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 DALA2021070603732Skin · dentedSHIP 651 IN REF MON 2349057 DENTS OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00743-DENT ON FUSELAGE SKIN STA 1600-1620, S-14L TO S-15L WAS REPAIRED PER ETI-57-21-319 REV.2 AND ER/A 592561-14 REV. ORIGINAL. (1861204)SDR 2021FA0000193Skin · corrodedCORROSION ON STRINGER AFT UPPER SKIN ASSEMBLY PN: 6912640-15.SDR FDEA202107011633Skin · dentedFUSELAGE LEFT HAND SIDE , SKIN FORWARD OF MAIN CARGO DECK CARGO DOOR FORWARD JAMB AT APPROXIMATELY STA 604.75 LONGERON 24 LEFT AREA HAS A SMALL DENT. EA # 1-5300-T0357118A P4 REQUIRES A PERMANENT REPAIR TO BE CARRIED OUT. FUSELAGE LEFT HAND SIDE , SKIN FORSDR DALA2021070603717Skin · dentedSHIP 651 DENT ON FUSELAGE SKIN BTW STA 1260 TO 1280 AND S-7R (FUS). CORRECTIVE ACTION: SUMMARY OF NRC 00403-DENT ON FUSELAGE SKIN BTW STA 1260 TO 1280 AND S-7R WAS REPAIRED PER ETI-57-21-313 REV.1 AND ER/A 592530-14 REV. ORIGINAL. (1860374)SDR DALA2021070203650Skin Splice · corrodedAFT CARGO INTERNAL SKIN SPLICE CORRODED AT STA 900 BETWEEN STR 30 AND 29LT. SUMMARY SEE NRC 061-0008:5331-2001/005 00304: REPAIRED PER ER/A 592326-14 REV A ASSOCIATED ER/A 00-592326 ADDED FOR AC 9525. (LP #1860302)SDR CALA2021070101009Skin · crackedAFT PIT LT FRAME 61 CRACK INDICATION NOTED IN THE VERTICAL WEB OF THE FRAME AT LT STRINGER 37. INTERIM REPAIR ACCOMPLISHED IAW PART 1 OF ECRA 5341-01251. REAMED THE EFFECTED HOLE IN THE AFT PIT LH FRAME 61 VERTICAL WEB OF THE FRAME AT LH STRINGER 37 TO .190. ASDR SWIA2021091360925Skin · chafed* EXTERNAL FUSELAGE SKIN CHAFED AT APPROX. FS 911.00 STGR 27. (C-CHECK RO 9/8/2021) FOUND CHAFE TO BE OUT OF LIMITS ON EXT FUSELAGE AT APPROX FS911 STGR 27 REF. CRJ-900 SRM, 53-00-01-101-001-A01 AND CRJ-900SRM, 53-51-01-001-003-A02. REMOVED GOUGE AT FS9SDR REXA2021090300685Skin · gougedAT FS 910. AT BL0 FUSELAGE SKIN IS GOUGED FROM AFT WING TO BODY FAIRING AFT ANGLE. "REPAIRED GOUGE ON F.S. 910 LWR FUSELAGE SKIN IAW ENDEAVOR AIR EA# CRJ953-11855, REV IR"SDR SWIA202159595Skin · chafedFORWARD FUSELAGE SKIN CHAFED BETWEEN FRAMS 8/9 AND STRINGERS 21R/22R. (C-CHECK RO 7/16/2021) REPAIRED FORWARD FUSELAGE SKIN CHAFED DAMAGE BETWEEN FRAMS 8/9 AND STRINGERS 21R/22R.BY CUT OUT, FILLER AND DOUBLER FABRICATION REPAIR DOUBLER AND FILLER WEIGHTSDR DALA2021063003587Skin · corrodedSHIP 663 CORROSION ON WASTE PANEL TRAY INNER AND OUTER SKIN BTW STA 700 TO STA 720 BTW S-20R TO S-22R (SETTLEMENT AREA OF WASTE DRAIN VALVE) IN REF NRC 00674. CORRECTIVE ACTION: SUMMARY OF NRC 00847. WASTE PANEL WAS REPAIRED PER ER/A 592467-14 REV. ORG. AND ETSDR SWAA2021073088883Doubler · crackedEXT. POWER RECEPTACLE CUT-OUT FWD EDGE DOUBLER CRACKED ABOVE AND BELOW THE LWR HINGE ; / [01] REMOVED POWER RECEPTACLE ACCESS DOOR #114AR PER B737-700 SRM 53-10-15-2R-5; [02] REMOVED ACCESS PANEL# 114AW AND 114AC FROM NOSE WHEEL WELL PER B737-700 SRM 51-40-02-SDR SWAA2021073088882Bear Strap · crackedCRACK FOUND AT INTERNAL MAIN CABIN BEAR STRAP STA 294.5 JUST BELOW STR 8-R; CRACK LENGTH :2.362' / [01] STRIPPED PAINT AT THE REPAIR AREA OF R-1 UPPER FWD. CORNER; STA. 294.5; S-8R; CUT AND REMOVED DAMAGE PART OF THE BEAR STRAP PER B737-700 SRM 53-10-01-2R-6 PSDR SWAA2021072688969Doubler · crackedEXTERNAL POWER DOOR CUTOUT BARE STRAP ALONG AFT EDGE IS CRACKED AT PREVIOUS REPAIR ; / [01] SRM 53-10-15-2R-4 REPAIR 4 IS APPLICABLE TO THIS A/C; [02] VERIFIED APPLICABILITY OF SRM 53-10-15-2R-4 REPAIR 4. IS APPLICABLE.; [03] REMOVED PREVIOUS -1 REPAIR DOUBLERSDR DALA2021070203622Skin · crackedDURING INSPECTION OF THE EXTERNAL SURFACE OF THE FUSELAGE SKIN MAINTENANCE FOUND CRACKS ON S-14AR BETWEEN FRAMES 1629 -1654 AND S-13AR BETWEEN FRAMES 1654-1678. REPAIRED PER SRM 53-80-01. (LP 1857296)SDR DALA2021070103604Skin · damagedWORKING LOG PG. 6425050, DENT REPAIR. CUT OUT SKIN DAMAGE I.A.W.A321 SRM 53-11-11-300-041 FIG 003 WIP 881490, ACCOMPLISHED HFEC I.A.W. A321 NTM 51-10-08, NO CRACKS QC2070. FER A321 SRM 51-70-20-801 FIG 1 FLAGNOTE 3 EXISTING SKIN IS DETERMINED BY THE MILLED SKISDR DALA2021062903526Skin · dented(LOG 1856614) DURING INSPECTION FOUND 2 DENTS ON FUSELAGE SKIN STA 834 BTW S27 LH AND S26 RH. DENTS ON FUSELAGE SKIN STA 834 BTW S27 LH AND S26 RH WERE REPAIRED PERMANENTLY PER ETI-37-21-378 REV. 7 AND ERA 592459-14.SDR SWAA2021081188555Skin · corrodedCORROSION ON FUSELAGE SKIN AT FASTENER HOLE BEHIND FCB AFT SCUFF PLATE; BS 480 +6; RBL 28; WL 153 (MARKED) ; / [01] REMOVED 1 NUT PLATE AT BS 480 +6; RBL 28; WL 153 TO FOM IAW SRM 51-40-02; [02] REMOVED CORROSION AT FUSELAGE SKIN AT FASTENER HOLE BEHIND FCB AFSDR FDEA202106271609Skin · corrodedCORROSION AT STA.1926-1942 L47-49 BELOW AFT CARGO DOOR. REPAIRED CORROSION AT STA.1926-1942 L47-49 PER EA #T 8-5310-T0362734 TITLED: FUSELAGE - MAINFRAME - SKIN STA 1910-1942, L48 - L44 AFT CARGO DOOR UNDER SCUFF PLATE - CORRSIONSDR SWAA2021080488665Bear Strap · crackedCRACK ON F.S.D. FWD BEAR STRAP; BS 294.5 +4; BETWEEN S-7R AND S-8R; WL 266 (MARKED) ; / [01] REMOVED STUB FRAME REVEAL FOR ACCESS PER SRM 51-40-02-0G-0; [02] ET INSPECTED IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23; NO CRACKS NOTED.<BR><BR>CAL ID ATS1465 N600; [SDR SWAA2021072688515Skin · crackedCRACK INDICATION FOUND ON SKIN OPEN HOLE LOCATED BS 540 RH AND STR 22R ; 2021-269911 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25MAR22; [02] EA 21-153-01821 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q005KZZF.; [03] RASDR DALA2021062903525Skin · dented(LOG 1855733) DURING INSPECTION FOUND 2 DENTS IN FUSEAGE SKIN BETWEEN S-26L - BLO AND STATION 827-847. MAINTENANCE REPAIRED DAMAGE PER ERA 592459-14.SDR SWAA2021072690620Skin · dentedDENT EXTERNAL SKIN LOC AT BS 360 MORE 12 INCH AT STR 19 L AT LOWER FUSELAGE ; 2021-296403 / [01] TOOL USED P/N: NORTEC 600D; S/N2000053402; DUE DATE: 23-APR-22; [02] TOOL USED CALIPER P/N: DIGITAL 150 ; S/N: AE-412604 DUE DATE: 28-MAY-22 AND DENT GAUGE P/N:PGKSDR REXA2021071300491Doubler · corrodedFWD LOWER TCAS ANTENNA DOUBLER CORRODED, BLO, FS 295.00 - FS 310. REMOVED AND REPLACED FWD LWR TCAS ANTENNA DOUBLER FROM FS 295 - FS 310 IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.SDR DALA2021062903517Skin · dentedSHIP 651: DURING HCK AT QRO, WHILE PERFORMING DECAL INSPECTION OF DENTS DOCUMENTED IN LP 0951388, EIGHT DENTS, BETWEEN STA 1300-1340 AND S-28L & S-30, WERE REEVALUATED AND FOUND OUT OF B757-200 SRM 53-00-01. C/W ERA 592359-14. (LP 1854646)SDR CALA2021062800979Skin · corrodedTIOLET EXHAUST VENT HAS COROSION AROUND OPENING. REMOVED VACUUM WASTE VENT NOZZLE ASSY REF 53-70-01-2R-3. REMOVED CORROSION AREA FOUND TO BE OUT OF LIMIT REF SRM 53-00-01-1A-1 AD1. ACCOMPLISHED STEPS 4.A,B, AND D OF SRM 53-70-2R-3 REV. 72 REPAIR 3. AND ECRA 5SDR DALA2023012400529Skin · damagedDURING CCK IN QRO, WHILE PERFORMING STEP 17 OF WORK CARD 2330-01337-1001, ELONGATED HOLES WERE FOUND BEYOND THE ALLOWABLE LIMITS COMMON TO FUSELAGE SKIN, BONDED DOUBLER, STRINGER S-2L, STRINGER S-1 & STRINGER S-2R. MAINTANENCE REPAIRED DAMAGE PER ERA 592449-14SDR SWIA2021081860350Skin · damagedELONGATED HOLE IN FUSELAGE SKIN JUST FWD OF FS333.00 BETWEEN STGR 27 AND STGR 26R FROM REMOVAL OF RIVET SECURING DRAIN DOUBLER. (C-CHECK RO 8/16/2021) UPSIZED HOLE TO 0.225", FABRICATED AND INSTALLED NEW DOUBLER REF REO 670-53-21-2072 REV -A DATED 2021-SDR SWAA2021072687890Skin · crackedCRACK INDICATION FOUND ON OPEN HOLE LOC BS 539 RH AND STR-22R ; 2021-269908 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25MAR22; [02] EA 21-153-01821 HAS BEEN APPROVED; ACTIVATED; AND ADDED AS A SUBTASK TO FAULT TTG8Q005KZZF.; [03] RAISED NEW SDR SWAA2021072687889Skin · crackedCRACK INDICATION FOUND ON OPEN HOLE LOC BS 540 RH AND STR-22R ; 2021-269907 / [01] TOOL USED CALIPER P/N 700-113-10 S/N 0019289 DUE DATE 25MAR22; [02] TOOL USED PN: 25DL PLUS; SN: 071504410; DUE DATE: 20-NOV-21; [03] TOOL USED P/N:NORTEC600D; S/N 60007161486; SDR A6WA202107087816Skin · corrodedCORROSION ON SKIN AT UPPER TCAS ANTENNA AT TWO LOCATIONS BETWEEN FS295 TO FS310. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION AT TWO LOCATIONS ON SKIN AT UPPER TCAS ANTENNA LOCATION FS295 + 4Ï¿½, RH STR 0 + 2Ï¿½, DIMENSION L = 3.00Ï¿½ X W = 2.00Ï¿½ SDR MASA20210625239Skin · dentedFUS FWD LH FS437 AREA NEAR STR 22L IS DENTED|REPAIRED SKIN STA 437 NEAR STR 27L IAW SRM 53-00-01SDR SWIA2021091060835Skin · dentedADM# N750SK-1285 / THERE IS A DENT APPROXIMATELY 15" AFT OF SVC DOOR AS FS 364 AND 17" UP FROM BOTTOM OF SERVICE DOOR AT STRINGER 15R. PLEASE PLOT/MAP AND EVALUATE THE DAMAGE. IF THE DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFSDR CALA2021062500955Skin · dented(B757-06-3-0253) EXTERIOR FUSELAGE L/H SIDE, 3EACH DENTS ON THE FUSELAGE SKIN BTWN BS 740 AND BS 760 AND BTWN STRINGERS S-15L AN D S-17L. REF HAECO GSO NRC #9286611 REPAIR ACCOMPLISHED IAW HAECO REO-G23222 AND ECRA 5331-02232. PG 2, PART 1,ITEM 2 REQUIRES TO SDR CALA2021062500954Skin · damagedB757-06-3-0222, ZONE 100, LOWER HALF FUSELAGE, STA 1605, AFT OF WASTE DRAIN DOOR, SKIN IS DENTED FROM INSIDE HAECO/GSO LOG 9286586, V899290 2EA DENTS AT STA 1605 R/H SIDE AFT OF WASTE DR, GOUGE 0.018 DEEP GOUGE''S NOT ALLOWED. OUT OF LIMITS PER SRM 53-00-01. CSDR SWIA2021082060610Skin · dentedFORWARD FUSELAGE SKIN DENTED FRAME 19 STRINGERS 20L/21L (C-CHECK RO 8/18/2021) / PERFORMED CUTOUT AND DOUBLER REPAIR ON FWD FUSELAGE SKIN AT FR 19 BETWEEN STGR 20L-21L. REF EMB ETD2021-170-020197. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. NO APPRECISDR YENA2021062900408Skin · gougedFLT 6102, BNA-BOS. FUSELAGE / CENTER FUSELAGE I / EXTERNAL SKIN FR23-24 & STGR15L-16L / DENT & GOUGE - PERMANENT REPAIR (EC E21-714-01); CLASSIFIED AS MAJOR REPAIR.SDR SWIA202161434None · corroded*MULTIPLE AREAS OF CORROSION ON EXTERNAL FUSELAGE SKIN, MATING SURFACE FOR PANEL 196DR BETWEEN FS 847.00 €“ 1015.00, STGR 18R - 27 (C-CHECK RO 9/27/2021) REMOVED MULTIPLE AREAS OF CORROSION ON EXTERNAL FUSELAGE SKIN, MATING SURFACE FOR PANEL 196DR BETWSDR SWIA202161433None · corroded*CORROSION ON EXTERNAL FUSELAGE SKIN REPAIR DOUBLERS LOCATED BETWEEN FS 969.00 €“ 1000.00, STGR 26L €“ 26R (C-CHECK RO 9/27/2021) REMOVED CORRODED DOUBLERS AND INSTALLED NEW REPAIR DOUBLERS REF REO 670-53-00-290, REV F, 2019/04/26 , COMPLIED WITH ALLSDR DALA2021062503463Skin · dented(LOG 1849394) DURING INSPECTION FOUND DENT ON FUSELAGE SKIN BETWEEN S-9R AND S-10R AT STATION 540. MAINTENANCE REPAIRED DENT PER ERA 592312-14.SDR DALA2021062503462Skin · damaged(LOG 1849734) DURING INSPECTION FOUND PROTUBERANCE ON EXTERNAL FUSELAGE SKIN BTW S-9RH / S-10RH AND STA 539. EXTERNAL FUSELAGE SKIN BTW S-9RH / S-10RH AND STA 539 WAS REPAIRED PER ETI-37-21-385 REV. 3 AND ERA NO.592312-14.SDR CALA2021062300927Skin · corrodedFWD CGO COMPT SLOPE AREA FR26-FR30 STGR38L-STGR37L INTERNAL SKIN FND CORROSION REF HAECO NON-ROUTINE NO.9439977,ORIGINATED BY EM P V906550,SPEC NO.A3NB-53-3-6105. PERFORMED BY EMP V906550,FWD COMPT SLOPE AREA FR29-FR30 STGR38L- STGR37L INTERNAL SKIN CORROSION SDR IPXA2021062170847Skin · crackedINSPECTION TYPE:N/ADAMAGE TO RIGHT SIDE FUSELAGE SKIN CONSISTING OF A CRACK AT STA 535 L33R APPROX 1"ACCOMPLISH PERMANENT DOUBLER REPAIR PER EO MD11-5330-80168-BSDR SWIA2021091360893Skin · dentedADM# N170PQ-7319. AFT CARGO DOOR FUSELAGE STATION FS 1044.74 TO 1002.26, UPPER RIGHT HAND SIDE OF THE AFT CARGO DOOR 7 1/2 INCHES FROM THE AFT EDGE OF THE CARGO DOOR. IF DAMAGE IS REWORKED, OR WITHIN ACCEPTABLE LIMITS, ELIMINATE EVIDENCE USING STANDARD AIRCRAFSDR SWIA2021091360892Skin · dentedADM# N170PQ-7271. EVALUATE AFT CARGO DOOR,AFT BOTTOM CORNER FS1044.74 TO FS 1002.26 3 24/32"FROM THE AFT EDGE TO THE CENTER OF DENT 5 1/4" FROM BOTTOM TO CENTER OF CIRCULAR DENT. IF DAMAGE IS REWORKED, OR WITHIN ACCEPTABLE LIMITS, ELIMINATE EVIDENCE USING STANSDR SWIA2021091360891Skin · dentedADM# N170PQ-7270. EVALUATE AFT CARGO DOOR,AFT BOTTOM CORNER. FS 1044.74 TO FS 1002.26 4 20/32" FROM THE AFT EDGE TO CENTER OF DENT 6 12/32 " FROM THE BOTTOM AFT EDGE TO CENTER OF CIRCULAR DENT. IF DAMAGE IS REWORKED, OR WITHIN ACCEPTABLE LIMITS, ELIMINATE EVIDSDR SWIA2021081860349Skin · crackedLH FUSELAGE EXTERIOR SKIN HAS CRACK AT APPROXIMATELY FS202 WL79.50 (C-CHECK RO 8/16/2021) REMOVED AND INSTALLED NEW LH FUSELAGE EXTERIOR SKIN PN CC670-33106-1 REF BOMBARDIER DWG CC670-33040 REV G & DWG CC670-32010 REV C AND CRJ 700 SRM 51-42-06-001-001SDR CALA2021062000910Skin · dentedSUPPORT TASK: FUSELAGE EXTERIOR SKIN REPAIR DOUBLER DENTED AND G OUGED BS 604-BS 612, STR 15L-STR 16L. REF HAECO GSO NRC 9284071 . DOUBLER WAS REMOVED AND REPLACED PER ECRA 5330-05310 BY HAECO GSO ON HAECO NON ROUTINE 9284071 AND / ELB DIP # 9757625 HAS BEESDR REXA2021080600531Skin · crackedINBOUND WALK - FUSELAGE SKIN DENT AT FS453 AND BETWEEN STR22L AND STR23 L NEEDS EVALUATED DIDN'T SEE ON "SCRATCH/DENT" LOG. - REPAIRED DAMAGE ON FUSELAGE SKIN IAW EA CRJ953-11755SDR A6WA202107207829Skin · damagedELONGATED FASTENER HOLE AND TOOLING DAMAGE LH AFT FUSELAGE SKIN AT FS559.00 + 64 Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED A REPAIR AT LH AFT FUSELAGE SKIN AT FS559.00 + 64Ï¿½ FS559.00 + 80 AND S17L Ï¿½ S18L. ELONGATSDR FDEA202106181665Skin · corrodedAFT FUSE WASTE TANK COMPT, CORROSION ON INTERIOR OF FUSELAGE SKIN, AT EXISTING EXTERIOR DOUBLER AREA, AT STA 2000 BETWEEEN L-45 AND L-45 R/H. (MARKED #11) REMOVED CORROSION FOUND TO BE WITHIN LIMETS REF SRM 53-20-00 FIG 4 SHT 2 NOTE 16 VOL 1 .
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