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 SCNA20201117316Panel · damagedPANEL 192AL HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 53-40-70-2R-1, 51-70-05-2R-8.SDR SCNA20201117315Panel · damagedPANEL 192AR HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 53-40-70-2R-1, 51-70-05-2R-8.SDR A6WA202011067401Skin · corrodedTCAS ANTENNA SKIN HAS CORROSION AT FS 295+4. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION ON FUSELAGE SKIN UNDER TCAS ANTENNA IN 4 EA LOCATIONS (P1) FS 295 +4 STR 0+1.165 (P2) FS 295+4 STR 0-1.765 (P3) FS 295+10.394 AND STR 0+1.394 438?L X .08?W (P4) FS SDR FDEA202011022761Skin · corrodedCORROSION DISCOVERED ON LEFT SIDE FUSELAGE SKIN UNDER LONGERON 46L AT STA BS 1957 TO BS 1961.SDR DALA2020110303562Skin · damagedDURING INSPECTION UNABLE TO EDDY CURRENT INSPECT HOLES IN STR 2L & STR 2R DUE TO DAMAGE/OUT OF ROUND HOLES. REPAIRED DAMAGE, PER ERA 588435-14AD.SDR SWAA2021081027652Skin · corroded***CORROSION*** FOUND AT STA907+2.2'-907+9.2'; STR-2R; RBL10; WL308.5 AROUND FASTENER HEAD.MARKED / REMOVED DAMAGE AT BS 907+2.2'-907+9.2' STR 2R RBL 10 W/L 308.5 DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1. REPAIRED AREA PER ATS ER 20-03531 REV IR SDR SWAA2021081027651Skin · corroded***CORROSION*** FOUND AT STA888+10; BETWEEN STR 2L AND 2R; WL308.5 AROUND FASTENERS HEAD.MARKED / REMOVED DAMAGE AT BS 888+10' BETWEEN STR 2L AND 2R W/L 308.5. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1. REPAIRED AREA PER ATS ER 20-03531 REV IR ANDSDR HNAA2020121200359Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 77 BETWEEN STRINGERS 6R-7R. REPAIRED FUSELAGE EXTERNAL SKIN AT FRAME77 BETWEEN STRINGERS 6R-7R, IAW EMB 145 SRM53-32-01 AND EO1-53-20-0423.SDR HNAA2020121200358Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 6R-7R. FABRICATED AND INSTALLED SKIN BUSHING REPAIR AT FRAME 79 BETWEEN STRINGERS 6R-7R, IAW EMB 145 SRM 53-32-01-RE AND EO1-53-20-0423.SDR HNAA2020121200357Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 3L-4L. FABRICATED AND INSTALLED BUSHING RE-PAIR AT FRAME 79 BETWEEN STRINGERS 3L-4L, IAW EMB145 SRM 53-32-01-RE AND EO1-53-20-0424.SDR HNAA2020121200356Skin · crackedFUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 78. ONE BETWEEN STRINGERS 4L-5L, AND ONE BETWEEN STRINGERS 6L-7L. FABRICATE AND INSTALLED SKIN BUSHING REPAIR AT FRAME 78 BETWEEN STRINGERS 6L-7L, IAW EMB 145 SRM 53-32-01-RE AND EO1-53-20-0424, NO RELEVANT INDICATISDR FDEA202011012751Skin · damagedNR 3 PACK DOOR CUT OUT UPPER AFT CORNER SKIN LOOKS TO BE CRACKED. PERFORMED HFEC OF SUSPECTED DAMAGED AREA, REF BOEING NTSPM 06-10-.01 PROCEDURE 11. CONFIRMED CRACK DEFECT INDICATION AND MARKED LENGTH. SHGN 02NOV20 06:31 MEM U. DUCT IN PACK 3 BAY REMOVED TSDR SWIA202054987Skin · dentedPROTRUDING DENT ON EXTERNAL FUSELAGE SKIN AT FS 250 STGR 19L. C-CHECK RO 12/30/2020. REPAIRED DENTS ON EXTERNAL FUSELAGE SKIN AT FS 250.00 STGR 19L, IAW REO. REFER TO CONTINUE CARD FOR WORK PERFORMED. MAJOR REPAIR TASK CARD & FORM M337 COMPLETED AND ATTACHSDR SWIA202054756Panel · chafedPANEL 584 BB IS CHAFED AROUND FAIRING CONTACT. C-CHECK RO 12/24/2020. RECEIVED NEW SERVICEABLE PANEL 584BB, REF ATTACHED CONTINUATION FOR WORK PERFORMED. REF CAMP 21674490 FOR INSTALL OF PANEL.SDR 6PMR202012094844Skin · dentedAIRBORNE/PEMCON N/R 10248.0044 DISCREPANCY: EXT FUSELAGE SKIN HAS GOUGES AT STA 1680-1690 AT STR 17L. CORRECTIVE ACTION: BLENDED GOUGES ON EXT FUSELAGE SKIN STA 1680-1690 BELOW STR 17L, IAW B757-200 SRM 51-10-02. CUT GAUGED BLENDED AREAS LOWEST READING OF .1SDR R61A2020111900783Doubler · corrodedWHILE A/C WAS IN FOR HEAVY CHECK FOUND CORROSION FOUND ON PREVIOUS REPAIR DOUBLER BETWEEN FR 13-14 RT SIDE AT MONUMENT MOUNT FLOOR SUPPORT. REPLACED DOUBLER PN 2024-T3.080 BETWEEN FR 13-14 RT SIDE AT MONUMENT MOUNT FLOOR SUPPORT, IAW EMB SRM 53-10-10 REPAIR 0SDR IPXA2020111762496Skin · damagedINSPECTION TYPE: 4C FUSELAGE SKIN FWD LOWER CARGO DOOR CUTOUT AFT JAMB EXISTING REPAIR AT STA 1002 HAS EDGE DAMAGE. REPAIRED DAMAGED FUSELAGE SKIN FWD LOWER CARGO DOOR CUTOUT AFT JAMB EXISTING REPAIR AT STA 1002, IAW VT-SAA EA 011-5330-01-A8704 REV IR AND UPSSDR R61A2020110900737Skin · corrodedWHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK. CORROSION ON FUSELAGE INNER SKIN DOUBLER FOR WASTE AND WATER BOX BETWEEN FR 88-89 S26R. REPAIRED AREA IAW E-175 SRM 53-23-60/REP 01. MAJOR REPAIR. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.SDR DALA2020110603613Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BETWEEN FR 21 TO FR 23 AND BETWEEN STR 43R TO STR 44 LOWER FUSELAGE (1 EA) REFERENCE A. CORRECTIVE ACTION: CONFIRMED DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BETWEEN FR 21SDR DALA2020110303572Skin · dentedDENT EXTERNAL SKIN LOCATED BETWEEN FR 1 TO FR 2 AND 7 IN ABOVE LOWER STRINGER LT SIDE LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BETWEEN FR 1 TO FR 2 AND 7 IN ABOVE LOWER STRINGER LT SIDE LOWER FUSELAGE, AS PER SRM.SDR DALA2025032702297Skin · crackedSHIP 3166 FOLLOW UP INSPECTION REQUIRED FOR ERA 588264-14AD CRACK IN SKIN. COMPLIED WITH INSPECTION PER ERA 588264-14AD. (1644267)SDR DALA2021102906689None · noneAMOC TRACKING LOG. ER/A 588339-14 SECTION I ISSUED FOR A REPAIR OF THE FUSELAGE SKIN AND INTERCOSTAL FWD OF FRAME 10, BL 5.76R. FOLLOW ON ACTION IS REQUIRED. THE REPAIR APPROVAL IS LIMITED TO 16000 TOTAL A/C FLIGHT CYCLES. AN AMOC TO AD 2019-23-15 IS REQUIRED SDR DALA2021102906688None · noneDTE TRACKING LOG. ER/A 588339-14 SECTION I WAS ISSUED FOR A FUSELAGE SKIN AND INTERCOSTAL REPAIR FWD OF FRAME 10 AT BL 5.76R FOLLOW ON ACTION IS REQUIRED. THE REPAIR APPROVAL IS LIMITED TO 12 MONTHS FROM SECTION I ACCOMPLISHMENT. A DAMAGE TOLERANCE EVALUATION SDR SWIA202054349Skin · chafedWHILE PERFORMING REINSPECT FOR RA REPAIRED CENTER WING LOWER PLANK CHAFFED AT LT AFT OUTBOARD CORNER UNDER PANEL 193AB, PER REO, REQUIRES SPECIAL DETAILED INSPECTIONS, NDT INSPECT REWORKED AREA. ADDITIONAL DAMAGE WAS FOUND AND EDDY CURRENT WAS UNABLE TO BE PESDR R61A2020111800774Doubler · corrodedWHILE AC WAS IN FOR HEAVY CHECK FOUND CORROSION ON LOWER FUSELAGE ANTENNA DOUBLER BETWEEN FR 16-17 AND STR 27-28L. AAR MX REPLACED LOWER FUSELAGE ANTENNA DOUBLER (P/N 170-14431-001) BETWEEN FR 16-17 AND STR 27-28L, IAW EMB SRM 51-41-02. FOR DETAILS OF WORK PSDR DALA2020110603609Skin · damagedCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED BETWEEN FR 27 TO FR 28 STR 41R TO STR 42R LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR LOCATED EXTERNAL SKIN LOCATED BETWEEN FR 27 TO FR 28 AND STR 41R TO STR 42R AT LOWER FUSELAGE, ASSDR SWAA2021081226798Filler · crackedFILLER IS CRACKED ON THE AFT EDGE OF THE EXTERNAL POWER DOOR CUTOUT 'MARKED' / REMOVED AND REPLACED -1 FILLER ON EXTERNAL POWER DOOR CUTOUT 7075-T6 .040 LOT # 1425360-1 REFERENCE EA: 1-A53-9269SDR MASA20201215095Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER IN STA FS 295 TO FS 310 BETWEEN STGR 26LT TO 26RT. CORRECTIVE ACTION: INTERNAL PRODUCTION DOUBLER IN STA FS 295 TO 310 BETWEEN STGR 26LT TO 26RT WAS REPLACED, PER CRJ900 SRM 51-42-06-001-001-A01 PAR 6C.SDR SCNA20201117321Panel · damagedPANEL 192E HAS DAMAGED SCREW HOLES. REPAIRED DAMAGED SCREW HOLES, IAW SRM 51-70-04-2R-9 ON PANEL 192F.SDR SCNA20201117314Skin · damagedPANEL 194CL HAS DAMAGED SCREW HOLE. REPAIRED DAMAGED SCREW HOLE ON PANEL 194CL, IAW SRM 51-70-04-2R-9.SDR DALA2020102903524Skin · corrodedTHE SUBJECT AIRCRAFT WAS FOUND WITH BULGED SKIN AND PULLED FASTENERS IN THE AREA JUST AFT OF THE FS 360 CIRCUMFERENTIAL BUTT SPLICE OVER STRINGER S-28R. INSPECTION OF THE CONDITION REVEALED CORROSION OF THE EXTERNAL SKIN PANEL AND THE FORWARD END OF S-28R AFTSDR MASA20201029075Buttstrap · corrodedC-CHECK FABRICATE BUTT STRAP FS 280 BETWEEN STRINGER 20L AND 15R. FABRICATED BUTT STRAP.SDR JGVR20201029001Skin · damagedBLENDED 85 AREAS OF CORROSION ON THE UPPER SURFACE OF THE LOWER FUSELAGE SKIN AND STRINGERS, COMMON TO THE DROPPED AISLE FLOOR. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCEPTABLE. FABRICATED AND INSTALLED SDR MK1Y20201029015Skin · dentedFUSELAGE SKIN, STA 1898, 10 O'CLOCK APPROXIMATELY. DURING MAINTENANCE INSPECTION AT IAI, A DENT WAS FOUND ON THE FUSELAGE SKIN ON THE UPPER TAIL SIDE. THE DENT WAS MEASURED OUT AND IT WAS FOUND THAT THE WIDTH OF THE MINOR AXIS OF THE DENT WAS A=1.23" AND THESDR MK1Y20201029014Skin · damagedFUSELAGE SKIN STA 1266 2.5 BELOW STR-24R. FOUND EXISTING BLEND OUT ON FUSELAGE EXTERNAL SKIN THAT NOT PERMITTED, IAW SRM 53-00-01, FIG 101, ADL1, TABLE I, DETAIL II. PERFORMED NDT INSPECTION FOUND ORIGINAL THICKNESS SKIN 0.209 AND NOMINAL 0.205.SDR MK1Y20201029007Skin · dentedDURING MAINTENANCE INSPECTION AT IAI FOUND DENT ON THE FUSELAGE SKIN ON THE UPPER TAIL SIDE.SDR MK1Y20201029004Skin · damagedFUSELAGE SKIN, STA 1197+132, STR 39L TO STR 39R. DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND. PER NDT REPORT NO U-20-029 THE TOTAL LOSS IN SKIN THICKNESS IS ABOUT 9.8% 9 FROM 0.071 TO 0.064, 0.007 LOSS, WHITHIN SRM LIMITS. HOWEVER,SDR MK1Y20201029003Skin · damagedFUSELAGE SKIN STA 1547 STR-23L. DURING MAINTENANCE INSPECTION AT IAI AN EXISTING BLEND OUT WAS FOUND. PER NDT REPORT NR U-20-030 THE TOTAL LOSS IN SKIN THICKNESS IS ABOUT 11.1% (FROM 0.072” TO 0.064” 0.008 LOSS) WITHIN SRM LIMITS. HOWEVER, THERE ARE SEVERALSDR SWIA202055154Stringer · corrodedMAIN AVIONICS BAY STR 22R CORRODED BETWEEN FS 280.00 AND FS 333.00. C-CHECK RO 1/5/2021. REMOVED AND REPLACED 22R BETWEEN FS 280.00 TO FS 333.00, REF CRJ 700 SRM 53-21-03-101-002-A01, EO SH670-31630 SNIEO S05, CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51SDR SWIA202055153Skin · corrodedMAIN AVIONICS BAY INNER FUSELAGE SKIN AT FS 361.00 BETWEEN STR 25R AND STR 24R CORRODED. C-CHECK RO 1/5/2021. MAIN AVIONICS BAY INNER FUSELAGE SKIN AT FS 361.00 BETWEEN STR 25R AND STR 24R FOUND TO BE WITHIN LIMITS, REF REO 670-53-21-1882 REV- DATED 2020-11-SDR SWIA202055152Skin · corrodedMAIN AVIONICS BAY INNER FUSELAGE SKIN AT FS 361.00 BETWEEN STR 27 AND STR 26R CORRODED. C-CHECK RO 1/5/2021. BLENDED MAIN AVIONICS BAY INNER FUSELAGE SKIN AT FS 361.00 BETWEEN STR 27 AND STR 26R, FOUND TO BE WITHIN LIMITS, REF REO 670-53-21-1882 REV DATED 20SDR SWIA202054616Access Panel · damagedACCESS PANEL 598BB HAS ELONGATED AND OVERSIZE FASTENER HOLE. C-CHECK RO 12/14/2020. REPLACED ACCESS PANEL 598BB AND REPAIRED ELONGATED AND OVERSIZE FASTENER HOLE COMMON WITH WING TRAILING EDGE, REF REO AND DWG. COMPLIED WITH SKYWEST TASKCARD. SEE CONTINUATSDR SWIA202054521Skin · gougedEXTERNAL SKIN AFT OF LOW PRESSURE AIR GROUND CONNECTION ACCESS DOOR HAS IMPACT DAMAGE RESULTING IN MULTIPLE GOUGES AND TWO DENTS FROM APPROXIMATELY FS 589 TO FS 599 AND BETWEEN STRINGERS 21R AND 26R. C-CHECK RO 12/05/2020. REPAIRED EXTERNAL SKIN AFT OF LOW PSDR DALA2020102903528Skin · corrodedWHILE ON LAYOVER IN ATL, DAL A/C 3703 (LN 123) WAS FOUND TO HAVE CORROSION IN THE SKIN PANEL (P/N 143A3232-2) AT STA 362 AND STR 28R. MAINTENANCE REPAIRED DAMAGE, PER ERA 588378-14.SDR SWIA202055139Lintel · crackedLINTEL AT STGR 3LH AT THE FS 280 JOINT IS CRACKED THROUGH THE FIRST THREE FASTENER HOLES COMMON TO THE SKIN. C-CHECK RO 1/5/2021. REPAIRED THE STR 3L LINTEL CRACK, REF SB 670BA-53-040 AND REO 670-53-21-493 REV D DATED 2015-07-10. SEE CONTINUATION CARD FOR SDR SWAA2020120229116Skin · chafedCHAFING EXTERNAL SKIN ON CLOSURE ANGLE LOCATED BETWEEN BS 1088 TO BS 1132 AND STR 2R RT SIDE AT UPPER FUSELAGE. PERFORMED PERMANENT REPAIR LOCATED EXTERNAL SKIN ON CLOSURE ANGLE BETWEEN BS 1088 TO BS 1132 AND STR 2R RT SIDE AT UPPER FUSELAGE, IAW B737-700 SRMSDR SWAA2020111726285Skin · corrodedCORROSION, ON UPPER FUSELAGE SKIN BS 1016-BS 1064 S-3L TO S-3R WL 306. REPAIRED DAMAGE ON UPPER FUSELAGE SKIN BS 1016-BS 1083, STR 3L-STR 3R, WL 306 PER ER NR 20-03521 REV IR AND EA 20-153-02163 REV IR.SDR SWAA2020111730329Skin · dentedFUSELAGE SKIN DENT BS 1006+8' 1' ABOVE 16R (REFERENCE CUSTOMER CARD 9414632). DENT ON FUSELAGE SKIN BS 1006+8'; 1' ABOVE STR 16R. WAS FOUND OUT OF LIMITS BECAUSE OF W/Y WAS LESS THAN 30, PER SRM 53-00-01 ALLOWABLE DAMAGE 1 & TRIMMED OUT. REPAIRED PER EA 20-1SDR SCNA20201116260Skin · gougedGOUGE IN INNER SURFACE OF BELLY SKIN IN AREA AFT OF CARGO COMPARTMENT STA 963 2.5 INCHES INBOARD OF STRINGER 24R. REPAIRED INNER SURFACE OF BELLY SKIN IN AREA AFT OF CARGO COMPARTMENT STA 963, 2.5 INCHES INBOARD OF STRINGER 24R, IAW ATS ER 20-03422 DATED 14OCSDR R61A2020110900741Skin · dentedWHILE A/C WAS OUT OF SERVICE FOR HEAVY CHECK. DENT IN FUSELAGE EXTERNAL SKIN AT FR 11-12 AND STR 16L-17L. DENT WAS FOUND TO BE PERMANENT ALLOWABLE DAMAGE, PER ETD2020-170-031744. A/C REMAINS OUT OF SERVICE FOR HEAVY CHECK COMPLETION.
Back to JASC 5330