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.

SDR P5CA2021033000076Skin · damagedDURING A-CHECK FUSELAGE SKIN DAMAGE, SIZE 10"L X 5.1"W, AND STRINGER DAMAGED SIZE 1.5" L X 0.3" W. REFER TO RAM FORM N453PA-21-01 AND N453PA-21-02. ACCOMPLISHED A PERMANENT REPAIR TO / THE DAMAGED SKIN (PN: 65B23900-1) BETWEEN STA 2577 TO BSTA 2598 AND STRIMar 31, 2021 · N452PA · Boeing 74746NFSDR DALA2021033101918Skin · gougedSHIP 3302 GOUGE EXTERNAL SKIN BETWEEN FR 54 AND FR 56 S-39L AND S-50L AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN BETWEEN FR 54 AND FR 56 AND STRG 39L AND STRG 50L AS PER ER/A #590395-14. (1769173)Mar 31, 2021 · N802NW · Airbus A330323SDR SWAA2021042660006Skin · crackedCRACK INDICATION FOUND AT FASTENER AT R-1 DOOR CUTOUT BETWEEN STA 291.5 AND STA 294.5 BETWEEN STR 8R AND STR 9R. SEE FIG 4 AT FASTENER SHOWING TYPICAL CRACK. / ACCOMPLISHED INTERIM REPAIR PER RES-W1 2017205-2 REV P.1; P.2; IR AND EA 21-153-00875 IR AT R-1 DOORMar 30, 2021 · N734SA · Boeing 7377H4SDR CALA2021040100405Skin · crackedFUS AT TAIL CONE UPPER SURFACE FRAME 80 FOUND SKIN CRACK REF NON -ROUTINE NR.: 9429743, ORIGINATED BY EMP, SPEC NR: A3NB- 53-3-6145. PERFORMED BY EMP. THE FUS AT TAIL CONE UPPER SKIN (FR80 AREA) REPAIRED AS PER SRM 53-51-11-300-010 REV 135. RII BY TA768.Mar 30, 2021 · N872UA · Airbus A319132SDR DALA2021033101919Skin · gougedSHIP 3302 GOUGE EXTERNAL SKIN BETWEEN FR 54 AND FR 56 S-33R AND S-50R AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN BTW FR 54 AND FR 56 STR 33R AND STR 50R AS PER ER/A NR 590395-14. (1768720)Mar 30, 2021 · N802NW · Airbus A330323SDR A6WA202104067736Skin · damagedL/H ACCESS PANEL 131AL HAS A LOOSE FREEZE PLUG AT FS226.75 AND STR 19L-1.05. ***AIRCRAFT REMOVED FROM SERVICE*** REPAIRED FUSELAGE SKIN AT STATION 226.75 AND STR19L-1.05 REF ASAP EA# AWAC CRJ253-01593 REV IR DATED 3/31/2021.Mar 29, 2021 · N435AW · Cndair CL6002B19SDR IPXA2021032967416Skin · crackedINSPECTION TYPE:N/AFUSELAGE CRACKED NEAR #3 PACK DOOR AT UPPER AFT CORNERREPAIRED IAW UPS EO MD11-5330-79787-AMar 29, 2021 · N259UP · Doug MD11FSDR SWIA202159002Skin · gougedADM# N800SK-6856(CRJ900) EVALUATE GOUGE BETWEEN FS 897 AND FS 887 AT STGR 17R. IF DAMAGE IS REWORKED, OR WITHIN ACCEPABLE LIMITS, ELIMINATE EVIDENCE USING STANDARD AIRCRAFT PRACTICES. (C-CHECK RO 6/22/2021) PERFORMED PERMANENT REPAIR TO DENT DAMAGE AS PMar 28, 2021 · N800SK · Cndair CL6002D24SDR ABXA2021327051Skin · crackedDURING AIRCRAFT CURRENT C-CHECK AT AIRBORNE (TPA), MAINTENANCE DISCOVERED A CRACK IN FUSELAGE SKIN (P/N 143T3262-4) AT STA 782 BETWEEN STRINGERS 37R AND 38R. THE CRACK WAS REMOVED BY TRIMMING OUT (2.3” X 2.75”), SEE (FIGURE 1, SHEET 2). THE SKIN IS FABRICATED Mar 27, 2021 · N220CY · Boeing 767383SDR SWIA202157765Skin · dentedFOUND DENT ON LH EXTERNAL SKIN AT FS501.00 BETWEEN STGR 19L AND STGR 20L. (C-CHECK RO 4/22/2021) COMPLIED WITH DENT REPAIR AT LH EXTERNAL SKIN FS501.00 BETWEEN STGR 19L AND STGR 20L REF-CRJ-700 REO 670-53-31-629 REV -- DATED 2021-04-08 & REO 670-51-00-0Mar 27, 2021 · N713EV · Cndair CL6002C10SDR SWIA202157461Skin · dentedTRANSFER FROM EAML 604995 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 604978, FOUND DENT AT 8.5" AFT OF FUSE STA 589, 2"ABOVE STR 25 MEASURING .066 DEEP. (FLIGHT 5300 - FILED CLOSED) COMPLIED WITHREO 601R-53-61-7619 REV:-- DATED 2021-04-05Mar 27, 2021 · N494CA · Cndair CL6002B19SDR CALA2021033000384Skin · corrodedBULK CGO COMPT AT STA 1540 BILGE AREA S-39L DRAIN HOLE AREA FOUND CORROSION REFER NR LP 9131172 BULK CGO COMPT STA 1540 BTW S39L TO S39R WATER DRAIN VALVE AREA SKIN INTERIM REPAIRED AS PER ECRA 5361-01082 REV - ADD EMP:V897545 RII BY HX 102369Mar 27, 2021 · N651UA · Boeing 767322SDR LR7A2021032702809Skin · dentedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND THE FUSELAGE LH SKIN DENTED AT FS321.0E, WL201, LBL85. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000430699.Mar 27, 2021 · N410LC · Lkheed 382GSDR LR7A2021032702805Skin · dentedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND THE BELLY SKIN DENTED & GOUGED AT FS251, RBL31, WL126. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000430233.Mar 27, 2021 · N410LC · Lkheed 382GSDR LR7A2021032702804Skin · gougedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5301, FOUND THE BELLY SKIN GOUGED AT FS397, RBL17.5, WL126. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-12. NR# 1000430231.Mar 27, 2021 · N410LC · Lkheed 382GSDR SWAA2021033059483Skin · delaminatedPANEL 192K DELAMINATED UNDER LWR ANTI-COLLISION LIGHT / REMOVED AND REPLACED PANEL 192K WITH A NEW ONE PER AMM 53-51-21.Mar 26, 2021 · N8712L · Boeing 7378SDR SWIA2021072859754Skin · dentedFOUND 4 DENTS UNDER FWD FUSELAGE BETWEEN STGRS 26L-25R, AND FUSELAGE STATIONS FS250.0-FS280.0 REFERANCE CP 18607833 AND REO (SPECIFIC) 601R-53-11-3418 REV -- FOR ALL DAMAGE COVERED 600 FLIGHT HOUR VISUAL REINSPECT PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEMar 25, 2021 · N909EV · Cndair CL6002B19SDR SWIA202158213Skin · dented* DENT ON FUSELAGE BETWEEN FS295 AND FS310 BETWEEN STR25R AND STR26R (C-CHECK RO 5/16/2021) EVALUATED DENT DIMENSION AND FOUND TO BE OUT OF LIMITS. DENT IS LESS THEN 1 INCH FROM FASTENER REF CRJ200 SRM 53-00-31. SUBMITTED TO ENGINEERING AND RECEIVED MHIMar 25, 2021 · N925EV · Cndair CL6002B19SDR SWAA2021050358872Doubler · crackedPOWER RECEPTACLE INNER DOUBLER CRACKED @ LOWER FWD CORNER. / ACCOMPLISHED RT POWER RECEPTACLE INNER DOUBLER REMOVED AND INSTALLED NEW DOUBLER REF B737-7 SRM 51-40-02-0G-0 AND DWG #141A0640Mar 25, 2021 · N435WN · Boeing 7377H4SDR IPXA2021041468223Skin · corrodedINSPECTION TYPE: C2, CENTER WING BOX UPPER SKIN IS CORRODED BETWEEN STA.XCW= -101 AND XCW=-110 STRINGER 9.REPAIRED CORRODED UPPER SKIN IAW EA 011-5730-01-A9008 REV I/R AND EO MD11-5730-79967-A (MINOR).Mar 25, 2021 · N289UP · Doug MD11FSDR IPXA2021041468222Skin · corrodedINSPECTION TYPE: C2 CENTER WING BOX UPPER SKIN IS CORRODED BETWEEN STA. XCW=103 AND XCW=100.REPAIRED CORRODED UPPER SKIN IAW EA 011-5730-01-A9017 REV I/R AND EO MD11-5730-79964-A (MINOR).Mar 25, 2021 · N289UP · Doug MD11FSDR 21GA20210401002Skin · corrodedCENTER WING - UPPER PLATTING BETWEEN LBL 7-LBL 9.5 AROUND REAR SPAR, CORROSION DAMAGE REPAIR.Mar 25, 2021 · N881YV · Boeing 767241SDR DALA2021033001899Fastener · missingSHIP 3302 TWO FASTENERS SHOWN IN WC FIGURES WERE FOUND MISSING. CORRECTIVE ACTION: DRILLED HOLES IN FUSELAGE POSITION B12 LH SIDE AND K12 RH SIDE LOC. CIRCUMFERENTIAL JOINT BTW FR53.6 TO FR53.7 AND STGR-26 TO STGR-30 AS PER VARIATION AUTHORIZATION VA 99000. (1Mar 25, 2021 · N802NW · Airbus A330323SDR DALA2021032501777Skin · damagedSHIP 3253 ELONGATED HOLES EXTERNAL SKIN (24EA) LOCATED ON BELLY FAIRING PANEL FR34 BTW STR43LH AND 43RH ON LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 590140-14AD REV. ORIGINAL AND PRI 590140-14 REV .0,1,2. (1764022)Mar 25, 2021 · N353NW · Airbus A320212SDR EE4Y2021032512490Skin · dentedFORWARD LOWER FUSELAGE AT FR13, 40MM BELOW STR 20RH SKIN WITH DENT. NOTE: THE DENT WAS REPAIRED AS PER EMB ETD2021-190-007526 REV A REFERENCE JOB: A1J224 SPECIAL ITEM: 997-2.Mar 25, 2021 · N124NH · Emb ERJ190100IGWSDR SWIA2021071459536Skin · dentedUPON INSTALL OF DRAIN VALVE BETWEEN F.S. 280 - F.S. 295 STRINGER 27 - 26R FOUND EXTERIOR SKIN DERNTED APPROX. 0.260"D X 3.800"L X 1.900" W (C-CHECK RO 7/10/2021) REPAIRED DENT BETWEEN FS 280 AND FS 295, STRINGER 27-26R IAW REO 670-53-21-1993 REV-- DATMar 24, 2021 · N613SK · Cndair CL6002C10SDR IPXA2021041068023Skin · corrodedINSPECTION TYPE:2CCENTER WING TANK UPPER SKIN HAS CORROSION BETWEEN L/H XCW 100 - XCW 118 AT STRINGER 2.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN L/H XCW 101 - XCW 110 IAW VT-SAA EA 011-5730-01-A9013 REV. IR AND UPS EO MD11-5730-79968-A. (MINOR)Mar 24, 2021 · N294UP · Doug MD11FSDR IPXA2021040967985Skin · corrodedINSPECTION TYPE:C2CENTER WING BOX/TANK UPPER SKIN HAS CORROSION BETWEEN XCW=-101.8 AND XCW=-110 ABOVE AFT SPAR.REPAIRED CORRODED SKIN IAW VT-SAA EA 011-5730-01-A8997 REV I/R AND UPS EO MD11-5730-79907-A (MINOR).Mar 24, 2021 · N294UP · Doug MD11FSDR MK1Y20210324010Skin · dentedDURING MAINTANENCE INSPECTIONS AT IAI, FOUNDED LARGE DENT WITH GOUGE ON EXTERNAL FUSELAGE SKIN AT STA 1197+101 AND 2" BELOW STRINGER 9L.DAMAGED AREA CUT OUT 5.5"X3". THE CUT OUT IS 10" FROM LAP JOINT SKIN THICKNESS AT CUT OUT IS 0.056".Mar 24, 2021 · N393AN · Boeing 767323SDR DALA2021032501787Skin · damagedSHIP 6707 DURING THE OPEN HOLE EDDY CURRENT OF THE DELEATION MODIFICATION FOR THE ET-PAC IDTV ANTENNA 2 HOLES FOUND WITH DEFECTES. CORRECTIVE ACTION: REPAIRED 2EA HOLES ON FUSELAGE CROWN IAW ERA 590697-14 REV.ORIGINAL. (1763602)Mar 24, 2021 · N6707A · Boeing 757232SDR MK1Y20210324007Skin · corrodedSATCOM – FUSELAGE SKIN, SEC 45, STA 977 TO STA 1043, STR 2L TO 2R: AS PER CUSTOMER REQUEST, SATCOM ANTENNA WAS DEACTIVATED AND DISMANTLED FROM A/C. EXISTIN COAX CABLE CUTOUT AND TWO BLEND OUT AREA SHOULD BE REPAIRED. SRM DOESN'T ALLOW SKIN REPAIR DOUBLER TO EMar 24, 2021 · N29430 · Boeing 767323SDR MK1Y20210324005Skin · corrodedDURING MAINTENANCE INSPECTIONS AT IAI, THE CORROSION DAMAGE WAS FOUND ON THE UPPER AFT SKIN (111T3017-1) OF CENTER WING WHEN EXCEEDS UNDER THE TENSION FITTING (100T1432-3). THE CORROSION ON THE UPPER SURFACE OF THE SKIN WAS BLENDED OUT PER SRM 51-10-02. THE MAMar 24, 2021 · N29430 · Boeing 767323SDR MK1Y20210324004Skin · damagedDURING CONVERSION PROCESS, THE GLOBAL COMMUNICATION SUITE (G.C.S) ANTENNA WAS REQUESTED TO BE DEACTIVATED AND REMOVED FROM THE AIRCRAFT PER CUSTOMER REQUEST – PRODUCTION ORDER #13. THE SKIN UNDERNEATH ANTENNA REQUIRES REPAIR DUE TO COAX PIERCE POINTS.Mar 24, 2021 · N29430 · Boeing 767323SDR MK1Y20210324003Skin · damagedPROBLEM DESCRIPTION: REPAIR – FUSELAGE SKIN STA 474.5, STA 476, STA 615.5, STA 1346 AND STA 1373, STR 26R/36R (SECTION 43 & 46), SKIN PANEL P/N 143T3521-5, P/N 146T3531-3. DURING MAINTENANCE INSPECTIONS AT IAI, EXISTING BLEND OUTS WERE FOUND ON THE R/H SIDE Mar 24, 2021 · N29430 · Boeing 767323SDR MK1Y20210324002Skin · damagedMAINTEANCE REPORTED BLENDEOUT ON EXTERNAL FUSELAGE SKIN AT STA 1417-1429 STR 32L-34L. THE BLENDOUT EXTENDS INTO FASTENERS AREAS. SRM 53-00-01 FIG 101 ALLOWABLE DAMAGE 1 DOESN'T PROVIDE DAMAGE LIMITS IN CLOSE PROXIMITY TO FASTENERS.Mar 24, 2021 · N29430 · Boeing 767323SDR MK1Y20210324001Skin · damaged: MAINTEANCE REPORTED BLENDEOUT ON EXTERNAL FUSELAGE SKIN AT STA 1417 STR 29L-32L. THE BLENDOUT EXTENDS INTO FASTENERS AREAS. SRM 53-00-01 FIG 101 ALLOWABLE DAMAGE 1 DOESN'T PROVIDE DAMAGE LIMITS IN CLOSE PROXIMITY TO FASTENERS.Mar 24, 2021 · N29430 · Boeing 767323SDR SWIA202158385Skin · chafed* REPAIR AT APPROX. FS969 €“ FS985 STGR26L €“ STGR26R IS CHAFED (C-CHECK RO 5/22/2021) FABRICATED AND INSTALLED REPAIR PARTS -17, -18, -19, -20, -21, -22, -23, & -24 IAW REO# 670-53-00-290 REV-F DATE 2019/04/26 INSTALLED AND RESTORED FINISH IAW REO# Mar 23, 2021 · N720EV · Cndair CL6002C10SDR SWAA2021042760250Skin · delaminatedPANEL 193D HAS A DELAMINATION ON OUTER SKIN CENTER OF PANEL. REPAIRED DELAMINATION 2 EA ON PANEL 193D OUTER SKIN CENTER OF PANEL PER SRM 5170052R2 AND SRM 5170052R11.Mar 23, 2021 · N934WN · Boeing 7377H4SDR DALA2021032401767Skin · dentedSHIP 3311 DENT NEAR AFT LAV SVC PANEL BETWEEN FR72 AND FR73 AND STRINGER 47L ON EXTERNAL SKIN AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED FR 72 TO 73 AND BTW STR 47L TO 48L ON LOWER REAR FUSELAGE AS PER A330 SRM 53Mar 23, 2021 · N811NW · Airbus A330323SDR SWIA2021070759280Skin · dentedDENT FOUND AT FS 501 BETWEEN STRINGERS 16 AND 17 (MARKED) (C-CHECK RO 7/5/2021) REPAIRED DENT FOUND AT FS501.00 BETWEEN STGR 16 AND 17. REF CRJ-700 SRM 53-00-01-201-001-A01. RESTORED FINISH. PRESSURE CHECK GOOD. COMPLIED WITH 51-900-1002-SKY.Mar 22, 2021 · N612QX · Cndair CL6002C10SDR SWIA202159201Doubler · corrodedFWD CARGO COMPARTMENT DOUBLER PLATE AT F.S. 533.00 STGR 26L TO STGR 25L IS CORRODED. (C-CHECK RO 6/29/2021) REPLACED DOUBLER PLATE IN FWD CARGO COMPARTMENT AT F.S. 533.00 STGR 26L TO STGR 25L IAW MHIRJ REO 670-53-31-656 REV -- DATED 2021-05-17 REFERENCEMar 22, 2021 · N656CA · Cndair CL6002C10SDR SWIA202158236Doubler · chafed*AFT FUSELAGE EXTERNAL SKIN DOUBLER AT AT APPROXIMATELY FS969.0 AT STGR27 IS CHAFED (C-CHECK RO 5/20/2021) .REPLACED AFT FUSELAGE EXTERNAL SKIN DOUBLER AT APPROXIMATELY FS969.0 AT STGR27 IAW REO 670-53-00-290 REV-D DATED 2015-09-10 AND IAW CRJ-700 SRM 5Mar 22, 2021 · N658CA · Cndair CL6002C10SDR SWAA2021050357880Skin · crackedCRACK EXTERNAL GROUND ELECTRICAL POWER INTERNAL AREA FORWARD CORNER CUT OUT AT LOWER FUSELAGE / REPAIRED FUSELAGE EXTERNAL GROUND ELECTRICAL POWER SKIN FORWARD CUT OUT AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-5 REPAIR 5 THIS REPAIR IS CONSIDERED CATEGORYMar 22, 2021 · N408WN · Boeing 7377H4SDR SWAA2021042759651Skin · corrodedCORROSION FUSELAGE SKIN AROUND BELLY DRAIN VALVE OPENINGS BS 500A+2; WL 148 BL0 / REMOVED CORROSION FROM EXTERNAL SKIN AT BS 500A+2 BL0 CAVITY DRAIN PER SRM 51-10-02-0G-0 STEP 15.A.(3) BLEND MEASURES 1.9'L X 1.7'W X 0.003'D. ORIGINAL MATERIAL THICKNESS IS 0.08Mar 22, 2021 · N934WN · Boeing 7377H4SDR SWIA202157362Skin · corrodedEXTERNAL FUSELAGE SKIN HAS CORROSION JUST AFT OF FS985 BETWEEN STGR 26L-26R (C-CHECK RO 4/3/2021) BLENDED CORROSION ON EXTERNAL FUSELAGE SKIN AFT OF FS985 BETWEEN STGR 26L-26R REF CRJ700 SRM 51-21-06-001-001-A01. BLEND-OUT IS STRUCTURALLY ACCEPTABLE PER MMar 22, 2021 · N765SK · Cndair CL6002C10SDR SWAA2021042358189Skin · corrodedCORROSION ON EXTERNAL CROWN SKIN BS 1027-1035 STR 2 L/H - STR 2 R/H LBL14-RBL-14 WL308.5 / REPAIRED EXTERNAL CROWN SKIN BS 1027-1035 STR 2 L/H- STR 2 RH LBL14-RBL14 WL 308.5 IAW EA 21-153-01059 REV IR DATED 04/14/2021 & ATS ER 21-01566 REV IR DATED 04/15/2021Mar 21, 2021 · N551WN · Boeing 73776QSDR SWAA2021032558341Skin · crackedREF LP 0990749 WHILE PERFORMING EA 1-A53-36784 AND MT 5331-I-11783-NG PART 6; 53-30-25 FOUND CRACK INDICATION AT BS 639 + 9' S4R AT CHEM MILLED EDGE. CRACK WAS LOCATED WITH PART 6; 53-30-18 AND VERIFIED WITH PART 4; 53-30-07. / ACCOMPLISHED ALL EA 1-A53-10228 Mar 21, 2021 · N717SA · Boeing 7377H4SDR SWIA202158545Doubler · corrodedT-CAS DOUBLER CORRODED AT STR 27 BETWEEN FS 295.00-310.00 (C-CHECK RO 5/25/2021) REMOVED CORROSION AND FOUND T-CAS DOUBLER AT STGR27, FS295 - FS310 TO BE OUT OF LIMITS. REPLACED DOUBLER REF CRJ-900 SRM 51-42-06-001-001-A01, CRJ-900 SRM 51-42-21-001-001-Mar 20, 2021 · N548CA · Cndair CL6002D24SDR ASAA2021032034416Skin · corrodedLAP AT STR-23L HAS MULTIPLE AREAS OF CORRONSION BETWEEN STA 727F AND STA 887 GROUNDED - YES. EVALUATED STE 23L STA 727F TO 887 AND REMOVED CORROSION AND REPAIRED IAW ALASKA AIRLINES EA NO 800-53EA-23333. THIS IS A CAT B REPAIR. THIS REPAIR IS APPROVED FIRST SMar 20, 2021 · N588AS · Boeing 737890SDR SIMA20210320003Skin · crackedCOCKPIT UPPER SKIN CRACKED 2 CRACKS 1.5" IN LENGTH-C/A-INSTALLED DOUBLER/ TRIPLER PER ERS-EM-53MR-4302RMar 20, 2021 · N615AE · Emb EMB145LR
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