED LH TRU DOOR PANEL LANDING IAW CRJ 200 SRM 51-42-06 AND AWAC SUPP 17-280SDR DALA2018111956680Skin · damaged(AIRCRAFT 5650, L/P 0827290) LOCATED NON STANDARD FASTNER STA 1450 BTWN 28L-29L. REPAIRED FUSELAGE SKIN AT STA 1450 BETWEEN STR 28L- AND 29L IAW B757 SRM 53-00-01 REPAIR 3. CUT OUT DIM 1.65" X 1.47". INSPECTION REQUIRED AT 37,500 FC FROM DATE OF REPAIR INSTALLSDR CALA2018111402368Skin · chafedREF NR LP 9131788 B767-55-3-6018: RH FX SKIN FOUND CHAFING MARK AT STA 1809.5 TO 1820 WL241 RH FX SKIN AT STA 1809 TO STA 1820 WL241 REPAIRED AS PER ECRA 5331-02281 ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 24 ACCOMPLISHED ADD EMP:V897491 INSPESDR SWAA2022022831037Scuff Plate · crackedAFT CARGO BAY AFT CORNER THRESHOLD CRACKED. / RECIEVED AFT CARGO BAY AFT CORNER THRESHOLD P.O. NUMBER 716841 59359U 03DEC18SDR AALA2018121989018Skin · crackedA CRACK INDICATION WAS FOUND ON THE SKIN AT FRAME 35, STRINGER 30R. REPAIRED THE SKIN IAW 287099.SDR AALA2018121989017Skin · crackedA CRACK INDICATION WAS FOUND ON THE SKIN AT FRAME 35, STRINGER 30L. REPAIRED THE SKIN IAW EA 287098.SDR AALA201811276003Skin · corrodedLT FUSELAGE SKIN AT AFT VACUUM BLOWER EXHAUST CUTOUT WAS CORRODED AND BULGING BETWEEN BS 1958 AND 1979, STRINGERS 35L AND 36L. REPAIRED THE SKIN IAW SRM 53-70-01-2R-1, FIG 202.SDR RAIA2018111630001Skin · puncturedPLEASE FIND THE ATTACHED INFORMATION CONCERNING; 16112 SDR RAIA201811130001
FORWARD FUSELAGE II - LOWER SKIN AT JACK POINT - PUNCTURE – PERMANENT REPAIR HAS BEEN PERFORMED IAW: ETD2018-145-117303
DETAILS FOR THIS REPAIR HAVE BEEN EMAILED TO 9-AMC-SDR-PRSDR CALA2018111402367Skin · chafedREF NR LP 9131787 B767-55-3-6018 LH FX SKIN FOUND CHAFING MARK AT STA 1809.5 TO 1820 WL241 LH FX SKIN AT STA 1809 TO 1820 WL241 REPAIRED AS PER ECRA 5331-02281 ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 25 ACCOMPLISHED AND FASTENER HOLE SHORT EDSDR C77A2018111300001Skin · puncturedAIRCRAFT 216NN WAS AOG IN LAX DUE TO THE DISCOVERY OF PUNCTURE DAMAGE ON THE CENTER FUSELAGE III LOWER SKIN PANEL,
P/N 170-91883-005, BETWEEN FR89/FR90 AND STGR25R/STGR29R. THE DAMAGE CONSISTED OF A DENT AND PUNCTURE THAT ARE
LOCATED BETWEEN FR89/FR90 AND ST
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