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 UIEA2022101001113Skin · out of limitsFWD CARGO DOOR CUTOUT INTERIOR SKIN, MATERIAL LOSS AT EDGE OF SKIN, 4.0" UP FROM FWD LOWER CORNER (DAMAGE ON EDGE OF FWD CARGO DOOR, LOWER FWD ORNER IN AREA OF .9"L X .150"W X .110"D FOUND OUT OF LIMITS DUE TO BEING WITHIN 3.0" OF DOOR CUTOUT PER SRM 53-00-01-SDR UIEA2022101101116Skin · corroded***CORROSION***EXTERNAL SKIN LOWER EDGE OF AFT CARGO DOOR CUTOUT, STA. 807+2 - STA. 807+5 (CORROSION FOUND IN AREA 3.0"L X 1.0"W X .002"D @STA. 807+2 - STA. 807+5 @ EDGE OF AFT CARGO DOOR CUTOUT. FOUND OUT OF LIMITS PER SRM 53-00-01-1A-1 #4.B.(2)(A) DET. Q. RSDR UIEA2022101101118Skin · gougedFOUND 2 EA. GOUGES IN EXTERIOR FUELAGE SKIN @STA. 792+2 TO 792+4@AFT CARGO DOOR LOWER CUTOUT(<P>FOUND 2 EA. GOUGES IN EXTERIOR FUSELAGE SKIN @STA. 792+2 TO STA. 792+4 WITHIN 3.0" OF AFT CARGO DOOR LOWER CUTOUT OUT OF LIMITS PER SRM 53-00-01-1A-1, #4.B.(2)(A), SDR UIEA2022101101119Skin · gougedFOUND 4 EA. GOUGES IN EXTERIOR FUSELAGE SKIN @STA. 792+10 TO 807+4(<P>FOUND 4EA. GOUGES IN EXTERIOR SKIN @STA. 792+10 TO STA. 807+4 WITHIN 3.0" OF AFT CARGO DOOR LOWER CUTOUT OUT OF LIMITS PER SRM 53-00-01-1A-1 #4.B.(2)(A), DETAIL Q. REPAIRED EXTERIOR FUSELAGESDR UIEA2022101201122Skin · gougedFOUND 4 EA. GOUGES IN EXTERIOR FUSELAGE SKIN @STA. 807+11 TO 827 @AFT CARGO DOOR CUTOUT(<P>FOUND 4 EA. GOUGES IN EXTERIOR FUSELAGE SKIN @STA. 807+11 TO STA. 827 WITHIN 3.0" OF AFT CARGO DOOR LOWER CUTOUT OUT OF LIMITS PER SRM 53-00-01-1A-1, #4.B.(2)(A) DETAIL SDR UIEA2022101201123Skin · gougedFOUND 3 EA. GOUGES IN EXTERIOR FUSELAGE SKIN @STA. 827+8 TO 827+17 @AFT CARGO DOOR LOWER CUTOUT (FOUND 3 EA. GOUGES IN EXTERIOR FUSELAGE SKIN @STA. 827+8 TO STA. 827+17 WITHIN 3.0" OF AFT CARGO DOOR CUTOUT OUT OF LIMITS PER SRM 53-00-01-1A-1, #4.B.(2)(A) DETAISDR JJBA20221026018Skin · corrodedREAR FUSE I, RH SILL BTW FRAME 61-65 CORRODED. RH SILL BTW FR61-65 CORROSION BLENDED AND FOUND OUT OF LIMIT. RH SILL BTW FR 61-65 REPLACED. IN ADDITION MIS DRILLED HOLE AT FR 63 REPAIRED.SDR ABXA20221025119Skin · crackedDURING LINE MAINTENANCE IN CVG A CRACK WAS FOUND BETWEEN STA 698 AND 720 BETWEEN S35 – S36R. MAINTENANCE GROUNDED AIRCRAFT. REPAIRED SKIN IAW B767 SRM 53-00-01-2R-12. AICRAFT RETURNED TO SERVICE.SDR DALA2022102106836Skin · handler errorSHIP 663 GROUND CREW LOWERED STAIRS WHILE STILL UP AGAIST A/C CAUSING A GOUGE 19 INCHES AFT OF 2L DOOR. CORRECTIVE ACTION: C/W INSP AND BLEND STEPS 1 AND 2 PER ERA 603152-14. SECTION 1. PREFORMED HFEC INSPECTION OF BLENDED AREA PER ERA 603152-14 SECTION 1 STEPSDR SWAA2022111761391Gusset · crackedFWD CARGO BAY GUSSET CRACKED AT BS 500D STR 19L / [01] PRIOR TO REMOVAL ;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 STEP 9.;[02] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLSDR SWAA2022111761394Gusset · crackedFORWARD CARGO BAY GUSSET CRACKED AT BS 500D STR 19R / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 STEP 9.;[02] REMOVED GUSSET CRACKED AT BS500D;STR. 19R;IAW SRM 51-40-02.;[03] RECEIVED;LOCATESDR FDEA202210182587Skin Splice · crackedRADIOGRAPHY INSPECTION CARRY OUT ON TRANSVERSE SKIN SPLICE AT STATION 6-100 AND FOUND 01 EACH CRACK INDICATION APPROXIMATE 1 INCH IN LENGTH AT RIGHT HAND LONGERON 4 RIGHT FORWARD CENTER SPLICE BETWEEN FASTENER 1 AND 2. CRACKED SPLICE AT STATION 6-100 AT RISDR DALA2022102006792Skin · dentedSHIP 655 DENTS 2(EA) ON FUSELAGE SKIN BETWEEN S-17R/S -18R AND STA 1660/ STA 1680. CORRECTIVE ACTION: SUMMARY OF NRC 00049- DENTS 2(EA) ON FUSELAGE SKIN BETWEEN S-17R /S-18R AND STA 1660/ STA1680 WAS REPAIRED PER ER/A 602842-14 REV . ORIGINAL SECTION 1 PRI 602SDR DALA2022102006791Skin · dentedSHIP 655 DENT ON EXTERNAL AFT FUSELAGE, STA. 1936, BTW S-1 AND S-2L. CORRECTIVE ACTION: SUMMARY OF NRC 00016- DENT ON EXTERNAL AFT FUSELAGE, STA. 1936, BTW S-1 AND S-2L WAS REPAIRED PER ER/A 602913-14 REV. ORIGINAL SECTION 1 PRI 602913-14 REV. 0. (2457882)SDR DALA2022102106828Doubler · corrodedSHIP 5805 CORROSION ON INTERNAL PRODUCTION DOUBLER AT AFT LAVATORIES SERVICE PANEL STA 1546 APPROX BTW S-28 RH & S- 28RH, UNDER WASTE SYSTEM ENCLOSURE. C2. CORRECTIVE ACTION: SUMMARY OF NRC 00183: INTERNAL PRODUCTION DOUBLER WAS REPLACED PER PRI 602868-14 REV.SDR DALA2022102106823Doubler · corrodedSHIP 5805 CORROSION ON EXTERNAL SKIN DOUBLERS BTW STA 1540-1560 BTW STRINGER 27RH-29RH IN REF NRC 00179. CORRECTIVE ACTION: SUMMARY OF NRC 00280: EXTERNAL SKIN DOUBLERS BTW STA 1540-1560 BTW STRINGER 27RH-29RH WAS REPLACED WERE REPLACED PER PRI 545850-14 REV. SDR IPXA2022101987251Floor Support · crackedINSPECTION TYPE:CMDC FLOOR LEVEL ARMWEB CRACKED BETWEEN FR38.1 AND FR38.2REMOVED AND REPLACED FLOOR SUPPORT IAW-SRM 51-40-21.SDR N6WA2022112501Skin · crackedFWD ELECTRICAL BAY RH SKIN CRACKED BY AFT DOOR LATCH CUTOUT. FWD ELECTRICAL BAY RH SKIN CRACKED BY AFT DOOR LATCH CUTOUT.SDR VNAA202211209991Skin Panel · nickedNICKS ON FWD CARGO CUT OUT SURROUND SKIN (FWD, REAR & UPPER FRAMES).SDR IPXA2022103187691Skin · gougedINSPECTION TYPE:1CFWD CARGO DOOR AFT LWR SILL AREA EXISTING REPAIR HAS A GOUGE.REPAIRED FWD CARGO DOOR AFT LWR SILL AREA EXISTING REPAIR IAW VT-SAA EA 011-5330-01-A9740 REV I/R AND UPS EO MD11-5330-85131-A DATED 10/28/2022 (MINOR)SDR JJBA20221026021Skin · crackedCRACK SUSPECTED (5X) ON LH SKIN AROUND FASTENERS BTW FR77-80 BTW STR 3L-9L. SKIN REPAIRED WITH 5 BUSHINGS REPAIR.SDR SWAA2022101860669Skin · crackedREPAIR EA - 22-153-03096(N465WN - - REPAIR - EXTERNAL GROUND POWER RECEPTACLE (EGPR) DOOR CUTOUT DAMAGE/CRACK - PERMANENT) / [01] PERFORMED REPAIR IAW EA 22-153-030096 AND WO TTG8Q00FHNJL.SDR DALA2022102006789Skin · dentedSHIP 655 DENT ON EXTERNAL FUSELAGE SKIN, STA. 394, BTW S-3R AND S-4R. CORRECTIVE ACTION: SUMMARY OF NRC 00027- DENT ON EXTERNAL FUSELAGE SKIN, STA. 394, BTW S-3R AND S-4R WAS REPAIRED PER ER/A602587-14 REV. ORIGINAL SECTION 1 PERMANENT REPAIR PRI 602587-14 REVSDR DALA2022102006788Skin · wornSHIP 655 WEAR ON FUSELAGE SKIN APROX AT S-13R BETWEEN STA 1844 AND STA 1885.20. CORRECTIVE ACTION: SUMMARY OF NRC 00451- FUSELAGE SKIN APROX AT S-13R BETWEEN STA 1844 AND STA 1885.20 WAS REPAIRED PER B757-200 SRM. (2456655)SDR DALA2022101806723None · noneSHIP 195 -HFEC SURFACE INSPECTION FOUND 01EA CRACK APPROX.0.200 INCH IN LENGTH ON THE LH FUSELAGE SKIN ABOVE THE 11TH STRINGER-ATTACH RIVET AT STR S-13AL, CORRECTIVE ACTION: DAMAGE DOUBLE REPAIRED AS PER B767-300 SRM 53-80. REPEAT INSPECTIONS INTERVAL 7500 FLISDR HNAA2022102500274Skin · crackedE937122 - THERE IS A POSSIBLE SKIN CRACK AT A RIVET, AT FR78, STGR 6R-5R .... ACCOMPLISHED REPAIR OF SKIN CRACK AT A RIVET BY CUT OUT AND INSTALLATION OF BUSHING AT FR78, STGR 6R-5R IAW EO1-53-22-0211.SDR R61A2022102000643Skin Panel · gougedDAMAGE TO CENTER FUSELAGE III SKIN PANEL DUE TO BELT LOADER STRIKE AT FRA 85-86 AND STR 28L-29L. REPAIRED IAW ETD2022-170-031686. REF VP-045103-2022 N/R 1,10,11,12,13 FOR REPAIR ALSO.SDR FDEA202210152573Skin · crackedRADIOGRAPHY INSPECTION CARRIED OUT ON TRANSVERSE SKIN SPLICE AT STATION 6-100 AND FOUND 01 EACH CRACK INDICATION AT FORWARD SIDE OF STRINGER 7 LEFT CENTER SPLICE, PROPAGATE FROM SECOND FASTENER FROM CENTER APPROXIMATELY 0.5 INCHES LENGTH. MAIN DECK CARGSDR IXXA2022101501Panel · corrodedPANEL 195QL CORRODEDSDR DALA2023110409094Unknown · unknownAIRCRAFT 3830, FUSELAGE SKIN BETWEEN 727J-727K & STR 2L-3L DENTED. THE REPORTED DIMENSIONS OF DENT 1 ARE 1.00 X 0.3 X 0.018, W/Y = 17, AND DENT 2 ARE 1.125 X 0.4 X 0.038, W/Y = 10.5. THE SUBJECT DAMAGE IS OUTSIDE OF THE ALLOWABLE LIMITS PER B737-900ER SRM 53-0SDR SWAA2022112260104Skin · delaminatedDELAMINATED EXTERNAL SKIN RIGHT LOWER SIDE LOCATED AT 4.5IN BELOW ACCESS DOOR CUTOUT AND 8.5IN FROM FWD EDGE AT TAIL CONE. REPAIRED EXTERNAL SKIN RIGHT LOWER SIDE LOCATED AT 4.5IN BELOW ACCESS DOOR CUTOUT AND 8.5IN FROM FWD EDGE AT TAIL CONE IAW SRM 53-80-70-SDR SWAA2022111659748Bear Strap · cracked0.300' CRACK EXTENDING FWD OF FASTENER ON R1 BEAR STRAP INTERIOR SIDE . REMOVED RAIN GUTTERS (2EA) FROM REPAIR AREA IAW SRM 51-40-02-0G-0. FABRICATED TAPERED SHIM IAW EA 21-153-03542 STEP 10 FIG.1. COMPLETED FABRICATION OF REPAIR IAW EA 21-153-03542 STEPSDR CALA2022101802826Stringer · corrodedBULK CARGO STRINGER 41L BET FR63-64 IS CORRODED. REMOVED AND REPLACED STRG 41L IAW A320 SRM 51-42-11/001, RECEIVE D NEW STRG 41L P/N=D5347041821600 B/N:0003899727. EMP# V936039 W ORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM ON NR# 38657.SDR DALA2022101706690None · noneSHIP 5805 WEAR ON EXTERNAL FUSELAGE SKIN BTW STA 1180+ 100-1180+120 STRG-1 ( AFT SETTLEMENT AREA OF SATELLITE TV ANTENNA RADOME). CORRECTIVE ACTION: SUMMARY OF NRC 00193: WEARS ON EXTERNAL FUSELAGE SKIN BTW STA 1180+100-1180+120 STRG-1 WERE BLENDED OUT PER B75SDR IPXA2022101487137Skin · dentedINSPECTION TYPE:SEG1FUSELAGE SKIN AT STA 434 BETWEEN S23L AND 25L HAS 2 DENTS DENT 1 IS L-1.0" W=1.030" DEPTH=.046" AND DENT 2 L=.632" W=.621" AND DEPTH=.048" MAKING THE SKIN OUT OF LIMITS PER SRM 53-00-01-1A-1 DET 3.REPAIRED SKIN PER EA# B757-5310-27-A3062 PRSDR DALA2023101608486Unknown · unknownSHIP 5805 DTE - 602903-14 - ERA A WORN AREA WAS FOUND ON THE FUSELAGE SKIN AT STA 1180+104 AND S-1. CORRECTIVE ACTION: REF ERA 602903-14 REV A. (2450512)SDR SWAA2022111759815Attach Angle · crackedCRACK ON FWD CARGO BAY FRAME TO BAFFLE ATTACH ANGLE AT LBL 24 BS 500B+19. / [01] REMOVED INTERCOSTAL FROM FCB BS 500B-500C LBL 24 IAW SRM 51-40-02-0G-0;[02] RECIVED; LOCATED AND DRILLED NEW ATTACH ANGLE AT BS 500B+19 LBL24; IAW B 737-700 SRM 51-40-05-0G-0 DWG SDR SWAA2022111759827Attach Angle · crackedCRACK ON FWD CARGO BAY FRAME TO BAFFLE ATTACH ANGLE AT LBL 24 BS 500C+1. / [01] REMOVED INTERCOSTAL FROM FCB BS 500C-500D LBL 24 IAW SRM 51-40-02-0G-0;[02] RECIVED; LOCATED AND DRILLED NEW ATTACH ANGLE<BR>N/P 143A7502-5 <BR>AT LBL 24 BS 500C+1 IAW SRM 51-40-05SDR SWAA2022111759814Attach Angle · crackedCRACK ON FWD CARGO BAY FRAME TO BAFFLE ATTACH ANGLE AT LBL 24 BS 400+19. / [01] REMOVED ATTACH ANGLE FROM FCB BS 400+19 LBL 24 IAW SRM 51-40-02-0G-0;[02] RECIVED; LOCATED AND DRILLED NEW ATTACH ANGLE AT BS 400+19 LBL24; IAW B 737-700 SRM 51-40-05-0G-0 DWG 134ASDR HNAA2022102500294Skin · corrodedE938783 - INTERIOR PAX, THE SKIN AT THE BASE OF THE AFT HEATED NIPPLE HAS CORROSION. SSI 53-20-07 .... ACCOMPLISHED REPAIR OF CORROSION ON INTERNAL FUSELAGE SKIN AROUND HEATED NIPPLES BTW FR 57-58 IAW EO1-53-22-0210 AND ETD# ETD2022-145-030530. SEE NRTC# E9383SDR HNAA2022102500282Skin · corrodedE938371 - SSI 53-20-27 INTERIOR PAX, THE SKIN AT THE BASE OF THE FWD HEATED NIPPLE HAS CORROSION .... ACCOMPLISHED REPAIR OF CORROSION ON INTERNAL FUSELAGE SKIN AROUND HEATED NIPPLES BTW FR 57-58 IAW EO1-53-22-0210 AND ETD# ETD2022-145-030530.SDR SWAA2022110758628Seal · chafedLT HORIZONTAL STAB FWD SLIDE SEAL FWD TRACK IS CHAFFED / [01] REMOVED L/H HORIZONTAL STAB FWD LOWER SLIDE SEAL FOR ACCESS PER AMM 53-31-31-000-803 STEPS 4. E. (1)-(4).;[02] REMOVED SKIN PANEL FWD OF L/H HORIZONTAL STAB FWD SLIDE SEAL TRACK FOR ACCESS PER AMM 2SDR SWAA2022110359298Scuff Plate · crackedCRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-576747 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189362;DUE DATE:03-DEC-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND SDR DALA2022101406638None · none(LOG 2448667) DURING INSPECTION FOUND DENT AT FS 847-857 AND STR 22R-23R. REPAIRED IT PER B737-900ER SRM 53-00-01, REPAIR 23.SDR DALA2023061304810Unknown · unknown(LOG 2447032) DURING THE HEAVY MAINTENANCE CHECK/ENTRY INTO SERVICE AT FLIGHTSTAR (VQQ), WHILE ACCOMPLISHING INSPECTIONS PER SECTION I OF ER/A, A DENT WAS FOUND COMMON TO THE EXISTING REPAIR LOCATED BETWEEN STA-727K AND STA-727L AT S-23R LEVEL. ADDITIONALLY, SSDR DALA2022121308039Plate · cracked(LOG 2447590) DURING INSPECTION FOUND FUSELAGE SKIN FR 727E - 727F/ S-2R - S-3R WIFI DEMOD GROUND PLATE CRACKED. DAMAGE REPAIRED PER ERA 602901-14.SDR SWAA2022110758741Seal · crackedR/H HORIZONTAL STAB. AFT UPPER SLIDING SEAL FWD TRACK CRACKED / [01] R&R'D TRACK PER SOPM 20-50-01;[02] VERIFIED C/A #1.SDR FDEA202210112538Doubler · crackedREFERENCE TO SNRM #N01411 - UPON REMOVAL OF DOUBLER NCA 6244-3 FOUND INNER WEB DOUBLER NCA 6244-85 CRACKED (01 EACH OF APPROXIMATELY 0.5" LENGTH). FUSELAGE - MAIN FRAME AT STATION 595 CRACKED WEB DOUBLER NCA 6244-85 CARRIED OUT REPAIR IN ACCORDANCE WITH EASDR SWAA2022103158317Shield · corrodedAFT CARGO BAY SHIELD FWD OF THE DOOR HAS CORROSION AT NUT PLATE HOLE BS767+4 RBL22 WL156 / [01] UPDATED MEASUREMENT TABLE FOR PICTURE OF CORROSION ATTACHED;[02] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[03] AMT ISDR SWAA2022103158318Plate · corrodedAFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION COMMON TO NUT PLATE HOLE BS767+3 LBL22 WL156 / [01] UPDATED MEASUREMENT TABLE FOR PICTURE OF CORROSION ATTACHED;[04] REMOVED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT AT BS 727E+10' TO 847 LBL2
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