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 DALA2022042702974None · noneSHIP 668 AMOC REQUIRED (AD 2019-07-04) - TRACKING - ER/A 590828-14AD REV A. CORRECTIVE ACTION: REF ERA 590828-14AD. (1803464)SDR SWIA2021070959345Doubler · corrodedCORROSION ON TCAS OMNIDIRECTIONAL ANTENNA DOUBLER BETWEEN FS295 & FS310 AND BETWEEN STGR26L & SGTR26R (C-CHECK RO 7/7/2021) REPLACED TCAS ANTENNA DOUBLER BETWEEN FS 295.00 AND FS310.00 BETWEEN STRINGERS26L AND 26R AS PER CRJ 900 SRM 51-42-06-001-001-A01SDR DALA2021051202683Skin · dentedSHIP 3140 - DENT EXTERNAL SKIN LOCATED FR 21 AND 6 INCHES BTW STR 22L TO STR 23L LOWER FUSELAGE. CORRECTIVE ACTION: FOUND WITHIN LIMITS AS PER A319 SRM 53-00. (1803109)SDR DALA2021051202682Skin · dentedSHIP 3140 - DENT EXTERNAL SKIN LOCATED ON FR 69 AND 11 INCHES AT STR 23L LOWER FUSELAGE. CORRECTIVE ACTION: FOUND WITHIN LIMITS AS PER A319 SRM 53-00. (1803105)SDR DALA2021051202681Skin · dentedSHIP 3140 - DENT EXTERNAL SKIN LOCATED FR 25 AND 18.5 INCHES BTW STR 42L TO STR 43L LOWER FUSELAGE. CORRECTIVE ACTION: FOUND WITHIN LIMITS AS PER A319 SRM 53-00. (1803103)SDR DALA2023071305706Unknown · unknownSHIP 0687 ERA 591491-14 ISSUED FOR TIME LIMITED REPAIR FOR DENTS COMMON TO FUSELAGE SKIN AND STRAP AT STA 460-480, STRINGER 28R. CORRECTIVE ACTION: SUMMARY DENTS COMMON TO FUSELAGE SKIN AND STRAP AT STA. 460-480, STRINGER 28R WERE REPAIRED PER ER/A 591491-14. SDR FDEA202105071149Doubler · damagedELONGATE HOLE FOUND ON THE DOUBLER AT STA993 STGR34LH-35LH DURING PERFORMING EO EG-5310-E0332629 K P5 STEP 11.P . REPAIR CARRIED OUT TO THE ENLONGATED HOLE ON THE DOUBLER AT STA993 STGR34LH- 35LH, AS PER EA: G-5310-T0361432 PART1 STEP3,4, TITLE: FUSELAGE-MSDR FDEA202105071147Skin · damagedDURING PERFORMING EO EG-5310-EO332629K P6 STEP 11.P,FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA 998 STGR 35R NEAR THE EDGE OF MACHINED STEP OF DOUBLER (P/N:143W2314Y406),AND RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE OF COUNTERSUNSDR MASA20210521194Doubler · crackedCRACK AT UPPER WEB OF ADG COMPARTMENT, BELOW OF SETLEMENT AREA OF ADG PUMB|UPPER WEB OF ADG COMPARTMENT WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01SDR FDEA202105071150Skin · gougedDURING PERFORMING EO G-5310-EO332629 K P6 STEP 9A FOUND SOME GOUGES ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN COMMON TO LONGERON FITTING AFTER REMOVAL OF THE LONGERON FITTING. REPAIR CARRIED OUT TO GOUGES ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN CSDR AALA202105189011Skin · dentedAIRCRAFT IN BASE MAINTENANCE: DENT IN FUSELAGE SKIN AT STA 913 AT STR 20R, MEASURING L=2.9 IN, W=3.7 IN, D=0.08 IN. ACCOMPLISHED PERMANENT REINFORCING DOUBLER REPAIR IAW EA# 327430 AND SRM 53-00-0-1-2R.SDR REXA2021050700326Skin · chafedFUSELAGE LOWER SKIN AND RIVETS CHAFFED AT APPROXIMATELY FS985.00 STGR 27. - REPAIRED DAMAGE IAW ENDEAVOR EA CRJ753-11451 REV IR, DATED 4/21/2021SDR SWIA2021073059792Skin · dentedADM#N881AS-6539. 26 BLENDS FOUND ON LOWER FUSELAGE, FS265.00- FS295.00 STGR24R FOR REPAIR REFERENCE REO 601R-53-00-733 FOR MEASUREMENTS OF BLENDS. PERMANENT REPAIR REQUIRED AT C CHECK. (C-CHECK RO 7/27/2021) EVALUATED, HAND DRESSED 26 IDENTIFIED DENTS, SDR SWIA2021072159613Skin · gouged* GOUGES AROUND SCREW HOLE AT 1 O'CLOCK POSITION IN EXTERNAL SKIN CUT-OUT FOR PANEL 132AL (MARKED) (C-CHECK RO 7/18/2021) REPAIRED GOUGE DAMAGE TO ACCESS PANEL DOOR SURROUND DOUBLER BETWEEN FS220.00-FS235.00 AND STR19R-STR20R REF REO 601R-53-11-3695, RSDR AALA202105079017Skin · corrodedAIRCRAFT WAS GROUNDED: LAVATORY VENT EXTERNAL CORROSION FOUND. REPAIRED EXTERNAL SKIN PANEL AT LAVATORY VENT PER EA 327494.SDR SWAA2021061469811Skin · corrodedFUSELAGE SKIN AT FWD CARGO DOOR CUT OUT AFT CORNER STA 485 TO 495 BELOW STRINGER 25 RT HAS LIGHT CORROSION ; FUSELAGE SKIN AT FWD CARGO DOOR CUT OUT AFT CORNER STA 485 TO 495 BELOW STRINGER 25 RT HAS LIGHT CORROSION / CHEMICALLY REMOVED FINISH PER AMM 51-21-31SDR A6WA202105197783Skin · corrodedCORROSION ON UPPER FUSELAGE SKIN AT ADF ANTENNA FS409.00 + 84 TO FS409.00 + 87.5 LH STR 0 + 1 TO RH STR 0 + 2.5. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON UPPER SKIN FS409.00 + 84 TO FS409.00 + 87.5 LH STR 0 + 1 TO RH STR 0 + 2.5. ORIGINAL SDR SCNA20210514033Strap · brokenPANEL 191D ACCESS DOOR GROUND STRAP BROKEN. REMOVED AND REPLACE BROKEN GROUND STRAP ON PANEL 191D ACCESS DOOR IAW SRM 51-40-02-0G-0.SDR SWAA2021051069485Skin · corrodedCORROSION - THERE IS EVIDENCE OF CORROSION AT THE AFT EDGE OF THE WATER SERVICE DOOR CUTOUT. ; CORROSION - THERE IS EVIDENCE OF CORROSION AT THE AFT EDGE OF THE WATER SERVICE DOOR CUTOUT. /SDR DALA2021051002628Skin · corrodedCORROSION ON INTERIOR SKIN STA 1003 STR 26R TO STR 28R. NEC 001-0002:2040-0016/004 00518: REPAIRED PER ER/A 591313-14 REV A. ASSOCIATED ER/A 00-591313 ADDED FOR AC 9502. (LP #1802011)SDR CALA2021050600621Skin · corrodedCORROSION FOUND AT LAV VENT HOLE DOUBLER REPAIR AT FR68-70 & STR 30RH-34RH REF LP 3570424 AND ECRA 5341-01071 USED FOR INITIAL RE PAIR. REMOVED EXISTING REPAIR, INSTALLED NEW DOUBLER RPR IAW NEW ECRA 5330-06822. DIP CREATED IAW ECRA 5330-06822 REQUIREMENTS ACCSDR SWIA2021072259712Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN UNDER TCAS ANTENNA AT APPROX. FS295.00 AND STRG 27. (C-CHECK RO 7/20/2021) REPAIRED CORROSION FOUND ON FUSELAGE SKIN UNDER TCAS ANTENNA AT APPROX. FS295.00 AND STRG 27 REF CRJ-700 SRM 51-42--21-001-001-A01 AND MHIRJ RESDR SWAA2021061778042Bear Strap · crackedR1 DOOR BEAR STRAP BS290 - 296 (S-8R - S-9R) CRACK FOUND ON THE AFT FASTENER 2ND ROW DOWN ; R1 DOOR BEAR STRAP BS290 - 296 (S-8R - S-9R) CRACK FOUND ON THE AFT FASTENER 2ND ROW DOWN. / 21-153-01251-WIP1 IS COMPLETED AND SIGNED OFF; 21-153-01251-WIP1 IS COMPLETSDR SWAA2021060469371Skin · damagedSKIN DAMAGE AT STA 1008 1.5' ABOVE STR 15L ; / N/A MEASUREMENT TABLE DUE TO NO DENT IN AREA; VERIFIED DENT TABLE MEASUREMENTS ARE N/A'D DUE TO DENT BEING PREVIOUSLY REPAIRED; VERIFIED AND AUDITED.SDR ASAA2021050534890Skin · corrodedLEFT AFT FUSELAGE SKIN, VACUUM WASTE VENT EXHAUST OPENING CORRODED. GROUNDED - YES. REMOVE CORROSION BY BLENDING ON THE FUSELAGE SKIN AT STA 917, BETWEEN STR-21L AND STR-22L, ORIGINAL THICKNESS 0.125", REMOVED 0.100", REMAININGTHICKNESS 0.025" FOUND TO BE OUT SDR R61A2021052000437Doubler · corrodedWHILE AC WAS IN FOR HVY CK FOUND FR84 RBL12 CORROSION ON DOUBLER AS MARKED. REPLACED DOUBLER PN 170-92856-001 IAW SRM 51-43-02.SEE AAR NRC#4500901-1000-0102. AC REMAINS IN YQG FOR COMPLETION.SDR IXXA20210516036Skin · damagedAIRCRAFT GROUNDED FOR C-23 CHECK. DAMAGE TO FUSELAGE SKIN SECTION 43 BETWEEN STA 522 AND STA 566, BETWEEN STR 28R TO 34R . ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE SECTION 43 BETWEEN STATION 522 TO STATION 566 BETWEEN STRINGERS 28R TO 34R IAW ENGINEERING ORDSDR IXXA20210516032Skin · scratchedAIRCRAFT GROUNDED FOR C-23 CHECK. IN ACCOMPLISHMENT OF TASK CARD ATI-53-552-01-01 MAINTENANCE IDENTIFIED D-15 DOT 163 AFT CARGO FUSELAGE SKIN SCRATCHED BETWEEN STATION 1356 AND 1363 AND STRINGERS 31L TO 33L. MATERIAL THICKNESS IAW B767-200 SRM 53-60-01 OUT OF SDR A6WA202105147780Skin · dentedFUSELAGE SKIN DENTS BETWEEN FS621-FS640, S 24 + 3L -S 24 + 5L. NOTED AS D3, D4, D5. ***AIRCRAFT REMOVED FROM SERVICE*** HAND FORMED DENT D3) AT FS 621 + 3.5Ï¿½ AND S24 + 5Ï¿½L, 6.500Ï¿½L X 0.900Ï¿½W X 0.002Ï¿½D, D4) FS 625.00 + 1Ï¿½ AND S24 + 5Ï¿½, 2.850ÏSDR A6WA202105147778Skin · dentedFUSELAGE DENTED BETWEEN FS574+11.40Ï¿½ TO FS589+3.5Ï¿½ AND S21L+1.32Ï¿½ TO S21L+3.75Ï¿½ ***AIRCRAFT REMOVED FROM SERVICE*** CUT OUT DAMAGE BETWEEN FS574+11.40Ï¿½ TO FS589+3.5Ï¿½ AND S21L+1.32Ï¿½ TO S21L+3.75Ï¿½ MEASURING 8.2Ï¿½L X 4.1Ï¿½W, HFEC PERFORMED WITSDR A6WA202105127777Skin · dentedFUSELAGE SKIN DENT AT FS 654.50+2.5" S26L+3.4" ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT AT FS 654.50+2.5" S26L+3.4" TO ORIGINAL CONTOUR, HFEC PERFORMED WITH NO INDICATIONS, REF ASAP EA# AWAC-CRJ253-01631 REV IR DATED 5/7/2021.SDR IPXA2021051169301Skin · gougedINSPECTION TYPE:2CEXTERIOR FUSELAGE SKIN AT STA 1781 AND BETWEEN LONGERON 10L - 11L IS GOUGED.REPAIRED GOUGED EXTERIOR FUSELAGE SKIN AT STA 1781 AND BETWEEN LONGERON 10L - 11L IAW SRM 53-00-01, REPAIR 1, CLASS 1, FIGURE 201. (MAJOR)SDR SWAA2021051271525Skin · crackedFUSELAGE CRACK INDICATION AT BS 520 +13 AND S4R; REPAIRED PER EA 211531243SDR SWAA2021051169225Skin · crackedFUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R; ISSUED EA 2115301243WIP1 AS A SUBTASK TO THE FAULT.SDR SWAA2021051168968Skin · crackedFUSELAGE CRACK INDICATION AT BS 500A +11 AND S4RSDR SWAA2021051070442Skin · crackedFUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; / COMPLIED WITH EASDR SWAA2021051070441Skin · crackedFUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R ; /SDR SWAA2021051070440Skin · crackedFUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; / C/W STEP3.DO A HIGH FREQUENCY EDDY CURRENT (HFEC) HOLE PROBE INSPECTION OF ANY ADDITIONAL EXISTING FASTENER HOLES COMMON TO THE REPAIR AREA PER 737 NDT PART 6; 51-00-00 PROCEDURE 16 USING A 0.030' NOTCH STANSDR SWAA2021051069940Skin · crackedFUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; /SDR SWAA2021051069667Skin · crackedFUSELAGE CRACK INDICATION AT BS 500A +11 AND S-4R ; /SDR SWAA2021051069666Skin · crackedFUSELAGE CRACK INDICATION AT BS 520 +13 AND S-4R ; /SDR CALA2021050600616Skin · corrodedCORROSION FOUND AT LAV VENT HOLE DOUBLER REPAIR AT FR68-70 & STR 30RH-34RH REF LP 3570424 AND ECRA 5341-01071 USED FOR INITIAL RE PAIR. REMOVED EXISTING REPAIR, INSTALLED NEW DOUBLER RPR IAW NEW ECRA 5330-06822. DIP CREATED IAW ECRA 5330-06822 REQUIREMENTS ACCSDR SWIA2021072159611Skin · corroded* UNDER AFT CARGO PLATE, MULTABLE AREA'S OF CORROSION ON ACFT SKIN. FLAGGED (C-CHECK RO 7/18/2021) BLENDED CORROSION FROM AFT CARGO PLATE, MULTIPLE AREAS OF CORROSION ON AFCT SKIN. REF REO 601R-53-61-7683, REV--, DATED 2021-06-28. FOUND TO BE WITHIN LISDR AALA202105189013Skin · damagedAIRCRAFT IN BASE MAINTENANCE: DAMAGE TO FUSELAGE SKIN AT STA 727I-7 AND STR 24L, MEASURING L=6.625 IN, W=3.5 IN, D=0.08 IN. ACCOMPLISHED PERMANENT REINFORCING EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01-2R AND EA 327338.SDR AALA202105079015Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON RIGHT HAND AFT FUSELAGE SKIN PANEL AT LAVATORY EXHAUST OUTLET BETWEEN FR69 AND FR70, S31R AND S32R. ACCOMPLISHED REPAIR PER SRM 53-41-11-300-004 AND EA 327494.SDR JJBA20210510009Skin · crackedLH FUSE, RF2, CRACKS SUSPECTED AROUND RIVETS AT FR 77-78-79-80 BTW STR 3L-9L. LH FUSE RF2 BTW FR 77-80 AND BTW STR 3L-9L CRACKS REMOVED. LH FUSE RF 2 CRACKS AROUND RIVETS AT FR 77-80 BTW STR 3L-9L REPAIRED. AT FR 79, BTW STR 5L-6L, 2 CONSECUTIVE CRACKED HOLES SDR AALA202105206743Skin · wornAIRCRAFT IN BASE MAINTENANCE: WEAR FOUND ON SKIN PANEL LOCATED AT STA FR26 + 18 INCHES, BETWEEN STR 41L TO STR 42L. L= 0.125 INCHES, W= 0.120 INCHES, D= 0.006 INCHES. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN AT FR 26 + 18 BETWEEN STR 41L TO 42L ON LOWER FUSSDR SWAA2021052474723Skin · dentedHAS A DENT ON FUSELAGE SKIN LOCATED AT BST 827 AND 1 INCH ABOVE STRINGER 24 LH. THE DENT MEASURES ARE W:0.971; L:1.086; Y:0.024 AND W/Y 40 / REPAIRED FUSELAGE SKIN BETWEEN BST 807 TO BS 847 AND BETWEEN STRINGER 23L TO STRINGER 25L IAW SW EA # 21-153-01289 REV SDR CALA2021050300595Skin · chafedB767-53-3-7093 FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BL, 322AL , 323AL, 324AL, IS CHAFFED FROM THE PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. REF AMES NR 0446 AND UAL JOB CARD 63-5330-1-2602 ADD EMP:V92955SDR CALA2021050300594Skin · chafedREF AMES NR 0448 AND UAL JOB CARD 63-5330-1-2602. B767-53-3-7093 AFT FUSELAGE SKIN ON SEC 48 BELOW PANELS 321BR, 322AR, 323AR, 3 24AR IS CHAGGED FROM PANEL BLADE SEAL REPAIRED BLENDED AREA IAW EC/RA 5381-01012. SEE BACK OF R25U FOR PARTIAL WORK. ADD EMP:V92955
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