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 CALA2020021700454Skin · crackedFR 35-36 RH FOUND 12 HOLES WITH CRACK INDICATIONS 1,4,17,18,20,2 1,22,24,25,26,27,28 CONTACT ENGINEERING FOR REPAIR INSTRUCTION A ND REPAIR BEFORE NEXT FLIGHT PER HAECO LCQ NR LP 9292402 ACCOMPLISHED INTERIM REPAI RS TO ALL 12 HOLES FR35-36 R/H IAW ECRA 5331-SDR HDNA2020020218Skin · crackedTAIL CONE SKIN CRACKED WITH APPROXIMATELY 3.3 INCH CRACK TO RIGHT TAILCONE SKIN P.N. L533M1022216.SDR DALA2022050703191Doubler · dented(LOG 6669454) DURING INSPECTION FOUND DENT / SCRAPE FOUND ON PREFLIGHT INSPECTIN UNDER 2L DOOR. PERMANENT REPAIR WAS PERFORMED ON BELOW 2L DOOR I.A.W. B737 SRM 53-00-01-2R-3 FIG.201 REV. 75.00 03/18/22 DOUBLER REPAIR: L=11.3 " W=9.1" AND LOCATED AT STA 959 ANDSDR SWAA2021081023032Doubler · corroded***CORROSION*** DOUBLER UNDER THE VHF ANTENNA AT STATION 727D + 10; BL 0; WL 150 HAS CORROSION. / REMOVED CORROSION FROM EXTERIOR SURFACE UNDER THE VHF ANTENNA AT BS 727D+10 BL 0 WL 150 PER SRM 51-10-02. REMOVED IN AREA OF 5.4' X 3.0' X .002' AND FOUND TO BE OSDR DALA2020022051277Skin · dentedDURING EVAL OF MONITER LOG #0706231 FOUND DENT AT BS434+11 3" ABOVE STR 25R CREASED. PERFORMED EXTERNAL SKIN REPAIR PER SRM 53-00-01. (LP 1489930)SDR RAIA2020021940001Skin · damagedFWD FUSELAGE SKIN DAMAGED ABOVE CAPTS WINDOW.................REMOVED DAMAGED AREA INSTALLED DOUBLER AND TRIPLER ON FWD FUSELAGE SKIN ABOVE CAPTS WINDOW IAW ETD 2020-145-005075SDR IPXA2020030252616Skin · damagedINSPECTION TYPE:2CPREVIOUS MAJOR REPAIR AT LOWER FWD CARGO DOOR CUTOUT AFT SIDE HAS EDGE DAMAGE.REPAIRED DAMAGED PREVIOUS MAJOR REPAIR AT LOWER FWD CARGO DOOR CUTOUT AFT SIDE IAW VT-SAA EA 011-5330-01-A8036 REV. IR AND UPS EO MD11-5330-75654-A. (MINOR)SDR FDEA202002140333Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE UNDERWING LONGERON AND FUSELAGE SKIN FOUND 02 EACH CRACKS WHICH APPROXIMATE 0.3" AT STATION 1032. STRINGER 37 RIGHSDR SWAA2020022871767Skin · incorrectSKIN INTERNAL BETWEEN BS. 611 TO BS. 615, BETWEEN STR. 1 TO STR. 2R REQUIRED REPLACEMENT. / R&R FUSELAGE SKIN IAW EA.SDR YENA2020021730176Skin · not reportedDUIRNG HEAVY MAINTENANCE, EXISTING REPAIR EXTERNAL SKIN FR69-FR70 STR29R-STR32R LWR FUSELAGE(AGING A/C PROGRAM); REF AE NR 2020-20462 W/O 2020-71/1 REMOVED AND REPLACED EXISTING REPAIR FR69-FR70 STR29R-STR32R IAW SRM 53-41-11-300-004 CAT A REPAIR NO FURTHER INSDR CALA2020021600426Skin · crackedDURING INSPECTION OF RIGHT HAND FRAME 35-36 EA5330-05216 FOUND MULTIPLE HOLES WITH DEFECTS/CRACKS ACCOMPLISHED INTERIM REPAIR IN REF TO ECRA 5331-02607 PART 1, ACCOMPLISH PERMANENT REPAIR IN REF TO PER PART 3 OF ECRA 5331-02607 ON OR BEFORE 76,475CYCLES OR 166SDR SWIA2020040749991Skin · dentedDENT FOUND BELOW CARGO DOOR 6.8" AFT OF F.S. 605.0 AND BETWEEN STGR 18L AND 19L. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/4/2020 REPAIRED DENT PER REO. COMPLESDR SWIA2020033049548Plate · corrodedTHE PLATE UNDER THE TRANSMITTER ANTENNA NO.2 HAS CORROSION. (MARKED) (C CHECK) RO 3/27/2020 REMOVED CORROSION FROM PLATE UNDER TRANSMITTER ANTENNA #2 REF CRJ 200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW PLATE UNDER THE TRANSMITTER ANTENSDR DALA2020021421159Doubler · cracked(LOG 1485967) DURING INSPECTION FOUND CRACKS ON INTERNAL PRODUCTION DOUBLER AT EXTERNAL PWR RECEPTACLE CUT OUT. CRACKS ON INTERNAL PRODUCTION DOUBLER AT EXTERNAL PWR RECEPTACLE CUT OUT WAS REPAIRED PER ETI-37-20-310 REV.1 AND ER/A 585248-14.SDR HALA2020021210035Skin · corrodedDURING 1C CHECK, AFT FUSELAGE EXTERIOR SKIN HAS SEVERAL AREA'S OF CORROSION AROUND APU RAM AIR DOOR.(I/B OF 313AL). // SUMMARY OF WORK COMPLETED. CORROSION LEVEL 2. ACCOMPLISH ALL STEPS ON PRI 585237-14 REV ORIG. REPAIRED PER ERA 585237-14 REV. ORIGINAL.SDR ASOA202002117017Skin · dentedDAMAGE TO FUSELAGE AT FRAME 22, STRINGER 15L-16L. REPAIRED AREA BY CUTTING OUT DAMAGE, FABRICATING AND INSTALLING FILLER & DOUBLER.SDR SWAA2020022041556Skin · corrodedEXTERNAL SKIN AT POTABLE WATER SERVICE DOOR CUTOUT CORRODED FORWARD LOWER CORNER AT BS. 915, ABOVE STR. 27R.SDR SWAA2020021941473Skin · corrodedFUSELAGE EXTERNAL SKIN CORRODED AT BS. 889, BL 0. / REPAIRED SKIN IAW ER AND EA.SDR DALA2020021301111Skin · damaged(AIRCRAFT 5649, L/P 1482636) COMPLY WITH DELTA LOGPAGE 1552495 EA 182033 REVISION D IS CURRENT REVISION FOLLOW ON ACTION IS REQUIRED ACCOMPLISH SECTION I INSPECTION AT 23,000 TOTAL FLIGHT CYCLES THEN AT 3,000 FLIGHT INTERVALS THEREAFTER. CORRECTIVE ACTION: ACCSDR DALA2020020901023Skin · damagedFUSELAGE DAMAGE FOUND BELOW C2 CARGO DOOR WHILE LOOKING FOR HYDRAULIC LEAKS. CLEANED AREA FOR ENGINEERING, DAMAGE IS LOCATED ON LAP JOINT OF DOUBLER BELOW C-2 CARGO DOOR BETWEEN STRINGER 30&29R STATION 674 . ENGINEERING NOTIFIED. REMOVED DAMAGE PER PRI ER/A 58SDR DALA2020020901022Skin · damagedFUSELAGE DAMAGE FOUND BELOW C-2 CARGO DOOR WHILE LOOKING FOR HYDRAULIC LEAK FROM A/C LOG 6896790. C/W ERA585163-14 REV ORIG PRI REV 0, ERA585163-14 REV ORIV PRI REV 1 , ERA585163-14 REV ORIG PRI REV 2, ERA585163-14 REV ORIG PRI REV 3, ERA585163-14 REV ORIG PRISDR SWAA2021081081996Doubler · damagedLT TWLU-S-BAND ANTENNA DOUBLER HAS MATERIAL LOSS AND ELONGATED HOLES. / UPON FURTHER INSPECTION OF THE DOUBLER AND FUSELAGE SKIN FOUND ONLY 2 EACH HOLES ELONGATED SLIGHTLY PER SRM 51-10-02. (FWD HOLE AND I/B MIDDLE HOLE) OVERSIZED TO 0.1875' PER SRM 51-40-02. SDR SWIA2020032649403Skin · corroded* CORROSION ON FUSELAGE SKIN BETWEEN APPROXIMATELYFS559+32 AND FS559+64 AND BETWEEN STR 26R AND STR 26L (AREA MARKED). (C-CHECK) RO 3/25/2020 REMOVED CORROSION ON FUSELAGE SKIN APPROX. FS 559+32" AND FS 559+64" AND BETWEEN STR 26R AND STR 26L. REF:L CRJ 20SDR SWIA2020032649359Skin · corroded* CORROSION ON FUSELAGE SKIN BETWEEN APPROXIMATELY FS559+8 AND FS559+32 AND BETWEEN STR 26R AND STR 26L (AREA MARKED). (C-CHECK) RO 3/25/2020 REPAIRED FUSELAGE SKIN BETWEEN APPROXIMATELY FS559+8 AND FS559+32 AND BETWEEN STR 26R AND STR 26L REF BOMBARDIER SDR SWIA2020022748854Doubler · corrodedCORROSION IN L/H O/B DOUBLER BETWEEN FR.87-88. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED CORRODED LH O/B DOUBLER BETWEEN FR87-88 REF SRM. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020022748842Skin · corrodedCORROSION IN FR.84 RBL 27". (C-CHECK) RO 2/22/2020 REMOVED CORROSION AT FR 84 RBL 27" . INSTALLED DOUBLER AND FILLER REF ETD.SDR SWAA2020022641700Skin · corrodedFUSELAGE SKIN UNDER DORSAL FIN CORRODED BETWEEN BS. 927 TO BS. 1016, BETWEEN STR. 3L TO STR. 3R. / REPAIRED SKIN UNDER DORSAL FIN PER ER AND EA.SDR VNAA2020020799902Skin · crackedORIGINAL SDR VNAA2019120511101 12/05/2019 ".300" CRACK FOUND DURING RE INSPECTION OF EA 69-2019-278. THE LOCATION IS FS 1196 BETWEEN STGR 17R AND 18R. FERRY TO
ORF. COMPLIED WITH TEMP REPAIR IAW BOMBARDIER REO 690-53-71-042. PERMANENT REPAIR DUE IN 310 FLIGHTSDR SWAA2020032442638Skin · crackedMOD TYPE: 6 NBR: 28564 REV: POS: DURING SI # 12043-53, FOUND SKIN CRACK INDICATION, BS 540, BELOW STRINGER 22R, / SECOND FASTENER FROM THETOP IN THE AFT ROW. / REPAIRED PER EA.SDR SWIA2020022748859Doubler · corrodedCORROSION FOUND ON FWD LH DOUBLER ON FR 16 AS MARKED (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED FWD LH DOUBLER ON FR 16 REF SRM.SDR SWIA2020022748858Doubler · corrodedCORROSION FOUND ON LH AFT DOUBLER FR 19- FR 20 AS MARKED (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED LH AFT DOUBLER AT FR19-20. REF SRM. SEE CONTINUATION CARD FOR DETAILS.SDR DALA2020021071060Fastener · abnormalSHIP 3707 PROTUDING FASTENER ON EXTERNAL FUSELAGE SKIN ON STA 727I+2" AND S-8LH . CORRECTIVE ACTION: REPLACED THE BLIND FASTENERS WITH SOLID RIVET AS FOLLOWS PER B737-800 SRM 53- 00-01-2R-41 PAR 6 B (3) AND DEFERRED. (1478798).SDR CALA2020020800354Skin · dentedFWD CARGO COMPARTMENT DOOR CUTOUT APROX STA 450 UPPER FWD EDGE HAS DENT REF AAR N/R 99873551 DENT FOUND OUT OFLIMITS PER B737 SRM 53-00-01 AD5 NO DAMAGE PERMITTED AT THE EDGE OF DOOR CUTOUT. ACCOMPLISHED REPAIR AT FWD UPPER CORNER APPROX STA 450 PER B737 SRM SDR CALA2020020800363Skin · corrodedCENTER TANK LOWER SKIN LOWER SURFACE CORRODED AT STA.541 AND RBL 52 APPROX. REF AAR NR 99867509 REMOVED CORROSION AT CTR TANK LWR SKIN SURF. AT STA 541 & RBL 52, FOUND OUT OF LIMITS AS PER B737-7 SRM 51-10-02 & 57-10-01 FIG 101, PERFORMED REPAIR AT AREA AS PERSDR A6WA20200207155Access Panel · crackedPANEL 630BL HAS CHAFFING ON INNER SURFACE. CRACK INDICATIONS NOTED DURING HFEC INSPECTION OF REPAIRED SURFACE. AIRCRAFT REMOVED FROM SERVICE REPAIRED PANEL 630BL IAW AWAC SUPPLEMENT 19-218A.SDR SWAA2020030542164Skin · corrodedCORROSION AROUND LOWER ATC ANTENNA(MOUNT LOCATION) STA 355, COMMON TO FUSELAGE SKIN WL 148, BL 0 CORROSION AT LWR ATC ANT. BS 355 WL 148 BL 0 FOUND TO BE OUT OF LIMITS .5"L X .5"W X .075"D DAMAGE NEXT TO FAST HOLE SRM 53-00-01-1A-5. REPAIRED DAMAGE IASDR SWAA2020022041555Skin · misrepairedTHE AFT ROW OF FASTENERS FOR FUSELAGE SKIN REPAIR LOCATED APPROXIMATELY BS. 1016+16, BETWEEN STR. 13L TO STR. 15L WERE INSTALLED IN THE RADIUS OF THE CHEM MILL POCKETS. (REF ESR 20-01334). / ACCOMPLISHED REPAIR AT FUSELAGE SKIN IAW EA.SDR DALA2020021861220Skin · cracked(AIRCRAFT 7108, L/P 1476890) DURING ACCOMPLISHMENT OF HFEC INSPECTION ON LH UNDERWING LONGERON FUSELAGE SKIN, FOUND CRACK INDICATION AROUND 02 EA FASTENER HOLES AT STA 1024 AND STA 1035, STR37L, APPROX 1.5" IN LENGTH EACH. CORRECTIVE ACTION: AREA REPAIR AND MOSDR DALA2020021861218Skin · damaged(AIRCRAFT 7108, L/P 1476773) LAYOUT FASTENER ON LH SIDE MOD DOUBLER FOUND COUNTERSUNK HOLE APPROX STA998, STR35L FALL ON NEAR MILLING STEP. CORRECTIVE ACTION: COMPLIED WITH 584527-14AD REV 1 AND FINAL ISSUED DELTA ER/A 584527-14AD REV ORIGINAL DATED: 05 FEB 20SDR DALA2020021461146Skin · damaged(AIRCRAFT 7108, L/P 1476795) DURING ACCOMPLISHMENT OF BS B777-53-0087 MOD, DOUBLER PILOT HOLE PICKED UP ON RH FX SKIN AT APPROXI STA 995 BTW 34R - 35R FOUND 03EA. CORRECTIVE ACTION: HOLES SURRENDING SKIN REWORK JOB PERFORMED IAW DELTA PRI 584566-14AD REV 1 ISSSDR DALA2020021461145Skin · damaged(AIRCRAFT 71008, L/P 1476780) DURING ACCOMPLISHMENT OF BSB777-53-0087, LAYOUT FASTENER ON RH SIDE MOD DOUBLER FOUND COUNTERSUNK HOLE APPROXI STA998, STR35R FALL ON NEAR MILLING STEP. CORRECTIVE ACTION: FASTENER HOLE INSTALLED WITH BACB30NX8K* + BACN10YT4CD FASSDR DALA2020021461144Skin · damaged(AIRCRAFT 7108, L/P 1476764) DOUBLER PILOT HOLE PICKED UP ON LH FX SKIN AT APPROXI STA 995 BTW 34L-35L FOUND 03EA HOLES FAIL ON MILLING STEP. CORRECTIVE ACTION: HOLES SURROUNDING SKIN REWORK JOB PERFORMED AS PER DELTA PRI 584527-14AD REV 1 ISSUE DATED : 21 JANSDR DALA2020021061047Skin · corroded(AIRCRAFT 5801, L/P 1476052)CORROSION WAS FOUND ON AROUND HOLES AT SKIN UNDER INTERCOSTAL BTW STA 780+140 - 780+160 FROM S-27R TO S-28R IN REF. NRC 00190. CORRECTIVE ACTION: REPAIRED PER ER/A 584766-14 REV ORIG, SECTION 1.SDR CALA2020020800346Skin · chafedB757-53-3-0586 SUPPORT BRACKET CHAFING INTO AFT FUSELAGE SKIN PA NEL STA 1800 STR 17L REF. ST. ENGINEERING N/R 0086941 CUT DAMAGE SECTION OF FUSELAGE SKIN PANEL (HORZ. STAB FWD CUTOUT FAIRING SKIN) AT STA 1800 STR 17L AND ACCOMPLISHED A CATEGORY "A" PERMANENT SDR SIMA202002065009Skin · damagedEXT. FUSELAGE SKIN HAS AREA OF DAMAGE BETWEEN FS 969.00 AND 985.00 AT STR 27.-C/A-C/W REPAIR IAW ERS-CR-53MR-4025SDR AALA202002069020Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT BS 1895 AND S44L. REPAIRED SKIN PER EA 302821.SDR SIMA20200205003Skin · crackedRH REAR FUSELAGE 1, FR 75 ABOVE STR2R CRACK FOUND AT .500 ABOVE STR 2R.-C/A- REPAIR CARRIED OUT IAW SRM 53-31-01. NEEDED TO STOP FACE CARRIED OUT IAW SRM 51-75-00.SDR SIMA20200205002Skin · crackedREAR FUSELAGE 1, LH SIDE AT FR75, 2 CRACK FOUND 1 IS .500 ABOVE STR 2L AND OTHER .750 BELOW STR 2L-C/A- REPAIRED IAW SRM53-31-01.SDR SWAA2021082623013Skin · corrodedEVAL PEELING PAINT CORROSION AT BS 887 BL 0 WL 159 / REPAIRED DAMAGE AT BS 887 BL 0 ON SKIN IAW ATS ER 20-01674 REV IR AND SWA EA 1-753-36547 IRSDR SWAA2021082623014Skin · corrodedEXTERIOR SKIN HAS PEELING PAINT (CORROSION) AT BS 1016 BL 0 AROUND DRAIN WL 186 / REPAIRED FUSELAGE SKIN AT STA 1016 BL 0 AROUND DRAIN WL 186 IAW EA 1-753-36560 REV IR AND ER 20-01675 REV IR. APPLIED DENT DOT TO AFFECTED AREA IAW SWA MPM 52.03.01.02 PAR. 3.
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