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 FDEA202205161223Skin · noneFUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 632/654 AND STG 2/3 RH FUSELAGE SKIN BETWEEN STA 632/654 AND STG 2/3 RH WAS REPAIRED. SRM 53-00-01-2R REV 82 DEC 15,2021SDR FDEA202205161222Skin · noneFUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 220.5 / AND STG 30LH / BL0 FUSELAGE SKIN WITH LIGTINING STRIKE BETWEEN STA 220.5 / AND STGR 30LH WAS REPAIRED IAW E.A # M-5330-T0368423SDR YENA2022051700493Skin · damagedDURING HEAVY MAINTENANCE, PROTUBERANCE EXTERNAL SKIN FR 30-31 STR 26-27; MAJOR REPAIR REF TOMX NR 1894-00330 - EVALUATED AND REPAIRED PROTUBERANCE IAW EMB 190 SRM 53-21-01/AD52, SRM 53-21-01/R62P, 51-75-13 PAR. 5 AND SRM 51-75-00F.SDR YENA2022051700491Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION ON INTERNAL SKIN BTW FR86/FR87 AND STGR 29L/28L; REMOVED CORROSION AND EVALUATED. FOUND OUT OF LIMITS. PER EMB 190 SRM 53-23-01/ADS51. PERFORMED REPAIR PER EC E22-324-01, ETI 190-22-561 REV 6 AND EDT2022-190-015055 REVD. WORSDR SWAA2022060808177Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2022-283950 / [01] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SING OFFS.;[02] REMOVED GUSSET AND FASTESDR SWAA2022060808178Gusset · crackedCRACK GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT 2022-283951 / [01] REMOVED GUSSET AND FASTENER LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 REV:- SEE INDIVIDUAL SING OFFS.;[02] CORRECTED STEP 1 <BR>REMSDR SWAA2022060808179Angle · crackedCRACK ANGLE - CLIP LOCATED BS500C FWD FACE AND STR26L FWD CARGO COMPARTMENT 2022-283956 / [01] REPLACED ANGLE CLIP LOCATED BS500C FWD FACE AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW.;[02]SDR SWAA2022060808180Angle · crackedCRACK ANGLE - CLIP LOCATED BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT 2022-283957 / [01] REPLACED ANGLE-CLIP LOCATED BS400 AFT FACE AND STR26L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM:9 AND DWG:143A7505 SHEET:81 REV:-.;[02] SDR SWAA2022060708294Shield · crackedFWD CARGO COMP. AFT SHIELD BETW. STA 492.4 THRU STA 500A STR 25R RBL 25 HAS .750' CRACK AT LOWER AREA / [01] REPLACED FWD CARGO COMP. AFT SHIELD BETWEEN STA 492.4 THRU STA 500A STR 25R RBL 25 REF. B737-700 SRM 51-40-02-0G-0. SHIELD WILL BE INSTALLED ON FWD CARSDR CALA2022051601255Skin · damagedLIGHTNING STRIKE AT STATION 500A BETWEEN STRINGERS 1 AND 2L LOCATION MARKED AT RADIUS OF CHEM-MILLED DOES NOT MEET MINIMUM DRILLED PER ENGINEER INSTRUCTIONS SEE PIC. INFO ONLY PER ENG LENGTH AWAY REF SRM 53-00-01-2R-38 REPAIR 38. (SECTION 43 ZONE 1) BLENDING WSDR CALA2022051601252Skin · dentedA3NB-53-3-6358, RH FWD LOWER FUSELAGE 1EA DENT TO OUT SIDE BETWE EN FR31-FR32 AND STR28R AND STR29R. DOT #54-46() M ON NR# 0029972. REPETITIVE INSPECTIONS REQUIRED PER SRI 53-21 TH SUBSEQUENT INSPECTIONS EVERY 1700 FC OR 3400 FH WHICH EVER O -11-205-071 AT 4SDR MK1Y20220515002Skin · damagedDURING MAINTENENCE INSPECTION FOUND SEVERAL BLED OUTS ON FUSELAGE SKIN, STA 1458- STA 1544, STR 20L-STR 22L COMMON TOFASTENERS.SDR MK1Y20220515Skin · damagedDURING MAINTENENCE INSPECTION FOUND SEVERAL BLEED OUTS ON FUSELAGE SKIN, STA 434 - STA 544, STR 36R.SDR SWAA2022060907878Shield · crackedFWD CARGO BAY FWD SHIELD CRACKED AT FASTENER HOLE BS 420 - BS 440 RBL 23 WL 156 / [01] LOCATED AND DRILLED NEW SHIELD 143A8126U21 IAW SRM 51-40-05-0G-0 AND DWG 143A0080; ID:0019; REV:-;[02] VERIFIED NEW SHIELD 143A8126U21 IAW SRM 51-40-05-0G-0 AND DWG 143A0080SDR DALA2022051603338None · noneCORROSION ON DOUBLER STA Y=1053 IN FRONT BULKHEAD LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00210: CORROSION LEVEL 2, DOUBLER STA Y=1053 IN FRONT BULKHEAD LONG 30 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 DWG 5910130-61 REV. ET AND SRM 51-41-05-0G.SDR SWAA2022053107529Stiffener · crackedCRACK ON STIFFENER LOCATED ON FWD FACE OF VAPOR BARRIER LH BS663 BTW LBL 5.00 TO LBL 32 2022-239636 / [01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N:A16165044; DUE DATE: 01/FEB/23.;[02] REPLACED NEW STIFFENER AND FASTENERS LOCATED ON FWD FACE OF VAPOR BARRSDR SWAA2022053107530Shield · corrodedCORROSION ON SHIELD LOCATED ON FWD CARGO COMPARTMENT BTW BS 492 TO BS 500A AND AT LEVEL OF RBL 21.8 2022-239648 / [01] REPLACED SHIELD AND FASTENERS LOCATED ON FWD CARGO COMPARTMENT BTW BS 492 TO BS 500A AND AT LEVEL OF RBL 21.8 I.A.W B737-700 SRM 51-40-02 ANDSDR DALA2022051703383Skin · dentedSHIP 671 ER/A 599012-14; FUSELAGE / SKIN / STA. 1500 TO 1503 BETWEEN S29L TO S30 / DENTS. CORRECTIVE ACTION: REF ERA 599012-14. (2234637)SDR DALA2022051703382Skin · corrodedSHIP 671 DTE, ER/A 599124-14; FUSELAGE / SKIN / STA. 455 TO 470 BETWEEN S27L TO S27R / CORROSION. CORRECTIVE ACTION: REF ERA 599124-14. (2234183)SDR DALA2022051703380Access Door · corrodedSHIP 671 CORROSION ON E&E ACCESS DOOR CUT OUT AT LOWER FUSELAJE (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00065: CORROSION ON E&E ACCESS DOOR CUT OUT AT LOWER FUSELAJE WAS REPAIRED PER ER/A 599124-14 REV. ORIGINAL SECTION I (PERMANENT REPAIR). (2234779)SDR SWAA2022061607585Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 RBL25. / [01] VERIFIED APPLICABILITY PER SRM NOT ALLOWABLE DAMAGE PART THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CSDR SWAA2022061607586Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE RBL25. / [01] VERIFIED APPLICABILITY PER SRM NOT ALLOWABLE DAMAGE PART DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9C.;[02] REMOVED INTERCOSTAL ATTACH ANGSDR SWAA2022061607587Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25. / [01] DAMAGE FOUND AT FWD CARGO BAY INTERCOSTAL ATTACH ANGLE BS 500C FWD SIDE LBL25 FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PART WILL BE REPAIRED BY REPLACMENT IAW SRM 51-10-02-0SDR SWAA2022060707293Gusset · crackedFWD CARGO SIDEWALL GUSSET ANGLE AT S-19R AND STA 500 CRACKED / [01] REMOVED FWD CARGO SIDEWALL GUSSET ANGLE AT S-19R AND STA 500D AS REF SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET P/N 143A9481-5 PER B737-700 SRM 51-10-02-0G-0;[03] VERIFIED DRILLING.SDR DALA2022052503632None · noneSHIP 675 ERA 502438-14 DENT WAS FOUND ON FUSELAGE SKIN PANEL OF SKIN INSTALLATION LOCATED NEAR STA 1661 BETWEEN S-21L AND S-22L. CORRECTIVE ACTION: REF ERA 502438-14 REV B.SDR CALA2022051301222Skin · crackedJET BRIDGE HIT LEFT SIDE OF FUSELAGE APPROX 2 FEET AFT OF L1 DOOR C/W HFEC INSP PER STEPS 6, 7, 8, AND 9. NO DEFECTS NOTED. OK TO MAKE .040 INSURANCE CUT. AVO9722. COMPLIED WITH STEP 1-5 REPAIR INSTRUCTIONS REF AVO9722. NEED PERFORMED INSURANCE CUT REF AVO9722SDR VNAA202206269999Skin · corrodedCORROSION ON DRAIN HOLES AT FUSELAGE EXTERNAL SKIN BTW FS939.00/953.00 AND STGR 26LH/RH.SDR VNAA202206259991Skin Panel · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS BETWEEN STGR 16R-STGR 24R AND FS 1000.00-FS 1108.00SDR SWAA2022060306569Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT CUT OUT 2022-262271 / [01] TOOL USED: DIGITAL CALIPER P/N:500-197-30; S/N:A18229508; DUE DATE: 29/SEP/22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SDR DALA2022051603359Repair · installedSHIP 651 DAMAGE TOLERANCE ANALYSIS REQUIRED. REF LOGPAGE 1812010. ER/A 591111-14 SECTION I ISSUED FOR FUSELAGE SKIN REPAIR AT BS 200, RBL 12 -22. CURRENT ER/A REVISION IS 'A'. CORRECTIVE ACTION: REF ERA 591111-14 REV A. (2231907)SDR IPXA2022051181992Shear Plate · corrodedINSPECTION TYPE:SEG4SURFACE CORROSION FOUND AT AFT DECK PLATE STA 1692, LBL 20.5REMOVED CORROSION AND CHECK LIMITS PER SRM 53-60-51-1A. IN LIMITS AFTER REWORK. NDT PERFORMED HFEC SURFACE INSPECTION AND ROTO INSPECTION ON AFFECTED AREA. NO REJECTABLE INDICATIONSDR IPXA2022051181991Shear Plate · corrodedINSPECTION TYPE:SEG4SURFACE CORROSION FOUND AT AFT DECK PLATE STA 1680, RBL 18.5REMOVED CORROSION AND CHECK LIMITS PER SRM 53-60-51-1A. IN LIMITS AFTER REWORK. NDT PERFORMED HFEC SURFACE INSPECTION AND ROTO INSPECTION ON AFFECTED AREA. NO REJECTABLE INDICATIONSDR SWAA2022060706267Cap · crackedAFT CARGO COMP. RT SIDE CAPSTRIP BETWEEN STA 727D THRU STA 807 RBL 25 WITH 1' CRACK / [01] REPLACED AFT CARGO COMP. RT SIDE BETW. STA 727D THRU 807 CAPSTRIP REF. B737-700 AMM 25-52-10-400-801. THIS CAPSTRIP WILL BE INSTALLED ON AFT CARGO COMP. MOC CARD #TTG8Q0SDR WX0A1900010074086None · noneRH MLG DOOR ACTUATOR FITTING, AFT SIDE PLAIN BUSH MIGRATED OUT OF FITTING./INSTALLED 1 EA STRAIGHT BUSHING AS REQUIRED IAW ERO R5336-0015. / WITH REFERANCE TO SRM 51-72-12-911-002."SDR AALA202205105743Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN BETWEEN FR 63 AND FR 64 AND BETWEEN S41R AND S42R. REPAIRED SKIN PER EA 335693.SDR DALA2022051003227Doubler · corrodedCORROSION ON DOUBLERS ON FWD AND AFT CUT OUT AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00016: CORROSION LEVEL 2, DOUBLERS ON FWD AND AFT CUT OUT AT FWD CARGO COMPARMENT WERE REPLACED PER B717 SRM 53- 20-15-2R-6 FIG. 201. (LP #2229744)SDR R61A 202206040078Doubler · corrodedMAJOR REPAIR ON CORRODED CFIII LWR SKIN INNER DOUBLER AT WASTE ACCESS DOOR CUT-OUT BTWN FR 88-89 BTWN STR 25-27 RH. REPAIRED IAW EMB 170/175 SRM 53-23-60 REV. 01.SDR R61A2022060300371Skin Panel · corrodedCFIII LWR SKIN PNL WASTE WATER DOOR BTWN FR 86-88 CORRODED. R&R IAW EMB 175 AMM 53-03-60 / 400.SDR ASAA2022050938238Doubler · corrodedCORROSION NOTED ON EXTERNAL FWD ATG4 ANTENNA DOUBLER SKIN APPROXIMATELY BL 0., STA 500B - 500C. GROUNDED - YES. REPAIRED DOUBLER PER ASA EA 900-53EA-24372 REV 00 DATED 05/07/2022.SDR ASAA2022050938237Skin · corrodedCORROSION NOTED ON EXTERNAL SKIN APPROXIMATELY BL 0, STA 500B - 500C. GROUNDED - YES. REPAIRED PER ASA EA 900-53EA-24372 REV 00 DATED 05/07/2022.SDR VNAA202206269996Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN AT SETTLEMENT AREA OF WING-TO-FUSELAGE FAIRING BTW FS STA 847.00 TO FS STA 1015.00.SDR CALA2022050901180None · corrodedMAIN CABIN BETWEEN FR69-70 STRINGER 23L SHEAR PLATE HAS SPOTS OF CORROSION ON UPPER SURFACE. GENERATED BY V919150 PER HAECO LCQ NR 9292781/44781. REMOVED AND REPLACED SHEAR PLATE AT FR69-70 STR. 23L IAW A319 SR M 51-72-11, SRM 51-11-12 AND SRM 51-42-11. MECH VSDR SWAA2022051005343Skin · crackedFUSELAGE HAS 5.0IN SKIN CRACK AT BS520 +11IN AT STR 4R. / [01] VERIFIED CRACK USING THE FOLLOWING METHODS<BR>ULTRASONIC PHASED ARRAY (UTPA) PER 737 NDT MANUAL; PART 4; 53-30-07<BR>MEDIUM FREQUENCY EDDY CURRENT (MFEC) INSPECTION PER 737 NDT MANUAL; PART 6; 53-3SDR FDEA202205061136Skin · crackedCABIN - R3 DOOR CUT OUT AFT JAMB BETWEEN STATION 1305.25 AND STATION 1315.42 UPPER EDGE SKIN FOUND WITH CRACK. CABIN - R3 DOOR CUTOUT AFT JAMB BETWEEN STATION 1305.25 AND STATION 1315.42 , CRACKED UPPER EDGE SKIN REPAIRED AS PER E.A.#: 1-5310-T0368568 P1. SDR SWAA2022060305176Angle · crackedCRACK ANGLE LOCATED BS 500B FWD SIDE STR 26L FWD CARGO COMPARTMENT 2022-262252 / [01] REPLACED ANGLE LOCATED BS 500B FWD SIDE STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A7505 SHEET 5 REV B; AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFSSDR SWAA2022060305177Angle · crackedCRACK ANGLE LOCATED BS 500C FWD SIDE STR 26L FWD CARGO COMPARTMENT 2022-262251 / [01] REPLACED ANGLE LOCATED BS 500C FWD SIDE STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A7505 SHEET 9 REV A; AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFSSDR SWAA2022060305178Angle · crackedCRACK ANGLE LOCATED BS 500C AFT SIDE STR 26L FWD CARGO COMPARTMENT 2022-262250 / [01] REPLACED ANGLE LOCATED BS 500C AFT SIDE STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A7505 SHEET 5 REV B; AND SRM 51-40-02; SEE INDIVIDUAL SIGN OFFSSDR SWAA2022051204964Bear Strap · crackedCRACK INDICATIONS FOUND ON BEARSTRAP 1 EA FASTENER HOLE LOCATED AT BS 291.5 PLUS 10 INCHES AND 4.5 INCHES ABOVE STR 8R CRACKS DIRECTIONS ARE 1 AND 7. O CLOCK. REFER TO FAULT TTG8Q00BVSVZ WHERE EA 22-153-01280 WAS ADDED AS A SUBTASK.SDR DALA2022050903207None · noneSHIP 3223 CRACK EXTERNAL SKIN LOCATED BTW FR28 TO FR29 AND BTW STR43R TO STR44 AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 598647-14AD REV. ORIGINAL. (2225506)SDR CALA2022050901168None · corrodedMAIN CABIN BETWEEN FR69-70 STRINGER 23R SHEAR PLATE HAS SPOTS OF CORROSION ON UPPER SURFACE. GENERATED BY V919150 PER HAECO LCQ NR 9292782/44782 REMOVED AND REPLACED SHEAR PLATE ON STRINGER 23R AT FR69-70 IAW UAL A319 SRM 51-42-11-001-A. ACMP BY MECH V061616 I
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