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 A6WA202102087623Skin · dentedOUTWARD DENT C/T EXTERIOR SKIN AT FS682.00 +21 STR 23R+4. AIRCRAFT REMOVED FROM SERVICE. REPAIR PERFORMED IAW ASAP EA #AWAC - CRJ253 - 01558 REV IR DATED 01/29/2021. REPAIR PERFORMED IAW W/O 003154 CARD NO 20128.CID 533818.SDR A6WA202102087622Skin · dentedDENTS WITH CREASES FOUND BETWEEN FS682.00 AND FS700.00 STR 23R-24R AIRCRAFT REMOVED FROM SERVICE. REPAIR PERFORMED IAW ASAP EA# AWAC CRJ253-01558 REV IR DATED 01/29/2021. REPAIR PERFORMED ON AERSALE W/O 003154 CARD NO 20128.CID 533818.SDR A6WA202102087624Skin · dentedOUTWARD DENT C/T EXTERIOR SKIN AT FS 682.00+16 & S23R+3" ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED DOUBLER REPAIR ON SKIN AT FS 682 TO FS 700 AND S23R TO S24R. HFEC INSPECTION PERFORMED WITH NO INDICATIONS NOTED. REF. ASAP EA# AWAC-CRJ253-01558. REV IR SDR FDEA202101290232Skin · damagedEXTERIOR FUSELAGE @ STA 518, STRINGER 12R HAS STATIC DISCHARGE REPAIRED EXTERNAL FUSELAGE SKIN WITH EXTERNAL DOUBLER IAW B767 SRM 53-00-01-2R, FIGURE 201, REPAIR 29SDR DALA2021020100603Skin · puncturedLOG 1718008 DUE TO EXTREMELY HIGH WINDS, ENTRY STAND BLEW INTO ACFT CAUSING A PUNCTURE AND A GOUGE BETWEEN BS 5OOB-500D ABOVE STR 20 LT. FABRICATED AND INSTALLED REPAIR PARTS FROM BS 500B-500D BETWEEN STR 18-21 LT IAW DELTA ERA 589642-14 REV ORG.SDR DALA2021013100574Skin · dentedDURING HEAVY MAINTENANCE CHECK MAINTENANCE FOUND 2 EACH DENTS AT FUSELAGE SKIN BETWEEN STA 640-680 BETWEEN STR 21R-23R. REPAIRED PER ERA 589617-14.SDR MK1Y01292021006Skin · damagedDURING MAINTENENCE INSPECTION FOUND DENT DAMAGE ON FUSELAGE SKIN COMMON TO DOCUMENTED EXISTING REPAIR.SDR MK1Y01292021002Skin · corrodedAFTER REMOVAL OF SATCOM ANTENNA FOUND CORROSION ON FUSELAGE SKIN UNDER ANTENNA ADAPTER.SDR SWIA202157588Doubler · corrodedCORROSION FOUND ON EXTERNAL DOUBLER @ FS 985.00 STGR 26R TO 26L (C-CHECK RO 4/20/2021) REMOVED CORRODED DOUBLER AND TRIPLER FROM F.S. 985.00 STR 26R TO STR26L IAW CRJ700 SRM 51-42-21. FABRICATED NEW DOUBLER AND TRIPLER FROM .063 2024-T3 P.O.# 7992 IAW SDR FDEA202101280215Longeron · corrodedFORWARD CARGO COMPARTMENT - STATION 1119 TO STATION 6-10, LONGERON 45 LEFT FOUND WITH CORROSION. CORRODED LONGERON AT FORWARD CARGO COMPARTMENT BETWEEN STATION 1119 TO STATION 6-10, LONGERON 45 LEFT REPAIRED AS PER SRM 53-00-05-2R REPAIR 1 FIGURE 202 BY SDR FDEA202101280212Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE AT STA 1033 STR 37R, APPROX 1.5" IN LENGTH. COMPLIED WITH E.O.#:G-5310-E0332629 I P6 TITLE:FUSELAGE-MAINFRAME-INSPSDR JJBA20210128004Skin · dentedDENT FOUND ON LH CTR FUSE 1, ON FR 20 AND ON STR 14L. DENT ON LH CENTER FUSELAGE-1 ON FRAME 20 BETWEEN STR 13L-15L REPAIREDSDR SWAA2021020145012Doubler · crackedCRACK INDICATION AFT OF FASTENER ON ROW 44 DOUBLER OUTER ROW AT STATION 727D +7 INCH, 3 INCHES BELOW STR 3R. ACCOMPLISHED EA 21-153-00216.SDR SWAA2021020145815Skin · corrodedCORROSION ON FUSELAGE SKIN AT BS 860-1016; LBL 14 TO RBL 14; WL 306.SDR DALA2021012900562Skin · dentedDENT EXTERNAL SKIN BETWEEN FR 30 TO FR 31 AND BETWEEN STR 26L TO STR 27 L AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED TIME LIMIT REPAIR ON DENT LOCATED EXTERNAL SKIN BETWEEN FR 30 TO FR 31 AND BETWEEN STR 26L TO STR 27L, AS PER ERA.SDR DALA2021012900565Skin · damagedWHILE IN MCI, A SKIN REPAIR WAS INSTALLED AT STA 500B AND 500C ABOVE STRINGER 20L, PER ERA 00-589642.SDR DALA2021012900551Skin · dentedDENT EXTERNAL SKIN LOCATED FR 65 BETWEEN STR 40R AND STR 41R LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR ON EXTERNAL SKIN, PER ER/A 589496-14 REV ORIGINAL AND PRI 589496-14 REV 0 AND REV 1.SDR A6WA202102087611Bulkhead Web · crackedAFT PRESSURE BULKHEAD CRACKED AT FS. 621.00, WL 100.5 TO WL 102, LBL 18.00 + .375, CRACK 1.75Ï¿½ L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUT-OUT ON DAMAGED AREA OF AFT PRESSURE BULKHEAD AT FS. 621.00, LBL 18.00, CUT-OUT DIMENSIONS: 6.900Ï¿½ L X 1.79SDR A6WA202102087613Bulkhead Web · crackedAFT PRESSURE BULKHEAD CRACKED AT FS. 621.00, WL 106.5 TO WL 107.5, RBL 9.50 + .375, CRACK 1.0Ï¿½ L. ***AIRCRAFT REMOVED FROM SERVICE*** PERFORMED CUT-OUT ON DAMAGED AREA OF AFT PRESSURE BULKHEAD AT FS. 621.00, RBL 9.50, CUT-OUT DIMENSIONS: 9.00Ï¿½ L X 1.793ÏSDR V0XD20210127Skin · gougedLOWER FUSELAGE SKIN GOUGED AT FRAME STATION 913.00 AND STRINGER 27. CORRECTIVE ACTION: BLENDED DAMAGED AREA AND FOUND TO BE WITHIN LIMITS, IAW BOMBARDIER REO 670-53-00-290 REV-F DATED: 2019/04/26.SDR SWAA2021030845532Skin · damagedPANEL 194CR OUTER SKIN IS DAMAGED. (MARKED) / PANEL 194CR WITH OUTER SKIN IS DAMAGED WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2021030445504Drain · crackedDRAIN AT BS 1019 BETWEEN S-25R AND S-26R IS CRACKED / REMOVED DRAIN BS 1019 BETWEEN S-25R AND S-26R. PER SRM 51-40-02-0G-0 87713U 01FEB21 1035C 01FEB21 SEALED AND INSTALLED NEW DRAIN BS 1019 BETWEEN S-25R AND S-26R AND APPLIED AERO DYNAMIC SEAL. PER DWG 148A33SDR SWAA2021030445505Drain · crackedDRAIN AT BS 1019 BETWEEN S-26R AND S-27R IS CRACKED / REMOVED DRAIN BS 1019 BETWEEN S-26R AND S-27R. PER SRM 51-40-02-0G-0 87713C 01FEB21 1035C 01FEB21 01FEB21 SEALED AND INSTALLED NEW DRAIN BS 1019 BETWEEN S-26R AND S-27R AND APPLIED AERODYNAMIC SEAL. PER DWGSDR SWAA2021030445506Drain · crackedDRAIN AT BS 1019 BETWEEN S-27R AND S-27L IS CRACKED / REMOVED DRAIN BS1019 BETWEEN S-27R AND S-27L. PER SRM 51-40-02-0G-0 87713U 01FEB21 1035C 01FEB21 SEALED AND INSTALLED NEW DRAIN BS1019 BETWEEN S-27R AND S-27L AND APPLIED AERODYNAMIC SEAL. PER DWG 148A3320;SDR SWAA2021021644734Skin · corrodedCORROSION***ON LWR SURFACE OF LWR CTR WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541. / ACCOMPLISHED REPAIR OF CORROSION FOUND ON LWR SURFACE OF WING SKIN AROUND 2 FWD BOLTS LBL 56 BS 541 PER INSTRUCTIONS ON AAR RES-WI 2016690-11 REV IR AND SOUTHWEST EA 21-157-002SDR 7C7A2021012600001Skin · dentedDENT IN FUSELAGE SKIN 85330131 BETWEEN F.S. X580.5 AND X600.0, STRS 23S AND 24S. DENT DIMENSIONS ARE 3.0"X1.75"X0.075".SDR SWAA2021020144554Skin · crackedGROUND POWER DOOR CUTOUT LOWER FLAUGE IS CRACKED / REMOVED DAMAGE PER SRM 51-10-02. ACCOMPLISHED HFEC OF TRIMMED EDGE AND NOT OF INTERIOR SURFACE TO ENSURE NO DAMAGE EXISTS. PER NDT-PART 6;51-00-00 PROCEDURE 23. NO DEFECTS NOTED. REPAIED PER SRM 53-10-15-2R-4 SDR JJBA20210126044Skin · damagedLT EXTERNAL FUSE BELOW GPU ACCESS PANEL, TOOL MARK. EXTERNAL FUSELAGE BELOW GPU ACCESS PANEL, TOOL MARK REPAIRED.SDR SWAA2021012744627Skin · dentedREFERENCE DEFECT NR 9282 SEC 43 FUSELAGE SKIN DENT LOCATED AT STA 360+5.5' BETWEEN STR 14R AND 15R. EVALUATED DENT ON FUSELAGE SKIN AT STA 360+5.5' BETWEEN STR 14R AND 15R. FOUND OUT OF LIMITS DUE TO PROXIMITY TO STA 360 BUTT SPLICE & STR 14R LAP SPLICE, IAWSDR V0XD20210126Skin · gougedLOWER FUSELAGE SKIN GOUGED BETWEEN FRAME STATION 913.00 AND 927.00, STRINGERS 27 AND 26L. CORRECTIVE ACTION: BLEND DAMAGED AREA AND FOUND TO BE WITHIN LIMITS, IAW BOMBARDIER REO 670-53-00-290 REV-F DATED: 2019/04/26.SDR SWAA2021051345477Access Door · chafedACCESS DOOR 192DR MATING SURFACE IS CHAFED. / REPLACED DOOR 192DR FOR AN NEW DOOR 192DR P.O. #814054/1 PER SRM 51-40-02-OG-0 AND AIPC 52-48-11-01.SDR SWIA202156454Intercostal · crackedINTERCOSTAL BETWEEN FS621 AND FS625 AT APPROX STR13R, IS CRACKED. (C-CHECK) RO 2/25/2021. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS621 AND FS625 AT STGR 13R P/N 601-35012-52 REF CRJ200 SRM51-42-21.SDR SWAA2021021748067Skin · deterioratedDETERIORATED SERVICE DOOR CUT OUT MOUNT AT FWD GALLEY AREA (2 EA). REPLACED MOUNT LOCATED AT SERVICE DOOR CUT OUT AT FWD GALLEY AREA (2 EA) IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.SDR SWAA2021020847421Skin · crackedFUSELAGE SKIN SUBSURFACE CRACK INDICATION AT BS 691 ABOVE STR 1 USING MFEC INSPECTION; 737 NDT MANUAL; PART 6; 53-30-18. VERIFIED SUBSURFACE INDICATION USING UTPA INSPECTION; 737 NDT MANUAL; PART 4; 53-30-07 AND HFEC PART 6; 51-00-00 PROCEDURE 23. CRACK MEASURSDR F3LA2021012900006Skin Panel · damagedDAMAGE DURING STORGE IN ROW, HEAVY LOCALIZED WIND CAUSED A/C FROM AN OTHER OPERATOR TO MOVE FROM PARKING CHOCK, STRUCK & DAMAGED LT - RT THS AND AFT FUESLAGE OF AC N714FR. REPAIR/CORRECTIVE ACTION--EA A1-53R-35616 (MAJOR REPAIR) PROVIDES PERMANENT REPAIR INSTSDR JR2R20210125Doubler · corrodedDOUBLER AT FR 17 RBL 42 CORRODED.SDR SWAA2021021544800Skin · gougedAFT CARGO DOOR CUT OUT AFT 2 GOUGES STR 21R (MARKED #5) / FUSELAGE SKIN AT AFT CARGO DOOR CUT OUT. BS' 846; 0.5' BELOW STR 23R. REMOVED DAMAGE L=1.5'; W=0.7'; D=0.008'. ORG 0.080'. REMAINING 0.072'. DAMAGE WITHIN LIMITS PER SRM 53-00-01-1A-5 PARAGRAPH 4.B. HFESDR SWAA2021021544798Skin · gougedGOUGE AT LWR FWD CARGO DOOR CUTOUT (MARKED #1 / FUSELAGE SKIN AT FWD CARGO DOOR CUT OUT. BS 440+1; 2' BELOW STR 24R REMOVED DAMAGE L=2.8'; W=0.6'; D=0.006'. ORG 0.080'; REMAINING 0.074'. HFEC AREA NO CRACKS NOTED PER D6-37239 PT 6 51-00-00 PROC 23. DAMAGE WITHSDR DALA2024081508168Skin · damaged-AD- LIGHTNING STRIKE DAMAGE TO THE UPPER FWD CORNER OF THE RH #19 WINDOW (RHS STA 579-598). SECTION I: TIME-LIMITED REPAIR ACCOMPLISHMENT PER ER/A 554700-14 REV ORIG. REQUIRED PRIOR TO DEPARTURE FROM EWR. PERMANENT REPAIR ACCOMPLISHMENT PER THIS ER/A REQUIREDSDR SWIA202156446Doubler · elongatedELONGATED HOLES FOUND ON DOUBLER AT FS621 LBL9 ATTACHED TO LH OUTBOARD END ATTACH ANGLE. (C-CHECK) RO 2/25/2021. INSTALLED NEW DOUBLER AT FS621, LBL9, REF CRJ 200 SRM 51-42-21, & BOMBARDIER REO 601R-53-61-117, REV -E, DATE 2018-01-15 / COMPLIED WITH TASK SDR DALA2021012600492Skin · damagedDURING INSPECTION FOUND TWELVE (12 EA) HOLES OF IDTV ANTENNA RADOME WERE FOUND WITH FOLLOWING DAMAGES: GOUGE (1 EA), CRACKS (6 EA), ELONGATED (2 EA), WEAR (3 EA), IN REF TASK CARD 2330-01337-1001. FUSELAGE SKIN STA 727G TO 727H (WHERE THE IDTV ANTENNA RADOME SDR SWIA202156864Skin · corrodedEXTERIOR SKIN SURFACE HAS MINOR CORROSI0ON IN MULTIPLE SPOTS FROM F.S. 559.00+32 TO F.S. 559.00+48 FROM STRGR 25L TO 25R (C-CHECK) RO 3/10/2021 COMPLIED W. REO 601R-53-51-557 REV-- DATED 2021-02-04. REFERENCE CONTINUATION TO SEE WORK PERFORMEDSDR SWIA202156838Skin · corrodedEXTERIOR SKIN SURFACE HAS MINOR CORROSI0ON IN MULTIPLE SPOTS FROM F.S. 559.00+80 TO F.S. 559.00+112 FROM STRGR 25L TO 25R (C-CHECK) RO 3/10/2021 REPAIRED MINOR CORRODED AREAS OF EXTERIOR SKIN FROM FS559.00+80 TO FS 559.00+112 FROM STRGR 25L TO 25R IAW MSDR SWIA202156081Doubler · corrodedFWD WET AREA- CORROSION L/H DOUBLER FRAMES 19 TO 20 AS MARKED. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED L-H DOUBLER BETWEEN FR 19-20. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.SDR YENA2021012900082Skin · corrodedDURING HMV, LT WING UPPER SKIN TRAILING EDGE BETWEEN RIBS 6 AND 22 CORROSION. TEMPORARY REPAIR & LT WING REAR SPAR WEB BETWEEN RIBS 13 AND 14 TOOL MARKING. PERMANENT REPAIR. THIS IS A MAJOR REPAIR.SDR SWIA202156670Doubler · corrodedMAIN AVIONICS BAY LOWER TCAS ANTENNA DOUBLER BETWEEN FS295.00 AND FS310.00 CORRODED (C-CHECK) RO 3/4/2021 REPLACED MAIN AVIONICS BAY LOWER TCAS ANTENNA DOUBLER BETWEEN FS295.00 TO FS310.00 REF CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 & DSDR V0XD20210302009Skin · corrodedLOWER TCAS ANTENNA BASE CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REMOVED AND REPLACED TCAS ANTENNA BASE IAW CRJ900 SRM 51-42-06. REFER TO AVMAX W/O: 80989 W/C: 1165.SDR JJBA20210121021Doubler · corrodedCARGO AREA UNDER FLOOR CORROSION FOUND RAD ALT ANTENNA. CORROSION LEVEL 2: AT REAR FUSELAGE RADIO ALT ANTENNA, DOUBLER AND LOUVER FOR INVESTIGATION CUT OUT DONE. CARGO AREA UNDER FLOOR RAD ALT ANTENNA REPAIR CARRIED OUT.SDR FDEA202101210166Skin · crackedR2 DOOR CUTOUT FWD FRAME UPPER HINGE CUTOUT IS CRACKED ACCOMPLISHED FEDEX EA F-5210-T0312598-B. DOORS-PASSENGER/CREW R2 DOOR EXISTING REPAIR.SDR DALA2021012200433Skin · scratchedSCRATCH ON EXTERNAL SKIN SEVERAL LOCATED FROM FR 51 TO FR 61 AND BETWEEN STR 42LT TO STR 42RT AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR, PER PRI 581972-14AD REV 0 AND ER/A 581972-14AD.
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